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1412.5634v2.Energy_spectra_of_two_interacting_fermions_with_spin_orbit_coupling_in_a_harmonic_trap.pdf | arXiv:1412.5634v2 [cond-mat.quant-gas] 7 Apr 2015Energy spectra of two interacting fermions with spin-orbit coupling in a harmonic trap
Cory D. Schillaci∗
Department of Physics, University of California, Berkeley , California 94720, USA
Thomas C. Luu†
Institute for Advanced Simulation,
Institut f¨ ur Kernphysik and J¨ ulich Center for Hadron Phys ics,
Forschungszentrum J¨ ulich, D-52425 J¨ ulich, Germany
(Dated: December 17, 2014)
We explore the two-body spectra of spin-1 /2 fermions in isotropic harmonic traps with external
spin-orbit potentials and short range two-body interactio ns. Using a truncated basis of total angular
momentum eigenstates, nonperturbative results are presen ted for experimentally realistic forms of
the spin-orbit coupling: a pure Rashba coupling, Rashba and Dresselhaus couplings in equal parts,
and a Weyl-type coupling. The technique is easily adapted to bosonic systems and other forms of
spin-orbit coupling.
PACS numbers: 71.70.Ej, 67.85.-d, 03.75.Mn, 03.65.Ge
I. INTRODUCTION
Cold atomic gases with spin-orbit coupling (SOC) have recently been a n area of intense interest because of the
potential to simulate interesting physical systems with precisely tu nable interactions [1]. In condensed matter physics,
spin-orbit couplings are essential for many exotic systems such as topological insulators [2, 3], the quantum spin Hall
effect [4], and spintronics [5]. The experimental setup which induces s pin-orbit coupling is intimately related to
simulation of synthetic gauge fields [6–9]. Because these couplings ar e parity violating, they potentially play similar
roles within nuclear systems that undergo parity-violating transitio ns due to the nuclear weak force. Atomic gases
provide an excellent testing ground both to explore universal beha vior of these real life systems and to create new
types of spin-orbit coupling which are not yet known to exist (or hav e no solid-state analog) in other materials but
are interesting in their own right. Further, these experiments can be performed in an environment with few or no
defects and impurities.
Spin-orbit coupling was first realized in a Bose condensate of87Rb [10] and extended shortly after to Fermi gases
of40K [11] and6Li [12]. These spin-orbit interactions are ‘synthetic’ in the sense th at a subset of the hyperfine states
stand in as virtual spin states. A particularlyinteresting conseque nce ofthis is the possibility ofstudying systems with
synthetic spin-1 /2 spin-orbit interactions but bosonic statistics [10, 13]. From anoth er point of view, the couplings
are equivalent to applying external electromagnetic forces via syn thetic gauge couplings on the physically uncharged
particles in the gas [14, 15]. It has alsobeen conjectured that thes e systems could be used to physicallysimulate lattice
gauge theories [16, 17]. Spin-orbit couplings in solid-state systems a rise in two-dimensional (2D) systems (Rashba
and Dresselhaus types, described in Sec. II), but recently an exp erimental setup has been proposed that can simulate
the Weyl-type SOC which is fundamentally three dimensional [18].
Spin-orbit couplings are also of interest from the perspective of fe w-body physics where they arise in a variety of
fields, e.g., theweaknuclearinteractionsgoverningproton-proto nscattering[19,20]. Becausethespin-orbitcouplingis
long range, it can significantly modify both the threshold scattering behavior and the spectrum of two-body systems
[21]. For low-energy scattering, Duan et al.[22] showed analytically that parity-violating SOC leads to the the
spontaneous emergence of handedness in outgoing states, a find ing later confirmed in [23]. Even in the presence of
a repulsive two-body interaction, an arbitrarily weak SOC has been s hown to bind dimers [24]. For three-particle
systems, a new type of universality is conjectured to occur for bo und trimers with negative scattering length [25].
Few-atom systems undergoing SOC within trapping potentials have a lso been explored. For example, the spectrum
of particles within a trap with an external SOC of the Weyl type (but no relative interaction) has been theoretically
determined [26]. The Rashba SOC with two-particle systems interact ing via short-ranged interactions was investi-
gated perturbatively in [27], where it was shown that the leading orde r corrections due to the SOC and short-range
interaction are independent when the scattering length is equal fo r all channels. In one dimension, the spectrum for
∗schillaci@berkeley.edu
†t.luu@fz-juelich.de2
this type of system has been calculated when the SOC consists of eq ual parts Rashba and Dresselhaus interactions
[28]. Information learned from trapped systems augments that fr om scattering experiments while also being relevant
to interesting phenomena in trapped many-body systems with SOC s uch as solitons [29, 30] or novel phase diagrams
[31].
In all these calculations, the emergent spectrum is rich and complex , offering new insights into few-body behavior.
Our objective is to provide some additional insight into two-body phy sics of Fermi gases with spin-orbit interactions
in the presence of both three-dimensional trapping potentials and short-ranged two-body interactions, which are
necessarily present in dilute cold-atom experiments. Our approach is to numerically diagonalize the Hamiltonian
within a suitably truncated basis, and is thus nonperturbative in nat ure. Eigenstates of the interacting Hamiltonian
without SOC are used for the basis. Section II introduces the spec ific forms of spin-orbit coupling and two-body
interactions which we consider. The general method is detailed in Sec . III for the simplest SOC. In the remaining
Secs. IV-V we study the spectra of additional spin-orbit couplings in order of increasing computational complexity.
II. HAMILTONIAN FOR SPIN-ORBIT COUPLINGS WITH CONTACT INTE RACTIONS
In this paper we simply refer to our systems by their ‘spin’ degrees o f freedom and use the standard notation for
spin quantum numbers. We consider three different types of spin-o rbit coupling. The form of spin-orbit coupling
realized in experiments is a linear combination of the Rashba [32] and line ar Dresselhaus [33] types,
VR≡αR(σxky−σykx), (1)
VD≡αD(σxky+σykx), (2)
which were originally recognized in two-dimensional solid-state syste ms. In a 2D system, these form a complete
basis for spin-orbit couplings linear in momentum. Note that some ref erences use the alternate definitions VR∝
(σxkx+σyky) andVD∝(σxkx−σyky) which are equivalent up to a pseudospin rotation. For solids, these parity-
violating interactions are allowed only in the absence of inversion symm etries. Rashba-type SOC typically arises in
the presence of applied electric fields or in 2D subspaces such as the surfaces of materials where the boundary breaks
the symmetry. Dresselhaus couplings were first studied in the cont ext of bulk inversion asymmetry, when the internal
structure leads to gradients in the microscopic electric field.
To date, experiments have produced only SOC potentials in which the Rashba and Dresselhaus terms appear with
equal strength (also known as the “persistent spin-helix symmetr y point” [34]),
VR=D≡αR=Dσxky. (3)
After a pseudospin rotation, this potential can be seen as a unidire ctional coupling of the pseudospin and momentum
along a single axis. A proposal for tuning the ratio αR/αDhas been given in [35]. An experimental setup which gives
the simple three-dimensional Weyl coupling,
VW≡αW/vectork·/vector σ, (4)
has also been proposed in [18] and [36].
In the following sections we calculate the spectra of two particles wit h a short-range two-body interaction, an
isotropic harmonic trapping potential and spin-orbit coupling. The s ingle particle Hamiltonian is
H1=/planckover2pi12k2
2m+1
2mω2r2+VSO. (5)
For the spin-orbit term VSO, we consider equal Rashba and Dresselhaus (3), pure Rashba (1) , and Weyl (4) spin-orbit
couplings because these are generally considered to be experiment ally feasible.
We assume that the range of interaction between particles is small c ompared to the size of the oscillator well. The
relative interaction between the particles can then be approximate d as a regulated s-wave contact interaction, which
in momentum space (as a function of relative momentum) is given by
4π/planckover2pi12
ma(Λ). (6)
Here the argument Λ refers to some cutoff scale and a(Λ) is some function of the cutoff and physical scattering length
aphys. The exact form of this function depends on the type of regulator used and is not relevant for this work; the
only constraint is that a(Λ) reproduce the physical scattering length given by the scatte ringTmatrix at threshold,3
FIG. 1. (Color online) Spectrum of the two-body contact inte raction Hamiltonian as a function of ˜ a. The horizontal lines
indicate the dimensionless energy eigenvalues in the unita ry limit|˜a| → ∞.
T(E= 0) = 4π/planckover2pi12aphys/m[37]. In the limit Λ → ∞the spectrum of two particles in an oscillator well (without
external spin-orbit interaction) was solved by Busch et al.[38] using the method of pseudopotentials. In Ref. [39]
the solution for general Λ was given using a Gaussian regulator, whic h in the limit Λ → ∞recovered the Busch et al.
solution. For our work below we use the eigenstates and eigenvalues of this two-particle system given in Ref. [38].
III. WEYL COUPLING
We tackle the Weyl form first because of its mathematical and nume rical simplicity. In the absence of the two-body
interaction, this problem was treated in Ref. [26]. Our approach is to determine the matrix elements of the SOC in
an appropriate basis. The eigenvalue is then solved numerically at the desired precision by choosing an appropriately
large truncated basis of harmonic oscillator (HO) eigenstates.
As usual, the two-body problem is best approached in the dimensionle ss Jacobi coordinates
R=r1+r2√
2b, r=r1−r2√
2b(7)
andthecorrespondingconjugatemomenta q,Qrepresentingthe relativeandtotalmomenta. Foranisotropichar monic
oscillator, distances can be expressed in terms of the ground-sta te length scale b=/radicalbig
/planckover2pi1/mωand energies will be
similarly measured in units of E0=/planckover2pi1ω. We also define the spin operators
/vector σ≡/vector σ1−/vector σ2,/vectorΣ≡/vector σ1+/vector σ2. (8)
With thesedefinitions, the two-bodyHamiltoniancanbe nondimension alizedandseparatedintorelativeandcenter-
of-mass (c.m.) parts,
1
/planckover2pi1ωH=/parenleftbigg
h0,rel+˜αW√
2/vector q·/vector σ+√
2π˜a(Λ)δ(3)(r)/parenrightbigg
+/parenleftbigg
h0,c.m.+˜αW√
2/vectorQ·/vectorΣ/parenrightbigg
, (9)
whereh0,rel=r2/2 andh0,c.m.=R2/2. Notably, the spin-orbit coupling appears in both terms. The tilde o ver the
coupling constants indicates that they are dimensionless, related t o the original coupling constants by dividing out the
oscillator length (e.g., ˜ α=α/b). Throughout the remainder of this paper we will refer to dimension less eigenvalues
ofH//planckover2pi1ωas the energies of the system.
Eigenstates of two particles with a short-range interaction in a har monic oscillator trapping potential form a
convenient basis for these calculations. These basis functions wer e first derived in [38] for the isotropic case considered
here, and the more general case of an anisotropic trap has been e xplored in [40]. The dependence of the energy
spectrum on the scattering length ais shown in Fig. 1 for reference. Qualitatively, the effect of the shor t-range
interaction is to shift the harmonic oscillator energies by ±/planckover2pi1ωas the scattering length goes to ±∞. For positive
scattering length, there is also an additional negative-energy dime r state.
We choose the particular coupling scheme of angular momentum eigen states,
|n(ls)j;NL;(jL)J∝angb∇acket∇ight, (10)4
which simplify the matrix elements for the relative-coordinate opera tors. Here nandlrefer to the principal and
orbital angular-momentum quantum numbers of the two-particle s ystem in the relative coordinates. NandLrefer
to the analogous numbers in the center-of-mass frame. The tota l spin of the two spin-1 /2 particles is denoted by
s=s1+s2and may be either 0 or 1. First sandlto make angularmomentum j, which is then recoupled with the c.m.
angular momentum Lto make the state’s total angular momentum J. Because all terms in the Hamiltonian (9) are
scalars, the interaction is independent of Jzand so we omit this quantum number for clarity. Due to Pauli exclusion ,
l+smust be even to enforce antisymmetry under exchange of the par ticles.
Forl∝negationslash= 0 the states (10) are identical to the well known harmonic oscillato r, withnandl(NandL) indicating
the relative (center-of-mass) HO quantum numbers. We use the c onvention that n,N= 0,1,2,..., and therefore
E= 2n+l+2N+L+3. The short range interaction (5) modifies the l= 0 states and their spectrum. The principal
relative quantum number nfor these states is obtained by solving the transcendental equat ion
√
2Γ(−n)
Γ(−n−1/2)=1
a(11)
and is no longer integer valued. For the relative-coordinate part of thel= 0 wave function,
φ(r) =1
2π3/2A(n)Γ(−n)U(−n,3/2,r2)e−r2/2, (12)
A(n) =/parenleftbiggΓ(−n)[ψ0(−n)−ψ0(−n−1/2)]
8π2Γ(−n−1/2)/parenrightbigg−1/2
, (13)
whereU(a,b,x) is Kummer’s confluent hypergeometric function and ψ0(x) = Γ′(x)/Γ(x) is the digamma function. A
derivation of the normalization factor A(n) is given in the Appendix.
Standard angular momentum algebra can be used to determine the m atrix elements of the two spin-orbit coupling
terms; we follow the conventions of [41]. For Weyl SOC of two spin-1 /2 fermions, the matrix elements of the coupling
in the relative momentum are
∝angb∇acketleftn′(l′s′)j′;N′L′;(j′L′)J′|/vector q·/vector σ|n(ls)j;NL;(jL)J∝angb∇acket∇ight
=δN,N′δL,L′δj,j′δJ,J′(−1)l+s′+j3√
2/braceleftbigg
j s′l′
1l s/bracerightbigg
(s′−s)∝angb∇acketleftn′l′||q||nl∝angb∇acket∇ight.(14)
To preserve anti-symmetry of the two-particle system, the relat ive momentum term in the Weyl SOC must couple
states with relative angular momentum ltol±1, leavingl+seven but changing the parity.
For basis states with both l,l′∝negationslash= 0, reduced matrix elements of the momentum operator are calcula ted between
pure harmonic oscillator states,
∝angb∇acketleftn′l′||q||nl∝angb∇acket∇ight=(−1)l′(−1)l+l′+1
2/radicalBigg
2(2l+1)(2l′+1)
(l+l′+1)∝angb∇acketleftn′l′0|(−i∇0)|nl0∝angb∇acket∇ight (15)
=i(−1)l/radicalbigg
l+l′+1
2/radicalbig
n!n′!Γ(n+l+3/2)Γ(n′+l′+3/2)
×n,n′/summationdisplay
m,m′=0
(−1)m+m′/bracketleftBig
2mΓ/parenleftBig
m+m′+1+l+l′
2/parenrightBig
−Γ/parenleftBig
m+m′+1+l+l′
2/parenrightBig/bracketrightBig
m!m′!(n−m)!(n′−m′)!Γ(m+l+3/2)Γ(m′+l′+3/2)ifl′=l−1
(−1)m+m′+1/bracketleftBig
(2m+2l+1)Γ/parenleftBig
m+m′+1+l+l′
2/parenrightBig
−Γ/parenleftBig
m+m′+1+l+l′
2/parenrightBig/bracketrightBig
m!m′!(n−m)!(n′−m′)!Γ(m+l+3/2)Γ(m′+l′+3/2)ifl′=l+1
0 otherwise(16)
Ifl= 1 andl′= 0 or vice versa, reduced matrix elements between one modified wav e function of the form (12) and
one pure harmonic oscillator state are needed. These are given by
∝angb∇acketleftnl= 0||q||n′l′= 1∝angb∇acket∇ight=−iA(n)/radicalbigg
Γ(n′+5/2)
2π3n′!2n−2n′−1
2(n′−n)(1+n′−n)(17)
and its Hermitian conjugate.
Our choice of basis makes the relative matrix elements (14) simple at t he cost of complicating the center-of-mass
term. We take the approach of expanding the states (10) in the alt ernate coupling scheme,
|n(ls)j;NL;(jL)J∝angb∇acket∇ight= (−1)l+s+L+J/radicalbig
2j+1/summationdisplay
J√
2J+1/braceleftbigg
l s j
L JJ/bracerightbigg
|nl;N(Ls)J;(lJ)J∝angb∇acket∇ight. (18)5
FIG. 2. (Color online) Absolute value of the matrix elements |/angbracketleftn′(11)0;00;(00)0 |/vector σ·/vector q|n(00)0;00;(00)0 /angbracketright|between the ground
state andl= 1excited states. The horizontal axis is the principal quan tumnumber of the ground state obtained bysolving (11).
From left to right, the vertical lines on the negative axis in dicate the values obtained for ˜ a= 1/4, ˜a= 1, ˜a=±∞, and ˜a=−1,
respectively.
FIG. 3. (Color online) A convergence plot giving the change i n energy eigenvalue, ∆ E, for the lowest eight energy levels when
a shell is added as a function of Emax. The left figure shows convergence for ˜ a=−1 and ˜αW= 0.5. In the right panel we show
˜a= 1 and ˜αW= 0.5, demonstrating that convergence of the states with large n egativenis poor.
Using this notation, the matrix elements can be written
∝angb∇acketleftn′(l′s′)j′;N′L′;(j′L′)J′|/vectorQ·/vectorΣ|n(ls)j;NL;(jL)J∝angb∇acket∇ight=δn,n′δl,l′δJ,J′δs,1δs1,16(−1)L
×∝angb∇acketleftN′L′||/vectorQ||NL∝angb∇acket∇ight/summationdisplay
J(−1)J(2J+1)/braceleftbigg
l1j′
L′JJ/bracerightbigg/braceleftbigg
l1j
L JJ/bracerightbigg/braceleftbigg
J1L′
1L1/bracerightbigg
.(19)
Again, the reduced matrix element of the center-of-mass moment um changes the parity by connecting states with
∆L=±1. Matrix elements are nonzero only for ∆ s= 0 because the antisymmetry of the spatial wave function
depends only on l, which does not change. We also note that the c.m. term does not aff ect states with singlet spin
wave functions ( s= 0).
Using these matrix elements, we calculated the spectrum of the two interacting particles with Weyl spin-orbit
coupling. Our calculations are performed by numerically diagonalizing in a truncated basis of the harmonic oscillator
states (10), where a cutoff 2 N+L+2n+l+3≤Emaxis set high enough that the eigenvalues of the matrix have
converged to the desired accuracy.
This approach converges well only when the ground-state energy is not too low. In particular, for apositive but
very small the principal quantum number of the ground state is incr easing from negative infinity as seen in Fig. 1.6
FIG. 4. (Color online) Spectrum of states with total angular momentum J= 0 for the dimensionless Hamiltonian (9). The
bottom left figure shows the ground-state energy for ˜ a=−1 as a function of ˜ αW; above are the first few excitation energies.
The right figure shows the results in the unitary limit of the t wo-body interaction, |˜a| → ∞. The spectrum is symmetric about
˜αW= 0.
FIG. 5. (Color online) For different values of the two-body co upling strength ˜ a, we show the magnitude of the ground state
projected onto even parity basis states as a function of the S OC strength. This is given by/vextendsingle/vextendsingleP+|ψGS/angbracketright/vextendsingle/vextendsingle2=/vextendsingle/vextendsingle(1−P−)|ψGS/angbracketright/vextendsingle/vextendsingle2,
whereP+(P−) is the projection operator onto the positive- (negative-) parity basis states. The left figure shows negative ˜ a,
while the right shows positive ˜ a. Note that the limits ˜ a→ ±∞are physically identical.
From Fig. 2, we can see that as nbecomes more negative, the principal quantum number of the domin ant matrix
element is also increasing. Because convergenceof any energyleve l requires a cutoff much largerthan the energyof the
most strongly coupled states, a sufficiently high Emaxto ensure an accurate ground-state energy becomes infeasible
for small positive a. For excited states, nis always positive and matrix elements with similar nalways dominate.
The strength of the matrix elements follows a similar qualitative behav ior for the spin-orbit couplings treated in the
following sections where the same issues recur.
As a result, convergence of the ground state is actually slower tha n that for nearby excited states. Furthermore,
our approach gives the fastest convergence when ais not small and positive. We compare the rate of convergence of
the ˜a=−1 and ˜a= 1 spectra in Fig. 3 to demonstrate the dependence of convergen ce on the matrix truncation. The
actual energy spectrum is shown in Fig. 4.
One consequence of parity violation in this system is that the eigenst ates are mixtures of the even- and odd-parity
basis states described by Eq. (10). In Fig. 5 we visualize how these s ubspaces are mixed in the ground state as the7
SOC strength increases. For the noninteracting system, ˜ a= 0, more than half of the ground state projects onto
negative-parity states even at fairly small values of ˜ αW. However, we see that the short-range interaction reduces
this effect. With negative ˜ a, the mixing of the negative-parity states is suppressed as the str ength of the two-body
interaction increases. When ˜ ais positive the effect is more striking. Mixing with negative-parity stat es is most
strongly suppressed for small positive values of ˜ a, while the projection onto these states increases for larger posit ive
values. The admixture is qualitatively the same when considering othe r forms of SOC as described in the following
sections.
IV. THE PURE RASHBA COUPLING
In order to find the matrix elements of the pure Rashba coupling give n in (1), we first note that it can be written
as a spherical tensor
VR=i√
2αR[k⊗σ]10. (20)
We therefore have the two-body Hamiltonian
1
/planckover2pi1ωH=/parenleftBig
h0,rel+i˜αR[/vector q⊗/vector σ]10+√
2π˜a(Λ)δ(3)(r)/parenrightBig
+/parenleftBig
h0,c.m.+i˜αR[/vectorQ⊗/vectorΣ]10/parenrightBig
. (21)
Because the spin-orbit coupling is now a k= 1 tensor rather than a scalar operator, the total angular mome ntumJ
isnolongerconserved. Additionally, the matrixelements nowdepend onthe quantumnumber Jz(whichis conserved).
For the relative-coordinate part of the SOC, some algebra gives
∝angb∇acketleftn′(l′s′)j′;N′L′;(j′L′)J′J′
z|[/vector q⊗/vector σ]10|n(ls)j;NL;(jL)JJz∝angb∇acket∇ight= 6i(−1)J+J′−J′
z+j′+L+1δN,N′δL,L′δJz,J′z
×/radicalbig
(2J+1)(2J′+1)(2j+1)(2j′+1)/parenleftbigg
J′1J
−Jz0Jz/parenrightbigg/braceleftbigg
j′J′L
J j1/bracerightbigg/braceleftBiggl′l1
s′s1
j′j1/bracerightBigg
(s′−s)∝angb∇acketleftn′l′||q||nl∝angb∇acket∇ight.(22)
For the center-of-mass part of the Hamiltonian we again expand th e basis states in the alternate coupling scheme (18)
to obtain the matrix elements
∝angb∇acketleftn′(l′s′)j′;N′L′;(j′L′)J′J′
z|[/vectorQ⊗/vectorΣ]10|n(ls)j;NL;(jL)JJz∝angb∇acket∇ight=δn,n′δl,l′δJz,J′zδs,1δs′,1
×6i√
2(−1)J+J′−J′
z+l/radicalbig
(2J+1)(2J′+1)(2j+1)(2j′+1)/parenleftbigg
J′1J
−Jz0Jz/parenrightbigg
∝angb∇acketleftN′L′||Q||NL∝angb∇acket∇ight
×/summationdisplay
J,J′(−1)J(2J+1)(2J′+1)/braceleftbigg
l1j′
L′J′J′/bracerightbigg/braceleftbigg
l1j
L JJ/bracerightbigg/braceleftbigg
J′J′l
JJ1/bracerightbigg/braceleftBiggL′L1
1 1 1
J′J1/bracerightBigg
.(23)
Our results for the Rashba SOC are shown in Fig. 6. Because the Ras hba spin-orbit coupling is a vector operator,
states of all possible Jmust be included in any calculation and the size of the basis scales much more quickly with
Emax. These spectra were computed with an Emaxof 24/planckover2pi1ω, for which there are approximately 36000 basis states.
All displayed eigenvalues of the Hamiltonian shift by less than 10−2/planckover2pi1ωif an additional shell of states is included.
This interaction was also studied perturbatively for small αRin [27], including the possibility of a spin-dependent
two-body interaction, under the assumption that center-of-ma ss excitations are unimportant. For the specific case of
identical fermions with spin-independent scattering length conside red here, they found that the first correction to the
energies occurs at order α2
Rand is independent of the scattering length a. We compare their perturbative predictions,
which are derived from the non-degenerate theory, with our nume rical results in Fig. 7.
By setting all matrix elements with N,L >0 in the bra or ket to zero, we also explored the approximation of
ignoring center-of-mass excitations. Fig. 8 shows that this is very accurate for the ground state, but less accurate for
excited states. Suppression of the c.m. coordinate has a similar effe ct for the SOCs considered in Secs. III and V. We
also note that in the case of small positive a, the landscape of low-lying excited states is dominated by center-o f-mass
excitations. When a→0+in the absence of spin-orbit coupling, there are an infinite number of states with nonzero
c.m. quantum numbers whose energies lie between the ground state and the first relative-coordinate excitation.
V. EQUAL-WEIGHT RASHBA-DRESSELHAUS SPIN-ORBIT COUPLING
Experiments have thus far realized only the effective Hamiltonian with equal strength Rashba and Dresselhaus
couplings in the form (3). Energy levels of the two-body system in th e one-dimensional equivalent of this Hamiltonian8
FIG. 6. (Color online) Spectrum of states with total angular momentum quantum number Jz= 0 for the Hamiltonian (21).
The left figure shows the energies with negative scattering l ength ˜a=−1. The right figure shows the results in the unitary
limit|˜a| → ∞. The spectrum is symmetric about ˜ αR= 0.
FIG. 7. (Color online) Comparison of selected spectral line s (dashed black) with the perturbative predictions from [27 ] (solid
red) when ˜a=∞.
with the additional magnetic field couplings present in experimental r ealizations have been calculated in [28]. Here
we treat the problem in three dimensions.
This is also the most computationally difficult of the three cases. When decomposed into spherical tensors, the
interaction (2) becomes
VD=iαD/parenleftBig
[k⊗σ]2,−2−[k⊗σ]2,2/parenrightBig
, (24)
and the two-particle Hamiltonian in the presence of equal strength Rashba and Dresselhaus SOC is given by (21)
withαR→αR=Dplus the additional spin-orbit terms
∆H=i˜αR=D√
2/parenleftBig
[/vector q⊗/vector σ]2,−2−[/vector q⊗/vector σ]2,2+[/vectorQ⊗/vectorΣ]2,−2−[/vectorQ⊗/vectorΣ]2,2/parenrightBig
. (25)
Yet again the number of basis states with nonzero matrix elements h as increased; no angular momentum quantum
numbers are conserved. The only remaining selection rule will be that the interaction does not change the total
magnetic quantum number Jzbetween even and odd.9
FIG. 8. (Color online) A comparison of the energy levels with (dashed black) and without (solid red) the inclusion of exci tations
in the c.m. coordinate for ˜ a=−1. The approximation of ignoring c.m. excitations provides very accurate results for the ground
state, but not for excited states.
Using the same approach as in the previous sections, the matrix elem ents of the relative Dresselhaus term are
∝angb∇acketleftn′(l′s′)j′;N′L′;(j′L′)J′J′
z|i˜αR=D√
2/parenleftBig
[/vector q⊗/vector σ]2,−2−[/vector q⊗/vector σ]2,2/parenrightBig
|n(ls)j;NL;(jL)JJz∝angb∇acket∇ight
=i√
30(−1)J+J′−J′
z+j′+LδN,N′δL,L′/radicalbig
(2J+1)(2J′+1)(2j+1)(2j′+1)∝angb∇acketleftn′l′||q||nl∝angb∇acket∇ight
×(s′−s)/bracketleftbigg/parenleftbigg
J′2J
−J′
z−2Jz/parenrightbigg
−/parenleftbigg
J′2J
−J′
z2Jz/parenrightbigg/bracketrightbigg/braceleftbigg
j′J′L
J j2/bracerightbigg/braceleftBiggl′l1
s′s1
j′j2/bracerightBigg
,(26)
while the center-of-mass part is
∝angb∇acketleftn′(l′s′)j′;N′L′;(j′L′)J′J′
z|i˜αR=D√
2/parenleftbigg/bracketleftBig
/vectorQ⊗/vectorΣ/bracketrightBig
2,−2−/bracketleftBig
/vectorQ⊗/vectorΣ/bracketrightBig
2,2/parenrightbigg
|n(ls)j;NL;(jL)JJz∝angb∇acket∇ight
= 2i√
15(−1)J+J′−J′
z+l+1δn,n′δl,l′δs,1δs′,1
×/radicalbig
(2J+1)(2J′+1)(2j+1)(2j′+1)/bracketleftbigg/parenleftbigg
J′2J
−J′
z−2Jz/parenrightbigg
−/parenleftbigg
J′2J
−J′
z2Jz/parenrightbigg/bracketrightbigg
∝angb∇acketleftN′L′||Q||NL∝angb∇acket∇ight
×/summationdisplay
J,J′(−1)J(2J+1)(2J′+1)/braceleftbigg
l1j′
L′J′J′/bracerightbigg/braceleftbigg
l1j
L JJ/bracerightbigg/braceleftbigg
J′J′l
JJ2/bracerightbigg/braceleftBiggL′L1
1 1 1
J′J2/bracerightBigg
.(27)
The richly structured excitation spectrum of low-lying states is sho wn in Fig. 9 for a cutoff of Emax= 17. All
displayed energies shift by less than .02 /planckover2pi1ωwhen the final shell is added, giving a slightly faster convergence th an in
the pure Rashba case.
VI. CONCLUSIONS
In this paper we have nonperturbatively calculated the spectrum o f interacting two-particle systems with realistic
spin-orbit couplings when the trapping potential cannot be ignored . Matrix elements of a short-range pseudopotential
and three types of spin-orbit coupling were determined analytically in a basis of the total angular momentum eigen-
states of the interacting two-body problem without SOC. With the a nalytic matrix elements, exact diagonalization
of the Hamiltonian within a finite basis was possible.
Our energy calculations were performed in a basis truncated in a con sistent way by including all states below
an energy cutoff. The resulting spectra show good convergence e xcept in the case where the two-body interaction
generates a small positive scattering length. In this regime coupling of the ground state to higher relative-coordinate
excited states dominates and convergence in the cutoff paramete rEmaxwas numerically intractable. We are currently
investigating alternative methods to deal with this issue. In the limit o f weak SOC we have compared our results to10
FIG. 9. (Color online) Spectrum of states with even total ang ular momentum magnetic quantum number Jz= 0,2,...for the
equal-weight Rashba-Dresselhaus SOC (3). The left figure sh ows the energies with negative scattering length ˜ a=−1. The
right figure shows the results in the unitary limit |˜a| → ∞. The spectrum is symmetric about ˜ αR=D= 0.
the perturbative calculations of [27] and found good agreement. W e also observed that although the ground state
does not couple strongly to center-of-mass excitations, their inc lusion is crucial for the excited state spectrum. The
relatively weak center-of-mass coupling of the ground state, how ever, suggests that cold atoms with SOC can be used
as a surrogate system to probe properties of two-body spin-orb it couplings, e.g., the parity-violating weak interaction
in nuclear systems.
We provided plots of a variety of spectra calculated with Weyl, Rashb a, and equal weight Rashba-Dresselhaus
couplings. Although in this paper we show spectra only within certain s ubspaces of conserved angular momentum
quantum numbers, the approach presented is fully capable of gene rating results for all possible states. Larger SO-
coupling constants are also accessible with larger basis sizes. The ge neral method can easily be adapted to calculate
energies for bosonic systems, or to new forms of SOC such as the r ecently proposed spin-orbital angular momentum
coupling [42].
Using the eigenvectors of the truncated basis Hamiltonian, we also e xplored the effect of parity violation on the
system. In particular we show how the SOC induces mixing of the posit ive- and negative-parity subspaces for the
ground state. Without a two-body interaction, the ground state preferentially projects onto negative parity basis
states even for modest SOC strength. The short-range interac tion was seen to suppress this mixing, especially when
the scattering length is positive.
A natural extension of this work is to consider three particles within a trap. Because of the complex spectrum
that is associated with three-body physics at the unitary limit (e.g., E fimov states, limit cycles, etc.), the spectrum
under the influence of an external SOC is expected to be quite rich. Couplings between the center-of-mass and
relative motion due to the SOC present a potential challenge to trad itional few-body techniques, such as the Faddeev
equations, which work only within the relative coordinates. However , in our two-body calculations we found that the
coupling of the ground state to the c.m. motion is weak. If this is also t rue in the three-body case, then to a good
approximation we can ignore the c.m. motion and utilize existing few-bo dy techniques with little or no modification.
ACKNOWLEDGEMENTS
We thank Paulo Bedaque, Jordy de Vries and Timo L¨ ahde for their inp ut and discussions related to this work.
This paper is based in part on work supported by the U.S. Departmen t of Energy, Office of Science, Office of Nuclear11
Physics, under Award No. de-sc00046548.
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Appendix: Derivation of the normalization factor for Busch wave functions
In the original paper by Busch et al.[38], the normalization factor of the wave functions is not given. The closed
form expression for this normalization does not seem to be widely kno wn. It was originally presented in [43] without
derivation, which we provide here. To find the norm of the wave func tion (12), one must integrate (using a change of
variables to z=r2)
A−2=Γ(−n)2
8π3/integraldisplay∞
01
z/bracketleftBig
U(−n,3/2,z)e−z/2z3/4/bracketrightBig2
dz. (A.1)
The term in brackets is equal to a Whittaker function [44] and so th is can be rewritten,
A−2=Γ(−n)2
8π3/integraldisplay∞
01
z/bracketleftbig
Wn+3/4,1/4(z)/bracketrightbig2dz. (A.2)
This integral can be found in [45]
/integraldisplay∞
01
z[Wκ,µ(z)]2dz=π
sin(2πµ)ψ0(1
2+µ−κ)−ψ0(1
2+µ−κ)
Γ(1
2+µ−κ)Γ(1
2−µ−κ). (A.3)
Applying this to (A.1) with κ=n+3/4 andµ= 1/4 gives the desired result,
A−2=1
8π3Γ(−n)
Γ(−n−1/2)[ψ0(−n)−ψ0(−n−1/2)]. (A.4) |
1607.08724v1.Twisted_spin_vortices_in_a_spinor_dipolar_Bose_Einstein_condensate_with_Rashba_spin_orbit_coupling.pdf | arXiv:1607.08724v1 [cond-mat.quant-gas] 29 Jul 2016Twisted spin vortices in a spinor-dipolar Bose-Einstein co ndensate with Rashba
spin-orbit coupling
Masaya Kato,1Xiao-Fei Zhang,1,2Daichi Sasaki,1and Hiroki Saito1
1Department of Engineering Science, University of Electro- Communications, Tokyo 182-8585, Japan
2Key Laboratory of Time and Frequency Primary Standards,
National Time Service Center, Chinese Academy of Sciences, Xi’an 710600, China
(Dated: September 20, 2018)
We consider a spin-1 Bose-Einstein condensate with Rashba s pin-orbit coupling and dipole-dipole
interaction confined in a cigar-shaped trap. Due to the combi ned effects of spin-orbit coupling,
dipole-dipole interaction, and trap geometry, the system e xhibits a rich variety of ground-state spin
structures, including twisted spin vortices. The ground-s tate phase diagram is determined with
respect to the strengths of the spin-orbit coupling and dipo le-dipole interaction.
PACS numbers: 03.75.Mn, 03.75.Lm, 67.85.Bc, 67.85.Fg
I. INTRODUCTION
Spin-orbit coupling is of fundamental importance in
many branches of physics, such as quantum spin-Hall ef-
fect, topological insulators, and superconductivity [1–4].
Recently, the NIST group has realized the light-induced
vector potentials and the synthetic electric and magnetic
fields in Bose-Einstein condensates (BECs) of neutral
atoms using Raman processes [5–8]. Remarkably, they
also created a two-component spin-orbit coupled con-
densate of Rb atoms [9]. Artificial spin-orbit coupling
(SOC) offers us a tremendous opportunity to study ex-
otic quantum phenomena in many-body systems, which
exhibit various symmetry-broken and topological con-
densate phases in pseudospin-1 /2 systems [10–18]. For
spin-1 and -2 condensates, more exotic patterns form due
to the competition between the SOC and spin-dependent
interactions [19–23].
On the other hand, recent experimental realization of
BECs of atomic species with large magnetic moments
boosts interest in the field of quantum gases with dipole-
dipole interaction (DDI) [24–27]. Previous studies on
spinor-dipolar BECs have shown that the interplay be-
tween spin-dependent interaction and DDI leads to rich
topological defects and spin structures [28–34]. Conse-
quently, it is of particular interest to explore the effects
of long-rang and anisotropic DDI on such a spin-orbit
coupled system, which has recently drawn considerable
attentions. More specifically, Deng et al. [35] proposed
anexperimentalschemetocreateSOCinspin-3Cratoms
using Raman processes. Wilson et al. have investigated
the effects of DDI on a pseudospin-1 /2 spin-orbit cou-
pled condensate, and predicted the emergence of a ther-
modynamically stable ground state having a spin con-
figuration called meron [36]. Furthermore, a number of
quantum crystalline and quasicrystalline ground states
were found in two-dimensional (2D) dipolar bosons with
Rashba SOC [37].
In this work, we consider a BEC of spin-1 bosons con-
fined in a cigar-shaped trap potential, subject to both
2D SOC and DDI. The 2D SOC tends to create spintextures in the x-yplane, while the DDI can generate
z-dependent spin textures in an elongated system. As a
result, 3D spin structures emerge in this system. We elu-
cidate the ground-state spin textures as functions of the
strengths of the SOC and DDI by numerically minimiz-
ing the energy functional. We will show a rich variety of
ground-state spin textures, such as twisted spin vortices,
in which spin vortices twist around each other along the
zdirection.
The paper is organized as follows. In Sec. II, we for-
mulate the theoretical model and briefly introduce the
numerical method. In Sec. III, the ground-state phase
diagram of the system is determined, and a detailed de-
scription of each phase is given. In Sec. IV, the main
results of the paper are summarized.
II. FORMULATION OF THE PROBLEM
We consider a BEC of spin-1 atoms with mass Mcon-
fined in a harmonic potential, which are subject to the
2D SOC. We employ the mean-field approximation and
the state of the system is described by the spinor order
parameter Ψ(r) = (ψ1(r),ψ0(r),ψ−1(r))T.The single-
particle energy is given by
E0=/integraldisplay
dr؆/bracketleftbigg
−/planckover2pi12
2M∇2+V(r)+gsoc/planckover2pi1
i∇⊥·f⊥/bracketrightbigg
Ψ,
(1)
where gsocparametrizes the SOC strength, ∇⊥=
(∂x,∂y), andf⊥= (fx,fy) are the 3 ×3 spin-1 ma-
trices. The trap potential is axisymmetric, V(r) =
Mω2
⊥(x2+y2+λ2z2)/2, whereω⊥is the radial trap fre-
quency and λ=ωz/ω⊥is the aspect ratio between the
axial and radial trap frequencies. The s-wave contact
interaction energy is written as
Es=1
2/integraldisplay
dr/bracketleftbig
g0ρ(r)+g1F2(r)/bracketrightbig
, (2)
where g0= 4π/planckover2pi12(a0+ 2a2)/(3M) and g1= 4π/planckover2pi12(a0−
a2)/(3M) withas(s= 0,2) being the s-wave scattering2
length for the scattering channel with total spin s. The
totalatomicdensity ρ(r) =|ψ1(r)|2+|ψ0(r)|2+|ψ−1(r)|2
satisfies/integraltext
ρ(r)dr=N, whereNis the total number of
atoms. The spin density has the form
F(r) =Ψ†
fx
fy
fz
Ψ=
√
2Re[ψ∗
1ψ0+ψ∗
0ψ−1]√
2Im[ψ∗
1ψ0+ψ∗
0ψ−1]
|ψ1|2−|ψ−1|2
.(3)
The DDI energy is given by
Eddi=gdd
2/integraldisplay
drdr′ˆF(r)·ˆF(r′)−3(ˆF(r)·e)(ˆF(r′)·e)
|r−r′|3,
(4)
where gdd=µ0µ2
d/(4π),µ0is the magnetic permeability
of the vacuum, µdis the magnetic dipole moment of the
atom, and e= (r−r′)/|r−r′|. The total energy of the
system is thus given by E=E0+Es+Eddi.
The ground state is numerically obtained by minimiz-
ing the totalenergy Eusingthe imaginary-timepropaga-
tionmethod. Fortheimaginary-timeevolution, thepseu-
dospectral method with the fourth-order Runge-Kutta
scheme is used. In the following numerical simulations,
we work in dimensionless unit. The energy and length
are normalized by /planckover2pi1ω⊥anda⊥=/radicalbig
/planckover2pi1/(Mω⊥). In this
unit, the wave function, the SOC coefficient gsoc, and the
interaction coefficients g0, g1, and gddare normalized by
N1/2/a3/2
⊥,a⊥ω⊥, and/planckover2pi1ω⊥a3
⊥/N, respectively.
III. GROUND-STATE SPIN STRUCTURES
The richness of the present system lies in the large
number of free parameters, including the strength and
sign of the contact interactions, DDI, SOC, aspect ratio,
and so on. To highlight the effects of the SOC and DDI,
we fixλ= 0.2, g0= 4000, and g1= 0, implicitly assum-
ing that the ground-state spin texture is dominated by
the SOC and DDI.
Our main results are summarized in Fig. 1, which
shows the ground-state phase diagram of a spin-orbit
coupled dipolar condensate with respect to gsocand gdd.
There are eight different phases marked by A-H, which
differ in density profiles, spin texture and angular mo-
mentum. In the following discussion, we will give a de-
tailed description of each phase. In the white region of
Fig. 1, the condensatecollapsesdue tothe attractivepart
of the DDI [38], where no stable mean-field solution ex-
ists [39]. The critical value of gddfor the collapse seems
almost independent of gsoc.
We start from the case where both the SOC and DDI
are sufficiently weak, indicated by the gray region F in
Fig. 1. In this phase, the central region of the poten-
tial is occupied by mf= 0 component and the system
is condensed to such component, leading to vanishing
magnetization of the system. We note that this phase
disappears with increasing either the SOC or DDI.
In the limit of strong SOC but weak DDI, the system
exhibits a spin-stripe pattern, indicated by A-phase incollapse
HGFA
EBC
D
1000 500 2.0
1.0
0
03.0
FIG. 1: (color online) Ground-state phase diagram of the
spin-orbit coupled dipolar BEC with respect to gsocand gdd
for g0= 4000, g1= 0, andλ= 0.2. There are eight different
phasesmarkedbyA-H.Thewhiteregionrepresentsinstabili ty
against dipolar collapse.
Fig. 1. Typical density and spin distributions of such
phase are shown in Fig. 2(a). In this phase, the spin
texture on the x-yplane shows typical spin stripe struc-
ture, which is almost unchanged along the z-axis. Actu-
ally,previousstudiesontrappedspin-orbitcoupledBECs
haveshown that the spin stripe structure is known as one
of the ground states at strong SOC in harmonic poten-
tial [15]. In the present system, this state also exists for
a strong SOC, but with a weak DDI.
With an increase in the strength of the DDI, B-phase
emerges as the ground state, as shown in Fig. 1. Typical
density and spin distributions of such phase are shown
in Fig. 2(b). This phase is characterized by the checker-
board lattice of spin vortices on the x-yplane, in which
spin vortices with Fz>0 andFz<0 are alternately
aligned. Such a pattern may be understood by the long-
range nature of the DDI, which leads to a regular density
distribution of each component. Similar to A-phase, the
spin texture is almost independent of z.
Increasing the DDI further, the spin vortex structures
begin to have a zdependence, and C-phase emerges as
the ground-state of the system, as the yellow-green re-
gion in Fig. 1. Typical density and spin distributions
of such phase are shown in Fig. 3(a). This phase has a
spin-vortex train structure on the x-yplane, where com-
ponents 1 and −1 are surrounded by component 0. The
numbers of spin vortices with Fz>0 andFz<0 are
equal to each other, which increase with SOC. Three-
dimensional (3D) isodensity surfaces of the state are
shown in Fig. 4, which indicates that the spin vortex
structure depends on zdue to the DDI.
WithafurtherincreaseintheDDI,C-phasetransforms
to D-phase, as shown in Fig. 1. Its density and spin dis-
tributions and 3D structures are shown in Figs. 3(b) and
5, respectively. Interestingly, the spin structure signifi-3
0.000 0.002 -0.002 0.002
0total spin (b) B-phase
-2 0 2 -2 0 2 -2 0 2total spin (a) A-phase
-2 0 2 -2 0 2 -2 0 2
FIG. 2: (color online) Typical density distribution and spi n
texture of the system for (a) gdd= 0.0 and gsoc= 2.4 and
(b) gdd= 100 and gsoc= 2.4, corresponding to the states
represented in A and B phases in Fig. 1, respectively. The
arrows in the spin texture represent the transverse spin vec tor
(Fx,Fy) with background color representing Fz.
cantly depends on zand form a helical structure, leading
to twisted spin vortices. We note that this spin struc-
ture, as well as C-phase, reflects the features of the SOC
and DDI: multiple spin vortices are created by the SOC
and they are twisted along the z-axis by the DDI. In the
region D of Fig. 1, we also observe three twisted spin
vortices for a larger SOC. Our numerical results show
that the degree of torsion increases with DDI, while the
separation between the spin-vortices decreases. In the
limit of strong DDI, the separation almost disappears
and E-phase emerges as the ground state, as shown in
blue region in Fig. 1.
E-phase is characterized by its axisymmetric density
distribution of each component, where the central region
is occupied by component 1 and outer regions by com-
ponents 0 and −1, as shown in Fig. 6(a). Components
0 and−1 have vorticities ±1 and±2, respectively. The
spin texture in the x-yplane has a single spin vortex
at the center, which is similar to the chiral spin-vortex
state [29, 30]. This phase exists for strong DDI or weak
SOC, and occupies the largest phase in the ground-state
phase diagram in Fig. 1.
0.000 0.002 -0.002 0.002
0total spin (b) D-phase
-2 0 2 -2 0 2 -2 0 2total spin (a) C-phase
-2 0 2 -2 0 2 -2 0 2
FIG. 3: (color online) Typical density distribution and spi n
texture of the system for (a) gdd= 250 and gsoc= 2.0 and
(b) gdd= 300 and gsoc= 1.5, corresponding to C and D
phases in Fig. 1, respectively. The arrows in the spin textur e
represent the transverse spin vector ( Fx,Fy) with background
color representing Fz.
Finally, we move to another limit of weak SOC and
strong DDI. In this region, there are two phases marked
G and H in Fig. 1. The G-phase is shown in Figs. 6(b)
and 7. This phase has a helical structure along the z-
axis, in which component 0 are twined by the other two
components, resulting in a double helix of Fz>0 and
Fz<0. The state shown in Figs. 6(b) and 7 has not
only the spin angular momentum but also the orbital
angular momentum in the zdirection. For a small gsoc,
+1 and−1 components are balanced and the spin and
orbital angular momenta disappear. In the present case
of g1= 0, this state is not the ground state for gsoc= 0,
while it can be a stationary state. It is found in Ref. [33]
that this state can be the ground state for g1<0 even
without SOC.
The density and spin distributions of H-phase are
shown in Fig. 6(c). The spin texture of this state is sim-
ilar to that of the polar-core vortex, i.e., |F|= 0 on the
z-axis and the transverse spin vectors rotate around the
core. However, this state is different from the polar-core
vortex, in that the axisymmetry is broken in |ψ±1|2and
Fz/negationslash= 0.4
02 4
FIG. 4: (color online) Isodensity surfaces of the three com-
ponents |ψ1|2= 0.001 (red), |ψ0|2= 0.0007 (green), and
|ψ−1|2= 0.001 (blue), corresponding to C-phase shown in
Fig. 3(a). See the Supplemental Material for a movie showing
the three-dimensional (3D) structure [40].
02 4
FIG. 5: (color online) Isodensity surfaces of the three com-
ponents |ψ1|2= 0.001 (red), |ψ0|2= 0.0007 (green), and
|ψ−1|2= 0.0004 (blue), corresponding to D-phase shown in
Fig. 3(b). See the Supplemental Material for a movie showing
the 3D structure [40].
In all the phases demonstrated above, space- and time-
reversed states of the ground states are also the ground
states because of the symmetry of the Hamiltonian, that
is, ifψm(r) is a ground state, ( −1)mψ∗
−m(−r) is also a
ground state. The rotation about the z-axis also does
not change the energy. A-, C-, F-, and H-phases have
the space-time reversal symmetry and E-phase has the
rotation symmetry about the z-axis.
Thez-component of the orbital angular momentum,
/angb∇acketleftLz/angb∇acket∇ight=/integraltext
rΨ†(r)(xpy−ypx)Ψ(r)isnotableinconsidering
our system. Figure 8 shows /angb∇acketleftLz/angb∇acket∇ightas a function of gsocfor
gdd= 700 being fixed. The C- and H-phases scarcely
have angular momentum, since there is the space-time
reversal symmetry and /angb∇acketleftLz/angb∇acket∇ightis canceled between ψ1and
ψ−1. The first rapid increase in /angb∇acketleftLz/angb∇acket∇ightoccurs in the G-
phase(0.06<∼gsoc<∼0.17). TheE-phasealsohasnonzero
/angb∇acketleftLz/angb∇acket∇ight, sinceψ0andψ−1have singly and doubly quantized
vortices, respectively. In the D-phase, /angb∇acketleftLz/angb∇acket∇ightchanges at
gsoc≃2.0, sincethenumberofspinvorticeschangesfrom
0.000 0.002 -0.002 0.002
0total spin (c) H-phase
-2 0 2 -2 0 2 -2 0 2total spin (b) G-phase
-2 0 2 -2 0 2 -2 0 2
total spin (a) E-phase
-2 0 2 -2 0 2 -2 0 2
0.000 0.004
total
FIG. 6: (color online) Typical density distribution and spi n
texture of the system for (a) gdd= 300 and gsoc= 0.6, (b)
gdd= 700 and gsoc= 0.1, and (c) gdd= 700 and gsoc=
0, corresponding to the states represented in E, G and H
phases in Fig. 1, respectively. The arrows in the spin textur e
represent the transverse spin vector ( Fx,Fy) with background
color representing Fz.
two to three. The maximum of /angb∇acketleftLz/angb∇acket∇ightis attained in the
D-phase, and at gsoc≃2.4,/angb∇acketleftLz/angb∇acket∇ightdramatically decreases
and the ground state transforms to the C-phase with an
increase in SOC.
We have also examined the cases of g1/negationslash= 0, and
found that the B-E phases remained almost unchanged
for|g1| ∼0.1g0; the phaseboundariesareslightlyshifted.
Our main results are thus unchanged for finite g1.5
02 4
FIG. 7: (color online) Isodensity surfaces of the three com-
ponents |ψ1|2= 0.001 (red), |ψ0|2= 0.001 (green), and
|ψ−1|2= 0.001 (blue), corresponding to G-phase shown in
Fig. 6. See the Supplemental Material for a movie showing
the 3D structure [40].
0 0.5 1.0 1.5 2.0 2.5 3.0 00.5 1.0 1.5 2.0 2.5 3.0
H
G
E D C
FIG. 8: (color online) Orbital angular momentum /angbracketleftLz/angbracketrightas a
function of gsocfor gdd= 700. The vertical lines separate the
phases and the solid curve is guide to the eyes.IV. CONCLUSIONS
We have investigated the ground-state structures of
a spin-1 Bose-Einstein condensate with the 2D Rashba
SOC and DDI, confined in a cigar-shaped trap potential.
Due to the interplay between the 2D-like pattern for-
mation by the Rashba SOC and the zdependence aris-
ing from the long-range DDI, we found a rich variety
of ground-state phases, including the twisted spin vor-
tices. We systematically explored the parameter space
and obtained the ground-state phase diagram as a func-
tion of the strength of the SOC and DDI, which con-
sists of eight different phases. For strong SOC and weak
DDI, the stripe or plane-wavephase is obtained. Increas-
ing the DDI, the spin-vortex lattice emerges (B-phase),
which form square pattern due to the long-range nature
of the DDI. In the opposite limit, i.e., for strong DDI
and weak SOC, we have two symmetry broken states (G-
and H-phases). The chiral spin-vortex state (E-phase) is
the ground state for a wide parameter region. Between
B- and E-phases, we found novel spin structures having
both SOC and DDI features, which we call C-and D-
phases. In the C-phase, bunches of spin vortices with
opposite directions are twisted along the z-axis, and in
the D-phase, a few spin vortices form helical structures.
Both SOC and DDI couple the internal and external
degrees of freedom in a BEC. Combining such effects, a
wide variety of spin textures will be realized.
Acknowledgments
This work was supported by JSPS KAKENHI Grant
Numbers JP16K05505,JP26400414,and JP25103007,by
the key project fund of the CAS for the “Western Light”
Talent Cultivation Plan under Grant No. 2012ZD02,and
by the Youth Innovation Promotion Association of CAS
under Grant No. 2015334.
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the three-dimensional structures of the ground states. |
1907.00974v2.Spin_dynamics_of_moving_bodies_in_rotating_black_hole_spacetimes.pdf | Spin dynamics of moving bodies in rotating black hole spacetimes
Balázs Mikóczi1;yand Zoltán Keresztes2;z
1Research Institute for Particle and Nuclear Physics,
Wigner RCP H-1525 Budapest 114, P.O. Box 49, Hungary
2Department of Theoretical Physics, University of Szeged, Tisza Lajos krt. 84-86, Szeged 6720, Hungary
yE-mail: mikoczi.balazs@wigner.huzE-mail: zkeresztes@titan.physx.u-szeged.hu
The dynamics of spinning test bodies, moving in rotating black hole (Kerr, Bardeen-like and
Hayward-like) spacetimes, are investigated. In Kerr spacetime, all the spherical, zoom-whirl and
unbound orbits are considered numerically. Along spherical orbits and for high spin, an amplitude
modulation is found in the harmonic evolution of the spin precessional angular velocity, caused
by the spin-curvature coupling. Along the discussed zoom-whirl and unbound orbits, the test body
approachesthecentersomuchthatitpassesthroughtheergosphere. Nearandinsidetheergosphere,
the variation of the spin direction can be very rapid. The effects of the spin-curvature coupling is
also investigated. The initial values are chosen such a way, that the body and its spin move in
the equatorial plane of the coordinate space and of the comoving frame, respectively. Hence, a
clear effect of the spin-curvature coupling is observed as the orbit and the spin vector leave the
equatorial plane. Additional effects in the spin precessional angular velocity and in the evolution
of the Boyer-Lindquist coordinate components of the spin vector is also considered. Finally, in case
of different regular black holes, the spin-curvature coupling influences differently the orbit and the
spin evolutions.
Keywords: black hole physics, spinning test particles, Mathisson-Papapetrou-Dixon equations, Kerr space-
time
I. INTRODUCTION
Both the orbital and the spin dynamics of compact bi-
nary systems have a renewed interest. All observed grav-
itational waves originated from compact binary systems
composed of black holes or neutron stars ([1–8]). In two
cases the spin of the merging black holes was identified
with high significance [2, 8, 9]. In addition, in a binary
system the dominant supermassive black hole spin pre-
cession was identified from VLBI radio data spanning
over 18 years [10].
In the post-Newtonian (PN) approximation the lowest
order spin contributions to the dynamics come from the
spin-orbit, spin-spin and quadrupole-monopole interac-
tions [11–14]. The spin effects on the orbit leaded to set
up generalized Kepler equations [15–18]. The analytical
description of the secular spin dynamics for black holes is
given in Refs. [19] and [20]. Based on the PN description
several interesting spin related behaviours were identified
in compact binary systems, like transitional precession
[21], equilibrium configurations [22], spin-flip [23], spin
flip-flop [24] and wide precession [25].
The Mathisson–Papapetrou–Dixon (MPD) equations
[26–30] describe the dynamics of binaries with signif-
icantly different masses more accurately than the PN
approximation in the strong gravitational field regime,
where the PN parameter is not small. The black hole
binary systems with small mass ratio are among the
most promising sources for gravitational waves in the fre-
quency sensitivity range of the planned LISA - Laser In-
terferometer Space Antenna [31, 32]. In addition, near
the central supermassive black holes in the galaxies many
stellar black holes are expected to exist [33–35].
The MPD equations are not closed, a spin supplemen-tary condition1(SSC) is necessary to choose [28, 37–44],
which defines the point at which the four-momentum and
the spin are evaluated. The Hamiltonian formulations in
different SSCs are discussed in Refs. [45–49]. A non-
spinning body follows a geodesic trajectory, while a spin-
ning one does not [50, 51]. Spinning bodies governed by
the MPD equations were already studied on Kerr back-
ground. Circular orbits in the equatorial plane can be
unstable not only in the radial direction but also in the
perpendiculardirectiontotheequatorialplaneduetothe
spin [52]. The spin-curvature effect strengthens with spin
and with non-homogeneity of the background field [51].
The MPD equations admit many chaotic solutions, how-
ever, these do not occur in the case of extreme mass ra-
tiobinaryblackholesystems[53–56]. Analyticstudieson
the deviation of the orbits from geodesics due to the pres-
enceofasmallspinarepresentedinRefs. [57–59]. Highly
relativistic circular orbits in the equatorial plane occur in
much wider space region for a spinning body than for a
non-spinning one [60]. Spin-flip-effects may occur when
the magnetic type components of quadrupole tensor are
non-negligible [61]. Corrections due to the electric type
components of quadrupole tensor to the location of in-
nermost stable circular orbit in the equatorial plane and
to the associated motion’s frequency were determined in
Ref. [62]. An exact expression for the periastron shift
of a spinning test body moving in the equatorial plane is
derived in Ref. [63]. The influences of the affine param-
eter choice on the constants of motion in different SSC
1Both the PN dynamics with spin-orbit coupling and the gravita-
tional multipole moments depend on the SSC [13, 36].arXiv:1907.00974v2 [gr-qc] 9 Feb 20222
were also considered [64]. Frequency domain analysis of
motion and spin precession was presented in Ref. [65].
The evolution of spinning test particles were investigated
in the
space-time [66], in non-asymptotically flat space-
times [67], and in wormholes [68].
Considering geodesic trajectories, the periastron ad-
vance can become such significant in the strong gravita-
tional field regime that the test particle follows a zoom-
whirl orbit[69–71]. For non-spinningparticles, thetopol-
ogy of these orbits was encoded by a rational number
[72, 73]. Numerical relativity confirmed the existence of
zoom-whirl orbits [74–79], and they also occur in the 3
PN dynamics with spin-orbit interaction [80, 81]. Here
we will present zoom-whirl orbits occurring in the MPD
dynamics for the first time. In addition, these orbits pass
over the ergosphere where the PN approximation fails.2
Hyperbolic orbits of spinning bodies were analytically
studied in both the PN [82] and the MPD [83] dynamics.
Analytic computations in Ref. [83] were carried out for
small spin magnitudes, when the spin is parallel to the
central black hole rotation axis and the body moves in
the equatorial plane. In this configuration both the spin
magnitude and direction are conserved, but they have
non-negligible influences on the orbit. In our numerical
consideration the spin is not parallel to the black hole
rotation axis. As a consequence, the body’s orbit is not
confined to the equatorial plane and the spin direction
evolves. In addition, the closest approach distance is in-
side the ergosphere where the PN approximation cannot
be used.
Our investigations are not only applied in the Kerr
spacetime but also in regular black hole backgrounds.
The first spacetime containing a nonrotating regular
black hole was suggested by Bardeen [84]. This metric
was interpreted as the spacetime surrounding a magnetic
monopole occurring in a nonlinear electrodynamics [85].
Another nonrotating regular black hole was introduced
by Hayward [86] having similar interpretation [87]. The
spacetime family containing the Bardeen and Hayward
cases was generalized for rotating black holes [88] which
we will use here3.
In this paper, we investigate the orbit and spin evo-
lutions of bodies moving in Kerr, Bardeen-like and
Hayward-like spacetimes and governed by the MPD
equations with Frenkel–Mathisson–Pirani (FMP) and
Tulczyjew–Dixon (TD) SSCs. When the covariant
derivatives of the spin tensor and the four-momentum
alongtheintegralcurveofthecentroiddeterminedbythe
2At the ergosphere the value of the PN expansion parameter is
typically about 1=2.
3There are discussions (see Refs. [89–91]) on that the rotating
regular black hole spacetimes given in Ref. [88] are not exact
solutions of the field equations. However the spacetime family
given analytically differs only perturbatively from the exact so-
lution [91], therefore it is suitable for consideration of spinning
bodies evolutions.SSC are small, this system reduces to a geodesic equation
with parallel transported spin discussed in Ref. [92]. In
thissensethepresentarticlecanbeconsideredasthegen-
eralizationofRef. [92]withnon-negligiblespin-curvature
correctionscausingthatthecentroidorbitisnon-geodesic
andthespinisnotparalleltransported. AsBini,Geralico
and Jantzen pointed out that the spin dynamics can be
described suitably in the comoving Cartesian-like frame
obtained by boosting the Cartesian-like frame associated
to the family of static observers (SOs). This is because
SOsdonotmovewithrespecttothedistantstars. Hence,
the Cartesian-like axes locked to SOs define good refer-
ence directions to which the variation of the spin vector
can be compared. Here, we derive the spin evolution
equation in the comoving Cartesian-like frame based on
the MPD system. However, SO does not exist inside the
ergosphere of the rotating black hole, and thus its frame
cannot be used for description of the dynamics when the
spinning body passes over this region. Therefore, the
spin dynamics in a Cartesian-like frame obtained by an
instantaneous Lorentz-boost from the frame associated
to the zero angular momentum observer (ZAMO) is also
presented, which can be used inside the ergosphere. The
boosted SO and ZAMO frames relate to each other by
a spatial rotation outside the ergosphere. The rotation
angle between these boosted frames is unsignificant far
from the rotating black hole.
In Section II, the MPD equations, the spin supple-
mentary conditions, the rotating (Kerr, Bardeen-like and
Hayward-like) black hole spacetimes and the frames as-
sociated with the families of SOs and ZAMOs are intro-
duced. In Section III the representations of spin evo-
lution are given. For this purpose, we introduce two
framesbyinstantaneousLorentzboostsofSOandZAMO
frames, which comoves with an observer having an arbi-
trary four velocity U. The relation between the boosted
frames is discussed (additional expressions are given in
Appendix VII). We use the TD SSC, and Umeans ei-
ther the centroid or the zero 3-momentum observer four
velocity. The spin evolution equation is derived in these
U-frames. First, the spin precession is described with
respect to the boosted spherical coordinate triad associ-
ated with either the SOs or ZAMOs. Then, we intro-
duce Cartesian-like triads in the rest spaces of SOs and
ZAMOs. The spin precession with respect to the corre-
sponding boosted Cartesian-like frames is also derived.
The relations between the spin angular velocities in the
boosted SO and ZAMO frames are discussed. In Section
IV, we apply the derived spin equations for numeric in-
vestigations when the body moves along spherical-like,
zoom-whirl and unbound orbits. In Subsection IVA the
background is the Kerr spacetime, while in Subsection
IVB, it is one of the rotating regular black hole space-
times. In Appendix VIII, the avoidance of paradoxical
behaviour of the MPD equations is checked. Finally, Sec-
tion V contains the conclusions.
We use the signature + ++, and units where c=
G= 1, with speed of light cand gravitational constant3
G. The bold small Greek indices with or without prime
take values 1,2and3, while the bold capital and the
small Latin indices 0,1,2and3. In addition, the fol-
lowing small bold Latin indices i,j,kandi0,k0take
values fromfx;y;zg. Finally, the bold indices are frame
indices, while the non-bold indices are spacetime coordi-
nate indices.
II. EQUATIONS OF MOTION FOR SPINNING
BODIES IN ROTATING BLACK HOLE
SPACETIMES
A. MPD equations and SSC
In the pole-dipole approximation, the motion of an ex-
tended spinning body in curved spacetime is governed by
the MPD equations [26–30] which read as
Dpa
ducrcpa=Fa; (1)
DSab
ducrcSab=paub uapb; (2)
with
Fa= 1
2Ra
bcdubScd: (3)
Herercis the covariant derivative, paandSabare the
four-momentum and the spin tensor of the moving body,
respectively, and Ra
bcdis the Riemann tensor. Finally,
ua=dxa=dis the four-velocity of the representative
point for the extended body at spacetime coordinate
xa()with an affine parameter . Note that higher mul-
tipoles of the body should occur in the MDP equations
when they are nonvanishing. Here they are taken to be
zero.
Choosing the affine parameter as the proper time
[48, 93]uaua= 14, Equation (2) can be written as
pa=mua ubDSab
d; (4)
wherem= uapais the mass in the rest frame of the
observer moving with velocity ua. Equation (4) shows
that the momentum paand the kinematic four velocity
uaare not proportional to each other for a spinning body
in general.
We note that if the covariant derivatives of the spin
tensor and the four-momentum along the integral curve
ofuaare small, i.e. the right hand sides of Equations
(1) and (2) are negligible, pabecomes proportional to ua
4Below we derive a condition for the spin magnitude in TD SSC
when the proper time parametrization has a sense.which satisfies the geodesic equation because mis a con-
stant. Then introducing a spin four-vector perpendicular
toua(see Equation (2.5) of Ref. [94]), it will be parallel
transported along the trajectory. The geodesic equations
with parallel transported spin vector was investigated in
Ref. [92].
Ingeneral, inordertoclosetheMPDequationsanSSC
is necessary to choose, which defines the representative
point of the extended body referred as the center of mass
or the centroid. There are some proposed SSC, namely
the Frenkel-Mathisson-Pirani [26, 37, 38], the Newton-
Wigner-Pryce [40, 41], the Corinaldesi-Papapetrou [27,
39], and the Tulczyjew-Dixon [28, 42]. We will apply the
Tulczyjew-Dixon SSC imposing that
paSab= 0: (5)
This SSC yields two constants of motion, the spin mag-
nitudeS2=SabSab=2and the dynamical mass M=p papa(see Ref. [51]). In addition, the TD SSC to-
gether with the MPD equations results in the following
velocity-momentum relation [51, 95, 96]:
ub=m
M2
pb+4S2
vb
; (6)
with
vb=SbaRaecdpeScd
2S2; (7)
and
= 4M2+ 2RS2; (8)
whereR=RaecdSaeScd=2S2. Sincepbandubare not
parallels,ubmay become spacelike from timelike along
an integral curve. Where the causal character of a curve
is changed, it is known as superluminal bound and has
been discussed in different cases (e.g. Refs.: [51, 66–68]).
The superluminal motion has no physical meaning, and
the timelike condition for ubyields a bound for the spin
magnitude as
S2<2M3
2v RM; (9)
wherev=pvava5. When the spin magnitude obeys
this constraint, the proper time parametrization has
sense and the normalization ubub= 1gives a relation
m2=m2
pa;Sbc
as
m2=M4
M2 16S4
2v2: (10)
5Note thatvandRdo not carry information on the spin mag-
nitude since Sab=p
2Shas unit norm.4
Since the relation (6) can be inverted [97], both initial
data sets
xa;pa;Sab
jinand
xa;m;ua;Sab
jinpro-
vide a unique solution of the MPD equations with TD
SSC.
Thespinvectorbeingperpendicularto paisintroduced
as
Sa= 1
2MabcdpbScd: (11)
Since
SaSab= 0 =Sapa= 0; (12)
the contraction of Equation (6) with Sbresults inSbub=
0. Finally, the covariant derivative of Saalong the world-
line of the centroid is
DSa
d=SbFb
M2pa: (13)
IfFais negligible, Sais parallel transported along the
worldline of the centroid, and the centroid moves along a
geodesic curve. The latter can be shown from the MPD
equations together with (4) and (13).
Finally, we mention that the MPD equations are valid
only for test particles whose backreaction to the back-
ground spacetime curvature are negligible. Hence, when
the spinning body is moving in a spacetime around a
black hole with a mass parameter , the dimensionless
spin magnitude S=Mmust be small [53, 98]. This is
consistent with the constraint (9), which becomes for the
dimensionless spin magnitude as
S
M2
<2
2v RMM
; (14)
where the mass ratio M=gives a small factor.
B. Rotating black hole spacetimes
The line element squared describing the considered ro-
tating black hole spacetimes in Boyer-Lindquist coordi-
nates reads as [88, 99]
ds2= a2sin2
dt2 2aBsin2
dtd
+
dr2+ d2+A
sin2d2;(15)
with
=r2+a2cos2 ;
=r2+a2 2 [+(r)]r ;
B=r2+a2 ;
A=
r2+a22 a2sin2: (16)
In the Kerr spacetime (r)vanishes and andade-
note the mass and rotation parameters, respectively. Thefunction(r)occurs when a non-linear electromagnetic
field is present. It is given by
(r) =emr
(r+qm)
=; (17)
whereem=q3
m=is the electromagnetically induced
ADM mass. Here controls the strength of nonlinear
electrodynamic field and carries the dimension of length
squared,qmis related to the magnetic charge (see Ref.
[87]), and the powers are (
= 3,= 2) for the Bardeen-
like and (
= 3,= 3) for the Hayward-like spacetimes.
The stationary limit surfaces and the event horizon (if
they exist) are determined by the solutions of equations
gtt= a2sin2= 0andgrr= = 0 , respectively.
The structure of the spacetime depends on the number
of real, positive solutions of these equations. For the
Kerr spacetime em= 0, then there are two stationary
limit surfaces and event horizons for a= < 1. The re-
gion which is located outside the outer event horizon but
inside the outer stationary limit surface is called ergo-
sphere. The spacetime is free from the singularity for
= 0and
3. The first and the second panels of
Figure 3 in Ref. [88] indicate the regions in the param-
eter space of aandq=qm=emfor the Bardeen and
the Hayward subcases, respectively, where the above line
element squared describes a regular black hole.
In the spacetimes having symmetries, constants of mo-
tion associated to each Killing vector a(which obeys
the Killing equation r(ab)= 0) emerge [29]. Since the
rotating black hole spacetimes have a timelike @tand a
spatial@Killing vectors due to the staticity and axial
symmetry, there are two constants of motion [53]:
E= pt 1
2Sab@agbt;
Jz=p+1
2Sab@agb: (18)
At spatial infinity Emeans the energy of the spinning
body andJzis the projection of the total momentum to
thesymmetryaxis. Theseconstantsareusedforchecking
the numerical accuracy.
1. Static and zero angular momentum observers
The worldlines of static observers are the integral
curves of the Killing vector field @t. This family of ob-
servers exists outside the ergosphere, where their frame
is given by
e0=u(SO)=1p gtt@t; e1=r
@r; e2=@p
;
e3= 1p
aBsin
p gtt@t p gtt
sin@
: (19)
The dual basis is obtained as eA
a=gabABeb
B, where
AB=diag( 1;1;1;1).5
The orbit of a zero angular momentum observer is or-
thogonal to the t=const. hypersurfaces [100, 101]. The
four velocity along this orbit is
u(ZAMO )=r
A
@t+aB
A@
;(20)
which corresponds to the 1-form: dt=p
gtt. In con-
trasttotheSOs, thisfamilyofobserversalsoexistsinside
the ergosphere but outside the outer event horizon. The
frame of the ZAMOs is given by
f0=u(ZAMO ); f1=r
@r;
f2=@p
; f3=r
A@
sin; (21)
with dual basis: fA
a=gabABfb
B.
III. REPRESENTATIONS OF SPIN
EVOLUTION
The spin vector (11) will be considered in both co-
moving and zero 3-momentum frames. The definitions
of comoving and zero 3-momentum observers will be in-
troduced in the next subsection. Then the spin evolution
equations will be derived using the boosted spatial spher-
ical and Cartesian-like triads.
A. Comoving and zero 3-momentum frames
In the TD SSC, the center of mass is unique and mea-
sured in the zero 3-momentum frame with four velocity
pa=M. Ontheotherhandthefourvelocityofthecentroid
isua. The comoving indicative will refer to that observer
which moves along the centroid worldline. The spin dy-
namics will be described in both the zero 3-momentum
and the comoving observer’s frames. The velocity of the
chosen observer will be denoted by U. The comoving and
zero 3-momentum observers’ frames will be set up from
the frames of the static and the zero angular momentum
observers by an instantaneous Lorentz-boost knowing U
numerically.
The comoving and zero 3-momentum frames (hereafter
unanimously referred as U-frame) obtained from the SO
frame are given by
E0(e;U)U= (S)
e0+v(S)
;
E(e;U) =e+Ue
1 + (S)
U+u(SO)
:(22)
Here=f1;2;3g,v(S)= 1
(S)U u(SO)is the rela-
tive spatial velocity of either the comoving or the zero
3-momentum observer with respect to the SO frame,which is perpendicular to e0, and the Lorentz factor is
(S)= Uu(SO). The dot denotes the inner product
with respect to the metric gab. The inverse transforma-
tion is given by
e0= (S)
E0(e;U) +w(S)
;
e=E(e;U) +u(SO)E(e;U)
1 + (S)
U+u(SO)
;(23)
where
w(S)=w
(S)E(e;U) = 1
(S)u(SO) U;(24)
is the relative spatial velocity of the static observer with
respect to the U-frame.
The corresponding Lorentz-boost from the ZAMO
frame reads as
E0(f;U)U= (Z)
f0+v(Z)
;
E(f;U) =f+Uf
1 + (Z)
U+u(ZAMO )
;(25)
with relative spatial velocity v(Z)= 1
(Z)U u(ZAMO )
of theU-frame with respect to the ZAMO frame, and
Lorentz factor: (Z)= Uu(ZAMO ). The inverse boost
transformation is given by
f0= (Z)
E0(f;U) +w(Z)
;
f=E(f;U) +u(ZAMO )E(f;U)
1 + (Z)
U+u(ZAMO )
;
(26)
where
w(Z)=w
(Z)E(f;U) = 1
(Z)u(ZAMO ) U;(27)
is the relative spatial velocity of the ZAMO with respect
to either the comoving or the zero 3-momentum frame.
SinceE0(e;U) =U=E0(f;U), the transformation
between the frames EA(e;U)andEA(f;U)is a rota-
tion in the rest space of either the comoving or the zero
3-momentum observer. The rotation axis has the follow-
ing non-zero components in both the EA(e;U)and the
EA(f;U)frames:
n1= w2
(Z)q
w1
(Z)2+
w2
(Z)2
= w2
(S)q
w1
(S)2+
w2
(S)2; (28)
and
n2=w1
(Z)q
w1
(Z)2+
w2
(Z)2
=w1
(S)q
w1
(S)2+
w2
(S)2: (29)6
The rotation angle is determined by
sin ="
1 s
gttA!
(Z)w3
(Z)
1 + (Z)+aBsinp gttA#
(Z)r
w1
(Z)2
+
w2
(Z)2
1 + (S)
= "
1 s
gttA!
(S)w3
(S)
1 + (S) aBsinp gttA#
(S)r
w1
(S)2
+
w2
(S)2
1 + (Z); (30)
and
cos 1
1 q
gttA= 2
(Z)
w1
(Z)2
+
w2
(Z)2
1 + (S)
1 + (Z)
= 2
(S)
w1
(S)2
+
w2
(S)2
1 + (S)
1 + (Z):(31)
The frame E(e;U)(E(f;U)) is obtained from
E(f;U)(E(e;U))byarotationwiththeangle ( )
about the axis n. The rotation angle exists outside
the ergosphere where the terms under the square roots in
Equations(30)and(31)arepositive. Thetransformation
betweenE(e;U)andE(f;U)in another form is given
in Appendix VII. The above transformation is a special
caseoftheWigner-rotation[102], whichwasdiscussedre-
cently in Ref. [103]. However explicit expressions for the
rotation between the frames which we denote E(f;U)
andE(e;U)were not presented in [103].
B. MPD spin equations in comoving and zero
3-momentum frames
Weinvestigatetwocasesrelatedtothechosen U-frame:
i)Ua=pa=Mwhen we work in the zero 3-momentum
frame; and ii)Ua=uawhich is the four velocity of the
center of mass measured in the zero 3-momentum frame.
In all cases the spin vector can be expanded as
S=SE; (32)
sinceS0= 0. Here, the spatial frame vector Ein the
U-frame denotes either E(e;U)orE(f;U), which are
obtained by boosting the SO and ZAMO frames, respec-
tively.
The covariant derivative of the spin vector along the
integral curve of uis
DS
d=dS
dE+SDE
d: (33)Since the frame vectors are perpendicular to each other,
we have
EADEB
d= EBDEA
d; (34)
forA6=B, and because of the normalization:
EADEA
d= 0: (35)
Therefore the covariant derivatives of the spatial frame
vectors along the integral curve of ucan be expressed as
DE
d=
E0DE
d
E0 "
E
;(36)
where"
Levi-Civita symbol in the 3-dimensional Eu-
clidean space, whose frame indices are raised and lowered
by the 3-dimensional Kronecker , and the frame compo-
nents of the angular velocity are
= 1
2"
EDE
d: (37)
Due to Equation (34), the first term6in (36) can be writ-
ten as
E0DE
d= Ea; (38)
where adenotes the acceleration a=DE0=d. Now the
spin Equation (33) becomes as
DS
d=dS
d+"
S
E+ (Sa)E0:(39)
Finally, we take into account the spin Equation (13).
When considering the spin evolution in the zero 3-
momentum frame, we find the following equation for the
spin:
dS
d+"
S
= 0: (40)
The second case when considering the evolution of S
in the comoving frame, requires somewhat longer com-
putation. Equations (13) and (39) results in
dS
d+"
S
E+= 0;(41)
with
=
(Sa)uA (SF)pA
M2
EA:(42)
6Notethatthistermvanisheswhenthefirstorderspincorrections,
i.e. the right hand sides of Equations (1) and (2), are neglected
(see Ref. [92]).7
Using Equations (6) and (12), a straightforward compu-
tation shows that u= 0. Therefore, can be ex-
panded as = E. On the other hand is perpen-
dicular toS, hence, we can introduce a vector !, whose
frame components obey the relation
"
!S
=: (43)
The vector !is determined ambiguously since its frame
component parallel with Svanishes in the cross product.
As a natural choice, we choose !to be perpendicular to
S. Using the definition (43), Equation (41) reads as
dS
d+"
+!
S
= 0: (44)
The Equations (40) and (44) can be considered in ei-
ther theE(e;U)or theE(f;U)frame. Introducing
the notations
k=fe;fg; =
(S); (Z)
; (45)
the angular velocity components
(k;U)can be deter-
mined by using
E(k;U)DE(k;U)
d
=kDk
d
+1
1 + [(Uk)k (Uk)k]Dk0
d
+1
1 + [(Uk)k (Uk)k]DU
d;(46)
where6=. This can be computed once Uis deter-
mined.7
When both SO and ZAMO frames exist, a rotation
about the axis ndefined by Equations (28) and (29) [see
also Appendix VII for the explicit expressions] relates
E(f;U)toE0(e;U)which can be written as
E(e;U) =R0
E0(f;U): (47)
HereR0
denotes the components of the corresponding
rotation matrix. From the definitions of
(e;U)and
0(f;U), the following relation between them can be
derived:
R0
(e;U) =
0(f;U) +R0
(R):(48)
Here we have introduced
(R)as
R 1
0dR0
d="
(R); (49)
7We note that when the right hand sides of Equations (1) and (2)
are neglected, the centroid moves along a geodesic, thus !and
the last term in (46) vanish. The four-velocity Uis determined
from the geodesic equation, and for k=e, we obtain the same
system which was investigated in Ref. [92].which is the angular velocity of rotation between the
frame bases along the body’s trajectory.
1. Cartesian-like triads and the characterization of spin
evolution
The evolution of the spin vector can be illustrated
suitably by comparison its direction with Cartesian axes
which are fixed with respect to the distant stars. The
static observers are those fiducial observers, whose frame
doesnotmovewithrespecttotheblackhole’sasymptotic
frame [104]. A static observer sees the same “nonrotat-
ing” sky during the evolution. In this sense the static
observers are preferred fiducial observers in the investiga-
tion of spin dynamics. Following Ref. [92], we introduce
a spatial Cartesian-like triad ex,eyandezin the local
rest space of the static observer as e=Ri
ei, where
=f1;2;3g,i=fx;y;zgandRis the same rotation
matrix, which relates the Cartesian and spherical coordi-
nates in the 3-dimensional Euclidean space (see Equation
(85) of [92]). Since the rotation Rand the boost can be
interchanged, we have E(e;U) =Ri
Ei(e;U).
The family of static observers only determines a frame
outside the ergosphere. Therefore, we introduce another
Cartesian-like triad fx,fyandfzin the local rest space
of ZAMO for representation of the spin evolution inside
the ergosphere8asf=Ri
fi. Then the boost transfor-
mation results in E(f;U) =Ri
Ei(f;U).
The Cartesian-like triad components of the spin vector
in both the boosted SO and ZAMO frames are obtained
as
Si=Ri
S; (50)
which obeys the following equation of motion:
dSi
d= Ri
"
(prec)S
: (51)
Here the precession angular velocity is9
(prec)=
(p)+!; (52)
with
(p)=
(orb)+
; (53)
where
(orb)defined [see also Ref. [92]] as
R 1
jdRj
d="
(orb); (54)
8Note that the frame associated to the ZAMO moves with respect
to the distant stars.
9Note that that the expression of
(prec )reduces to -1 times that
of Ref. [92] for = 0.8
and= 0in the zero 3-momentum frame, while = 1
in the comoving frame. The angular velocity
(prec)de-
scribes the spin precession in the Cartesian-like frame.
The Cartesian-like triad components of
(prec)are ob-
tained from Equation (50) with notation change S!
(prec).
The quantity
(p)can also be expressed in terms of
the inner product of the Cartesian-like triad vectors Ei
and their derivatives along the considered worldline as
i
(p)Ri
(p)= 1
2"ijkEjDEk
d:(55)
This expression is analogous with Equation (37). The
angular velocities
i
(p)(e;U)and
i0
(p)(f;U)defined in
terms ofEi(e;U)andEi0(f;U), respectively, are related
by
Tk0
i
i
(p)(e;U) +Sk0
(orb)(e;U)
=
k0
(p)(f;U) +Rk0
(f)0
0
(orb)(f;U) +Sk0
(R);(56)
with
Tk0
i
R 1
(e)
iR0
Rk0
(f)0; Sk0
Rk0
(f)0R0
:(57)
Noting that !in Equation (43) transforms as a vec-
tor for real rotation R0
. The transformation rules for
(prec)and
i
(prec)follow from the definitions (52) and
(56).
IV. NUMERICAL INVESTIGATIONS
The orbit of the spinning body will be represented in
the coordinate space:
x=rcossin; y=rsinsin; z=rcos:(58)
We characterize the instantaneous plane of the motion in
the (x,y,z)-space by the unit vector:
l=RV
jRVj; (59)
whereis the cross product in Euclidean 3-space, R
is the position vector with components Rx=x,Ry=
y,Rz=z, and Vis a spatial velocity vector with10
Vx=dx
d; Vy=dy
d; Vz=dz
d: (60)The absolute value in the denominator denotes the “Eu-
clidean length” of the numerator. Since the considered
spacetimes are asymptotically flat, the quantity licoin-
cides with the direction of the orbital angular momen-
tum11at spatial infinity.
The initial data for the spin vector will be character-
ized by its magnitude and two angles in the boosted SO
Cartesian-like frame as
S=SiEi(e;u); (61)
with
Si=jSj
cos(S)sin(S);sin(S)sin(S);cos(S)
:
(62)
Since we use dimensionless quantities during the nu-
mericalinvestigation, theparameters ,a,mandMonly
appear through the ratios a=andm=M. We choose the
initial data set in the TD SSC as pa
(TD)=MandSa=M
(by Equation (62)), then the initial spin tensor is derived
from the inverse of (11), while m(0)=M(0)and the four
velocityua
(TD)of the centroid from (6).
The SSC choice determining the representative world-
line of a spinning test body corresponds to a gauge choice
in an action approach [113]. In the following we will con-
sider the evolution of the spin precessional angular ve-
locity and will check its dependence on the SSC choice.
For the numerical comparison, we will use the Frenkel–
Mathisson–Pirani (FMP) SSC which imposes uaSab= 0.
The definition of the spin vector is sa= abcdubScd=2,
which is Fermi-Walker transported along the worldline
of the centroid making the FMP SSC preferred from
mathematical point of view [114–116]. Its frame com-
ponents obey the same precessional equation in the co-
moving frame like the TD spin vector Sain the zero
3-momentum frame (13). In the FMP SSC, there ex-
ists also a velocity-momentum relation, Equation (19) of
Ref. [97], like in the TD SSC. Hence the initial data
set
xa;pa;Sab
jinprovides a unique solution of the
MPD equation with FMP SSC. However, we must men-
tion that, this velocity-momentum relation does not au-
tomatically ensure that uaSab= 0for arbitrary paand
Sab. In order to ensure this, we have a constraint be-
tween the four momentum and the spin tensor emerging
from the contraction of this equation with Sab. In ad-
dition, the data set
xa;pa;Sab
jincannot be inverted
for the set
xa;m;ua;Sab
jinlike in the TD SSC. One
needs the data set
xa;m;ua;Sab;aa
jinto fix the tra-
jectory. For a set
xa;m;ua;Sab
jin, we can obtain a
non-helical and infinite number of helical trajectories for9
Ω1(prec)(e,u)
Ω2(prec)(e,u)
Ω3(prec)(e,u)
50 100 150 200τ/μ
-0.010-0.0050.0050.0100.0150.020[1/μ]
Ω1(prec)(e,u)
Ω2(prec)(e,u)
Ω3(prec)(e,u)
50 100 150 200τ/μ
-0.010-0.0050.0050.0100.0150.020[1/μ]
Ω1(prec)(e,u)
Ω2(prec)(e,u)
Ω3(prec)(e,u)
50 100 150 200τ/μ
-0.010-0.0050.0050.0100.0150.020[1/μ]
Ω1(prec)(e,u)
Ω2(prec)(e,u)
Ω3(prec)(e,u)
5001000 1500 2000 2500τ/μ
-0.010-0.0050.0050.0100.0150.020[1/μ]
Ω1(prec)(e,u)
Ω2(prec)(e,u)
Ω3(prec)(e,u)
5001000 1500 2000 2500τ/μ
-0.010-0.0050.0050.0100.0150.020[1/μ]
Ω1(prec)(e,u)
Ω2(prec)(e,u)
Ω3(prec)(e,u)
5001000 1500 2000 2500τ/μ
-0.010-0.0050.0050.0100.0150.020[1/μ]
0500 1000 1500 2000 2500τ /μ0.0010.0020.0030.004Sin (Θ)
0500 1000 1500 2000 2500τ /μ0.0010.0020.0030.004Sin (Θ)
0500 1000 1500 2000 2500τ /μ0.0010.0020.0030.004Sin (Θ)
Figure 1: (color online). The evolution of spinning body moving on spherical-like orbits around the Kerr black hole with a= 0:5. From left to
right the magnitude of the body’s spin increases as jSj=M = 0:01,0:1and0:9. The rows represent the following: 1. the orbit in coordinate space
(x=,y=,z=) (the ergosphere of the central black hole is marked by blue and the initial and the final positions of the spinning body are denoted
by green and red dots, respectively,), 2. the instantaneous orbital plane orientation li(initial and final directions are marked by purple and black
arrows, respectively), 3. unit spin vector in the boosted SO comoving Cartesian-like frame Ei(e;u)(initial and final spin directions are marked
by green and blue arrows, respectively), 4. and 5.
(prec )(e;u)on shorter and longer timescales, respectively, 6. sin . The initial place of the
body isr(0) = 8,(0) ==2and(0) = 0. The direction of the initial spin vector is given by (S)(0) ==2and(S)(0) = 0in the boosted SO
frame (resulting in Sr(0)=jSj= 0:8682,S(0)=jSj= 0andS(0)=jSj= 0in Boyer-Lindquist coordinates). The four momentum pa
(TD)=M
is chosen for the TD SSC as pr
(TD)(0)=M(0) = 0,p
(TD)(0)=M(0) = 0:0442andp
(TD)(0)=M(0) = 0:0316. The initial centroid four velocity
ua
(TD)is determined from Equation (6).10
differentaa. In principle all worldlines where the condi-
tionsuaua= 1,uaSa= 0andpaSa= 0are satisfied
can be used for representation of the moving body. Since
the tangent vector of the centroid orbit occurs in the spin
precessional equation through EAand their derivatives,
the spin axis may describe very complicated motion in
such observer’s frame, which follows a helical trajectory.
In order to characterize the self rotation of the body in
the easiest way possible, the helical trajectories should
be avoided. However, there is no generic rule for deter-
mination of the non-helical trajectory. According to the
Authors’ knowledge, the best ansatz is suggested in Ref.
[115] as taking
pa=mua+SabFb
m: (63)
In this case aa/Fa=mat leading order in spin, which is
plausible for a non-helical trajectory since aa/O
S 1
for the helical ones. However, the ansatz (63) cannot
be imposed as a constraint for the dynamics with signifi-
cant spin magnitude in the consideration. We require the
ansatz (63) for setting initial conditions in the numeri-
cal investigations. This is not forbidden because (63) is
consistent with the algebraic velocity-momentum equa-
tion. The corresponding initial data set in the FMP SSC
are chosen by identifying the initial centroid four velocity
and spin vector as ua
(FMP )=ua
(TD)andsa=m=Sa=M.
Then the initial spin tensor and pa
(FMP )=mare computed
fromSab=ab
cducsdand(63),respectively. Bringingfor-
ward the result of the SSC dependence, we have found
that the evolutions of the spin vectors defined in the TD
and the FMP SSCs are barely distinguishable from each
other in all cases. The differences in the evolutions of
the different considered quantities considered in the sub-
sequent subsections remains below 1%. This is in agree-
ment with result of Ref. [117], where the evolution of
test bodies moving on circular equatorial orbits around
a Schwarzschild black hole were investigated.
A. Spinning bodies moving in the Kerr spacetime
In this subsection, we set em= 0anda= < 1, i.e.
the background is a Kerr black hole’s spacetime. Figure
1 shows spherical-like orbits. The initial values are listed
in the caption. The orbits, the black curves in the upper
row, are shown in the coordinate space ( x=,y=,z=)
defined in Equation (58). The initial and the final po-
sitions of the body are marked by green and red dots,
respectively. The initial position is in the equatorial
plane(0) ==2atr(0) = 8and(0) = 0. The
blue surface at the center depicts the outer bound of the
Kerr black hole’s ergosphere. In the columns from left
to right, the spin magnitude jSj=Mvariates as 0:01,
0:1and0:9, respectively, while the other initial values
are fixed. For small spin, the orbit is spherical ( _r= 0)
and reproduces Figure 3 of [92]. For higher spins (secondand third columns) the orbit becomes less and less spher-
ical, but because of _r1, it is spherical-like. On the
purplish spheres in the second row, the evolutions of the
kinematical quantity defined in Equation (59) are shown
under the corresponding orbits. Their initial and final di-
rections are marked by purple and black arrows, respec-
tively. The evolution of this vector clearly shows that the
increasing spin magnitude due to the nonvanishing spin-
curvaturecoupling(i.e. thenon-vanishingrighthandside
of Equation (1)) in the spin precession, which was not in-
cluded in the investigation of Ref. [92]) affects the orbit.
On the greenish spheres in the third row, the evolutions
of the spin direction are represented in the boosted SO
frameEi(e;u). The initial and final spin directions are
marked by green and blue arrows, respectively. In Boyer-
Lindquist coordinates, the initial spin four vector Sahas
only non-vanishing component Sr. The fourth and fifth
rows image the evolutions of spin precessional angular
velocity
(prec)(e;u)on shorter and longer timescales,
respectively. For jSj=M = 0:01, the frame compo-
nents of this angular velocity oscillates (see also Figure
3 of Ref. [92] and remembering for that the definition
of
(prec)carries an extra sign). For jSj=M = 0:1
and0:9, an amplitude modulation occurs. This is also
a clear sign of the spin-curvature effect. We mention
that, the evolution of
(prec)(f;u)differs less than 1%
from that of
(prec)(e;u). This is because the boosted
SO and ZAMO frames are almost the same, i.e. the ro-
tation angle between them is small as shown in the
last row. We also mention that, all precessional angular
velocities
(prec)(e;p=M ),
(prec)(e;u),
(prec)(f;p=M )
and
(prec)(f;u)in the frames E(e;p=M ),E(e;u),
E(f;p=M )andE(f;u), respectively, describe the
same evolutions within 1%. The Boyer-Lindquist com-
ponents of the spin vector are frame independent quan-
tities. Their evolutions are presented on Figure 2. The
blue, the green and the red curves belong to the different
spin magnitude cases jSj=M = 0:01,jSj=M = 0:1and
jSj=M = 0:9, respectively. An amplitude modulation
due to the spin-curvature coupling occurs in the oscil-
lation around a harmonic evolution of the -component,
which can be mostly seen along the red curve.
In the following, we will consider zoom-whirl and un-
bound orbits passing over the ergosphere. In all cases
we choose such initial conditions that the body moves in
theequatorialplanefornegligiblespinmagnitude. Hence
the deviation of the trajectory from this plane is a clear
sign of the spin-curvature effect. Zoom-whirl orbits of a
nonspinning test body around a spinning black hole were
already investigated in Refs. [69–73]. Those orbits did
not passed through the ergosphere for which we will fo-
cus. In addition, when the test body is spinning, some
effects from the spin-curvature coupling are waited which
we will consider. In addition, zoom-whirl orbits of com-
parable mass black holes, when only one of them is spin-
ning, were analyzed in Ref. [80] within the framework of
PN approximation. Hyperbolic orbits of spinning11
200 400 600 800 1000 1200 1400τ/μ
-0.4-0.20.20.4St/|S|
200 400 600 800 1000 1200 1400τ/μ
-0.50.5Sr/|S|
200 400 600 800 1000 1200 1400τ/μ
-0.10-0.050.050.10μSθ/|S|
200 400 600 800 1000 1200 1400τ/μ
-0.2-0.10.10.2μSϕ/|S|
Figure 2: (color online). The evolutions of the Boyer-Lindquist coordinate components of the unit spin vector are shown. The blue and the green
curves belonging to the spin magnitude jSj=M = 0:01andjSj=M = 0:1, respectively, almost cover each other. The red curve represents the
high spin magnitude case jSj=M = 0:9. An amplitude modulation occurs in the oscillation around a harmonic evolution of the -component
which can be mostly seen along the red curve.
5 10 15ρμ
-3-2-1123z/μ
5 10 15ρμ
-3-2-1123z/μ
Figure 3: (color online). The evolution of spinning body moving on zoom-whirl orbits around the Kerr black hole with a= 0:99. The magnitudes
of the body’s spin are jSj=M = 0:01(left panel) and 0:1(right panel). The rows represent the following: 1. the orbit in coordinate space
(x=,y=,z=) (outer and inner bounds of the ergosphere of the central black hole is marked by blue and red surfaces, respectively, and initial and
final positions of the spinning body are denoted by green and red dots, respectively), 2. the orbit in the coordinate space ==rsin=and
z==rcos=with marked initial and final positions and bounds of the ergosphere, 3. the unit spin vector in the boosted SO Cartesian-like
comoving frame Ei(e;u)on a shorter timescale including the first whirling period, and 4. the unit spin vector in the boosted ZAMO Cartesian-like
comoving frame Ei(f;u)on the total timescale (initial and final spin directions are marked by green and blue arrows, respectively). The initial
data set:t(0) = 0,r(0) = 14:05,(0) ==2,(0) = 0,pr(0)=M= 0:03,p(0)=M= 0,p(0)=M= 0:012,(S)(0) ==2and(S)(0) = 0
(the spatial Boyer-Lindquist coordinate components are Sr(0)=jSj= 0:9293,S(0)=jSj= 0andS(0)=jSj= 0:0002).12
0 100 200 300 400τ /μ0.0050.010.015Sin (Θ)
0 100 200 300 400τ /μ0.0050.010.015Sin (Θ)
Ω1(prec)(f,u)
Ω1(prec)(e,u)
100 200 300 400τ /μ
-0.008-0.006-0.004-0.0020.0020.004[1/μ]
Ω1(prec)(f,u)
Ω1(prec)(e,u)
100 200 300 400τ/μ
-0.08-0.06-0.04-0.020.020.04[1/μ]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
100 200 300 400τ/μ0.20.40.60.8[1/μ]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
100 200 300 400τ/μ0.20.40.60.8[1/μ]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
100 200 300 400τ/μ
-0.006-0.004-0.0020.0020.004[1/μ]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
100 200 300 400τ/μ
-0.06-0.04-0.020.020.04[1/μ]
Figure 4: (color online). The left and right columns belong to the same evolution which are shown on Figure 3. The first row shows sin . The
next three rows present the evolutions of the spherical triad components of the spin precessional angular velocities
(prec )(e;u)and
(prec )(f;u).
test bodies based on the MPD equations were analyti-
cally studied in Ref. [83]. The perturbations caused by
the spin-curvature coupling in the equatorial orbits were
considered in the case when the spin is parallel to the
central black hole rotation axis. In this configuration the
spin vector is conserved. Here, in order to discuss non-
trivial spin evolution and spin-curvature coupling effects,
we choose the initial spin direction to be perpendicular
to the central black hole rotation axis.
ThefirstrowofFigure3showstheorbitsinthe( x,y,z)-
space for increasing spin magnitude jSj=M = 0:01(left
panel) and 0:1(right panel). The other initial values
listed in the caption are the same. The blue and red sur-
faces at the center depict the outer and interior bounds
of the ergosphere, respectively (i.e. the outer stationarylimit surface and the outer event horizon). The initial
and final positions of the body are marked by green and
red dots, respectively. The initial position is in the equa-
torial plane (0) ==2atr(0) = 14:05and(0) = 0,
and both the initial four momentum and centroid four
velocity have vanishing -component. With this initial
location and four velocity a non-spinning particle moves
in the equatorial plane. However, since the spin direction
is not parallel with the rotation axis of the central black
hole, the body’s centroid leaves the equatorial plane due
to the effect of spin-curvature coupling. This is high-
lighted in the second row representing the orbits in coor-
dinates==rsin=andz==rcos=. The bounds
of the ergosphere are drawn by blue and red curves. The
body is inside the ergosphere when it whirls around the13
100 200 300 400τ/μ
-2-1123St/|S|
100 200 300 400τ/μ
-1.0-0.50.51.0Sr/|S|
100 200 300 400τ/μ
-0.10-0.05μSθ/|S|
100 200 300 400τ/μ
-1.0-0.50.51.0μSϕ/|S|
μ
SdSt
dτ
100 200 300 400τ/μ
-0.50.5
μ
SdSr
dτ
100 200 300 400τ /μ
-0.2-0.10.10.2
μ2
SdSθ
dτ
100 200 300 400τ/μ
-0.04-0.020.020.04
μ2
SdSϕ
dτ
100 200 300 400τ/μ
-0.4-0.20.20.4
St
S
μ
SdSt
dτ
60 65 70 75 80τ /μ
-0.50.51.01.52.02.5
Sr
S
μ
SdSr
dτ
60 65 70 75 80τ/μ
-0.6-0.4-0.20.20.40.60.8
μSθ
S
μ2
SdSθ
dτ60 65 70 75 80τ/μ
-0.10-0.08-0.06-0.04-0.020.02
μSϕ
S
μ2
SdSϕ
dτ
60 65 70 75 80τ/μ0.51.0
Figure 5: (color online). The evolution of the Boyer-Lindquist coordinate components of the unit spin vector and their derivatives rescaled to
dimensionless variables is presented for that case which is shown on the right hand sides of Figures 3 and 4. The first and the second rows show
the evolution on a timescale which includes the first three whirling period when the body is inside the ergosphere. The third row zooms in on that
evolution period where the body is first in the ergosphere which is indicated by the purplish shadow on all panels. In the first row, the black and
the red curves represent the evolutions without and with spin-curvature coupling, respectively.
central Kerr black hole. This happens during all whirling
period. The unit spin vector evolutions in the boosted
SO Cartesian-like comoving frame ( Ei(e;u)) during a
timescale including the first whirling period are shown
in the third row. The initial and final directions are
marked by green and blue arrows, respectively. The
rotation of the projection of spin vector in the plane
(Ex(e;u),Ey(e;u)) is counterclockwise in both cases.
In the boosted SO frame the evolution is not contin-
uous due to the motion through the ergosphere. The
black dots denote the spin directions when the body
first enters and leaves the ergosphere. The magnitude
of the jump shows that the spin direction changed sig-
nificantly inside the ergosphere. The fourth row shows
the unit spin vector evolution on the total timescale
in the boosted ZAMO Cartesian-like comoving frame
(Ei(f;u)). This frame can be used for the spin repre-
sentation inside the ergosphere, hence the evolution is
continuous. For higher spin, when the spin-curvature
coupling is stronger the deflection of the spin direction
moves more out of the equatorial plane of ZAMO frame.
The first row in Figure 4 shows the rotation angle
between the boosted SO and ZAMO frames. Here and
in the following pictures the purplish shadow indicates
the time interval where the body moves inside the ergo-
sphere during the first whirling period. The next three
rows in Figure 4 depict the evolutions of
(prec)(e;u)
and
(prec)(f;u). Each row shows one component of
these angular velocities. The red and blue curves rep-
resent the precessional angular velocities in the boosted
ZAMO and SO frames, respectively. The blue curves
diverge at the ergosphere where the description in theboosted SO frame fails. The magnitude of the preces-
sional angular velocities rapidly increases near and in-
side the ergosphere and becomes higher for higher spin
magnitude. Finally, we note that the precessional veloc-
ities
(prec)(e;p=M )(
(prec)(f;p=M )) and
(prec)(e;u)
(
(prec)(f;u)) describe the same evolutions within 1%.
From the consideration of the moving body near and
inside the ergosphere, we have found that the spin pre-
cession was highly increased. Since the presented inves-
tigation was based on the introduction of ZAMO, and
the precessional angular velocity
(prec)(f;u)described
the spin evolution with respect to the boosted ZAMO
frame, the highly increased precession effect could be an
observer dependent statement. However, this effect is
supported in another way. The static observers play fun-
damentalroleincomparingthevariationofspindirection
with respect to the distant stars. The third row of Figure
3showsintheboostedSOframethatthejumpofthespin
direction (between the black dots) happening during that
period when the body is staying first in the ergosphere.
This jump happens during relatively short period indi-
cated by the purplish shadow on Figure 4. More exactly,
the evolution period presented in the third row of Fig-
ure 3 is given by = [0;94:7]from which the body is
inside the ergosphere in the interval = [68:6;73:4].
The evolution of the spin together with these timescales
result in the same conclusion that the precession angular
velocity is highly increased in the ergosphere. In addi-
tion, this effect can also be supported without using any
particular reference frame. For the case presented on the
right hand side of Figure 4, we show the evolution of the
Boyer-Lindquist coordinate components of the unit14
5 10 15ρμ
-3-2-1123z/μ
5 10 15ρμ
-3-2-1123z/μ
Ω1(prec)(f,u)
Ω1(prec)(e,u)
100 200 300 400τ /μ
-0.06-0.04-0.020.020.040.06[1/μ]
Ω1(prec)(f,u)
Ω1(prec)(e,u)
100 200 300 400τ /μ
-0.06-0.04-0.020.020.040.06[1/μ]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
100 200 300 400τ/μ0.20.40.60.8[1/μ]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
100 200 300 400τ/μ0.20.40.60.8[1/μ]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
100 200 300 400τ /μ
-0.050.05[1/μ]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
100 200 300 400τ /μ
-0.050.05[1/μ]
Figure 6: (color online). The same as on the right column of Fig-
ures 3 and 4 (apart from sin ), but the initial direction of the spin
vector is rotated by =2(left column) and by =2(right column).
(The spatial Boyer-Lindquist coordinate components of the spin vec-
tor areSr(0)=jSj= 0:0025(left column), 0:0025(right column),
S(0)=jSj= 0(both left and right columns) and S(0)=jSj=
0:0720(left column), 0:0720(right column).
spin vector and their derivatives rescaled to dimen-
sionless variables on Figure 5. The first and the second
rows represent the evolution on a timescale which in-
cludes the first three whirling period when the body isinside the ergosphere. The third row zooms in on that
evolution period where the body is first inside the ergo-
sphere. As mentioned, this period is indicated by the
purplish shadow. All panels of Figure 5 confirm that the
rate of change in the direction of the spin vector is highly
increased near and inside the ergosphere. As a reference,
the black curves in the first row represent the evolution
of the unit spin coordinate components when the spin-
curvature coupling is turned off. While the red curves
show the evolutions when the spin-curvature coupling is
taken into account. Significant differences in the evolu-
tions can be seen in the case of the randcoordinate
components. The coordinate component identically
vanishes when the spin-curvature coupling is neglected.
Finally, we mention that since paanduaare not parallel
with each other it may happen that uaua= 0[51, 66–
68] orpaua= 0[118–120]. The first case was discussed
previously in Section IIA. The second case is equivalent
with becoming the momentum light-like papa= 0, which
can be seen from the contraction Equation (6) with pa.
We have checked in the Appendix VIII that the MPD
equations are applied only in that domain where such
pathological behaviours do not occur.
When the initial direction of the spin vector is oppo-
site with respect to the case presented in the Figures 3
and 4, while all other initial conditions are the same, we
have found the following. The centroid trajectory be-
comes the reflection of the orbit presented on Figure 3
through the equatorial plane. The instantaneous direc-
tions of the spin vector in the boosted SO (ZAMO) frame
can be obtained from the corresponding picture of Fig-
ure 3 by a rotation with an angle about the axis zand
Ez(e;u)(Ez(f;u)), respectively. The angle describes
thesameevolution. Finally, thecomponents
2
(prec)(e;u)
and
2
(prec)(f;u)remain unchanged, while
1
(prec)(e;u),
1
(prec)(f;u),
3
(prec)(e;u)and
3
(prec)(f;u)get an extra
sign.
On Figure 6, the initial spin direction is rotated by
=2(left column) and =2(right column) in the plane
(Ex(e;u),Ey(e;u)) with respect to the case presented
on Figure 3. These two cases have opposite initial spin
directions leading to the following differences in the orbit
and spin evolutions. The zoom-whirl orbit on the right
hand side is the reflection of the trajectory on the left
hand side through the equatorial plane, which are shown
in the first two rows. The spin the evolutions presented
on the left and the right hand sides in the third and
fourth rows are related to each other by a rotation with
an angleabout the axis connecting the south and north
poles. The evolution of
2
(prec)are the same on the left
and right hand sides, while
1
(prec)and
3
(prec)have a
sign difference, as it can be seen in the last three rows.
For the consideration of evolutions of spinning bodies
which follow unbound orbits crossing through the ergo-
sphere, the spin magnitude is chosen as jSj=M = 0:1.
The initial spin directions on the left (right) hand side of
Figure 7 are the same as on Figure 3 (on the left hand15
123456ρμ
-1.5-1.0-0.50.51.01.5z/μ
123456ρμ
-1.5-1.0-0.50.51.01.5z/μ
Figure 7: (color online). The evolutions of spinning body moving on unbound orbits around Kerr black hole with a= 0:99. The spin magnitude
chosen asjSj=M = 0:1. The considered unbound orbits are shown in the first row. The near black hole parts of these orbits are represented
in the second and third rows in ( x=,y=,z=) and (=,z=) coordinates, respectively. The fourth and fifth rows present the evolutions of
the spin vector in the boosted SO and ZAMO frames, respectively. The initial spin direction is determined by (S)(0) = 0 (left col.),=2
(right col.) and (S)(0) ==2(both cols.). The spatial Boyer-Lindquist coordinate components [ Sr(0),S(0),S(0)]=jSjof the spin vector
are [ 0:0134,0, 3:110 9] and [ 0:000006,0,0:000005] in the left and right columns, respectively. Additional initial data set is t(0) = 0,
r(0) = 2000,(0) ==2,(0) = 0,pr(0)=M= 0:9,p(0)=M= 810 7andp(0)=M= 0. The final locations [ t()=,r()=,(),()]
at= 4433are [6033:2,1999:7,1:527,14:24] (left col.) and [ 6033:3,1999:7,1:671,14:25] (right col.). The final values of the spatial Boyer-
Lindquist coordinate components [ pr(),p(),p()]=Mof the four momentum are [ 0:900002, 7:6510 8,8:0010 7] (left col.) and
[0:900003, 3:4810 8,8:0110 7] (right col.). The final values of the spatial Boyer-Lindquist components [ Sr(),S(),S()]=jSjof the
spinvector are [ 0:86, 2:910 5,3:810 4] (left col.) and [ 1:11, 8:610 5,2:710 4] (right col.). The final spin directions [ (S)(),(S)()]
in the boosted SO frame are determined by [ 1:48, 0:59] (left col.) and [ 1:31,1:09] (right col.). The angles [ (l)(),(l)()] characterizing the
final orbital plane orientations in coordinate space ( x=,y=,z=) are [ 0:11, 0:33] (left col.) and [ 0:11,1:27] (right col.).16
side of Figure 6). The first row depicts the unbound or-
bits in the ( x,y,z)-space. The initial data set is chosen
atr(= 0) = 2000 where the body is in the equatorial
plane ((= 0) ==2and(= 0) = 0 ) and the cen-
troid four velocity has vanishing -component. We nu-
merically checked that r!1as!1. Second and
third rows represent the orbits near the black hole in the
(x,y,z)andthe(,z)spaces, respectively. Theintervalfor
is determined by 5before and +5after the body
crossed the outer stationary limit surface. As the body
penetrates the ergosphere, it makes two turns around the
black hole, then it leaves the ergosphere going to the
spatial infinity. These evolutions describe such scatter-
ing processes where the center is extremely approached.
The deviation of the trajectory from the equatorial plane
is an effect of the spin-curvature coupling. The fourth
and fifth rows image the evolutions of the unit spin vec-
tor represented in the boosted SO and ZAMO frames,
respectively. The deviation of the spin vector direction
from the equatorial plane also occurs because of the spin-
curvaturecoupling. Thejumpintheevolutionofthespin
vector in the boosted SO frame (marked by black dots)
shows that the variation of spin direction takes place
mainly inside the ergosphere. The large part of the vari-
ation of spin direction happens during that period when
the body is inside the ergosphere. This time interval is
2[2214:8;2218:6]which is short with respect to the
considered total evolution period = [0;4433]. The fi-
nal value of the proper time = 4433was chosen in
such a way, that for >the spin angles undergo only
unsignificant changes. Figure 8 presents the evolutions
of
(prec)(e;u)and
(prec)(f;u)for that time interval
which is determined by 25before and +25after the
body crossed the outer stationary limit surface. The pur-
plish shadow denotes that period when the body is inside
the ergosphere where the spin precessional angular veloc-
ity components increases.
The spin-curvature coupling mainly influences the
smaller components of the precessional angular velocity
1
(prec)(f;u)and
3
(prec)(f;u), as it can be seen in the
first row of Figure 9. The black curve represents the evo-
lutions without the spin-curvature coupling. In the case
of the red curves, the spin-curvature coupling is taken
into account, and they are the same as in the second col-
umn of Figure 8. The spin-curvature coupling increases
the amplitude of the precessional angular velocity com-
ponents.
The reparametrization invariance of the representative
worldline also implies a gauge freedom [121]. Usually,
the following choices for this timelike parameter are ap-
plied in the literature: i)the proper time ( uaua= 1)
[51, 92] also used in this paper; ii)the parameter deter-
mined by the normalization uapa=M= 1[122, 123];
iii)the coordinate time t[96, 124]. Employing the TD
SSC, considerable differences were not found in both the
orbit and the spin dynamics when using the parameters
eitheri)orii)[64]. The orbit and the spin evolutions
are unaffected when using the coordinate time tinstead
of the proper time . However, the precessional angularvelocity is changed for
(prec)=u0which is shown in the
second row of Figure 9 as a function of t. The black and
the red curves represent the evolution without and with
the spin-curvature coupling. We can conclude the same
effects when we have considered the spin evolution with
respect to the proper time.
The relatively rapid change in the direction of the spin
vector can also be confirmed without using any partic-
ular reference frame. In the first row of Figure 10, we
present the evolutions of the Boyer-Lindquist coordinate
components of the unit spin vector for the case imaged
on the right hand sides of Figures 7 and 8. The spin-
curvature coupling is included in the evolutions depicted
by the red curves. The black curves represent the corre-
spondingevolutionswhenthiscouplingisturnedoff. The
effect of the spin-curvature coupling can be seen in the
evolution of St,SrandScomponents. The latter van-
ishes identically in the absence of the spin-curvature cou-
pling. However, if the spin-curvature coupling is included
in the analysis, the Scomponent deviates significantly
fromzerowhenthebodyisclosetothecentralblackhole.
In addition, the effect of the spin-curvature coupling re-
mains in the StandSrcomponents far from the cen-
tral black hole. They approach another constant values
when the spin-curvature coupling is taken into account.
The evolutions of the components of the unit spin vector
and their derivatives rescaled to dimensionless variables
on a smaller timescale, when the spinning test body is
close the central black hole are represented in the second
row. All panels supports a relatively rapid change of the
spin vector near and inside the ergosphere. Finally, we
mention that the MPD equations were applied only in
its validity domain, this check is given in the Appendix
VIII.
In a wider range of initial conditions, the final values of
the polar(S)and azimuthal (S)spin angles (the scat-
tering angles) are represented on Figure 11 as functions
of gauge invariant, dimensionless energy ^E=E=Mand
angular momentum ^Jz=Jz=M. The small black dots
in the plane of the initial spin angles ( (S)(0) ==2and
(S)(0) = 0) indicate the region, where the body crosses
the event horizon of the Kerr black hole. Then, instead
of a scattering process, the body falls into the black hole.
Close to the left corner, i.e. at smaller ^Eand higher ^Jz
values, the body approaches the central black hole less
than for higher ^Eand/or for smaller ^Jzvalues. As a con-
sequence, the precession and hence the variation of the
spin angles are both small. However, close to the diago-
nal in the ^E,^Jzplane indicated by the edge of the black
dots region, the body enters into the ergosphere, and
due to the high precession there, the spin angles undergo
a relatively large change. In all case, the initial values
are chosen such that, if the spin-curvature coupling is
neglected, the polar angle (S)remains=2during the
whole evolution, and the spin precession influences only
(S). Hence, the variation of (S)shown on the left panel
is a clear effect of the spin-curvature coupling. We17
Ω1(prec)(f,u)
Ω1(prec)(e,u)
2200 2210 2220 2230 2240τ/μ
-0.10-0.050.05[1/μ]
Ω1(prec)(f,u)
Ω1(prec)(e,u)
2200 2210 2220 2230 2240τ/μ
-0.10-0.050.05[1/μ]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
2200 2210 2220 2230 2240τ/μ0.51.01.52.02.5[1/μ]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
2200 2210 2220 2230 2240τ/μ0.51.01.52.02.5[1/μ]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
2200 2210 2220 2230 2240τ /μ
-0.050.05[1/μ]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
2200 2210 2220 2230 2240τ /μ
-0.050.05[1/μ]
Figure 8: (color online). On the left and right columns the evolutions of the spherical triad components of the spin precessional angular velocities
are presented along those orbits which are shown in the left and right columns of Figure 7, respectively.
2200 2210 2220 2230 2240τ/μ
-0.10-0.050.05Ω1
(prec) (f,u)[1/μ]
2200 2210 2220 2230 2240τ/μ0.51.01.52.02.5Ω2
(prec) (f,u)[1/μ]
2200 2210 2220 2230 2240τ/μ
-0.050.05Ω3
(prec) (f,u)[1/μ]
2990 3000 3010 3020 3030 3040 3050t/μ
-0.010-0.0050.005Ω1
(prec) (f,u)/u0
2990 3000 3010 3020 3030 3040 3050t/μ0.050.100.150.200.250.30Ω2
(prec) (f,u)/u0
2990 3000 3010 3020 3030 3040 3050t/μ
-0.010-0.0050.0050.010Ω3
(prec) (f,u)/u0
Figure 9: (color online). In the first line, the black and the red curves show the precessional angular velocity spherical frame components without
and with spin-curvature coupling, respectively. The second line shows them when the spin evolution is considered as a function of the coordinate
timet. These evolutions belong to the case which is presented in the right hand sides of Figures 7 and 8.
mention that, both functions (S)and(S)steeply in-
crease as approaching the edge of the black dots region.
Those maxima, which can be seen on the panels, belong
to the chosen grid in the ^E,^Jzplane.
B. Spinning bodies moving on zoom-whirl orbits in
rotating regular black hole spacetimes
In this subsection, we set = 0,
= 3anda=
0:99em. The background is either a regular, rotatingBardeen-like ( = 2) or Hayward-like ( = 3) black hole
spacetime. For = 2and= 3, the spacetime contains
a black hole for q0:081andq0:216, respectively.18
2000 2200 2400 2600τ/μ
-6-5-4-3-2-1St/|S|
2400 2600-0.74-0.72-0.70
2000 2200 2400 2600τ/μ
-1.0-0.50.5Sr/|S|
2000 2200 2400 2600τ/μ
-0.20-0.15-0.10-0.05μSθ/|S|
2000 2200 2400 2600τ/μ
-2.5-2.0-1.5-1.0-0.5μSϕ/|S|
2210 2215 2220 2225τ/μ
-6-4-22St/|S|
2210 2215 2220 2225τ/μ
-1.0-0.50.5Sr/|S|
2210 2215 2220 2225τ/μ
-0.20-0.15-0.10-0.050.050.10μSθ/|S|
2210 2215 2220 2225τ/μ
-2-11μSϕ/|S|
Figure 10: (color online). In the first line, the black and the red curves present the Boyer-Lindquist coordinate components of the unit spin vector
without and with spin-curvature coupling. In case of St, the relatively small deviation of the curves when the test body is moving away from
the central black hole is shown in a small box. The second line presents the evolutions of the unit spin vector and their derivatives rescaled to
dimensionless variables when the spinning test body is close to the central black hole. These evolutions belong to the case, which is presented in
the right hand sides of Figures 7 and 8 and also in Figure 9. The time interval, when the body is inside the ergosphere, is indicated by a purplish
shadow on all panels.
Figure 11: (color online). The left and right panels present the final value of the spin angles (S)()and(S)(), respectively, as functions of
the dimensionless energy ^E=E=Mand angular momentum ^Jz=Jz=M. The final values were computed at = 4433. We have checked that
the spin angles undergo only unsignificant changes for > . The initial spin is given by jSj=M = 0:1,(S)(0) ==2and(S)(0) = 0. The
initial momentum has vanishing component: p(0)=M= 0, and its additional components were determined from ^E,^Jzandpapa=M2= 1.
The small black dots in the plane of the initial spin angles represent the region, where the body crosses the event horizon of the Kerr black hole,
hence, unbound orbits do not develop.
We consider three cases: ( = 2,q= 0:081), (= 3,q=
0:081) and (= 3,q= 0:216). For these parameters the
regular black holes have two stationary limit surfaces and
event horizons. In addition, the spin magnitude for the
moving body is chosen as jSj=M = 0:1.
On Figure 12, zoom-whirl orbits in different regular ro-
tating black hole spacetimes are presented. The columns
from left to right correspond to ( = 2,q= 0:081),
(= 3,q= 0:081) and (= 3,q= 0:216). With the
notation change !em, the initial values are chosen
the same as in the second column of Figure 3. Each row
represents the same quantity which was shown on Fig-
ure 6. The first two columns show that both the orbit
and the spin evolutions are significantly different in the
cases of the Bardeen-like and Hayward-like black holes
for the same emandqvalues. In addition, the second
and the third columns show in the case of Hayward-like
backgroundthattheseevolutionsarealsosensitiveforthe
value ofq. The way of deviation of the orbit from the
equatorial plane, which is the effect of the spin-curvaturecoupling, is also very sensitive for the parameters of the
regular black holes. The spin vector evolutions includ-
ing the first whirling period in the boosted SO frame is
presented in the third row. The black dots represent a
jump in the evolution. The part of the evolution which is
not shown takes place inside the ergosphere. The amount
of the jumps is somewhat different for each cases. The
fourth row shows the total evolution of the spin vec-
tor in the boosted ZAMO frame. The final directions
(blue arrows) of the spin direction are significantly differ-
ent. The evolutions of the spherical frame components of
the precessional angular velocity including the first three
whirling period are shown in the last three rows. These
are perturbatively different for the different regular black
holes. However, the effects of these small differences add
up over the evolution.
Finally, we mention that a consideration of unbound
orbits about regular black holes can be found in Ref.
[125].19
5 10 15ρμem
-3-2-1123z/μem
5 10 15ρμem
-3-2-1123z/μem
5 10 15ρμem
-3-2-1123z/μem
Ω1(prec)(f,u)
Ω1(prec)(e,u)
100 200 300 400τ/μem
-0.08-0.06-0.04-0.020.020.04[1/μem]
Ω1(prec)(f,u)
Ω1(prec)(e,u)
100 200 300 400τ/μem
-0.08-0.06-0.04-0.020.020.04[1/μem]
Ω1(prec)(f,u)
Ω1(prec)(e,u)
100 200 300 400τ/μem
-0.08-0.06-0.04-0.020.020.04[1/μem]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
100 200 300 400τ /μem0.20.40.60.8[1/μem]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
100 200 300 400τ /μem0.20.40.60.8[1/μem]
Ω2(prec)(f,u)
Ω2(prec)(e,u)
100 200 300 400τ /μem0.20.40.60.8[1/μem]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
100 200 300 400τ/μem
-0.06-0.04-0.020.020.040.06[1/μem]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
100 200 300 400τ/μem
-0.06-0.04-0.020.020.040.06[1/μem]
Ω3(prec)(f,u)
Ω3(prec)(e,u)
100 200 300 400τ/μem
-0.06-0.04-0.020.020.040.06[1/μem]
Figure 12: (color online). Zoom-whirl orbits are represented around regular, rotating black holes with
= 3anda= 0:99em. The first column
shows the orbit around a Bardeen-like black hole ( = 2) while the middle and the last around a Hayward-like black hole ( = 3). The parameter
qis0:081in the first two columns while 0:216in third one. Applying the notation change !em, the initial values are chosen the same as in
the second column of Figure 3. The quantities in each line are the same which are presented in Figure 6.20
V. CONCLUSIONS
Wehaveconsiderednumericallytheevolutionofaspin-
ning test body governed by the MPD equations, mov-
ing along spherical-like, zoom-whirl and unbound orbits
around a Kerr black hole. When the spacetime curva-
ture and the spin contributions on the right hand sides
of the MPD equations can be neglected, we recovered the
corresponding results of Ref. [92] for a spherical orbit.
However, for higher spin, an amplitude modulation oc-
cured in the harmonic evolution of the spin precessional
angular velocity caused by the spin-curvature coupling.
This amplitude modulation also occured in the Boyer-
lindquist coordinate component of the spin vector.
Theexistenceofzoom-whirlorbitsareconfirmedbyus-
ing the MPD dynamics. The considered zoom-whirl and
unbound orbits of spinning body passed over the ergo-
sphere, where the PN approximation cannot be applied.
In all cases the numerical investigations showed that the
spin precessional angular velocity highly increased near
and inside the ergosphere. Thus the direction of the spin
vector is significantly variated during the evolutionary
phase inside the ergosphere. The initial values were cho-
sen such that the test body moved in the equatorial plane
when the spin-curvature coupling is neglected. Hence,
the effect of this coupling occured as a deviation of the
orbit from the equatorial plane. In order to investigate
non-trivial spin evolution, the initial spin direction was
chosen to be perpendicular to the rotation axis of the
central black hole. Then, the spin vector evolved in the
equatorial plane of the boosted SO and ZAMO frames
when the spin-curvature coupling is neglected. The de-
viation of the spin vector from this equatorial plane was
also the effect of the spin-curvature coupling. Additional
effects of the spin-curvature coupling was observed in the
evolutions ofthespin precessionalangularvelocityandof
the Boyer-Lindquist coordinate components of the spin
vector.Zoom-whirl orbits and spin precession including the
spin-curvature coupling were also considered in regular
spacetimes containing a central rotating black hole. Sig-
nificant differences were observed in the way of deviation
oftheorbitfromtheequatorialplanewhichweresensitive
for the parameters of the regular black hole. Small devi-
ations were found in the spin precession angular velocity,
which add up over the evolutions. Hence, the direction
of the final spin vector can be very different for different
parameters of the regular black hole.
Finally, wementionthatthenumericinvestigationpre-
sentedherecouldbegeneralizedinthefollowingway. Be-
sides the spin-curvature coupling another effects would
occur if the backreaction of the body to the metric was
not neglected. This backreaction appears as a self-force
in the equation of motion [126–129], and also causes a
deviation from the geodesic orbit like the spin-curvature
coupling.
Acknowledgements
The work of B. M. was supported by the János Bolyai
Research Scholarship of the Hungarian Academy of Sci-
ences. The work of Z. K. was supported by the János
Bolyai Research Scholarship of the Hungarian Academy
of Sciences, by the UNKP-18-4 New National Excellence
Program of the Ministry of Human Capacities and by the
Hungarian National Research Development and Innova-
tion Office (NKFI) in the form of the grant 123996.
VI. CONFLICT OF INTEREST
The authors declare no conflict of interest.
VII. APPENDIX A: THE RELATION
BETWEEN THE FRAMES E(e; U )AND E(f; U )
The frame vectors E(e;U)derived from the SO’s frame are the following linear combination of E(f;U):
E1(e;U) =E1(f;U) + (Z)w1
(Z)
1 + (S)"
aBsinp gttAE3(f;U) +
1 s
gttA!
(Z)w(Z)
1 + (Z)#
;
E2(e;U) =E2(f;U) + (Z)w2
(Z)
1 + (S)"
aBsinp gttAE3(f;U) +
1 s
gttA!
(Z)w(Z)
1 + (Z)#
;
E3(e;U)= s
gttA+ (Z)!
E3(f;U)
1 + (S) (Z)w(Z)
1 + (S)"
1 s
gttA!
(Z)w3
(Z)
1 + (Z)+aBsinp gttA#
:(64)
The inverse relations are
E1(f;U) =E1(e;U) (S)w1
(S)
1 + (Z)"
aBsinp gttAE3(e;U)
1 s
gttA!
(S)w(S)
1 + (S)#
;21
E2(f;U) =E2(e;U) (S)w2
(S)
1 + (Z)"
aBsinp gttAE3(e;U)
1 s
gttA!
(S)w(S)
1 + (S)#
;
E3(f;U)= s
gttA+ (S)!
E3(e;U)
1 + (Z) (S)w(S)
1 + (Z)"
1 s
gttA!
(S)w3
(S)
1 + (S) aBsinp gttA#
:(65)
The frame components of any vector field
V=(e)
VE(e) =(f)
VE(f); (66)
obey the following transformation rule
(e)
V1=(f)
V1+"
1 s
gttA!
(Z)w(Z)V
1 + (Z)+aBsinp gttA(f)
V3#
(Z)w1
(Z)
1 + (S);
(e)
V2=(f)
V2+"
1 s
gttA!
(Z)w(Z)V
1 + (Z)+aBsinp gttA(f)
V3#
(Z)w2
(Z)
1 + (S);
(e)
V3= s
gttA+ (Z)! (f)
V3
1 + (S) (Z)w(Z)V
1 + (S)"
aBsinp gttA+
1 s
gttA!
(Z)w3
(Z)
1 + (Z)#
;(67)
withw(Z)introduced in Equation (27).
The inverse relations are
(f)
V1=(e)
V1+"
1 s
gttA!
(S)w(S)V
1 + (S) aBsinp gttA(e)
V3#
(S)w1
(S)
1 + (Z);
(f)
V2=(e)
V2+"
1 s
gttA!
(S)w(S)V
1 + (S) aBsinp gttA(e)
V3#
(S)w2
(S)
1 + (Z);
(f)
V3= s
gttA+ (S)! (e)
V3
1 + (Z)+ (S)w(S)V
1 + (Z)"
aBsinp gttA
1 s
gttA!
(S)w3
(S)
1 + (S)#
;(68)
withw(S)introduced in Equation (24).
200 400 600 800 1000 1200 1400τ/μ
-2.5×10-6-2.×10-6-1.5×10-6-1.×10-6-5.×10-7u2+1
65 70 75 80τ/μ
-3.×10-7-2.×10-7-1.×10-71.×10-72.×10-7u2+1
200 400 600 800 1000 1200 1400τ/μ
-0.000020-0.000015-0.000010-5.×10-6g+1
65 70 75 80τ/μ
-0.000020-0.000015-0.000010-5.×10-6g+1
Figure 13: (color online). The evolutions of u2=uauaandgon longer and shorter timescales for a zoom-whirl orbit presented on the left hand
sides of Figures 3 and 4.22
1000 2000 3000 4000τ/μ
-3.5×10-6-3.×10-6-2.5×10-6-2.×10-6-1.5×10-6-1.×10-6-5.×10-7u2+1
2212 2214 2216 2218 2220 2222τ/μ-3.×10-6-2.8×10-6-2.6×10-6-2.4×10-6u2+1
1000 2000 3000 4000τ/μ
-0.00008-0.00006-0.00004-0.00002g+1
2212 2214 2216 2218 2220 2222τ/μ
-0.00014-0.00012-0.00010-0.00008-0.00006-0.00004-0.00002g+1
Figure 14: (color online). The evolutions of u2=uauaandgon longer and shorter timescales are shown for an unbound orbit presented on the
left hand sides of Figures 7 and 8.
VIII. APPENDIX B: CHECKING THE
VALIDITY OF THE MPD EQUATIONS
The contraction of the inverse of the velocity-
momentum relation (6) with uagives that the sign of
pauais determined by the quantity:
g=uaua 1
2M2ubRebcdScdSaeua;(69)which corresponds to _x~T_x= _xG_xin Ref. [119]. Both the
functionsganduauaare shown on Figures 13 and 14 for
twocaseswhenthetestbodyfollowsazoom-whirlandan
unbound orbit, respectively. In both cases gtakes values
close to -1 during the whole evolution and uaua= 1.
Hence, the MPD equations are applied where they are
valid. Similar is hold along the all trajectories presented
in the article.
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1403.0378v1.Chaos_in_two_black_holes_with_next_to_leading_order_spin_spin_interactions.pdf | arXiv:1403.0378v1 [gr-qc] 3 Mar 2014Eur. Phys.J.C manuscriptNo.
(will beinsertedbytheeditor)
Chaos in two black holes with next-to-leading order spin-sp in
interactions
GuoqingHuang1, XiaotingNi1,Xin Wua,1
1Department ofPhysics, Nanchang University, Nanchang 3300 31, China
Received: date /Accepted: date
Abstract We take intoaccountthe dynamicsofa complete
thirdpost-NewtonianconservativeHamiltonianoftwospin -
ning black holes, where the orbital part arrives at the third
post-Newtonian precision level and the spin-spin part with
the spin-orbit part includes the leading-order and next-to -
leading-order contributions. It is shown through numerica l
simulationsthatthenext-to-leadingorderspin-spincoup lings
play an important role in chaos. A dynamical sensitivity to
thevariationofsingleparameterisalsoinvestigated.Inp ar-
ticular,thereareanumberof observable orbitswhoseinitial
radiiarelargeenoughandwhichbecomechaoticbeforeco-
alescence.
Keywords black hole ·post-Newtonian approximations ·
chaos·Lyapunovexponents
PACS04.25.dg·04.25.Nx ·05.45.-a·95.10.Fh
1 Introduction
Massivebinaryblack-holesystemsarelikelythemostpromi s-
ingsourcesforfuturegravitationalwavedetectors.Thesu c-
cessful detection of the waveforms means using matched-
filtering techniques to best separate a faint signal from the
noise and requiresa very precise modelling of the expected
waveforms. Post-Newtonian (PN) approximations can sat-
isfy this requirement. Up to now, high-precision PN tem-
plates have already been known for the non-spin part up to
3.5PN order ( i.e.the order 1 /c7in the formal expansion in
powers of 1 /c2withcbeing the speed of light) [1,2], the
spin-orbitpartupto3.5PNorderincludingtheleading-ord er
(LO,1.5PN),next-to-leading-order(NLO,2.5PN)andnext-
to-next-to-leading-order(NNLO, 3.5PN) interactions[3- 5],
and the spin-spinpart up to 4PN orderconsisting of the LO
(2PN),NLO (3PN)andNNLO(4PN)couplings[6-9].
ae-mail: xwu@ncu.edu.cnHowever, an extremely sensitive dependence on initial
conditions as the basic feature of chaotic systems would
pose a challenge to the implementation of such matched
filters, since the number of filters required to detect these
waveforms is exponentially large with increasing detectio n
sensitivity. This has led to some authors focusing on re-
search of chaos in the orbits of two spinning black holes.
Chaoswasfirstlyfoundandconfirmedinthe2PNLagrangian
approximation of comparable mass binaries with the LO
spin-orbit and LO spin-spin effects [10]. Moreover, it was
reported in [11] that the presence of chaos should be ruled
out in these systems because no positive Lyapunov expo-
nents could be found. As an answer to this claim, Refs.
[12,13]obtainedsomepositiveLyapunovexponentsandpoin ted
out these zero Lyapunov exponents of [11] due to the less
rigorouscalculationoftheLyapunovexponentsoftwonearb y
orbits with unapt rescaling. In fact, the conflicting result s
on Lyapunovexponentsare because the two papers [11,12]
used different methods to compute their Lyapunov expo-
nents, as was mentioned in [14]. Ref. [11] computed the
stabilizing limit values of Lyapunov exponents, and Ref.
[12] worked out the slopes of fit lines. This is the so-called
doubt regarding different chaos indicators causing two dis -
tinct claims on the chaotic behavior.Besides this, there wa s
second doubt on different dynamical approximations mak-
ing the same physical system have distinct dynamical be-
haviors.The 2PN harmonic-coordinatesLagrangianformu-
lation of the two-black hole system with the LO spin-orbit
couplings of one spinning body allows chaos [15], but the
2PN ADM (Arnowitt-Deser-Misner) -coordinates Hamilto-
nian does not [16,17]. Levin [18] thought that there is no
formal conflict between them since the two approaches are
not exactly but approximately equal, and different dynam-
ical behaviors between the two approximately related sys-
tems are permitted according to dynamical systems theory.
Seen from the canonical, conjugate spin coordinates [19],2
the former non-integrability and the latter integrability are
clearer. As extensions, both any PN conservative Hamilto-
nian binary system with one spinning body and a conser-
vativeHamiltonianof two spinningbodieswithoutthe con-
straint of equal mass or with the spin-orbit couplings not
restricted to the leading order are still integrable. Recen tly,
[20,21]arguedtheintegrabilityofthe2PNHamiltonianwit h-
outthespin-spincouplingsandwiththeNLOand/orNNLO
spin-orbitcontributionsincluded.Onthecontrary,theco rre-
spondingLagrangiancounterpartwithspineffectslimited to
the spin-orbit interactionsup to the NLO terms exhibitsthe
stronger chaoticity [22].Third doubt relates to different de-
pendence of chaos on single dynamical parameter or initial
condition.Thedescriptionofthechaoticregionsandchaot ic
parameter spaces in [15] are inconsistent with that in [23].
The differentclaims are regardedto be correct accordingto
thestatementof[24]thatchaosdoesnotdependonlyonsin-
glephysicalparameterorinitialconditionbutacomplicat ed
combinationofallparametersandinitial conditions.
It isworthemphasizingthatthe spin-spineffectsarethe
most important source for causing chaos in spinning com-
pact binaries, but they were only restricted to the LO term
in the published paperson research of the chaotic behavior.
It should be significant to discuss the NLO spin-spin cou-
plings included to a contribution of chaos. For the sake of
this, we shall considera complete3PN conservativeHamil-
tonian of two spinning black holes, where the orbital part
is up to the 3PN order and the spin-spin part as well as the
spin-orbitpartincludestheLOandNLOinteractions.Inthi s
way, we want to know whether the inclusion of the NLO
spin-spin couplings have an effect on chaos, and whether
thereischaosbeforecoalescenceofthe binaries.
2 Third post-NewtonianorderHamiltonianapproach
Itistoodifficulttostrictlydescribethedynamicsofasyst em
oftwomasscomparablespinningblackholesingeneralrel-
ativity.Instead,thePNapproximationmethodisoftenused .
Suppose that the two bodies have masses m1andm2with
m1≤m2. Other mass parameters are the total mass M=
m1+m2,thereducedmass µ=m1m2/M,themassratio β=
m1/m2andthemassparameter η=µ/M=β/(1+β)2.As
tootherspecifiednotations,a 3-dimensionalvector rrepre-
sentstherelativepositionofbody1tobody2,itsunitradia l
vectorisn=r/rwiththeradius r=|r|,andpstandsforthe
momentaofbody1relativetothecentre.Themomenta,dis-
tancesandtime tarerespectivelymeasuredintermsof µ,M
andM.Additionally,geometricunits c=G=1areadopted.
The two spin vectors are Si=SiˆSi(i=1,2) with unit vec-
torsˆSiandthespinmagnitudes Si=χim2
i/M2(0≤χi≤1).
InADMcoordinates,thesystemcanbeexpressedasthedi-mensionlessconservative3PN Hamiltonian
H(r,p,S1,S2) =Ho(r,p)+Hso(r,p,S1,S2)
+Hss(r,p,S1,S2). (1)
In the following, we write its detailed expressionsalthoug h
theyaretoolong.
Fortheconservativecase,theorbitalpart Hodoesnotin-
cludethedissipative2.5PNterm(whichistheleadingorder
radiationdampinglevel)buttheNewtonianterm HNandthe
PNcontributions H1PN,H2PNandH3PN, thatis,
Ho=HN+H1PN+H2PN+H3PN. (2)
Asgivenin [25],theyare
HN=p2
2−1
r, (3)
H1PN=1
8(3η−1)p4−1
2[(3+η)p2+η(n·p)2]1
r
+1
2r2, (4)
H2PN=1
16(1−5η+5η2)p6+1
8[(5−20η−3η2)p4
−2η2(n·p)2p2−3η2(n·p)4]1
r+1
2[(5+8η)p2
+3η(n·p)2]1
r2−1
4(1+3η)1
r3, (5)
H3PN=1
128(−5+35η−70η2+35η3)p8+1
16[(−7
+42η−53η2−5η3)p6+(2−3η)η2(n·p)2
×p4+3(1−η)η2(n·p)4p2−5η3(n·p)6]1
r
+[1
16(−27+136η+109η2)p4+1
16(17
+30η)η(n·p)2p2+1
12(5+43η)η(n·p)4]1
r2
+{[−25
8+(1
64π2−335
48)η−23
8η2]p2
+(−85
16−3
64π2−7
4η)η(n·p)2}1
r3
+[1
8+(109
12−21
32π2)η]1
r4. (6)
The spin-orbit part Hsois linear functions of the two
spins. It is the sum of the LO spin-orbit term HLO
soand the
NLOspin-orbitterm HNLO
so,i.e.
Hso(r,p,S1,S2)=HLO
so(r,p,S1,S2)+HNLO
so(r,p,S1,S2).
(7)
Ref.[5]gavetheirexpressions
Hso=1
r3[g(r,p)S+g∗(r,p)S∗]·L, (8)3
wheretherelatednotationsare
S=S1+S2,S∗=1
βS1+βS2,
g(r,p) =2+[19
8ηp2+3
2η(n·p)2−(6+2η)1
r],
g∗(r,p) =3
2+[−(5
8+2η)p2+3
4η(n·p)2
−(5+2η)1
r],
and the Newtonian-lookingorbital angularmomentumvec-
toris
L=r×p. (9)
The constant terms in gandg∗correspond to the LO part,
andtheothers,theNLO part.
Similarly,thespin-spinHamiltonian Hssalsoconsistsof
theLOspin-spincouplingterm HLO
ssandtheNLOspin-spin
couplingterm HNLO
ss, namely,
Hss(r,p,S1,S2)=HLO
ss(r,S1,S2)+HNLO
ss(r,p,S1,S2).(10)
Thefirst sub-Hamiltonianreads[25]
HLO
ss=1
2r3[3(S0·n)2−S2
0] (11)
withS0=S+S∗. The second sub-Hamiltonian is made of
threeparts,
HNLO
ss=Hs2
1p2+Hs2
2p2+Hs1s2p2. (12)
Theyarewrittenas[7,8]
Hs2
1p2=η2
β2r3[1
4(p1·S1)2+3
8(p1·n)2S2
1
−3
8p2
1(S1·n)2−3
4(p1·n)(S1·n)(p1·S1)]
−η2
r3[3
4p2
2S2
1−9
4p2
2(S1·n)2]
+η2
r3β[3
4(p1·p2)S2
1−9
4(p1·p2)(S1·n)2
−3
2(p1·n)(p2·S1)(S1·n)
+3(p2·n)(p1·S1)(S1·n)
+3
4(p1·n)(p2·n)S2
1
−15
4(p1·n)(p2·n)(S1·n)2], (13)
Hs2
2p2=HS2
1p2(1↔2), (14)Hs1s2p2=η2
2r3{3
2{[(p1×S1)·n][(p2×S2)·n]
+6[(p2×S1)·n][(p1×S2)·n]
−15(S1·n)(S2·n)(p1·n)(p2·n)
−3(S1·n)(S2·n)(p1·p2)
+3(S1·p2)(S2·n)(p1·n)
+3(S2·p1)(S1·n)(p2·n)
+3(S1·p1)(S2·n)(p2·n)
+3(S2·p2)(S1·n)(p1·n)
−1
2(S1·p2)(S2·p1)+(S1·p1)(S2·p2)
−3(S1·S2)(p1·n)(p2·n)
+1
2(S1·S2)(p1·p2)}
+3η2
2r3β{−[(p1×S1)·n][(p1×S2)·n]
+(S1·S2)(p1·n)2
−(S1·n)(S2·p1)(p1·n)}
+3η2β
2r3{−[(p2×S2)·n][(p2×S1)·n]
+(S1·S2)(p2·n)2
−(S2·n)(S1·p2)(p2·n)}
+6η
r4[(S1·S2)−2(S1·n)(S2·n)]. (15)
Here,p1=−p2=p. In a word, the conservative Hamilto-
nian (1) up to the 3PN order is not completely given until
Eq. (15) appears. Clearly, Hamiltonian (1) does not depend
onanymassbutthemassratio.
Theevolutionsofposition randmomentum psatisfythe
canonicalequationsofthe Hamiltonian(1):
dr
dt=∂H
∂p,dp
dt=−∂H
∂r. (16)
Thespinvariablesvarywithtimeaccordingtothefollowing
relations
dSi
dt=∂H
∂Si×Si. (17)
Besides the two spin magnitudes, there are four con-
served quantities in the Hamiltonian (1), includingthe tot al
energyE=Handthreecomponentsofthetotalangularmo-
mentumvector J=L+S.Afifthconstantofmotionisab-
sent,sotheHamiltonian(1)isnon-integrable.1Itshighnon-
linearity seems to imply that it is a richer source for chaos.
Next,we shall search forchaos, andparticularlyinvestiga te
1Based on the idea of [19], the Hamiltonian (1) can be expresse d as a
completely canonical Hamiltonian with a 10-dimensional ph ase space
when the canonical, conjugate spin coordinates are used ins tead ofthe
original spin variables. If the system is integrable, at lea st five inde-
pendent integrals of motion beyond the constant spin magnit udes are
necessary.4
theeffectoftheNLOspin-spininteractionsonthedynamics
ofthesystem.
3 Detectionofchaosbeforecoalescence
With numerical simulations, we use some chaos indicators
to describe dynamical differences between the NLO spin-
spincouplingsexcludedandincluded.Theappropriateones
of the indicators are selected to study dependence of chaos
on single parameter when the NLO spin-spin couplingsare
included. Finally, we expect to find chaos before coales-
cencebyestimatingtheLyapunovandinspiraldecaytimes.
3.1 Comparisons
Numerical methods are convenient to study nonlinear dy-
namics of the Hamiltonian (1). Symplectic integrators are
efficientnumericaltoolssincetheyhavegoodgeometricand
physical properties, such as the symplectic structure con-
servedandenergyerrorswithoutsecularchanges.However,
they cannot provide high enough accuracies, and the com-
putationsare expensivewhenthemixedsymplecticintegra-
tionalgorithms[21,26]withacompositeofthesecond-orde r
explicitleapfrogsymplecticintegratorandthesecond-or der
implicit midpoint rule are chosen. In this sense, we would
prefer to adopt an 8(9) order Runge-Kutta-Fehlberg algo-
rithm of variable time steps. In fact, it gives such high ac-
curacy to the energy error in the magnitude of about order
10−13∼10−12whenintegrationtimereaches106,asshown
in Fig. 1. Here, orbit 1 we consider has initial conditions
(p(0);r(0))=(0,0.39,0;8.55,0,0),whichcorrespondtothe
initial eccentricity e0=0.30 and the initial semi-majoraxis
a0=12.2. Other parameters and initial spin angles are re-
spectively β=0.79,χ1=χ2=χ=1.0,θi=78.46◦and
φi=60◦, where polar angles θiand azimuthal angles φi
satisfy the relations ˆSi=(cosφisinθi,sinφisinθi,cosθi), as
commonly used in physics. The NLO spin-spin couplings
are not included in Fig. 1(a), but in Fig. 1(b). It can be
seen clearly that the inclusion of the NLO spin-spin cou-
plings with a rather long expression decreases only slightl y
thenumericalaccuracy.Therefore,ournumericalresultsa re
showntobereliablealthoughtheenergyerrorshavesecular
changes.
We apply several chaos indicators to compare dynam-
ical behaviors of orbit 1 according to the two cases with-
out and with the NLO spin-spin couplings. The method of
Poincarésurfaceofsectioncanprovideacleardescription of
the structureof phasespace toa conservativesystem whose
phasespaceis4dimensions.Asapointtonote,itisnotsuit-
able for such a higher dimensional system (1). Fortunately,
power spectra, Lyapunov exponents and fast Lyapunov in-dicatorswould work well in finding chaos regardlessof the
dimensionalityofphasespace.
3.1.1 Powerspectrumanalysis
Power spectrum analysis reveals a distribution of various
frequencies ωof a signal x(t). It is the Fourier transforma-
tion
X(ω)=/integraldisplay+∞
−∞x(t)e−iωtdt, (18)
whereiis the imaginary unit. In general, the power spec-
traX(ω)are discrete for periodic and quasi periodic orbits
but continuous for chaotic orbits. That is to say, the classi -
fication of orbits can be distinguished in terms of different
featuresofthespectra.Onthebasisofthis,weknowthrough
Fig.2thattheorbitseemstoberegularwhentheNLOspin-
spin couplingsare not included, but chaotic when the NLO
spin-spin couplingsare included.Notice that the method of
power spectra is only a rough estimation of the regularity
and chaoticity of orbits. More reliable chaos indicators ar e
stronglydesired.
3.1.2 Lyapunovexponents
The maximum Lyapunov exponent is used to measure the
averageseparationrateoftwoneighboringorbitsinthepha se
spaceandgivesquantitativeanalysistothestrengthofcha os.
Its calculations are usually based on the variational metho d
andthetwo-particlemethod[27].Theformerneedssolving
thevariationalequationsaswellastheequationsofmotion ,
and the latter needs solving the equations of motion only.
Considering the difficulty in deriving the variational equa -
tions of a complicated dynamical system, we pay attention
to the application of the latter method. In the configuration
space,it is definedas[28]
λ=lim
t→∞1
tln|Δr(t)|
|Δr(0)|, (19)
where|Δr(0)|and|Δr(t)|are the separations between the
two neighboring orbits at times 0 and t, respectively. The
initialdistancecannotbetoobigortoosmall,and10−8isre-
gardedasto its suitablechoice in the doubleprecision[27] .
Forthesakeoftheoverflowavoided,renormalizationsfrom
time to time are vital in the tangent space. A bounded orbit
is chaotic if its Lyapunov exponent is positive, but regular
when its Lyapunov exponent tends to zero. In this way, we
canknowfromFig.3thatorbit1isregularforthecasewith-
out the NLO spin-spin couplings, but chaotic for the case
withthe NLO spin-spincouplings.Of course,it takesmuch
computational cost to distinguish between the ordered and
chaoticcases.5
3.1.3 FastLyapunovindicators
A quicker method to find chaos than the method of Lya-
punov exponents is a fast Lyapunov indicator (FLI). This
indicator that was originally considered to measure the ex-
pansion rate of a tangential vector [29] does not need any
renormalization,whileitsmodifiedversiondealingwithth e
useofthe two-particlemethod[30]does.Themodifiedver-
sionisoftheform
FLI(t)=log10|Δr(t)|
|Δr(0)|. (20)
Itscomputationisbasedonthefollowingexpression:
FLI=−k(1+log10|Δr(0)|)+log10|Δr(t)|
|Δr(0)|, (21)
wherekdenotes the sequential number of renormalization.
The FLI of Fig. 4(a) corresponding to Fig. 3(a) increases
algebraically with logarithmic time log10t, and that of Fig.
4(b)correspondingtoFig.3(b)doesexponentiallywithlog -
arithmic time. The former indicates the character of order,
butthelatter,thefeatureofchaos.Onlywhentheintegrati on
time addsupto 1 ×105, canthe orderedandchaotic behav-
iorsbe identifiedclearly forthe use of FLI unlikethe appli-
cation of Lyapunov exponent.There is a threshold value of
the FLIs between order and chaos, 5. Orbits whose FLI are
largerthan5arechaotic,whereasthosewhoseFLIsareless
than5areregular.
The above numerical comparisons seem to tell us that
chaosbecomeseasierwhentheNLOspin-spintermsarein-
cluded. This sounds reasonable. As claimed in [20,21], the
system(1)isintegrableandnotatallchaoticwhenthespin-
spin couplings are turned off. The occurrence of chaos is
completely due to the spin-spin couplings, which include
particularly the NLO spin-spin contributions leading to a
sharpincreaseinthestrengthofnonlinearity.Infact,wee m-
ploy FLIs to find that there are other orbits (such as orbits
2-5in Table1),whichare notchaoticforthe absenceofthe
NLO spin-spin couplings but for the presence of the NLO
spin-spincouplings.Inaddition,the strengthofthechaot ic-
ity of orbits 6-8 increases. As a point to illustrate, the oth er
initial conditions beyond Table 1 are those of orbit 1; the
starting spin unit vectorsof orbit 2 are those of orbit 1, and
those of orbits 3-8 are θ1=84.26◦,φ1=60◦,θ2=84.26◦
andφ2=45◦. Hereafter,onlythe dynamicsof the complete
Hamiltonian (1) with the NLO spin-spin effects included is
focusedon.
3.2 Lyapunovandinspiraldecaytimes
Takingβ=0.5,theinitialconditionsandtheinitialunitspin
vectors of orbit 1 as reference, we start with the spin pa-
rameterχat the value 0.2 that is increased in increments
of 0.01 up to a final value of 1 and draw dependence ofFLI onχin Fig. 5(a). This makes it clear that chaos oc-
curs when χ≥0.7. Precisely speaking, the larger the spin
magnitudes get, the stronger the chaos gets. Note that this
dependence of chaos on χrelies typically on the choice of
the initial conditions, the initial unit spin vectors and th e
other parameters. As claimed in [24], there is different de-
pendenceof chaoson χif the choice changes. On the other
hand,takingtheinitialspinanglesoforbit3,fixingthespi n
parameter χ=0.90andtheinitialconditions (p(0);r(0))=
(0,0.39,0;8.4,0,0), which correspond to the initial eccen-
tricitye0=0.28 and the initial semi-major axis a0=11.6,
we study the range of the mass ratio βbeginningat 0.5 and
ending at 1 in increments of 0.01. At once, dependence of
FLIonβcanbedescribedinFig.5(b).Thereischaoswhen
β≤0.86 and chaos seems easier for a smaller mass ratio.
Asinthepanel(a),thisresultisgivenonlyunderthepresen t
initialconditions,initialunitspinvectorsandotherpar ame-
ters.
Dothe above-mentionedchaoticbehaviorsoccurbefore
themergerofthebinaries?Toanswerit,wehavetocompare
the Lyapunov time Tλ=1/λ(i.e.the inverse of the Lya-
punov exponent)with the inspiral decay time Td, estimated
by[31]
Td=12
19c4
0
γ/integraldisplaye0
0e29/19[1+(121/304)e2]1181/2299
(1−e2)3/2de,(22)
wherethetwo parametersare
c0=a0(1−e2
0)e−12/19
0(1+121
304e2
0)−870/2299(23)
andγ=64m1m2M/5.WhenTλislessthan Td(orλTd>1),
chaoswouldbeobserved.Because Tλ=3.0×103andTd=
1.3×103for orbit 1, the chaoticity can not be seen before
the merger. Values of λTdfor orbits 2-8 are listed in Table
1. Clearly, only chaotic orbit 8 is what we expect. Besides
these,we plottwo panels(a) and(b)of Fig. 6 regardingde-
pendenceofLyapunovexponentonsingleparameter,which
correspondrespectively to Figs 5(a) and 5(b). Here are two
facts.First,theresultsinFig.6arethesameasthoseinFig .
5. Second, lots of chaotic orbits whose Lyapunovtimes are
many times greater than the inspiral times should be ruled
out, and there are only a small quantity of desired chaotic
orbitsleft.
InordertomaketheaccuracyofthePNapproachbetter,
weshouldchooseorbitswhoseinitialradiiarelargerenoug h
thanroughly10 M.AllchaoticorbitsinTable2areexpected.
Noticethattheotherinitialconditionsoftheseorbitsbey ond
this table are y=z=px=pz=0, and the starting spin an-
gles are still the same as those of orbit 3. Althoughan orbit
hasa largeinitialradius,it maystill bechaoticwhenitsin i-
tial eccentricity is high enough. This supports the result o f
[23]thata higheccentricorbitcaneasilyyieldchaos.6
Table1ValuesofFLIsand λTdfordifferent orbits.FLIacorresponds totheNLOspin-spin couplingsturned off.FLIb, λ,λdandλTdcorrespond
tothe NLO spin-spin couplings included.
Orbit β χ x p ye0a0FLIa FLIb λ λ dλTd
2 0.90 1.0 8.55 0.390 0.30 12.2 3.6 10.2 1.9E-4 8.1E-4 0.2
3 0.50 0.93 18.6 0.195 0.29 14.4 4.5 9.0 1.7E-4 3.7E-4 0.5
4 0.71 0.95 17.5 0.200 0.30 13.5 3.9 12.4 2.8E-4 5.3E-4 0.5
5 0.65 0.90 35.4 0.100 0.65 21.5 4.2 9.8 2.1E-4 3.8E-4 0.7
6 0.86 0.90 8.40 0.390 0.28 11.6 6.5 20.4 4.2E-4 9.3E-4 0.5
7 0.50 0.83 19.5 0.185 0.33 14.6 7.0 11.5 2.5E-4 3.8E-4 0.7
8 0.50 0.97 18.7 0.190 0.32 14.1 9.4 22.5 5.5E-4 4.3E-4 1.3
Table 2Values of λTdfor chaotic orbitswithbig initialradii when the NLOspin-s pin contributions are included.
Orbit χ β x p ye0a0λ λ dλTd
9 0.95 0.50 14.5 0.240 0.16 12.5 6.8E-4 5.2E-4 1.3
10 0.97 0.50 19.5 0.185 0.33 14.6 3.8E-4 3.7E-4 1.0
11 0.93 0.50 20.5 0.175 0.37 14.9 4.4E-4 3.9E-4 1.1
12 0.93 0.50 25.5 0.140 0.50 17.0 4.7E-4 3.8E-4 1.2
13 0.90 0.48 35.4 0.100 0.65 21.5 4.2E-4 3.5E-4 1.2
14 0.90 0.44 35.4 0.100 0.65 21.5 4.3E-4 3.4E-4 1.3
4 Conclusions
This paper is devoted to studying the dynamicsof the com-
plete3PNconservativeHamiltonianofspinningcompactbi-
naries in which the orbital part is accurate to the 3PN order
and the spin-spinpart as well asthe spin-orbitpart include s
theLO andNLO contributions.Because ofthehighnonlin-
earity,theNLOspin-spincouplingsincludedgiverisetoth e
occurrenceof strong chaos in contrast with those excluded.
By scanning single parameter with the FLIs, we obtained
dependence of chaos on the parameter. It was shown suffi-
ciently that chaos appears easier for larger spins or smalle r
mass ratios under the present considered initial condition s,
starting unit spin vectors and other parameters. So does for
a smaller initial radius. In spite of this, an orbit with a lar ge
initialradiusisstill possiblychaoticifitsinitialecce ntricity
ishighenough.Aboveall,therearesome observable chaotic
orbits whose initial radii are suitably large and whose Lya-
punovtimesarelessthanthecorrespondinginspiraltimes.
Acknowledgements This research is supported by the Natural Sci-
ence Foundation ofChina under Grant Nos. 11173012 and 11178 002.
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/s48 /s50 /s52 /s54 /s56 /s49/s48/s48/s46/s48/s48/s46/s53/s49/s46/s48/s49/s46/s53/s50/s46/s48/s50/s46/s53/s51/s46/s48/s51/s46/s53
/s78/s111/s32/s32/s32/s32 /s32/s72
/s115/s115/s78/s76/s79
/s40/s97/s41
/s32/s32/s69/s47/s49/s48/s45/s49/s51
/s116/s32/s47/s49/s48/s53/s48 /s50 /s52 /s54 /s56 /s49/s48/s48/s50/s52/s54/s56/s49/s48/s49/s50/s49/s52
/s72
/s115/s115/s78/s76/s79
/s40/s98/s41
/s32/s32/s69/s47/s49/s48/s45/s49/s51
/s116/s47/s49/s48/s53
Fig.1Energy errors of orbit1. The NLO spin-spin couplings are not included inpanel (a) butin Panel (b).
/s48 /s49 /s50 /s51 /s52 /s53/s48/s46/s48/s48/s46/s50/s48/s46/s52/s48/s46/s54/s48/s46/s56/s49/s46/s48
/s78/s111/s32/s32/s32/s32 /s72
/s115/s115/s78/s76/s79
/s40/s97/s41
/s32/s32/s112/s111/s119/s101/s114/s32/s32/s115/s112/s101/s99/s116/s114/s117/s109
/s102/s114/s101/s113/s117/s101/s110/s99/s121/s32/s47/s32/s49/s48/s45/s52/s48 /s49 /s50 /s51 /s52 /s53/s48/s46/s48/s48/s46/s49/s48/s46/s50/s48/s46/s51/s48/s46/s52/s48/s46/s53/s48/s46/s54
/s72
/s115/s115/s78/s76/s79
/s40/s98/s41
/s32/s32/s112/s111/s119/s101/s114/s32/s32/s115/s112/s101/s99/s116/s114/s117/s109
/s102/s114/s101/s113/s117/s101/s110/s99/s121/s32/s47/s32/s49/s48/s45/s52
Fig.2Power spectra corresponding toFig. 1.
/s50/s46/s48 /s50/s46/s53 /s51/s46/s48 /s51/s46/s53 /s52/s46/s48 /s52/s46/s53 /s53/s46/s48 /s53/s46/s53 /s54/s46/s48/s45/s53/s46/s48/s45/s52/s46/s53/s45/s52/s46/s48/s45/s51/s46/s53/s45/s51/s46/s48/s45/s50/s46/s53/s45/s50/s46/s48/s45/s49/s46/s53
/s78/s111/s32/s32/s32/s32 /s72
/s115/s115/s78/s76/s79
/s40/s97/s41
/s32/s32/s108/s111/s103
/s49/s48/s32/s124 /s124
/s108/s111/s103
/s49/s48/s32/s116/s50/s46/s48 /s50/s46/s53 /s51/s46/s48 /s51/s46/s53 /s52/s46/s48 /s52/s46/s53 /s53/s46/s48 /s53/s46/s53 /s54/s46/s48/s45/s52/s46/s48/s45/s51/s46/s53/s45/s51/s46/s48/s45/s50/s46/s53/s45/s50/s46/s48/s45/s49/s46/s53/s45/s49/s46/s48
/s72
/s115/s115/s78/s76/s79
/s40/s98/s41
/s32/s32/s108/s111/s103
/s49/s48/s32/s124 /s124
/s108/s111/s103
/s49/s48/s32/s116
Fig.3The maximum Lyapunov exponents λcorresponding to Fig.1.8
/s50/s46/s48 /s50/s46/s53 /s51/s46/s48 /s51/s46/s53 /s52/s46/s48 /s52/s46/s53 /s53/s46/s48/s49/s46/s48/s49/s46/s53/s50/s46/s48/s50/s46/s53/s51/s46/s48/s51/s46/s53/s52/s46/s48/s52/s46/s53
/s78/s111/s32/s32/s32/s32 /s72
/s115/s115/s78/s76/s79
/s40/s97/s41
/s32/s32/s70/s76/s73
/s108/s111/s103
/s49/s48/s32/s116/s50/s46/s48 /s50/s46/s53 /s51/s46/s48 /s51/s46/s53 /s52/s46/s48 /s52/s46/s53 /s53/s46/s48/s48/s50/s52/s54/s56/s49/s48/s49/s50/s49/s52/s49/s54
/s72
/s115/s115/s78/s76/s79
/s40/s98/s41
/s32/s32/s70/s76/s73
/s108/s111/s103
/s49/s48/s32/s116
Fig.4The fast Lyapunov indicators (FLIs) corresponding to Fig.1 .
/s48/s46/s52 /s48/s46/s53 /s48/s46/s54 /s48/s46/s55 /s48/s46/s56 /s48/s46/s57 /s49/s46/s48/s48/s53/s49/s48/s49/s53/s50/s48/s50/s53/s51/s48/s51/s53/s52/s48
/s32/s32/s70/s76/s73/s40/s97/s41
/s48/s46/s53/s48 /s48/s46/s53/s53 /s48/s46/s54/s48 /s48/s46/s54/s53 /s48/s46/s55/s48 /s48/s46/s55/s53 /s48/s46/s56/s48 /s48/s46/s56/s53 /s48/s46/s57/s48 /s48/s46/s57/s53 /s49/s46/s48/s48/s48/s53/s49/s48/s49/s53/s50/s48/s50/s53/s51/s48/s51/s53/s52/s48/s52/s53/s53/s48/s53/s53/s54/s48
/s32/s32/s70/s76/s73/s40/s98/s41
Fig.5(color online)The FLIs asa function of χorβwhen the NLO spin-spin interactions are included. AllFLIs l arger than 5 mean chaos.
/s48/s46/s50 /s48/s46/s51 /s48/s46/s52 /s48/s46/s53 /s48/s46/s54 /s48/s46/s55 /s48/s46/s56 /s48/s46/s57 /s49/s46/s48/s48/s50/s52/s54/s56/s49/s48/s49/s50/s49/s52/s49/s54
/s99/s61/s49/s48/s45/s52/s100/s61/s55/s46/s49/s56/s42/s49/s48/s45/s52/s40/s97/s41
/s32/s32/s47/s49/s48/s45/s52
/s48/s46/s53/s48 /s48/s46/s53/s53 /s48/s46/s54/s48 /s48/s46/s54/s53 /s48/s46/s55/s48 /s48/s46/s55/s53 /s48/s46/s56/s48 /s48/s46/s56/s53 /s48/s46/s57/s48 /s48/s46/s57/s53 /s49/s46/s48/s48/s48/s50/s52/s54/s56/s49/s48/s49/s50/s49/s52/s49/s54/s49/s56
/s99/s61/s49/s48/s45/s52/s40/s98/s41
/s100
/s32/s32/s47/s49/s48/s45/s52
Fig. 6(color online) The maximum Lyapunov exponents λcorresponding to Fig. 5. Note that λ>λcmeans chaos, and λ>λdwithλd=1/Td
indicatesthe occurrence of chaos before coalescence. |
2006.08253v1.Control_of_Spin_Relaxation_Anisotropy_by_Spin_Orbit_Coupled_Diffusive_Spin_Motion.pdf | Control of Spin Relaxation Anisotropy by Spin-Orbit-Coupled Diusive Spin Motion
Daisuke Iizasa,1Asuka Aoki,1Takahito Saito,1Junsaku Nitta,1, 2, 3Gian Salis,4and Makoto Kohda1, 2, 3, 5
1Department of Materials Science, Tohoku University, Sendai 980{8579, Japan
2Center for Spintronics Research Network, Tohoku University, Sendai 980{8577, Japan
3Center for Science and Innovation in Spintronics (Core Research Cluster), Tohoku University, Sendai 980{8577, Japan
4IBM Research-Zurich, S aumerstrasse 4, 8803 R uschlikon, Switzerland.
5Division for the Establishment of Frontier Sciences, Tohoku University, Sendai 980-8577, Japan
(Dated: June 16, 2020)
Spatiotemporal spin dynamics under spin-orbit interaction is investigated in a (001) GaAs two-
dimensional electron gas using magneto-optical Kerr rotation microscopy. Spin polarized electrons
are diused away from the excited position, resulting in spin precession because of the diusion-
induced spin-orbit eld. Near the cancellation between spin-orbit eld and external magnetic eld,
the induced spin precession frequency depends nonlinearly on the diusion velocity, which is unex-
pected from the conventional linear relation between the spin-orbit eld and the electron velocity.
This behavior originates from an enhancement of the spin relaxation anisotropy by the electron ve-
locity perpendicular to the diused direction. We demonstrate that the spin relaxation anisotropy,
which has been regarded as a material constant, can be controlled via diusive electron motion.
Precise control of spin motion is a prerequisite from
fundamental physics to spintronics and quantum infor-
mation technology [1{4]. In a semiconductor quantum
well (QW), Rashba [5, 6] and Dresselhaus [7] spin{orbit
(SO) interactions act as eective magnetic elds for mov-
ing electrons, enabling coherent spin control via preces-
sion, whereas spin relaxation occurs simultaneously be-
cause of an interplay between the SO eld and the ran-
dom motion of electrons [8]. Both spin precession and
relaxation processes are closely tied to one another solely
by SO interaction [9]. For stationary electrons with mean
zero velocity, the correlation between precession and re-
laxation triggers a modulation of spin precessional mo-
tion, known as spin relaxation anisotropy [10{19]. For
spin rotation by external and/or SO elds in a QW, spins
along growth and in-plane orientations do not experience
identical torques because of the in-plane orientation of
the SO elds. This situation induces anisotropic spin
relaxation [10{19] and modulates the spin precession fre-
quency [13{16, 18, 19]. Because SO elds are well dened
for stationary electrons, the spin relaxation anisotropy
has been regarded as a material constant. However, for
moving electrons with a nite net velocity induced by
drift [20{25] and diusion [24{27], the electron trajectory
further modulates SO elds and directly aects the spin
relaxation anisotropy through the momentum-dependent
spin precession. Moreover, the spin relaxation anisotropy
is not limited to particular materials such as III{V semi-
conductors because the anisotropic SO elds are ubiqui-
tous in solid states, with spin-momentum locking in topo-
logical insulators [28, 29], Rashba interface in oxides [30],
metal interfaces [31], and Zeeman-type SO eld in 2D ma-
terials [32]. Consequently, unveiling the eects of moving
electrons on the modulation of spin relaxation anisotropy
and induced precession frequency are expected to be cru-
cially important for future spintronics, topological elec-
tronics, and quantum information technologies. Despitethis, earlier studies of spin relaxation anisotropy have re-
mained limited only to stationary cases [13{16, 18, 19].
Here, we experimentally manifest control of spin pre-
cessional motion via spin relaxation anisotropy by dif-
fusive spin motion in a GaAs-based QW. When the SO
eld under diusive motion is nearly compensated by a
constant external magnetic eld, the spin precession fre-
quency is no longer linear to the diusion velocity. This
behavior cannot be anticipated from a conventional spin
drift/diusion model. It is explained by a modulation
of the spin relaxation anisotropy. The evaluated spin re-
laxation anisotropy, which exhibits six-fold enhancement
from the stationary case, is explained by a tilting of the
spin precession axis from the direction of external mag-
netic eld caused by the electron diusive motion. We
in
uence the spin relaxation anisotropy, as reported for
the rst time, by precisely controlling the electron mo-
tion.
The structure examined for this study was an n-doped
20-nm-thick (001) GaAs QW. In this system, we obtain
SO elds characterized by the Rashba parameter (<0),
the Dresselhaus parameter =1 3(>0), with linear
1=
hk2
ziand cubic term 3=
k2
F=4. Here,hk2
zi
denotes the expected value of the squared wavenumber
in the QW. The bulk Dresselhaus coecient is
< 0.
The Fermi wavenumber is kF=p2ns. The carrier
density and mobility measured using a Hall bar device
werens= 1:721011cm 2and 11:2104cm2V 1s 1,
respectively, at 4.2 K. To detect the diusive spin dy-
namics, spatiotemporal Kerr rotation microscopy is per-
formed using a mode-locked Ti:sapphire laser emitting
2-ps-long pulses at a 79.2 MHz repetition rate. Fig-
ure 1(a) depicts an experimental conguration for pump
and probe beams with Rashba and Dresselhaus SO elds.
Therein,
Rand
Drespectively represent the spin pre-
cession frequency vectors. A circularly polarized pump
beam with Gaussian sigma-width ppis focused onto thearXiv:2006.08253v1 [cond-mat.mes-hall] 15 Jun 20200
r
x|| [110]-y|| [110]
Ωex,yΩex,x
ΩD
ΩRFIG. 1. (a) Sketch of a pump-probe scanning Kerr microscopy
setup with Rashba (
R) and Dresselhaus (
D) elds as pre-
cession vectors. An external magnetic eld is depicted as
ex;xand
ex;yas a precession vector for y- andx-scans con-
gurations, respectively. A circularly polarized pump beam
excites a spin polarization sz. A linearly polarized probe
beam detects szat a delay time tand a position ( x;y). (b)
Measuredszat dierent xpositions highlighted as colored
circles in (a).
sample surface to excite spin polarization szalong the
growth direction. A linearly polarized probe beam (spot
sizepr) detectsszat delay time tand arbitrary posi-
tion by a motor-controlled scanning mirror. All optical
measurements are taken at 30 K.
The spin precession frequency induced by a velocity
v= (vx;vy) in an external magnetic eld Bex= (Bx;By)
is generally described as
x;y(vy;x) =2m
~2(+)vy;x+gB
~Bx;y: (1)
Hereg <0 stands for the electron gfactor,Bdenotes
the Bohr magneton, ~is the reduced Plancks constant,
andm= 0:067m0expresses eective electron mass of
GaAs. The diusion velocity vdif, which is controlled by
the center-to-center distance rbetween pump and probe
spots, is dened as
vdif= 2Dsr=(2Dss+2
e); (2)
whereDsis the spin diusion constant, srepresents the
D'yakonov-Perel' spin relaxation time, and the convo-
luted spot size eis dened by 2
e=2
pp+2
pr[26].
Also,sis a result of the replacement of t=sbe-
cause our system satises 2 Dss2
eand smalls.
By changing the probe position along the x-axis (y-axis)
[26], i.e., the distance rin Eq. (2) , one can set the dif-
fusion velocity vdif=vx(vdif=vy) and thereby modu-
late the spin precession frequency [
y(vx) or
x(vy) in
Eq. (2)]. Figure 1(b) shows the time evolution of the ex-
perimental Kerr signal ( sz) at dierent probe positions
(x= 9:7;0:8 and 12:5m) in anx-scan (e= 8:1
m andBy= +0:45 T). The spin precession frequency
depends strongly on the probe position, re
ecting the
momentum (velocity) dependent SO eld induced by
the nite diusion velocity. We systematically measured
Kerr signals with dierent positions on the x- andy-axes
with several spot sizes e. We extracted the precession
1
ΩD
0x|| [110]
ΩR-
0y|| [110]
ΩRΩD10,167,209
FIG. 2. Measured spin precession frequency j
measjobtained
for dierent eandBexand for scans of the pump-probe
separation along x(a) andy(b). Diusing spins experience
strong SO elds for x-scan, but weak elds for y-scan. All
symbols represent experimental data. All solid lines show
linear ts. Dashed lines in (a) correspond to the nonlinear
ts based on Eq. (3) with at= 0:076 GHz.
frequencyj
measjby tting the normalized Kerr signal
sz= exp ( t=s) cos (2j
measjt+) with phase shift .
Figures 2(a) and 2(b) summarize extracted j
measj
inx- andy-scans. For the y-scan [Fig. 2(b)], j
measj
varies linearly with the yposition for all conditions of
Bxande, re
ecting the linear dependence of vdifon
theyposition, as presented in Eq. (2). In addition, when
edecreases from 11.6 to 6.8 m, the slope d
meas=dy
increases gradually, which agrees well with Eq. (2) and
which is consistent with earlier reports of the literature
[20, 22, 23, 25{27]. For the x-scan [Fig. 2(a)], however,
a linear variation of j
measjon thexposition is only ob-
served fore= 9:8m andBy= +0:45 T (diamond
symbols). Reducing eto 8.1 and 5.6 m exhibits a de-
viation from a linear variation; notably most pronounced
whenj
measjapproaches zero. This cannot be explained
using the conventional linear relation between electron
velocity and SO eld. To understand this eect, we rst
evaluate the SO parameters from the linear frequency
variation. From linear ts depicted as solid lines in
Figs. 2(a) and 2(b), we obtain = 2:8910 13eVm,
1= 1:8610 13eVm, and 3= 0:2210 13eVm.
Also,g= 0:268 is estimated at r= 0 (vdif= 0).
We assume g < 0 based on the QW thickness [23].
Also,Ds= 0:0195 m2=s is derived from the measured
s= 75 ps at Bex=0T [33]. Using evaluated 1;3,
andns, we obtain
= 8:31 eV A3which is consistent
with values reported in the literature [34]. To explain our
observation, we introduce in analogy to anisotropic spin
relaxation for stationary electrons modied spin preces-
2sion frequencies [13{16, 18, 19],
x=q
x(vdif)2 2
at;
y=q
y(vdif)2 2
at;(3)
where the anisotropic term [15, 18] is
at() = ( xcos2 + ysin2)=2: (4)
Here the relaxation rate of spins oriented along x- and
y-axes is x;y= (4Dsm2=~4)[(+)2+2
3], respec-
tively, and 2[0;2] is the direction of the spin pre-
cession axis, dened as in-plane polar angle from + x- to-
ward +y-axis. The term at() describes the relaxation
anisotropy between the two relevant orthogonal crystal
axes and is responsible for a correction of the precession
frequency [Eq. (3)]. For the y-scan ( Bex= (Bx;0)) spins
precess in the y-zplane, and at( = 0) = x=2 =
( y z)=2 denotes half of the dierence of the relax-
ation rate between y- andz-axes, where z= x+ y
is the relaxation rate along the z-axis. For the x-scan
(Bex= (0;By)), at(=2) = y=2. Because at()
additionally contributes to the spin precession frequency
shown in Eq. (3),
x;yshows a nonlinear dependence on
the probe position r, which becomes pronounced when
the precession frequency induced by external and SO
elds becomes comparable to x;y=2. Based on the ex-
perimentally evaluated values for ;1;3, andDs, we
calculate y=2 = 0:076 and x=2 = 0:99 GHz.
Fore= 5:6 and 8.1m, the calculated
yare shown
as dashed lines in Fig. 2(a). The calculated values only
reproduce the experimental data in a linear frequency
region. The rapid decrease of
ythat occurs below 0.8
GHz cannot be explained by y=2 = 0:076 GHz.
According to Eq. (4), the frequency modulation caused
by the relaxation anisotropy depends on the direction of
the precession axis (). For stationary electrons under
Bex, where the SO eld does not contribute to frequency
modulation, is well-dened by the direction of Bex.
However, for moving electrons, the precession axis is de-
ned by the sum of Bexand the SO eld, implying that
the electron trajectories under diusion further modu-
late . Because various electron trajectories can lead
from the pump spot to the probe spot, the precession
axis is no longer well dened by Bexbecause of dierent
diusion velocity vectors v= (vx;vy) in times[dier-
ent arrows in Fig. 3(a)]. Specically examining one single
trajectory with average velocity v, its direction of aver-
age precession axis ( vx;vy) = arctan(
y(vx)=
x(vy))
can be obtained from Eq. (1). Entering ( vx;vy) into
Eq. (4) directly reveals the velocity-dependent form of
the anisotropic term
at(vx;vy) = x
x(vy)2+ y
y(vx)2
2 (
x(vy)2+
y(vx)2): (5)
It is noteworthy that the precession frequencies caused
by opposite velocities ( vy;x) do not cancel each other
2
(a)
x|| [110]-y
(x, 0)
vyvx1
2
3
PumpProbe(b)
(x, 0)
x xy(c)FIG. 3. (a) x-scan conguration where the probe center is
separated by a vector ( x;0) from the pump center (0 ;0). Elec-
tron trajectories exist with an average velocity that is tilted
from thex-axis, contrary to the macroscopic diusion veloc-
ity [Eq. (2)]. (b) Mean velocity components of horizontal and
vertical directions, v
handv
v. (c) Calculated v
h,v
vbased
on Eqs. (6) and (7). v
vare constant with respect to rhere,
whereasv
hdepends on the position.
because
x;yenter as squares. This nding contrasts
to the notion of a single (averaged) diusion velocity for
given pump and probe spots [described by Eq. (2)], corre-
sponding to the mean value of all velocity vectors leading
from the pump to the probe spots [Fig. 3(a)]. Actually,
Eq. (5) rather suggests that the anisotropic term is de-
ned by the microscopic behavior of the electron motion
(velocity). Therefore, we sort all diusion velocity vec-
tors along the x- andy-axes according to their sign and
evaluate the mean values of horizontal and vertical ve-
locities at probe positions v
handv
v, respectively, as
indicated by silver bold arrows in Fig. 3(b). Each veloc-
ity is described as
v
h=es
se r2s
2
eff+ rerfc
rps
e!
;(6)
v
v=ep
=(s); (7)
where = Ds=(2Dss+2
e). The complementary error
function is denoted by erfc. The signs inv
handv
v
respectively correspond to the positive/negative velocity
components along the horizontal or vertical axes. Fig-
ure 3(c) shows calculated v
handv
v. Thev+
hincreases
rapidly in the + xregion, whereas v
hhas the opposite
tendency because of radial diusion of electrons from the
excited pump spot.
When the probe spot is displaced along the x-axis
[Fig. 3(a)], the average velocity vector points to the x-
axis because there, jv
hj>jv+
hj. Remarkably, vertical
velocitiesv
vare independent of probe position and are
of similar size as v
h. This suggests that the tilted veloc-
ity vectors should contribute to atand the precession
axis () no longer points along Bex. For the total mean
velocityv+
h+v
h+v+
v+v
vas sketched in Fig. 3(b), the
v
vcancel out each other and are linear in the position
[dashed line in Fig. 3(c)], corresponding to the conven-
tional macroscopic diusion velocity [Eq. (2)].
By considering both horizontal and vertical velocities
[Eqs. (6) and (7)] depicted in Fig. 3(b), we average over
301530
x ( 7m)0!atx (GHz)
01530
y ( 7m)!aty (GHz)<eff = 5.6 7m
By<eff = 8.1 7m
By = 0.45 T<eff = 9.8 7m
By = 0.45 T
<eff = 6.8 7m
Bx = 0.4 T
<eff = 8.1 7m
Bx = 0.55 T<eff = 11.6 7m
Bx = 0.65 T(a) (b)FIG. 4. (a) Calculated anisotropy term x;y
atforx-scan (a)
andy-scan (b) as obtained from using Eq. (8). Both x;y
at
are modulated by r. Parameters for the calculation are all
experimentally determined values.
all contributions to the anisotropic term [Eq. (5)] for the
x-scan with
x
at=
at(v+
h;v+
v) + at(v+
h;v
v)
+ at(v
h;v+
v) + at(v
h;v
v)
=4: (8)
For they-scan conguration, y
atis obtained from Eq. (8)
by
ipping vhandvvwith each other. We calculate x;y
at
in Figs. 4(a) and 4(b) with parameters evaluated from the
experimental conditions. The x
atexhibits a peak struc-
ture corresponding to the cancellation between external
and SO elds, i.e.
y(vdif) = 0. At this position, x
atis
enhanced by more than six times from y=2 = 0:076
GHz. Such a peak structure is observed consistently for
dierent spot sizes and Byvalues. The enhanced x
atis
the consequence of a tilting of the spin precession axis
away from Bexdirection due to the v
vcomponents that
introduce a precession contribution
x(v
v)2. As seen
from Eq. (5), x
x(v
v)2is introduced in the numera-
tor of the expression for at. Fory-scan, y
atis only
gently modulated with ybecause, in this case, the ad-
ditional contribution proportional to y
y(v
v) is weak
compared to the case of x-scan (because x y). In
other words, a small SO eld along the y-axis does not
tilt the spin precession axis signicantly. In both x- and
y-scans, when the magnitude of Bexbecomes suciently
large compared to the SO eld, x;y
atconverges respec-
tively to the stationary cases of 0:076 GHz and 0:99
GHz.
Finally, we reproduce the nonlinear behavior of the
x-scan quantitatively by considering the calculated x;y
at
in Fig. 4. Figure 5(a) shows the experimentally obtained
results of color-coded szin anx-scan and a frequency
analysis (circles) for e= 5:6m withBy= 0:4 T.
Solid and dashed lines respectively correspond to the cal-
culated
ybased on Eq. (3) with our new x
at[Eq. (8)]
and the conventional y=2 = 0:076 GHz. The re-
maining parameters of Eq. (3) are all experimentally ob-
tained. The
yobtained with the new x
atshows excel-
lent agreement with the experimental values, including
the nonlinear variation. To conrm the enhancement of
atfurther, we conducted Monte Carlo (MC) simulation.
Figure 5(b) presents the simulated Kerr traces, showing
01
sz (arb. units)00.20.40.60.8
t (ns)
000.20.40.60.8t (ns)
000.511.5
| +meas| (GHz)
00.5100.20.40.60.8
t (ns)
015
x ( 7m)00.20.40.60.8t (ns)
015
x ( 7m)0123
| +meas| (GHz)
00.51
sz (arb. units)00.20.40.60.8
t (ns)
02040
y ( 7m)00.20.40.60.8t (ns)
012
| +meas| (GHz)
01
sz (arb. units)x = -8.7 7m
x = -8.6 7m(a) (b) (c)x = 17.2 7m
x = 17.2 7m(d) (e) (f)Experiment Monte Carlo
Experiment I Monte Carlo Iy = -18.2 7m
(g)(h) Monte CarloFIG. 5. Experimental and Monte Carlo simulated times-
pace records of szinx-scan for (a) and (b) with e= 5:6
m atBy= 0:4 T, and for (d) and (e) with e= 8:1
m atBy= 0:45 T. All solid lines are
ycalculated with
new x
at, and dashed lines with conventional anisotropic term
y=2 = 0:076 GHz. The time evolution of szis shown at
(c) forx 8:6m and in (f) for x= 17:2m for ex-
perimental data (diamonds) and for Monte Carlo simulation
results (red solid lines). (g) Monte Carlo simulated time-space
records ofszin ay-scan withe= 5:6m,Bx= 0:4 T and
g= 0:268: the solid line shows
xwith new y
at; the dashed
line is obtained with conventional value x=2 = 0:99 GHz.
The gray diamond is the extracted frequency from the (h)
time evolution of szaty= 18:2 m with Monte Carlo simu-
lation (red solid) and the tted curve (dotted black).
good agreement with the experimentally obtained result.
Atx 8:6m, whereas
ywith conventional y=2
suggests nite precession with 0.19 GHz,
ywith the
new x
atshows a halt of spin precession. As presented in
Fig. 5(c), the time evolution of szfor both the experiment
(diamond) and MC simulation (red solid) at x 8:6m
conrms a simple exponential decay with no oscillatory
behavior. Similar results also hold for e= 8:1m with
By= 0:45 T in Figs. 5(d){5(f), supporting enhancement
of the anisotropic term. We also compare y-scan by MC
simulation for parameters e= 5:6m andBx= 0:4 T
[Fig. 5(g)]. Solid and dashed lines are calculated values of
xwith new y
atand conventional x=2 = 0:99 GHz,
respectively, where
xis enhanced for negative yvalues
for new y
at. This point is conrmed further in Fig. 5(h)
by plotting the time evolution of szaty= 18:2m.
The spin precession frequency obtained from MC simula-
tion aty= 18:2m [grey diamond in Fig. 5(g)] shows
good agreement with our new model. The quantitative
4agreement shown above reveals clearly that precession by
the relaxation anisotropy is not a material constant pa-
rameter, but is rather controlled by diusive spin motion.
In conclusion, we have experimentally observed an en-
hancement of the spin relaxation anisotropy by diusive
spin motion. We measured the precession frequency in an
external magnetic eld by changing the relative distance
between excited pump and detected probe positions in
a spatiotemporal Kerr rotation microscope. Because of
various electron trajectories for electrons travelling from
the pump to the probe position, the spin precession axis
is tilted substantially from the external magnetic eld di-
rection when the diusion-induced SO eld nearly com-
pensates the magnitude of the external magnetic eld.
Such a SO-coupled spin-diusive motion controls the re-
laxation anisotropy. It is detected as a nonlinear pre-
cession frequency modulation. Whereas the relaxation
anisotropy is regarded as a constant parameter for sta-
tionary electrons, it becomes controllable for moving elec-
trons. This eect also points out a threshold to start spin
precession at a certain velocity. Because this eect is not
limited only to diusive motion, but also can be con-
trolled by drift and ballistic transport, our ndings link
the eect of the precise control of spin states to future
spintronics and quantum information technology.
We acknowledge nancial support from the Japanese
Ministry of Education, Culture, Sports, Science, and
Technology (MEXT) Grant-in-Aid for Scientic Research
(Nos. 15H02099, 15H05854, 25220604, and 15H05699),
EPSRC-JSPS Core-to-Core program, and the Swiss Na-
tional Science Foundation through the National Center of
Competence in Research (NCCR) QSIT. D.I. thanks the
Graduate Program of Spintronics at Tohoku University,
Japan, for nancial support.
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5 |
2110.07094v3.Thermalization_in_a_Spin_Orbit_coupled_Bose_gas_by_enhanced_spin_Coulomb_drag.pdf | Thermalization in a Spin-Orbit coupled Bose gas by enhanced spin Coulomb drag
D. J. Brown1, 2,and M. D. Hoogerland1
1Dodd-Walls Centre for Photonic and Quantum Technologies, Department of Physics,
University of Auckland, Private Bag 92019, Auckland, New Zealand
2Present address: Light-Matter Interactions for Quantum Technologies Unit,
Okinawa Institute of Science and Technology Graduate University, Onna, Okinawa 904-0495, Japan
An important component of the structure of the atom, the eects of spin-orbit coupling are
present in many sub-elds of physics. Most of these eects are present continuously. We present a
detailed study of the dynamics of changing the spin-orbit coupling in an ultra-cold Bose gas, coupling
the motion of the atoms to their spin. We nd that the spin-orbit coupling greatly increases the
damping towards equilibrium. We interpret this damping as spin drag, which is enhanced by spin-
orbit coupling rate, scaled by a remarkable factor of 8 :9(6) s. We also nd that spin-orbit coupling
lowers the nal temperature of the Bose gas after thermalization.
INTRODUCTION
The understanding of the transport, diusion and
damping of spin, in contrast to those of charge, is im-
portant to the eld of spintronics [1], where the spin of
particles, rather than the quantity of particles (charge)
carries information. Spin currents, in contrast to charge
currents, are damped due to collisions between particles
of opposite spin, as their relative momentum is not con-
served. This damping is known as Spin Drag [2, 3].
Analogous to the spin drag in bilayer electron systems,
systems of ultracold bosons can also demonstrate spin
drag, with the drag enhanced by the familiar bosonic
enhancement [4] prominent in ultracold boson systems.
There is a detailed collection of work over the years into
the presence of spin Coulomb drag in ultracold atomic
systems [5{7] with a small selection of the work featuring
the inclusion of spin-orbit coupling [8].
The other important eect in two dimensional elec-
tron systems is spin-orbit coupling (SOC) [9{11]. How-
ever, solid state materials used to investigate the eects
of spin-orbit coupling are often challenging due to the
limited control of individual experimental parameters.
The body of work surrounding surrounding the topic of
spin-drag with added spin-orbit coupling is limited with
theoretical investigations looking at the impact of weak
coupling on the drag in a 2D electron system [12], or
the behaviour of impurities in a spinor condensate sys-
tem [13].
In depth understanding of this combination could lead
to better understanding of systems such as the topo-
logical insulators [14, 15] with their famed protected
edge states are dependent on the spin-momentum locking
caused by the SOC within the material and have been in-
vestigated as a potential platform for fault tolerant quan-
tum computation [16, 17].
Ultracold atoms provide an ideal environment for test-
ing the eects of SOC on the spin coulomb drag in quan-
tum systems due to the ability to control many of the
crucial parameters accurately.Previous experimental and theoretical work by Li et.
al. [8] demonstrated the generation of spin currents using
the same technique of a quench of a spin-orbit coupled
Bose-Einstein condensate (BEC) and investigated the in-
creased damping of the out of equilibrium system. GPE
simulations showed good qualitative agreement with the
experimental results, and gathering insight into the BEC
shape oscillations and the miscible-imiscible phase tran-
sition. As stated by Li et. al. the simulations underes-
timate the damping of the BEC oscillations, potentially
due to the lack of thermal atoms in the simulations. In
particular, it was shown in [4] that the spin-Coulomb
drag between thermal atoms and the condensate domi-
nates over the mean eld eects, rendering the mean eld
GPE only partially eective.
In this article we present our experiments on investi-
gating the thermodynamic behaviour of spin-orbit cou-
pled systems within a conservative potential, and at-
tempt to explain the enhanced damping of the atomic
oscillations in the presence of SOC as Coulomb spin drag
[4] by comparing the results to theoretical calculations.
We create synthetic SOC using the ground state man-
ifold of a Rubidium-87 (87Rb) BEC, following the Ra-
man laser scheme rst demonstrated in the experiments
of Spielman et. al [18].
A bias magnetic eld induces a Zeeman shift, breaking
the degeneracy of the F=1 ground state of the atom sepa-
rating them in energy. A quadratic Zeeman shift shifts
themF= +1 state further than the mF= 1, allow-
ing us to eectively decouple the latter from the system.
The atoms in the dierent Zeeman sublevels also dier
in momentum by ky= 2kR, wherekR= 2= is the
recoil momentum gained by the atom due to absorption
of a photon with wavelength . The Hamiltonian of the
coupledF= 1 state as a function of the atomic quasi-
momentum ~ky, is as follows,arXiv:2110.07094v3 [cond-mat.quant-gas] 15 Feb 20222
(a) (b)
FIG. 1: Schematic of the experimental setup. (a)
Geometry of the laser orientation and polarization,
along with the bias magnetic eld. (b) The level scheme
of theF= 1 ground state and the Raman transitions
induced by the coupling lasers. The Rabi frequencies of
the individual transitions are
1and
2.
^Hy(~ky) =0
BB@h2(~ky+2kR)2
2m hh
R
20
h
R
2h2~k2
y
2m hh
R
2
0h
R
2h2(~ky 2kR)2
2m+ h1
CCA
(1)
Diagonalizing the Hamiltonian gives the energies of the
spin-orbit coupled dressed states which for Raman cou-
pling strengths h
R<4ERfeatures a double minimum.
Here,ER= h2k2
R=2m,is the two photon detuning be-
tween the bare states, and indicates the quadratic shift.
Correctly choosing the detuning for a given coupling re-
sults in the ground state being an equal superposition of
the two pseudospin states j"i,j#i, corresponding to a
spin-orbit coupled state.
However, when h
R>4ER, there is only a single min-
imum at quasimomentum ~ky=kR. In the experiments
reported here, we initially prepare a Bose-Einstein Con-
densate, trapped in a harmonic trap, in the latter state
with h
R= 5:5ER. The system is then quenched to a
lower h
R<2ER, which takes the system out of equi-
librium, and allowed to thermalise. We nd the time
constant for this thermalisation, and nd that the rate
scales with the coupling strength
R.
EXPERIMENTAL APPARATUS
Our experiments begin with an all-optical BEC com-
posed of approximately 104 87Rb atoms, optically
pumped into the jF= 1;mF= 0ibefore evaporation,
as described in our previous work [19]. The BEC is held
in a harmonic trap, with aspect ratios !y:!x:!z=
1 : 1:2 : 2, formed by a crossed-beam optical dipole trap.
We use two values of !yfor our experiments. The lowesttrapping frequencies correspond to the the experiments
performed with the trap held at the nal power 66 mW
achieved after evaporation, with !y= 285 s 1. For
the larger trapping frequencies, we adiabatically increase
the power of the dipole trapping laser to 90 mW, cor-
responding to !y= 2112 s 1. Note that the larger
trap frequency corresponds to a larger trap depth, and
thus increases the number of atoms retained in the trap
during the thermalization process and increases the rate
of collisions between the atoms.
During the evaporation to BEC a magnetic bias eld
Byis ramped up in the last 2 seconds to 8.35 G providing
the a measured !B=2= 5:845 MHz Zeeman shift, and
a measured quadratic Zeeman shift of =2= 5 kHz. A
schematic of the coupling scheme and geometry is shown
in Fig. 1. The two-photon coupling strength
Ris ex-
perimentally determined by observing the Rabi oscilla-
tions between the populations of the states j 1i,j0iand
j+ 1izero detuning, and tting the time evolution with
the three state optical Bloch equations.
To induce spin-orbit coupling we use two orthogonally
polarized laser beams with wavelength = 790:2 nm
counter-propagating along ythat are focused to an
150m diameter beam onto the center of the dipole trap.
This wavelength of 790 :2 nm was chosen to minimise the
scalar AC Stark shift in the atoms, which would have led
to undesirable extraneous forces induced by these beams.
The two beams are derived from the same laser, but dier
in frequency by !!B+and couple two of the inter-
nalmFlevels of the BEC atoms. For sucient quadratic
Zeeman shift, that is h > E RthemF= +1 internal
state is tuned out of resonance for the two photon Ra-
man coupling. The coupled system becomes an eective
two level system of spin-momentum states which we label
jmF= 1;~ky+ 2kRi=j"0iandjmF= 0;~kyi=j#0i.
EXPERIMENTAL PROCEDURE
The condensate is prepared in the lowest energy
dressed band of the Raman coupled system by adia-
batically increasing the Raman coupling to 5.5 ERover
50 ms, where there is a single minimum in the dispersion
curve as illustrated in Fig.2(a). The adiabatic increase of
the coupling prevents unwanted heating and oscillations
of the condensate in the trap caused by synthetic electric
elds [18]. We hold the Raman coupling on for a further
30 ms at a constant value in order to ensure the system is
in the lowest energy dressed band. We conrm that the
ramp is adiabatic by measuring the total momentum of
the atoms, obtained from the weighted sum of the quasi-
momentum of all momentum components, during this
30 ms period and conrming that it is zero at each point
in time. If the total momentum is non-zero during this
phase, the ramp speed must be adjusted to ensure the
atoms remain in the lowest energy dressed state.3
(a)
(b)
FIG. 2: Dispersion relations for the coupled BEC for
two coupling strengths. (a) h
R= 5:5ER, features a
single minima where both spins have equal populations
and the same quasimomentum. (b) h
R= 1ERfeatures
two minima of the dispersion. Each pseudospin occupies
one of the minima with the corresponding
quasimomentum.
To take the system out of equilibrium, a synthetic elec-
tric force is imparted on the dressed BEC by abruptly
reducing the Raman coupling strength from the initial
i= 5:5ER=hto a nal value
fin 1 ms. The rapid
decrease of Raman coupling constitutes a quench of the
system. The condensate separates into the two pseu-
dospin statesj"0iandj#0ithrough the synthetic electric
force, each accelerating towards one of the new minima
(see Fig. 2(b)) of the dispersion relation, where they then
oscillate in the harmonic trap with maximal momentum
jk";#j=1hkR.
To compensate for both the impact of the mF= +1
state and the changing AC stark shift as the laser in-
tensity changes, we adjust the laser frequency dierence
to maintain equal populations of the two states, by an
amount up to hAC= 1ER. This shift in the two pho-
ton resonance condition is extremely sensitive to small
changes in experimental parameters, such as the mag-
netic elds. Although care is taken to maintain equal
populations of the spin components, the nal spin-orbit
coupled state after the quench will occasionally have non-
equal populations in each component. To group the data
we calculate the population imbalance
F"#=N" N#
N"+N#; (2)
(a)
(b)FIG. 3: Plots of the momentum dierence between the
two components of the system for two coupling
strengths (a) h
f= 1:5ERand (b) h
f= 2ERt with
a decaying cosine function. The insets show the
spin-momentum distribution after the system has
returned to equilibrium, and clearly demonstrate the
return of the system to a spin orbit coupled state with
the nal momentum distribution re
ecting the non-zero
quasimomentum before release from the trap.
whereN"is the population of the mF= 1 state and
N#is the population of the mF= 0 state. In this paper
we focus on the case with balanced populations, where
jF"#j<0:1, by post-selecting the data.
We let the two pseudospin states oscillate in the dipole
trap for time tup to 20 ms before switching the trap and
Raman coupling o simultaneously, projecting the atoms
onto their bare spin-momentum states. The bare states
expand for 15 ms in a Stern-Gerlach gradient separat-
ing the spin components in the xdimension before being
imaged with a resonant absorption method.
We measure the rate of thermalization of the system by
evaluating the momentum distribution of both spin states
as a function of time. We numerically determine the
mean momentum of each of the spin ensembles as they
oscillate in the trap with a decaying amplitude. We t
the decay of the oscillation of the momentum dierence
kt=jk" k#jand measure the nal temperature of the
thermalized ensembles.4
THERMALIZATION OF A SPIN-ORBIT
COUPLED BEC
It is important to note that the momentum imparted
on the pseudospins during the quench depends of the
nal coupling strength, which arises from the quasimo-
mentum minima shifting as a function of the coupling
strength. The shift in this work on the order of 0:05hk
for each spin, accounting for a 5% dierence in the total
momentum of the atoms of h
f= 0 and h
f= 2ER
Once the system has thermalized and the oscillations
have completely damped, a small fraction of the conden-
sate remains, with the atoms occupying the minima of
the new spin-orbit coupled band. For Raman coupling
above h
R= 1ERthe time-of-
ight images show clearly
the system has returned to equilibrium in a spin-orbit
coupled state with the pseudospin momentum clearly be-
ing non-zero. We conrm the non-zero momentum of the
atoms comes from the quasimomentum of the spin-orbit
coupled state, rather than residual oscillation energy, by
noting the momentum remains unchanged over 5 ms of
evolution.
Fig. 3 demonstrates two cases where the nal pseu-
dospins are separated from zero momentum when reach-
ing equilibrium. A clear example is shown in the in-
set of Fig. 3(b) shows the pseudospins are positioned
k";#=0:25hkR, corresponding to quasimomentum be-
fore release ~ky=0:75hkR, the locations of the disper-
sion minima obtained from exact diagonalization of the
Hamiltonian. Even though the trap frequencies are the
same for the two situations in the gure, the dispersion
relation is dierent for dierent coupling, giving rise to
the observed dierence in oscillation frequency. It is also
clear that the higher coupling strength (b) gives rise to
a stronger damping of the oscillation.
As mentioned, some data was also obtained for im-
balanced populations. In this case, qualitatively we ob-
serve that the smaller population oscillation damps more
rapidly while the larger population continues to oscil-
late. Accurately controlling the imbalanced populations
proves to be dicult and therefore we do not include
these results in this paper.
SPIN COULOMB DRAG
For a situation with no spin-orbit coupling, the damp-
ing coecient can be determined theoretically for an ul-
tracold Bose gas. The spin drag between two compo-
nents can be calculated from two expressions for the non-
condensed and the condensed atoms respectively [4],
22=na2
"#
h1
621
(n3)2Z1
0dqd!q2
sinh2(!=2)
ln
exp
q2=16+gn 0 !=2 +!2=q2
exp [ !]
exp [q2=16+gn 0 !=2 +!2=q2] 1!
;
(3)
and
12=na2
"#
h64n0a
3(2)3nZ1
0dp1dp3p1p3
3
1 +1
exp [(p2
1+p2
3)=4+ 2gn 0] 1
1
exp [p2
1=4+gn 0] 11
exp [p2
3=4+gn 0] 1
p1p3
2 gn 0
: (4)
Here, is the Heaviside function, =q
2h2=mk BT
is the thermal de Broglie wavelength, = 1=kBTthe
inverse thermal energy and g= 4h2a=2mthe interpar-
ticle interaction strength. Calculations were performed
using a script provided by Jogundas Armaitis [4] with our
experimental parameters, returning the total spin drag
relaxation rate for a given density of atoms. Due to the
fact the atoms are oscillating in the trap and only overlap
and only interact periodically, we multiply by a scaling
factor calculated based on the interaction time of the two
spin clouds overlapping in the trap.
At the time of writing we are unable to obtain theo-
retical calculations for the eects of the spin-orbit cou-
pling on the spin drag, so we compare the experiments for
the uncoupled case with the theory. For the ytrapping
frequencies !y= 285 s 1and!y= 2112 s 1,
we calculate a spin drag damping rate of
s=
12+
22=13.6 s 1. Comparing this to our experimentally
observed damping rate of
= 72(9) s 1, we observe that
part of
eis caused by collisions of the condensate with
thermal atoms, and is dependent on the atomic density
and is also present regardless of spin drag.
Taking into account the elastic collision rate, it is clear
from Fig. 4 that the increase in the spin-orbit coupling
corresponds to a signicantly increased damping rate,
with a linear dependence over the range measured. We
nd that the damping rate also scales with the calculated
spin-drag damping rate and e summarize our results for
the damping coecient
by the expression
=
e+
R
s (5)
whereis a constant. The t parameters in Fig. 4, as
well as the spin drag constant without spin-orbit coupling
are summarised in table I.5
0.0 0.5 1.0 1.5 2.0
Final Coupling Strength (ER)050100150200250Damping rate (S1)
FIG. 4: The damping rate of the system as a function of
the Raman coupling strength, for low (green circles) and
high (red crosses) trapping frequencies. The damping
increases linearly over the range of coupling, with the
gradient being a combination of both collisional
damping and spin drag. The red and green dashed lines
indicates the theoretical spin drag damping rates.
!y=2(s 1)
e(s 1)
s
s(s 1)
85 18(6) 63(4) 6.4
112 67(14) 107(13) 13.6
TABLE I: Scaling of the t parameters in gure 4
At the time of writing, we have not found a way to nd
from theoretical considerations for our experimental
conguration, but from table I we nd that = 8:9(6) s,
which is remarkably large as spin-orbit coupling aects
the condensate fraction much more strongly than the
thermal fraction. We envision that nding an accurate
theoretical value may take a truncated Wigner type simu-
lation [19, 20] to include both spin components, the spin-
orbit coupling along with their interactions with both the
opposing spin condensate atoms, but also the atoms be-
longing to the thermal cloud.
Finally, we measure the nal temperature of the system
once it has reached equilibrium. We integrate the time-
of-
ight region for each spin to obtain a 1D density prole
and t them with a sum of a Bose enhanced Gaussian and
a Thomas-Fermi prole. Integrating the ts we obtain
the atom number for the BEC and thermal component,
which we use to obtain the fractional temperature T/T c.
We plot the measured temperatures in Fig. 5 along with
the initial temperature and uncertainty. We t a straight
line to the temperature, obtaining T=Tc= 1:08(0:01)
0:11(0:02)
R.
It is interesting to note that the condensate is o cen-
1.0 1.2 1.4 1.6 1.8 2.0
Final Coupling Strength (ER)0.800.850.900.951.00Fractional Temperature (T/Tc)
FIG. 5: Fractional temperature T/T cof the system as a
function of the nal coupling strength. The blue line
shows the temperature before the quench averaged over
many shots, with the shaded region indicating the error.
The temperature of the equilibrium state is shown with
red circles, demonstrating a clear decrease in the
heating for larger coupling strengths. Inset: The
integrated 1D prole showing the bimodal t to one of
the spin components
ter with respect to the thermal cloud, consistent with
the quasimomentum of the nal spin orbit coupled state
mentioned in an earlier section. The results surprisingly
show that for increasing Raman coupling, the damping
results in a reduced nal temperature, possibly indicat-
ing the spin-orbit coupling plays a signicant role in the
relaxation process. The means by which the temperature
decreases is not so obvious, however the condensate frac-
tion remaining at the end of the experiment is increased
for increasing coupling.
CONCLUSION
We have presented experiments performed to investi-
gate the impact of spin-orbit coupling on the thermal-
ization processes present in an out of equilibrium system
of ultracold bosons. We measure the spin drag damping
rate of the atoms and compare the uncoupled case to the-
oretical calculations. We show that introducing the spin-
orbit coupling into the system strongly increases the rate
at which the system returns to equilibrium, while also
reducing the temperature increase caused by the excita-
tion. Finally, we have shown that the equilibrium state
of the system after rethermalization is a spin-orbit cou-
pled BEC, with the quasimomentum measurements af-
ter reaching equilibrium corresponding to the dispersion6
relation calculated through exact diagonalization of the
Hamiltonian. We anticipate that this work will lead to
new understanding of thermalization in the presence of
spin-orbit coupling.
dylan.brown@oist.jp
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1606.04426v2.Modulation_instability_in_quasi_two_dimensional_spin_orbit_coupled_Bose_Einstein_condensates.pdf | Modulation instability in quasi two-dimensional spin-orbit coupled Bose-Einstein
condensates
S. Bhuvaneswari,1K. Nithyanandan,2P. Muruganandam,1and K. Porsezian2
1Department of Physics, Bharathidasan University, Palkalaiperur, Tiruchirappalli 620024, India.
2Department of Physics, Pondicherry University, Puducherry 605014, Puducherry, India.
We theoretically investigate the dynamics of modulation instability (MI) in two-dimensional spin-
orbit coupled Bose-Einstein condensates (BECs). The analysis is performed for equal densities of
pseudo-spin components. Dierent combination of the signs of intra- and inter-component interac-
tion strengths are considered, with a particular emphasize on repulsive interactions. We observe
that the unstable modulation builds from originally miscible condensates, depending on the com-
bination of the signs of the intra- and inter-component interaction strengths. The repulsive intra-
and inter-component interactions admit instability and the MI immiscibility condition is no longer
signicant. In
uence of interaction parameters such as spin-orbit and Rabi coupling on MI are
also investigated. The spin-orbit coupling (SOC) inevitably contributes to instability regardless
of the nature of the interaction. In the case of attractive interaction, SOC manifest in enhancing
the MI. Thus, a comprehensive study of MI in two-dimensional spin-orbit coupled binary BECs of
pseudo-spin components is presented.
PACS numbers: 05.45.Yv, 03.75.Lm, 03.75.Mn
I. INTRODUCTION
Study of spin-orbit (SO) coupled Bose-Einstein con-
densates (BECs) is one among the important topics of
current research in the context of macroscopic quantum
phenomena. Spin-orbit coupling (SOC) describes the in-
teraction between the particle's spin and orbital momen-
tum and plays a crucial role for many physical phenom-
ena in condensed matter systems including spin-Hall ef-
fect, topological insulators, spintronics and so on [1{6].
The synthetic SOC in BECs was experimentally achieved
very recently. In this realization techniques, two Ra-
man laser beams were used to couple with two compo-
nent BECs [7]. The momentum transfer between laser
beams and atoms leads to synthetic SOC [8{11]. SOC
has been realized with cold atomic gases by designat-
ing the hyperne atomic states as pseudo-spins and cou-
pling them with Raman laser beams [12{14]. For in-
stance, in the case of87Rb the pseudo-spin states are
j"i=jF= 1;mF= 0iandj#i=jF= 1;mF= 1i,
which are generated using pair of Raman laser beams.
SO coupled BECs have been studied extensively
in dierent contexts including phase separation, strip
phases [15], spotlighting the phase transition [16], vor-
tices with or without rotations [17], and so on. In ad-
dition, the study of topological excitations, for exam-
ple, skyrmions, has also attracted much along these di-
rections [18]. Further, matter wave solitons such as
bright and dark solitons have been studied in quasi-
one-dimensional with attractive and repulsive SO cou-
pled BEC [19, 20]. It should be noted that most of the
studies on SO coupled BECs were primarily focused on
quasi-one-dimensional systems. Only a few studies were
devoted on multi-dimensional SO coupled BECs. How-
ever, there were few important studies reported in the
context of two-dimensional SO coupled BECs, for in-
stance, the dynamics of vortices, the existence of vortex-antivortex pair, to mention few [21{25]. Recently, the
study on two-dimensional SO coupled BEC of mixed
Rashba-Dresselhaus type and Rabi couplings have earned
particular interest [26, 27]. Thus, it is more appropriate,
realistic and interesting to study SO coupled BECs in
two- and three-dimensions systems. Particularly, here
we emphasize on the study of instability of plane wave in
two-dimensional SO coupled BECs, in the framework of
MI analysis [21, 22].
The degree of instability in a BEC can be character-
ized by the MI. MI is an instability process and identied
as a requisite mechanism to understand various physics
eects in nonlinear systems. The phenomenon of MI was
rst observed in hydrodynamics by Benjamin and Feir
in 1967 [28]. In the same year, Ostrovskii predicted the
possibility of MI in optics [29] and later explained in de-
tail by Hasegawa et. al. in 1973 in the context of opti-
cal bers [30]. The MI is a general phenomenon occur-
ring in many nonlinear wave equation and is of particu-
lar interest in dispersive nonlinear systems. In conven-
tional dispersive nonlinear systems, MI manifest as a re-
sult of the constructive interplay between dispersion and
nonlinearity. Such that any deviation from the steady
state in the form of perturbation leads to an exponential
growth of the weak perturbation, resulting in a break-
up of the carrier wave into trains of soliton-like pulses
[31]. In addition, MI has been widely studied in various
branches such as
uid dynamics [28], magnetism [32],
plasma physics [33] and BEC [34].
In the context of BEC, the MI has been given consid-
erable importance over a long period of time, owing to
its fundamental and applied interest in various aspects.
In particular, MI has been found to be relevant in un-
derstanding the formation and propagation of solitonic
waves [35], and also apparent in explaining the domain
formation [36] and quantum phase transition [37]. MI has
been studied extensively in BECs for both single [38] andarXiv:1606.04426v2 [cond-mat.quant-gas] 15 Jun 20162
two-component systems [39], and realized experimentally
as well [40]. In the case of single-component BECs, the
MI has been found to be feasible only for attractive in-
teraction (self-focusing nonlinearity), in such case, the
phase
uctuations caused by MI leads to the formation
of soliton trains. However, the breakthrough work by
Goldstein and Meystre opens up the possibility of MI
even for the repulsive interactions [41], in similar lines to
the case of cross-phase modulation induced instability in
nonlinear optics [42, 44]. Thus, the two component BEC
nds particular interest in the study of MI, as it helps to
achieve instability even in repulsive interactions. In the
case of SO coupled BEC, the MI in one-dimensions was
recently explored in Ref. [45], and the higher dimensional
case is still an open problem. Thus, inspired by the spe-
cial features of SO coupling and the physical relevance
of two-component BEC system, we intend to study the
dynamical behavior of MI in SO coupled BEC in two-
dimensions. In this paper, we present a systematic study
of MI in quasi-two-dimensional SO coupled BECs with
the inclusion of Rashba and Dresselhaus SO couplings.
By considering small perturbation approximation, we ob-
tain linearized GP equation. Further, the interplay be-
tween dispersion and nonlinear eects have been studied
in terms of system parameters. We have also summa-
rized the growth of MI gain for dierent combinations
of intra- and inter-component of interaction strengths in
the presence and absence of SO coupling.
The organization of the paper is as follows: After a
detailed introduction in Sec. I, the Sec. II features the
theoretical model for the case of SO coupled BECs. In
Sec. III, we present the MI dispersion relation through
linear stability analysis, and systematically explained the
eect of SOC and Rabi coupling for a dierent combina-
tion of inter- and intra-component interactions strength.
Sec. IV, features the results and discussion followed by
conclusion in Sec. V.
II. THEORETICAL MODEL
We consider the spin-orbit coupled Bose-Einstein con-
densates conned in a harmonic trap with equal Rashba
and Dresselhaus couplings described, within the frame-
work of mean eld theory by an energy functional of the
following form [7]
E=Z+1
1"d~xd~y; (1)
where,
"=1
2
yH0 + ~g11j "j4+ ~g22j #j4+ 2~g12j "j2j #j2
;
(2)
= ( "; #)Tis the condensate wave function, "and
#are associated with the pseudo-spin components. Themodel Hamiltonian H0in Eq. (2) assumes the form,
H0=^p2
2m+V(~r)
+~
2x ~~kL
m^p~xz (3)
where, ^p= i~(@~x; @ ~y) is the momentum operator,
V(~r) =1
2m[!2
?(~x2+ ~y2) +!2
z~z2] is a quasi-2D harmonic
trapping potential where !z!?,is the frequency of
Raman coupling, x;zare Pauli spin matrices and ~kLis
the wave number of the Raman laser which couples the
two hyperne states. The eective two dimensional cou-
pling constant ~ gij= 4~2aij=m, (i;j= 1;2) represents
the intra- (~ g11;~g22) and inter- component (~ g12) interac-
tion strengths, which are dened by the corresponding
s-wave scattering lengths aijand atomic mass m. Mea-
suring energy in units of the radial trap frequency ( !?),
i.e.,~!?, length in units of harmonic oscillator length,
a?=p
~=(m!?), and time in units of ! 1
?the follow-
ing dimensionless Gross-Pitaevskii (GP) equations can
be derived for dierent components of 1;2from Eq. (2)
as [43]
i@ 1
@t=
1
2r2
?+V(r) +g11j 1j2+g12j 2j2
1
+ ikL@
@x 1+ 2; (4a)
i@ 2
@t=
1
2r2
?+V(r) +g22j 2j2+g12j 1j2
2
ikL@
@x 2+ 1; (4b)
where,V(r) = (x2+y2)=2,x= ~x=a?,y= ~y=a?,t=
!?~t,kL=~kLa?, ==2!?,gij= 4Naij=a?and
1;2= ";#a3=2
?=p
N. In the following, we shall proceed
with the study of modulational instability in the above
two-dimensional model Eq. (4) for spin-orbit coupled
BECs.
III. ANALYSIS OF MODULATION
INSTABILITY
A. Linear Stability Analysis
The fundamental framework of MI analysis relies on
the linear stability analysis (LSA), such that the steady
state solution is perturbed by a small amplitude/phase,
and then study whether the perturbation amplitude
grows or decays [31]. For this purpose, we consider a
continuous wave (CW) state of the miscible SO coupled
BECs with the two-dimensional density nj0=j j0j2of
the form
j(x;y;t ) =pnj0e it: (5)
Then the stability of the SO coupled BECs can be exam-
ined by assuming the perturbed wave functions as
j(x;y;t ) = (pnj0+j) e it; (6)3
A set of linearized equations for the perturbation can be
obtained by using Eq. (6) in Eq. (4)
i@(1)
@t= 1
2@2(1)
@x2+@2(1)
@y2
+ ikL@(1)
@x
+
2 rn20
n10(1)
+g11n10(1+
1)
+g12pn10n20(2+
2); (7a)
i@(2)
@t= 1
2@2(2)
@x2+@2(2)
@y2
ikL@(2)
@x
+
1 rn10
n20(2)
+g22n20(2+
2)
+g12pn10n20(1+
1); (7b)
where the symboldenotes complex conjugate. Assum-
ing a general solution of the form
j=jcos (kxx+kyy
t) + ijsin (kxx+kyy
t);
(8)
wherekxandky, are the wavenumbers and jandj(j=
1;2) are the amplitudes of wavefunction, and
is the
eigenfrequency. We further assume that two pseudo-spin
states of equal density n10=n20=n. A straightforward
substitution of Eq. (8) in Eq. (7) yields the following
dispersion relation for
.
4
21
4(K 2 ) (2K+G1+G2) + 2k2
xk2
L+ 2 G12
+
2kxkL(K 2 )(G1 G2)
+K
k2
L
k2
xk2
L+ 2 G12 1
4(K 2 ) (2K+G1+G2)
+K
4 1
4(K+G1)(K+G2) G2
12
1
2k2
Lk2
y2 K
2(G1+G2 4 ) + 2k2
Lk2
x K2
+ 4 (G12+K )
= 0; (9)
whereK=k2
x+k2
yandG1= 4g11n 2 ,G2= 4g22n 2 ,
andG12= 2g12n+ are the modied intra- and inter-
components interaction strengths, respectively. For equal
strengths of intra-component interactions, i.e., a11=a22
(g11=g22=g), the dispersion relation recast into a
simpler form as
2
=1
2
p
2+ 4
; (10)
with
=1
2(K 2 ) (K+G) + 2k2
xk2
L+ 2 G12;(11a) =1
2k2
Lk2
y
(2 K)(G 2 ) + 2k2
Lk2
x K2
+ 4 (G12+K )
K
k2
L
k2
xk2
L+ 2 G12 1
2(K 2 ) (K+G)
+K
4 1
4(K+G)2 G2
12
; (11b)
where,G1=G2=G. The above Eq. (10) is the disper-
sion relation corresponding to the stability of the miscible
SO coupled BECs. As it is known from the theory of MI,
the system exhibit stable conguration for all real val-
ues ofkxandky, if
2
is positive (
2
>0). If > 0,
the eigenfrequency
+is always real but
may be real
or imaginary, which is dependent on . If the eigenfre-
quency
has an imaginary part, the spatially modu-
lated perturbation become exponential with time, as it
is obvious from the form of j. On the other hand, for
negative value of (<0),
2
need not to be positive.
In such case,
2
is characterized by the values of . For
>0 the value of lower branch
2
is negative if, <0.
Similarly for >0 the value of upper branch
2
+is neg-
ative when <0. Regardless of anything
2
is always
negative, and therefore, the MI sets in via the exponen-
tial growth of the weak perturbations. The MI growth
rate is dened as jIm(
)j. Following the mathe-
matical calculation pertaining to the dispersion relation
corresponding to the stability/instability of the system,
the subsequent sections are dedicated to the study on the
eect of SOC in the MI.
B. Eect of Rabi coupling in the MI of SO coupled
BECs
In order to study the eect of Rabi coupling in the
MI, we turn o the SOC by making kL= 0. For better
insight, we consider two special cases, (i) one without
Rabi coupling ( = 0) and (ii) other in the presence of
Rabi coupling ( 6= 0).
1. Zero Rabi coupling
In absence of Rabi coupling ( = 0), the eigenfre-
quency of the system for kx6=kyassumes the form,
2
=1
2[K(K+ 2n(gg12))] (12)
One can infer from the above Eq. (12), that based on
the sign/nature of the interaction strength, the
may
be real or imaginary. It is obvious from the combination
of signs of intra and inter-component interactions,
+is
found to be real in the following cases:
(i) both intra- (g) and inter- (g 12) component interac-
tions are repulsive,4
(ii) attractive intra-component and repulsive inter-
component interactions, and
(iii) repulsive intra-component and attractive inter-
component interactions.
For attractive intra- and inter-component interactions
+becomes imaginary and thereby inevitably con-
tributes to MI. However,
becomes imaginary for all
cases. Thus, as far as MI is concern,
contribute better
to the instability in all means than the
+counterpart.
It is worth mentioning, at ky= 0, our results completely
agree with the Ref. [45], and could reproduce the results
of the MI in the conventional two-component system as
in Ref. [39].
2. Non-zero Rabi coupling
Next, we study the eect of Rabi coupling on MI by
considering any nite value for ( 6= 0). Here the
dispersion relation as given by Eq. (10) can be modied
as follows
2
+=1
2[K(K+ 2n(gg12))]:; (13)
withkx6=ky, and in order to highlight the eect of Rabi
coupling, the coecient of SOC is turned o, i.e., kL= 0.
It is straightforward to notice that
2
+given by Eq. (13)
for = 0 is similar to Eq. (12) for the case of zero Rabi
coupling. Therefore, the instability/stability condition as
dened by the zero Rabi coupling in the earlier section is
completely applicable here as well. Hence, for non-zero
Rabi coupling,
2
+is not dierent from that of zero Rabi
coupling, which implies that
2
+is independent of . On
the other hand,
2
is found to be signicantly in
uenced
by Rabi coupling and can be expressed as
2
=K2
4+ (Kn 4 ) (g g12) + 2 (2 K):(14)
The eect of Rabi coupling from Eq. (14) can be better
explored for three representative cases of , namely (i)
= 0, (ii) >0, and (iii) <0. For = 0, Eq. (14)
reverts to the expression for
as given by Eq. (12),
and therefore, will not be discussed again here. Our par-
ticular focus is on = 0 and >0. For <0,
is
imaginary only for repulsive intra- and attractive inter-
component interaction, and for all other cases
does
not contribute to MI, as it is real. However, the eect
of Rabi coupling is more pronounced for >0, as the
instability/stability conditions qualitatively dier from
the previous cases. It is found that the
is unsta-
ble for all combination interactions, except the repulsive
intra- and attractive inter-component interaction. Per-
haps, the magnitude of intra- and inter-component inter-
action strengths are rather identied to be deterministic
for MI. It is observed that for repulsive intra- and inter-
component interactions the instability is possible onlywhenjgj>jg12j. Similarly, for attractive interaction, the
condition for MI can be modied as jg12j>jgj.
For a better understanding of the eect of Rabi cou-
pling, as a representative case, we have shown in Fig. 1,
the MI gain corresponding to the repulsive intra- and
inter-component interactions with kL= 0, = 1, g= 2,
g12= 1 andn= 1. It should be noted, the condition for
instability (jgj>jg12j) in repulsive interactions is true for
the above choice of parameters. It is evident, from the
−3−2−10123kx−3−2−10123
ky00.250.50.751ξ
00.20.40.60.81
−3.0−1.50.0 1 .5 3 .0
kx−3.0−1.50.01.53.0ky
0.00.51.0
(a) (b)
FIG. 1. (color online) (a) Three-dimensional (3D) surface plot
showing the MI gain, =jIm(
)j, and (b) the corresponding
two-dimensional (2D) contour plot for the parameters kL= 0,
= 1,n= 1,g= 2 andg12= 1.
existence of instability region, that the MI is caused by
Rabi coupling for repulsive intra- and inter-component
interactions. It should be noted that the instability re-
gion is symmetric in momentum space on either side of
the wave numbers, kxandky.
Overall, it is apparent from the above discussion on the
in
uence of Rabi coupling in the instability that out of
the dierent choices of Rabi coupling strengths, the con-
dition >1 is found to carry more information about
the MI. Therefore, in the subsequent section we shall
study the eect of SO coupling by xing the Rabi cou-
pling strength as = 1.
IV. THE EFFECT OF RABI AND SPIN-ORBIT
COUPLING
One can draw out a conclusion from the previous sec-
tion, that the sign/nature of the interaction signicantly
in
uences the stability/instability of the system. For bet-
ter insight, in the following section, we would like to
brie
y emphasize the eect of dierent combinations of
intra- and inter- component interaction strength with the
inclusion of both Rabi ( 6= 0) and SOC ( kL6= 0). We
consider following four representative cases to study MI
in the SO coupled BEC system.
A. Both repulsive intra- and inter- component interac-
tions (g>0,g12>0).
B. Attractive intra- and repulsive inter- component in-
teractions ( g<0,g12>0).
C. Repulsive intra- and attractive inter- component in-
teractions ( g>0,g12<0).5
D. Both attractive intra- and inter- component inter-
actions (g<0,g12<0).
A. Repulsive intra- and inter-component
interactions
Here, we consider self repulsive intra- ( g >0) and re-
pulsive inter- ( g12>0) components of modied interac-
tionsG1;G2andG12. Our investigation follows from the
general dispersion relation for non-zero SO and Rabi cou-
pling as given by Eq. (10). It is apparent from Eq. (10),
the expression
can be real or complex depends on the
sign of>0 and2+ 4. For>0, the upper branch
+will be imaginary only for 2+ 4<0, and there-
fore contribute to MI. Fig. 2 shows the MI gain for
+
−1.5−1.0−0.5 0.0 0.5 1.0 1.5
ky0.00.10.20.30.40.5ξMiscibleImmiscible
g= 0.2
g= 0.5
g= 0.6
g= 0.8
g= 1.0
FIG. 2. (color online) Plot of the MI gain, =jIm(
+)j,
as a function of kyfor dierent intra-component interaction
strengths with kL= 1, = 1, n= 1,g12= 1 andkx= 1.
as a function of one of the momentum component ( ky)
for dierent values of intra-component ( g) at xed inter-
component interaction strength ( g12= 1). The choice of
parameters are kL= = 1,n= 1,g12= 1 andkx= 1.
It is evident from Fig. 2, there exist two symmetrical in-
stability region on either side of the zeros of kxandky.
As the intra-component interactions strength increases
further, the two instability region approaches to the zero
wave number and merge into a single coalesced instability
region with elevated gain at higher values of g.
On the other hand,
from Eq. (10) is more in-
teresting, since
leads to unstable region even for
2+ 4>0. Fig. 3 shows the MI gain for
as a
function of momentum component for similar values as
used for
+. One can straightforwardly notice, that there
exist two pairs of instability region for
as against, the
single pair of instability region observed for the case
+.
As the strength of the intra- component interaction in-
creases, the instability region at the center unies into
single band (similar to the case of
+), while the other
−3−2−1 0 1 2 3
ky0.00.20.40.60.81.0ξMiscibleImmiscible
g= 0.2
g= 0.5
g= 0.6
g= 0.8
g= 1.0FIG. 3. (color online) Plot showing the MI gain, =jIm(
)j
as a function of kyfor dierent gwithkL= 1, = 1, n= 1,
g12= 1 andkx= 1.
pair of instability region at higher values of kysubstan-
tially decreases in gain and width of the instability re-
gion. For insight, we plot in Fig. 4 the 3D variation of
−4−2024 kx012345
g00.51ξ
00.20.40.60.81
−4−20 2 4
kx012345g
0.00.51.01.2
(a) (b)
FIG. 4. (color online) 3D surface plot of the MI gain,
=jIm(
)jin thekx-gplane and (b) the corresponding
2D contour plot for kL= 1, = 1, n= 0:3,g12= 1 and
ky= 1.
MI gain for a range of kxandgwith the inter-component
interaction xed ( g12). It is obvious that the two insta-
bility regions merge into a single instability region with
elevated gain. To explore the eect of inter-component
−4−2024 kx012345
g1200.511.3ξ
00.40.81.2
−4−20 2 4
kx012345g12
0.00.51.01.3
(a) (b)
FIG. 5. (color online) 3D surface plot showing the MI gain,
=jIm(
)j, in thekx g12plane and (b) the corresponding
2D contour plot for the parameters kL= 1, = 1 for n= 0:3,
g= 1 andky= 1.
interaction in the instability, in Fig. 5, we depict the MI6
gain for a range of g12with xedg. It is apparent from
Fig. 5, for smaller values of g12, the gain in the inner in-
stability band decreases gradually to zero, while the gain
in the instability region at higher values of kxgrows with
increase in g12. In order to explore the eect of the wave
numbers,kxandky, we plot the MI gain as a function of
kxfor dierent values of kyand vice-versa. Figs. 6 and
0 1 2 3
kx0.00.10.20.30.40.50.6ξMiscibleImmiscible
ky= 0.5
ky= 1.0
ky= 1.5
ky= 2.0
FIG. 6. (color online) Plot showing the MI gain, =jIm(
)j
as a function of kxfor dierent kyvalues with kL= 1, = 1,
n= 0:3g= 1 andg12= 2.
0.0 0.5 1.0 1.5 2.0 2.5
ky0.00.10.20.30.40.50.6ξMiscibleImmiscible
kx= 0.5
kx= 1.0
kx= 1.5
kx= 2.5
FIG. 7. (color online) Plot of the MI gain, =jIm(
)jas
a function of kyfor dierent kxvalues with kL= 1, = 1,
n= 0:3,g= 1 andg12= 2.
7 show that the MI bands drift towards the center and
coalesced into single instability band with the increase
in the wave numbers. Thus, there are no changes in the
general trend of shifting of MI band for both cases, how-
ever the peak gain and the width of instability region
substantially diers. One can infer that the maximum
gain is observed for kxas evident from Fig. 6 in compar-ison to the plot of MI gain for kyin Fig. 7. Fig. 8 shows
−3−1.501.53ky−3−1.501.53
kx00.20.40.6ξ00.20.40.6
−3.0−1.50.0 1 .5 3 .0
kx−3.0−1.50.01.53.0ky
0.00.20.40.6
(a) (b)
FIG. 8. (color online) (a) 3D surface plot showing the MI
gain,=jIm(
)j, and (b) the corresponding 2D contour
plot for the parameters kL= 1, = 1, n= 0:3,g= 5 and
g12= 3.
the instability gain on the momentum space as a func-
tion ofkxandkyfor some representative values of intra-
and inter-components interaction strength. It is observed
that there exist two instability bands corresponding to kx
andky. The inner pair of bands corresponds to kxwith
slightly higher gain than the outer band as a result of
ky. This combination of intra- and inter-components in-
teraction is of particular interest, because the instability
is generally not feasible, as both interaction components
are repulsive and therefore does not contribute to MI.
However, the above results suggest that the MI is still
possible even in the repulsive two component BEC with
the aide of SOC.
B. Attractive intra-component and repulsive
inter-component interactions
This condition corresponds to the binary BEC with at-
tractive intra- component and repulsive inter-component
interactions, which is subject to the MI even in the ab-
sence of the SOC. Although SOC is not fundamental to
the occurrence of MI in this particular case, but signif-
icantly aects the instability. The MI corresponding to
+produces the same number of bands as in the previ-
ous case for repulsive interaction. However, the MI corre-
−4−2024 kx−5−4−3−2−10
g00.51ξ
00.511.2
−4−20 2 4
kx−5−4−3−2−10g
0.00.51.01.2
(a) (b)
FIG. 9. (color online) 3D surface plot of the MI gain,
=jIm(
)jin thekx-gplane and (b) the corresponding
2D contour plot for xed g12withkL= 1, = 1, n= 0:3,
g12= 1 andky= 1.
sponding to
qualitatively diers, and it can be better
explained in the following two combinations, namely, (i)7
MI gain as a function of gfor xedg12, and (ii) vari-
ation of MI gain as a function of g12at constant value
ofg. Fig. 9 shows the possibility of three pairs of instabil-
ity bands for attractive intra-component at constant g12,
and the instability bands grow in gain with the increase
ing. Fig. 10 depicts the MI gain for a range of repulsive
−4−20 2 4
kx0
2
4
6
8
10g12
0123
−4
−2
0
2
4kx0
2
4
6
8
10g120123ξ0 1 2 3
(a) (b)
FIG. 10. (color online) 3D surface plot of the MI gain,
=jIm(
)jin thekx-g12plane and (b) the corresponding
2D contour plot for xed gwithkL= 1, = 1, n= 0:3,
g= 1 andky= 1.
inter-component interaction strength ( g12) at constant g.
It is obvious, there exist two pairs of instability bands on
either side of ky, the inner one decreases with increase in
g12, while the outer own grow with the increase in g12.
The instability gain in momentum space for some repre-
sentative value of intra- and inter-components interaction
strength is shown in Fig. 11. It is observed that there ex-
−4−2024ky −4−2024
kx00.511.52ξ
00.511.5
−4−20 2 4
kx−4−2024ky
0.00.51.01.5
(a) (b)
FIG. 11. (color online) (a) 3D surface plot showing the MI
gain,=jIm(
)j, and (b) the corresponding 2D contour
plot for the parameters kL= 1, = 1, n= 0:3,g= 5 and
g12= 1.
ist three symmetric instability bands corresponding to
kx, while only two for ky. Unlike the previous case, the
instability gain is maximum for the bands corresponding
tokyas shown in Fig. 11.
C. Repulsive intra-component and attractive
inter-component interactions
Here, we consider the binary BEC with repulsive intra-
component ( g>0) and attractive inter-component inter-
actiong12<0. It is obvious from our earlier discussion,
in the absence of Rabi and SO coupling, the MI (through
) is observed provided the condition jg12j>jgjis sat-
ised. But in the presence of SO coupling, the MI is said
to occur regardless of the sign of the interaction strength
and there are no conditions imposed. In similar lines withthe previous section, we discuss MI in the two particular
cases, i.e. constant intra-component interaction strength
with varying inter-component strength and vice-versa.
Fig. 12 shows the MI gain at constant gas a function of
−4−2024 kx−5−4−3−2−10
g1200.511.5ξ
00.511.5
−4−20 2 4
kx−5−4−3−2−10g12
0.00.51.01.5
(a) (b)
FIG. 12. (color online) 3D surface plot of the MI gain,
=jIm(
)jin thekx-g12plane and (b) the corresponding
2D contour plot for xed gwithkL= 1, = 1, n= 0:3,g= 1
andky= 1.
g12. As the strength of the inter-component interaction
increases, the outer instability band grows and merges
with inner instability band of higher gain. The variation
−4−2024 kx012345
g00.511.5ξ
00.511.5
−4−20 2 4
kx012345g
0.00.51.01.5
(a) (b)
FIG. 13. (color online) 3D surface plot of the MI gain,
=jIm(
)jin thekx-gplane and (b) the corresponding
2D contour plot for xed g12withkL= 1, = 1, n= 0:3,
g12= 1 andky= 1.
of MI gain for g12at constant gshows a similar trend, ex-
cept the changes in the numerical value of gain as shown
in Fig. 13. Fig. 14 depicts the MI gain in momentum
space forkxandky. Unlike the earlier cases, the gain of
−4
−202
4ky −4−2024
kx0123ξ
0123
−4−20 2 4
kx−4−2024ky
0123 3
(a) (b)
FIG. 14. (color online) (a) 3D surface plot showing the MI
gain,=jIm(
)j, and (b) the corresponding 2D contour
plot for the parameters kL= 1, = 1, n= 0:3,g= 2 and
g12= 13.
the inner band is quantitatively same for both bands cor-
responding to kxandky. However, the instability gain
of the outer band corresponding to kyis slightly larger
than the outer band of ky.8
D. Attractive intra-and inter-component
interactions
In this region, both intra- and inter-component interac-
tions are attractive, i.e. g<0 andg12<0, and therefore,
MI occurs naturally even without the aide of Rabi and
SOC. This case has already been discussed thoroughly in
the context of MI in two component BEC, and hence, an
extensive investigation is needless. However, for the sake
of completeness, we focus on the eect of SOC in the in-
stability. Fig. 15 shows that the growth of MI gain with
−4−2024kx−5−4−3−2−10
g00.511.5ξ0 0 .5 1 1 .5
−4−20 2 4
kx−5−4−3−2−10g
0.00.51.01.5
(a) (b)
FIG. 15. (color online) 3D surface plot of the MI gain,
=jIm(
)jin thekx-gplane and (b) the 2D corresponding
contour plot for xed g12withkL= 1, = 1, n= 0:3,
g12= 1, andky= 1.
the variation of g12for constant g= 1. The current
case completely concur with our earlier discussion, and
the MI becomes independent of the gfor the strong g12
interaction. The variation of MI gain in momentum space
is shown in Fig. 16. Like in the previous section, the MI
−4−20 2 4
kx−4−2024ky
0.00.51.01.5
(a) (b)−4
−2
0
2
4ky −4−2024
kx00.511.5ξ00.511.5
FIG. 16. (color online) (a) 3D surface plot showing the MI
gain,=jIm(
)j, and (b) the corresponding 2D contour
plot for the parameters kL= 1, = 1, n= 0:3,g= 1,
g12= 5.
bands are symmetric across the zero wave number, and
the maximum gain occurs for the bands corresponding to
ky.
E. Results and Discussion
For the ease of understanding and to make the analysis
self-explanatory, we summarize our results of MI in the
two-dimensional SO coupled two-component BEC in Ta-
ble I. We systematically discussed the presence/absence
of SO/Rabi coupling under dierent combination of signs
of intra- and inter-component interaction strength. Asit is evident from our extensive investigation that SO
coupling inevitably destabilizes the initial steady state
for equal densities of binary BEC, and thereby makes
the system unstable for all combinations of interaction
strength. Also, we have shown the conventional MI im-
miscibility condition, g12> g for repulsive two compo-
nent BEC system is no longer signicant for MI. Our par-
ticular focus is on repulsive intra- and inter-component
interaction, as it is proven to be stable against the pertur-
bation, and therefore, MI is generally not feasible. How-
ever, we have shown that MI can be achieved with the
eect of SOC as demonstrated through Figs. 2 - 8. We
discussed the MI gain in momentum space as a function
ofkxandkyand emphasize the variation of gain over
the wave numbers in the two directions. We noted that
the MI gain is not identical on kxandky, and signicant
changes in MI gain, width of instability region and the
number of instability bands are readily observed.
In Sec. IV B, we discussed the MI condition for attrac-
tive intra- and repulsive inter-component interactions.
Figs. 9 - 11 show the instability gain as a function of
gandg12. One can straightforwardly observe the emer-
gence of new instability bands in the MI gain plot, which
is identied to be the consequence of the incorporation
of SOC. Following that, we discussed in Sec. IV C, the
MI scenario in the case of repulsive intra- and attractive
inter-component interactions. Figs. 12 - 14 portray the
variation of MI gain for gandg12. Along the similar
lines with the earlier cases, the SOC results in new in-
stability bands and thereby help in enhancing the MI in
such systems. Finally, we studied MI in attractive intra-
and inter-component interactions in Sec. IV D. It is very
well known from the theory of MI in BEC, that attrac-
tive interactions naturally support MI. Although, SOC
is not fundamental for the origin of MI, however, SOC
signicantly in
uences the instability region in terms of
peak gain and width as evident from Figs. 15 and 16.
Overall, the eect of SOC can be understood as a means
to achieve MI in repulsive interactions, and also enhance
instability in the system.
Last but not least, it is also important to see the impact
of SO and Rabi couplings on MI gain for xed wavenum-
berskxandky. Fig. 17 depicts the MI gain as a func-
−4−2024Γ −4−2024
kL00.20.40.6ξ
00.20.4
−4−20 2 4
Γ−4−2024kL
0
(a) (b)
FIG. 17. (color online) (a) 3D surface plot showing the MI
gain,=jIm(
)j, and (b) the corresponding 2D contour
plot for the parameters kL= 1, = 1, g= 1,g12= 1,
n= 0:3,kx= 2 andky= 1.
tion of SO and Rabi coupling. As it is evident from our9
TABLE I. Summary of MI in SO coupled two dimensional binary BEC
SO coupling Rabi coupling MI gain Dierent combinations Inference
both interaction are repulsive Always stable
g<0,g12>0 Always stable
+g>0,g12<0 Always stable
both interaction are attractive Always unstable
= 0 both interaction are repulsive
g<0,g12>0 stable for all cases
g>0,g12<0
both interaction are attractive
both interaction are repulsive
g<0,g12>0 Similar to the case
+g>0,g12<0 with = 0 and
+
both interaction are attractive
kL= 0 <0 both interaction are repulsive Always stable
g<0,g12>0 Always unstable
g>0,g12<0 Always stable
both interaction are attractive Always stable
both interaction are repulsive
g<0,g12>0 Similar to the case
+g>0,g12<0 with = 0 and
+
both interaction are attractive
>0 both interaction are repulsive Unstable ifjgj>jg12j
g<0,g12>0 Always stable
g>0,g12<0 Always unstable
both interaction are attractive Unstable ifjg12j>jgj
both interaction are repulsive Always stable
g<0,g12>0 Unstable ifjg12j>jgj
+g>0,g12<0 Always stable
both interaction are attractive Unstable ifjgj>jg12j
= 0 both interaction are repulsive Unstable ifjg12j>jgj
g<0,g12>0 Always unstable
g>0,g12<0 Unstable ifjgj>jg12j
both interaction are attractive Always unstable
both interaction are repulsive
g<0,g12>0 stable for all cases
+g>0,g12<0
both interaction are attractive
kL= 1 <0 both interaction are repulsive Always stable
g<0,g12>0 Always unstable
g>0,g12<0 Unstable ifjgj>jg12j
both interaction are attractive Always unstable
both interaction are repulsive Always unstable
g<0,g12>0 Always unstable
+g>0,g12<0 Unstable ifjgj>jg12j
both interaction are attractive Always unstable
>0 both interaction are repulsive
g<0,g12>0 Always unstable
g>0,g12<0
both interaction are attractive
choice of parameters, the instability bands are symmetric for both positive and negative values of the Rabi and SO10
coupling. One can also infer, that the MI is possible even
for zero SOC, provided the Rabi coupling is >0.
V. CONCLUSIONS
To summarize, we investigated the dynamics of MI
gain in two-dimensional SO coupled binary BEC at an
equal density of pseudo-spin components. The disper-
sion relation corresponding to the instability of the
at
CW background against small perturbation was stud-
ied using linear stability analysis. For a comprehensive
study, we consider all the possible combination of signs
of intra- and inter-component interactions, with a partic-
ular, emphasize on repulsive interactions. Our analysis
illustrates that SOC inevitably contributes to instability,
regardless of the nature of the interaction strength. With
detailed interpretation, we have shown that the repulsive
intra- and inter-component interaction admit instability
and the MI immiscibility condition g12> gis no longer
essential for MI. We also have shown, for the strong at-
tractive inter-component interaction, the nature of the
intra- component interaction is immaterial for constantSO and Rabi coupling. We also analyzed the variation
of instability domain in momentum space for kxandky.
The MI gain is not identical on kxandky, and signicant
changes in MI gain and a number of bands are observed.
In the case of systems naturally admitting MI (attractive
interactions), the SOC and Rabi coupling manifest in the
generation of new instability bands, thereby enhances the
MI. Thus, we presented a comprehensive analysis with
detailed interpretation and graphical illustration of MI in
two-dimensional SO coupled binary BEC for equal den-
sities. We believe, the aforementioned results could po-
tentially provide new ways to generate and manipulate
MI and solitons in two-dimensional BECs.
ACKNOWLEDGMENTS
The work of PM forms a part of Science & Engi-
neering Research Board, Department of Science & Tech-
nology, Government of India sponsored research project
(No. EMR/2014/000644). KP thanks the DST, IFC-
PAR, NBHM, and CSIR, Government of India, for the
nancial support through major projects.
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2311.00362v1.Theory_of_Orbital_Pumping.pdf | Theory of Orbital Pumping
Seungyun Han∗∗,1Hye-Won Ko∗∗,2Jung Hyun Oh,2Hyun-Woo Lee,1,∗Kyung-Jin Lee,2,†and Kyoung-Whan Kim3,‡
1Department of Physics, Pohang University of Science and Technology, Pohang 37673, Korea
2Department of Physics, Korea Advanced Institute of Science and Technology, Daejeon 34141, Korea
3Center for Spintronics, Korea Institute of Science and Technology, Seoul 02792, Korea
We develop a theory of orbital pumping, which corresponds to the emission of orbital currents from orbital
dynamics. This phenomenon exhibits two distinct characteristics compared to spin pumping. Firstly, while
spin pumping generates solely spin (angular momentum) currents, orbital pumping yields both orbital angular
momentum currents and orbital angular position currents. Secondly, lattice vibrations induce orbital dynamics
and associated orbital pumping as the orbital angular position is directly coupled to the lattice. These pumped
orbital currents can be detected as transverse electric voltages via the inverse orbital(-torsion) Hall effect,
stemming from orbital textures. Our work proposes a new avenue for generating orbital currents and provides a
broader understanding of angular momentum dynamics encompassing spin, orbital, and phonon.
Introduction.– Orbital transport in solids has recently at-
tracted considerable theoretical and experimental interest be-
cause nonequilibrium orbital quantities arise from strong
crystal field coupling rather than weak spin-orbit coupling
(SOC) [1]. It results in intriguing phenomena associated
with orbital angular momentum (OAM), including the or-
bital Hall effect [2–11] and orbital magnetoresistance [12, 13].
In the presence of SOC, these OAM-related phenomena are
intimately connected to spin-related ones; the spin Hall ef-
fect [14, 15] and spin magnetoresistance [16]. Moreover, anal-
ogous to spin torque, which arises from spin injection into a
ferromagnet [17, 18], the injection of OAM into a ferromagnet
results in orbital torque [19–24] contributing to the net mag-
netic torque. These findings underscore the electron’s orbital
as an essential degree of freedom for understanding angular
momentum transport in solids and realizing novel orbitronic
devices.
Despite its importance, identifying orbital transport presents
challenges because OAM shares the same symmetry opera-
tions with spin. Symmetry-wise, distinguishing OAM from
spin is thus impossible. Consequently, previous experi-
ments have relied on the quantitative difference between spin
Hall and orbital Hall conductivities to identify the orbital
physics [11, 13, 21–24]. While the spin Hall conductivity
is significant only in a limited number of materials, the orbital
Hall conductivity is large in a broad range of materials and
often surpasses the maximum value of spin Hall conductiv-
ity [8, 25].
Although these quantitative differences are valuable, qual-
itative differences between the orbital and spin properties are
crucial for understanding orbital physics and its unambigu-
ous identification. In this regard, orbital angular position
(OAP), which describes different aspects of orbital states from
OAM [26], emerges as a crucial element for such qualitative
distinctions. It is noted that three OAM operators ( Lx,Ly,Lz)
are insufficient to completely describe orbital states and addi-
tional OAP operators, composed of even-order symmetrized
products of L, are essential. Physically, OAP operators capture
real orbital states with zero OAM expectation value, such as
pxandpyorbitals, and mediate the orbital-lattice (i.e., crystal
field) coupling [26]. Unlike OAM, which bears analogies to
NM2NM1NM1xzy
c
M(t)
c
Oscillating magnetic fieldOscillating lattice
jLyz,j{Lz,Lx}z
jx
FIG. 1. Schematic illustration of orbital pumping in a model sys-
tem, NM1/NM2/NM1 (NM = normal metal), driven by an oscillating
magnetic field or vibrating lattice. For the magnetic-field-driven case,
NM2 may be considered a ferromagnet. ji
zis an orbital current flow-
ing along zwith orbital i, and jxis a charge current flowing along x.
spin in various aspects, OAP notably lacks a spin counterpart.
Adiabatic pumping [27] provides critical insights into the
dynamics of physical systems [28]. For spin dynamics, adi-
abatic spin pumping has elucidated phenomena such as en-
hanced magnetic damping [29] and spin motive force [30–
34], and served as an efficient means for generating pure
spin currents [35, 36]. Spin pumping is connected with spin
torque through the Onsager reciprocity [37]. Given orbital
torque [19–24], the Onsager reciprocity also guarantees the
presence of orbital pumping. Recent studies have investi-
gated orbital pumping [38–40], focusing on OAM pumping
but neglecting the contribution of OAP. Therefore, a complete
description of orbital pumping is yet to be established.
In this Letter, we present a theory of orbital pumping that
incorporates the entire orbital degrees of freedom, encom-
passing both OAM and OAP. We consider two distinct types
of adiabatic orbital pumping. The first type involves the OAM
dynamics induced by an AC magnetic field (Fig. 1), similar to
the approach used for spin pumping with ferromagnet/normal
metal bilayers. The second type, which does not require a
ferromagnet, arises from the lattice dynamics, which is real-
ized by applying AC stress to a nonmagnet (Fig. 1). ResultingarXiv:2311.00362v1 [cond-mat.mes-hall] 1 Nov 20232
AC strain gives rise to orbital pumping through strong orbital-
lattice coupling mediated by OAP. We show that both methods
generate not only OAM pumping but also OAP pumping. The
latter pumping has no spin counterpart and causes an even-
order harmonic AC transverse voltage, which is absent for
spin pumping and thus allows for unambiguous identification
of orbital pumping in experiments.
Orbital pumping by oscillating magnetic field.– For the first
type, we examine orbital pumping arising from the dynamics
of the orbital moment (i.e., OAM) driven by an AC magnetic
field. We ignore the spin degree of freedom to focus solely on
orbital responses and neglect SOC for the same reason. To get
a tractable analytic formula, we consider a p-orbital system
as a minimal model and assume an ideal case where three p-
orbitals are degenerate in equilibrium. This ideal case reveals
critical qualitative differences between orbital pumping and
spin pumping. However, this ideal case is not realized in real
materials since p-orbitals are split due to crystal fields. We
consider the crystal field effects on orbital pumping in numer-
ical calculations below and demonstrate that the predictions
from the ideal case persist in real situations.
We construct a model system of NM1/NM2/NM1 structure
(Fig. 1; NM = normal metal) and derive orbital pumping cur-
rents induced by time-dependent perturbations to NM2. The
perturbation Hamiltonian is H(t)=JexL·M(t), where M(t)
is the unit vector of time-dependent magnetic field, Jexis the
coupling strength, and Lis the (dimensionless) OAM operator,
which is a 3×3matrix in p-orbital space.
For a degenerate p-orbital system, the orbital is conserved,
and the 3×3Green’s function is given by,
g=g0I+g1−g−1
2L·M(t)+g1+g−1−2g0
2[L·M(t)]2,(1)
where gmis the Green’s function associated with an eigenstate
having an eigenvalue m(=−1,0,1)ofL·M(t)andgincludes a
term quadratic in L(i.e., OAP). We abbreviate the explicit po-
sition dependence of gmfor simplicity. Employing the method
developed in Ref. [34], we compute the 3×3matrix pumped
current density operator jαwhereαis the flow direction:
jα/(−e)=jOAM
α·L+/summationdisplay
βγjOAP
α,βγ{Lβ,Lγ}, (2)
where the first and second terms represent the OAM and OAP
currents, respectively. After some algebra, we obtain
jOAM
α=1
4πRe/bracketleftigg/parenleftiggG1,0
α+G0,−1
α
2/parenrightigg/parenleftigg
M×dM
dt−idM
dt/parenrightigg/bracketrightigg
,(3)
jOAP
α,βγ=1
8πRe/bracketleftigg/parenleftiggG1,0
α−G0,−1
α
2/parenrightigg
×Mβ/parenleftigg
M×dM
dt/parenrightigg
γ−iMβdMγ
dt+(β↔γ),(4)
Gµ,ν
α=Jexℏ2
me/integraldisplay
dr′[gR
µ(r,r′)↔
∂αgA
ν(r′,r)], (5)where gR/Arepresents retarded/advanced Green’s function of
the NM1/NM2/NM1 heterostructure,↔
∂αis the antisymmetric
differential operator, and/integraltext
dr′denotes the volume integral.
The OAM pumping current [Eq. (3)] has the same form
as the spin pumping current [29], except for replacing the
spin mixing conductance with the orbital mixing conductance
[Eq. (5)]. The spin (orbital) mixing conductance arises from
the scattering caused by an abrupt change of the spin (orbital)
environment at an interface. Since the orbital space encom-
passes additional degrees of freedom (OAP), the orbital mixing
conductance has more components than the spin mixing con-
ductance. More specifically, 9 conductances are required to
completely describe p-orbital scattering whereas 4 conduc-
tances ( G↑,G↓,Re[Gmix],Im[Gmix]) are sufficient for a full
description of spin scattering [41]. The OAP pumping current
derived in Eq. (4) corresponds to the additional components
and is of the distinct form (including higher order terms in M)
from the OAM pumping current (thus from the spin pumping
current as well). This OAP current corresponds to a flow of
real-orbital-polarized electrons with zero OAM and lacks a
counterpart in spin pumping, marking a qualitative distinction
between orbital pumping and spin pumping.
As an example, when M(t)rotates in the zxplane
(M(t)=ˆzcosωt+ˆxsinωt),jOAM
z =jOAM
α·Land jOAP
z=/summationtext
βγjOAP
α,βγ{Lβ,Lγ}become
jOAM
z=ω
4π/braceleftig
Re[G+
L]Ly+Im[G+
L](Lxcosωt−Lzsinωt)/bracerightig
,
(6)
jOAP
z=ω
4πIm[G−
L]/parenleftig
{Lz,Lx}cos 2ωt−(L2
z−L2
x) sin 2ωt/parenrightig
+ω
4πRe[G−
L]/parenleftig/braceleftig
Ly,Lz/bracerightig
cosωt+/braceleftig
Lx,Ly/bracerightig
sinωt/parenrightig
,(7)
where G±
L=(G1,0
z±G0,−1
z)/2. Here, jOAM
zandjOAP
zare the op-
erator expressions of the OAM and OAP currents, respectively,
which we use to show the dynamics of each orbital degree of
freedom explicitly. Equations (6) and (7) predict that orbital
pumping currents in ideal situations (i.e., no crystal field spit-
ting) consist of a DC component carrying Ly, first-harmonic
(1ω) ones carrying Lx,Lz,{Ly,Lz}, and{Lx,Ly}, and second-
harmonic ( 2ω) ones carrying{Lz,Lx}and(L2
z−L2
x).
Next, we examine orbital pumping in a more realistic situa-
tion, where the degeneracy of orbitals is lifted by crystal fields.
We adopt a sp3tight-binding model in a simple cubic lattice.
With sphybridization, the orbital nature of eigenstates varies
with the crystal momentum. Such variation (called orbital
texture) is common in real materials [12, 42].
We consider the same M(t)oscillation as above and calcu-
late numerically the pumped orbital current using the linear
response theory in the adiabatic limit (see Supplementary Ma-
terials (SM) for details [43]). We find that all of the orbital cur-
rents predicted by Eqs. (6) and (7) are pumped by the M(t)os-
cillation, although additional types of orbital currents are also
pumped. Figure 2 presents some of the numerical results: DC
OAM current ( jLy,DC
z ), DC OAP current ( j{Lz,Lx},DC
z ) [Fig. 2(a)],3
-1.0-0.50.00.51.0j(t)
wtjLyz(t) j{Lz,Lx}
z (t) jx(t)
2p p 0
-30 -20 -10 0 10 20 30-1.0-0.50.00.51.0jDC
z(lattice constant, a0)jLy,DC
z j{Lz,Lx},DC
z jDC
x(a)
(b)
FIG. 2. (a) Spatial profile of DC pumping currents, jLy,DC
z (red),
j{Lz,Lx},DC
z (blue), and jDC
x(gray), driven by the time-dependent mag-
netic field, L·M(t)forM(t)=ˆzcosωt+ˆxsinωt, on NM2 layer. (b)
Temporal dependence of pumping currents j(t)at the right interface
(z=16a0). The thick dashed horizontal line in (b) shows the DC
component of transverse charge current jx(t).
and second-harmonic OAM current ( jLy
z(t)), second-harmonic
OAP current ( j{Lz,Lx}
z (t)) [Fig. 2(b)]. We note that the DC OAP
current and the second-harmonic OAM current are unexpected
from the analytic theory [Eqs. (6) and (7)]. We attribute these
unexpected orbital currents to the fact that the crystal field
splitting can convert OAM current to OAP current, and vice
versa [26]. Note that the relatively short decay length of orbital
currents in NM1 [Fig. 2(a)] arises from the orbital characters
of the band structure used in our model. It increases with de-
creasing the orbital splitting [44], as demonstrated in SM [43].
The pumped OAM and OAP currents are converted to trans-
verse charge currents jxthrough the inverse orbital Hall ef-
fect [26, 45, 46] and inverse orbital-torsion Hall effect [26],
respectively [Figs. 2(a) and (b)]. A recent orbital pumping
experiment [39] reported a DC charge current and attributed
it entirely to conversion from pumped DC OAM current [44].
However, the measured DC charge current may contain an ad-
ditional contribution due to conversion from pumped DC OAP
current. The converted charge current also contains a second-
harmonic component since pumped OAM and OAP currents
contain second-harmonic components [Fig. 2(b)]. The second-
harmonic charge current remains unexplored experimentally.
It is worth noting that the generalized pumping equation de-
rived in SM [43] indicates that a d-orbital system may also
produce a fourth-harmonic component. As a spin pumping
current contains only DC and first-harmonic components [29],
higher-harmonics pumping signals are a unique feature of or-
bital pumping.
In addition to orbital pumping, we find that the pumped
-1.0-0.50.00.51.0jLy,DCztime-dependent hopping integrals
[L×u(t)]2(´102)
-30 -20 -10 0 10 20 30-1.0-0.50.00.51.0jDCx
z(lattice constant, a0)time-dependent hopping integrals
[L×u(t)]2(´102)
-1.0-0.50.00.51.0j{Lz,z
Lx},DCtime-dependent hopping integrals
[L×u(t)]2(´102)(a)
(b)
(c)FIG. 3. Spatial profile of DC pumping currents (a) jLy,DC
z, (b)
j{Lz,Lx},DC
z , and (c) jDC
xdriven by the lattice dynamics, which is imposed
by time-dependent variations of tight-binding hopping integrals (solid
circles) and [L·u(t)]2foru(t)=ˆzcosωt+ˆxsinωt(open diamonds).
orbital current is converted to another orbital current, i.e.,
the orbital swapping effect. Analogous to the spin swapping
effect [47–49], it results in the type I conversion (e.g., jLy,DC
z→
jLz,DC
y) and the type II conversion (e.g., jLz,DC
z→jLx,DC
x) , which
can be called the OAM swapping effect and is in line with a
recent theory [50]. We find that the OAP swapping effect also
arises (see SM [43]). Similar to the orbital Hall effect [7],
the orbital swapping effect arises even without SOC. But it
vanishes in the absence of the orbital texture.
Orbital pumping by lattice dynamics–. In the second case,
we explore orbital pumping due to lattice dynamics, which can
be realized by a time-dependent variation of strain, i.e., a time-
dependent deformation of crystal. For a crystal under arbitrary
deformations, three effects need to be considered: variations
of i) orbital splitting, ii) bonding lengths, and iii) bonding
angles. Each factor manifests in the tight-binding model as
corrections to on-site energies, magnitudes of hopping inte-
grals, and directional cosines, respectively. By assuming the
time-dependent hopping integrals to follow a power law of
bonding length [51, 52], we integrate the periodic lattice dy-
namics driven by biaxial strains into our model and numer-
ically calculate orbital pumping due to this lattice dynamics
(see SM [43] for details).
We consider two biaxial strains in the zxplane with a phase
difference, which makes the cubic lattice undergo a circularly
rotating strain. It resembles a generation of phonon angu-4
lar momentum (PAM) polarized along the ydirection under
surface acoustic wave [53]. Numerical calculations with the
time-dependent hopping integrals show that DC OAM cur-
rent [ jLy,DC
z ; Fig. 3(a)], DC OAP current [ j{Lz,Lx}DC
z ; Fig. 3(b)],
and associated DC transverse charge current [ jDC
z; Fig. 3(c)]
are pumped. OAM pumping induced by lattice dynamics is
the reverse process of crystal field torque [54], where non-
equilibrium OAM, generated by external perturbations such as
an electric field, is absorbed by the lattice. The reverse process
of the OAP current may offer another mechanism of the crystal
field torque, which has not been identified yet.
Orbital pumping driven by lattice dynamics can be under-
stood through an OAP-type perturbation, which is qualitatively
distinct from the previously considered perturbation, L·M(t),
for the case of oscillating M(t). To demonstrate this, we con-
sider the long-wavelength limit ( k→0) of lattice vibration,
where we may neglect the effects of spatial variations and fo-
cus on the time-dependent variations of orbital splitting (i.e.,
time-dependent lifting of orbital degeneracy in the analytic
model). If the crystal experiences a strain along the udirec-
tion, the energy of the puorbital becomes different from that
of the other porbitals perpendicular to it. It is important to
note that the eigenvalue of (L·u)2with respect to the former
is 0 while those with respect to the latter are 1. Therefore, the
time-dependent strain in a p-orbital system can be modeled by
a perturbation of [L·u(t)]2. In a general sense, a lattice distor-
tion is time-reversal even, and thus the corresponding pertur-
bation Hamiltonian should be expressed in terms of even-order
products of the OAM operators, which is essentially OAP. The
open diamonds in Fig. 3 confirm that the [L·u(t)]2perturba-
tion incorporated to the numerical model can reproduce the
characteristics of orbital pumping from the lattice dynamics
described by time-dependent hopping integrals in reasonable
consistency, despite the simplicity of the model.
Further insight can be gained through a simplified ana-
lytic treatment. Assuming that all equilibrium orbitals are
degenerate at the Γpoint for simplicity, the Green’s func-
tion for the perturbation of [L·u(t)]2can be expressed as
g=g0I+(g1−g0)[L·u(t)]2. Utilizing Eqs. (3) and (4), we
derive
jOAM
α=1
4πRe[G1,0
α]u×du
dt, (8)
jOAP
α,βγ=1
8πIm[G1,0
α]d(uβuγ)
dt, (9)
which explain that both OAM and OAP currents are pumped
by lattice dynamics. Equation (8) indicates the presence of
nonzero DC OAM pumping when urotates in time, for exam-
ple,u(t)=ˆzcosωt+ˆxsinωt. OAM pumping induced by the
rotating strain can be understood as the transfer of PAM to elec-
tron OAM [55]. Conversely, Eq. (9) suggests the absence of
DC OAP pumping for a periodic u, as demonstrated by its time
average (1/T)/integraltextT
0jOAP
α,βγdt=(1/8πT) Im[G1,0
α]uβ(T)uγ(T)→0
asTincreases. The emergence of DC OAP pumping in nu-
merical calculations (Fig. 3) is attributed to the orbital tex-
ture, resulting in an interconversion between OAM and OAP,as generally proven in Ref. [26]. Its detailed analytical de-
scription would require going beyond our simplified approach
and considering the Green’s function more complicated than
g=g0I+(g1−g0)[L·u(t)]2, which we leave for future work.
Discussion and outlook.– We demonstrated orbital pump-
ing driven by either oscillating M(t)or lattice dynamics. In
both pumping methods, not only OAM currents but also OAP
currents are pumped. The simultaneous emergence of OAM
and OAP pumping highlights the necessity of considering both
orbital degrees of freedom when describing orbital dynamics.
This is a fundamental requirement since a complete descrip-
tion of entire orbital degrees of freedom can be achieved only
by incorporating both OAM and OAP operators. As a result,
OAP pumping always plays a role in physical phenomena aris-
ing from OAM pumping. An important consequence is that
OAP current contributes to orbital torque. It has been believed
that orbital torque originates solely from the injection of OAM
current [19]. However, the emergence of OAP current through
magnetization dynamics suggests the existence of its inverse
process: the generation of magnetic torque through the injec-
tion of OAP current. This previously unrecognized inverse
process, which we term ”OAP torque”, introduces a new di-
mension to the understanding of orbital torque. Moreover,
the Onsager reciprocity between orbital pumping and orbital
torque is validated only when one considers both OAM and
OAP contributions.
Our theory of orbital pumping offers an exploitable method
for generating and detecting the OAP degree of freedom. We
note that previous suggestions in Ref. [26] rely on twisted
heterostructures, which can be challenging to implement, or
on low-gap semiconductors with limited availability of the
required materials. In contrast, the high-harmonics pumping,
driven by the OAP degree of freedom, can be realized with
various materials. We also note that this property stems from
the distinct behaviors of high-order products of Loperators
with respect to rotational transformations. Thus, it is a general
property that is not limited to p-orbital systems.
Furthermore, orbital pumping is not limited to multilayer
structures. Recalling that the spin motive force is a continuum
version of spin pumping [56], we anticipate the presence of
an orbital motive force when a single-layer system exhibits an
inhomogeneous crystal field. Thus, the orbital motive force
would encompass OAP contributions, which lack their spin
counterparts. Notably, the physical properties of the orbital
motive force would differ from those of the spin motive force
due to the presence of orbital texture, a factor not accounted
for in the theory of the spin motive force. The exploration of
this topic remains a subject for future work.
Lastly, our work sheds light on the transfer of angular mo-
mentum between electrons and phonons. Theoretical estima-
tions [57–59] and experimental measurements [53, 60, 61] il-
lustrate that PAM can have a considerable magnitude contrary
to early assumptions and plays a nontrivial role in various phe-
nomena such as magnetization relaxation [62] and ultrafast de-
magnetization [63, 64]. Intriguingly, recent many-body treat-
ment [65] shows that a complete picture of angular momen-5
tum transfer between electron and phonon subsystems requires
OAM as a key ingredient since the electron-phonon coupling
is independent of spin. The strain-induced orbital pumping
weighs heavily on this connection of orbital and lattice and
call for a wider viewpoint on PAM dynamics [55, 66, 67]
assisted by the orbital degree of freedom [68].
Note added.– During the preparation of our manuscript, we
became aware of a recent theoretical work on orbital pumping
that focuses only on OAM pumping induced by magnetization
dynamics [40].
This work was supported by the National Research Foun-
dation of Korea (NRF) funded by the Ministry of Science
and ICT (2020R1A2C3013302, 2022M3I7A2079267) and the
KIST Institutional Program. S.H. and H.-W.L. were supported
by the Samsung Science and Technology Foundation (BA-
1501-51).
∗∗S.H. and H.-W.K. contributed equally to this work.
∗hwl@postech.ac.kr
†kjlee@kaist.ac.kr
‡kwk@kist.re.kr
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I. GENERAL PUMPING FORMULA FOR ARBITRARY ORBITAL SYSTEMS
A. Generalized algebra for high- lorbital spaces
In the case of spin, one can completely describe the dynamics using the Pauli matrix, enabling us to represent arbitrary
traceless operators as vectors. Consequently, the pumping formula can also be expressed in vector form. However, in the case of
orbitals with angular momentum quantum number l, it is imperative to define a vector space of (2 l+1)2dimensions, leading to the
necessity of generalizing the dot product and cross product. This section will provide these definitions and outline their essential
algebraic properties. In the following section, we will employ these concepts to demonstrate the straightforward generalization
of the pumping formula.
We define a new symbol ” ˙ =” to denote the mapping of an (2 l+1)×(2l+1) matrix Ato an (2 l+1)2-dimensional vector as
follows,
A˙=A, (S1)
where A=AiLi(Einstein convention), Tr[ LiLj]=2δi j, and Ai=Tr[ALi]/2. The orthogonality guarantees the uniqueness and
existence of the representation. We can generalize the cross product and dot product that map Rn2×Rn2toRn2as,
A⊙B/doteq1
2{A,B}, (S2)
A⊗B/doteq1
2i[A,B]. (S3)
Below, we present some useful properties of generalized dot and cross products.
1. Property 1: Bilinearity
(A+B)⊙(C+D)=A⊙B+B⊙C+A⊙D+B⊙D, (S4)
(A+B)⊗(C+D)=A⊗B+B⊗C+A⊗D+B⊗D. (S5)
2. Property 2: (anti)commutativity
A⊗B=−B⊗A, (S6)
A⊙B=B⊙A. (S7)
3. Property 3: Representation of matrix multiplication
AB=A⊙B+iA⊗B. (S8)
c.f. (a·σ)(b·σ)=a·b+i(a×b)·σfor the spin case.
4. Property 4: Traces
Definition: Tr v[A]/doteqTr[A].
Trv[A⊗B]=0, (S9)
Trv[A⊙B]=2A·B. (S10)arXiv:2311.00362v1 [cond-mat.mes-hall] 1 Nov 20232
5. Property 5: Completeness relation.
Trv[A⊙B]=1
2Trv[A⊙Li]Trv[Li⊙B]. (S11)
6. Property 6: Trace of matrix multiplication.
Tr[AB]=2A·B, (S12)
Tr[ABC ]=2A·(B⊙C+iB⊗C), (S13)
where A·B=AiBi.
7. Property 7: Jacobi identities
A⊗(B⊗C)+B⊗(C⊗A)+C⊗(A⊗B)=0, (S14)
A⊗(B⊙C)+B⊗(C⊙A)+C⊗(A⊙B)=0. (S15)
8. Property 8: Non-associativity relations
A⊙(B⊙C)−(A⊙B)⊙C=−B⊗(C⊗A), (S16)
A⊗(B⊗C)−(A⊗B)⊗C=−B⊗(C⊗A), (S17)
A⊗(B⊙C)−(A⊗B)⊙C=−B⊙(C⊗A). (S18)
c.f. The second relation is equivalent to the first Jacobi identity.
9. Property 9: Triple scalar products
A·(B⊙C)=(A⊙B)·C(=1
4Tr[ABC +ACB ]), (S19)
A·(B⊗C)=(A⊗B)·C(=1
4iTr[ABC−ACB ]). (S20)
c.f.A·(B×C)=(A×B)·Cfor usual cross product.
10. Property 10: spin limit
ForLi=σi(i=0,1,2,3),
A⊙B˙=(A·B,A0B1+B0A1,A0B2+A2B0,A0B3+A3B0), (S21)
A⊗B˙=(0,A2B3−A3B2,A3B1−A1B3,A1B2−A2B1). (S22)3
11. Property 11: Equation of motion
For physical operator Aand Hamiltonian H,
dA
dt=1
iℏ[H,A] ˙=2
ℏH⊗A. (S23)
B. The Green’s function formalism for orbital pumping
In this section, we derive a pumping formula applicable to arbitrary orbital systems with angular momentum quantum number
l. We extend the formula derived in the reference [1] for spin pumping, utilizing the Green’s function approach, to operate even
in states with higher angular momentum ( l≥1/2). For state with total angular momentum l, we need (2 l+1)2-dimensional
vector space to completely describe pumping e ffects. We define unit vector in (2 l+1)2space as follows,
ˆα˙=Lα. (S24)
Thenν-direction total current is given by,
jν=ℏ
4πJexℏ2
mei/integraldisplay
dr′/bracketleftbigg
gR(r,r′)ˆα↔
∂νgA(r′,r)/bracketrightbiggduα
dt, (S25)
where gR/A(r,r′) is retarded and advanced Green’s function defined in (2 l+1)2-dimensional vector space and ( duα/dt)ˆαconsti-
tutes external perturbations also defined in (2 l+1)2-dimensional vector space. Then, we use orbital algebra introduced in the
previous section to simplify above equation. Using generalized products defined in previous section, the orbital current is given
by,
jν=ℏ
4πJexℏ2
meIm/integraldisplay
dr′×
/bracketleftbigg/parenleftig
gR(r,r′)⊙ˆα/parenrightig
⊙↔
∂νgA(r′,r)−/parenleftig
gR(r,r′)⊗ˆα/parenrightig
⊗↔
∂νgA(r′,r)+i/parenleftig
gR(r,r′)⊙ˆα/parenrightig
⊗↔
∂νgA(r′,r)+i/parenleftig
gR(r,r′)⊗ˆα/parenrightig
⊙↔
∂νgA(r′,r)/bracketrightbiggduα
dt.
(S26)
By projecting the expression for gR/Aonto unit vectors, we can obtain pumping expressions with a generalized mixing conduc-
tance,
jν=ℏ
4πJexℏ2
me/integraldisplay
dr′×
/summationdisplay
βγIm[gR
β(r,r′)↔
∂νgA
γ(r′,r)][(ˆβ⊙ˆα)⊙ˆγ−(ˆβ⊗ˆα)⊗ˆγ]+Re[gR
β(r,r′)↔
∂νgA
γ(r′,r)][(ˆβ⊙ˆα)⊗ˆγ+(ˆβ⊗ˆα)⊙ˆγ]duα
dt, (S27)
where gR/A
m=gR/A·ˆm.
II. ORBITAL PUMPING BASED ON THE SCATTERING MATRIX APPROACH
In this subsection, we show that the pumped orbital current by the magnetization dynamics using the scattering matrix ap-
proach [2] is consistent with that of the Green’s function approach. Following the conventional scattering matrix approach [2],
the pumped current density operator jαwhereαis the flow direction is given by,
jα/(−e)=∂nα
∂XdX(t)
dt, (S28)
∂nα
∂X=1
4πi∂S
∂XS†+h.c., (S29)
where X(t) is a time-dependent system parameter, ∂nα/∂Xis 3×3 emissivity matrix along αdirection, and Sis the 3×3
scattering matrix in p-orbital space. We then define the orbital mixing conductance as the orbital counterpart of the spin mixing
conductance,
Gi,j/doteq1−rir∗
j, (S30)4
where riandrjare the reflection coe fficients. Now we calculate the pumped orbital currents by the magnetization dynamics
where the Hamiltonian is given by,
H(t)=L·M(t). (S31)
For this case, scattering matrix is given by,
S=/summationdisplay
mrm|m⟩⟨m|, (S32)
where|m⟩is the eigenstate of the Eq. (S31). Then, the pumped OAM and OAP currents are given by,
jOAM
α=1
8πRe/bracketleftigg/parenleftiggG1,0+G0,−1
2/parenrightigg/parenleftigg
M×dM
dt−idM
dt/parenrightigg/bracketrightigg
, (S33)
jOAP
α,βγ=1
16πRe/bracketleftigg/parenleftiggG1,0−G0,−1
2/parenrightigg
×Mβ/parenleftigg
M×dM
dt/parenrightigg
γ−iMβdMγ
dt+(β↔γ), (S34)
whereαis the surface-normal direction. We can see there is direct mapping between pumped orbital currents calculated by
Green’s function approach. The same conclusion can be drawn for the orbital pumping by the lattice dynamics.
III. LINEAR RESPONSE CALCULATION
We consider currents carrying a physical quantity Q. An increase of Qin the region less than the ( ℓ+1)-th layer is given by,
dNQ(ℓ)
dt=d
dt/angbracketleftiggℓ/summationdisplay
i=−∞Q(i)(t)/angbracketrightigg
,Q(i)(t)=/summationdisplay
α,α′C†
iα(t)Qiα,iα′Ciα′(t).
From the Heisenberg equation of motion, the increasing rate of Qis expressed as,
dNQ(ℓ)
dt=1
iℏ/angbracketleftiggℓ/summationdisplay
i=−∞Q(i)(t),/summationdisplay
C†
i1α1Hi1,i2α1,α2Ci2α2/angbracketrightigg
,
where His the Hamiltonian matrix. Using the commutation relations of {Ciα,C†
jα′}=δi jδαα′, we derive an increase of Qin terms
of the generation and transfer terms:
dNQ(ℓ)
dt=WQ
L(ℓ)+IQ
L(ℓ).
Here, WQ
L(ℓ) is the generation rate and IQ
L(ℓ) is the current of increasing Qin the region less than ( ℓ+1),
IQ
L(ℓ)=1
iℏQℓα,ℓα′/angbracketleftig
C†
ℓαHℓ,ℓ+1
α′,α1Cℓ+1α1−C†
ℓ+1α1Hℓ+1,ℓ
α1,αCℓα′/angbracketrightig
.
By defining the lesser Green function by ⟨C†
αCβ⟩=−iℏG<
βα, we arrive at
IQ
L(ℓ)=2 Re Tr/bracketleftig
Hℓ+1,ℓQℓ,ℓG<(ℓ,ℓ+1)/bracketrightig
.
In a similar way, we can calculate an increase of Qin the region greater than the ℓ-th layer that is given by,
IQ
R(ℓ)=2 Re Tr/bracketleftig
Hℓ,ℓ+1Qℓ+1,ℓ+1G<(ℓ+1,ℓ)/bracketrightig
.
In an averaged sense, we define the current carrying Qas,
jQ(ℓ)=1
2/bracketleftig
IQ
R(ℓ−1)−IQ
L(ℓ)/bracketrightig
=Re Tr/bracketleftig
Qℓ,ℓ/parenleftig
G<(ℓ,ℓ−1)Hℓ−1,ℓ−G<(ℓ,ℓ+1)Hℓ+1,ℓ/parenrightig/bracketrightig
. (S35)5
If a time-dependent term U(t) in the Hamiltonian is slow enough relative to electron dynamics, we can treat its time-derivative
˙U(t) as a perturbation. Then, the lesser Green function is expressed as
G<(t,t)=−1
2πℏ/integraldisplay
dE f o(E)/bracketleftigg
GC(E)+iℏ/parenleftigg∂GR
∂E˙U(t)GC(E)−GC(E)˙U(t)∂GA
∂E/parenrightigg
+···/bracketrightigg
.
Here, fo(E) is the Fermi-Dirac distribution and GC(E)≡GR(E)−GA(E).GR,A(E)=gR,A[E−U(t)] is the retarded and advanced
Green function, respectively, and we express them as the adiabatic modulation of the unperturbed Green functions, gR,A(E)=
(E−H±iΓ)−1for given level broadening Γ =25 meV. Because the zeroth order term is irrelevant to the spin pumping currents,
we omit it and obtain the lesser Green function up to the first order as
δG<(t,t)=−1
iℏ/integraldisplay
dE/parenleftigg∂fo
∂EδN(E)+fo(E)δD(sea)(E)/parenrightigg
.
Here,δNandδD(sea)are called Fermi surface and sea contributions, respectively, given by
δN(E)=ℏ
4π/bracketleftig
GR˙U(t)GC−GC˙U(t)GA/bracketrightig
,
δD(sea)(E)=ℏ
4π/bracketleftigg
GR˙U(t)∂GR
∂E−∂GR
∂E˙U(t)GR+h.c./bracketrightigg
.
UsuallyδD(sea)is considered to be small and is neglected in this work. By associating the lesser Green function and the currents
of Eq. (S35), we obtain
jQ(ℓ)=1
ℏImTr/integraldisplay
dE∂fo
∂E/braceleftbigg
Qℓ,ℓ/parenleftbigg/bracketleftig
δN(E)/bracketrightigℓ,ℓ+1Hℓ+1,ℓ−/bracketleftig
δN(E)/bracketrightigℓ,ℓ−1Hℓ−1,ℓ/parenrightbigg/bracerightbigg
=−1
a0ImTr/braceleftbigg
Q/bracketleftig
δN(E)iv/bracketrightigℓ,ℓ/bracerightbigg
E=µ,T−→ 0 (S36)
where a0is a lattice constant and the velocity matrix is given by
vℓ,ℓ′=±ia0
ℏHℓ,ℓ′δℓ′,ℓ±1. (S37)
IV . TIGHT-BINDING MODEL
Consider a three-dimensional NM1 /NM2 /NM1 system of simple cubic structure (Fig. 1 in the main text). The tight-binding
Hamiltonian composed of sandporbitals is given as [3]
H(0)(k)=...
T(0)†
llh(0)
lT(0)
la0 0 0 0
0T(0)†
lah(0)
aT(0)
aa 0 0 0
...
0 0 0T(0)†
aa h(0)
aT(0)
al0
0 0 0 0 T(0)†
alh(0)
lT(0)
ll
..., (S38)
where
h(0)
i−E(0)
i=2V(0)
ssσ(cx+cy) 2 iV(0)
spσsx 2iV(0)
spσsy 0
−2iV(0)
spσsx2V(0)
ppσcx+2V(0)
ppπcy 0 0
−2iV(0)
spσsy 0 2 V(0)
ppπcx+2V(0)
ppσcy 0
0 0 0 2 V(0)
ppπ(cx+cy),
E(0)
i=ϵ(0)
s 0 0 0
0ϵ(0)
px0 0
0 0ϵ(0)
py0
0 0 0 ϵ(0)
pz,T(0)
i j=V(0)
ssσ 0 0 V(0)
spσ
0 V(0)
ppπ0 0
0 0 V(0)
ppπ0
−V(0)
spσ0 0 V(0)
ppσ,6
with abbreviations cx(y)≡coskx(y)a0andsx(y)≡sinkx(y)a0are used for brevity. The basis of h(0)
iandT(0)
i jis{|s⟩,|px⟩,|py⟩,|pz⟩}
where subscripts stand for the active region ( a), leads ( l), and interfaces ( alandla). The tight-binding parameters are set as
ϵ(0)
s=0.50,ϵ(0)
px=ϵ(0)
py=ϵ(0)
pz=−0.70,V(0)
ssσ=−0.30,V(0)
ppσ=0.50,V(0)
ppπ=−0.20, and V(0)
spσ=0.40 for both NM1 and NM2
layers, all in units of eV .
To impose the boundary condition that both NM1 layers are semi-infinite, we utilize the repetitive structure of Hamiltonian [4].
Namely, the Hamiltonian is constructed as
H(0)(k)=HllIla 0
IalHaaIar
0IraHrr,
whereHandIis the on-site and interaction matrices of each region: the left contact ( l), the right contact ( r), and the active
region ( a). We define the retarded Green function in a similar manner,
GR=GllGlaGlr
GalGaaGar
GrlGraGrr,
thereby obtain the Green function of the active region as
(Haa−Σl−Σr)GR
aa=1,
with the surface self energies defined as
Σl=IalH−1
llIla,Σr=IarH−1
rrIra.
A. Time-dependent lattice dynamics
Now, suppose that a time-dependent biaxial stress is applied along two axes perpendicular to each other, ˆe1=ˆzcosϕ+ˆxsinϕ
andˆe2=−ˆzsinϕ+ˆxcosϕ, with phase di fferenceφ. Then, the position vector of nearest neighbors is modified as
δδδ(t)=ˆe1δ(0)
1(1+ε1sinωt)+ˆe2δ(0)
2[1+ε2sin(ωt+φ)],
whereε1(2)is the maximum strain along the axis ˆe1(2)andδ(0)
1(2)=limε→0δδδ(t)·ˆe1(2). Due to the deformation of crystal structure,
the directional cosines for nearest-neighbor bonds and the magnitude of hopping integrals should be altered. The bond-length
dependence of hopping integrals is usually fitted to a power law [5, 6]
Vαβτ(d)=Vαβτ(d0)/parenleftiggd0
d/parenrightiggηαβτ
, (S39)
in whichα,βdenote orbitals under consideration and τis the bonding type σ,π,δ,···. In general, the exponent ηαβτis orbital-
and material-specific parameter obtained by comparing tight-binding and ab initio data. For simplicity, however, we arbitrarily
choose the exponent to be a constant for all hopping integrals, i.e., ηαβτ=2. Then, the Hamiltonian at instantaneous time tis
H(k;t)=...
T(0)†
llh(0)
lT(0)
la0 0 0 0
0T(0)†
laha(t)Taa(t) 0 0 0
...
0 0 0T†
aa(t)ha(t)T(0)
al0
0 0 0 0 T(0)†
alh(0)
lT(0)
ll
...,7
where
⟨s;k|ha(t)|s;k⟩=ϵ(0)
s+2V(0)
ssσ(˜cx+cy),
⟨px;k|ha(t)|px;k⟩=ϵ(0)
px+2(V(0)
ppσl2
x+V(0)
ppπn2
x)˜cx+2V(0)
ppπcy,
⟨py;k|ha(t)|py;k⟩=ϵ(0)
py+2V(0)
ppπ˜cx+2V(0)
ppσcy,
⟨pz;k|ha(t)|pz;k⟩=ϵ(0)
pz+2(V(0)
ppσn2
x+V(0)
ppπl2
x)˜cx+2V(0)
ppπcy,
⟨s;k|ha(t)|px;k⟩=2iV(0)
spσlx˜sx,
⟨s;k|ha(t)|py;k⟩=2iV(0)
spσsy,
⟨s;k|ha(t)|pz;k⟩=2iV(0)
spσnx˜sx,
⟨px;k|ha(t)|pz;k⟩=2(V(0)
ppσ−V(0)
ppπ)lxnx˜cx,
and
Taa(t)=1
|dz(t)|2V(0)
ssσ lzV(0)
spσ 0 nzV(0)
spσ
−lzV(0)
spσl2
zV(0)
ppσ+n2
zV(0)
ppπ 0lznz(V(0)
ppσ−V(0)
ppπ)
0 0 V(0)
ppπ 0
−nzV(0)
spσlznz(V(0)
ppσ−V(0)
ppπ) 0 n2
zV(0)
ppσ+l2
zV(0)
ppπ.
Here, we neglect the time-dependent variation of on-site energies and assume ε1=ε2=ε. Note that the strain is uniformly
applied in the active region, i.e., ∂ε/∂ y=0. The position vectors directing nearest neighbors are
dz(t)=a0ˆz[1+ε{cos2ϕsinωt+sin2ϕsin(ωt+φ)}]+a0ˆxεcosϕsinϕ[sinωt−sin(ωt+φ)],
dx(t)=a0ˆzεcosϕsinϕ[sinωt−sin(ωt+φ)]+a0ˆx[1+ε{sin2ϕsinωt+cos2ϕsin(ωt+φ)}],
and corresponding directional cosines are defined as li=ˆx·di(t)/|di(t)|andni=ˆz·di(t)/|di(t)|fori=x,z. The revised
abbreviations ˜ cx≡coskxa0/|dx(t)|2and ˜sx≡sinkxa0/|dx(t)|2are used. Up to the linear order of strain ε,
ha(t)−h(0)
a≈−2ε/parenleftig
sin2ϕsinωt+cos2ϕsin(ωt+φ)/parenrightig2V(0)
ssσcx2iV(0)
spσsx 0 0
−2iV(0)
spσsx2V(0)
ppσcx 0 0
0 0 2 V(0)
ppπcx 0
0 0 0 2 V(0)
ppπcx
+εcosϕsinϕ(sinωt−sin(ωt+φ))0 0 0 2 iV(0)
spσsx
0 0 0 2( V(0)
ppσ−V(0)
ppπ)cx
0 0 0 0
−2iV(0)
spσsx2(V(0)
ppσ−V(0)
ppπ)cx0 0,
and
Taa(t)−T(0)
aa≈−2ε/parenleftig
cos2ϕsinωt+sin2ϕsin(ωt+φ)/parenrightigV(0)
ssσ 0 0 V(0)
spσ
0 V(0)
ppπ0 0
0 0 V(0)
ppπ0
−V(0)
spσ0 0 V(0)
ppσ
+εcosϕsinϕ(sinωt−sin(ωt+φ))0 V(0)
spσ 0 0
−V(0)
spσ 0 0 V(0)
ppσ−V(0)
ppπ
0 0 0 0
0 V(0)
ppσ−V(0)
ppπ0 0.
We superpose two biaxial strains to generate lattice vibration with finite net angular momentum. One biaxial strain with
ϕ1=0 andφ1=πand the other strain with ϕ2=π/4 andφ2=πare overlapped where overall phase of the latter is shifted
byπ/2 with respect to the former.Note that the strength of each set of strains is set to ε=0.5%. To obtain an insight on the
perturbation we take, consider the tight-binding Hamiltonian of porbitals in bulk simple cubic lattice. Then, the time-dependent
perturbation Ubulk(t) in the long-wavelength limit is given as
Ubulk(t)≈−4ε(V(0)
ppσ−V(0)
ppπ)/bracketleftig
{Lz,Lx}cosωt−(L2
z−L2
x) sinωt/bracketrightig
, (S40)
which resembles [ L·u(t)]2with halved frequency for ˆu(t)=ˆzcosωt+ˆxsinωt. Thus, one can conclude that the e ffective
perturbation [ L·u(t)]2captures the lattice dynamics characterized by the circular motion of an atom about its equilibrium
position, which in turn gives rise to adiabatic transformation of the OAP.8
-30 -20 -10 0 10 20 30-1.0-0.50.00.51.0 jLz,DCz
z(lattice constant, a0)Vsps(eV)
0.40 0.20 0.00
FIG. S1. Spatial profile of DC orbital pumping current driven by the time-dependent magnetic field L·M(t) for ˆM(t)=ˆxcosωt+ˆysinωtfor
various strengths of sphybridization Vspσ.
V . DECAY LENGTH OF ORBITAL CURRENTS
The transmission of OAM current into adjacent layers depends on the orbital character [7]. For a given geometry, an electron
propagating toward the leads experiences the crystal field which splits |pz⟩from|px⟩and|py⟩. Therefore, one can suppress
the spatial oscillation of OAM response by choosing ˆM(t)=ˆxcosωt+ˆysinωtthat conveys the OAM Lz. The calculated
OAM current jLz,DC
z (Fig. S1) exhibits a monotonically decaying behavior rather than an oscillatory decay near the interface as
illustrated in Fig. 2. Still, the OAM penetration length is not strikingly enhanced as that previously reported in ferromagnets when
the orbital texture exists. Under consideration of all electrons participating in the propagation, we recognize that degenerate |px⟩
and|py⟩states with nonzero in-plane wave vectors are gapped into |pr⟩≡cosϕk|px⟩+sinϕk|py⟩and|pt⟩≡− sinϕk|px⟩+cosϕk|py⟩
by the orbital texture while the degeneracy at k=±kFˆzare preserved. Note that ϕk=arg(kx+iky) is an azimuthal angle of wave
vector k. As the operator ˆLz=i|py⟩⟨px|−i|px⟩⟨py|=i|pt⟩⟨pr|−i|pr⟩⟨pt|, the broken degeneracy between |pr⟩and|pt⟩results
in increased oscillation for states carrying Lz, and thus short-ranged orbital transport. Conversely, the overall penetration length
can be extended by decreasing the strength of orbital texture as shown in Fig. S1.
VI. ORBITAL SWAPPING EFFECT
The pumped orbital current serves as a primary input of the orbital swapping e ffect, which is an orbital counterpart of the spin
swapping e ffect [8–10]. Similar to the spin swapping e ffect which is categorized into two types, the orbital swapping e ffect can
be classified into one that illustrates the conversion of OAM current jOAM
α,β→jOAM
β,αforα/nequalβ[Fig. S2(a)] and the other which
represents the conversion of OAM current jOAM
α,α→jOAM
β,βforα/nequalβ[Fig. S2(c)]. Furthermore, we observe the swapping of OAP
current jOAP
α,αβ→jOAP
γ,βγ[Fig. S2(b)] and jOAP
α,βγ→jOAP
β,γα(not shown). Note that the latter process converts AC OAP current to another
AC OAP current in our model. All processes are suppressed when the orbital texture vanishes.9
-1.0-0.50.00.51.0jDCj{Lz,Lx},DC
z j{Lx,Ly},DC
y
-30 -20 -10 0 10 20 30-1.0-0.50.00.51.0jDC
z(lattice constant, a0)jLz,DC
z jLx,DC
x
-1.0-0.50.00.51.0jDCjLy,DC
z jLz,DC
y(a)
(b)
(c)
FIG. S2. Spatial profile of DC orbital pumping currents and resultant orbital swapping currents driven by the time-dependent magnetic field
L·M(t) for (a,b) ˆM(t)=ˆzcosωt+ˆxsinωtand (c) ˆM(t)=ˆxcosωt+ˆysinωt.
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[3] J. C. Slater and G. F. Koster, Simplified LCAO Method for the Periodic Potential Problem, Phys. Rev. 94, 1498 (1954).
[4] M. Luisier, A. Schenk, W. Fichtner, and G. Klimeck, Atomistic simulation of nanowires in the sp3d5s∗tight-binding formalism: From
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1512.01660v1.Kinetic_theory_of_spin_polarized_systems_in_electric_and_magnetic_fields_with_spin_orbit_coupling__I__Kinetic_equation_and_anomalous_Hall_and_spin_Hall_effects.pdf | arXiv:1512.01660v1 [cond-mat.str-el] 5 Dec 2015Kinetic theory of spin-polarized systems in electric and ma gnetic fields with spin-orbit
coupling: I. Kinetic equation and anomalous Hall and spin-H all effects
K. Morawetz1,2,3
1M¨ unster University of Applied Sciences, Stegerwaldstras se 39, 48565 Steinfurt, Germany
2International Institute of Physics (IIP) Federal Universi ty of Rio Grande
do Norte Av. Odilon Gomes de Lima 1722, 59078-400 Natal, Braz il and
3Max-Planck-Institute for the Physics of Complex Systems, 0 1187 Dresden, Germany
The coupled kinetic equations for density and spin Wigner fu nctions are derived including spin-
orbit coupling, electric and magnetic fields, selfconsiste nt Hartree meanfields suited for SU(2) trans-
port. The interactions are assumed to be with scalar and magn etic impurities as well as scalar and
spin-flip potentials among the particles. The spin-orbit in teraction is used in a form suitable for
solid state physics with Rashba or Dresselhaus coupling, gr aphene, extrinsic spin-orbit coupling,
and effective nuclear matter coupling. The deficiencies of th e two-fluid model are worked out con-
sisting of the appearance of an effective in-medium spin prec ession. The stationary solution of all
these systems shows a band splitting controlled by an effecti ve medium-dependent Zeeman field.
The selfconsistent precession direction is discussed and a cancellation of linear spin-orbit coupling
at zero temperature is reported. The precession of spin arou nd this effective direction caused by
spin-orbit coupling leads to anomalous charge and spin curr ents in an electric field. Anomalous Hall
conductivity is shown to consists of the known results obtai ned from the Kubo formula or Berry
phases and a new symmetric part interpreted as an inverse Hal l effect. Analogously the spin-Hall
and inverse spin-Hall effects of spin currents are discussed which are present even without magnetic
fields showing a spin accumulation triggered by currents. Th e analytical dynamical expressions for
zero temperature are derived and discussed in dependence on the magnetic field and effective mag-
netizations. The anomalous Hall and spin-Hall effect change s sign at higher than a critical frequency
dependent on the relaxation time.
PACS numbers: 72.25.-b, 75.76.+j, 71.70.Ej, 85.75.Ss
I. INTRODUCTION
A. Motivation and outline
The interest in spin transport has regained a renais-
sance due to the promising application as next genera-
tion information storage. The experiments have reached
such high precession that single spin transport and spin
wave processes can be resolved and investigated in view
of applications to new nanodevices where spin-field tran-
sistors are proposed1. Many interesting effects have been
reported such as anomalous spin segregation in weakly
interacting6Li in a trap2which effect has been described
by the meanfield, spin-Hall effects and spin-Hall nano-
oscillators3. Different spin transport effects have led to
the spin current concept4which tries to summarize these
effects with respect to the current.
Thespin-orbitcouplinghasleadtotheideaofthe spin-
Hall effect5–7which was proposed8,9and first observed
in bulkn-type semiconductors10and in 2D heavy-hole
systems11. Spin and particle currents are coupled such
that one observesan accumulationof transversespin cur-
rent near the edges of the sample. The spin conductance
has been measured in mesoscopic cavities12to extract
the part due to spin-orbit coupling. Within the anoma-
lous Hall effect first described in Ref.13the spin polariza-
tion takes over the role of a magnetic field and creates a
current contribution14–16. This effect occurs when time-
symmetry is broken17and is related to the inverse spinHall effect18. For the latter one spin-orbit coupling takes
the role of an additional electric field.
Anisotropic magnetoresistance together with the
anomalous Hall coefficients have been measured and
attributed to spin-orbit coupling19,20and treated in
quantum wires21and mesoscopic rings22. The lattice
structure causes strong dependencies on the transport
direction23.
One distinguishes between extrinsic and intrinsic spin-
Hall effects. The extrinsic is due to spin-dependent scat-
teringbymixing ofspin and momentum eigenstates. The
intrinsic effect is an effect of the momentum-dependent
internal magnetic field due to spin-orbit coupled band
structures. This leads to a spin splitting of the en-
ergy bands in semiconductors due to lacking of inver-
sion symmetry. Most observations are performed with
the extrinsic10,24–26and only some for the intrinsic spin-
Hall effect11,27. There are different model treatments of
intrinsic28,29and extrinsic spin-Hall effects30sometimes
usingBerrycurvatures17,31–33,theLandauerformula31or
even relativistic treatments34,35. A theoretical compar-
ison of the relativistic approach with the Kubo formula
is found in36. A detailed discussion of possible occur-
ring spin-orbit couplings in semiconductor bulk struc-
tures and nanostructures can be found in37and in the
book5. For the Rashba coupling and quadratic disper-
sion in disordered two-dimensional systems it has been
shown that the spin-Hall effect vanishes38–40. This is not
the case if magnetic scatters are considered41. The in-2
trinsic anomalous Hall effect is treated also in Ref.42and
in disordered band ferromagnets43.
The (pseudo)spin-Hall effect in graphene is cur-
rently a very heavily investigated field44reporting also
the anomalous Hall effect in single-layer and bilayer
graphene45,46and which is treated like a spin-orbit cou-
pled system47. Recently even spin-orbit coupled Bose-
Einstein condensates have been realized48.
The main motivation of the present paper is to derive
in an unambiguous way a kinetic equation of interacting
spin-polarized fermions including magnetic and electric
fields with spin-orbit coupling. Normally one finds all
four problems treated separately in the literature. First,
there exists a vast literature to derive kinetic equations
with spin-polarized electrons49–60. Second, other quan-
tum kinetic approaches focus exclusively on the spin-
orbit coupling61–64. Third, the transport in high and low
magnetic fields itself is involved due to precession mo-
tionsofchargedparticlesandtreatedapproximately65–71.
Fourth, the interaction with scalar and magnetic impu-
rities requires a certain spin-coupling which is important
for transport effects in ferromagnetic materials72–74.
Here we will combine all four difficult problems into a
unifying quantum kinetic theory. First we restrict our-
selves to approximate the many-body interactions by the
mean field and a conserving relaxation time. The out-
lined formalism is straight forward to derive proper col-
lision integrals as done in the literature51,53,56,75–77. The
reasons to consider once again the lowest-order many-
body approximation is twofold. On one side during the
derivation of the proper kinetic equations it turned out
that even on the meanfield level all four effects together
create additional terms when considered on a common
footing not known so far. On the other side, with a
meanfield quantum kinetic equation including all these
effects we have the possibility to linearize with respect
to an external perturbation and to obtain in this way
the response function in the random phase approxima-
tion (RPA). As a general rule, when a lower-level kinetic
equation is linearized, a response of higher-order many-
body correlations is obtained78.
Most treatments of the response function use approxi-
mations already at the beginning and concentrate only
on specific effects, such asthe diffusive regime31,79or
currents80. We will explicitly work out these response
functions in the second paper of this series. Here in the
first paper we want to focus on the derivation of the
quantum kinetic equation including all these effects as
transparently as possible. With the aim to derive the
RPA response we concentrate on the correct mean-field
formulation and restrict ourselves to a relaxation-time
approximation of the collision integral as a first step.
This relaxation time will be understood with respect to
a local equilibrium which accounts for local conservation
laws81–85. Though it can be derived from Boltzmann col-
lision integrals, this relaxation time approximation omits
quantum interference effects such as weak localization
due to disorder, for an adequate treatment of these ef-fects see, e.g.,86.
The outline of this first paper is as follows. After ex-
plaining the basic notation we present in the second sec-
tion the phenomenological two-fluid model and show the
insufficiency due to the missing self-consistent precession
direction. We present an educative guess for the proper
kinetic equation from the demand of SU(2) symmetry.
Interestingly, this leads already to the correct form of
the kinetic equation except for four parameters which
have to be derived microscopically in Sec. III. We use
the nonequilibrium Green’s function technique in the no-
tation of Langreth and Wilkins87. The obtained kinetic
equations lead to a unique static solution which shows
the splitting of the band due to spin-orbit interference.
The anomalous current is shown to cancel the normal
one in the stationary state pointing to the importance
of the anomalous currents when the balance is disturbed
like in transport. The selfconsistent precession direction
is calculated explicitly for zero temperature and linear
spin-orbit coupling. In Sec. IV we compare the derived
kineticequationwiththeguessedoneofSec. IIdetermin-
ing the remaining open parameters. The anomalous Hall
and spin-Hall effects are calculated in Sec. IV and ap-
pear in agreement with other approaches using the Kubo
formula or helicity basis. We obtain a dynamical sym-
metric contribution interpreted as inverse spin-Hall and
inverse Hall effects. Analytical expressions are discussed
for the dynamical conductivities at zero temperature and
linearspin-orbitcoupling. Asummaryconcludesthefirst
paper of this series.
B. Basic notation
The spin of a fermion/planckover2pi1
2/vector σwith the Pauli matrices /vector σ
as an internal degree of freedom analogously to circular
motion leads to the elementary magnetic moment for the
spin in terms of the Bohr magneton µB,
ˆ/vector m=ge
2me/planckover2pi1
2/vector σ=g
2µB/vector σ (1)
with the anomalous gyromagnetic ration g≈2 for elec-
trons. If there are many fermions with densities n±of
spins parallel/antiparallel to the magnetic field, the to-
tal magnetization is mz=gµBszwith the polarization
sz= (n+−n−)/2 We want to access the density and
polarization density distributions and use therefore four
Wigner functions
ˆρ(/vector x,/vector p) =f(/vector x,/vector p)+/vector σ·/vector g(/vector x,/vector p) =/parenleftbigg
f+gzgx−igy
gx+igyf−gz/parenrightbigg
(2)
with the help of which the density and polarization den-
sity are given by
/summationdisplay
pf=n(/vector x),/summationdisplay
p/vector g=/vector s(/vector x) (3)3
where/summationtext
p=/integraltext
dDp/(2π/planckover2pi1)DforDdimensions and the
magnetization density becomes /vectorM(/vector x) =gµB/vector s(/vector x). The
advantage is that we can describe any direction of mag-
netization density created by microscopic correlations
which will be crucial in this paper. Sometimes one finds
the probability distribution of spin up/down in the di-
rection/vector eof the mean polarization by the spin projection
or a twofold additional spin variable69,70is used. Since
thereareinversionformulas88alltheseapproachesshould
be equivalent. However, we prefer the presentation of
the Wigner function in terms of the scalar and vector
parts (2) since the coupling between these functions bear
clear physical meaning which is somewhat buried in the
sometimes used super distribution. Moreoverthe Wigner
functions (3) yield directly the total density andthe spin-
polarizations.
C. Spin-orbit coupling
Any spin-orbit coupling used in different fields, say
plasma systems, semiconductors, graphene or nuclear
physics can be recast into the general form
Hs.o.=A(/vector p)σx−B(/vector p)σy+C(/vector p)σz=/vectorb·/vector σ(4)
with a momentum-dependent /vectorbillustrated in table I and
which can become space and also time-dependent in
nonequilibrium. Also the Zeeman term is of this form.
The time reversal invariance of spin current due to spin-
orbit coupling requires that the coefficients A(p) and
B(p) be odd functions of the momentum kand there-
fore such couplings have no spatial inversion symmetry.
Also 3D systems of spin-1/2 particles can be recast into
the form (4). Let us shortly discuss different realizations
since we want to treat all of them within the quantum
kinetic theory.
1. Extrinsic spin-orbit coupling
First we might think on the direct spin-orbit coupling
as it appears due to expansion of the Dirac equation
where only the Thomas term is relevant
/vector σ·ie/planckover2pi12
8m2c2/parenleftbigg
∂R×/vectorE−2i
/planckover2pi1/vectorE×/vector p/parenrightbigg
≈λ2/vector σ·(/vector p
/planckover2pi1×∇V)(5)
withλ2=/planckover2pi12/4m2
ec2≈3.7×10−6˚A2for electrons. The
electric field is not an external one, but e.g. created by
the nucleus /vectorE=−/vector∇V, and is called extrinsic spin-orbit
coupling. The spin-orbit coupling mixes different mo-
mentum states and is coupled to inhomogeneities in the
material. The matrix elements ofthe spin-orbit potential
reads
/an}b∇acketle{t/vector p2|Vs.o.|/vector p1/an}b∇acket∇i}ht=iλ2
/planckover2pi12V(/vector p)(/vector p×/vector σ)·/vector q (6)with the center-of-mass momentum /vector q= (/vector p1+/vector p2)/2 and
/vector p=/vector p1−/vector p2. Any such spin-orbit coupling possesses the
general structure (4).
2. Intrinsic spin-orbit coupling in semiconductors
For direct gap cubic semiconductors such as GaAs
the form (4) of spin-orbit coupling arises by coupling of
the s-type conductance band to p-type valence bands.
With in the 8 ×8 Kane model the third-order perturba-
tion theory5yieldsλ=P2/3[1/E2
0−1/8(E0+∆0)2] with
the gapE0and the spin-orbit splitting ∆ 0between the
J= 3/2 andJ= 1/2 hole bands and a matrix element
P. For GaAs one finds λ= 5.3˚A2which shows that
in n-type GaAs the spin-orbit coupling is six orders of
magnitude stronger than in vacuum and has an opposite
sign89. The cubic Dresselhaus spin-orbit corrections are
usually neglected since they are small and does not ap-
pear in the 8 ×8model. Therefore the spin-orbit coupling
is considered to come from the potential of the driving
field and the impurity centers.
In a GaAs/AlGaAs quantum well there can be two
types of spin-orbit couplings that are linear in momen-
tum. One considers a narrow quantum well in the /vector n=
[001] direction. The linear Dresselhaus spin-orbit cou-
pling is due to the bulk inversion asymmetry of the zinc-
blende type lattice. It is proportional to the kinetic en-
ergy of the electron’s out-of-plane motion and decreases
therefore quadratically with increasing well width. In
lowest-order momentum one obtains
Hs.o.
D=βD
/planckover2pi1(−pyσy+pxσx) (7)
again of the form (4) with /vectorb=βD(−px,py,0)//planckover2pi1.
The Rashba spin-orbit coupling (SOC)
Hs.o.
R=βR
/planckover2pi1(−pxσy+pyσx) =βR
/planckover2pi1/vector σ·(/vector p×/vector n) (8)
is finally due to structure inversion asymmetry and the
strength can be tuned by a perpendicular electric field,
for example by changing the doping imbalance on both
sides of the quantum well. The Rashba coupling is again
of the form (4) with /vectorb=βR(py,−px,0)//planckover2pi1. Note that
the Rashba SOC has winding number +1 as the momen-
tum direction winds around once in momentum space,
whereas the linear Dresselhaus has the opposite winding
-190.
There are further types of spin-orbit expansion
schemes for quasi-2D systems such as cubic Rashba and
cubic Dresselhaus expansions whose competing inter-
play is treated too91. These terms including wurtzite
structures92all together can be recast into the form of
(4) and seen in table I.4
TABLE I: Selected 2D and 3D systems with the Hamiltonian
described by (4) taken from92,93
2D−system A(p) B(p) C(p)
Rashba βRpy βRpx
Dresselhaus[001] βDpx βDpy
Dresselhaus[110] βpx −βpx
Rashba−Dresselhaus βRpy−βDpxβRpx−βDpy
cubicRashba(hole) iβR
2(p3
−−p3
+)βR
2(p3
−+p3
+)
cubicDresselhaus βDpxp2
y βDpyp2
x
Wurtzitetype ( α+βp2)py(α+βp2)px
single−layergraphene vpx −vpy
bilayergraphenep2
−+p2
+
4mep2
−−p2
+
4mei
3D−system A(p) B(p) C(p)
bulk Dresselhaus px(p2
y−p2
z)py(p2
x−p2
z)pz(p2
x−p2
y)
Cooperpairs ∆ 0p2
2m−ǫF
extrinsic
β=i
/planckover2pi1λ2V(p)qypz−qzpyqzpx−qxpzqxpy−qypx
neutrons in nuclei
β=iW0(nn+np
2)qzpy−qypzqxpz−qzpxqypx−qxpy
3. Spin-orbit coupling in graphene
Solving the tight-binding model on the honeycomb
lattice including only nearest neighbor hopping gives
an effective two-band Hamiltonian for the Bloch wave
function which can be considered as coupled pseudo-
spins. The interband coupling of these different bands
in graphene leads to the spin-orbit coupling of the form
(4).
4. Spin-orbit coupling in nuclear matter
In nuclearmatter the spin-orbitinteractionis strongin
heavy elements and the reason for magic numbers. Shell
structures cannot be described properly without consid-
eration of the spin-orbit interaction coming from the ten-
sor part of the nuclear forces94. The effective spin-orbit
couplinginnuclearmatterwithneutronsandprotonscan
be considered as a meanfield expression due to schematic
Skyrme forces and is expressed in the Rashba form (8)
which reads for neutrons95
Hs.o.=−W0
2/vector σ[/vector p×(/vector∇np+2/vector∇nn)] (9)
and interchanging np↔nnfor protons. One sees that in
this Hartree-Fock expression the effective direction /vector nof
Rashba form (8) is given by the gradient of the densities.
Therefore the structure appears as in extrinsic spin-orbit
coupling. The coupling constant is a matter of debateand dependent on the used density functional96. Further
terms can be considered if more involved Skyrme poten-
tials are used leading to additional current coupling97,98.
It is expected that the spin-orbit coupling plays an im-
portantrolein heavy-ionreactions99and in rareisotopes.
II. PHENOMENOLOGICAL KINETIC
EQUATION
A. Deficiencies of two fluid model
Nowweconsiderthewidelyusedtwo-fluidmodel100,101
developed from the two-current conduction in iron102.
It consists of a distribution for spin-up f↑and spin-
downf↓parts. Until recently it was used to explain
even anisotropic magnetic resistance103with its limits
observed there. Indeed we will show that an important
part is missing in this model. Besides the two distribu-
tion functions we have to consider the direction of the
mean spin or polarization. As we will see this leads to a
third equation which is silently overlooked in these mod-
els. From general SU(2) symmetry considerations one
can already conclude that this part is missing in the two-
fluidmodelandhowitsformshouldappear. Thedetailed
derivation will be performed in the next section. Here we
repeat briefly the two-fluid model and develop the miss-
ing parts from general physical grounds.
We start with the linearized coupled kinetic equations
for the two components
∂tδf↑+/vector p
me/vector∂rδf↑−/vector∂r(Uext+U↑↑δn↑+U↑↓δn↓)/vector∂pf0
↑
=−δf↑
τ↑↑−δf↑−δf↓
τ↑↓
∂tδf↓+/vector p
me/vector∂rδf↓−/vector∂r(Uext+U↓↓δn↓+U↓↑δn↑)/vector∂pf0
↓
=−δf↓
τ↓↓−δf↓−δf↑
τ↓↑(10)
with the external electric field e/vectorE=−/vector∂rUext. The
relaxation due to collisions is considered as relaxation
times with respect to the same kind of particle τ↑↑or
τ↓↓and with respect to the other sort which is described
by the cross relaxation time τ↑↓=τ↓↑due to symmetric
collisions. For later use we have added also the spin-
dependent meanfields U/angbracketrightand their linearization Uij=
∂Ui/∂njwith respect to the densities n↑,↓=/summationtext
pf↑,↓.
Multiplying (10) with /vector pand integrating together with
Fourier transform ∂t→ −iωand/vector∂r→i/vector qleads to
the coupled equations for the currents in lowest-order
wavevector /vector q
(ρ↑+r↑↓)δJ↑−r↑↓δJ↓=E
−r↓↑δJ↑+(ρ↓+r↓↑)δJ↓=E (11)
where we have introduced the partial and crossed resis-5
ρ
ρ ρρ /2
/2/2
/2r
FIG. 1: Resistor scheme of (13) illustrating the spin mixing .
tivities [(i,j) =↑,↓]
1
ρi=σi=nie2τii
me(1−iωτii), r ij=me
nie2τij.(12)
The partial currents (11) are easily solved and one ob-
tains the total resistivity
ρ=E
δJ↑+δJ↓=ρ↑ρ↓+ρ↑r↑↓+ρ↓r↑↓
ρ↑+ρ↓+2(r↑↓+r↓↑).(13)
Assuming further that r=r↓↑=r↑↓this resistivity al-
lows an interpretation as composed resistivity illustrated
in figure 1 which shows the role of the cross scattering
between different species known as spin mixing.
Despite the successful application of this model104it
has an important inconsistency which is not easy to rec-
ognize. We therefore rewrite the kinetic equations (10)
into a form for the total density distribution and total
density
f=1
2(f↑+f↓);n=1
2(n↑+n↓) (14)
and the polarization distribution and total spin
g=1
2(f↑−f↓);s=1
2(n↑−n↓) (15)
which reads (Fourier transform /vector∂r→i/vector q)
∂tδf+i/vector q/vector p
meδf+e/vectorE/vector∂pf0−Mf=−δf
τ+−δg
τ−
∂tδg+i/vector q/vector p
meδg+e/vectorE/vector∂pg0−Mg=−δf
τ−−δg
τ+−2δg
τD
(16)
with the meanfield parts abbreviated as
Mf=i/vector q/vector∂pf0(V1δn+V3δs)+i/vector q/vector∂pg0(V2δn+V4δs)
Mg=i/vector q/vector∂pg0(V1δn+V3δs)+i/vector q/vector∂pf0(V2δn+V4δs).
(17)
Here it was convenient to introduce the relaxation times
1
τ±=1
2/parenleftbigg1
τ↑↑±1
τ↓↓/parenrightbigg
;τD=τ↑↓=τ↓↑(18)and the meanfield potentials
V1/2=U↑↑+U↑↓±(U↓↑+U↓↓)
V3/4=U↑↑−U↑↓±(U↓↑−U↓↓).(19)
The crucial point is now that the polarization or total
spin has a direction /vector ewhich means we have to consider
thevectorquantity /vector g=g/vector ewhichtranslatesintotwoparts
when linearized δ/vector g=gδ/vector e+/vector eδg. Only the second part is
obviously covered by the second equation of (16). The
equation for δ/vector eremains undetermined so far.
B. Educated guess from SU(2) symmetry
However from general consideration of SU(2) symme-
try we can infer the form in which this missing equation
will appear and which we will derive in the next section
from microscopic theory.
It is convenient to write both scalar distribution fand
vector distribution /vector gtogether in spinor form (2). Then
any collision integral and therefore any kinetic equation
must be possible to write as commutator and anticom-
mutator in spin-space where the forms
1
2/bracketleftig
δˆρ,a+/vector σ·/vectorb/bracketrightig
+=aδf+/vectorb·δ/vector g+/vector σ·/parenleftig
aδ/vector g+/vectorbδf/parenrightig
1
2[δˆρ,a+/vector σ·/vector c]−=i/vector σ·(δ/vector g×/vector c) (20)
can appear making use of ( /vector a·/vector σ)(/vectorb·/vector σ) =/vector a·/vectorb+i/vector σ·(/vector a×/vectorb).
Therefore the expected kinetic equation reads
∂tδˆρ+i/vector p/vector q
meδˆρ+e/vectorE/vector∂pˆρ0
−i
2/bracketleftig
/vector q/vector∂pˆρ0,a+/vectorb/vector σ/bracketrightig
+−i
2/bracketleftig
/vector q/vector∂pˆρ0,/vector c/vector σ/bracketrightig
−−i
2[ˆρ0,/vectorh·/vector σ]−
=−1
2/bracketleftbigg
δˆρ,1
τ+/vector τ−1·/vector σ/bracketrightbigg
+−1
2/bracketleftig
δˆρ,/vectord·/vector σ/bracketrightig
−(21)
with the yet undetermined constants a,/vectorb,/vector c,/vectord,/vectorh. Here
the first line describes the scalar drift which can be triv-
ially written in anticommutators. The commutator and
anticommutator on the second line are the meanfields
including a possible precession in the second and third
terms. The third line expresses possible relaxations.
Now the compact equation (21) is decomposed into
the components δfand/vectorδg=/vector eδg+gδ/vector ewith the help of
(20). The aim is to specify the three remaining vectors
/vector c,/vectordand/vectorhsuch that the results of the two-fluid model
(16) are reproduced. The two values a=V1δn+V3δs
and/vectorb= (V2δn+V4δs)/vector ecan be already determined since
only this choice creates the meanfield terms in (16). It is
convenient to decompose the so far unspecified vectors
/vector c=c/vector e+c1δ/vector e+c2/vector e×δ/vector e
/vectord=d/vector e+d1δ/vector e+d2/vector e×δ/vector e (22)6
accordingto the three orthogonaldirections since /vector e·∂/vector e=
0 due to |/vector e|2= 1. We obtain from (21) the analogous
equations to (16)
∂tδf+i/vector q/vector p
meδf+e/vectorE/vector∂pf0−Mf=−δf
τ−δ/vector g·/vector τ−1
+ig0/vectorb·q∂pδ/vector e
∂tδg+i/vector q/vector p
meδg+e/vectorE/vector∂pg0−Mg=−δf(/vector e·/vector τ−1)−δg
τ
+c1g0/vector e·(q∂p/vector e×δ/vector e)−c2q∂p/vector e·δ/vector e−ig0d2(δ/vector e)2(23)
Comparing the two-fluid model (16) with (23) we find
the unique identification c2=d2=c1= 0. Further one
sees that we have to set
1
τ=1
τ++2
τD;/vector e·/vector τ−1=1
τ−(24)
and the cross relaxation time has to be determined by
2
τDδf=−g0(/vector τ−1·δ/vector e)+ig0/vector e·q∂pδ/vector e(V2δn+V4δs).
(25)
Only with these settings we obtain exactly the two-fluid
model (16). The resulting equation (25) reveals that the
cross relaxation time τD, see (18), can be only obtained
with the solution of the equation for the direction δ/vector e
which, however, is a dynamical (frequency-dependent)
one. This shows what one silently approximates when
using a constant cross relaxation time τD.
Finally from (21) the equation for δ/vector etakes the form
∂tδ/vector e+i/vector q/vector p
meδ/vector e+e/vectorE/vector∂p/vector e+/vector e×/bracketleftbigg
c/vector q/vector∂p/vector e+/vectorh−i(d−δg
gd1)δ/vector e/bracketrightbigg
=−δf
g/bracketleftbig
/vector e×(/vector τ−1×/vector e)/bracketrightbig
−δ/vector e
τ+i/vector q/vector∂p/vector e(V1δn+V3δs).(26)
The drift side has the usual form extended by a preces-
sion term around the axes /vector e. This spin-precession term
is expected and the values of d,d1,cand/vectorhwill be de-
rived in the next section which should include the exter-
nal magnetic field as one part of the defining axes. The
righthandsidein(26)containstherelaxationmechanism
which shows a coupling to the solution δfand mean field
contributions which will be obtained from a proper mi-
croscopic theory.
Summarizingthe resultsofthis sectionwe havestarted
with the often used two-fluid model together with mean-
field terms. Fromaproperwritingofthe kinetic equation
in spinor form (21) required by SU(2) symmetry we have
seen that a third equation for the change of the spin di-
rection is needed. Further it reveals that the cross relax-
ation time canbe consideredonly approximatelyastime-
independent and constant. The general possible form of
the kinetic equation for the scalar (total density) distri-
bution, the polarization(total spin) distribution, and the
total spin direction is already settled except three scalars
c,d,d1and one vector /vectorhto be derived from a microscopictheory, see later (102). It is remarkable that the demand
of SU(2) symmetry leads already to such a far leading
determination of the structure of equations.
III. QUANTUM KINETIC EQUATION
A. Green-functions
Let us consider spin-polarized fermions which interact
with impurity potential Viand are themselves coveredby
the Hamiltonian
ˆH=/summationdisplay
iΨ+
i/bracketleftigg
(/vector p−e/vectorA(/vectorRi,t))2
2me+eΦ(/vectorRi,t)
−µB/vector σ·/vectorB+/vector σ·/vectorb(/vector p,/vectorRi,t)+ˆVi(/vectorRi)/bracketrightig
Ψi
+1
2/summationdisplay
ijΨ+
iΨ+
jˆV(/vectorRi−/vectorRj)ΨjΨi (27)
with the spinor Ψ i= (ψi↑,ψi↓) such that any of the spin-
orbit couplings discussed above and the Zeeman term are
included. Weassumeatwo-particleinteractionwhichhas
a scalar and a spin-dependent part
ˆV=V0+/vector σ·/vectorV (28)
wherethe latteris responsibleforspin-flip reactions. The
vectorpart ofthe potential describese.g. spin-dependent
scattering. The scattering off impurities consists of a
vector potential from magnetic impurities and a scalar
one from charged or neutral impurities
ˆVi=Vi0+/vector σ·/vectorVi. (29)
In this way we have included the Kondo model as spe-
cific case which was solved exactly in equilibrium105and
zero temperature. Here we will consider the nonequilib-
rium form of this model in the meanfield approximation
including relaxation due to collisions.
We use the formalism of the nonequilibrium Green’s
function technique in the generalizedKadanoff-Baymno-
tation introduced by Langreth and Wilkins87. The two
independent real-time correlation functions for spin-1 /2
fermions are defined as
G>
αβ(1,2)=/an}b∇acketle{tψα(1)ψ†
β(2)/an}b∇acket∇i}ht, G<
αβ(1,2)=/an}b∇acketle{tψ†
β(2)ψα(1)/an}b∇acket∇i}ht(30)
whereψ†(ψ) are the creation (annihilation) operators, α
andβare spin indices, and numbers are cumulative vari-
ables for space and time,1 ≡(/vector r1,t1). Accordingly, all the
correlation functions without explicit spin indices, are
understood as 2 ×2 matrices in spin space, and they can
be written in the form ˆC=C+/vector σ·/vectorC, whereC(/vectorC) is the
scalar (vectorial) part. This will result in preservation of
the quantum mechanical behavior concerning spin com-
mutation relations even after taking the quasi classical
limits of the kinetic equation. The kinetic equation is7
obtained from the Kadanoff and Baym (KB) equation106
for the correlation function ˆG<
−i(ˆG−1
R◦ˆG<−ˆG<◦ˆG−1
R) =i(ˆGR◦ˆΣ<−ˆΣ<◦ˆGA) (31)
whereˆΣ is the self-energy, and retarded and advanced
functions are defined as
CR,A(1,2) =∓iθ(±t1∓t2)[C>(1,2)+C<(1,2)]+CHF
(32)
whereCHFdenotes the time-diagonal Hartree-Fock
terms discussed later. Products ◦are understood as in-
tegrations over intermediate variables, space and time,
A◦B=/integraltext
d¯t/integraltext
d¯/vector rA(/vector r1,t1;¯/vector r,¯t)B(¯/vector r,¯t;/vector r2,t2). The nota-
tion of Langreth and Wilkins87used here has the ad-
vantage that the correlation functions G≷bear a direct
physical meaning of occupation of particles and holes.
Alternatively sometimes the Keldysh function is used107
which has to be linked to physical quantities. Moreover
in this latter Keldysh-matrix notation a superfluous de-
gree of freedom occurs canceling in any diagrammatic
expansion108which is absent when directly using corre-
lationfunctions andtheretarded/advancedGreen’sfunc-
tions.
We are interested in the Wigner distribution function
(2) which is given by the equal time ( t1=t2=T,t= 0)
correlation function ˆG<(/vectork,/vectorR,t= 0,T)
ˆρ(/vector p,/vectorR,T) =ˆG<(/vector p,/vectorR,t= 0,T)
=/integraldisplaydω
2πˆG<(/vector p,ω,/vectorR,T) =f+/vector σ·/vector g.(33)
We use the Wigner mixed representation in terms of the
center-of-mass variables /vectorR= (/vector r1+/vector r2)/2 and the Fourier
transform of the relative variables /vector r=/vector r1−/vector r2→/vector p
which separatesthe fast microscopicvariations from slow
macroscopic variations.
To derive the kinetic equation we expand the convolu-
tion up to second-order gradients. Matrix product terms
A◦Bappearing in the KB equation can be written as
A◦B→ei
2(∂Ω∂B
T−∂A
T∂B
Ω−∂A
p∂B
R+∂A
R∂B
p)AB. (34)
The quasi-classical limit is obtained by keeping only the
first gradients in space and time of the above gradient
expansion
A◦B→AB+i
2{A,B}, (35)
where curly brackets denote Poisson’s brackets, i.e.,
{A,B}=∂ΩA∂TB−∂TA∂ΩB−∂pA∂RB+∂RA∂pB.
Therefore, in the lowest-order gradient approximation,
we have the following rule to evaluate the commutators
[A,B]−in the KB equation
[A◦,B]−→[A,B]−+i
2({A,B}−{B,A})
= [A,B]−+i
2/parenleftbigg
[∂RA,∂pB]+−[∂pA,∂RB]+
+[∂ΩA,∂TB]+−[∂TA,∂ΩB]+/parenrightbigg
.(36)Please note that the quantum spin structure remains un-
touched even after gradient expansion due to the com-
mutators.
B. Gauge
In order to prevent ambiguous results for different
choice of gauges, we need to formulate the theory in
a gauge-invariant way. Under U(1) local gauge the
wave function and vector potential transform as Φ′=
e−ie
/planckover2pi1α(x)Φ andA′
µ=Aµ+∂µα(x) such that the Green-
function transform itself as
G′(12) =/an}b∇acketle{tΦ′
1Φ′
2/an}b∇acket∇i}ht=/an}b∇acketle{tΦ1Φ2/an}b∇acket∇i}hte−ie
/planckover2pi1α(X+x
2)−ie
/planckover2pi1α(X−x
2)
=/an}b∇acketle{tΦ1Φ2/an}b∇acket∇i}hte−ie
/planckover2pi1xµ1/2/integraltext
−1/2dλ∂µα(X+λx)
.
(37)
This shift can be compensated if a corresponding phase
is added. This is achieved by using a modified Fourier
transform
G(kX) =/integraldisplay
dxei
/planckover2pi1xµ/parenleftBigg
kµ+e1/2/integraltext
−1/2dλAµ(X+λx)/parenrightBigg
×G/parenleftig
X+x
2,X−x
2/parenrightig
. (38)
whereA= (φ(/vectorR,T),/vectorA(/vectorR,T)) and we used four-vector
notationx= (t,/vector r)andX= (T,/vectorR). Itisobviousthatthis
gauge-invariant Fourier transform leads to gradients as
well. To see this we consider the general gauge-invariant
Fourier transform for Aµ= (Φ(/vectorR,T),/vectorA(/vectorR,T)) in gradi-
ent expansion
/vector p=/vectork+e1
2/integraldisplay
−1
2dλ/vectorA(/vectorR+λ/vector r,T+λτ)
=/vectork+e1
2/integraldisplay
−1
2dλeλ/vector r∂A
Reλτ∂A
T/vectorA(/vectorR,T)
→/vectork+e1
2/integraldisplay
−1
2dλe−i/planckover2pi1λ∂p∂A
Rei/planckover2pi1λ∂ω∂A
T/vectorA(/vectorR,T)
=/vectork+esinc/parenleftbigg/planckover2pi1
2∂p∂A
R/parenrightbigg
sinc/parenleftbigg/planckover2pi1
2∂ω∂A
T/parenrightbigg
/vectorA(/vectorR,T)(39)
with sinc(x) = sinx/x= 1−x2/3!+−...and analogously
Ω =ω+esinc/parenleftbigg/planckover2pi1
2∂p∂Φ
R/parenrightbigg
sinc/parenleftbigg/planckover2pi1
2∂ω∂Φ
T/parenrightbigg
Φ(/vectorR,T).(40)
One sees that up to second order gradients we
have correctly the following rules for gauge invariant8
formulation109,110: (1) Fourier transform of the differ-
ence variable xto the canonical momentum /vector p. (2) Shift
from canonical momentum to the gauge invariant (kine-
matical) momentum kµ=pµ−e/integraltext1/2
−1/2dλAµ(X+λx),
which becomes kµ=pµ−eAµin the lowest-order gradi-
ent expansion. (3) Then the gauge invariant functions ¯G
reads
¯G(/vectork,ω,/vectorR,T) =G(/vectork+e/vectorA,ω+φ,/vectorR,T) =G(/vector p,Ω,/vectorR,T).
(41)
This treatment ensures that one has even included all
orders of a constant electric field.
C. Meanfield
We want to consider now the meanfield selfenergy for
impurity interactions as well as spin-orbit couplings. A
general four-point potential can be written
/an}b∇acketle{tx1x2|ˆV|x′
1x′
2/an}b∇acket∇i}ht=/summationdisplay
p,p′e−ip(x1−x2)+ip′(x′
1−x′
2)
×/an}b∇acketle{tp|ˆV/parenleftigg
x1+x2
2−x′
1+x′
2
2,x1+x2
2+x′
1+x′
2
2
2/parenrightigg
|p′/an}b∇acket∇i}ht
=ˆV−p,p′δ/parenleftbiggx1+x2
2−x′
1+x′
2
2/parenrightbigg
(42)
with
ˆV−p,p′=
V0(p′−p)
/vector σ·/vectorV(p′−p)
iλ2
/planckover2pi1/vector σ·(/vector p×/vector p′)V(p′−p)(43)
for scalar, magnetic impurities (29), the two-particle
interaction (28), and extrinsic spin-orbit coupling (6).
Since the potential is time-local, the Hartree-meanfield is
the convolution with the Wigner function (33) and writ-
ten with Fourier transform of difference coordinates
ˆΣ(p,R,T) =/summationdisplay
R′qQeiq(R−R′)ˆρ(Q+p,R′,T)ˆVq−Q
2,q+Q
2.(44)
Due to the occurring product of the potentials (28), (29)
and the Wigner function (33) one has
ˆVˆρ=V0f+/vector g·/vectorV+/vector σ·[f/vectorV+V0/vector g+i(/vectorV×/vector g)].(45)
The last term in (45) is absent since we work in sym-
metrized products as they appear on the left side of (31)
from now on. Consequently the selfenergy possesses a
scalar and a vector component
ˆΣH(/vector p,/vectorR,T) = Σ0(/vector p,/vectorR,T)+/vector σ·/vectorΣH(/vector p,/vectorR,T).(46)
The interaction between a conduction electron and the
magnetic impurity /vector σ·/vectorViwhere the direction of /vectorViis the
local magnetic field deserves some more discussion. Weassume that this magnetic field is randomly distributed
on different sites within an angle θlfrom the/vector ezdirection.
The directional average74leads then to
/summationdisplay
pf/vectorV=|V|sinθl
θl/vector ezn=/vectorV(q)n
/summationdisplay
p/vector g/vectorV=|V|sinθl
θl/vector ezs=/vectorV(q)s. (47)
The angleθlallows us to describe different models. A
completely random local magnetic field θl=πis used
for magnetic impurities in a paramagnetic spacer layer
and in a ferromagnetic layer one uses θl=π/4. The
latter one describes the randomly distributed orientation
against the host magnet74.
For impurity potentials the spatial convolution with
the density and spin polarization reads when Fourier
transformed, /vectorR→/vector q,
Σimp
0(p,q,T) =n(q)V0(q)+/vector s(q)·/vectorV(q)
/vectorΣimp(p,q,T) =/vector s(q)V0(q)+n(q)/vectorV(q).(48)
For extrinsic spin-orbit coupling we obtain
Σs.o.
0(/vector p,/vector q,T) =iλ2
/planckover2pi12V(q)/bracketleftig
me(/vectordj(q)×/vector q)j−/vector s(q)·(/vector p×/vector q)/bracketrightig
/vectorΣs.o.(/vector p,/vector q,T) =iλ2
/planckover2pi12V(q)/bracketleftig
me(/vectorj(q)×/vector q)−n(q)(/vector p×/vector q)/bracketrightig
.
(49)
The used particle density and current are
n=/summationdisplay
pg(/vector p,/vector q,T);/vectorj=/summationdisplay
p/vector p
meg(/vector p,/vector q,T) (50)
and the spin polarization and spin current
/vector s=/summationdisplay
p/vector g(/vector p,/vector q,T);/vectordi=/summationdisplay
p/vector p
me[/vector g(/vector p,/vector q,T)]i;dij=Sji.
(51)
Please note the summation over indices in the first line
of (49) after cross products.
Collecting these results the inverse retarded Green’s
function reads
ˆG−1
R(/vectork,Ω,/vectorR,T) = Ω−H−/vector σ·/vectorΣ(/vectork,/vectorR,T) (52)
with the effective scalar Hamiltonian
H=k2
2m+Σ0(/vectork,/vectorR,T)+eΦ(/vectorR,T) (53)
and/vectork=/vector p−e/vectorA(/vectorR,t). We have summarized the Zeemann
term, the intrinsic spin-orbit coupling, and the vector
part of the Hartree-Fockselfenergy due to impurities and
extrinsic spin-orbit coupling into an effective selfenergy
/vectorΣ =/vectorΣH(/vectork,/vectorR,T)+/vectorb(/vectork,/vectorR,T)+µB/vectorB (54)9
such that the effective Hamiltonian possessesPaulistruc-
ture
ˆHeff=H+/vector σ·/vectorΣ. (55)
Pleasenote thatone canconsider(54) asan effectiveZee-
man term where the spin-orbit competes with the mag-
netic field leading to additional degeneracies in Landau
levels111.
D. Commutators
Nowwe arereadyto evaluatethe commutatorsaccord-
ing to (36). In the following we drop the vector notation
where it is obvious. We calculate first the commutator
with the scalar parts of (52) where we use the gauge-
invariant Green’s function (41) such that one has
∂pG=∂k¯G
∂RG=∂R¯G−e∇Φ∂ω¯G−e(∇Ai)∂ki¯G
∂TG=∂T¯G−e∂TA∂k¯G−e∂TΦ∂ω¯G
∂ΩG=∂ω¯G. (56)
Further one calculates
∂TH=e˙Φ−ek
me˙A−e˙A∂kΣ0+˙Σ0
∂pH=k
me+∂kΣ0
∂RH=e∂RΦ+1
me[k×∂R×(p−eA)+(k·∂R)(p−eA)]
+∂RΣ0−e∂RAi∂kiΣ0
=e∇Φ−k
me×eB−e
me(k·∇)A+∂RΣ0−e∂RAi∂kiΣ0
(57)
where we have used1
2∇u2=u×∇ ×u+(u· ∇)u. We
obtain for the commutator with the scalar part of (52)
according to (36)
1
i[(Ω−H)◦,G<]−→/bracketleftbigg
∂T+(˙Σ0+evE)∂ω
+v∂R+(eE+ev×B−∂RΣ0)∂k/bracketrightbigg
¯G<(58)
where the mean velocity of the particles is given by
v=k
me+∂kΣ0 (59)
andE=−e∂RΦ−e˙AandB=∂R×A.
InordertogettheequationfortheWignerdistribution
we integrate over frequency and the second term on the
right hand side of (58) disappears. This term has the
structure of the power supplied to the particles which is
composed of the contribution by the electric field and the
time change of the scalar field which feeds energy to thesystem. The first and third part of (58) together are the
co-movingtime derivativeofaparticlewith velocity(59).
The fourth term in front of the momentum derivative of
¯G<represents the forces exercised on the particles which
appears as the Lorentz force and the negative gradient of
the scalar part of the selfenergy which acts therefore like
a potential.
Next we calculatethe commutator(36) with the vector
components of (52). Therefore we employ the relations
[/vector σ·/vectorA,ˆG<]+= 2/vector σ·/vectorAG<+2/vectorA·/vectorG<
/bracketleftig
/vector σ·/vectorA,ˆG</bracketrightig
−= 2i/vector σ·(/vectorA×/vectorG<) (60)
whereˆG<=G<+/vector σ·/vectorG<and using (56) we obtain
−i[−/vector σ·/vectorΣ◦,ˆG<]−→/bracketleftbigg
∂T+(˙Σ0+evE)∂ω+v∂R
+(eE+ev×B−∂RΣ0)∂k/bracketrightbigg
/vector¯G<
−2(/vectorΣ×/vector¯G<
)
+/bracketleftig
(˙/vectorΣ+evE)∂ω+∂k/vectorΣ∂R+(e∂k/vectorΣ×B−∂R/vectorΣ)∂k/bracketrightig
¯G<.
(61)
We recognize the same drift terms as for the scalar self-
energy components (58). Additionally, the vector self-
energy couples the scalar and spinor part of the Green
function by an analogous drift but controlled by the vec-
tor selfenergy instead of the scalar one.
E. Coupled kinetic equations
Integrating (58) over frequency and adding (61) we
have the complete kinetic equation as required from the
Kadanoff and Baym equation (31). In order to make it
more transparent we separate the equation according to
the occurring Pauli matrices. This is achieved by once
forming the trace and once multiplying with /vector σand form-
ing the trace. We obtain finally two coupled equations
for the scalar and vector part of the Wigner distribution
DTf+/vectorA·/vector g= 0
DT/vector g+/vectorAf= 2(/vectorΣ×/vector g) (62)
whereDT= (∂T+/vectorF/vector∂k+/vector v/vector∂R) describes the drift and
force of the scalar and vector part with the velocity (59)
and the effective Lorentz force
/vectorF= (e/vectorE+e/vector v×/vectorB−/vector∂RΣ0). (63)
The coupling between spinor parts is given by the vector
drift
Ai= (/vector∂kΣi/vector∂R−/vector∂RΣi/vector∂k+e(/vector∂kΣi×/vectorB)/vector∂k).(64)
Remember that we subsumed in the vector selfenergy
(54) the magnetic impurity meanfield, the spin-orbit cou-
pling vector, and the Zeeman term.10
The term (64) in the second parts on the left sides of
(62) represent the coupling between the spin parts of the
Wigner distribution. The vector part contains addition-
ally the spin-rotation term on the right hand side. These
coupled mean field kinetic equations including the mag-
netic and electric field, Zeeman coupling, and spin-orbit
coupling are the final result of the section. On the right
hand side one has to consider additionally collision inte-
grals which can be derived from the KB equation taking
the selfenergy beyond the meanfield approximation. In
the simplest way we will add a relaxation time.
Thesystem(62)isthemainresultofthispaperandthe
basisforthe further discussionincluding collectivemodes
in the secondpaper ofthe series. Thereforeit is time now
to compare with other approaches and lay out the gen-
eralizations obtained here. If one neglects the coupling
of the scalar distribution fto the vector distribution /vector g
in the second equation of (62) one has the Eilenberger
equation112extended here by magnetic and electric fields
as well as selfenergy effects. Compared to51we write
both scalar and vector components and have included
meanfield quasiparticle renormalizations and the vector
self energy. The coupling of the vector equation to the
scalar one has been neglected in113,114too but selfconsis-
tent quasiparticle energies and Zeeman fields have been
taken into account. In75,115only the transverse compo-
nents have been considered75which approximates two of
the four degrees of freedom in (62). The same reduction
of degrees of freedom at the beginning has been used
by the projection technique in56,116since the focus of all
these papers had been on the proper collision integral in-
stead. Selfconsistent quasiparticle equations have been
presented in54,60which have been decoupled by Landau
Fermi-liquid assumptions57and variational approaches.
The coupled kinetic equations have been derived with-
out spin-orbit coupling terms and reduced vector selfen-
ergies in117which disentangle the equation of moments.
Here we present all these effects without the assump-
tions found in different places of the above-mentioned
approaches.
F. Quasi stationary solution
The time-independent stationary solution should obey
the stationary mean-field equation (62) since any colli-
sion integral is then zero providing the Fermi distribu-
tion. However,the argumentsand functional dependence
as well as spin structure of the solution are already de-
termined from the stationary equation of the mean field
equation (62). We write them in formal notation
Df+/vectorA·/vector g= 0
D/vector g+/vectorAf= 2(/vectorΣ×/vector g) (65)
with
D={ǫk,...}, Ai={Σi,...} (66)and the Poisson bracket {a,b}=/vector∂ka·/vector∂Rb−/vector∂Ra·/vector∂kb.
The electric field is given by a scalar potential e/vectorE(R) =
−/vector∇Φ(R) such that we have the quasiparticle energy
ǫk(R) =k2
2me+Σ0(k,R)+Φ(R). (67)
The choice of gauge is arbitrary since we have ensured
that the kinetic equation is gauge invariant.
We rewrite (65) into one equation again by the spinor
representation ˆ ρ=f+/vector σ·/vector gusing the identity
/vector c·/vector g+(/vector σ·/vector c)f−2/vector σ·(/vector σ×/vector g) =
/vector σ·/vector c+2i/vector σ
2ˆρ+ ˆρ/vector σ·/vector c−2i/vector σ
2(68)
to arrive at
[D+/vector σ·/vectorA,ˆρ]++2i[/vector σ·/vectorΣ,ˆρ]−= 0 (69)
which is equivalent to (65). Now we search for a solu-
tion which renders both anticommutator and commuta-
tor zero separately.
For the anticommutator, the equation
(D+/vector σ·/vectorA)ˆρ= 0 (70)
and correspondingly ˆ ρ(D+/vector σ·/vectorA) = 0 are solved by any
function of the argument
ˆρ0/bracketleftig
ǫk(R)+/vectorΣ(k,R)·/vector σ/bracketrightig
(71)
due to (66). Employing the relation
e/vector σ·/vectorΣ= cosh |/vectorΣ|+/vector σ·/vector esinh|/vectorΣ|=/summationdisplay
s=±ˆPses|/vectorΣ|(72)
with the projectors ˆP±=1
2(1±/vector e·/vector σ) and/vector e=/vectorΣ/|/vectorΣ|we
have to have the stationary solution in the form
ˆρ0/bracketleftig
ǫk(R)+/vectorΣ(k,R)·/vector σ/bracketrightig
=/summationdisplay
±P±ˆρ±(ǫk±|/vectorΣ|).(73)
The demand of vanishing commutator in (69) works
further down the still general possibility of distribution
ˆρ±=¯f±+/vector σ·/vector g±. In fact it demands
0 = [/vector σ·/vectorΣ,ˆρ]−= [/vector σ·/vectorΣ,/vector σ·/vector g]−=i/vector σ·(/vectorΣ×/vector g) (74)
which implies that /vector g=/vector egwith the effective direction
/vector e=/vectorΣ/|/vectorΣ|. Together with (73) we obtain the stationary
solutionof(69) and consequentlyof(65) to havethe form
ˆρ(ˆε) =/summationdisplay
±ˆP±f±=f++f−
2+/vector σ·/vector ef+−f−
2
≡ρ+/vector σ·/vector ρ (75)
withf±=¯f±+g±=f0(ǫk(R)± |/vectorΣ(k,R)|) andf0an
unknown scalarfunction which is determined by the van-
ishing of the collision integral to be the Fermi-Dirac dis-
tribution.11
G. Currents
Duetothespin-orbitcoupling(4)thecurrentpossesses
annormalandanomalypart. Using[ /vectorb(/vector p),/vector x] =−i/planckover2pi1∂/vector p/vectorb(/vector p)
from elementary quantum mechanics we have
ˆvj=i
/planckover2pi1[ˆH,ˆxj] =vj+∂pj/vectorb·/vector σ (76)
andthequasiparticlevelocity vj=∂pjǫifthesingleparti-
cle Hamiltonian is given by the quasiparticle energy ǫ(p).
Together with the Wigner function ˆ ρ=f+/vector g·/vector σone has
ˆρˆvj=fvi+/vector g·/vectorβj+/vector σ·(vj/vector g+f∂pj/vectorb+i∂pj/vectorb×/vector g) (77)
and the particle current and spin current density reads
ˆJj=1
2/summationdisplay
p[ˆρ,vj]+=/summationdisplay
p/bracketleftig
fvj+/vector g·∂pj/vectorb+/vector σ·(vj/vector g+f∂pj/vectorb)/bracketrightig
=Jj+/vector σ·/vectorSj. (78)
Thescalarpartdescribestheparticlecurrent /vectorJ=/vectorJn+/vectorJa
consisting of a normal and anomaly current and the vec-
tor part describes the spin current Sijnot to be cinfused
with the polarization /vector s.
The stationary solution allows one to learn about the
seemingly cumbersome structure of the particle current
(78) consisting of normal and anomalous parts. In fact
both parts are necessary to guaranteethe absence of par-
ticlecurrentsinstationaryspin-orbitcoupledsystems. In
fact both partsseparatelyarenonzeroand onlytheirsum
vanishes. We expand the normal particle current with
(75) and/vectorΣ =/vectorΣn+/vectorblinear in the spin-orbit coupling /vectorb
to get
Jn
i=1
2/summationdisplay
p∂piǫ[f(ǫp+Σ)+f(ǫp−Σ)]
=1
2/summationdisplay
p∂piǫ/vectorΣn·/vectorb
Σn∂ǫ[f(ǫp+Σn)−f(ǫp−Σn)].(79)
The anomalous current reads linear in /vectorb
Ja
i=1
2/summationdisplay
p(∂pi/vectorb)·/vector e[f(ǫp+Σ)−f(ǫp−Σ)]
=1
2/summationdisplay
p/vectorΣn·∂pi/vectorb
Σn[f(ǫp+Σ)−f(ǫp−Σ)].(80)
Combining both currents one obtains
Ji=Ja
i+Jn
i
=/vectorΣn
Σn·1
2/summationdisplay
p∂pi/braceleftig
/vectorb[f(ǫp+Σ)−f(ǫp−Σ)]/bracerightig
= 0 (81)
as one should. This demonstrates the importance of the
anomalous current. One can consider the spin-orbit cou-
pling as a continuous current of normal quasiparticlescompensated by the spin-induced one. Any disturbance
and linear response will lead to interesting effects due to
this disturbed balance such as the anomalous Hall and
spin-Hall effects discussed in Sec. IV.
H. Selfconsistent precession direction
The meanfield approximation establishes a nonlinear
relationforparametersofthe distribution functions. The
quasi-stationary distribution (75) is determined by the
selfenergy(48), (45) and(54) whichin turn is determined
againbythe distribution. Without spinpolarizationusu-
ally this leads to the selfconsistent determination of the
chemical potential.
Now we have to accept that the spin precession direc-
tion obeys a similar selfconsistency and has to be deter-
mined accordingly.
Let us assume that the external magnetic field is in
the z-direction as is the mean local magnetic field of the
magnetic impurities (47) and write µBBeff=nV+µBB.
Since the effective local spin (precession) direction is /vector e=
/vectorΣ/Σ the mean polarization reads with (54)
/vector s=/summationdisplay
p/vectorb(p)+µBBeff/vector ez+V0/vector s
|/vectorΣ|g
=/summationtext
p/vectorbg
|/vectorΣ|
1−V0/summationtext
pg
|/vectorΣ|+µBBeff/vector ez/summationtext
pg
|/vectorΣ|
1−V0/summationtext
pg
|/vectorΣ|.(82)
Since|/vectorΣ|=|/vectorb(p) +µBBeff/vector ez+V0/vector s|one recognizes the
selfconsistent equation for the mean polarization /vector swhich
in turn determines the local spin precession direction
/vector e. In other words the usual selfconsistency due to the
meanfields is extended towards a scalar density and a
vector polarization yielding the values and the selfcon-
sistent precession direction. The procedure is as follows.
One calculates the density and spin-polarization accord-
ing to (3) where the distributions (75) are dependent on
the vector selfenergy (54) which in turn is again deter-
mined by the density and spin polarization. The scalar
selfenergy we absorb into an effective chemical potential.
This selfconsistent precession direction is solely due to
the momentum dependence of the spin-orbit coupling /vectorb.
Let us inspect all the equations in first order of spin-
orbit coupling. We write /vectorΣ =/vectorΣn+/vectorbpwhere we denote
the momentum-independent selfenergy with /vectorΣn=n/vectorV+
V0/vector s+µB/vectorB. We expand all directions in first order of /vectorb.
The direction of effective polarization becomes
/vector e=/vectorΣ
|Σ|=/vector ez/parenleftbigg
1−b2
⊥
2/parenrightbigg
+/vectorb⊥(1−b3) (83)
where we will use the convenient separation in the z-
direction and the perpendicular direction
/vectorbp
Σn=/vectorb⊥+/vector ezb3. (84)12
The first impression of (83) suggests that one has a
deviation from the z-direction due to the perpendicular
direction/vectorb⊥. Let us calculate the selfconsistency and see
what remains from this deviation. Since the distribution
functions in equilibrium are functions of |/vectorΣ|according to
(75), i.e. a function of b2
⊥andb3, and since the latter
ones are even in the momentum direction, the distribu-
tions are even in the momentum direction. Therefore the
polarization becomes
/vector s=/summationdisplay
pg/vector e=/vector ez/summationdisplay
pg/parenleftbigg
1−b2
⊥
2/parenrightbigg
=/vector ez/parenleftigg
s0−B2
g
2/parenrightigg
(85)
with
s0=/summationdisplay
pg;B2
g=/summationdisplay
pb2
⊥g. (86)
Now the effective precession direction /vector e=/vectorΣ/|/vectorΣ|is seen
to be in the z-direction up to second order in the spin-
orbit coupling in contrast to our first view (83).
It is instructive to calculate the selfconsistent preces-
sion explicitly up to any order now for zero temperature
inquasitwodimensionsandlinearDresselhaus β=βDor
Rashbaβ=βRspin-orbit coupling. We have the density
and the polarization
n=/summationdisplay
pf=me
2π/planckover2pi12(ǫf+ǫβ)
s=/summationdisplay
pg=−me
2π/planckover2pi12/radicalig
ǫβ(ǫβ+2ǫf)+Σ2n(87)
with the spin-orbit energy ǫβ=meβ2. On sees how the
Fermienergy ǫfisshifted bythespin-orbitcoupling. The
effective Zeeman term Σ ndetermines the polarization in
the absence of spin-orbit coupling as s/n=−Σn/ǫf.
Since Σ n=µBBeff+sV0withµBBeff=nV+µBB
we might conclude from the quadratic equation for sin
(87) that the selfconsistent polarization becomes
sself
=me
2π/planckover2pi12meV0
2π/planckover2pi12µBBeff±/radicalig
(µBBeff)2+ǫβ(ǫβ+2ǫf)/parenleftbigmeV0
2π/planckover2pi12/parenrightbig2
1−/parenleftbigmeV0
2π/planckover2pi12/parenrightbig2
(88)
However, this procedure oversees just the selfconsistent
precession/vector e=/vectorΣ/|/vectorΣ|. In fact instead of (87) we have to
calculate the vector quantity
/vector s=/summationdisplay
p/vector eg=∞/integraldisplay
0dpp
(2π/planckover2pi1)22π/integraldisplay
0/vector eg
=/vector ezp2/integraldisplay
p1dpp
4π/planckover2pi12µBBeff+V0sz/radicalbig
β2p2+(µBBeff+V0sz)2
=−/vector ezme
2π/planckover2pi12/parenleftbig
µBBeff+V0sz/parenrightbig
(89)with
p2
1/2
2me=ǫf+ǫβ±/radicalig
ǫβ(2ǫf+ǫβ)+(µBBeff+V0sz)2(90)
originating from the zero-temperature Fermi functions.
We obtainjust theresult(88)but without spin-orbitcou-
plingǫβ→0
/vector sself=−/vector ezme
2π/planckover2pi12nV+µBB
1+meV0
2π/planckover2pi12(91)
which is quite astonishing. Though the selfconsistent
Fermi functions and the selfconsistent precession both
contain an involved spin-orbit coupling separately, they
cancel each other in the polarization in quasi two dimen-
sions and for Rashba or Dresselhaus coupling.
It remains to show that this observation is consistent
with the general expression for the linearized result (85).
With the help of (87) one obtains in fact just (91)
/vector s=/vector ez/parenleftigg/summationdisplay
pg−1
2/summationdisplay
pgb2
⊥/parenrightigg
=−me/vector ez
2π/planckover2pi12/parenleftbig
µBBeff+V0sz/parenrightbig
+o(β3) =−me/vector ez
2π/planckover2pi12nV+µBB
1+meV0
2π/planckover2pi12
(92)
and the effective magnetic field becomes renormalized
µBBeff=nV+µBB→nV+µBB
1+meV0
2π/planckover2pi12(93)
due to selfconsistency. We can conclude that the self-
consistency will determine an effective precession direc-
tiondeviatingfromthedirectionofthe externalmagnetic
field due to the spin-orbit coupling. However this effect
is of higher than second order in spin-orbit coupling /vectorb
and vanishes in quasi two-dimensional systems at zero
temperature and linear spin-orbit coupling.
IV. BALANCE EQUATION
A. Linearization to external electric field
We consider now the linearization of kinetic equation
(62) with respect to an external electric field, no mag-
netic field, and a homogeneous situation. We Fourier
transform the time ∂t→ −iωand the spatial coordi-
nates/vector∂R→i/vector q. The distribution is linearized accord-
ing to ˆρ(pRT) =f(p)+δf(pRT)+/vector σ·[/vector g(p)+δ/vector g(pRT)]
due to the external electric field perturbation eδ/vectorE=
e/vectorE(R,T) =−∇Φ. Further we assume a collision inte-
gral of the relaxation time approximation59
−1
2[ˆτ−1,δˆρl]+ (94)13
with a vector and scalar part of relaxation times ˆ τ−1=
τ−1+/vector σ·/vector τ−1and
τ=τ−1
τ−2−|/vector τ−1|2, /vector τ=−/vector τ−1
τ−2−|/vector τ−1|2.(95)
The scalar relaxation is assumed not towards the ab-
solute equilibrium f0(ǫ± |Σ| −µ) characterized by the
chemical potential µbut towards a local one fl=f0(ǫ±
|Σ|−µ−δµ). The latter one can be specified such
δn=/summationdisplay
p(f−f0) =/summationdisplay
p(f−fl+fl−f0)
=/summationdisplay
p(fl−f0) =∂µnδµ (96)
such that the density is conserved81,82as expressedin the
step to the second line. Therefore the relaxation term
becomes
−δˆρl
τ=−δˆρ
τ+δn
τ∂µn∂µˆρ0. (97)
In this way the density is conserved in the response func-
tion which could be extended to included more conserva-
tion laws85,118. If we consider only density conservation
but no polarization conservation, of course, we can re-
strict ourselves to the ∂µf0terms.
Abbreviating −iω+i/vector p·/vector q/m+τ−1=aandiq∂p/vectorΣ +
/vector τ−1=/vectorb, the coupled kinetic equations (62) take the form
aδf+/vectorbδ/vector g=S0
aδ/vector g+/vectorbδf−2/vectorΣ×δ/vector g=/vectorS (98)
withe/vectorE=−i/vector qΦ and
S0=iq∂pf(Φ+δΣ0)+iq∂p/vector g·δ/vectorΣ+δn
τ∂µn∂µf0
/vectorS=iq∂p/vector g(Φ+δΣ0)+iq∂pfδ/vectorΣ+2(δ/vectorΣ×/vector g)+δn∂µ/vector g
τ∂µn.
(99)
In order to facilitate the vector notation we want to un-
derstandq∂p=/vector q·/vector∂pin the following.
B. Density and spin current
The linearized kinetic equations (98) allow us to write
the balance equations for the magnetization density δ/vector s,
the density δn, and the currents by integrating over the
corresponding moments of momentum
∂tδn+∂Ri/vectorJi+/vector τ−1·δ/vector s= 0
∂tδ/vector s+∂Ri/vectorSi+/vector τ−1δn−2/summationdisplay
p/vectorΣ×δ/vector g= 2δ/vectorΣ×/vector s(100)where we Fourier transformed the wavevector qback to
spatial coordinates R. Exactly the expected density cur-
rents and magnetization currents (78) appear
/vectorJ=/summationdisplay
p/parenleftig
∂pǫpδf+∂p/vectorb·δ/vector g/parenrightig
/vectorSi=/summationdisplay
p/parenleftig
∂piǫpδ/vector g+∂pi/vectorbδf/parenrightig
.(101)
The right hand side of (100) can be reshuffled to the left
sinceδ/vectorΣ =V0δ/vector s+/vectorVδn. Theonlyproblemmakestheterm/summationtext
p/vectorΣ×δ/vector gsince the momentum-dependence of the spin-
orbit coupling prevents the balance equations from being
closed. We need the complete solution of δ/vector gin order to
write the correct balance equation for the magnetization
density. This will be given in the second part of this
paper series.
The method ofmomentsdoes not yield a closedsystem
of equations since the density couples to the currents,
the balance for the currents to the energy currents and
so on. Only with specific approximationsthese equations
can be closed. One can find a great variety of methods in
the literature. Many treatments neglect certain Landau-
liquid parameters119based on the work of120. A more
advancedclosingprocedurewasprovidedby114wherethe
energy dependence of δ/vector swas assumed to be factorized
from space and direction /vector pdependencies.
We will not follow these approximations but solve the
linearized equation exactly in the second part of this pa-
per seriesto providethe solutionofthe balanceequations
and the dispersion exactly. Amazingly this yields quite
involved and extensive structures with many more terms
then usually presented in the literature.
C. Comparison with two-fluid model
We are now in a position to compare the result of mi-
croscopic theory with the two-fluid model (16) and the
form for the direction (26) extracted from general sym-
metric considerations. The first observation is that the
momentum-dependence of the direction /vector edue to, e.g.,
spin-orbit coupling is not covered by the original two-
fluid model. We can, however, redefine certain relaxation
times to account for these effects as we did in (25). The
priceto pay wasthat one hasto considera third equation
forthe precessiondirection. The undetermined constants
in (26) are now derived to be
/vectorh= 2δ/vectorΣ, d=−2iΣ, d 1=c= 0 (102)
which one can see from decomposing (98) and (99) into
equations for δf,δgandδ/vector eand compare with (23) and
(26).
The problem with the two-fluid model becomes appar-
ent if we try to extract the values for the meanfields (19).
One obtains the unique identification
V1δn+V3δs=δΣ0 (103)14
and two different forms from the δfand theδgequation
/vector e·q∂p/vectorΣδg+η=q∂pg(V2δn+V4δs−/vector e·δ/vectorΣ)
/vector e·q∂p/vectorΣδf=q∂pf(V2δn+V4δs−/vector e·δ/vectorΣ)(104)
withη= (Σδ/vector e−δ/vectorΣ)q∂p/vector eg≈0. One sees that we have
two determining equations which are consistent only if
δf/q∂pf=δg/q∂pgwhich is not ensured in general.
Therefore the mapping of the momentum-dependent
spin-orbit coupling terms to a two-fluid model is not pos-
sible in general. Only if we approximate the momentum-
dependence of /vectorΣ by a constant direction /vector e(p)≈/vector edo we
have the two unique equations (103) and
V2δn+V4δs=/vector e·δ/vectorΣ. (105)
For illustration we decompose the change of precession
directionintothe componentsproportionaltothe density
and polarization change δ/vector e=/vector e1δn+/vector e2δsand obtain in
this way
V1=V0+/vectorV·/vector e, V 2=/vector e·/vectorV+V0/vector e·/vector e1,
V4=V0+V0/vector e·/vector e2, V 3=/vector e·/vectorV+/vectorV·/vector e2(106)
which provides indeed four different meanfield potentials
(19) which in turn can be translated into the original Uij
potentials. In the case that U↑↓=U↓↑we must have
V0/vector e·/vector e1=/vectorV·/vector e2.
V. SPIN-HALL AND ANOMALOUS HALL
EFFECT
A. Homogeneous situation without magnetic field
It is interesting to note that the coupled kinetic equa-
tion (62) allowsforafinite conductivityevenwithout col-
lisions and a Hall effect without external magnetic field.
This is due to the interference between the two-fold split-
ting of the band and will be the reason for the anomalous
Hall effect. We haveseenalreadyanexpressionofthis in-
terference by the two compensating currents, the normal
and anomalous ones, in Sec. IIIG.
For a homogeneous system neglecting magnetic fields
we have from (62)
(∂t+eE∂p)f= 0
(∂t+eE∂p)/vector g= 2(/vectorΣ×/vector g). (107)
Due to the spin-precession term a nontrivial solution for
the polarization part /vector ρof the distribution appears. We
will solve these coupled equations in the following by two
ways, once in the helicity basis16and once directly in the
spin basis. In order to gain trust in the result we then
compare the expressions with the Kubo formula.
With the help of an effective Hamiltonian
H=ǫ+/vector σ×/vectorΣ (108)withǫ=p2
2m+ Σ0+eΦ and the spin-orbit coupling as
well as the meanfield by magnetic impurities summarized
in/vectorΣ, one can rewrite both coupled kinetic equation ˆ¯ρ=
ρ+/vector σ×/vector ρinto
(∂t+eE∂p)ˆ¯ρ+i[H,ˆ¯ρ]−= 0. (109)
B. Helicity basis
Now we go into the helicity basis which means we use
the eigenstates
H|±/an}b∇acket∇i}ht=ǫ±|±/an}b∇acket∇i}ht (110)
and using the convenient notation
Σx−iΣy= Σe−iϕ:|Σ|=/radicalig
Σ2x+Σ2y+Σ2z(111)
we have
ǫ±=ǫ±|Σ|
|Σ|2= Σ2+Σ2
z
|±/an}b∇acket∇i}ht=1/radicalbig
2|Σ|/parenleftigg
−e−iϕ/radicalbig
|Σ|±Σz
∓/radicalbig
|Σ|∓Σz/parenrightigg
.(112)
The transformation matrix is U= (|+/an}b∇acket∇i}ht,|−/an}b∇acket∇i}ht) and the
Hamiltonian becomes diagonal
¯H=U+HU=/parenleftigg
ǫ+0
0ǫ−/parenrightigg
(113)
and since the transformed spin-projection operators read
¯P+=/parenleftigg
1 0
0 0/parenrightigg
,¯P−=/parenleftigg
0 0
0 1/parenrightigg
(114)
the equilibrium distribution (75) becomes diagonal
ˆ¯ρ=/summationdisplay
i=±ˆPifi=/parenleftigg
f+0
0f−/parenrightigg
(115)
or in general
ˆ¯ρ= ¯ρ+/vector¯ρ·U+/vector σU. (116)
The Pauli matrices transformed in the helicity basis can
be written with the notation (111) aslinearcombinations
of Pauli matrices
¯σx=1
|Σ|/parenleftigg
Σcosϕ −i|Σ|sinϕ−Σzcosϕ
i|Σ|sinϕ−Σzcosϕ −Σcosϕ/parenrightigg
=−Σz
|Σ|cosϕσx+sinϕσy+Σ
|Σ|cosϕσz
¯σy=i
|Σ|/parenleftigg
−iΣsinϕ i Σzsinϕ+|Σ|cosϕ
iΣzsinϕ−|Σ|cosϕ i Σsinϕ/parenrightigg
=−Σz
|Σ|sinϕσx−cosϕσy+Σ
|Σ|sinϕσz
¯σz=1
|Σ|/parenleftigg
ΣzΣ
Σ−Σz/parenrightigg
=Σ
|Σ|σx+Σz
|Σ|σz. (117)15
This allows us to transform the velocity operator in the
helicity basis
¯ˆvi=∂iǫ+
/parenleftig
Σ2
|Σ|∂iΣz
Σ/parenrightig
−Σ∂iϕ
∂i|Σ|
·/vector σ (118)
where∂idenotes the derivative with respect to the i-th
component of the momentum. The current would be
Ji=e
2Tr[¯ˆviδ¯ρ] (119)
where we need the linearized solution of (109) in the he-
licity basis with respect to an external electric field. Em-
ploying (∂U+)U=−U+∂Uone transforms
U+(∂f)U=∂¯f+[U+∂U,¯f]− (120)
such that the kinetic equation (109) reads
∂t¯ρ+[U+∂tU,¯ρ]−+e/vectorE·/vector∂p¯ρ+e/vectorE·[U+/vector∂pU,¯ρ]−
+i[¯H,¯ρ]−= 0.(121)
The correspondinglinearizedkinetic equation ¯ ρ= ¯ρ0+δ¯ρ
takes the same form
∂tδ¯ρ+[U+∂tδU,¯ρ0]−+e/vectorE·/vector∂p¯ρ0+e/vectorE·[U+/vector∂pU,¯ρ0]−
+i[¯H,δ¯ρ]−= 0. (122)
For further use we neglect the time-dependence ∂tδUdue
to selfconsistent mean field in the basis. The selfconsis-
tently induced meanfield term [ δ¯H,¯ρ0] can be considered
more convenient in the next paragraph in spinor repre-
sentation by the solution in the spin basis in the next
part of this series.
With the help of the diagonal Hamiltonian (113) one
has for any matrix A={aij}
/bracketleftigg/parenleftigg
ǫ+0
0ǫ−/parenrightigg
,A/bracketrightigg
= (ǫ+−ǫ−)/parenleftigg
0a12
−a210/parenrightigg
=1
2(ǫ+−ǫ−)[σz,A] (123)
such that we can write (122) with the equilibrium distri-
bution (116)
∂tδ¯ρ+e/vectorE·/vector∂p¯ρ0+1
2(f+−f−)e/vectorE·[U+/vector∂pU,σz]−
−i
2(ǫ+−ǫ−)[δ¯ρ,σz]−= 0. (124)
Consequently, the first part describes the diagonal re-
sponse and the second part the response due to off-
diagonal or band interference. The solution reads ex-
plicitly
δ¯ρ=−ie/vectorE·/parenleftigg/vector∂pf+
ω2g
∆ǫ−ω/an}b∇acketle{t+|/vector∂p|−/an}b∇acket∇i}ht
2g
∆ǫ+ω/an}b∇acketle{t−|/vector∂p|+/an}b∇acket∇i}ht/vector∂pf−
ω/parenrightigg
(125)with2g=f+−f−and∆ǫ=ǫ+−ǫ−= 2|Σ|. Thediagonal
part leads to the standard dynamical Drude conductivity
if a scattering with impurities is considered ω→ω+i/τ.
The second part is the reason for the anomalous Hall
effect which we consider in the following.
With the help of (112) one has explicitly
/an}b∇acketle{t±|∂|∓/an}b∇acket∇i}ht=−iΣ
2|Σ|∂ϕ∓Σ2
2|Σ|2∂/parenleftbiggΣz
Σ/parenrightbigg
/an}b∇acketle{t±|∂|±/an}b∇acket∇i}ht=−i|Σ|±Σz
2|Σ|∂ϕ (126)
and the off-diagonal parts of (125) can be expressed as
δ¯ρAH=Σ
|Σ|ge/vectorE·
ω2−(∆ǫ)2/bracketleftbigg
∆ǫ/parenleftbigg
/vector∂pϕσx+Σ
|Σ|/vector∂p/parenleftbiggΣz
Σ/parenrightbigg
σy/parenrightbigg
+iω/parenleftbigg
/vector∂pϕσy−Σ
|Σ|/vector∂p/parenleftbiggΣz
Σ/parenrightbigg
σx/parenrightbigg/bracketrightbigg
.
(127)
The current (119) reads then
Jα=σαβEβ (128)
with the two parts of conductivity
σαβ=e2
2/summationdisplay
pΣ2
|Σ|2g
ω2−4|Σ|2
×/bracketleftbigg
2Σ/parenleftbigg
∂βϕ∂α/parenleftbiggΣz
Σ/parenrightbigg
−∂αϕ∂β/parenleftbiggΣz
Σ/parenrightbigg/parenrightbigg
−iω/parenleftbigg
∂βϕ∂αϕ+Σ2
|Σ|2∂β/parenleftbiggΣz
Σ/parenrightbigg
∂α/parenleftbiggΣz
Σ/parenrightbigg/parenrightbigg/bracketrightbigg
.(129)
1. Dynamical asymmetric part
The first part of (129) is the standard anomalous Hall
effect since it represents an asymmetric matrix noting
∂αa∂βb−∂βa∂αb=ǫαβγ(/vector∂a×/vector∂b)γ.(130)
To simplify this asymmetric part further we perform the
derivatives explicitly
/vector∂/parenleftbiggΣz
Σ/parenrightbigg
×/vector∂ϕ=−1
Σ3ǫijkΣi/vector∂Σj×/vector∂Σk(131)
and the first asymmetric part of (129) can be written
σas
αβ=e2
2/summationdisplay
pg
1−ω2
4|Σ|2/vector e·(∂α/vector e×∂β/vector e) (132)
with/vector e=/vectorΣ/|Σ|. This describes the dynamical anomalous
Hallconductivityaswecanverifybythecomparisonwith
the dc Hall conductivity from the Kubo formula in the
next section.16
2. Dynamical symmetric part
The second symmetric part of (129) is a pure dynami-
cal conductivity and can be rewritten in a compact form
as well by noting
∂βϕ∂αϕ+Σ2
|Σ|2∂β/parenleftbiggΣz
Σ/parenrightbigg
∂α/parenleftbiggΣz
Σ/parenrightbigg
=/parenleftig
∂α/vectorΣ·∂β/vectorΣ−∂α|Σ|∂β|Σ|/parenrightig1
Σ2
= (∂α/vector e·∂β/vector e)|Σ|2
Σ2(133)
with/vector e=/vectorΣ/|/vectorΣ|. Therefore we obtain
σsym
αβ=ie2
2/summationdisplay
pω
2|Σ|g
1−ω2
4|Σ|2∂α/vector e·∂β/vector e. (134)
C. Anomalous Hall conductivity from Kubo
formula
For the reason of comparison we re-derive this results
from the Kubo formula and consider the dc limit of the
interband conductivity with band energies ǫn(p) and oc-
cupationsfn(p). Due to band polarizations one has a
finite current. The Kubo-Bastin-Streda formula reads
(/summationtextfn=nn)
σαβ=e2/planckover2pi1
i/summationdisplay
nm/summationdisplay
pfm−fn
(ǫn−ǫm)2vα
nmvβ
mn(135)
with the velocity in band basis
/vector vnm=/an}b∇acketle{tn|ˆ/vector v|m/an}b∇acket∇i}ht=1
i/planckover2pi1/an}b∇acketle{tn|[ˆ/vector x,ˆH]|m/an}b∇acket∇i}ht=/an}b∇acketle{tn|[/vector∂p,ˆH]|m/an}b∇acket∇i}ht
=/an}b∇acketle{tn|/vector∂p|m/an}b∇acket∇i}ht(ǫm−ǫn). (136)
The conductivity becomes therefore with the notation
(/vector∂p)α=∂α
σαβ=−e2/planckover2pi1
i/summationdisplay
nm/summationdisplay
p(fm−fn)/an}b∇acketle{tn|∂α|m/an}b∇acket∇i}ht/an}b∇acketle{tm|∂β|n/an}b∇acket∇i}ht
=e2/planckover2pi1
i/summationdisplay
n/summationdisplay
pfn/an}b∇acketle{tn|∂α∂β−∂β∂α|n/an}b∇acket∇i}ht
=ǫαβγe2/planckover2pi1
i/summationdisplay
n/summationdisplay
pfn/an}b∇acketle{tn|(/vector∂p×/vector∂p)γ|n/an}b∇acket∇i}ht
=ǫαβγe2/planckover2pi1
i/summationdisplay
n/summationdisplay
pfn(/vector∂p×/an}b∇acketle{tn|/vector∂p|n/an}b∇acket∇i}ht)γ
=−ǫαβγe2/summationdisplay
n/summationdisplay
pfn(/vector∂p×/vector an)γ (137)
whereweintroducedin thelaststep theBerry-phasecon-
nection
/vector an=i/planckover2pi1/an}b∇acketle{tn|/vector∂p|n/an}b∇acket∇i}ht=/an}b∇acketle{tn|/vector x|n/an}b∇acket∇i}ht (138)and/vector∂×/vector anis the Berry-phase curvature.
Now we specify this formula for the two-spin band
problem where the Berry phase connection with the help
of (126) reads
/vector a±=i/planckover2pi1/an}b∇acketle{t±|/vector∂p|±/an}b∇acket∇i}ht=/planckover2pi1Σ±Σz
2Σ/vector∂pϕ (139)
and the Berry curvature
/vector∂p×/vector a±=∓/planckover2pi1
2Σ3ǫijkΣi/vector∂pΣj×/vector∂pΣk(140)
or
(/vector∂p×/vector a±)γ=∓/planckover2pi1
2Σ3ǫαβγǫijkΣi∂αΣj∂βΣk
=∓/planckover2pi1
2Σ3ǫαβγ/vectorΣ·(∂α/vectorΣ×∂β/vectorΣ).(141)
Therefore the dc Hall conductivity reads finally
σdc
αβ=e2/planckover2pi1
2/summationdisplay
pg /vector e·(∂α/vector e×∂β/vector e) (142)
which is exactly the dc limit of (132).
D. Spin-Hall and anomalous Hall effect in spin
basis
1. Anomalous and inverse Hall effect
Now we solve the equations (107) once more directly
in the spin basis. This has the advantage that the am-
biguousterm U+∂tUin the helicitybasisdoesnotappear
and in this way we will see that it does not contribute to
the final result. Moreover we have the relaxation time in
the kinetic equation which means that in the end we can
understand ω→ω+i/τ. In ordertokeepthe comparison
as near as possible to the above two ways of derivation
we keepωand shift in the end.
Equations (107) are decoupled since we neglect mean-
field effects and magnetic fields. Linearizing and noting
that/vectorΣ×/vector g= 0 since/vector g=/vector e(f+−f−)/2 we obtain after
the Fourier transform of time
δf(ω,p) =−i
ωeE∂pf
δ/vector g(ω,p) =iω
4|Σ|2−ω2eE∂p/vector g
−4i1
ω(4|Σ|2−ω2)/vectorΣ(/vectorΣ·eE∂p/vector g)
−21
4|Σ|2−ω2/vectorΣ×eE∂p/vector g. (143)
With the help of
1
4|Σ|2−ω2
−iω
4i|Σ|2
ω
2|Σ|
=∞/integraldisplay
0eiωt
cos2|Σ|t
1−cos2|Σ|t
sin2|Σt|
,(144)17
one sees that each of the terms in (143) correspond to
a specific precession motion analogously to the one seen
in the conductivity of a charge in crossed electric and
magnetic fields
/vectorJ(t) =σ0t/integraldisplay
0d¯t
τe−¯t
τ/braceleftig
cos(ωc¯t)/vectorE(t−¯t)
+sin(ωc¯t)/vectorE(t−¯t)×/vectorB0+[1−cos(ωc¯t)][/vectorE(t−¯t)·/vectorB0]/vectorB0/bracerightig
(145)
as the solution of the Newton equation of motion
me˙/vector v=e(/vector v×/vectorB)+e/vectorE−me/vector v
τ. (146)
It illustrates the threefold orbiting of the electrons with
cyclotron frequency: (i) in the direction of the electric
and (ii) magnetic field, and (iii) in the direction perpen-
dicular to the magnetic and electric field.
The chargecurrent (78) or (101) consists of the normal
current as the first part,
e/summationdisplay
p∂αǫδf=ine2
ω+Eα=ine2τ
1−iωτEα(147)
and the anomalous current due to spin-polarization as
the second part of (101). The latter one contains the
standard anomalous Hall effect as the third term of (143)
and their first and second term will combine together to
the symmetric part of the anomalous conductivity as we
will demonstrate now. Since /vectorΣ·∂/vector e= 0, the third term
of (143) leads to
σas
αβ=−e2/summationdisplay
p∂α/vectorΣ(/vectorΣ×∂β/vector e)f+−f−
4|Σ|2−ω2
=−e2
2/summationdisplay
kpg
1−ω2
4|Σ|2∂α/vector e(/vector e×∂β/vector e) (148)
and one recognizes the anomalous Hall conductivity
(132).
The first and second term of (143) combine together
with the symmetric part
σsym
αβ=ie2
2ω/summationdisplay
p2∂α/vectorΣ
4|Σ|2−ω2/bracketleftbigg
ω2(g∂β/vector e+/vector e∂βg)−4/vectorΣ|Σ|∂βg/bracketrightbigg
=ie2
2ω/summationdisplay
p2
4|Σ|2−ω2/bracketleftbiggω2g
|Σ|(∂α/vectorΣ∂β/vectorΣ−∂α|Σ|∂β|Σ|)
+ω2∂α|Σ|∂βg−4|Σ|2∂α|Σ|∂βg/bracketrightbigg
=iωe2
4/summationdisplay
pg
1−ω2
4|Σ|21
|Σ|3/parenleftbigg
∂α/vectorΣ∂β/vectorΣ−∂α|Σ|∂β|Σ|/parenrightbigg
+ie2
ω/summationdisplay
pg∂α∂β|Σ| (149)where we have used in the second step the relation
∂α/vectorΣ∂β/vectorΣ
|Σ|=1
|Σ|/parenleftbigg
∂α/vectorΣ∂β/vectorΣ−∂α|Σ|∂β|Σ|/parenrightbigg
=|Σ|∂α/vector e·∂β/vector e.
(150)
Since the last term in (149) vanishes due to symmetry in
pwe obtain exactly (134).
Summarizing, the total charge current (101) is given
by
Jα=σDEα+(σas
αβ+σsym
αβ)Eβ (151)
with the usual Drude conductivity σD=ne2τ/meand
the symmetric and asymmetric parts of the anomalous
Hall conductivity (132) and (134)
σas
αβ
σsym
αβ
=e2
2/summationdisplay
pg
1−ω2
4|Σ|2
/vector e·(∂α/vector e×∂β/vector e)
iω
2|Σ|∂α/vector e·∂β/vector e(152)
and/vector e=/vectorΣ/|Σ|. Note that from our kinetic equation
with the relaxation time approximation we understand
the above formulas as ω→ω+i/τwhich leads in the
static limit the modifications of the Kubo expression due
to collisions.
ForzerotemperatureandlinearRashbaspin-orbitcou-
pling we can integrate these expressions analytically. We
consider the electric field in x-direction and obtain
σas
yx=e2
4π/planckover2pi1Σnτωarctan/bracketleftbigg2ǫβτω
/planckover2pi12+4(2ǫβǫF+Σ2n)τ2ω/bracketrightbigg
→e2
4π/planckover2pi1
ǫβΣn
2ǫβǫf+Σ2nω= 0,τ→ ∞
Σn
ωartanh/bracketleftig
2ǫβω
/planckover2pi12ω2−4(2ǫβǫF+Σ2n)/bracketrightig
ω/ne}ationslash= 0,τ→ ∞
(153)
with the Rashba energy ǫβ=mβ2
R//planckover2pi1and the dynamical
result is given τω=τ/(1−iωτ) in (153). We see that the
anomalous Hall effect vanishes with vanishing effective
Zeeman field
Σn=|n/vectorV+/vector sV0+µB/vectorB|. (154)
We see from figure 2 that the anomalous Hall conduc-
tivity is strongly dependent on the frequency showing
even a sign change at high frequencies which had been
reported before121. This sign change is connected with a
collisional damping which means that it is suppressed by
collisions. This damping as expressed by the imaginary
part of the conductivity vanishes in the static limit.
The absolute value is dependent on the effective Zee-
man field (154) as one sees from the scaling of the static
limit plotted in figure 3. The static anomalous Hall con-
ductivity possesses a maximum at certain Zeeman terms
which are dependent on the relaxation time.18
02468100.0000.0050.0100.0150.0200.025
Ω/LBracket1ΕF/RBracket1Σyxas/LBracket1e/Slash18Π/HBar/RBracket1
/CaΠSigman/Equal1ΕF/CaΠSigman/Equal0.5ΕF/CaΠSigman/Equal0ΕF
FIG. 2: The dynamical anomalous Hall conductivity (153)
vs. frequency for different values of the effective Zeeman fiel d
(154) and a relaxation time τ= 0.3/planckover2pi1ǫFand a Rashba energy
ofmβ2
R= 0.1ǫF. Real parts are thick and imaginary are thin
lines.
0.00.51.01.52.02.53.00.000.020.040.060.080.10
/CaΠSigma/LBracket1ΕF/RBracket1Σxxsym,Σyxas/LBracket1e/Slash18Π/HBar/RBracket1
Τ/Equal3/HBar/Slash1ΕFΤ/Equal1/HBar/Slash1ΕF
FIG. 3: The static anomalous Hall conductivity of (153)
(thick) and inverse Hall conductivity (155) (thin) vs. effec tive
Zeeman field for two different relaxation times and a Rashba
energy of mβ2
R= 0.1ǫF.
The symmetric part of (152) in fact yields σsym
yx= 0
and
σsym
xx=e2
16π/planckover2pi1/braceleftbigg4ǫβΣ2
nτω
2ǫβǫf+Σ2n
+ (1−4Σ2
nτ2
ω)arctan/bracketleftbigg4ǫβτω
/planckover2pi12+4(2ǫβǫF+Σ2n)τ2ω/bracketrightbigg/bracerightbigg
→e2
4π/planckover2pi1/braceleftigg
0ω= 0,τ→ ∞
imaginary ω/ne}ationslash= 0,τ→ ∞(155)
which shows that it represents a contribution in the di-
rection of the applied electric field and is caused by col-
lisional correlations. We interpret it as an inverse Hall
effect. This dynamical result is different from the spin
accumulation found in122basically by the arctanterm
and therefore no sharp resonance feature. Expanding,
however, in small spin-orbit coupling
σsym
xx=e2
2π/planckover2pi1ǫβτ
1+4Σ2nτ2+o(ǫ2
β) (156)0 510 150.000.010.020.03
Ω/LBracket1ΕF/RBracket1Σxxsym,Σyxas/LBracket1e/Slash18Π/HBar/RBracket1
ΣxxsymΣyxas
FIG. 4: The comparison of the dynamical anomalous Hall
conductivity (153) (solid) and the inverse Hall conductivi ty
(155) (dashed) for a relaxation time τ= 0.3/planckover2pi1ǫF, a Rashba
energy of mβ2
R= 0.1ǫFand an effective Zeeman energy Σ n=
1ǫF. The real parts are thick lines, and the imaginary parts
are thin lines.
showsthat the static limit agreeswith122,123. Pleasenote
that if one sets Σ n→0 before expanding a factor 1/2
appears which illustrates the symmetry breaking by the
effective Zeeman term.
In figure3we comparethis expressionwith the anoma-
lous Hall conductivity for two different relaxation times.
While the static anomalous Hall conductivity vanishes
with the effective Zeeman field the inverse Hall effect re-
mains finite which value is easily seen from (155). Both
the anomalous Hall conductivity as well as the inverse
Hall conductivity possess a maximum at certain effective
Zeeman fields.
The comparison of the dynamical anomalous Hall ef-
fect and the inverse Hall effect finally can be found in
figure 4. In contrast to the anomalous Hall effect the
inverse Hall effect does not show a sign change which
means the current remains in the direction of the applied
electric field as it should.
2. Spin-Hall effect
Now we can consider the spin current (101) with the
help of the long-wavelength solution (143) without mag-
netic fields. The part with δfvanishes after partial inte-
grationand symmetry in p. The other terms groupinto a
normal spin-current and an (anomalous) part represent-
ing the spin-Hall effect
/vectorSα=−eτ
me(1−iωτ)/vector sEα+/vector σαβEβ.(157)
The spin-Hall coefficient consists analogously as the
anomalous Hall effect of a symmetric and an asymmetric
part (ω→ω+i/τ)
/vector σas
αβ
/vector σsym
αβ
=e
meω/summationdisplay
ppαg
1−ω2
4|Σ|2
iω
2|Σ|/vector e×∂β/vector e
i∂β/vector e.(158)19
We see that both effects the spin-Hall effect and the
anomalous Hall effect appear without magnetic fields
and have their origin in the anomalous parts of the cur-
rents due to spin-orbit coupling. Though the normal and
anomalous currents exactly compensate in the station-
ary state, the current due to a disturbing external elec-
tric field shows a finite asymmetric and symmetric part
(158) not known in the literature.
Explicit integration of (158) is possible to carry out
in zero temperature and linear Rashba and Dresselhaus
coupling. We assume the electric field in the x-axis and
we get for the Rashba linear spin-orbit coupling
σz
yx=e
8π/planckover2pi1/bracketleftbigg
1−1+4Σ2
nτ2
ω
4ǫβτωarctan/parenleftbigg4/planckover2pi1ǫβτω
/planckover2pi12+4τ2ω(2ǫβǫF+Σ2n)/parenrightbigg/bracketrightbigg
(159)
withτω=τ/(1−iωτ). Only the z-axis survives in linear
spin-orbit coupling. Neglecting the selfenergy and using
the static limit it is just the result of6,124.
The so-called universal limit appears if one takes the
limit of vanishing collision frequency
σz
yx=e
8π/planckover2pi12ǫβǫf
2ǫβǫf+Σ2n+o(1/τ). (160)
We see how the selfenergy including the Zeeman term
(154) modifies this ”universal limit” which already hints
at questioning of this notion.
For the Dresselhaus linear spin-orbit coupling we ob-
tain just (159) with opposite sign. Therefore if we ap-
proximate the combined effect by adding the two specific
results we see that the constant term vanishes and the
difference of the expressions with corresponding Rashba
and Dresselhaus energies occur. The correct treatment
of both couplings together leads to involved angular in-
tegrations and escape analytical work.
The universal constant e/8π/planckover2pi1has been first de-
scribed by125and raised an intensive discussion. It
was shown that the vertex corrections cancel this
constant126,127. A suppression of Rashba spin-orbit cou-
pling has been obtained due to disorder128, or electron-
electron interaction129and found to disappearin the self-
consistent Born approximation38. The conclusion was
thatthetwodimensionalRashbaspin-orbitcouplingdoes
not lead to a spin-Hall effect as soon as there are re-
laxation mechanisms present which damp the spins to-
wards a constant value. In order to include such effects
one has to go beyond meanfield and relaxation-time ap-
proximation by including vertex corrections86. The spin-
Hall effect does not vanish with magnetic fields or spin-
dependent scattering processes6.
Please note that the universal constant in (159) is nec-
essary to obtain the correct small spin-orbit coupling re-
sult
σz
yx=e
π/planckover2pi1ǫfτ2
(1−iωτ)2+4Σ2nτ2ǫβ+o(ǫ2
β).(161)
Without the Zeeman term Σ n→0 and for small spin-
orbit coupling this agrees with the dynamical result of12202468100.000.020.040.06
Ω/LBracket1ΕF/RBracket1Σyxz/LBracket1e/Slash18Π/HBar/RBracket1
/CaΠSigman/Equal1ΕF/CaΠSigman/Equal0.5ΕF/CaΠSigman/Equal0ΕF
FIG. 5: The dynamical spin-Hall coefficient vs frequency for
different values of the effective Zeeman field and a relaxation
timeτ= 0.3/planckover2pi1ǫFand a Rashba energy of mβ2
R= 0.1ǫF, real
parts are shown as thick and imaginary parts as thin lines.
where the definition of spin current has been employed in
terms of physical argumentation. Again the result here
differs from the resonant structure found in122by the
arctanterm but the static limit agrees with the result
of6,124.
The dynamical result (159) describes the influence of
anexternalmagneticfieldaswellasmeanmagnetizations
due to magnetic impurities. The advantage of the result
here is the simplicity in which the frequency dependence
enters and the combined effect of external magnetic field,
spin polarizations and mean magnetization described by
one vector selfenergy (54) called the effective Zeeman
field.
The z-component of the spin-Hall coupling in the x-
direction becomes a modified coefficient (159)
σz
xx=2
/planckover2pi1Σnτσz
xy. (162)
The medium effects or magnetic field or magnetization
condensed in (54) triggers a second spin-Hall direction in
plane with the z-axes and the electric field. This obser-
vation is interpreted as the inverse spin-Hall effect. The
herepresentedinversespin-Halleffectsaretheunderlying
physics in the recently observed terahertz spin signals130
in magnetic heterostructures.
In figure 5 we plot the dynamical spin-Hall coefficients
for different effective Zeeman fields. The coefficients be-
comes suppressed with increasing Zeeman field as seen
also in figure 6 and with larger scattering frequency 1 /τ.
Interestingly the real part of the spin-Hall conductivity
shows a sign change at a specific frequency. Though
this effect is interesting this reversed current is strongly
damped represented by the imaginary part.
The static limit becomes suppressed as seen in Fig. 6
dependent on the relaxation time and the effective Zee-
man field. The in-plane component (162) is zero for the
absent Zeeman term and shows a characteristic maxi-
mum at certain effective Zeeman fields.
The dynamical spin Hall coefficient and the inverse20
0.00.51.01.52.00.00.20.40.60.81.01.21.4
/CaΠSigma/LBracket1ΕF/RBracket1Σxxz,Σyxz/LBracket1e/Slash18Π/HBar/RBracket1
Τ/Equal3/HBar/Slash1ΕFΤ/Equal1/HBar/Slash1ΕF
FIG. 6: The static spin-Hall coefficients of (159) (thick) and
(162) (thin) effective Zeeman field for two different relaxati on
times and a Rashba energy of mβ2
R= 0.1ǫF.
0246810/MinuΣ0.010.000.010.020.030.040.05
Ω/LBracket1ΕF/RBracket1Σxxz,Σyxz/LBracket1e/Slash18Π/HBar/RBracket1
ΣxxzΣyxz
FIG. 7: The comparison of the dynamical spin-Hall coeffi-
cients (159) (solid) and the inverse spin-Hall coefficient (1 62)
(dashed) for a relaxation time τ= 0.3/planckover2pi1ǫF, a Rashba energy
ofmβ2
R= 0.1ǫFand an effective Zeeman energy Σ n= 1ǫF.
spin Hall coefficient are compared in figure 7. We recog-
nize a sign change at higher frequencies connected with a
strongdampingforbotheffects. Comparedtothe inverse
Hall effect the inverse spin-Hall current can be directed
both parallel and anti-parallel to the electric field.
It is important to note that the here presented lin-
earized mean-field kinetic equation with a relaxation-
time approximation is not capable to describe correctly
the collisional correlationswhich has to be performed be-
yond the relaxation-time approximation. Especially the
above-mentioned vertex corrections seem to lead to can-
cellations of the result. Here we restrict ourselves to a
Drude level of conductivity.
VI. SUMMARY
The coupled kinetic equation for particle and spin po-
larization is derived including meanfields, spin-orbit cou-
pling and arbitrary magnetic and electric field strength.This is achieved by using a gauge-invariant formulation
and keeping the quantum spin structure as commuta-
tors/anticommutators through gradient approximations.
Bothequationshavetheexpectedstructureofadriftcon-
trolled by a mean quasiparticle velocity renormalized by
meanfields and the effective Lorentz force which contains
besidesthemagneticfieldalsothe vectorpartsoftheself-
energy. These equations arecoupled exactly by the latter
one. Additionally the polarization distribution exercises
a precession around a direction given by this vector self-
energy. This latter one together with the magnetic field
establishesan effective medium-dependent magnetic field
and can be considered as a many-body extension of the
Zeeman field. The stationary solution shows a unique
splitting into two bands controlled by the vector selfen-
ergy.
Here the selfconsistent precession direction appears.
For linear spin-orbit coupling and zero temperature an
exact cancellation of spin-orbit coupling is found for the
polarization.
We have calculated charge and spin currents and show
that besides the regular currents an anomalous part ap-
pearsduetospin-orbitcoupling. Theregularandanoma-
lous currents compensate exactly in the stationary state.
For transport with respect to an external electric field we
calculate the spin-Hall coefficient as well as the anoma-
lous Hall conductivity. Both consist of an asymmetric
part which in the case of the anomalousHall effect agrees
with the standard one from the Kubo formula or Berry
phases and an additional symmetric part interpreted as
the inverse Hall effect with an expression not presented
so far. The corresponding spin-Hall effects are described
as well and are presented here in their dynamical form
dependent on the magnetic field and the mean magneti-
zation of the system.
A sign change of the Hall conductivity is reported for
higher frequencies than a critical one given in terms of
the relaxation time. The inverse Hall effect does not
show such sign change in accordance with causality. The
spin-Hall and inverse spin-Hall effects both show such
sign change where the latter one is an expression of the
non-conserved spin current.
In the second part of this paper series we will present
the linear response results including the meanfield and
magnetic field which allows us to discuss the dynami-
cal response functions. From this we will see the collec-
tivemodesandhowthe spin-orbitcouplinginfluences the
screening properties.
Acknowledgments
Discussions with Janik Kailasvuori, Alvaro Ferraz and
OzgurBozataregratefullymentioned. Financialsupport
by the Brazilian Ministry of Science and Technology is
acknowledged.21
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1407.3446v1.Orbital_angular_momentum_driven_intrinsic_spin_Hall_effect.pdf | arXiv:1407.3446v1 [cond-mat.mes-hall] 13 Jul 2014Orbital angular momentum driven intrinsic spin Hall effect
Wonsig Jung,1Dongwook Go,2Hyun-Woo Lee,2,∗and Changyoung Kim1,†
1Institute of Physics and Applied Physics, Yonsei Universit y, Seoul 120-749, Korea
2Department of Physics, Pohang University of Science and Tec hnology, Pohang 790-784, Korea
(Dated: June 19, 2021)
We propose a mechanism of intrinsic spin Hall effect (SHE). In this mechanism, local orbital
angular momentum (OAM) induces electron position shift and couples with the bias electric field
to generate orbital Hall effect (OHE). SHE then emerges as a co ncomitant effect of OHE through
the atomic spin-orbit coupling. Spin Hall conductivity due to this mechanism is estimated to be
comparable to experimental values for heavy metals. This me chanism predicts the sign change of the
spin Hall conductivity as the spin-orbit polarization chan ges its sign, and also correlation between
the spin Hall conductivity and the splitting of the Rashba-t ype spin splitting at surfaces.
PACS numbers: 74.25.Jb,74.70.Xa,78.70.Dm
Spin Hall effect (SHE) [1] is a phenomenon in which
electrons with opposite spins are deflected in opposite
side ways. Its first experimental confirmation [2] was
achieved for n-doped GaAs and very small spin Hall con-
ductivity σSH∼1 Ω−1m−1was obtained, which was at-
tributed [3] to the extrinsic mechanisms [4] of SHE such
as skew scattering and side jump. For some heavy met-
als, on the other hand, much larger σSHwas reported [5].
For Pt, for instance, reported values range from 2 .4×104
Ω−1m−1[6] to 5.1×105Ω−1m−1[7]. Such large σSH
raises hope for device applications of SHE. The current-
induced magnetization switching observed in Ta/CoFeB
magnetic bilayer [8] is attributed to the large SHE in
Ta, which injects strong spin Hall current into CoFeB to
switch its magnetization direction.
LargeσSHis often attributed to intrinsic mecha-
nisms [9–16] of SHE, which do not resort to impurity
scattering. Their exact nature remains unclear however.
In one mechanism [12], a small spin-orbit energy gap
near the Fermi energy resonantly enhances the momen-
tumspaceBerryphaseeffecttoproduceastrongeffective
magnetic field in momentum space and σSH= 104∼105
Ω−1m−1is predicted for Pt. In another mechanism [13–
16], the orbital angular momentum (OAM) of atomic
orbitals generates the Aharonov-Bohm phase and pro-
duces a spin-dependent effective magnetic field in real
space. For various heavy metals with strong atomic
spin-orbit (SO) coupling, resulting σSHis estimated to
104∼105Ω−1m−1and predicted to exhibit a systematic
sign changeamongmaterialswith different spin-orbit po-
larization, in qualitative agreement with experiments [5].
We report another intrinsic mechanism of SHE based
on a special role of OAM with regard to electron posi-
tion, whichwasnotrecognizedinpreviousstudies[13–17]
on OAM effect. For illustration, we use for now a two-
dimensional (2D) square lattice in the plane z= 0. Later
we switch back to 3D. When pz±ipxorbitals ( Ly=±¯h)
at different lattice sites are superposed to form a Bloch
state with crystal momentum /vectorkalong +xdirection, the
resulting electron density is notcentered around thez= 0 plane but instead shifted out-of-plane along±z
direction due to the interference between atomic orbitals
at neighboring sites (see Fig. 2 and related discussion in
Ref. [18]). When /vectorkis small, this shift δ/vector ris given by
δ/vector r=αK
e/vectork×/vectorL, (1)
for general directions of /vectorkand/vectorL, where−eis the elec-
tron charge and αKis a proportionality constant, which
depends on the relative size of atomic orbitals with re-
spect to inter-atomic distance. Here /vectorLdenotes OAM of
atomicorbitals instead of /vector rׯh/vectork[19]. It thus commutes
with/vectorkand also with the position operator /vector r, which is the
canonical pair of /vectorkand measures the lattice position of
each atomic orbital. Nonzero δ/vector rimplies that /vector rdoes not
properly represent the true position of an electron. At
surfaces with broken inversion symmetry, this correction
couples with an internal electric field to produce large
Rashba-type spin splitting [18, 20].
Pedagogical discussion.— To illustrate effects of δ/vector rfor
nonmagnetic systems with inversion symmetry, we use
the free electron-like unperturbed band Hamiltonian H0,
H0=¯h2/vectork2
2m+HLS, (2)
where the atomic SO coupling HLS,
HLS=αSO/vectorL·/vectorS, (3)
is large in heavy metals. We regard the total angular
momentum Jas a good quantum number and illustrate
orbital Hall effect (OHE) and SHE for J= 1/2 states
of a 2D electron system. Note that H0is two-fold de-
generate for all /vectorkand provides a general description of
nonmagnetic systems with inversion symmetry for small
/vectork. We remark that for this H0, previous theories [12–16]
of intrinsic SHE do not work.
Ourtheorydeviatesfromprevioustheorieswhenacon-
stant external electric field /vectorEis applied. The coupling to
/vectorEis commonly given by
H′
1=e/vectorE·/vector r. (4)2
ky
k0(d)
ω(a)
ω
kxky(b)
ω
kxkyOAM
SAM
O
kxky
(c)
kxkk
kykk
OAM
SSAM
O
FIG. 1: (Color online) Electron dispersion for J= 1/2 in the
presence of the bias field /vectorE. Band structure based on (a) H0
and (b)H0+H′
2together with the occupation change due to
H′
1./vectorEis applied in the −x-direction. Average spin direction
of the split Jz=±1/2 bands is anti-parallel to the average
OAM direction. (c) Fermi surfaces of the split bands. Red
(blue) area represents occupied states with only down (up)
spins. (d) The band dispersion along the dash-dot line in (c) .
k0is the shift of each band along the kydirection.
However δ/vector rimplies that the correct coupling [18] should
beH′
1+H′
2, where
H′
2=e/vectorE·δ/vector r=αK/vectorE·(/vectork×/vectorL). (5)
Previous analyses [13–16] of OAM based intrinsic SHE
didnottakeintoaccount H′
2. ThusthetotalHamiltonian
becomes
Htot=H0+H′
1+H′
2. (6)
Its band, spin angular momentum (SAM), and OAM
structures are plotted for /vectorE=−E0/vector xwithH′
2neglected
[Fig.1(a)]andwith H′
2considered[Fig.1(b)]. Inaddition
to the overall band structure shift in the kx-direction as
shown in Fig. 1(a) (to be more exact, it is actually a shift
in the occupation), the originally degenerate Jz=±1/2
bands get split due to H′
2with the average OAM polar-
ized along the + z- or−z-directions as shown in Fig. 1(b)
(exaggerated for a better view). The split Fermi surfaces
are shown in Fig. 1(c), where the Fermi surfaces with
opposite OAM are shifted along opposite kydirections.
Consequently, there are k-space regions (shaded areas)
where electrons have net OAM; more electrons with up-
OAM in the + kyregion (shaded red) and more electrons
xyz
L
Wd
OAM
SAM
FIG. 2: (Color online) Schematic for OAM driven intrinsic
SHE. Electrons flow in the x-direction by /vectorEand are deflected
in side ways due to H′
2. Note that the deflection direction
depends on the direction of OAM, amounting to OHE. For
J= 1/2 band, HLSsets SAM anti-parallel to OAM. Thus
SHE arises a concomitant effect of OHE.
with down-OAM (shaded blue) in the −kyregion. This
naturally leads to OHE. This mechanism of OHE due to
δ/vector rdiffers from other mechanisms [13–17] of OHE.
For strong HLS, OHE implies SHE since OAM and
SAM are correlated; for J= 1/2 withL= 1, they are
anti-parallel. Thus the orbital Hall current implies the
spin Hallcurrentofopposite sign. Figure2illustratesthe
OAM driven intrinsic SHE for the J= 1/2 case. This
mechanism of SHE can be generalized to other situations
in a straightforward way. For instance, if we apply Htot
to theJ= 3/2 case with L= 1 [21], one again finds both
OHE and SHE, the only qualitative difference being that
the orbital and spin Hall currents now have the same
sign since /vectorL·/vectorS >0. This provides an alternative [13–16]
explanation for opposite signs of σSHfor materials with
opposite signs of the SO polarization /vectorL·/vectorS.
Conventional spin current.— The above discussion is
incomplete since it demonstrates only the Fermi surface
contribution to SHE and neglects a Fermi sea contribu-
tion. From now on, we consider a 3D system described
by Eq. (6), and evaluate systematically the conventional
spin current density operator ˆjS
α,βdefined by
ˆjS
α,β=1
V−e
¯h/2{Sα,vβ}
2, (7)
where{···}is the anti-commutator, Vis the volume of
the system, and the factor −e/(¯h/2) is introduced to
makeˆjS
α,βhave the same dimension as the charge cur-
rent density. Here vβis theβ(=x,y,z) component of
the velocity operator /vector v,
/vector v=[/vector r,Htot]
i¯h=¯h/vectork
m+αK
¯h(/vectorL×/vectorE) =/vector v(0)+/vector v(1).(8)
Note that /vector vcontains two contributions. When the
anomalous velocity /vector v(1)= (αK/¯h)/vectorL×/vectorEis neglected and3
(a)
kyE
kyE
Occupation
change
(b)
Anomalous
velocity
(c) E
J = 3/2
J = 1/2State
changeE
mixing
FIG. 3: (Color online) Schematic illustration of the three
terms tothe intrinsic SHE, (a) occupation change, (b)anoma -
lous velocity, and (c) state change. Figures on the left repr e-
sent the situation with H0while on the right with H0+H′
2.
the resulting ˆjS
α,βis averaged over the shaded momen-
tum space region in Fig. 1(c) [to be precise, 3D coun-
terpart of Fig. 1(c)], one obtains what we call the oc-
cupation change contribution ( jS
α,β)occoming from the
Fermi surface, as illustrated in the pedagogical discus-
sion. The magnitude of ( jS
α,β)occan be estimated eas-
ily. The density of electrons that contribute to the net
spin current density is proportional to 4 πk2
Fk0, where
kFis the Fermi wavevector for the unperturbed Fermi
surface and k0∼(m/¯h2)αK/vectorE×/vectorLis the Fermi surface
shift caused by H′
2[see Fig. 1(d)]. Each of such elec-
trons contributes ±efor [−e/(¯h/2)]Sα, and±¯hkF/mfor
vβ. Combined with a symmetry consideration, which re-
quires (jS
α,β) to be proportional to ǫαβγEγ, whereǫαβγis
the Levi-Civita symbol, one finds
(jS
α,β)oc= (ηJ)ocǫαβγEγeαK4πk3
F/3
(2π)3,(9)
where (ηJ)ocis a dimensionless constant. From the exact
evaluation [22] of ( jS
α,β)oc, we find ( ηJ=1/2)oc= 4/9 and
(ηJ=3/2)oc=−20/9 [21]. Note that the sign of ηJis
opposite for the two J’s as expected.
The anomalous velocity v(1)generates additional con-
tribution, which comes from the Fermi sea. When v(0)
is neglected and only v(1)is retained, the average of the
resulting ˆjS
α,βover the unperturbed Fermi sea of H0re-
sults in what we call the anomalous velocity contribution(jS
α,β)av. To estimate its magnitude, one first notes that
ǫαβγSαv(1)
β= (αK/¯h)[/vectorS×(/vectorL×/vectorE)]γ= (αK/¯h)[(/vectorS·/vectorE)/vectorL−
(/vectorS·/vectorL)/vectorE]γ. While the first term may fluctuate in sign, the
second term ( ∝/vectorS·/vectorL) has a definite sign over the Fermi
sea. Thus ( jS
α,β)avmay be estimated by multiplying the
secondterm with the electrondensity ∼(4πk3
F/3)/(2π)3,
which results in
(jS
α,β)av= (ηJ)avǫαβγEγeαK4πk3
F/3
(2π)3,(10)
where (ηJ)avis a dimensionless constant. From the exact
evaluation [22] of ( jS
α,β)av, we find ( ηJ=1/2)av=−4/3
and (ηJ=3/2)av= +4/3 [21]. The sign of ( ηJ)avis again
opposite for the two Jvalues due to the sign difference
of/vectorS·/vectorL. Figures 3(a) and (b) illustrate schematically
(jS
α,β)ocand (jS
α,β)av.
In addition, there exists a third contribution which is
illustrated in Fig. 3(c). When /vectorEis applied, /vectorJ=/vectorL+/vectorSis
not a good quantum number any more and H′
2induces
the inter-band mixing between the J= 1/2 andJ= 3/2
bands. This contribution ( jS
α,β)sc, which we call the state
changecontribution,isinverselyproportionaltotheband
separation between the J= 1/2 andJ= 3/2 bands, and
becomes smaller as HLSbecomes larger. From the exact
evaluation [22] of ( jS
α,β)sc, we find that ( jS
α,β)scis smaller
than (jS
α,β)ocand (jS
α,β)avby the factor (¯ h2k2
F/2m)/∆E,
where ∆E= 3¯h2αSO/2 is the energy separation between
theJ= 1/2 andJ= 3/2 bands. Since we are inter-
ested in the large HLSlimit, we ignore ( jS
α,β)scin the
subsequent discussion.
Proper spin current.— Next we examine whether the
OAM driven spin Hall current generates spin accumula-
tion at side surfacesofa system, which is what is actually
measuredinSHEdetectionschemessuchasKerrrotation
spectroscopy [2, 23–27] and photoluminescence [28, 29].
SinceHLSbreaks the spin conservation, nonzero conven-
tional spin current does not guarantee the spin accumu-
lation [30]. For transparent connection with the spin ac-
cumulation, we evaluate the proper spin current density
operator [31]
ˆjS,prop
α,β=1
V−e
¯h/2d(Sαrβ)
dt, (11)
which captures the combined effect of the conventional
spin current and the spin conservation violation. We
evaluate [22] the spin current for Htotby using ˆjS,prop
α,β
instead of ˆjS
α,β[Eq. (7)], and find identical results, con-
firming the spin accumulation by the OAM driven SHE.
To be more rigorous, however, both ˆjS,prop
α,βandˆjS
α,β
fail to capture the full effect of δ/vector r, since both operators
are defined in terms of /vector r, which does not represent the
true position of electrons. To remedy this problem, /vector rin
the definitions should be replaced by /vectorR≡/vector r+δ/vector r. Af-
ter this remedy to ˆjS,prop
α,β, we find [22] that the anoma-
lous contribution ( jS
α,β)avbecomes doubled. Thus in the4
strongHLSlimit, the total spin Hall conductivity σSH
[(jS
α,β)total=ǫαβγσSHEγ] is given by
σSH= (ηJ)totaleαK4πk3
F/3
(2π)3(12)
for small /vectork, where the dimensionless constant ( ηJ)total=
(ηJ)oc+2(ηJ)avis 4/9−8/3 =−20/9 forJ= 1/2 and
−20/9 + 8/3 = 4/9 forJ= 3/2. Note that σSHhas
opposite signs for J= 1/2 andJ= 3/2.
Discussion.— To understand better the mechanism of
the OAM driven SHE, it is useful to examine the equa-
tion of motion, d/vectorR/dt=/vector v(0)+2/vector v(1)−(αK/e)/vectork×d/vectorS/dt+
[δ/vector r,e/vectorE·δ/vector r]/i¯h. The factor 2 in the second term explains
why (jS
α,β)avis doubled after the remedy to ˆjS,prop
α,β. The
third term vanishes in the steady state and does not con-
tribute to σSH[22]. The last term ( ∝k2) is small in
the small /vectorklimit but is important conceptually. Fur-
ther insights can be gained by regarding δ/vector ras a momen-
tum space vector potential /vectorA≡ −δ/vector r. Then/vectorR=/vector r−/vectorA
amounts to the “gauge-invariant”position operator. The
equations of motion become
d/vectorR
dt=¯h/vectork
m+d/vectork
dt×/vectorB,d/vectork
dt=−e/vectorE
¯h, (13)
wherethemomentum spaceeffectivemagneticfield Bα=
(1/2)ǫαβγFβγwith
Fβγ=∂kβAγ−∂kγAβ+i[Aβ,Aγ].(14)
Note that Eq. (13) has the same form as the wavepacket
equations of motion [32] in the presence of the momen-
tum space Berry phase. There is however an important
difference; the momentum space Berry connection /vectorAis
now non-Abelian ([ Aβ,Aγ] = [δrβ,δrγ]∝ne}ationslash= 0). For the
non-Abelian case, the commutator in Eq. (14) is crucial
to keep the field strength tensor Fβγ“gauge-invariant”.
This indicates that δ/vector rinduces the momentum space non-
Abelian Berry phase, which is responsible for the Fermi
sea contribution 2( ηJ)avtoσSH. The non-Abelian /vectorA
also implies the noncommutative space, [ Rα,Rβ]∝ne}ationslash= 0.
Such noncommutative geometry arises generically when
the true position operatoris projected onto a sub-Hilbert
space[33]. A well known exampleis the quantum Hall ef-
fect, where the noncommutativity emerges after the pro-
jection onto the lowest Landau level [34]. For the present
case, the noncommutativity arises since /vectorRamounts to
the projection of the true position operator onto the sub-
Hilbert space with fixed /vectorL2(L= 1).
Difference from other mechanisms of intrinsic SHE is
now evident. Unlike previous works on the OAM based
SHE [13–16], what OAM generates is the momentum
space Berry phase instead of the real space Aharonov-
Bohm phase. Unlike previous works [12] based on the
momentum space Berry phase, its origin is δ/vector rinstead
of small SO gap. Thus this mechanism works even forJ= 1/2, for which SO gap is forbidden in nonmag-
netic systems with inversion symmetry. In this sense,
this mechanism is quite generic; it applies to all non- s-
character orbitals, with the only serious constraint being
largeHLS. When HLSis small, bands with opposite
signs of/vectorL·/vectorSoverlap and their contributions to σSHtend
to cancel each other.
Finally we estimate the magnitude of σSH∼eαKn,
wherenis the electron density. To estimate αK, we uti-
lize the connection between αKand the Rashba-type SO
coupling constant αRnear a surface where the structural
inversion symmetry is broken. Some of us have demon-
strated [18, 20] that the maximum αRin the large HLS
limit is roughly given by αK|/vectorEint|¯h, where/vectorEintdenotes
the internal electric field near surfaces produced by the
inversion symmetry breaking and is of order (work func-
tion)/(atomicspacing) ∼1 V/A. For αR∼10−11−10−10
eV·m [35–37], one obtains αK∼10−6−10−5m2V−1s−1.
Then for typical metallic electron density n∼(3 A)−3,
one obtains σSH∼104−105Ω−1m−1, which is compa-
rable to experimental values for heavy metals [5]. We
note however that this estimation is crude since Eq. (12)
is derived in the small /vectorklimit whereas /vectorkis not small in
metallic systems. Moreover it ignores complicated band
structures of real materials.
In conclusion, we presented a generic mechanism of
intrinsic SHE based on OAM, which is applicable to all
non-s-characterorbitals in nonmagnetic systems with in-
version symmetry. The position shift δ/vector rdue to OAM
gives rise to the non-Abelian Berry curvature in the mo-
mentumspace, whichproducesbothOHEandSHE.This
mechanism implies the sign change of σSHas the SO po-
larization /vectorS·/vectorLchanges its sign. The resulting σSHis
estimated to 104−105Ω−1m−1whenHLSis large. This
OAM based theory also predicts the correlation between
σSHand the strength of the Rashba-type spin splitting
at surfaces.
We acknowledge fruitful discussion with G. S. Jeon,
J. H. Han, K. J. Lee and B. C. Min. This research
was supported by the Converging Research Center Pro-
gram through the Ministry of Science, ICT and Fu-
ture Planning, Korea(2013K000312). HWL acknowl-
edges the financial support of the NRF (2011-0030784
and 2013R1A2A2A05006237).
∗Electronic address: hwl@postech.ac.kr
†Electronic address: changyoung@yonsei.ac.kr
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and H. W. Yeom, Phys. Rev. Lett. 110, 036801 (2013).arXiv:1407.3446v1 [cond-mat.mes-hall] 13 Jul 2014Supplementary Material: Orbital angular momentum driven i ntrinsic spin Hall effect
W. S. Jung,1Dongwook Go,2Hyun-Woo Lee,2,∗and C. Kim1,†
1Institute of Physics and Applied Physics, Yonsei Universit y, Seoul 120-749, Korea
2Department of Physics, Pohang University of Science and Tec hnology, Pohang, Kyungbuk 790-784, Korea
(Dated: June 19, 2021)
PACS numbers:
In Secs. I, II, III of the supplementary material, we
present the calculation of the spin current density in 3D.
Eventually we calculate in Sec. III the proper spin cur-
rent density jS,PROP
α,β, which is based on the concept of
the “proper” spin current1and formulated in terms of
the “proper” position operator /vectorR. However its calcula-
tion is rather technical and less illuminating. Thus for
pedagogical purpose, we present the calculation of more
conventional spin current density first in Secs. I and II.
In Sec. I, we presentthe calculationofthe conventional
spin current density jS
α,βformulated in terms of the con-
ventional position operator /vector r, where/vector ris the canonical
pair of the Bloch momentum /vectorkandjS
α,βis the expecta-
tion value of the conventional spin current density oper-
atorˆjS
α,β,
ˆjS
α,β=1
V−e
¯h/2{Sα,drβ/dt}
2. (S1)
Note that ˆjS
α,βis defined to have the same dimension as
the charge current density. We demonstrate that jS
α,β
has three independent contributions, which we call the
anomalous velocity contribution, the state change con-
tribution, and the occupation change contribution. The
physical meaning of each contribution will become clear
in Sec. I.
In Sec. II, we present the calculation of the proper spin
currentdensity jS,prop
α,βformulatedin termsofthe conven-
tionalpositionoperator /vector r. Theconceptoftheproperspin
current was proposed1to take into account the violation
of the spin conservation and to facilitate the connection
with the spin accumulation. jS,prop
α,βis the expectation
value of the operator ˆjS,prop
α,β,
ˆjS,prop
α,β=1
V−e
¯h/2d
dt{Sα,rβ}
2. (S2)
Compared to Eq. (S1), where the time derivative ap-
plies torβonly, Eq. (S2) differs since the time deriva-
tive now applies to the anti-commutator {Sα,rβ}. We
demonstrate that jS,prop
α,βis identical to jS
α,β.
In Sec. III, we finally present the calculation of the
proper spin current density jS,PROP
α,βformulated in terms
of the proper position operator /vectorR, where/vectorRdiffers from
/vector ras follows,
/vectorR=/vector r+αK
e/vectork×/vectorL, (S3)andjS,PROP
α,βis the expectation value of the operator
ˆjS,PROP
α,β,
ˆjS,PROP
α,β=1
V−e
¯h/2d
dt{Sα,Rβ}
2. (S4)
Note that Eq. (S4) is identical to Eq.(S2) except that Rβ
appears instead of rβ. While the calculation of jS,PROP
α,β
is more tedious than those of the former two counter-
parts, the value of jS,PROP
α,βturns out to be almost iden-
tical tojS
α,βandjS,prop
α,β, except that the magnitude ofthe
anomalous velocity contribution is now two times bigger.
I. CONVENTIONAL SPIN CURRENT DENSITY
Here we present the calculation of the conventional
spin current density jS
α,βformulated in terms of the con-
ventional position operator. jS
α,βis given by
jS
α,β= Tr/bracketleftBig
ˆjS
α,βˆρ/bracketrightBig
, (S5)
where ˆρis the density matrix and the operator ˆjS
α,βis
defined in Eq. (S1).
For/vectorE= 0, both H′
1andH′
2vanish and ˆ ρbecomes its
equilibrium form ˆ ρ(0), where
ˆρ(0)=/summationdisplay
nf(0)/parenleftBig
E(0)
n/parenrightBig
|n/an}bracketri}ht(0) (0)/an}bracketle{tn|,(S6)
Here|n/an}bracketri}ht(0)denotesaneigenstateof H0withenergyeigen-
valueE(0)
n, andf(0)(E) is the equilibrium Fermi occupa-
tion function. It is straightforward to verify that jS
α,β
vanishes in equilibrium.
When a nonzero /vectorEis applied, we evaluate jS
α,βup to
the first order in /vectorE. Up to this order, effects of H′
1and
H′
2may be considered separately. H′
1alone does not con-
tribute to jS
α,βat all since as far as H0+H′
1is concerned,
the dynamicsof /vector rinH′
1is decoupledfrom thatof /vectorS. This
is evident from the facts that H′
1commutes with both /vectorL
and/vectorSand that there is no coupling in H0+H′
1linking/vector r
(or/vectork) with/vectorS(or/vectorL). Below we thus ignore effects of H′
1
and consider effects of H′
2only.
In Secs. IA and IB, we evaluate two contributions to
jS
α,βunder the assumption that impurity scattering is
completely absent. In Sec. IC, we consider the effect of
the impurity scattering on jS
α,βin the limit of vanishingly
weak scatterers.2
A. Anomalous velocity contribution
One effect of H′
2is to modify the velocity operator /vector v.
For the total Hamiltonian H0+H′
2,/vector vis given by
/vector v=d/vector r
dt=[/vector r,H0+H′
2]
i¯h=¯h/vectork
m+αK
¯h/vectorL×/vectorE=/vector v(0)+/vector v(1),
(S7)
where/vector v(0)and/vector v(1)refer to the terms independent of and
linear in /vectorE. Here we call /vector v(1)the anomalous velocity
since it denotes the extra contribution to the velocity
generated by /vectorE.
/vector v(1)generateswhatwecallthe anomalousvelocitycon-
tribution ( jS
α,β)avto the spin current,
(jS
α,β)av=1
V−e
¯h/2Tr/bracketleftBigg
{Sα,v(1)
β}
2ˆρ/bracketrightBigg
.(S8)
Up to the first order in /vectorE, ˆρin the above equation may
be replaced by ˆ ρ(0)sincev(1)is already first order in /vectorE.
Then Eq. (S8) reduces to
(jS
α,β)av=1
V−e
¯h/2/summationdisplay
nf(0)/parenleftBig
E(0)
n/parenrightBig
(0)/an}bracketle{tn|Sαv(1)
β|n/an}bracketri}ht(0).
(S9)
Here one used Sαv(1)
β=v(1)
βSα. Since the eigenstates of
H0are completely specified by the three quantum num-
bers (/vectork,J,Jz) within the orbital angular momentum
L= 1 sector, the state |n/an}bracketri}ht(0)amounts to |/vectork,J,Jz/an}bracketri}ht(0). For
a givenJ, the summation over nin Eq. (S9) amounts to
the summations over /vectorkandJz. SinceE(0)
n=E(0)(/vectork,J)
is independent of Jz, the summation over Jzleads to the
following partial trace over jz,
/summationdisplay
Jz(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingleSαv(1)
β/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
.(S10)
One then utilizes the relations v(1)
β= (αK/¯h)ǫβηγLηEγ
and
/summationdisplay
Jz(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingleSαLη/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
(S11)
=δα,η/summationdisplay
Jz(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingleSzLz/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
=1
3δαη/summationdisplay
Jz(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingle/vectorS·/vectorL/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
.
Note that /vectorS·/vectorL= (¯h2/2)/bracketleftbig
J(J+1)−1·2−1
2·3
2/bracketrightbig
has
opposite signs for J= 3/2 andJ= 1/2. As confirmed
below, this sign difference leads to the sign difference in
(jS
α,β)avforJ= 3/2 andJ= 1/2. Subsequent calcula-
tion proceeds as follows. One first obtains
/summationdisplay
Jz(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingleSαv(1)
β/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
(S12)
=−ǫαβγEγαK
¯h¯h21
6/bracketleftbigg
J(J+1)−11
4/bracketrightbigg
(2J+1).Thentheanomalousvelocitycontributiontothespincur-
rent density becomes
(jS
α,β)av (S13)
=−e
¯h/2(−ǫαβγ)αK
¯hEγ¯h21
6/bracketleftbigg
J(J+1)−11
4/bracketrightbigg
(2J+1)
×1
V/summationdisplay
/vectorkf(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig
=ǫαβγEγeαK1
3/bracketleftbigg
J(J+1)−11
4/bracketrightbigg
(2J+1)4πk3
F/3
(2π)3
=±2
9π2ǫαβγEγeαKk3
F,
where the upper and lower signs apply to J= 3/2 and
J= 1/2, respectively. Note that ( jS
α,β)avindeed has op-
positesignsfor J= 3/2andJ= 1/2. Thissigndifference
stems from the fact that /vectorSis parallel (antiparallel) to /vectorL
forJ= 3/2 (J= 1/2).
B. State change contribution
Inaddition toEq.(S8), which capturestheeffect ofthe
anomalous velocity /vector v(1), the conventional velocity opera-
tor/vector v(0)also contributes to the spin current density. We
call this contribution the state change contribution for
the reason that will become clear below. It is given by
(jS
α,β)sc=1
V−e
¯h/2Tr/bracketleftBigg
{Sα,v(0)
β}
2ˆρ/bracketrightBigg
.(S14)
When ˆρin the above expression is replaced by ˆ ρ(0), the
above expression vanishes. Thus ( jS
α,β)scarises from the
first order correction to ˆ ρdue to/vectorE. Up to this order, one
obtains
(jS
α,β)sc=1
V−e
¯h/2Tr/bracketleftBig
Sαv(0)
βˆρ(1)/bracketrightBig
,(S15)
whereSαv(0)
β=v(0)
βSαis used. One way to evaluate
Eq. (S15) is to use the Kubo formula. Here we evaluate
Eq. (S15) in a slightly different way, since this alternative
method illustrates better why ( jS
α,β)scmay be called the
inter-band mixing contribution. It is straightforward to
verify that this method and the Kubo formula produce
the same result for ( jS
α,β)sc.
The adiabatic turning-on procedure allows a straight-
forward evaluation of ˆ ρ(1). When H′
2is turned on adi-
abatically from the far past t=−∞, ˆρat present time
t= 0 is given by
ˆρ=/summationdisplay
nf(0)/parenleftBig
E(0)
n/parenrightBig
|n/an}bracketri}ht /an}bracketle{tn|. (S16)
Here|n/an}bracketri}htdenotes the state at t= 0, to which |n/an}bracketri}ht(0)at
t=−∞evolves as H′
2is adiabatically turned on. Up3
to the first order in /vectorE,|n/an}bracketri}htdiffers from |n/an}bracketri}ht(0)by|n/an}bracketri}ht(1),
which is given by
|n/an}bracketri}ht(1)=/summationdisplay
n′/negationslash=n|n′/an}bracketri}ht(0)(0)/an}bracketle{tn′|H′
2|n/an}bracketri}ht(0)
E(0)
n−E(0)
n′. (S17)
Then ˆρ(1)becomes
ˆρ(1)=/summationdisplay
nf(0)/parenleftBig
E(0)
n/parenrightBig/parenleftBig
|n/an}bracketri}ht(0) (1)/an}bracketle{tn|+|n/an}bracketri}ht(1) (0)/an}bracketle{tn|/parenrightBig
,
(S18)
and (jS
α,β)scin Eq. (S15) becomes
(jS
α,β)sc=1
V−e
¯h/2/summationdisplay
n/summationdisplay
n′f(0)/parenleftBig
E(0)
n/parenrightBig
(S19)
×/parenleftBig(0)/an}bracketle{tn′|Sαv(0)
β|n/an}bracketri}ht(0) (1)/an}bracketle{tn|n′/an}bracketri}ht(0)
+(0)/an}bracketle{tn′|Sαv(0)
β|n/an}bracketri}ht(1) (0)/an}bracketle{tn|n′/an}bracketri}ht(0)/parenrightBig
.
To evaluate this expression, one recalls E(0)
nbeing in-
dependent of Jzand exploits this energy degeneracy to
introduce a new set of quantum numbers ( /vectork,J,J˜z) to
specify the state n. HereJ˜zdenotes the component of
the total angularmomentum along the direction ˜ z, which
points along /vectorE×/vectorkdirection. Note that ˜ zaxis is de-
pendent on /vectork. This change of the angular momentum
quantization axis from zto ˜zsimplifies the evaluation of
Eq. (S17). Considering that H′
2reduces to αK|/vectorE×/vectork|L˜z,
one finds
(0)/an}bracketle{tn′|H′
2|n/an}bracketri}ht(0)(S20)
=αK|/vectorE×/vectork|(0)/angbracketleftBig
/vectork′,J′,J′
˜z/vextendsingle/vextendsingle/vextendsingleL˜z/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
=δ/vectork′/vectorkδJ′
˜zJ˜zαK|/vectorE×/vectork|(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleL˜z/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
.
ThusH′
2induces the inter-band mixing between |/vectork,J=
1/2,J˜z/an}bracketri}ht(0)and|/vectork,J= 3/2,J˜z/an}bracketri}ht(0). It is now evident that
(jS
αβ)sccaptures the effect of the state change due to the
inter-band mixing caused by H′
2. The matrix elements
that capture this inter-band mixing effect are
(0)/angbracketleftbigg
/vectork,J=1
2,J˜z=±1
2/vextendsingle/vextendsingle/vextendsingle/vextendsingleH′
2/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=3
2,J˜z=±1
2/angbracketrightbigg(0)
=(0)/angbracketleftbigg
/vectork,J=3
2,J˜z=±1
2/vextendsingle/vextendsingle/vextendsingle/vextendsingleH′
2/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=1
2,J˜z=±1
2/angbracketrightbigg(0)
=αK|/vectorE×/vectork|/parenleftBigg
−√
2
3¯h/parenrightBigg
. (S21)All other matrix elements are zero. Then one obtains
/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=1
2,J˜z=±1
2/angbracketrightbigg(1)
(S22)
=/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=3
2,J˜z=±1
2/angbracketrightbigg(0)αK|/vectorE×/vectork|√
2
3¯h
∆E,
/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=3
2,J˜z=±1
2/angbracketrightbigg(1)
(S23)
=−/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=1
2,J˜z=±1
2/angbracketrightbigg(0)αK|/vectorE×/vectork|√
2
3¯h
∆E,
/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=3
2,J˜z=±3
2/angbracketrightbigg(1)
= 0. (S24)
where ∆ E≡E(0)(/vectork,J= 3/2,J˜z)−E(0)(/vectork,J=
1/2,J˜z) = 3αSO¯h2/2 is independent of /vectorkandJ˜z.
Then (jS
α,β)scin Eq. (S19) reduces to
(jS
α,β)sc (S25)
=∓1
V−e
¯h/2/summationdisplay
/vectork/summationdisplay
J˜z=±1/2f(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig
×αK|/vectorE×/vectork|√
2
3¯h
∆E/parenleftbigg(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleSαv(0)
β/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
+(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsingleSαv(0)
β/vextendsingle/vextendsingle/vextendsingle/vectork,J′,J˜z/angbracketrightBig(0)/parenrightbigg
,
where the upper and lower signs apply to J= 3/2 and
J= 1/2, respectively. J′= 1/2 (3/2) when J= 3/2
(1/2). Using the relation
(0)/angbracketleftbigg
/vectork,J=1
2,J˜z/vextendsingle/vextendsingle/vextendsingle/vextendsingleSαv(0)
β/vextendsingle/vextendsingle/vextendsingle/vextendsingle/vectork,J=3
2,J˜z/angbracketrightbigg(0)
(S26)
=√
2¯h
3(/vectorE×/vectork)α
|/vectorE×/vectork|¯hkβ
m,
one obtains
(jS
α,β)sc (S27)
=∓1
V−e
¯h/2/summationdisplay
/vectork2f(0)/parenleftBig
E(0)(/vectork,J)/parenrightBigαK(/vectorE×/vectork)α
∆E2¯h2
92¯hkβ
m.
From the relation
1
V/summationdisplay
/vectorkf(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig
(/vectorE×/vectork)αkβ(S28)
=1
V/summationdisplay
/vectorkf(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig/parenleftBig
−ǫαβγ
3Eγ/parenrightBig
k2
=−ǫαβγ
3Eγ4πk3
F/3
(2π)33k2
F
5, (S29)
one finally obtains
(jS
α,β)sc=∓16
135π2ǫαβγEγeαKk3
F¯h2k2
F/2m
∆E.(S30)4
Note that similarly to ( jS
α,β)av, (jS
α,β)scalso has opposite
signs for J= 3/2 (upper sign) and J= 1/2 (lower sign).
C. Occupation change contribution
So far we have neglected impurity scattering. Here we
consider the scattering effect in the vanishing scattering
strength limit. Even in this limit, the scattering is im-
portant since it violates the momentum conservation and
allows electrons to relax in momentum space. To illus-
trateitsimportance, it isusefultoconsiderthe casewhen
the scattering is completely absent. Then all throughout
the adiabatic turning-on procedure of H′
2,/vectorkremains a
good quantum number and the electron occupation in /vectork
space cannot be altered by H′
2, which is in contrast to
what we expect as illustrated in Fig. 2(b). In the Kubo
formalism, this effect is often addressed through the ver-
tex correction. Here we address this effect by noting that
the energy eigenvalues of H0+H′
2are bounded from be-
low. In such a situation, the electron occupation will
relax in/vectorkspace to minimize the total energy of the elec-
trons. Thus the occupation change contribution ( jS
αβ)oc
to the spin current density is given by
(jS
α,β)oc=1
V−e
¯h/2Tr/bracketleftBig
Sαv(0)
βˆρ(1)
oc/bracketrightBig
,(S31)
where ˆρ(1)
ocdenotes the first order correction to density
matrix due to scattering and is given by
ˆρ(1)
oc=/summationdisplay
nf(1)
n|n/an}bracketri}ht(0) (0)/an}bracketle{tn|. (S32)
Heref(1)
n=f(0)(En)−f(0)(E(0)
n) denotes the first order
correctionto the occupation function and Endenotes the
energy eigenvalue of H0+H′
2. (jS
αβ)ocis thus given by
(jS
α,β)oc=1
V−e
¯h/2/summationdisplay
nf(1)(En)(0)/an}bracketle{tn|Sαv(0)
β|n/an}bracketri}ht(0),
(S33)
where Tr[ Sαv(0)
βρ(0)] = 0 has been used.
To determine En, it is useful to use the quantum num-
bers/vectork,J,J˜zinstead of /vectork,J,Jzto specify nsince for given
Jsector, the state |/vectork,J,J˜z/an}bracketri}ht(0)diagonalizes H0+H′
2with
the eigenvalue En=E(/vectork,J,J˜z) given by
E(/vectork,J,J˜z) =E(0)(/vectork,J)+αK|/vectorE×/vectork|3∓1
3¯hJ˜z,(S34)
where the upper and lower signs apply to J= 3/2 and
J= 1/2, respectively. To understand the effect of the
second term, it is useful to consider one particular case;
/vectorE=Ezˆz. Then the second term is proportional to
(k2
x+k2
y)1/2. On the other hand, the first term is pro-
portional to /vectork2=k2
z+ (k2
x+k2
y). Thus the combined
effect of the first and second terms is to expand (shrink)theoriginallysphericalFermisurfacealongthe“equator”
direction when the second term is negative (positive).
The next step in the evaluation of ( jS
αβ)ocis to calcu-
late(0)/an}bracketle{tn|Sαv(0)
β|n/an}bracketri}ht(0)with|n/an}bracketri}ht(0)replacedby |/vectork,J,J˜z/an}bracketri}ht(0).
After straightforward calculation, one obtains
(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsingleSαv(0)
β/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
(S35)
=(/vectorE×/vectork)α
|/vectorE×/vectork|/parenleftbigg
±¯hJ˜z
3/parenrightbigg¯hkβ
m,
= sgn(Ez)kxδαy−kyδαx/radicalBig
k2x+k2y/parenleftbigg
±¯hJ˜z
3/parenrightbigg¯hkβ
m,
where the upper and lower signs apply to J= 3/2 and
J= 1/2, respectively. After the average over the az-
imuthal angle in /vectorkspace, the above expression reduces
to
(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsingleSαv(0)
β/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
(S36)
= sgn(Ez)/radicalBig
k2x+k2y
2(−ǫαβz)/parenleftbigg
±¯hJ˜z
3/parenrightbigg¯h
m,
Then (jS
αβ)ocbecomes
(jS
α,β)oc (S37)
=1
V−e
¯h/2/summationdisplay
/vectork/summationdisplay
J˜zf(0)/parenleftBig
E/parenleftBig
/vectork,J,J˜z/parenrightBig/parenrightBig
×sgn(Ez)/radicalBig
k2x+k2y
2(−ǫαβz)/parenleftbigg
±¯hJ˜z
3/parenrightbigg¯h
m.
After some tedious calculation, and for general direction
of/vectorE, one obtains
(jS
α,β)oc=/braceleftbigg
−10
+2/bracerightbigg
×1
27π2ǫαβγEγeαKk3
F.(S38)
Here the upper and lower results apply to J= 3/2 and
J= 1/2, respectively. Note that ( jS
αβ)ochas opposite
signs for J= 3/2 andJ= 1/2.
D. Summary
Finally,jS
α,βcan be obtained by summing up all three
contributions,( jS
αβ)oc, (jS
αβ)av, and(jS
αβ)sc. ForJ= 3/2,
one finds
jS
αβ=−2
9π2ǫαβγEγeαKk3
F/parenleftbigg5
3−1+8
15¯h2k2
F/2m
∆E/parenrightbigg
(S39)
and forJ= 1/2, one finds
jS
αβ=2
9π2ǫαβγEγeαKk3
F/parenleftbigg1
3−1+8
15¯h2k2
F/2m
∆E/parenrightbigg
(S40)5
II. PROPER SPIN CURRENT DENSITY FOR /vector r
In this section, we calculate the proper spin current
density operator jS,prop
α,βbased on the conventional posi-
tion operator /vector r. The corresponding operator ˆjS,prop
α,βin
Eq. (S2) may be divided into two pieces as follows,
ˆjS,prop
α,β=ˆjS
α,β+ˆjS,extra
α,β, (S41)
whereˆjS
α,βis the conventional spin current operator as
defined in Eq. (S1), and
ˆjS,extra
α,β=1
V−e
¯h/2/braceleftbigdSα
dt,rβ/bracerightbig
2=1
V−e
¯h/2αSOǫαγδLγSδrβ.
(S42)
Thus the difference ˆjS,extra
α,βbetween jS,prop
α,βandjS
α,β
amounts to the expectation value of ˆjS,extra
α,β,
jS,extra
α,β= Tr/bracketleftBig
ˆjS,extra
α,βˆρ/bracketrightBig
, (S43)
which will be evaluated below. Among the two perturba-
tionsH′
1andH′
2,H′
1cannot generateany contribution to
jS,extra
α,βsince it does not induce any correlation between
/vector r(or/vectork) and/vectorL(or/vectorS). Below we thus consider possible
contribution from H′
2only.
A. Anomalous velocity contribution
By the “anomalous velocity contribution”, we refer to
jS,extra
α,βwith ˆρin Eq. (S43) replaced by its equilibrium
counterpart ˆ ρ(0)in Eq. (S6). We find jS,extra
α,βvanishes
identically. Below we demonstrate this for α=z. The
generalization to the case with α=xoryis straightfor-
ward. For α=z, one obtains
jS,extra
z,β=1
V−e
¯h/2αSO/summationdisplay
/vectork,Jzf(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig
(S44)
×(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingle(LxSy−LySx)rβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
.
To evaluate the expectation value in the above equa-
tion, one uses the relations [ LxSy−LySx,/vectork] = [LxSy−
LySx,Jz] = [rβ,J] = 0 to obtain
(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingle(LxSy−LySx)rβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
(S45)
=(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingle(LxSy−LySx)/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
×(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsinglerβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
.
This expression vanishes since
(0)/angbracketleftBig
/vectork,J,Jz/vextendsingle/vextendsingle/vextendsingle(LxSy−LySx)/vextendsingle/vextendsingle/vextendsingle/vectork,J,Jz/angbracketrightBig(0)
= 0.(S46)This vanishing can be understood as follows. Since
LxSy−LySxis hermitian, its expectation value with re-
spect to|/vectork,J,Jz/an}bracketri}ht(0)must be real. On the other hand, the
conventional representations of LxSyandLySxare pure
imaginary. The only way to reconcile these two proper-
ties is to make its expectation value zero.
Thus one finds ( jS,extra
α,β)av= 0 and ( jS,prop
α,β)av=
(jS
α,β)av. This way, one finally obtains
/parenleftBig
jS,prop
α,β/parenrightBig
av=±2
9π2ǫαβγEγeαKk3
F.(S47)
B. State change contribution
The state change contribution is defined as the con-
tribution that arises from the deviation of ˆ ρfrom ˆρ(0).
Thus the state change contribution from the extra spin
current density operator is given by
/parenleftBig
jS,extra
α,β/parenrightBig
sc=1
V−e
¯h/2Tr/bracketleftBigg/braceleftbigdSα
dt,rβ/bracerightbig
2ˆρ(1)/bracketrightBigg
,(S48)
where ˆρ(1)is given in Eq. (S18). Substituting ˆ ρ(1)into
the above equation leads to
(jS,extra
α,β)sc=1
V−e
¯h/2/summationdisplay
n/summationdisplay
n′f(0)/parenleftBig
E(0)
n/parenrightBig
αSOǫαδγ(S49)
×/parenleftBig(0)/an}bracketle{tn′|LδSγrβ|n/an}bracketri}ht(0) (1)/an}bracketle{tn|n′/an}bracketri}ht(0)
+(0)/an}bracketle{tn′|LδSγrβ|n/an}bracketri}ht(1) (0)/an}bracketle{tn|n′/an}bracketri}ht(0)/parenrightBig
.
Note that this expression has the identical structure as
Eq. (S19) except that the conventional spin current den-
sity operator ˆjS
α,βis replaced by the extra spin current
density operator ˆjS,extra
α,β. The evaluation ofthis equation
proceeds in a similar way. One first adopts the quantum
numbers /vectork,J, andJ˜zto specify the state n, whereJ˜z
denotes the component of the total angular momentum
operator along /vectorE×/vectorkdirection. This allows one to utilize6
Eqs. (S22), (S23), and (S24), and one finds
(jS,extra
α,β)sc (S50)
=∓1
V−e
¯h/2/summationdisplay
/vectork/summationdisplay
J˜z=±1/2f(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig
×αSOǫαδγαK/vextendsingle/vextendsingle/vextendsingle/vectorE×/vectork/vextendsingle/vextendsingle/vextendsingle√
2
3¯h
∆E
×/parenleftbigg(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleLδSγrβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
+(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsingleLδSγrβ/vextendsingle/vextendsingle/vextendsingle/vectork,J′,J˜z/angbracketrightBig(0)/parenrightbigg
=∓1
V−e
¯h/2/summationdisplay
/vectork/summationdisplay
J˜z=±1/2f(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig
×αSOαK/vextendsingle/vextendsingle/vextendsingle/vectorE×/vectork/vextendsingle/vextendsingle/vextendsingle√
2
3¯h
∆E
×2Re/bracketleftbigg(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleǫαδγLδSγrβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)/bracketrightbigg
,
where the upper and lower signs apply to J= 3/2 and
J= 1/2, respectively. J′= 1/2 (3/2) when J′=
3/2 (1/2). Using [ /vector r,J] = [/vector r,J˜z] = [/vectork,Lδ] = [/vectork,Sγ] = 0,
the last line of the above equation can be written as
2Re/bracketleftbigg(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleǫαδγLδSγrβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)/bracketrightbigg
(S51)
= 2Re/bracketleftbigg(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleǫαδγLδSγ/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
×(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsinglerβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)/bracketrightbigg
.
Here,(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsinglerβ/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
is manifestly real since
rβis hermitian. It can be also verified that
(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleǫαδγLδSγ/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
is purely imaginary.
For this reason, the above equation vanishes identically
and one finds ( jS,extra
α,β)sc= 0. Therefore ( jS,prop
α,β)sc=
(jS
α,β)sc, and one obtains
(jS,prop
α,β)sc=∓16
135π2ǫαβγEγeαKk3
F¯h2k2
F/2m
∆E.
forJ= 3/2 (upper sign) and J= 1/2 (lower sign), re-
spectively.
C. Occupation change contribution
The occupation change contribution refers to the con-
tribution arising from the additional deviation of ˆ ρ
from ˆρ(0)due to the impurity scattering of infinitesimal
strength. Thus ( jS,extra
α,β)ocbecomes
(jS,extra
α,β)oc= Tr/bracketleftBig
ˆjS,extra
α,βˆρ(1)
oc/bracketrightBig
,(S52)where ˆρ(1)
ocdenotes the impurity scattering effect to ˆ ρ.
Using its expression in Eq. (S32), one obtains
(jS,extra
α,β)oc (S53)
=1
V−e
¯h/2/summationdisplay
nf(1)(En)αSO(0)/an}bracketle{tn|ǫαγδLγSδrβ|n/an}bracketri}ht(0).
By following the same analysis as in Sec. IIA, one can
verify that(0)/an}bracketle{tn|ǫαγδLγSδrβ|n/an}bracketri}ht(0)= 0. Thus ( jS,extra
α,β)oc
vanishes identically and ( jS,prop
α,β)oc= (jS
α,β)oc. Therefore
one obtains
(jS,prop
α,β)oc=/braceleftbigg
−10
+2/bracerightbigg
×1
27π2ǫαβγEγeαKk3
F,
where the upper and lower numbers apply to J= 3/2
andJ= 1/2, respectively.
D. Summary
In the preceding subsections, we showed that the extra
spin current density operator ˆjS,extra
α,βdoes not generate
any extra contributions, so the proper spin current den-
sityjS,prop
α,βis identical to the conventional spin current
densityjS
α,β. To summarize the result of this section, we
obtained
jS,prop
αβ=−2
9π2ǫαβγEγeαKk3
F/parenleftbigg5
3−1+8
15¯h2k2
F/2m
∆E/parenrightbigg
(S54)
forJ= 3/2, and
jS,prop
αβ=2
9π2ǫαβγEγeαKk3
F/parenleftbigg1
3−1+8
15¯h2k2
F/2m
∆E/parenrightbigg
(S55)
forJ= 1/2.
III. PROPER SPIN CURRENT DENSITY FOR /vectorR
In this section, we evaluate the proper spin current
densityjS,PROP
α,β, which is the expectation value of the
proper spin current density operator ˆjS,PROP
α,β[Eq. (S4)]
formulated in terms of the proper position operator /vectorR
[Eq. (S3)]. ˆjS,PROP
α,βdiffers from the proper spin current
density operator ˆjS,prop
α,βin that the “proper”position op-
erator/vectorRin Eq. (S3) is used instead of the conventional
position operator /vector r. One way to understand the differ-
ence between the two position operators is to compare
the corresponding velocity operators. The “proper” ve-7
locity operator /vectorVbecomes
/vectorV=d/vectorR
dt=[/vectorR,H0+H′
1+H′
2]
i¯h(S56)
=¯h/vectork
m+αK
¯h/vectorL×/vectorE
+αK
¯h/vectorL×/vectorE+α2
K
e/parenleftBig
/vectorE×/vectork/parenrightBig/parenleftBig
/vectork·/vectorL/parenrightBig
+αKαSO
e/vectork×/parenleftBig
/vectorS×/vectorL/parenrightBig
,
where the first two terms amount to /vector v. Compared to the
conventional velocity operator /vector vin Eq. (S7), /vectorVdiffers by
/vectorV−/vector v=δ/vector va+δ/vector vb+δ/vector vc, (S57)
where
δ/vector va=αK
¯h/vectorL×/vectorE, (S58)
δ/vector vb=α2
K
e/parenleftBig
/vectorE×/vectork/parenrightBig/parenleftBig
/vectork·/vectorL/parenrightBig
, (S59)
δ/vector vc=αKαSO
e/vectork×/parenleftBig
/vectorS×/vectorL/parenrightBig
. (S60)
Among the three terms δ/vector va,δ/vector vb, andδ/vector vc,δ/vector vais identical
to the anomalousvelocity /vector v(1)in Eq. (S7). Recallingthat
/vector v(1)isresponsiblefortheanomalousvelocitycontribution
(jS
α,β)av= (jS,prop
α,β)avin Eqs. (S13) and (S47), δ/vector vabeing
identical to /vector v(1)doubles the anomalous velocity contri-
bution, which will be verified explicitly in Sec. IIIA. /vector vbis
linear in /vectorEand thus generates a new piece of the anoma-
lous velocity. Comparedto /vector va, it is smallerby the dimen-
sionless factor αK¯hk2/e, which is much smaller than 1 in
the small /vectorklimit. Thus /vector vbis not important in the small /vectork
limit, but just for the sake of completeness, we evaluate
its contribution to jS,PROP
α,βin Sec. IIIA. On the other
hand,/vector vcis zeroth order in /vectorE. We examine its possible
contribution below.
For explicit evaluation of jS,PROP
α,β, one needs to deal
withˆjS,PROP
α,βin Eq. (S4). It is useful to compare
ˆjS,PROP
α,βwithˆjS
α,βandˆjS,prop
α,β,
ˆjS,PROP
α,β=ˆjS,prop
α,β+ˆjS,EXTRA
α,β(S61)
=ˆjS
α,β+ˆjS,extra
α,β+ˆjS,EXTRA
α,β,
whereˆjS,extra
α,βis defined in Eq. (S42) and ˆjS,EXTRA
α,βis
given by
ˆjS,EXTRA
α,β=ˆjS,a
α,β+ˆjS,b
α,β+ˆjS,c
α,β.(S62)Here
ˆjS,a
α,β=1
V−e
¯h/2αK
¯hSα/parenleftBig
/vectorL×/vectorE/parenrightBig
β, (S63)
ˆjS,b
α,β=1
V−e
¯h/2α2
K
eSα/parenleftBig
/vectorE×/vectork/parenrightBig
β/parenleftBig
/vectork·/vectorL/parenrightBig
,(S64)
ˆjS,c
α,β=1
V−e
¯h/2αKαSO
2e/bracketleftbigg¯h2
2/parenleftBig
δαβ/vectork·/vectorL−kαLβ/parenrightBig
(S65)
−/braceleftbigg/parenleftBig
/vectorS×/vectorL/parenrightBig
α,/parenleftBig
/vectork×/vectorL/parenrightBig
β/bracerightbigg/bracketrightbigg
.
It is evident that the expectation value of ˆjS,EXTRA
α,βde-
terminesthe differencebetween jS,PROP
α,βand the twofor-
mer spin current densities jS
α,βandjS,prop
α,β.
Simple order counting helps estimate effects of the
three terms of ˆjS,EXTRA
α,β. SinceˆjS,aandˆjS,bare linear
in/vectorE, they can affect only the anomalous velocity contri-
bution. They do not affect the state change contribution
and the occupation change contribution. Among these
termsˆjS,b
α,βis smaller than ˆjS,a
α,βbyαK¯hk2/e, which ap-
proaches zero in the small /vectorklimit. Thus ˆjS,a
α,βis expected
to be more important. Actually it can be easily verified
thatˆjS,a
α,βis identical to1
V−e
¯h/2Sαv(1)
β[see Eq. (S8)], which
is responsible for the anomalous velocity contribution of
jS
α,β. Thus the presence of ˆjS,a
α,βdoubles the anomalous
velocity contribution. On the other hand, ˆjS,c
α,βdiffers by
the factor αKαSO¯hm/efrom1
V−e
¯h/2Sαv(0)
β[see Eq. (S31)],
which is responsible for the occupation change contribu-
tion ofjS
α,β. Since this factor may not be small in the
strong spin-orbit coupling limit that we consider, it is yet
unclear how important ˆjS,c
α,βis.
Below we demonstrate through explicit calculation
thatˆjS,c
α,βdoes not generate any important contribution
and the only important effect of ˆjS,EXTRA
α,βis to double
the anomalous velocity contribution.
A. Anomalous velocity contribution
To calculate the anomalous velocity contribution
(jS,PROP
α,β)avtojS,PROP
α,β, it is sufficient to evaluate
(jS,EXTRA
α,β)av, which is given by
(jS,EXTRA
α,β)av= Tr/bracketleftBig
ˆjS,EXTRA
α,βˆρ(0)/bracketrightBig
(S66)
= (jS,a
α,β)av+(jS,b
α,β)av+(jS,c
α,β)av,
where
(jS,a
α,β)av= Tr/bracketleftBig
ˆjS,a
α,βˆρ(0)/bracketrightBig
, (S67)
(jS,b
α,β)av= Tr/bracketleftBig
ˆjS,b
α,βˆρ(0)/bracketrightBig
, (S68)
(jS,c
α,β)av= Tr/bracketleftBig
ˆjS,c
α,βˆρ(0)/bracketrightBig
. (S69)8
For (jS,c
α,β)av, it vanishes simply because ˆjS,c
α,βis linear
in/vectorkwhereas ˆ ρ(0)puts the same weighting independent
of the direction of /vectork. To evaluate ( jS,a
α,β)av, one notes
ˆjS,a
α,β=1
V−e
¯h/2Sαδva
β=1
V−e
¯h/2Sαv(1)
β.(S70)
Thus (jS,a
α,β)avis identical to ( jS
α,β)avin Eq. (S9), and one
obtains
/parenleftBig
jS,a
α,β/parenrightBig
av=±2
9π2ǫαβγEγeαKk3
F,(S71)
forJ= 3/2 (upper sign) and J= 1/2 (lower sign).
To evaluate ( jS,b
α,β)av, one notes
ˆjS,b
α,β=1
V−e
¯h/2Sαδvb
β. (S72)
We demonstrate the evaluation of ( jS,b
α,β)avfor/vectorE=Ezˆz.
In this case, it is straightforward to verify that ( jS,b
α,β)av
is proportional to ǫαβz. It then suffices to evaluate
ǫαβz(jS,b
α,β)av. One uses the following relation
ǫαβzSα/parenleftBig
/vectorE×/vectork/parenrightBig
β/parenleftBig
/vectork·/vectorL/parenrightBig
(S73)
= (Sxkx+Syky)/parenleftBig
/vectork·/vectorL/parenrightBig
Ez
to obtain
ǫαβz/parenleftBig
jS,b
α,β/parenrightBig
av(S74)
=1
V−e
¯h/2α2
K
eEzTr/bracketleftBig
(Sxkx+Syky)/parenleftBig
/vectork·/vectorL/parenrightBig
ˆρ(0)/bracketrightBig
.
Sincef(0)(E(0)
n) in ˆρ(0)[Eq. (S6)] does not depend on
the direction of /vectork, this expression may survive only when
the traced expression is even in components of /vectork. It thus
reduces to
ǫαβz/parenleftBig
jS,b
α,β/parenrightBig
av(S75)
=1
V−e
¯h/2α2
K
eEzTr/bracketleftBig/parenleftbig
SxLxk2
x+SyLyk2
y/parenrightbig
ˆρ(0)/bracketrightBig
.
Since the dependence on /vectorkis decoupled from the depen-
dencies on /vectorSand/vectorLas far as ˆ ρ(0)is concerned, k2
xand
k2
yin the above expression may be replaced by k2/3, and
SxLxandSyLyby/vectorS·/vectorL/3. Thus the above expression
reduces further to
ǫαβz/parenleftBig
jS,b
α,β/parenrightBig
av(S76)
=1
V−e
¯h/2α2
K
eEz2
9Tr/bracketleftBig/parenleftBig
/vectorS·/vectorL/parenrightBig
k2ˆρ(0)/bracketrightBig
.
Here/vectorS·/vectorLmay be replaced by (¯ h2/2)[J(J+1)−1·2−1
23
2],
which is ¯ h2/2 forJ= 3/2 and−¯h2forJ= 1/2. Theremaining calculation is straightforward. Generalizing to
general direction of /vectorE, one obtains
/parenleftBig
jS,b
α,β/parenrightBig
av=∓1
15π2ǫαβγEγ¯hα2
Kk5
F(S77)
forJ= 3/2 (upper sign) and J= 1/2 (lower sign).
Note that ( jS,b
α,β)avdiffers from ( jS,a
α,β)avby the factor
−3
5αK¯hk2
F/e, which is smallerthan 1 in the small /vectorklimit.
Therefore ( jS,EXTRA
α,β)avis given by
/parenleftBig
jS,EXTRA
α,β/parenrightBig
av=±2
9π2ǫαβγEγeαKk3
F/parenleftbigg
1−3
10αK¯hk2
F
e/parenrightbigg
.
(S78)
Consideringthe relationbetween ˆjS,EXTRA
α,βandˆjS,PROP
α,β
in Eq. (S61), one finally obtains
/parenleftBig
jS,PROP
α,β/parenrightBig
av=±4
9π2ǫαβγEγeαKk3
F/parenleftbigg
1−3
20αK¯hk2
F
e/parenrightbigg
,
(S79)
forJ= 3/2 (upper sign) and J= 1/2 (lower sign).
B. State change contribution
The perturbation H′
1andH′
2can modify the density
matrix ˆρ. To calculate the state change contribution
(jS,PROP
α,β)scarising from the density matrix change (in
the absence of any scattering), it is sufficient to retain
onlyˆjS,c
α,βout of the three terms for ˆjS,EXTRA
α,β[Eq. (S62)]
and calculate
(jS,c
α,β)sc= Tr/bracketleftBig
ˆjS,c
α,βˆρ(1)/bracketrightBig
, (S80)
where ˆρ(1)denotesthefirstorder(in /vectorE)changeof ˆ ρ. Here
we may ignorethe contributions from ˆjS,a
α,βandˆjS,b
α,β, since
these operators are already first order in /vectorEand generate
the second order contribution when combined with ˆ ρ(1).
BothH′
1andH′
2contribute to ˆ ρ(1). However ˆ ρ(1)
due toH′
1does not contribute to ( jS,c
α,β)scsince as far
asH0+H′
1is concerned, there is no coupling between
(/vectork,/vector r) and (/vectorL,/vectorS). Combined with the fact that ˆjS,c
α,βis
odd in/vectorLor/vectorS, this feature prohibits H′
1from generating
any contribution to ( jS,c
α,β)sc.
Below we confine ourselves to ˆ ρ(1)arising from H′
2,
which has been explicitly constructed in Sec. IB. Fol-
lowing the similar calculation procedure in Sec. IB, one
obtains
(jS,c
α,β)sc (S81)
=∓/summationdisplay
/vectork/summationdisplay
J˜z=±1/2f(0)/parenleftBig
E(0)(/vectork,J)/parenrightBig
×αK|/vectorE×/vectork|√
2
3¯h
∆E
×2Re/braceleftbigg(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleˆjS,c
α,β/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)/bracerightbigg
,9
where the upper and lower signs apply to J= 3/2 and
J= 1/2, respectively. J′= 1/2 (3/2) when J= 3/2
(1/2). ThisisthecounterpartofEq.(S25). Fromsymme-
try consideration, it can be verified that ( jS,c
α,β)scshould
be proportional to ǫαβγEγ. Also the expression for ˆjS,c
α,β
in Eq. (S65) indicates that ( jS,c
α,β)scin Eq. (S81) is of the
order of /vectorE¯hαKk5
F. Thus one finds
(jS,c
α,β)sc=ηǫαβγEγ¯hα2
Kk5
F, (S82)
whereηis a dimensionless constant. Explicit evalua-
tion of Eq. (S81) is necessary to determine η. How-
ever even without the explicit evaluation, it is evident
that (jS,c
α,β)scis smaller than ( jS,PROP
α,β)avby the factor
αK¯hk2
F/e, which is smaller than 1 in the smaller /vectorklimit.
Therefore in the small /vectorklimit, (jS,c
α,β)scis not important.
Below we demonstrate the explicit evaluate of ( jS,c
α,β)sc
to determine η. It suffices to assume /vectorE=Ezˆzand evalu-
ateǫαβz(jS,c
α,β)sc. Forthis, oneutilizes Eq. (S65) to obtain
ǫαβzˆjS,c
α,β=1
V−e
¯h/2αKαSO
2e/bracketleftbigg
−¯h2
2/parenleftBig
/vectork×/vectorL/parenrightBig
z(S83)
−Lz(/vectorS·/vectork×/vectorL)−(/vectork×/vectorL·/vectorS)Lz/bracketrightbigg
.
After some algebra, one finds
ǫαβz2Re/braceleftbigg(0)/angbracketleftBig
/vectork,J′,J˜z/vextendsingle/vextendsingle/vextendsingleˆjS,c
α,β/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)/bracerightbigg
(S84)
=1
V−e
¯h/2αKαSO
2e3√
2
2¯h3/vextendsingle/vextendsingle/vextendsingleˆz×/vectork/vextendsingle/vextendsingle/vextendsingle (S85)
The rest of calculation is straightforward and results in
(jS,c
α,β)sc=±2
45π2ǫαβγEγ¯hα2
Kk5
F.(S86)
Finally by combining with ( jS,prop
α,β)sc, one obtains
(jS,PROP
α,β)sc (S87)
=∓2
45π2ǫαβγEγeαKk3
F/parenleftbigg8
3¯h2k2
F/2m
∆E−αK¯hk2
F
e/parenrightbigg
,
forJ= 3/2 (upper sign) and J= 1/2 (lower sign).
C. Occupation change contribution
The occupation change contribution refers to the con-
tribution arising from the additional deviation of ˆ ρ
from ˆρ(0)due to the impurity scattering of infinitesimal
strength. Due to Eqs. (S61) and (S62), the calculation
of (jS,PROP
α,β)ocoverlaps a lot with that of ( jS,prop
α,β)ocand
(jS
α,β)oc. The only piece that requires additional calcula-
tion is (jS,c
α,β)oc, which is given by
(jS,c
α,β)oc= Tr/bracketleftBig
ˆjS,c
α,βˆρ(1)
oc/bracketrightBig
, (S88)where ˆρ(1)
ocdenotes the impurity scattering effect to ˆ ρ.
The perturbation H′
1does not make any contribution to
(jS,c
α,β)ocsince it does not induce any correlation among
(/vectork,/vector r) and (/vectorL,/vectorS). Below we thus consider the pertur-
bationH′
2only. Then using the expression for ˆ ρ(1)
ocin
Eq. (S32), one obtains
(jS,c
α,β)oc=/summationdisplay
nf(1)(En)(0)/an}bracketle{tn|ˆjS,c
α,β|n/an}bracketri}ht(0).(S89)
From symmetry consideration, one can verify that
(jS,c
α,β)ocshould be proportional to ǫαβγEγ. It then suf-
fices to assume /vectorE=Ezˆzand evaluate ǫαβz(jS,c
α,β)oc. For
its evaluation, one uses Eq. (S83) and also the relation,
/summationdisplay
kz/braceleftbigg(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsingle¯h2
2/parenleftBig
/vectork×/vectorL/parenrightBig/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
(S90)
+(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsingleLz/parenleftBig
/vectorS·/vectork×/vectorL/parenrightBig/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)
+(0)/angbracketleftBig
/vectork,J,J˜z/vextendsingle/vextendsingle/vextendsingle/parenleftBig
/vectork×/vectorL·/vectorS/parenrightBig
Lz/vextendsingle/vextendsingle/vextendsingle/vectork,J,J˜z/angbracketrightBig(0)/bracerightbigg
= 0,
which shows that ( jS,c
α,β)oc= 0. Finally by combining
with (jS,prop
α,β)oc, one obtains
(jS,PROP
α,β)oc=/braceleftbigg
−10
+2/bracerightbigg
×1
27π2ǫαβγEγeαKk3
F,
where the upper and lower results apply to J= 3/2 and
J= 1/2, respectively.
D. Summary
To summarize the result of this section, we obtained
jS,PROP
αβ=−2
9π2ǫαβγEγeαKk3
F (S91)
×/bracketleftbigg5
3−/parenleftbigg
2−3
10αK¯hk2
F
e/parenrightbigg
+/parenleftbigg8
15¯h2k2
F/2m
∆E−1
5αK¯hk2
F
e/parenrightbigg/bracketrightbigg
forJ= 3/2 and
jS,PROP
αβ=2
9π2ǫαβγEγeαKk3
F (S92)
×/bracketleftbigg1
3−/parenleftbigg
2−3
10αK¯hk2
F
e/parenrightbigg
+/parenleftbigg8
15¯h2k2
F/2m
∆E−1
5αK¯hk2
F
e/parenrightbigg/bracketrightbigg
forJ= 1/2. Note that jS,PROP
αβdiffers from jS
αβand
jS,prop
αβin two ways. One difference is the extra terms,
which are of order of /vectorEα2
K¯hk5
Fand thus smaller than10
other leading order terms by the factor αK¯hk2
F/e. Since
this factor approaches zero in the small /vectorkregime that
we consider, this difference is not important. The other
difference is the factor two enhancement of the anoma-
lous velocity contribution. Since this enhancement oc-curs at the leading order term of the order of /vectorEeαKk3
F,
this enhancement by factor 2 is relevant. Thus the only
important deviation of jS,PROP
αβfromjS
αβandjS,prop
αβis
the factor two enhancement of the anomalous velocity
contribution.
∗Electronic address: hwl@postech.ac.kr
†Electronic address: changyoung@yonsei.ac.kr
1J. Shi, P. Zhang, D. Xiao, and Q. Niu, Phys. Rev. Lett. 97,076604 (2006). |
1308.6349v1.Spin_orbit_coupling_and_spin_Hall_effect_for_neutral_atoms_without_spin_flips.pdf | Spin-orbit coupling and spin Hall effect for neutral atoms without spin-flips
Colin J. Kennedy, Georgios A. Siviloglou, Hirokazu Miyake, William Cody Burton, and Wolfgang Ketterle
MIT-Harvard Center for Ultracold Atoms, Research Laboratory of Electronics,
Department of Physics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139, USA
(Dated: August 8, 2018)
We propose a scheme which realizes spin-orbit coupling and the spin Hall effect for neutral atoms
in optical lattices without relying on near resonant laser light to couple different spin states. The
spin-orbit coupling is created by modifying the motion of atoms in a spin-dependent way by laser
recoil. The spin selectivity is provided by Zeeman shifts created with a magnetic field gradient.
Alternatively, a quantum spin Hamiltonian can be created by all-optical means using a period-
tripling, spin-dependent superlattice.
PACS numbers: 67.85.-d, 03.65.Vf, 03.75.Lm
Many recent advances in condensed matter physics are
related to the spin degree of freedom. The field of spin-
tronics [1], the spin Hall effect [2], and topological insu-
lators [3] all rely on the interplay between spin and mo-
tionaldegreesoffreedomprovidedbyspin-orbitcoupling.
Quantum simulations with neutral atoms have started to
implement spin-orbit coupling using Raman transitions
between different hyperfine states [4–8]. Since the Ra-
man process transfers momentum to the atom, the res-
onance frequency is Doppler sensitive, and thus couples
motion and spin.
The possibility of using spin-flip Raman processes to
create interesting gauge fields was first pointed out in
[9–11], and extended to non-Abelian gauge fields, which
imply spin-orbit coupling, in [12, 13]. With the exception
of an atom chip proposal where the spin-flips are induced
with localized microwave fields [14], all recently proposed
schemes are based on spin-flip Raman processes [8, 15–
20].
The major limitation of these Raman schemes is that
spin-flip processes are inevitably connected with heating
by spontaneous emission if they rely on spin-orbit cou-
pling in the excited state, as in alkali atoms or other
atoms with an Sorbital ground state. Since laser beams
interact with atoms via the electric dipole interaction,
they do not flip the spin. Spin-flips occur only due to
intrinsic spin-orbit interactions within the atoms; there-
fore, spin-orbit coupling by spin flip Raman processes
relies on the spin-orbit coupling withinthe atom. Since
the spontaneous emission rate and the two-photon Rabi
frequency for Raman spin-flip processes scale in the same
way with respect to the ratio of laser power to detuning,
for a given atom the coupling strength relative to the
spontaneous emission rate is fixed by the fine structure
splittingcomparedtothenaturallinewidth. Thishasnot
been a limitation for the demonstration of single-particle
or mean-field physics [4–8], but will become a severe re-
striction for many-body physics where the interactions
willintroduceasmallerenergyscaleandthereforerequire
longer lifetimes of the atomic sample. Some authors have
considered transitions involving metastable states of al-kaline earth atoms to reduce the effects of spontaneous
emission [21, 22].
Here we present a spin-orbit coupling scheme that does
not involve spin-flips, is diagonal in the spin component,
z, and corresponds to an Abelian SU(2)gauge field.
This scheme can be implemented with far-off resonant
laser beams, thus overcoming the limitationof short sam-
ple lifetimes due to spontaneous emission. In the field of
cold atoms, many discussions of spin-orbit coupling em-
phasize its close relationship to non-Abelian gauge fields
[17, 23] which are non-diagonal for any spin component
and therefore mix spin and motion in a more compli-
cated way. However, a scheme diagonal in the spin com-
ponent is sufficient for spin Hall physics and topologi-
cal insulators [24, 25], and its implementation has major
experimental advantages. In the theoretical proposals
[26, 27] and the demonstration [23] of the spin Hall effect
for quantum gases, Raman spin-flips are used to create
an Abelian gauge field diagonal with respect to one spin
component.
The physical principle of the spin-orbit coupling
scheme presented here is very different from spin-flip
schemes. It does not require any kind of spin-orbit cou-
pling within the atom. Rather, spin-dependent vector
potentials are engineered utilizing the Zeeman effect in
a magnetic field – atoms in the spin up and down states
interact with different pairs of laser beams, or differently
with the same pair, and the photon recoil changes the
atom’s motion in a spin-dependent way. This results in
spin-orbit coupling which is diagonal in the spin basis.
To begin, we summarize the relationship between spin-
orbit coupling and spin-dependent vector potentials. For
charged particles, the origin of spin-orbit coupling is
the relativistic transformation of electromagnetic fields.
Whenanelectronmovesthroughanelectricfield E, itex-
periences a magnetic field Bin its moving frame which
interacts with the spin (described by the Pauli spin
matricies). Spin-orbit coupling contributes a term pro-
portional to (pE)in the Hamiltonian. As such, an
electric field in the z-direction gives rise to the Rashba
spin-orbit coupling (p)z=xpy ypx.arXiv:1308.6349v1 [cond-mat.quant-gas] 29 Aug 20132
Assuming a 2D system confined to the x;yplane,
and an in-plane electric field, the spin-orbit interac-
tion conserves z. Following [25], a radial electric field
EE(x;y;0)leads to a spin-orbit coupling term in the
Hamiltonian of the form Ez(xpy ypx). Such a radial
field could be created by a uniformly charged cylinder,
or can be induced by applying stress to a semiconductor
sample [25]. This spin-coupling term is identical to the
Apterm for the Hamiltonian describing a spin in a
magnetic field, zB. Using the symmetric gauge for the
vector potential A=zB
2(y; x;0), one obtains a term
in the Hamiltonian proportional to zB(xpy ypx)or
equivalently to BL, where Lis the orbital angular
momentum of the atom. Therefore, this form of spin-
orbit coupling is equivalent to a spin-dependent magnetic
field which exerts opposite Lorentz forces on spin up and
down atoms. This leads to the spin Hall effect which
creates a transverse spin current and no charge or mass
currents [24, 25]. The A2term constitutes a parabolic
spin-independentpotentialwhichisirrelevantforthespin
physics discussed here.
We now present a scheme which realizes such an
Abelian gauge field and manifests itself as a spin-
dependent magnetic field. Recently, the MIT group
[28,29]andtheMunichgroup[30,31]havesuggestedand
implemented a scheme to generate synthetic magnetic
fields for neutral atoms in an optical lattice. The scheme
is based on the simple Hamiltonian for non-interacting
particles in a 2D cubic lattice,
H= X
m;n
Jx^ay
m+1;n^am;n+Jy^ay
m;n +1^am;n+h:c:
(1)
whereJx(y)describestunnelinginthe x-(y-)directionand
^ay
m;n(^am;n) is the creation (annihilation) operator of a
particle at lattice site (m;n). The setup is detailed in
[28] and summarized as follows: a linear tilt of energy
per lattice site is applied using a magnetic field gradient
in thex-direction, thus suppressing normal tunneling in
this direction. Resonant tunneling is restored with two
far-detuned Raman beams of two-photon Rabi frequency
, frequency detuning !=!1 !2, and momentum
transfer k=k1 k2. Considering only the case of reso-
nant tunneling, != =~, rapidly oscillating terms time
average out [32], yielding an effective Hamiltonian which
is time-independent [28].
H= X
m;n
Ke im;n^ay
m+1;n^am;n+J^ay
m;n +1^am;n+h:c:
(2)
This effective Hamiltonian describes charged particles
on a lattice in a magnetic field under the tight-binding
approximation [33, 34]. The gauge field arises from the
spatially-varying phase m;n=kRm;n=mkxa+nkya
whereais the lattice constant and has the form A=
~(kxx+kyy)=a^x. One can tune the flux per unit cell, ,
αk1,ω1k2,ω2
|á〉
Δ
k1,ω1k2,ω2
|â〉
Δ-αKeiφm,n
Ke-iφm,nFIG. 1. Spin-dependent tunneling in an optical lattice tilted
by a magnetic field gradient. When the two spin states have
opposite magnetic moments, then the role of absorbtion and
emission of the two photons is exchanged. The result is that
the two states have tunneling matrix elements with opposite
phases, leading to opposite synthetic magnetic fields and re-
alizing spin-orbit coupling and the quantum spin Hall effect.
for a given spin state over the full range between zero and
one by adjusting the angle between the Raman beams,
and consequently ky.
We now extend this scheme to the spin degree of free-
dom, and assume a mixture of atoms in two hyperfine
states, labeled spin up and down. If the potential en-
ergy gradient is the same for the two states, then the two
states experience the same magnetic field. This is the
situation when the tilt is provided by gravity, a scalar
AC Stark shift gradient, or a magnetic field gradient if
both states have the same magnetic moment – the phase
m;nis independent of z.
If the two states have the same value of the magnetic
moment, but opposite sign, then the potential gradient is
opposite for the two states. This can be realized by using
states of the same hyperfine level F, but with opposite
magnetic quantum number MF(e.g. in23Na or87Rb,
thejF;MFi=j2;2iandj2; 2istates), or by picking
another suitable pair of hyperfine states. In this case, for
laser-assisted tunneling between two sites mandm+ 1,
the roles of the two laser beams – absorption of a photon
versus stimulated emission of a photon – for the Raman
process are reversed as depicted in Fig. 1. Therefore, the
two states receive opposite momentum transfer, and this
sign change leads to a sign change for the enclosed phase:
m;n= (mkxa+nkya)z (3)
and also for the vector potential and the magnetic field.
The vector potential realized by this scheme:
A=~
a(kxx+kyy)^x^z (4)3
creates the spin-orbit coupling discussed in the introduc-
tion, although in a different gauge. The x-dependence in
thex-component of Ais necessary for a non-negligible
tunneling matrix element for the laser-assisted process
[28].
This system has now time reversal symmetry, in con-
trast to the system with the same synthetic magnetic
field for both states (since a magnetic field breaks time
reversal symmetry). It therefore realizes the quantized
spin Hall effect consisting of two opposite quantum Hall
phases. It is protected by a Ztopological index due to
fact thatzis conserved [24, 25].
When the values of the two magnetic moments are dif-
ferent, and the potential energy gradient is provided by
a magnetic field gradient, then the two states have differ-
ent Bloch oscillation frequencies, =h. Each state now
needs two separate Raman beams for laser-assisted tun-
neling (or they can share one beam). This implies that
the synthetic magnetic field can now be chosen to be the
same, to be opposite or to be different for the two spin
states. One option is to have zero synthetic magnetic
field for one of the states. Atoms in this state can still
tunnel along the tilt direction by using a Raman process
withouty-momentum transfer, or equivalently, by induc-
ingtunnelingthroughlatticemodulation[35]. Inthecase
of two different magnetic moments, one could also per-
form dynamic experiments, where laser parameters are
modified in such a way that one switches either suddenly
or adiabatically from the quantum Hall effect to the spin
quantum Hall effect.
An intriguing possibility is to couple the two states.
Sincezis no longer conserved, the system should be-
come a topological insulator with the Z2classification
[3, 36], provided that the coupling is done in a time-
reversal invariant way. This can be done with a term
which is not diagonal in z– ie. axpyterm – by adding
spin-flip Raman lasers to induce spin-orbit coupling, or
by driving the spin-flip transition with RF or microwave
fields. A coherent RF drive field would not be time-
reversal invariant, but it would be interesting to study
the effect of symmetry-breaking in such a state [37]. A
drive field where the phase is randomized should lead to
a time-reversal invariant Hamiltonian.
Our scheme implements the idealized scheme for a
quantum spin Hall system consisting of two opposite
quantum Hall phases. This is a starting point for break-
ing symmetries and exploring additional terms in the
Hamiltonian. Ref. [37, 38] discusses a weak quantum
spin Hall phase, induced by breaking the time-reversal
symmetry by a magnetic field - this can be achieved
by population imbalance between the two spin states.
A spin-imbalanced quantum Hall phase can turn into a
spin-filtered quantum Hall phase [37, 38] where only one
component has chiral edge states. This can be achieved
by realizing a finite synthetic magnetic field for one com-
ponent, and zero for the other. Changing the spin-orbit
|á〉
|â〉
790 nm @28.7˚Δ
Δ
Δ2ΔΔ1064 nm, kLat
kSup=kLat/3+–
2ΔA A B B C C =FIG. 2. Superlattice scheme for realizing the quantnum Hall
and quantum spin Hall effect. A superlattice with three times
the spatial period as the fundamental lattice leads to three
distinguishablesitesA,B,C.ForthequantumspinHalleffect,
the superlattice operates at a magic wavelength where the AC
Stark effect is opposite for the two spin states. For rubidium,
this is achieved at a wavelength of 790 nm.
coupling can induce topological quantum phase transi-
tions between a helical quantum spin Hall phase and
a chiral spin-imbalanced quantum Hall state. This can
probably be achieved in a population imbalanced system
by adding additional Raman spin-flip beams [37, 38].
So far, we have discussed single-particle physics.
Adding interactions, by increasing the density with
deeper lattices or through Feshbach resonances, will in-
duce interesting correlations and may lead to fractional
topological insulators [39]. Another option are spin-drag
experiments [40, 41], transport experiments where one
spin component transfers momentum to the other com-
ponent. For the situation mentioned above, where the
synthetic magnetic field is zero for one component (e.g.
spin up), a transport experiment revealing the Hall ef-
fect [42] for spin down would show a non-vanishing Hall
conductivity for spin up to due to spin drag. In addition,
one would expect that spin-exchange interactions destroy
the two opposite quantum Hall phases, and should lead
to the quantum spin Hall phase with Z2topological in-
dex.
We now present another way of realizing the physics
discussed above, using optical superlattices instead of a
potential energy gradient. This has the advantage of
purely optical control, and avoids possible heating due
to Landau-Zener tunneling [43] between Wannier Stark
states. So far, optical superlattices have allowed the ob-
servation of the ground state with staggered magnetic
flux [44], in contrast to experiments with magnetic tilts
[28, 31].
Figure 2 summarizes the new scheme. The super-
lattice has three times the period of the basic lattice,4
thus distinguishing sites A, B, C in energy. Resonant
tunneling is re-established using three pairs of Raman
beams with frequencies: !1+ AB=~,!2+ BC=~, and
!3 (AB+ BC)=2~collinear in one arm and !1,
!2, and!3collinear in another arm at an angle to the
first. Consequently, there is always the same momen-
tum transfer for tunneling in the y-direction, leading to
the same flux as the scheme with the magnetic tilt, and
Eqs. (3) and (4) apply. This is in contrast to schemes
with two distinguished sites A and B (by using internal
states [21, 32] or a superlattice [44]) which lead to a stag-
gered magnetic field. Rectification of the magnetic flux
in a staggered configuration by adding a tilt [32, 44] or
a superlattice [21] has also been proposed. In the lat-
ter scheme, this would result in four distinguishable sites
(two internal states A, B, doubled up by the superlat-
tice). Another rectification scheme uses three internal
states [45]. Our scheme avoids spin-flip transitions be-
tween internal states, and has the minimum number of
ingredients of three different sites to provide direction-
ality. Furthermore, by adjusting the spatial phase shift
between the fundamental and the superlattice, one can
choose the energy offsets AB= BC= CA=2(see
Figure 2). The scheme can then be implemented by shin-
ing Raman beams from two directions, each beam having
two frequencies.
This scheme would realize Hofstadter’s butterfly and
the quantum Hall effect. For the quantum spin Hall ef-
fect, one has to choose the superlattice laser to be at
the magic wavelength where the scalar AC Stark shift
vanishes, and only a vector AC Stark shift remains cor-
responding to a so-called fictitious magnetic field [46, 47].
By detuning the laser between the D1andD2lines, one
can achieve a pure vector AC Stark shift, which is equal
in magnitude, but opposite in sign when the atoms in the
two hypefine states have opposite magnetic moments. In
thiscase, thesuperlatticewillprovideoppositepotentials
forthetwostates, resultinginoppositemomentumtrans-
fers due to the Raman beams and opposite vector poten-
tials. The superlattice period is =(2 sin (=2)), where
is the angle between the two superlattice beams, which
is adjusted to make the superlattice period three times
the period of the basic lattice. This scheme realizes the
quantum spin Hall effect and a topological insulator with
two opposite quantum Hall phases with a purely optical
scheme and no Raman spin-flip transitions.
To replace the magnetic field gradient by a superlattice
that generates a fictitious magnetic field, the laser detun-
ing has to be on the order of the fine structure splitting,
resulting in heating due to spontaneous emission. For
atoms like rubidium, the lifetime is many seconds [46].
To be specific, we consider a low-density gas Rb atoms
in theF= 2,MF=2states in a lattice with a depth
of ten photon recoils at the wavelength of 1064 nm. A
superlattice with a lattice depth of 10 kHz is created by
interfering two laser beams at 790.0 nm of 1.0 mW oflaser power and a beam waist of 125 m. The result-
ing offset ABandACwill be approximately 4 and 8
kHz respectively, well placed in the bandgap of the basic
lattice. The spontaneous scattering rate induced by the
superlattice beams is less than 0.1 =s. Alternatively, the
superlatticeproducingthefictitiousmagneticfieldcanbe
replaced by a sinusoidal (real) magnetic field generated
by an atom chip [48].
There have been several suggestions how to detect
properties of the quantum Hall and quantum spin Hall
phases. Time-of-flight pictures will reveal the enlarged
magnetic unit cell due to the synthetic magnetic field
[44, 49–51]. Hall plateaus can be discerned in the den-
sity distribuion [52]. The Chern number of a filled band
can be measured interferometically [53] or using ballistic
expansion [54]. Topological edge states can be directly
imaged [55, 56] or detected by Bragg spectroscopy [57–
59].
Our work maps out a route towards spin-orbit cou-
pling, the spin Hall effect and topological insulators
which does not require coupling of different internal
states with spin-flipping Raman lasers. The Hamiltonian
describing the system is diagonal in the zspin com-
ponent. This follows closely the two original papers on
the spin Hall effect [24, 25]. In addition, we have pre-
sented two configurations for realizing a quantum spin
Hall Hamiltonian. The scheme with the magnetic tilt
completely avoids near resonant light, and the superlat-
tice scheme provides a purely optical approach.
This work was supported by the NSF through the Cen-
ter of Ultracold Atoms, by NSF award PHY-0969731,
under ARO Grant No. W911NF-13-1-0031 with funds
from the DARPA OLE program, and by ONR. This work
was completed at the Aspen Center for Physics (sup-
ported in part by the National Science Foundation under
Grant No. PHYS-1066293), and insightful discussions
with Hui Zhai, Jason Ho, and Nigel Cooper are acknowl-
edged. We thank Wujie Huang for a critical reading of
the manuscript.
After most of this work was completed [60] we became
aware of similar work carried out in the group of I. Bloch
in Munich [31, 61].
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1101.4656v3.Identifying_spin_triplet_pairing_in_spin_orbit_coupled_multi_band_superconductors.pdf | arXiv:1101.4656v3 [cond-mat.supr-con] 3 May 2012Identifying spin-triplet pairing in spin-orbit coupled mu lti-band
superconductors
Christoph M. Puetter1andHae-Young Kee1,2 (a)
1Department of Physics, University of Toronto, Toronto, Ont ario M5S 1A7, Canada
2Canadian Institute for Advanced Research, Quantum Materia ls Program, Toronto, Ontario M5G 1Z8, Canada
PACS74.20.-z – Theories and models of superconducting state
PACS74.20.Rp – Pairing symmetries (other than s-wave)
PACS74.70.Pq – Ruthenates
Abstract – We investigate the combined effect of Hund’s and spin-orbit (SO) coupling on su-
perconductivity in multi-orbital systems. Hund’s interac tion leads to orbital-singlet spin-triplet
superconductivity, where the Cooper pair wave function is a ntisymmetric under the exchange of
two orbitals. We identify three d-vectors describing even-parity orbital-singlet spin-tr iplet pairings
among t 2g-orbitals, and find that the three d-vectors are mutually orthogonal to each other. SO
coupling further assists pair formation, pins the orientat ion of the d-vector triad, and induces spin-
singlet pairings with a relative phase difference of π/2. In the band basis the pseudospin d-vectors
are aligned along the z-axis and correspond to momentum-dependent inter- and intr a-band pair-
ings. We discuss quasiparticle dispersion, magnetic respo nse, collective modes, and experimental
consequences in light of the superconductor Sr 2RuO4.
Introduction. – Since its inception, standard
Bardeen-Cooper-Schrieffer (BCS) theory has been con-
sidered a classic example for a collective phase emerging
from quantum many body effects. However, the discovery
of unconventional superconducting phases near antiferro-
magnetic order in heavy fermion compounds [1,2], organic
materials [3], and, most recently, Fe-pnictides [4] have ex-
posed the limits of a single-band BCS formulation. The
origin and nature of superconductivity in complex mate-
rials where multiple bands cross the Fermi level therefore
remains a field of active research, harbouring intriguing
challenges and mysteries.
In particular, when the electronic structure near the
Fermi energy is composed of different orbitals and spins
mixed via spin-orbit (SO) coupling, a pairing symmetry
analysis could be non-trivial. For example, a local micro-
scopic interaction such as Hund’s coupling may naturally
favour inter-orbital spin-triplet pairing between electrons.
However,whenorbitalandspinfluctuationsaresignificant
due to inter-orbital hopping and SO interaction, pairing
in definite orbital and spin channels ( e.g., spin-singlet or
-triplet pairing between electron in orbitals aandb) is
not well defined. Equivalently, from a Bloch band per-
(a)E-mail:hykee@physics.utoronto.caspective, where the kinetic Hamiltonian including SO ef-
fectsisdiagonal,thedecouplingofthemicroscopicinterac-
tion effectively leads to intra- and inter-band pairing with
pseudospin-singlet and/or -triplet character.
Below we present a systematic study of how SO and
Hund’s couplings jointly give rise to superconductivity in
t2g(i.e., dyz, dxz, and d xy) orbital systems. Our find-
ings may apply to a number of multi-orbital d-subshell
superconductors. To be specific we base our quantitative
considerations on the proposed chiral spin-triplet super-
conductor Sr 2RuO4. Here, despite intense investigation
for more than a decade, a clear picture for the pairing
symmetry, the pairing mechanism and the relevant bands
involved that is consistent with all experimental observa-
tions has not yet emerged [5,6].
The paper is organized as follows. In the second sec-
tion we discuss Cooper pairing in multi-orbital systems.
We find that superconductivity from local Hund’s ex-
change can naturally be characterized by three mutually
orthogonal d-vectors each describing inter-orbital even-
parity spin-triplet pairing. Wethen showhowSOcoupling
pins the orientation of the d-vector triad and induces and
enhances pairing via coupling to spin-singlet pairing order
parameters with a fixed relative phase difference of π/2.
In the third section, we map these local pairing order pa-
p-1Christoph M. Puetter and Hae-Young Kee
rameters, defined in an orbital and spin basis, to inter-
and intra-band pairing in the Bloch band basis. Pairing
in the Bloch bands has a strong momentum dependence
and the magnitude and direction of the d-vectors depend
on the orbital composition at each k-point. In the fourth
section, we present the complete self-consistent mean-field
(MF) results involving 9 complex order parameters using
band structure parameters that reproduce the Fermi sur-
face (FS) reported on Sr 2RuO4. In addition, the resulting
anisotropicquasiparticle(QP)dispersion,themagneticre-
sponse and the critical pairing strengths in the presence of
SO coupling are considered. We summarize our findings
and discuss the relevance for SO-coupled d-orbital super-
conductors such as Sr 2RuO4in the last section.
Pairing in SO coupled t 2gsystems via Hund’s in-
teraction. – For multi-orbital 3d-subshell systems such
astheFe-pnictides, itwasrecognizedthatHund’scoupling
(interaction strength denoted by J) is as important as on-
site Coulomb repulsion ( U) [7,8], while SO coupling (2 λ)
is relatively weak [9]. In contrast, recent x-ray measure-
ments on 5d transition metal compounds such as Ir-based
oxide materials found that the SO interaction of 0.6 eV
is roughly comparable to the on-site Coulomb energy [10],
suggesting that SO interaction is larger than Hund’s ex-
change (since J < U). Given that the effective pairing
interaction in the spin-triplet channel arising from Hund’s
couplingandinter-orbitalHubbardrepulsion( V=U−2J)
scales as V−J=U−3J(see below), we therefore ex-
pect that for 4d-subshell materials such as Sr 2RuO4both
SO and spin-triplet pairing interactions are intermediate
in strength and of similar magnitude [11–17]. Since nei-
ther interaction is negligible nor dominant, we treat both
on an equal footing in the present study.
While on-site Hund’s and further neighbor exchange in-
teractions have been recognized to be important for spin-
triplet pairing [7,18–21], the combined effect of SO and
Hund’s couplings on inter-orbital spin-triplet pairing has
not been investigated in t 2g-orbital systems. To under-
stand superconductivity in SO coupled t 2g-orbital sys-
tems,weconsideragenericHamiltonian H=Hkin+HSO+
Hintconsisting of kinetic, SO, and local Kanamori inter-
action terms. In this section we leave the kinetic Hamil-
tonianHkinunspecified and focus on the pairing proper-
ties arising from the interplay of the atomic SO coupling
HSO= 2λ/summationtext
iLi·Siand the local interaction, which, pro-
jected on the t 2gorbitals, are given by
HSO=iλ/summationdisplay
i/summationdisplay
ablǫablca†
iσcb
iσ′ˆσl
σσ′, (1)
Hint=U
2/summationdisplay
i,aca†
iσca†
iσ′ca
iσ′ca
iσ+V
2/summationdisplay
i,a/negationslash=bca†
iσcb†
iσ′cb
iσ′ca
iσ
+J
2/summationdisplay
i,a/negationslash=bca†
iσcb†
iσ′ca
iσ′cb
iσ+J′
2/summationdisplay
i,a/negationslash=bca†
iσca†
iσ′cb
iσ′cb
iσ.
(2)
Here and in the following, summation over repeated spin
Fig. 1: (Color online) The orbital-singlet spin-triplet d-vectors
form a triad whose orientation is pinned along ˆx,ˆy, andˆz(or
−ˆx,−ˆy, and−ˆz) in the presence of SO coupling. See main
text for details.
indicesσ,σ′=↑,↓is implied while the indices a,b∈
{yz,xz,xy }belong to an ordered set of t2g-orbitals. Fur-
thermore, ˆ σlstands for Pauli matrices, ca†
iσcreates an elec-
tron on site iin orbital awith spin σ, andǫabldenotes
the totally antisymmetric rank-3tensor. For transparency
we have also introduced separate interaction strengths
for Hund’s coupling ( J) and pair hopping ( J′), although
J=J′at the atomic level.
Let us apply a MF approach to study the particle-
particle instabilities of the microscopic interaction Hint
using the following zero momentum pairing channels
ˆ∆s
a/b=1
4N/summationdisplay
k[iˆσy]σσ′(ca
kσcb
−kσ′+cb
kσca
−kσ′),(3)
ˆdl
a/b=1
4N/summationdisplay
k[iˆσyˆσl]σσ′(ca
kσcb
−kσ′−cb
kσca
−kσ′),(4)
whereNis the number of kpoints. Here, ∆s
a/b=
/an}bracketle{tˆ∆s
a/b/an}bracketri}ht(= ∆s
b/a) stands for intra- ( a=b) and inter-
orbital ( a/ne}ationslash=b) spin-singlet pairing, which is even un-
der the exchange of orbital quantum numbers ( i.e.they
form “orbital triplets”). The vector order parameter
da/b= (/an}bracketle{tˆdx
a/b/an}bracketri}ht,/an}bracketle{tˆdy
a/b/an}bracketri}ht,/an}bracketle{tˆdz
a/b/an}bracketri}ht)(=−db/a)ontheotherhand
parametrizes inter-orbital ( a/ne}ationslash=b) spin-triplet pairing con-
sistent with the usual d-vector notation where i(d·ˆσ)ˆσy
describes the spin-triplet pairing gap [2,22]. Note that
da/bis odd under orbital exchange, which is characteristic
ofan“orbitalsinglet”(while da/a= 0). Note alsothat the
above order parameters are all even under a parity trans-
formationas they are locallydefined; this feature differs in
particular from conventional odd-parity spin-triplet pair-
ing where orbital degrees of freedom are absent.
Using the above pairing channels the interaction Hamil-
tonian takes the form
Hint→UN/summationdisplay
aˆ∆s†
a/aˆ∆s
a/a+(V−J)N/summationdisplay
a,b,lˆdl†
a/bˆdl
a/b
+J′N/summationdisplay
a/negationslash=bˆ∆s†
a/aˆ∆s
b/b+(V+J)N/summationdisplay
a/negationslash=bˆ∆s†
a/bˆ∆s
a/b,(5)
where it is clear that only Hund’s coupling can give rise
to an instability in a spin-triplet channel [7,19]. We thus
p-2Identifying spin-triplet pairing in spin-orbit coupled multi-band super conductors
concentrate on the effective pairing interaction
H′
int= (U−3J)N/summationdisplay
a,b,lˆdl†
a/bˆdl
a/b (6)
in the attractive regime U/3< J(< U). In gen-
eral, orbital-singlet spin-triplet pairing can also induce
spin-singlet pairing so that the remaining terms in Eq.
(5) would hamper spin-singlet pairing. However, we as-
sume that their effect is negligible to keep the follow-
ing self-consistent calculations feasible, and since the in-
duced spin-singlet pairing amplitudes are for the most
part smaller than the spin-triplet pairing amplitudes (see
below). For notational clarity we label in the follow-
ing inter-orbital pairing only by the three combinations
a/b=xz/xy,yz/xy,yz/xz .
To understand the effect of SO interaction, let us re-
mark on pairing in the absence of SO coupling first.
In the case of the layered compound considered below
(and for a rather large parameter range) the three spin-
triplet d-vectors dxz/xy,dyz/xy, anddyz/xzform a triad
of mutually orthogonal vectors with an arbitrary orien-
tation and chirality in spin space, and no relative com-
plex phase difference (hence preserving time reversal sym-
metry (TRS)). This can be understood by analyzing the
Ginzburg-Landau (GL) free energy, which without SO
coupling is given by
F ∼/summationdisplay
ν/bracketleftbig
Aν|dν|2+B(1)
ν(dν·d∗
ν)2+B(2)
ν|dν·dν|2/bracketrightbig
+/summationdisplay
ν/negationslash=κ/bracketleftbig
C(1)
νκ(dν·dν)(dκ·dκ)∗+C(2)
νκ|dν|2|dκ|2(7)
+C(3)
νκ|dν·dκ|2+C(4)
νκ|dν·d∗
κ|2+C(5)
νκ(dν·d∗
κ)2/bracketrightbig
up to fourth order, by analogy to He-3 [23]. Here ν,κ
stand for orbital pairs a/b, while the (real) quartic mix-
ing parameters obey C(i)
νκ=C(i)
κνand the asymmetry
between in-plane and out-of-plane orbitals due to e.g.
inter-orbital hopping is reflected in distinct coefficients
(Ayz/xz/ne}ationslash=Ayz/xy=Axz/xy, etc.). This form is dictated
by gauge symmetry, SU(2) spin rotationalsymmetry, time
reversal symmetry and the underlying lattice symmetries,
and shows that the C(3)
νκandC(4)
νκterms are sensitive to
the relative orientation of the d-vectors, whereas the C(1)
νκ
andC(5)
νκcontributions additionally depend on their rela-
tive complex phases.
However, once SO coupling is included, dxz/xy,
dyz/xy, anddyz/xzare pinned along x,y, andz
directions, respectively, as shown in fig. 1. In-
version/time reversal symmetry on the other hand
is still preserved and reflected in the degeneracy of
the orientations/chiralities {dxz/xy,dyz/xy,dyz/xz}and
{−dxz/xy,−dyz/xy,−dyz/xz}. The pinning of the d-
vectors occurs due to additional terms in the free en-
ergy such as ∼a(1)|dz
yz/xz|2+a(2)/bracketleftbig
|dz
yz/xy|2+|dz
xz/xy|2/bracketrightbig
+
b(1)/bracketleftbig
|dx
yz/xz|2+|dy
yz/xz|2/bracketrightbig
+b(2)/bracketleftbig
|dx
xz/xy|2+|dy
yz/xy|2/bracketrightbig
+c(1)/bracketleftbig
dx
yz/xy(dy
xz/xy)∗+dy
yz/xy(dx
xz/xy)∗+c.c./bracketrightbig
+···, where
the expansion parameters depend on the SO coupling
strength, naively suggesting that a(1),a(2)< b(1),b(2),c(1),
etc.1SO interaction furthermore leads to a linear cou-
pling between a particular component of (inter-orbital)
spin-triplet pairing and (intra-orbital) spin-singlet pair-
ing. For example, writing SO coupling between yzandxz
orbitals in the form of −iλ[ˆσz]σσ′(cyz†
kσcxz
kσ′−cxz†
kσcyz
kσ′) the
following linear coupling is allowed in the GL free energy:
−i λ[ˆσz]σσ′/an}bracketle{tcyz†
kσcxz
kσ′−cxz†
kσcyz
kσ′/an}bracketri}ht (8)
×[iˆσyˆσz]σσ′/an}bracketle{tcyz
kσcxz
−kσ′−cxz
kσcyz
−kσ′/an}bracketri}ht
×/parenleftBig
[iˆσy]σσ′/an}bracketle{tcyz†
kσcyz†
−kσ′/an}bracketri}ht+[iˆσy]σσ′/an}bracketle{tcxz†
kσcxz†
−kσ′/an}bracketri}ht/parenrightBig
→iλdz
yz/xz/parenleftBig
∆s
yz/yz+∆s
xz/xz/parenrightBig∗
+c.c. (9)
Note that dyz/xzprefers the z-direction by coupling to
spin-singlet pairing with a relative phase difference of
±π/2 depending on the sign of λ. This is consistent
with our findings below that the spin-triplet order param-
eters are purely real while the spin-singlet amplitudes are
purely imaginary. A similar analysis can be carried out
fordx
xz/xyanddy
yz/xy. The overall order parameter for
yzandxzorbitals then is dz
xz/yz+i(∆s
xz/xz+ ∆s
yz/yz).
Since the relative phase between the orbital-triplet spin-
singlet and the orbital-singlet spin-triplet order param-
eters is fixed, there should be a collective mode rep-
resenting a resonance of supercurrent flow between the
coupled order parameters with an energy scale of order
∼/radicalBig
|dz
a/b|2+|∆s
a/a|2+|∆s
b/b|2.
Note that the above result is fundamentally different
from similar two orbital models, which lead to a single
orbital-singletspin-triplet d-vector[19,21,24]. Thepresent
model is also distinguished from other models where the
momentum dependence in the band pairing usually orig-
inates from nonlocal momentum dependent interactions
[18], whereas here it arises from spin and orbital mixing
in the Bloch bands as described next.
Momentum-dependent pairing in the Bloch
bands. – Despite having uniform pairing amplitudes
dyz/xz,dyz/xy,dxz/xy,∆s
yz/yz,...thecorrespondinginter-
and intra-band pairings in the Bloch band basis (now car-
rying band and pseudospin quantum numbers – η,ρ=
α,β,γands=±) acquire a strong momentum depen-
dence due to the mixing of orbitals through hopping and
SO coupling. To understand how the above local pairing
in the orbital and spin basis corresponds to pairing in the
Blochbandbasis,letusintroducethekineticHamiltonian.
The most generic kinetic Hamiltonian for t 2gorbitals in a
1Analyzing the energetics of a corresponding two orbital mod el
one can indeed show that SO interaction tends to stabilize e.g.the
dz
yz/xz-component over dx
yz/xzordy
yz/xz.
p-3Christoph M. Puetter and Hae-Young Kee
(b)+ −k −|<ξ ξ >|α γ
k+ −k −|<ξ ξ >|α β
k+ −k −|<ξ ξ >|γ β
k+ −k −|<ξ ξ >|α α
k+ −k −|<ξ ξ >|γ γ
k+ −k −|<ξ ξ >|β β
(a)
k
Fig. 2: (Color online) Momentum-resolved pairing amplitud es
in the Bloch band basis for 3 J−U= 0.9 andλ= 0.15. Panel
(a) and (b) represent inter- and intra-band pairing, respec -
tively. The grey lines indicate the β,γ, andαFS sheets (from
inside to outside). Note that pairing from Hund’s coupling
preferentially involves electronic states near the FS shee ts and
that the intra-band pairing amplitudes are about one order o f
magnitude larger than inter-band pairing amplitudes.
single layer perovskite structure has the form
Hkin+HSO=/summationdisplay
k,σC†
kσ
εyz
kε1d
k+iλ−λ
ε1d
k−iλ εxz
kiλ
−λ−iλ εxy
k
Ckσ,(10)
whereC†
kσ= (cyz†
kσ,cxz†
kσ,cxy†
k−σ) and the dispersions
areεyz/xz
k=−2t1cosky/x−2t2coskx/y−µ1,εxy
k=
−2t3/parenleftbig
coskx+ cosky/parenrightbig
−4t4coskxcosky−µ2, andε1d
k=
−4t5sinkxsinky. For the MF calculation below we have
chosen the parameters t1= 0.5,t2= 0.05,t3= 0.5,
t4= 0.2,t5= 0.05,µ1= 0.55, and µ2= 0.65 (all en-
ergies here and in the following are expressed in units of
2t1= 1.0). The underlying FS obtained from diagonaliz-
ingHkinwith SO coupling strength λ= 0.15 is shown in
fig. 2 along with momentum-dependent band pairing am-
plitudes. The FS agrees well with first principles calcula-
tions[14]andthe experimentallymeasuredFS ofSr 2RuO4
[17,25,26], consisting of three bands labelled α,β, andγ.
In the presence of SO coupling the bands are mix-
tures of all three orbitals and different spins, e.g.ξη
k+=
˜fη
kcxz
k↑+ ˜gη
kcyz
k↑+˜hη
kcxy
k↓(η=α,β,γ). Hence consider-
ing inter- and intra-band pairing amplitudes in the band
basis, it is clear that the x- andy-components of the
inter-band pseudospin-triplets such as /an}bracketle{tξη
k±ξρ
−k±/an}bracketri}htvanish,
since/an}bracketle{tdxz
k↑dyz
−k↑/an}bracketri}ht,/an}bracketle{tdxz
k↑dxy
−k↓/an}bracketri}ht, and/an}bracketle{tdyz
k↑dxy
−k↓/an}bracketri}htamplitudes are
zero (similarly for ↑↔↓). Thus only finite z-components
of the three inter-band pseudospin-triplet d-vectors and
inter-band pseudospin-singlet order parameters (such as
/an}bracketle{tξη
k+ξρ
−k−±ξρ
k+ξη
−k−/an}bracketri}ht) can appear. Figure 2 reveals that
intra-band pairing is strongest and sharply peaked around
the FS due to the mixing of all orbitals via SO interac-
tion andinter-orbitalhopping, and the ideal conditionsfor
zero-momentum pairing. Inter-band pairing in contrast is
about an order of magnitude weaker and, in particular for0.5 1 1.5
3J-U00.05
|∆s
xy/xy|00.02
|∆s
yz/yz|=|∆s
xz/xz|
0.5 1 1.5
3J-U00.1|dyz/xz|00.10.2|dxz/xy|=|dyz/xy|
λ=0
0.075
0.15
0.225
0.3
Fig. 3: (Color online) MF solutions for different SO coupling
strengths for the Sr 2RuO4based band structure. Orbital-
singlet spin-triplet pairing dxz/xy,dyz/xy, anddyz/xz(purely
real) induces finite intra-orbital spin-singlet pairing ∆s
yz/yz,
∆s
xz/xz, and ∆s
xy/xy(purely imaginary). We also checked for
induced inter-orbital spin-singlet pairing amplitudes, w hich,
however, vanish.
/an}bracketle{tξγ
k+ξβ
−k−/an}bracketri}ht, more spreadout in momentum space, marking
Bloch band states that are energetically still close enough
to the FS to participate significantly in pairing.
This analysis demonstrates that inter-orbital pairing
arising from Hund’s interaction leads to k-dependent
inter- and intra-band pairing in pseudospin-singlet and
and pseudospin-triplet (z component only) channels. Fur-
thermore, the pairing instability occurs simultaneously
within and between all bands ratherthan in a singleactive
band with superconductivity leaking into passive bands
through, e.g., pair hopping. The role of intra-band spin-
triplet pairing between αandβbands in multi-orbital su-
perconductors like Sr 2RuO4has also been the focus of re-
cent studies, where the inter-band order parameter, how-
ever, breaks TRS [27] and an intrinsic anomalous Hall
effect can contribute significantly to a large TRS breaking
signal in Kerr rotation experiments [28,29].
Pairing transition, QP dispersion, and magnetic
response. – For concreteness we study the effect of SO
coupling on spin-triplet pairing originating from Hund’s
interaction, including the QP dispersion and the magnetic
response. As discussed in the previous sections the quali-
tative results are generic for SO coupled t2g-bands (or p-
orbital systems) and can be applied to specific materials
suchasthesinglelayerruthenate[5,6]andtheFe-pnictides
[7,30] using the appropriate band structure.
Using the kinetic Hamiltonian of eq. (10) with a pa-
rameter choice mimicking the single layer ruthenate band
structure, the MF solutions for various λare displayed in
fig. 3. As one can see, in the absence of SO interaction
an orbital-singlet spin-triplet pairing instability develops
at a large coupling strength 3 J−U/greaterorsimilar1.0 fordxz/xyand
dyz/xy. Although numerically difficult to resolve, we ex-
pect that dyz/xzand the intra-orbital spin-singlet order
parameters simultaneously become finite through quartic
or higher order couplings in the Landau free energy ex-
pansion. While the magnitudes of the order parameters
depend on the details of the band structure, a robust fea-
p-4Identifying spin-triplet pairing in spin-orbit coupled multi-band super conductors
Γ X M Γ-2-1012DOS (arb. units) -0.200.2 E-µ
ΓM
X(a) (b)
(c)
Fig. 4: (Color online) QP bands for 3 J−U= 0.9 andλ= 0.15.
Panel (a) is a magnification of panel (c) about the Fermi level ,
revealing the gaps opening up on the FS sheets. Panel (b)
shows the DOS and the QP gap near the Fermi level.
0 0.002 0.004 0.00600.010.02
Mz
<Si, z><Li, z>B || z
λ=0.075no pairing
with pairing
0 0.002 0.004 0.00600.010.02B || x
λ=0.075 Mx
<Li, x>
<Si, x>
0 0.002 0.004 0.006
B00.010.02B || z
λ=0.15 Mz
<Si, z><Li, z>
0 0.002 0.004 0.006
B00.010.02
Mx
<Li, x>
<Si, x>B || x
λ=0.15
Fig. 5: (Color online) Magnetization parallel to the applie d
magnetic field Bforλ= 0.075 (top)and0 .15 (bottom) andtwo
field orientations at 3 J−U= 0.9. The solid lines represent to-
tal magnetization, dashed lines stand for orbital contribu tion,
and dash-dotted lines for spin magnetization. For sake of co m-
parison the magnetic response both in the presence (orange)
and in the absence (grey) of superconductivity is displayed . (B
is expressed in units of 2 t1= 1.)
ture is that finite SO coupling drastically reduces the crit-
ical pairing strength. This reduction is mostly facilitated
by the additional hybridization provided by HSO, which
helps to overcome the momentum mismatch between or-
bitals/bands near the Fermi level. On the other hand the
same mechanism can have a slightly detrimental effect at
larger 3J−U, where the ideal inter-orbital pairing condi-
tions along the diagonals are weakened by the additional
hybridization. One may also wonder if the BogoliubovQP
dispersionshaveanisotropicgaps. TheresultingQPbands
are shown in fig. 4 and are fully gapped with a fourfold
symmetric gap modulation in kspace, even though the
gap minima are tiny.
Note that the present superconducting state does not
break TRS. The magnetic response is a combination of
paramagnetic (spin-triplet) and spin-singlet behaviours,
with a slightly larger out-of-plane than in-plane total
magnetic susceptibility as shown in fig. 5, where M=
/an}bracketle{tLi/an}bracketri}ht+ 2/an}bracketle{tSi/an}bracketri}htis the total magnetization including orbital
and spin contributions and HB=B·/summationtext
i(Li+ 2Si) cou-ples the orbital and spin degrees of freedom to the exter-
nal field B. Both orbital and spin expectation values are
finite with roughly equal contribution to the total mag-
netization. For comparison, the normal state magnetiza-
tions are also shown in fig. 5 and are larger than in the
superconducting state, as expected for a combination of
spin-singlet and -triplet pairing in the presence of SO in-
teraction. In particular, note that the spin magnetization
changes drastically in the superconducting state with in-
creasing λ. In general,the magnitudeofthe d-vectors,and
thus the magnetic response, can be modified by changing
the size of the FS sheets. For instance a larger overlap
between yz and xy dominated portions of the FS would
enhance dyz/xycompared to dyz/xzanddxz/xy. The spin
susceptibility then would be mostly dominated by dyz/xy,
a situation which may be facilitated by applying uniaxial
pressure.
Discussion and summary. – Given that we based
our MF study on the Sr 2RuO4compound to illustrate the
effect of SO interaction on pairing, let us comment on the
compatibility and the limitations of our results with what
is known about the superconducting state in Sr 2RuO4[5,
6]. Based on the QP gap variation along the FS sheets,
one expects that this modulation may also be reflected
in orientation sensitive specific heat measurements. Such
magnetic field dependent specific heat measurements on
Sr2RuO4have indeed been carried out [31,32], but the
interpretation of the experimental results is controversial,
making alink to ourQPdispersiondifficult. However,due
to the nature of inter-band pairing, the superconducting
state presented here is sensitive to any kind of impurities
associated with inter-band scattering, which is consistent
with the phenomena observed in Sr 2RuO4.
Our result on the magnetization indicates that the spin-
susceptibility is finite and different for in-plane and out-
of-plane magnetic field orientations in both the normal
and the superconducting state, as reported on Sr 2RuO4.
Yet below Tcthe in-plane and out-of plane susceptibilities
decrease, which is in contrast to NMR Knight shift mea-
surements [33,34], which revealed that a change in the
spin-response across Tcis absent for any field orientation.
This behaviourdiffersalsofromthe responseexpected ofa
chiralp+ipsuperconductor, where the spin-susceptibility
decreasesforfielddirectionsperpendiculartothe a-bplane
but remains constant for parallel orientations. While the
amountofchangein the presentmodel depends sensitively
on the SO interaction strength, as shown in fig. 5, the
question also arises as to how orbital and spin contribu-
tions were separated to obtain the Knight shift data when
SO interaction is significant. Besides this, we note that
the magnetic field effect on vortices will be highly non-
trivial as well, as it involves competition between various
types of vortices including half-quantum vortices [35,36]
in the presence of moderate SO coupling.
Finally, the lack of TRS breakingis compatible with the
absence of chiral supercurrents as observed in scanning
p-5Christoph M. Puetter and Hae-Young Kee
Hall probe and scanning SQUID measurements [37,38].
However, this contrasts with another proposal that the
chiral states due to p+ippairing on αandβbands cancel
each other leading to a topologically trivial superconduc-
tor [27]. It also contradicts Kerr rotation and µSR mea-
surements which have been interpreted in favour of TRS
breaking [39,40]. The issue as to whether TRS is broken
or not is not yet resolved in the experimental commu-
nity. While the current study supports a non-TRS break-
ing state, it can be modified by goingbeyondlocal interac-
tions. Anaturalextensionwouldbe toinclude theeffect of
further neighbour ferromagneticinteractionssuch as those
discussed by Ng and Sigrist [18], which could lead to a
small admixture of odd parity pairing with broken TRS
in addition to the pairingfound hereand which may be re-
sponsible for the broken TRS signaturesfound in µSR and
Kerr experiments [39,40]. Another possibility is a finite-
momentum pairing state such as a FFLO (Fulde-Ferrell-
Larkin-Ovchinnikov) state [41,42]. It is plausible that a
FFLO state between different bands can be stabilized over
the inter-band pseudospin-triplet pairing. These studies,
andmoredefinitepredictionsforSr 2RuO4orotherspecific
materials, however, go beyond the scope of the current 9
complex order parameter minimization and require more
detailed work.
In summary, we studied the combined effect of Hund’s
and SO coupling on t 2gorbital systems. Three orbital-
singlet spin-triplet pairings were found to form an or-
thogonal d-vector triad. A linear coupling between even-
parity inter-orbital spin-triplet and even-parity intra-
orbital spin-singlet pairings was allowed due to SO inter-
action, determining the orientation of the three d-vectors
and giving rise to a relative phase difference of π/2 be-
tween spin-singlet and spin-triplet order parameters. We
also showed that inter-orbital spin-triplet pairing in the
orbital basis corresponds to ever-parity inter- and intra-
band pairing in the Bloch band basis, and discussed how
the pairing strength varies within the Bloch bands. We
further found that SO coupling assists Hund’s coupling
driven pairing, which generally leads to an anisotropic QP
gap and an orbital dependent magnetic response.
∗∗∗
WethankS.R.Julian, A.Paramekanti,Y.-J.Kim,K.S.
Burch, and C. Kallin for useful discussions. HYK thanks
the hospitality of the MPI-PKS, Dresden, Germany where
a part of this work was carried out. This work was sup-
ported by the NSERC of Canada and Canada Research
Chair.
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p-6 |
1312.5809v1.Effects_of_the_spin_orbital_coupling_on_the_vacancy_induced_magnetism_on_the_honeycomb_lattice.pdf | arXiv:1312.5809v1 [cond-mat.str-el] 20 Dec 2013Effects of the spin-orbital coupling on the vacancy-induced magnetism on the
honeycomb lattice
Weng-Hang Leong, Shun-Li Yu, and Jian-Xin Li
National Laboratory of Solid State Microstructure and Depa rtment of Physics, Nanjing University, Nanjing 210093, Chi na
(Dated: October 7, 2018)
The local magnetism induced by vacancies in the presence of t he spin-orbital interaction is in-
vestigated based on the half-filled Kane-Mele-Hubbard mode l on the honeycomb lattice. Using the
self-consistent mean-field theory, we find that the spin-orb ital coupling will enhance the localization
of the spin moments near a single vacancy. We further study th e magnetic structures along the
zigzag edges formed by a chain of vacancies. We find that the sp in-orbital coupling tends to sup-
press the counter-polarized ferrimagnetic order on the upp er and lower edges, because of the open
of the spin-orbital gap. As a result, in the case of the balanc e number of sublattices, it will suppress
completely this kind of ferrimagnetic order. But, for the im balance case, a ferrimagnetic order along
both edges exists because additional zero modes will not be a ffected by the spin-orbital coupling.
I. INTRODUCTION
Graphene and related nanostructured materials have
attractedmuchinterestin solidstatephysicsrecentlydue
to their bidimensional character and a host of peculiar
properties1. Among them, the investigation of the mag-
netic properties in graphene is one of the fascinating top-
ics, as no dandfelements are necessaryin the induction
ofmagnetism in comparisonwith the usual magnetic ma-
terials. Theoretical predictions and experimental investi-
gations have revealed that a nonmagnetic defect such as
animpurity oravacancycan induce the non-triviallocal-
ized magnetism2–6. Similarly, a random arrangement of
a large number of vacancies which are generated by the
high-dose exposure of graphene to strong electron irradi-
ation7can also induce magnetism theoretically8. These
studies not only have the fundamental importance, but
also open a door for the possibility of application in new
technologies for designing nanoscale magnetic and spin
electronic devices.
On the other hand, the topological insulating elec-
tronic phases driven by the spin-orbital (SO) interaction
have also attracted much interest recently. The Kane-
Mele model for the topological band insulator is defined
on the honeycomb lattice9,10which is the same lattice
structure as graphene. Possible realization of an appre-
ciable SO coupling in the honeycomb lattice includes the
cold fermionic atoms trapped in an extraordinary optical
lattice11, the transition-metal oxide Na 2IrO312and the
ternaty compounds such as LiAuSe and KHgSb13. Topo-
logical band insulator has a nontrivial topological order
andexhibitsabulkenergygapwithgapless,helicalstates
at the edge14–16. These edge states are protected by the
time reversal symmetry and are robust with respect to
the time-reversal symmetric perturbations, such as non-
magnetic impurities. It is shown that a vacancy, acting
as a minimal circular inner edge, will induce novel time-
reversal invariant bound states in the band gap of the
topological insulator17–19. Theoretically, it is also shown
that the SO coupling suppresses the edge magnetism in-
duced in the zigzag ribbon of the honeycomb lattice inthe presence of electron-electron interactions20. Thus, it
is expected that the SO coupling would also affect the
local magnetism in the bulk induced by vacancies.
In this paper, we study theoretically the effects of the
SO coupling on the local magnetism induced by a sin-
gle and a multi-site vacancy on the honeycomb lattice,
based on the Kane-Mele-Hubbard model where both the
SO coupling and the Hubbard interaction between elec-
trons are taken into consideration. This model has been
extensively studied to explore the effect of the strong
correlation on the topological insulators21–27. Making
use of the self-consistent mean field approximation, we
calculate the local spin moments and their distribution
around the vacancies. For a single vacancy, we find that
the main effect of the SO coupling is to localize the spin
moments to be near the vacancy, so that it will enhance
the local spin moments. For a large stripe vacancy by
taking out a chain of sites from the lattice, we find that
the SO coupling tends to suppress the counter-polarized
ferrimagnetic order induced along the zigzag edges, be-
cause of the open of the SO gap. As a result, in the case
of the balance number of sublattices (with even number
of vacancies), the SO coupling will suppress completely
the counter-polarized ferrimagnetic order along the up-
per and lower edges. While, in the case of the imbalance
number of sublattices (with odd number of vacancies), a
ferrimagneticorder along both edges exists because addi-
tionalzeromodeswill notbe affectedbythe SOcoupling.
Wewillintroducethemodelandthemethodoftheself-
consistent mean-field approximation in Sec.II. In Sec.III
and IV, we present the results for a single vacancy and a
multi-site vacancy, respectively. Finally, a briefsummary
will be given in Sec.V.
II. MODELS AND COMPUTATIONAL
METHODS
We start from the Kane-Mele model9, in which the
intrinsic SO coupling with a coupling constant λis in-2
cluded.
H0=−t/summationdisplay
/angbracketleftij/angbracketright,σc†
iσcjσ+iλ/summationdisplay
/angbracketleft/angbracketleftij/angbracketright/angbracketrightσσ′vijσz
σσ′c†
iσcjσ′,(1)
wherec†
iσ(cjσ) is the creation(annihilation) operator of
the electron with spin σon the lattice site i,/angbracketleftij/angbracketrightrep-
resents the pairs of the nearest neighbor sites (the hop-
ping ist) and/angbracketleft/angbracketleftij/angbracketright/angbracketrightthose of the next-nearest neighbors.
vij= +1(−1) if the electron makes a left(right) turn to
get to the second bond. The size of our system is consid-
ered to be finite with periodic boundary condition. So,
the position of each lattice site can be described specif-
ically by i= Γ(m,n), representing that the lattice site
iis in the mth column and the nth row, and Γ = A,B
the sublattice labels. The number of the unit cells is
denoted by Nc=L2, therefore the total number of the
lattice sites is Nl= 2L2. To consider the correlation be-
tween electrons, we will include the Hubbard term in the
Hamiltonian, which is given by HI,
HI=U/summationdisplay
iˆni↑ˆni↓, (2)
where ˆniσ=c†
iσciσ. When vacancies are introduced, the
hoppings between the vacancy and the nearest neigh-
bors and the on-site interaction on that vacancy are sub-
tracted from the overall Hamiltonian. Hence the corre-
sponding number of the lattice sites is Nl= 2L2−Nv,
whereNvis the number of vacancies. The total number
of electrons Neis fixed to be at the half-filling ( Ne=Nl).
The Hubbard interaction term is treated with the self-
consistent mean field approximation, so that we will ob-
tain an effective single-particle Hamiltonian where the
electrons interact with a spin-dependent potential,
HI≃U/summationdisplay
i,σ/angbracketleftˆni−σ/angbracketrightˆniσ−U/summationdisplay
i/angbracketleftˆni↑/angbracketright/angbracketleftˆni↓/angbracketright.(3)
And the overall mean field Hamiltonian Hmfis then
given by,
Hmf=U/summationdisplay
iσ/angbracketleftˆni−σ/angbracketrightˆniσ+H0. (4)
After diagonalizing the Hamiltonian Hmf, we can de-
termine the occupation number /angbracketleftˆni−σ/angbracketrightat each site with
different spins using the eigenvectors of Hmf, and this
process is carried out iteratively until a required accu-
racy is reached. Then the magnetic moment of each site
mi=/angbracketleftˆni↑−ˆni↓/angbracketrightcan be calculated. We note that a
collinear magnetic texture is assumed in our system, as
used before for the investigations of Kane-Mele-Hubbard
model20,21. We have checked the results with the non-
collinear magnetic texture and found that the collinear
magnetic texture is favored.
III. MAGNETISM WITH ONE VACANCY
The calculation is carried out on the lattice with Nc=
14×14 unit cells in which a single vacancy is introduced/s49 /s50 /s51 /s52 /s53 /s54/s48/s46/s48/s48/s48/s46/s48/s52/s48/s46/s48/s56/s48/s46/s49/s50/s48/s46/s49/s54
/s32 /s61/s48/s46/s48/s48
/s32 /s61/s48/s46/s48/s53
/s32 /s61/s48/s46/s49/s48/s32/s109
/s105
/s32
/s32/s114/s47/s97/s40/s99/s41/s40/s98/s41
/s32/s48/s46/s48/s48
/s48/s46/s48/s52
/s48/s46/s48/s55
/s48/s46/s49/s49
/s48/s46/s49/s52
/s48/s46/s49/s56/s32/s40/s97/s41
FIG. 1: (color online). (a) and (b): Distribution of the spin
moments mion lattice sites around asingle vacancy at A(7,7)
withU= 1.0t, in which (a) corresponds to the SO coupling
constant λ= 0.0 and (b) λ= 0.1t. The area and color of the
hollow circles represent the magnitude of the spin moments.
(c)mion theBsublattice as a function of the distance r
away from the vacancy. The unit ais the distance between
the nearest sites.
on the site A(7,7). Figure 1 displays the distribution of
the magnetic moment when the Hubbard interaction is
taken to be U= 1.0t, in which the size and the color
of the circle on each lattice site denote the magnitude
of the local spin moment. From Fig.1(a) where the SO
couplingisturnedoff, onecanseethatlocalizedmagnetic
moments are induced around the vacancy in the presence
of a finite Hubbard interaction U. This is in agreement
with the prediction of the Lieb theorem28regarding the
total spin Sof the exact ground state of the Hubbard
model on bipartite lattices. It states that the total spin
Sis given by the sublattice imbalance 2 S=|NA−NB|,
withNAandNBthe number of atoms belonging to each
sublattice. With the introducing of a single vacancy on
theAsublattice, an imbalance NB−NA= 1 appears
and a magnetic structure near the vacancy with the total
spinS= 1/2 will form. Similar results have also been
obtained in recent studies in graphene2–4.
In the presence of the SO coupling, the magnitude of
the magnetic moments around the vacancy increases, as
shown in Fig. 1(b) for λ= 0.1t. At the meantime, if
we check the distribution of the magnetic moments, as
shown in Fig.1(c) where the magnitude of the magnetic
moments on sublattice Bas a function of the distance r
awayfromthe vacancyis presented, one will find that the
magnetic moments are more localized with the increase
of the SO coupling. These features demonstrate that the
SOcoupling will enhancethe magneticmoments nearthe
vacancy notably.
In order to show the emergence of the magnetism in-
duced by the vacancy in more detail, we calculate the3
spin resolved local density of state(LDOS) as defined by,
Dσ(ǫ) = Σn,i|un
i,σ|2δ(ǫ−ǫn), (5)
whereiruns over the lattice sites surrounding the va-
cancy up to the third-nearest neighbors, as those linked
by the green line in Fig.1(a) and (b). un
i,σis the single-
particle amplitude on the ith site with spin σand the
corresponding eigenvalue is ǫn. The Delta function in
Eq.(2)isreplacedbytheLorentzianfunction forplotting.
The results for the LDOS are presented in Fig. 2(a)-(h)
for different Hubbard interaction Uand SO interaction
λ. The red and blue lines represent the LDOS for the
spin up and spin down components respectively, and the
dash lines show the LDOS away from the vacancy for
a comparison. In the case of U=λ= 0.0 as shown
in Fig. 2(a), the LDOS shows a V-shape linear behavior
near the Fermi level for those lattice sites far away from
the vacancy (denoted by the dashed line) which is the
consequence of the linear dispersion relation of the elec-
trons, the so-called Dirac fermions. For those around the
vacancy, a peak at the Fermi level emerges as shown by
/s48/s46/s48/s48/s46/s53/s49/s46/s48
/s40/s101/s41/s76/s68/s79/s83
/s45/s51 /s45/s50 /s45/s49 /s48 /s49 /s50 /s51/s48/s46/s48/s48/s46/s52/s48/s46/s56/s49/s46/s50
/s40/s103/s41/s76/s68/s79/s83
/s69/s47/s124/s116/s124/s45/s51 /s45/s50 /s45/s49 /s48 /s49 /s50 /s51/s40/s104/s41
/s69/s47/s124/s116/s124/s40/s102/s41/s40/s100/s41
/s48/s46/s48/s48/s46/s53/s49/s46/s48
/s40/s99/s41/s76/s68/s79/s83/s40/s98/s41
/s48/s46/s48/s48/s46/s53/s49/s46/s48/s32/s76/s68/s79/s83/s40/s97/s41
FIG. 2: (color online). LDOS for λ= 0.0 [left column, includ-
ing (a),(c),(e),(g)] and for λ= 0.1t[right column, including
(b),(d),(f),(h)], where the Hubbard interaction U= 0.0 for
(a) and (b), U= 1.6tfor (c) and (d), U= 2.6tfor (e) and
(f), and U= 3.6tfor (g) and (h), respectively. LDOS for
different spins is resolved, those with the spin up are denote d
by the blue lines and the spin down the red lines. The grey
dash lines represent the LDOS on the lattice site away from
the vacancy./s49 /s50 /s51 /s52/s48/s46/s50/s48/s46/s52/s48/s46/s54/s48/s46/s56/s49/s46/s48/s40/s98/s41
/s77
/s32 /s108/s111/s99
/s85/s32/s47/s32/s116/s32 /s61/s48/s46/s48/s48
/s32 /s61/s48/s46/s48/s52
/s32 /s61/s48/s46/s49/s48
/s32 /s61/s48/s46/s49/s54
/s48/s46/s48/s48 /s48/s46/s48/s52 /s48/s46/s48/s56 /s48/s46/s49/s50 /s48/s46/s49/s54/s48/s46/s54/s48/s46/s55/s48/s46/s56/s48/s46/s57/s49/s46/s48
/s32/s32
/s32/s85/s61/s49/s46/s48
/s32/s85/s61/s50/s46/s50
/s32/s85/s61/s50/s46/s52
/s32/s85/s61/s50/s46/s56/s77
/s32 /s108/s111/s99
/s32/s47/s32/s116/s40/s97/s41
FIG. 3: (color online). Local moments Mloc(see text) are
shownasafunctionoftheSOcoupling λfordifferentHubbard
interaction U(a) and of Ufor different λ(b).
the solid line, which corresponds to the localized states
induced by the vacancy29. After turning on the SO cou-
pling, such as that for λ= 0.1t[see Fig.2(b)], we can see
that an energy gap opens for those lattice sites far away
from the vacancy9,10, so that now a U-shape LDOS near
the Fermi level occurs. In this way, the mid-gap peak is
enhanced noticeably because the decay rate of the local-
ized states into the continuum is reduced largely due to
the open of the energy gap. This will lead to the increase
in the spectral weight of the localized states around the
vacancy. However, for both cases, one will find that the
LDOS for the spin up and spin down components degen-
erates, so that the system will not show magnetism as a
whole without the Hubbard interaction.
The effect of a finite Hubbard interaction Uis to split
the spin degenerate LDOS, so that two peaks occur cor-
responding to different spins, as shown in Fig. 2(c)-(f).
Consequently, the localized spin up and down moments
will not cancel out in this case, and a net magnetism
around the vacancy is induced.
The magnetism may be quantified by the local mo-
mentMloc=/summationtext
imi, where the sum runs over the lat-
tice sites surroundingthe vacancy up to the third-nearest
neighbors as used above in the calculation for the LDOS.
The results are presented in Fig. 3(a) and (b) for dif-
ferentUandλ, respectively. The local moment Mloc
shows a monotonic increase with the SO coupling λ, so
it reinforces our observation that the local magnetism
is enhanced by the SO coupling as shown in Fig.1. On
the other hand, Mlocshows a nonmonotonic dependence
on the Hubbard interaction U, namely it increases with
Ufirstly and then decreases with a further increase of
Uafter a critical value Uc. As discussed above, the lo-
cal magnetism is determined by the spin-split localized
states induced by the vacancy, and it is the Hubbard in-
teraction Uto split the spin-degenerate states. Because
the open of the gap due to the SO coupling will decrease
the decay rate of the localized states into the continuum,
so it will enhance the spectral weight of the localized
states[see also Fig. 2], consequently the localized mag-
netism. The splitting between the two localized states
with different spins is proportional to U, so the two split4
localized states will situate in the SO gap for a small
U[Fig. 2(c)-(f)]. However, when U > U cthe splitting
will be larger than the SO gap, and it pushes the local-
izedstatestomergeintothecontinuum[Fig.2(g)and(h)],
so the local magnetism will decrease.
IV. THE CASE OF MULTI-SITE VACANCY
The multi-site vacancy can be formed by removing the
sites continuously. Here, we consider a large stripe va-
cancy by taking out a chain of sites from the lattice as
illuminated in Fig. 4. In this way, the stripe vacancy
consists of one upper and one lower zigzag edges. As
clarified by the Lieb theorem28, the sublattice imbalance
between the number of atoms belonging to different sub-
lattices will have significant effect on the magnetism. For
the stripe vacancy considered here, the imbalance is ex-
pressed by the parity of the number of vacancies, where
the number is even ( NA=NB) in Fig. 4(a) and (b), and
odd (NA/negationslash=NB) in Fig. 4(c) and (d), thus the total spin
of the system is S= 0 and 1 /2 respectively.
Inthecaseofevennumberofvacancies,aferrimagnetic
spin order emerges on both the upper and lower zigzag
edges around the stripe vacancies when there is no SO
coupling, as shown in Fig. 4(a). The ferrimagnetic ar-
rangement and the magnitude of the spin moments on
these two edges are symmetric, but they are counter-
polarized, so they cancel out exactly and the whole sys-
tem will not show magnetism. This is consistent with
the Lieb theorem28. The ferrimagnetic order on a suffi-
ciently long zigzag edge around the stripe vacancies here
issimilartothespin orderformedattheouteredgeofthe
zigzagribbon30–33and the graphenenanoisland34. In the
case of odd number of vacancies, a similar ferrimagnetic
spin order is also induced with a slightly large magnitude
[Fig. 4(c)]. Interestingly, this ferrimagnetic order occurs
only on the upper zigzag edge, not on the lower edge.
This phenomenon is ascribed to the presence of an extra
spin when a sublattice imbalance NA/negationslash=NBexists, as
/s40/s97/s41
/s32
/s32
/s32/s32 /s32/s32
/s40/s99/s41/s40/s98/s41
/s32
/s32/s45/s48/s46/s49/s56/s45/s48/s46/s49/s49/s45/s48/s46/s48/s52/s48/s46/s48/s52/s48/s46/s49/s49/s48/s46/s49/s56
/s40/s100/s41
/s32
/s32/s45/s48/s46/s50/s54/s45/s48/s46/s49/s54/s45/s48/s46/s48/s53/s48/s46/s48/s53/s48/s46/s49/s54/s48/s46/s50/s54
/s66/s65/s66/s65
FIG. 4: (color online). Distribution of the spin moments mi
on the lattice sites surrounding the vacancies for U= 1.0tand
L= 14. A cluster of vacancies is formed with the number of
missing sites for (a), (b) Nv= 8 and (c), (d) Nv= 7. SO
coupling is set to be λ= 0.0 for (a), (c) and λ= 0.1tfor
(b), (d). The area and color of hollow circles represent the
magnitude of the moments./s48/s46/s48/s48 /s48/s46/s48/s53 /s48/s46/s49/s48 /s48/s46/s49/s53 /s48/s46/s50/s48/s48/s46/s48/s48/s46/s50/s48/s46/s52/s48/s46/s54/s48/s46/s56/s40/s98/s41
/s32/s78 /s118/s61/s51
/s32/s78 /s118/s61/s53
/s32/s78 /s118/s61/s55
/s32/s78 /s118/s61/s57
/s32/s78 /s118/s61/s50
/s32/s78 /s118/s61/s52
/s32/s78 /s118/s61/s54
/s32/s78 /s118/s61/s56
/s32/s78 /s118/s61/s49/s48/s77
/s101
/s47/s32/s116/s48/s46/s48/s48 /s48/s46/s48/s53 /s48/s46/s49/s48 /s48/s46/s49/s53 /s48/s46/s50/s48/s48/s46/s53/s48/s46/s54/s48/s46/s55/s48/s46/s56/s48/s46/s57/s49/s46/s48
/s32/s78 /s118/s61/s51
/s32/s78 /s118/s61/s53
/s32/s78 /s118/s61/s55
/s32/s78 /s118/s61/s57
/s32/s32/s77
/s108/s111/s99
/s47/s32/s116/s40/s97/s41
FIG. 5: (color online). (a)Local moments Mlocare plotted as
a function of λwhileU= 1.0tandL= 14. The function in
different size of vacancy is distinguished by different color and
shape of points. The cases of even Nvare not plotted as local
moments are always zero obeying Lieb theorem28. (b) The
function of edge moments Meversusλare given in different
Nv.
described by the Lieb theorem28.
After turning on the SO coupling, such as for λ= 0.1t,
the ferrimagnetic spin order on both the upper and lower
zigzag edges around the stripe vacancies disappears com-
pletely in the case of even number of vacancies[Fig. 4(b)].
However, the effect of the SO coupling on local mag-
netism is quite different for the case of an odd number
of vacancies. Here, a ferrimagnetic spin order similar
to that on the upper edge emerges on the lower edge,
though the magnitude of the individual spin moment is
reduced[Fig. 4(d)]. To show variation of the total mag-
netism, we plot the quantity Mlocas a function of the
SO coupling λin Fig. 5(a), here Mlocis the sum of the
spin moments on the sites which are on the zigzag edges
around the vacancies. Since Mlocis always zero in the
case of even Nv, it is not plotted here. With an odd
Nv, the local moment Mlocincreases with the increase
ofλ, which shows a similar behavior as that in the case
of a single vacancy. This indicates that the total local
magnetism shown in Fig. 4(d) is in fact enhanced with
the introduction of the SO coupling and approaches the
saturation value 1 finally. From Fig. 5(a), one can also
find that Mlocincreases with the increase of the number
of vacancies Nv. This suggests that the SO coupling will
localize the induced spin moments to those lattice sites
which are neighboring the vacancies.
To quantify the variation of the spin moments with
λon the upper zigzag edge, we also present Meas a
function of λin Fig. 5(b), here Meis the sum of the
spin moments only on the sites on the upper zigzag edge.
Let us consider firstly the case of even number of Nv,
for a small number of even vacancies, Meis always zero.
Up toNv≥8, a finite Meoccurs and it increases with
Nvby the formation of the zigzag edges. However, Me
drops rapidly to zero after turning on the SO coupling.
These results quantify the physical picture derived from
Fig. 4(a) and (b). Now let us turn to the case of odd
number of Nv. Without the SO coupling, Mealso shows5
/s45/s49/s48 /s45/s53 /s48 /s53 /s49/s48/s45/s48/s46/s56/s45/s48/s46/s52/s48/s46/s48/s48/s46/s52/s48/s46/s56
/s40/s98/s41
/s32/s101/s110/s101/s114/s103/s121/s47/s116
/s32/s109/s45/s49/s48 /s45/s53 /s48 /s53 /s49/s48/s45/s48/s46/s56/s45/s48/s46/s52/s48/s46/s48/s48/s46/s52/s48/s46/s56
/s40/s97/s41/s32/s32/s101/s110/s101/s114/s103/s121/s47/s116
/s32/s109
FIG. 6: (color online). The single-particle energy levels l a-
beled with m(see text) near the Fermi level of the non-
interacting systems for (a) Nv= 8 and (b) Nv= 7. SO cou-
pling is set to be λ= 0.0 for the red circles and λ= 0.1tfor
the blue squares.
an increase with Nv. With the introduction of the SO
coupling, Meshows a decrease with λand saturates to
near one half of Mloc.
In fact, we can make an analogy between the stripe
vacancy and the graphene ribbon with zigzag edges. A
remarkable feature of the graphene ribbon with zigzag
edges is that it has a flat band localized on the zigzag
edge1. An important effect of this flat band is that a
counter-polarized ferromagnetic order along the upper
and lower edges will be induced when the Hubbard in-
teraction between electrons is included30–33. In view of
this, we plot the single-particle spectra for the systems
with the stripe vacancy without the Hubbard interaction
in Fig.6(a) and (b) for Nν= 8 and Nν= 7, respectively.
Each energy level is labeled with m=n−Ne−1/2 in
order to indicate that the energy level with m <0 is
occupied by electron. For the systems without SO cou-
pling, we find that there are four near-degeneracy local-
izedstates[redcirclesindicatedbyarrowsinFig.6(a)and
(b)] which is near the Fermi level for both Nν= 8 and
Nν= 7. These states will have the same effect as the flat
band in the zigzag ribbon when a suitable Hubbard U
is turned on. So, a counter-polarized ferrimagnetic order
as shown in Fig.4(a) will emerge. However, we note that
there are two additional zero modes for Nν= 7 relative
toNν= 8, due to the imbalance between the sublattices(NA> NB). Thesezeromodeswillinduceextraspinmo-
ments on both edges, which counteract the antiparallel
moments on the lower edge. Thus, in the case of Nν= 7,
only the ferrimagnetic order on the upper edge appears.
After turning on the SO coupling, those localized states
[blue squares indicated by arrows in Fig.6(a) and (b)] are
pushed away from the Fermi level due to the open of the
SO gap. Thus, as shown in Fig.4(b), a small Hubbard U
is not enough to induce the counter-polarized ferrimag-
netic order on the upper and lower edges. However, the
zero modes originating from the imbalance of sublattices
are not affected by the SO coupling [Fig.6(b)]. So, the
additional ferrimagnetic order on both edges induced by
these zero modes will remain for Nν= 7.
V. CONCLUSION
In a summary, we have studied the local magnetism
induced by vacancies on the honeycomb lattice based on
the Kane-Mele-Hubbard model. It is shown that the SO
coupling tends to localize and consequently enhances the
local magnetic moments near a single vacancy. Further-
more, along the zigzag edges formed by a chain of va-
cancies, the SO coupling will suppress completely the
counter-polarized ferrimagnetic order along the edges.
Therefore, the system will not show any local magnetism
in the case ofeven number ofvacancies. For an odd num-
ber of vacancies, a ferrimagnetic order along both edges
exists and the total magnetic moments along both edges
will increase.
Acknowledgments
This work was supported by the National Natural
Science Foundation of China (Grant Nos. 91021001,
11190023 and 11204125) and the Ministry of Science
and Technology of China (973 Project grant numbers
2011CB922101 and 2011CB605902).
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1709.09811v1.Spin_orbit_interaction_of_light_induced_by_transverse_spin_angular_momentum_engineering.pdf |
1
Spin-orbit interaction of light induced by transverse spin angular momentum
engineering
Zengkai Shao1*, Jiangbo Zhu2*, Yujie Chen1, Yanfeng Zhang1†, and Siyuan Yu1,2† 0F
1School of Electronics and Information Engineering, State Key Laboratory of Optoelectr onic Materials and Technologies, Sun
Yat-sen University, Guangzhou 510275, China .
2Photonics Group, Merchant Venturers School of Engineering, University of Bristol, Bristol BS8 1UB, UK .
*These authors contributed equally to this work.
†email: zhangyf33@mail.sysu.edu.cn ; s.yu@bristol.ac.uk
We report the first demonstration of a direct interaction between the extraordinary transverse spin angular momentum in
evanes cent waves and the intrinsic orbital angular momentum in optical vortex beams. By tapping the evanescent wave of
in a whispering -gallery -mode -based optical vortex emitter and engineering the transverse -spin state carried therein , a
conversion between the transverse -spin angular momentum and the intrinsic orbital angular momentum carried by the
emitted vortex beam takes place . This unconventional interplay between the spin and orbital angular momenta allows the
regulation the spin-orbital angular momentum states of the emitted vortex . In the reverse process, it further gives rise to an
enhanced spin -direction coupling effect in which waveguide or surface modes are unidirectional ly excited by an incident
optical vortex , with the directionality jointly control led by the spin and orbit al angular momenta states of the vortex . The
identification of this previously unknown pathway between the polarization and spatial degrees of freedom of light enrich es
the spi n-orbit interaction phenomena , and can enable a variety of functionalities employing spin and orbital angular
momenta of light in applications such as communications and quantum information processing .
Light waves possess intrinsic spin and orbital angular momentum (SAM and OAM), as determined by the polarization and
spatial degrees of freedom of light1-3. These two components are separately ob servable in paraxial beams4-7, where as it is
well known that fundamentally such a distinction faces difficulties in light fields with high nonparaxiali ty and/or
inhomogeneit y8-11. In fact, spin -orbit interactions (SOI) can be widely observed in light through scattering or focusing12,13,
propagation in anisotro pic/inhomogeneous media14,15, reflection/refractio n at optical interfaces16,17, etc. Notably, the spatial
and polarization properties of light are coupled and SOI phenomena must be considered in modern optics dealing with
sub-wavelength scale systems, including nano -photonics and plasmonics18-22. A variety of novel functionalities utilizing
structured light and materials are underpinned by SOI of light, e.g., optical micro -manipulations23, high -resolution
microscopy24, and beam shaping wi th planar structures (metasurfaces)25.
On the other hand, the stud y in SOI over the past few years is accompanied by a rising interest in the transverse spin
angular momentum of light, which has been revealed by recent advances in optics as a new member in the optica l angular
momentum (AM) family26-29. In sharp contrast to the longitud inal SAM predicted by Poynting1, the transverse SAM
exhibits spin axis orthogon al to the propagation of light28,30. Transverse SAM can be typically found in highly
2
inhomogeneo us light fields, including surface plasmon polaritons26, evanescent waves of gui ded and un -guided modes22,28
and strongly focused beams31, where longitudinal field components emerge due to the transversali ty of electromagnetic
waves32. Light fields possess ing transverse SAM can enable various applications in bio -sensing, nano -photonics, etc. More
interestingly, transverse spin in evanescent waves also originates from the SOI in laterally confined propagating modes11, or
can also be interpreted as the quantu m spin Hall effect (QSHE) of light33-35, and thus giving rise to robust spin -controlled
unidirectional coupling at opt ical interfaces18,21,22, 36. This extraordinary characteristic of transverse SAM results in the
breaking of the directional symmetry in mod e excitation at any interface supporting evanescent waves, and can find
applications in optical diodes37, chiral spin networks38,39, etc.
The ability to simultaneously tailor light fields in the polarization and spatial degrees of freedom via SOI phenomen a
has allowed for new functionalities in str uctured light manipulations40. Furthermore, combing SOI and transverse SAM
control will provide a more versatile platform for processing of light fields in the full AM domain. In this paper, we presen t
an enrich ment of the SOI effects revealed by the engineering of transverse spin in evanescent waves. Our method evolves
from a n optical vortex emitter based on a planar integrated whispering -gallery mode (WGM) resonator , which emits beams
with precisely controllabl e total angular momentum (TAM )41,42. Here we demonstrate that the engineering of transverse
spin in the evanescent waves of WGMs in the resonator leads to the spin -to-orbit al AM conversion in the emitted beams.
This is the first demonstration of a n SOI effe ct that features the interaction between the transverse SAM and intrinsic OAM
of light , providing a promising pathway towards more sophisticated light manipulation via SOI p henomena. By reversing
the emission process , we further demonstrate directional cou pling of optical vortices into this integrated photonic circuitry,
with the direction of the waveguide modes jointly controlled by the spin and orbital AM states, realizing the selective
reception of vector vortices without separate polarization and spatia l phase manipulation. These results can be used to bring
novel functionalities to nano -photonic devices, e.g., encoding and retrieving photonic states in the SAM -OAM space, and
provide the guidelines for the design of nano -photonic chiral interface between travelling and bounded vector vortices.
Results
Transverse spin in optic al vortex emitter . The schematic of the platform for the investigation of transverse spin
engineering based SOI is shown in Figure 1a, where a single -transverse -mode ring resonator is coupled with a two -port
access waveguide and embedded with periodic angular scatterers in the inner -sidewall evanescent region of the waveguide.
With the sub -wavelength scatterers arranged in a second -order grating fashion, the diffracted first -order ligh t from the
evanescent fields of WGMs collectively produce a vortex beam carrying optical OAM and travelling perpendicular to the
resonator plane41. In addition, the emitted vortex beams exhibit cylindrically symmetric polarization and intensity
distri butio ns, and thus referred to as cylindri cal vector vortices (CVVs)42,43.
Generally, for the quasi -transverse -electric (TE) WGMs propagating in the high -index waveguide, a local longitudinal
electric component ( Eφ) exists in the sidewall evanescent waves and is in quadrature phase with respect to the radial
component ( Er) (see Figure 1b) , as a direct result of the strong lateral confinement and transversa lity condition32.
Consequently, the local SAM in the evanesc ent field exhibits a ‘transverse’ sp inning axis in the z direction45, being
orthogonal to the local propagation direction (+ φ or φ) of the WGM. Note that for quasi -TE WGMs , the transverse SAM at
the inner - and outer - sidewalls always has opposite spin dir ections, and the transverse spin can also be flip ped by injecting
light from the alternative ports 1 or 2 and exciting counter -clockewise (CCW) or clockwise (CW) WGMs, as shown in
Figure 1 b.
3
Figure 1 . Illustration of the concept s. (a) Schematic of th e platform for the investigation of transverse spin induced SOI effect. A
single -transverse -mode ring resonator is coup led with an access waveguide and embedded with sub -wavelength scatterers arranged as 2nd order
grating in the evanescent wave region. (b) Each WGM possesses transverse spin of opposite signs in the inner - and outer -resonator evanescent
waves, and clock -wise (CW) and counter clock -wise (CCW) WGMs present opposite transverse spins on each side of the resonator. (c)
Illustration of the transve rse-spin-dependent geometric phase acquired by the vector evanescent wave as the WGM travels around the resonator.
For CCW and CW WGMs, a rotation angle of ∓φ·z is experienced by the local coordinates to be aligned with the global reference frame (i.e.,
from (r’’, φ’’) to (x, y)) for phase comparison of different locations , and the geometric phase acquired by evanescent wave is ΦG = ± 2σ/(1+σ2)·φ.
Interaction of transverse -spin and OAM . The emission of CVVs from such structures can be generally described in the
form of transfer matrices as Eout = M2·M1·Ein. By assuming the WGM evanescent wave maintains a uniform distribution
around the resonator, the generic i nput light for the matrices is the inner sidewall evanescent wave and can be written in the
locally transverse and longitudinal polarization basis . Here the CCW propagating WGM is considered as an example and
thus Ein ∝ eipφ[Er Eφ]T (see Supplementary Note 1 for details ), where the integer p > 0 is the azimuthal mode number and Ez
is negligible at the sidewalls46.
Firstly, the perturbation to WGM evanescent wave s induced by the scatterers is expressed by the matrix
1
1
20
0iδφ WeWM
(1)
where δ(φ) = qφ (see supplementary material of ref. 41) is the azimuthal phase acquired by the second -order grating
scattering , q is the number of scatterers, and Wi (i = 1, 2) is a coefficient quantifying the sca tterers’ modulation on the field
strength of the electric components. Here we define the transverse -spin state in the perturbed evanescent wave |M1|· Ein ∝
eipφ[W1Er W2Eφ]T based on the ratio of the two cylindrical components as28
1
12
2
2
12
1,
,r
r φ
φ
φ
r φ
rWEW E W EiW E
σiW E
W E W EWE
(2)
4
σ (|σ| <= 1) is a real number as Eφ and Er always oscillate in quadrature with each other at the sidewalls46, and it directly
characterizes the (spatial ) transverse -spin density in the evanescent wave as S⊥ ∝ σ (refs 6,11) . For the transvers e SAM of
left (right) handed spin here, σ > 0 (< 0). In addition, the vector fields of WGMs travelling along the resonator experience a
rotation of local coordinate frame, which is described by the matrix
2cos sin
sin cosM
(3)
By apply ing the transfer matrices M1 and M2, the Jones vector of the output CVV becomes
TC TC11
out2211 11
2 1 2 1i l i lσσeeiiσσ E
(4)
where lTC = p q is defined as the topological charge (T C)41. Here the Jones vector is formulated in the global reference
frame with the x- and y-polarization basis (i.e., [ Ex Ey]T). The constituent left - ([1 i]T) and right -hand ([1 i]T) circular
polarized (CP) vortices are out -of- and in -phase, respectively, when following the two definitions in Equation ( 2). It is
straightforward to find that the CVV possesses the SAM and OAM component s per photon as (see Supplementary Note 2)
z 22
1σS=
σ
,
z TC 22
1σL = l
σ
(5)
where ħ is the reduced Planck constant. Note that Sz here, which should be distinguished from the spatia l transverse spin
density S⊥, is the SAM in CVVs averaged over the transverse x -y plane. More profoundly, the variation in magnitude from
the local density ( S⊥ ∝ σ) to the average SAM ( Sz ∝ 2σ/(1+σ2)) is associated with a transverse -spin dependent geometri c
phase that stems from the rotation of local vector field . To be more specific, t he Pancharatnam phase44,47 is used to
described the spatial phase variation in the CVVs of space -variant polarization state ( see Supplementary Note 3)
TC 22+
1PσΦl
σ
(6)
where lTCφ = pφ – δ(φ) is the scattering phase solely resulted from the first -order diffraction of grating41. Meanwhile, the
second term, ΦG = 2σφ/(1+σ2), has a pure geometric nature and arises from the rotation of local transverse -spin state while
WGMs travel arou nd the resonator (see Figure 1c). It should be emphasized that ΦG differs from all the previous ly
discussed geometric phase s of light that can be identified either in artificial anisotropic structures44 or light beams of
curvilinear trajectories15, and originates essentially from the coupling between the transverse SAM of guided light and the
rotation of light’s path. Nevertheless, this transverse -spin dependent geometric phase is still in accordance with the unified
form of geometric phase of light ΦG = ħ-1∫S·Ωφ dφ (ref. 11), and here S = 2σ/(1+σ2)ħ·z = Sz·z is the SAM and Ωφ = z is
the angular velocity of coordinate rotation with respect to coordinate φ for CCW WGMs (see Figure 1c). For CW WGMs,
Ωφ = z and the geometric phase becomes ΦG = 2σφ/(1+σ2) (see Supplementary Figure 1 ).
On the other hand, it’s interesting to find that the z-compnent of TAM in CVVs (Jz = Lz + S z = lTCħ) is conserved with
the given WGM azimuthal mode order p and grating number q, regardless of the transverse -spin state. This is attributed to
the rotationally symmetric ‘anisotropy’ orientation of the scatterer group48, and consequently the net transfer of AM
betw een the WGMs (carrying TAM of pħ per photon ) and device is constantly qħ. More importantly, the transverse -spin
dependen t SOI can be identified in Equation ( 5), and by engineering the transverse -spin state σ and consequently the
transverse -spin dependent geometric phase ΦG, the OAM state of a CVV can be modulated and partially converted with
SAM . This is a new type of SOI, and the first manifestation of spin -to-orbit al AM conversion in optical vortices directly
stemming from the transverse spin of light. In addition , the left - and right -hand CP vortices in Equation ( 4) possess the
topological charges of lTC1 and lTC+1, resp ectively. The composition of this ‘superposition’ is subject to the
5
transverse -spin state of WGM evanescent wave. Particularly, when the polarization at the grating scatterer locations reaches
one of the CP states (i.e., σ = ± 1), this superposition reduces to a single CP scalar vortex state with a single OAM
eigen -state (l = lTC ∓ 1).
It should be mentioned that , by exciting WGMs from the alternative waveguide ports or scattering the evanescent
waves on the other side of resonator waveguide , the sign of th e transverse spin will be flipped, and using the alternative
waveguide port to excite CW propagating WGMs will also reverse the sign of lTC (see Supplementary Note 1 ).
Nevertheless, the general SOI phenomena and mode decomposition described in Equations ( 4) and ( 5) still hold.
Transverse spin engineering . The transverse -spin state σ in the WGM evanescent wave is dependent on the ratio of
cylindrical components as shown in Equation ( 3). In contrast to the evanescent waves of WGMs in bottle micro -resonators49
and unbounded evanesce nt waves at optical interfaces26, where this ratio is largely determined by the refractive index
contrast and the incident angle of light, the transverse spin of evanescent waves in highly confined waveguide modes is also
significantly altered by the lateral confinement conditions, especially the waveguide co re dimensions. By modifying the
mode profile of the transverse component in the core and its spatial derivative at the waveguide boundaries, the magnitude
of the longitudinal component can be engineered50. In other words, by tailoring the waveguide geometr y and consequently
the vector components of modes, σ can be adjusted and thus enabling the engineering of transverse spin in evanescent
waves.
Figure 2 . Numerically calculated field component distributions of the quasi -TE mode and the dependence of the component ratio on waveguide
dimensions. (a) The cross -sectional field distribution of the transverse component Etrans in a SiN x waveguide, and the dashed rectangular
indicates the waveguide of 0.6 μm width and 0.8 μm height. The results in (b) and (c) are obtained with the same waveguide. (b) The field
distribution of the longitudinal component (multiplied with the imaginary unit) iElong. (c) The distribution of the component ratio iElong/Etrans over
the waveguide cross -section and evanescent region. (d) T he contour map of the ratio iElong/Etrans over variable waveguide dimensions. Among all
the waveguide designs calculated, 8 waveguide dimensions marked in the map are employed for device fabrication and characteri zation,
consisting of two different heights (0.4 and 0.6 μm) and four widths (0.8, 1.0, 1.2, and 1.4 μm) as indicated in the subscripts.
As an example, the cross -sectional maps of the fundamental quasi -TE mode components in a straight silicon nitride
(SiN x) waveguide (surrounded by air and placed on a SiO 2 substrate) is depicted in Figure 2 , where the dashed rectangles
indicate the waveguide cores of 0.6 μm in height and 0.8 μm in width. Apart from the transverse component Etrans (Figure
6
2a), a strong longitudinal component Elong at the core -claddi ng interface can also be observed in ±π/2 phase difference to
Etrans, as shown in Figure 2b. The map of the ratio iElong/Etrans is also plotted in Figure 2c , and outside the waveguide
sidewalls it remains almost constant in the decaying evanescent wave, as both components decay at the same rate. More
importantly, a contour map of th is ratio is plotted in Figure 2d, in which a n effectively variable ratio of the two components
can be observed over various waveguide dimensions . Variable transverse -spin state in waveguide evanescent wave can thus
be achieved with routine waveguide design51. The 8 waveguide designs we choose for experimental investigation are
marked in the map, and their parameters are listed in Table 1. SiN x waveguide is employed for its moderat e refractive index
(~ 2.01) so that a larger range of transverse -spin state can be accessed than other materials (e.g., silicon) .
Table 1. Design parameters of the fabricated devices
Sample WG 4-8 WG 4-10 WG 4-12 WG 4-14 WG 6-8 WG 6-10 WG 6-12 WG 6-14
Waveguide Height (μm) 0.4 0.4 0.4 0.4 0.6 0.6 0.6 0.6
Waveguide Width (μm) 0.8 1.0 1.2 1.4 0.8 1.0 1.2 1.4
*These parameters apply both to the ring waveguide and access waveguide.
*The ring radius of all sample devices is 80 μm, gap between ring and access waveguide i s 200 nm, and each square -shape scatterer is 100 nm
by 100nm (with the same height as waveguide).
For the 8 sample devices, the ring radius of 80 µ m is used. For each device, q = 517 scatterers are embedded on the
inner -sidewall of ring. The ratio of evan escent cylindrical components may be perturbed by the presence of scatterers in the
evanescent region , as represented by matrix M1. In this proof -of-principle study , we consider square -shape scatterers
protruding from the waveguide sidewall . Each scatterer has the constant area of 100 nm by 100 nm, but is in the same
height as the ring waveguide . The gap between the access waveguide and ri ng resonator is fixed at 200 nm . The calculated
square of transverse -spin state (σ2) of all sample devices over the scat terer region is shown in Figure 3a. A wide σ2 range of
0.41 - 0.97 is predicted. σ > 0 holds for all cases with WGMs excited by injecting light into Port 1 and the evanescent wave
at the inner sidewall is left-hand e lliptical -polarized . Especially, near -circular transverse spin is expected from the devices
WG 6-8 and WG 4-10 with σ2 ≈ 0.95 and 0.97, respectively. Some scanning electron microscope (SEM) image s of device
WG 6-8 are shown in Figure 3b and 3c .
Figure 3. Calculated transverse -spin states of all designed devices and SEM images of fabricated device WG 6-8. (a) Calculated squared
transverse -spin states in the evanescent wave of all 8 designed devices . These results are obtained considering that the WGM is excited by
injection from Port 1. (b) SEM ima ge of the device WG 6-8. The inset shows a close -up of the coupling section between the access waveguide and
the resonator. (c) Top: junction point of the tapered coupler consisting of a tapered SiN x waveguide and a SU8 waveguide. Bottom: c ross-section
view s at various positions of the tapered coupler. The minimum width of the SiN x taper (shown in the right -hand side image) is 130 nm.
7
Polarization and t ransverse -spin state characterization . Firstly, t he average ‘cylindrical’ polarization ellipticity of the
CVVs is measured to show the overall effect of near -field transverse spin on the polarization of far -field CVVs . The
polarization of CVVs varies in space but ex hibits a cylindrical symmetry with respect to the propagation axis43, and
therefore here the com ponents Er and Eφ are measured to characterize the average ellipticity in the cylindrical basis (i.e., ε =
|Er|/|Eφ| or | Eφ|/|Er|), and compared with the calculated near-field transverse -spin state which is also defined in the same
basis . A Radial Polariza tion Convertor (RPC) is used to convert Er and Eφ in far -field CVVs into x- and y -polarized fields
respectively52, and the power of these two components (Pr and Pφ) is then recorded for ε2 calculation (ε2 = Pr/Pφ or Pφ/Pr)
(see Supplementary Note 4 ).
Figure 4. Characterization of average polarization state in CVVs. (a, b) Measured squared polarization ellipticity ε2 (solid markers) of the CVVs
from the devices of height 0.4 μm and 0.6 μm, respectively. The prediction from numerical calculations (plotted in Figure 3a) is plotted with
dashed lines, and the measured and calculated results for the same device are marked in the same colour.
The measured ε2 in CVVs of various lTC from all devices is shown in Figure 4 as solid markers , while the
corresponding pr edicted σ2 of each device from Figure 3a is plotted as the dashed line in the same color . Overall, the
measured ε2 exhibits high uniformity over all lTC. CVVs of a wide range of spin state s (ε2 from ~0.4 to ~1.0) is obtained
with various waveguide designs, and the agreement between the measured ε2 and calculated σ2 shows a definitive
correspondence from the transverse -spin state in guided evanescent waves to the polarization in e mitted vortices (ε2 = σ2).
Particularly, near -CP (|σ| ≈ 1) CVVs are observed with devices WG 4-10 and WG 6-8, indicating that the reduced sup erposition
of single spin-orbital eigen -state vortices predicted by Equation ( 4) can be reached.
Secondly , Stokes polarimetry is performed to characterize the local transverse -spin state distribut ion in near-field
CVVs . With the Jones vector shown in Equation ( 4), the normalized Stokes parameters as a function of the azimuthal
coordinate can be obtained as53
2
1 21cos 2
1
σS
σ
,
2
2 21sin 2
1σS
σ
,
3 22
1σS
σ
(7)
For a device of a larger | σ|, the trajectory of the Stokes vector [ S1, S2, S3] on the Poincare sphere circles the pole twice at a
higher latitude parallel to the equator. For | σ| = 1, the circle contracts to a single point at the poles, producing a CP CVV.
The measured Stokes parameters of near -field CVVs are depicted in Figure 5, in which the results of lTC = +4 CVVs
from the devices WG 6-8, WG 6-10, WG 6-12, and WG 6-14 are shown , respectively (see Supplementary Note 4 for details ). In
each case, panel (i) is the measured near -field intensity. For better comparison , the calculated Stokes parameters from
Equation (7) are shown as solid curves in panel (v) in each case , along with the measured values (dots) sampled from the
corresponding parameter panels of (ii)-(iv). The σ values used for calculations are imported from Figure 3a, and the
8
measured S1, S2, and S3 are sampled from the pixels on the periphery of the near -field circle of 80 μm radius (i.e., the radius
of ring resonator) . The agreement between the theore tical curves and measured dots shown in the S3 plots of (v) validates
the overall effect of waveguide geometry on the transverse -spin state in evanescent waves. For devices of larger | σ|, e.g.,
WG 6-8, S1 and S2 oscillate less, indicating local polarization states of larger ellipticity.
Generally, the jitters in the measured results are attributed to the non-uniformity of fabricated gratings, as well as the
decaying intensity of WGMs along the resonator. The deviation of measurements from the theory is more evident with
devices of smaller |S3|. This is possibly caused by the light that is scattered from the other (outer -) side of waveguide ,
carrying the opposite σ, due to sidewall roughness . In some devices, standing -wave -like patterns (e.g., map (iv) in Figure
5c) are introduced by the interference of scattered TE and TM modes, because in these waveguide designs these two modes
are more degenerate and single -polarization -mode excitation is more crit ical to polarization control in mode launching.
Figure 5. Stokes polarimetry of near-field polarization of CVVs . (a-d) Measured two -dimensional maps of near -field Stokes parameters and the
comparison with theoretical prediction for devices WG 6-8, WG 6-10, WG 6-12, and WG 6-14, respectively. Each map (i) is the near -field intensity
profile from the device with lTC = +4 . Maps (ii), (iii), and (iv) are the corresponding near -field profiles of the normalized Stokes parameter s S1,
S2, and S3, respectively. The plots in (v) show the comparison between the measured results (dots) sampled from (ii) -(iv) and the corresponding
predicti on (solid curves) from Equation (7). For each set of measured data in (v), 288 pixels intersecting with the circle of 80 μm radius along
the azimuthal direction ( φ) from 0 to 2π are sampled from the corresponding map. For each solid curve of prediction, the data is calculated by
substituting the transverse -spin state σ from Figure 3a into Equation (7).
Transverse spin induced SOI . The OAM component carried by CVVs is measured to verify the transverse -spin induced
spin-to-orbital conversion predicted by Equation ( 5) (see Supplementary Note 4 and 5 for characterization method of OAM
state and emission sp ectrum from devices ). The measured OAM spectra for the CVVs from the devices WG 6-8, WG 6-10,
WG 6-12, and WG 6-14 are plotted in Figure 6. In close agreement with the theory, each OAM spectrum (row) of CVV with lTC
contains two dominant peaks at lTC1 and lTC+1, carried by the constituent left - and right -hand CP vortices, respectively.
The intensities of all spurious modes are < 0.03. Note that each CP vortex can thus be confirmed as possessing a TAM of
lTCħ (see Supplementary Note 6), and this exper imentally validates the overall TAM in each CVV is preserved as lTCħ
regardless of waveguide geometries. More importantly, the average SAM in each CVV is subject to the near -field
9
transverse spin (Sz = 2σ/(1+σ2)ħ) as shown in Figure 5. Therefore, the remar kable transverse -spin dependent SOI effect is
revealed, as the OAM component carried by CCVs can be partially derived out of the transverse SAM in the evanescent
waves. This is the first demonstration of an SOI effect resulted from the interaction between the intrinsic OAM and
transverse SAM of light.
A direct and useful manifestation of this effect is that the relative intensities of the two dominant peaks, i.e., the two
constituent CP vortices , can be changed by modifying σ. For example, the normalized intensities of the left - and right -hand
CP vortices from WG 6-8 are around 0.93 and 0.07, respectively, while for WG 6-14 they account for about 0.62 and 0.36 of
the total intensity, respectively. This variab le superposition of AM states in CVVs provides a viable pathway for
information encoding in the spin -orbit space. Another implication of this SOI effect is that a vortex should appear even
when lTC = 0 but σ ≠ 0 (exemplified by the square in the yellow box in Figure 6a ); that is, without introducing any spatial
phase gradient that has been inherent to many optical vortex generation techniques5. This purely transverse -spin-derived
vortex essentially originates from the spatially varying ‘anisotropy’ of the gratings and the rot ational symmetry of vector
WGMs. In other words, this is an interesting demonstration of optical vortex generation controlled by the QSHE of light33,
and the spin state in the edge modes stemming from the intrinsic SOI at optical interfaces can thus be man ipulated for
spatial light modulation via the ‘extrinsic’ SOI in anisotropic structures11.
Figure 6. Characterization of OAM component s in CVVs. (a -d) The measured OAM spectra for the devices WG 6-8, WG 6-10, WG 6-12, and
WG 6-14, respectively. For each dev ice, the wavelengths of lTC = -5 to +5 are considered, and each column represents a spectrum of measured
OAM comp onents with the corresponding lTC.
Spin -orbit controlled unidirectional coupling . Given the principle of reciprocity, this device can also be used for
detection of AM componen ts in an incident CVV beam54. The ring resonator supports the degenerate CW and CCW WGMs
at each resonance wavelength λ0, and these two modes give rise to the emission of two CVVs of opposite T Cs, i.e., lTC = ±(p
q). Mean while, these two WGMs exhibit opposite σ in the inner -side evanescent waves, and therefore the two emitted
CVVs carry exactly opposi te spin and orbit al AM states , i.e., < 2σ/(1+σ2), lTC 2σ/(1+σ2)> and <2σ/(1+σ2), lTC +
2σ/(1+σ2)>. When receiving at λ0, this device can couple these two CVVs into the two opposite resonating directions and
guide their power to the two access -waveguide ports , respectively . All CVVs with λ ≠ λ0, or at λ0 but with other SAM and
OAM states are mismatched with this selection rule and will be denied by the device. Consequen tly, we obtain the effect of
unidirectional coupling into guided modes jointly controlled by spin and orbital AM states . Although this phenomenon is
essentially associated with the spin -direction locking induced by local SOI in evanescen t waves of guided modes21,22, this
new spin -orbit direction locking effect incorporates the orbital degree of freedom , using the close -loop waveguide for
10
filtering in the OAM space . This spin -orbit controlled coupling provides a po tential solution for spin and orbit al AM state
detection , avoiding the separate manipulations on these two degrees of freedom.
Generally, the input light for ideal r eception with the device should carry the identical spin and orbital AM states as
the outpu t CVVs , while exhibiting cylindrical symmetry in intensity and polarization profiles . But for this
proof -of-principle study here, the special case of σ = ±1 (where the spin -orbit states of CVVs reduce to <±σ, lTC∓σ>) is
demonstrated for simpler experimental configuration , using the device WG 4-10 of near-CP transverse -spin state (σ ≈ ±1) as
shown in Figure 4b.
Table 2. SAM and OAM states in CVVs at vari ous resonance wavelengths
Wavelength (nm) 1578.61 1583.11 1587.59 1592.11
Access port 1 2 1 2 1 2 1 2
lTC 4 +4 2 +2 0 0 +2 2
SAM
OAM 1
3 +1
+3 1
1 +1
+1 1
+1 +1
1 1
+3 +1
3
Figure 7. Proof -of-principle illustration of spin -orbit controlle d uni -directional coupling of waveguide modes. (a -d) Measured results for the
device WG 4-10 with incident light in the wavelength of 1578.61 nm, 1583.11 nm, 1587.59 nm, and 1592.11 nm, respectively. For each
wavelength, incident beams of 33 different spin -orbit states (σin = 1, 0, and +1, lin = -5, -4, …, and +5) are illuminated on the device. For each
11
incident polarization state ( σin = 1/0/+1), the received power with different incident OAM orders from the both ports are listed in a single
histogram. The data in each figure (a/b/c/d) is normalized to the highest value in the group.
The spin and orbital AM states of the CVVs at four resonant wavelengths from device WG 4-10 associated to Port 1 or 2
are listed in Table 2. For each wavelength, optical vortices of 3 SAM st ates (σin = 0, ± 1) and 11 OAM states ( lin from 5 to
+5) are prepared and illuminated on the device (see Supplementary Note 6 for details ). The measured (and calibrated with
respect to the lensed fiber coupling loss) output power P1 at port 1 and P2 at port 2 are normalized and plotted in Figure 7.
The first distinct ive observation is that P 1 in blue bars (P2 in red bars) is universally negligible with incidence of σin = +1
(1), in accordance with the predefined transverse -spin state σ ≈ 1 (+1) when inputting via Port 1 (2) and the underlying
prediction from the spin -direction locking effect21,22. With the incidence of an arbitrary polarization state, however, light is
coupled to the both ports and the resulting ratio of P 1 and P 2 is determined by the relative i ntensity of left - and right-hand
CPs in the incident CVV . For example, with the incident linear polarization (σin = 0, middle rows in Figure 7a to 7d) as an
equal superposition of two CPs, P 1 and P 2 exhibit comparable values. Moreover, the coupling strength is further subject to
the incident OAM state lin. For example, when measuring at Port 2 with incidence at 15 78.61 nm, a single dominant power
peak at port 2 appears only at the incident state of < σin = +1, lin = +3> (upper row in Figure 7a), while it can only be
observed at Port 1 with incident < σin = 1, lin = 3> (lower row in Figure 7a). This high ly directio nal and selective coupling ,
determined by the spin and orbital AM state <σin, lin>, is a higher -order phenomenon with respect to the basic
spin-controlled coupling via evanescent waves, as both the spatial and polarization properties of light must be taken into
account. This effect allows for a robust manipulation of light on the micron -scale using both the spin and orbital degrees of
freedom, e.g., encoding and retrieving information, without the necessity of separate controls on polarization and spatial
phase profile.
Discussion
To sum up, we have identified and demonstrated a new type of spin -orbit interaction of light, namely the interplay between
the intrinsic OAM and the transverse spin of light. This new SOI effect originates from the manipulation of local
transverse -spin-dependent geometric phase by artificially introducing a close -loop waveguide and sub -wavelength scatterers
of rotational symmetry. Engineering the local transverse spin by tailoring waveguide dimensions then controls the global
spin-to-orbital conversion in the generated optical vortices.
Our results have both fundamental and applied importance . The interaction between the intrinsic OAM and transverse
spin of light is an integral but thus far missing part of the rich SOI phenomena . The newly discovered interaction builds one
more path way between the polarization and spati al degrees of freedom of light, which could provide nano -photonic
technologies with additional tools of light manipulation at the subwavelength scales and of informatio n transfer over more
degrees of freedom. The resulting effects , e.g., the variable superposition of spi n-orbit states in optical vortices , may find
applications in optical quantum information processing. T he spin -orbit jointly controlled directional coupli ng can be used to
operate on the eigen -states involving both AM components, so that the device considered here can be regarded as a
prototype of a planar spin -orbit -controlled gate that interfaces propagating and bounded photons of two -dimensional
entangle ment. Better performance (e.g., power efficiency and AM state purity) can be brought about by further device
design and optimization. The demonstrated interaction should also exist in other systems that support evanescent modes,
including surface plasmon -polaritons which can significantly min iaturize the elements.
Methods
Numerical simulation s. Numerical simulations are performed with the finite difference eigenmode solver (FDE, Lumerical Solutions, Inc.). For
the calculation of squared transverse -spin sta te (σ2 shown in Figure. 3a) at the scatterer location of each designed device, first the distribution of
the two cylindrical components (Er and Eφ) over the scatterer region is calculated, and then the average σ2 (<=1) in the scattered evanescent wave
12
is obtai ned as the ratio of integrated intensities of Er and Eφ over one scatterer region . The effect of sactterer ’s modulation on field amplitudes
(W1/W2 in Equation (3)) is thus included in the calculated σ2.
Fabrication . The SiN x waveguide layers are first depo sited on a 5 -μm oxidized <100> silicon wafer using inductively coupled plasma chemical
vapor deposition (ICP -CVD) system (Plasmalab System 100 ICP180, Oxford ). The device structures are defined in a 450 -nm-thick negative
resist using electron -beam lithogra phy (EBL , EBPG5000 ES , Vistec). Reactive -ion-etch (RIE , Plasmalab System 100 RIE180, Oxford) with a
mixture of CHF 3 and O 2 gases is applied to etch through the waveguide layer to form the device . An inverse taper combined with a SU8
waveguide is used as th e coupler between external optical fiber and the access waveguide.
Experimental setup s for device characterizations, SOI measurement and spin -orbit controlled unidirectional coupling are shown and explained
in Supplementary Note 4 and 6.
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14
Supplementary Note 1. Formulation of Cylindrical Vector Vortices Emission
The evanescent wave of whispering -gallery modes (WGMs), written in the cylindrical polarization basis as Ein ∝ e±ipφ[Er Eφ]T, is
perturbed by the second -order grating when circulating around the resonator. Here we denote the positive integer p as the azimuthal mode
number of WGM s, and the two degenerate counter -propagating WGMs resonating in the same wavelength h ave the mode numbers of p
(counter -
p (clockwise, CW), respectively. The perturbation of gratings to the evanescent wave is generalized in a
matrix as
1
1
20
0iδφ WeWM
(1)
where W1 and W2 are real numb ers that reflect the modulation on the amplitudes of local transverse ( Er) and longitudinal ( Eφ) fields,
respectively, due to grating perturbation. The off -diagonal elements of M1 are vanishing as we assume the scattering does not introduce coupling
betwee n orthogonal field components. δ(φ) = ∓qφ is the phase imparted on the first -order diffracted wave derived using the coupled -mode
theory (cf. supplementary material of ref. [1]) and q the number of grating elements. In addition, as WGMs travel around the r esonator, the
vector evanescent wave experiences a rotation of local coordinates ([ Er Eφ]T) with respect to the global laboratory frame ([ Ex Ey]T), as shown in
Supplementary Figure 1. The effect of this rotation on the emitted CVVs (represented in the basi s of [ Ex Ey]T) can be written with a single matrix
M2 as
2cos sin
sin cosx rr
yE EE
E EE =M
(2)
The final output CVV ( Eout = M2·M1·Ein) can be obtained as
TC TC11
out2211 11
2 1 2 1i l i lσσeeiiσσ E
(3)
where σ is the transverse -spin state defi ned in Equation (2) in the main text, and lTC = ± (p – q) the topological charge. It should be emphasized
here that the constituent left - ([1 i]T) and right -
i]T) circular polarized vortices are out -of- and in -phase, respectively, only when
followi ng the two definitions of σ.
Supplementary Figure 1. Rotation of local coordinates as WGMs circulating around the resonator . For the counter -clockwise (CCW)
propagating WGM shown here, the rotation angle of local coordinates ( r, φ) from point a to b with respect to the global coordinates ( x, y) of
output CVVs is φ0z, and z is the unit vector. In other words, from the perspective of light field at point b
φ0z
should be applied in order to align with the global reference fra me (x, y) when its spatial (Pancharatnam) phase is compared with point a in the
15
CVV field. And therefore, the angular velocity of reference frame rotation with respect to coordinate φ for CCW WGM is Ωφ
z. Similarly,
Ωφ = z for clockwise propagating (CW) WGMs.
Supplementary Note 2. Angular Momentum in Cylindrical Vector Vortices
The cylindrical vector vortices (CVVs) emitted from the angular -grating based devices considered in this paper exhibit good paraxiality, as
the radius of ring resonator ( R = 80 μ m) is much larger than the wavelength ( λ = 1.5 um) [2, 3]. The angular momentum (AM) carried in paraxial
optical vortex beams can be essentially considered as the sum of the spin and orbital AM components, which are associated wit h the polarization
and spa tial properties of light, respectively [4, 5]. The cycle averaged z-component of the spin AM (SAM) and orbital AM (OAM) per unit
length per photon of a vortex beam can be written as [5]
x y y x
zrdrdφ E E E E
S
i rdrdφ
EE
(4)
,,jj
j x y z
zrdrdφ E Eφ
L
i rdrdφ
EE
(5)
By substituting the CVV shown in Equation (3) into the equations above, the SAM and OAM components carried by the CVV are
22
1zσS
σ
(6)
TC 22
1zσLl
σ
(7)
where σ is the transverse -spin state in the near -field evanescent wave. The total angular momentum (TAM) in a CVV ( Jz = Sz + Lz) is thus simply
written as
TC zJl
(8)
Supplementary Note 3. Geometric Phase Induced by Coordinate Ro tation
As the polarization state of CVVs is space -variant [2], here the Pancharatnam phase is used to define the phase difference of light fields in
different positions in CVVs [6], that ΦP = arg⟨E(r1, φ1), E(r2, φ2)⟩, where arg ⟨E1, E2⟩ is the argument of the inner product of the two Jones
vectors E1 and E2. Following this definition, the Pancharatnam phase of fields at two different positions ( r1, φ1) and ( r2, φ2) in a CVV is given by
TC 22arg cos sin
1PΦ l i
(9)
where Δφ = φ2 – φ1, and the CV
the azimuthal direction is
2
TC TC 2002arctan tan2 1lim lim
1PΦll
(10)
Clearly, the Pancharatnam phase in CVVs scales linearly with coordinate φ, and thus we can rewrite it as
TC 22
1PΦl
(11)
Considering the SAM component carried by CVVs shown in Supplementary Equation (6), the Pancharatnam phase can be generalized as
TC1
PΦ l d S
(12)
where S = Sz·z is the SAM per p hoton, and Ωφ is the angular velocity of reference frame rotation with respect to the coordinate φ for
Pancharatnam phase comparison (see Supplementary Figure 1). Here, Ωφ = ∓z for CCW and CW WGMs, respectively.
16
Supplementary Note 4. Techniques for Polarization and O AM States Characterization
Supplementary Figure 2 . Experimental setup for device characterization and the observation of the transverse -spin induced SOI effect.
The experimental characterizations of the devices are performed with the setup shown in Supplementary Figure 2. For the excitation of WGMs
and hence emission of CVVs, the continuous -wave light from the tunable laser source ( 8461B, Agilent) is controlled with a fiber polarization
controller ( FPC561, Thorlabs), and the quasi -TE mode in the waveguid e is excited by launching the horizontally polarized light into one of the
ports (e.g., Port 1 as shown in Figure 3a) using a lensed fiber ( SMF -28E+LL, Corning ). A small fraction, 1%, of the input light is tapped using a
coupler (PMC1550 -90B-FC, Thorlabs) and directed to another collimator (F240FC -1550, Thorlabs) to serve as the reference light for the
interference with the emitted CVVs.
For the measurement of the emission spectrum of the device, the vertically emitted beam from the device plane is collect ed and collimated with
a 20X objective lens (UPlanFLN, Olympus) positioned in the working distance (1.7mm) away from the device. A power meter (PM12 2D,
Thorlabs) is placed behind the collimating objective lens to record the dependence of emission power on the working wavelength, while the
output wavelength of the tunable laser is swept from 1500 nm to 1640 nm with the step of 10 pm.
For measuring the average cylindrical -basis polarization ellipticity of CVVs, a liquid crystal based element called Radial Po larization Converter
(RPC, ARCoptix S. A., Switzerland) is used to selectively measure the power of Eφ and Er components. The RPC can be typically used for its
spatially varying anisotropy to convert linearly polarized light into vector beams of azimuthal or radial polarizations [7]. Here the reversed effect
of this element is employed: by injecting the light into the exit side, Eφ and Er in the CVV will be converted into x - and y -polarized light leaving
the entrance side, respectively. A linear polarizer ( LPNIR100 -MP2, Thorlabs) is then used to filter out one of the components, and by detecting
the power of the two orthogonal components as Pφ and Pr, the squared polarization ellipticity ( ε2) in the CVV determined by the near -field
transverse spin state can be obtained as ε2 = Pr/Pφ or Pφ/Pr.
For Stokes parameter s measurements, the near -field pattern of the CVV is imaged onto an InGaAs camera (C14041 -10U, Hamamastu) with an
achromatic lens ( f = 250 mm, AC254 -250-C-ML, Thorlabs), and the linear - and circular -polarizations are obtained by adjusting the quarter -wave
plate (QWP, AQWP 10M -1600, Thorlabs) and the linear polarizer (LP) mounted on continuous rotation mounts (CRM1, Thorlabs).
For the characterization of OAM states in CVVs, a phase -only reflective spati al light modulator (PLUTO SLM, HOLOEYE Photonics AG)
loaded with grey -scale fork -grating patterns is used [8]. A linear polarizer is first used to acquire one of the linear -polarized components in the
CVV, which generally is a mixture of two topologically charged vortices as shown in Equation (4) in the main text. The central axis of the
polarized CVVs is then aligned with the center of fork -grating patterns on the SLM. For each incident CVV, the SLM is loaded with a series of
fork-grating images with conse cutive integer topological charges, e.g., lSLM = -5, -4, …, +5. The light reflected off each image is focused by an
achromatic lens ( f = 150 mm, AC254 -150-C-ML, Thorlabs) followed by the InGaAs camera, and the power of the corresponding OAM
component lSLM is obtained by integrating the intensity of the central Gaussian -like spot [9]. The process is repeated for the other
linear -polarized component, and the measured OAM spectrum of the incident CVV is then obtained by averaging the two corresponding OA M
comp onents over the two linear polarization components.
Supplementary Note 5. Preliminary Characterization of Devices
17
Supplementary Figure 3. Measured emission spectral response of sample device W 6-8 as input wavelength is swept from 1500 -1640 nm. The
inset shows a typical near -field intensity profile of emitted CVVs.
The measured emission spectral response of sample WG 6-8, as an instance, is plotted in Supplementary Figure 3 after normalization to the output
power of tunable laser. The central wavelength at which the emitted CVV has lTC = p
q = 0, is λc = 1596.6 nm, and the free spectral range is
around 2.2 nm. At the wavelengths longer (shorter) than λc, CVVs carry positive (negative) integer lTC at the resonance peaks. The inset shows a
typical near -field intensity profile of the device a t the resonance wavelengths. The long-range variation of peak emitted power across the spectr al
range is primarily caused by the fixed gap between access waveguide and ring resonator that couples varying power into the resonato r across the
spectrum.
Supplementary Figure 4. Far-field profiles and interferograms of left-hand circular -polarized components of CVV s from device WG 6-8.
Some typical far -field intensity profiles and interferograms of CVVs are illustrated in Supplementary Figure 4, in which the d evice WG 6-8 is
configured for the emission of CVVs with lTC from 2 to +4. The left -hand circular polarized (LHCP) component is obtained by filtering the
far-field CVVs with a QWP and LP combination, and then interferes with the LHCP Gaussian beam. For eac h CVV of lTC, the LHCP
component possesses the OAM state of lLHCP = lTC-1 (see Equation (4) in the main text), and therefore each interferogram shown in the figure
clearly exhibits the spiral fringes with the number of lLHCP [1].
Supplementary Note 6. Ex perimental Setup for Spin -Orbit Unidirectional Coupling
The experimental setup for the measurement of spin -orbit controlled unidirectional coupling is shown in Supplementary Figure 3. The polarized
light from the tunable laser is collimated with a collimat or and then reflected by the SLM for the conversion to the vortex carrying OAM state lin.
The linear -polarized vortex is imparted a certain polarization state ( σin) by the rotatable QWP. A 20X objective lens is used for focusing and
illuminating the prepared vortex of spin and orbital AM states < σin, lin> onto the device. Two lensed fibers are used for collecting the received
power from the waveguide Ports 1 and 2, respectively.
18
Supplementary Figure 5. Experimental setup for the measurement of spin -orbit controlled directional coupling of waveguide modes.
Supplementary References
[1] X. Cai, J. Wang, M. J Strain, B. Johnson -Morris, J. Zhu, M. Sorel, J. L. O’Brien, M. G. Thompson, and S. Yu, Science 338, 363-366
(2012 ).
[2] J. Zhu, X. Cai, Y. Chen, and S. Yu, Opt. Lett. 38, 1343 -1345 (2013).
[3] J. Zhu, Y. Chen, Y. Zhang, X. Cai, and S. Yu, Opt. Lett. 39, 4435 -4438 (2014).
[4] L. Allen, M. W. Beijersbergen, R. J. C. Spreeuw, an d J. P. Woerdman, Phys. Rev. A 45, 8185 -8189 (1992).
[5] S. M. Barnett and L. Allen, Opt. Commun. 110, 670 -678 (1994).
[6] S. Pancharatnam, Proc. Ind. Acad. Sci. 44, 247 -262 (1956).
[7] M. Stalder, and M. Schadt, Opt . Lett. 21, 1948 -1950 (1996 ).
[8] G. Gibson, J. Courtial , M. J. Padgett, M. Vasnetsov, V. Pas’ko, S. M. Barnett, and S. Franke -Arnold, Opt. Express 12, 5448 -5456
(2004).
[9] M. J. Strain, X. Cai, J. Wang, J. Zhu, D. B. Phillips, L. Chen, M. Lopez -Garcia, J. L. O’Brien, M. G. Thompson, M. Sorel, and S. Yu,
Nat. Com mun. 5, 4856 (2014) .
|
1411.3043v1.Fermi_Gases_with_Synthetic_Spin_Orbit_Coupling.pdf | Fermi Gases with Synthetic Spin-Orbit Coupling
Jing Zhang
State Key Laboratory of Quantum Optics and Quantum Optics Devices,
Institute of Opto-Electronics, Shanxi University, Taiyuan 030006, P. R. China
Hui Hu and Xia-Ji Liu
Centre for Atom Optics and Ultrafast Spectroscopy,
Swinburne University of Technology, Melbourne 3122, Australia
Han Pu
Department of Physics and Astronomy, and Rice Quantum Institute, Rice University, Houston, TX 77251, USA
(Dated: November 13, 2014)
We briefly review recent progress on ultracold atomic Fermi gases with different types of synthetic
spin-orbit coupling, including the one-dimensional (1D) equal weight Rashba-Dresselhaus and two-
dimensional (2D) Rasbha spin-orbit couplings. Theoretically, we show how the single-body, two-
body and many-body properties of Fermi gases are dramatically changed by spin-orbit coupling.
In particular, the interplay between spin-orbit coupling and interatomic interaction may lead to
several long-sought exotic superfluid phases at low temperatures, such as anisotropic superfluid,
topological superfluid and inhomogeneous superfluid. Experimentally, only the first type - equal
weight combination of Rasbha and Dresselhaus spin-orbit couplings - has been realized very recently
usingatwo-photonRamanprocess. Weshowhowtocharacterizeanormalspin-orbitcoupledatomic
Fermi gas in both non-interacting and strongly-interacting limits, using particularly momentum-
resolved radio-frequency spectroscopy. The experimental demonstration of a strongly-interacting
spin-orbit coupled Fermi gas opens a promising way to observe various exotic superfluid phases in
the near future.
PACS numbers: 05.30.Fk, 03.75.Hh, 03.75.Ss, 67.85.-d
Contents
I. Introduction 2
II. Theory of spin-orbit coupled Fermi gas 3
A. Theoretical framework 3
1. Functional path-integral approach 3
2. Two-particle physics from the particle-particle vertex function 5
3. Many-body T-matrix theory 6
4. Bogoliubov-de Gennes equation for trapped Fermi systems 7
5. Momentum- or spatially-resolved radio-frequency spectrum 8
B. 1D equal-weight Rashba-Dresselhaus spin-orbit coupling 9
1. Single-particle spectrum 10
2. Two-body physics 12
3. Momentum-resolved radio-frequency spectrum of the superfluid phase 13
4. Fulde-Ferrell superfluidity 15
5. 1D topological superfluidity 17
C. 2D Rashba spin-orbit coupling 19
1. Single-particle spectrum 20
2. Two-body physics 20
3. Crossover to rashbon BEC and anisotropic superfluidity 22
4. 2D Topological superfluidity 24
III. Experiments 25
A. The noninteracting spin-orbit coupled Fermi gas 26
1. Rabi oscillation 26
2. Momentum distribution 28
3. Lifshitz transition 28arXiv:1411.3043v1 [cond-mat.quant-gas] 12 Nov 20142
4. Momentum-resolved rf spectrum 28
B. The strongly interacting spin-orbit coupled Fermi gas 30
1. Integrated radio-frequency spectrum 30
2. Coherent formation of Feshbach molecules by spin-orbit coupling 32
IV. Conclusion 32
Acknowledgments 33
References 33
I. INTRODUCTION
Modern physical theories describe reality in terms of fields, many of which obey gauge symmetry. Gauge symmetry
is the property of a field theory in which different configurations of the underlying fields — which are not themselves
directly observable — result in identical observable quantities. Electromagnetism is an ideal example to illustrate this
point. A system of stationary electric charges produces an electric field E(but no magnetic field). It is convenient
to define a scalar potential V, a voltage, that is also determined by the charge distribution. The electric field at any
position is given by the gradient of the scalar potential: E(r) =rV(r). In this system, a global symmtry is readily
perceived: if the scalar potential everywhere is changed by the same amount, i.e., V(r)!V(r) +V0, the resulting
electric field is unchanged. A more non-trivial example is given by a system of moving charges which produces both
electric and magnetic field. In addition to the scalar potential, we now also introduce a vector potential A, the curl
of which gives the magnetic field: B(r) =rA(r). This system obeys the local gauge sysmmetry: any local change
in the scalar potential [ V(r)!V(r) @=@twith (r;t)being an arbitrary function of position and time] can be
combined with a compensating change in the vector potential [ A(r)!A(r) +r] in such a way that the electric
and magnetic fields are invariant.
Maxwell’s classical theory of electromagnetism is the first gauge theory with local symmetry. A related symmetry
can be demonstrated in the quantum theory of electromagnetic interactions, which describes the interaction between
charged particles. From first sight, Maxwell’s theory should not directly describe the center-of-mass motion of neutral
atoms. However, a beautiful series of experiments carried out at NIST [1–3] demonstrated that artificial gauge fields
can be generated in cold atomic vapours using laser fields, such that neutral atoms can be used to simulate charged
particles moving in electromagnetic fields [4]. How to engineer artificial gauge fields is reviewed by Spielman in an
article published in the previous volume of this book series [5].
Itwouldnotbeveryinterestingifalllight-inducedgaugefieldscoulddoistomakeneutralatomsmimicthebehavior
of charged particles. Indeed, artificial gauge field can be made non-Abelian, i.e., the Cartesian components of the field
do not commute with each other. By contrast, the familiar electromagnetic fields are Abelian since their Cartesian
components are represented by c-numbers, thus commuting with each other. A special feature of non-Abelian gauge
field is that it can induce spin-orbit coupling. The concept of spin-orbit coupling (SOC) is encountered, for example,
in the study of atomic structure, where the coupling between the electron’s orbital motion and its intrinsic spin gives
rise to the fine structure of atomic spectrum. In the current context, SOC refers to the coupling between the internal
pseudo-spin degrees of freedom and the external motional degrees of freedom of the atom. That such SOC can be
induced by laser fields can be easily understood as follows: The laser light induces transitions between atomic internal
states, and in the meantime imparts photon’s linear momentum to the atom. Thus the internal and the external
degrees of freedom are coupled via their interaction with the photon.
SOC in cold atoms was first realized in a system of87Rb condensate by the NIST group in 2011 [6]. Since
then, several groups have achieved SOC in both bosonic [7–10] and fermionic quantum gases [11–15]. SOC not only
dramatically changes the single-particle dispersion relation, but is also the key ingredient underlying many interesting
many-body phenomena and new materials such as topological insulators [16] and quantum spin Hall effects [17]. Due
to the exquisite controllability of atomic systems, one can naturally expect that SOC in cold atoms will give rise to
novel quantum states of matter and may lead to a deeper understanding of related phenomena in other systems. For
this reason, spin-orbit coupled quantum gases have received tremendous attention over the past few years, and they
no doubt represent one of the most active frontiers of cold atom research.
In this chapter, we will review the physics of spin-orbit coupled Fermi gas, both theoretically and experimentally.
Although we will mainly focus on the research from our own groups, results from others will also be mentioned.3
II. THEORY OF SPIN-ORBIT COUPLED FERMI GAS
We consider a spin-1/2 Fermi gas with SOC subject to attractively interaction between unlike spins. One great
advantage of the atomic system is its unprecedented controllability. The interatomic interaction can be precisely tuned
using the Feshbach resonance technique [18], which has already led to the discovery of the BEC-BCS crossover from a
Bose-Einstein condensate (BEC) to a Bardeen-Cooper-Schrieffer (BCS) superfluid [19]. Different forms of SOC, many
of which do not exist in natural materials, can also be engineered. The interplay between interatomic interactions and
different forms of SOC may give rise to a number of intriguing physical phenomena. Here let us make some general
remarks concerning the distinct features that can be brought out by SOC in a Fermi gas:
•SOC alters the single-particle dispersion which may lead to degenerate single-particle ground state, and may
render the topology of the Fermi surface non-trivial [20].
•In the presence of attractive s-wave interaction, two fermions may form pairs. In general such pairs contain both
singlet and triplet components [21–26] and have anisotropic (i.e., direction-dependent) effective mass [22–24].
In the many-body setting, a spin-orbit coupled superfluid Fermi gas contains both singlet and triplet pairing
correlation [20, 22, 24, 27] and therefore may be regarded as an anisotropic superfluid [22].
•SOC may greatly enhance the pairing instability and hence dramatically increases the superfluid transition
temperature [22, 23, 28].
•SOC, together with effective Zeeman fields, may generate exotic pairing [29–37] and/or topologically non-trivial
superfluid state [38–55]. At the boundaries of topologically trivial and non-trivial regimes, exotic quasi-particle
states (e.g., Majorana mode) may be created.
In the remaining part of this section, we will discuss two particular types of SOC. The first is the equal-weight
Rashba-Dresselhaus SOC [56] which is the only one that has been experimentally realized so far. The second is
the Rashba SOC which is of particular interest as it occurs naturally in certain semiconductor materials. However,
before we do that, in the next subsection we first summarize the theoretical framework and explain the basics of
momentum- or spatially-resolved radio-frequency (rf) spectroscopy, which turns out to be a very useful experimental
tool for characterizing spin-orbit coupled interacting Fermi gases. For those readers who are interested in the physical
consequences of a detailed type of SOC, this technical part may be skipped in their first reading.
A. Theoretical framework
In current experimental setups of ultracold atomic Fermi gases, the interactions between atoms are often tuned
to be as strong as possible, in order to have an experimentally accessible superfluid transition temperature. With
such strong interactions, there is a significant portion of Cooper pairs formed by two fermionic atoms with unlike
spin. Theoretically, therefore, it is very crucial to treat atoms and Cooper pairs on an equal footing. Without SOC,
a minimum theoretical framework for this purpose is the many-body T-matrix theory or pair-fluctuation theory
[57–62]. In this subsection, we introduce briefly the essential idea of the pair-fluctuation theory using the functional
path-integral approach and generalize the theory to include SOC [24]. Under this theoretical framework, both two-
and many-body physics can be discussed in a unified fashion [24]. We also discuss the mean-field Bogoliubov-de
Gennes equation, which represents a powerful tool for the study of trapped, inhomogeneous Fermi superfluids at low
temperatures [42, 45, 47, 48, 50, 51].
1. Functional path-integral approach
Consider, for example, a three-dimensional (3D) spin-1/2 Fermi gas with mass m. The second-quantized Hamilto-
nian reads,
H=
drh
y
^k+VSO
+U0 y
"(r) y
#(r) #(r) "(r)i
; (1)
where ^k^k2=(2m) = r2=(2m) with the chemical potential , (r) = [ "(r); #(r)]Tdescribes collectively
thefermionicannihilationoperator (r)forspin-atom, andVSO(^k)representsthespin-orbitcouplingwhoseexplicit
form we do not specify here. The momentum ^k i@(=x;y;z) should be regarded as the operators in real4
space. For notational simplicity, we take ~= 1throughout this paper. The last term in Eq. (1) represents the
two-body contact s-wave interaction between unlike spins. The use of the contact interatomic interaction leads to an
ultraviolet divergence at large momentum or high energy. To overcome such a divergence, we express the interaction
strengthU0in terms of the s-wave scattering length as,
1
U0=m
4as 1
VX
km
k2; (2)
whereVis the volume of the system.
The partition function of the system can be written as [61]
Z=
D[ (r;); (r;)] exp
S
(r;); (r;)
; (3)
where the action
S
;
=
0d"
drX
(r;)@ (r;) +H
; #
: (4)
is written as an integral over imaginary time . Here= 1=(kBT)is the inverse temperature and H
;
is
obtained by replacing the field operators yand with the Grassmann variables and , respectively. We can use
the Hubbard-Stratonovich transformation to transform the quartic interaction term into a quadratic form as:
e U0
drd " # # "=
D
;
exp(
0d
dr"
j (r;)j2
U0+ # "+ " ##)
; (5)
from which the pairing field (r;)is defined.
Let us now introduce the 4-dimensional Nambu spinor (r;)[ "; #; "; #]Tand rewrite the action as,
Z=
D[;; ;] exp(
dr0
dr
0d0
0d"
1
2(r;)G 1(r0;0) +jj2
U0(r r0)( 0)#
X
k^k)
;(6)
where the 44single-particle Green function is given by,
G 1=
@ ^k VSO(^k)i^y
i^y @+^k+VT
SO( ^k)
(r r0)( 0); (7)
with the Pauli matrices ^i(i= 0;x;y;z) describing the spin degrees of freedom. The Nambu spinor representation
treats equally the particle and the hole excitations. As a result, a zero-point energy appears in the last term of the
action. Integrating out the original fermionic fields, we may rewrite the partition function as
Z=
D[;] exp
Se
;
; (8)
where the effective action is given by
Se
;
=
0d
dr"
j (r;)j2
U0#
1
2Trln
G 1
+X
k^k: (9)
where the trace is taken over all the spin, spatial, and temporal degrees of freedom.
To proceed, we restrict ourselves to the Gaussian fluctuation and expand (r;) = 0(r)+ (r;). The effective
action is then decomposed accordingly as Se=S0+S, where the saddle-point action is
S0=
0d
drj0(r)j2
U0 1
2Trln
G 1
0
+X
k^k (10)
and the pair-fluctuating action takes the form
S=
0d
dr"
j (r;)j2
U0+1
21
2
Tr(G0)2#
(11)5
with
=
0i^y
i^y 0
: (12)
HereG 1
0is the inverse mean-field Green function and has the same form as G 1in Eq. (7) with (r;)replaced by
0(r). We note that the static pairing field 0(r)can be either homogeneous or inhomogeneous. In the latter case,
a typical form is 0(r) = 0eiqr, referred to as the Fulde-Ferrell superfluid [63], in which the Cooper pairs condense
into a state with nonzero center-of-mass momentum q.
Let us now focus on a homogeneous system, where the momentum is a good quantum number so that we take
k=^kandVSO(k) =VSO(^k). The fluctuating part of the effective action may be formally written in terms of the
many-body particle-particle vertex function (q;in)[61],
S=kBTX
Q=(q;in)
1(Q)
(Q)(Q); (13)
whereQ(q;in)andnis the bosonic Matsubara frequency. By integrating out the quadratic term in S, we
obtain the contribution from the Gaussian pair fluctuations to the thermodynamic potential as [61]
=kBTX
q;inln
1(q;in)
: (14)
Within the Gaussian pair fluctuation approximation, naïvely, the vertex function may be interpreted as the Green
function of “Cooper pairs”. This idea is supported by Eq. (14), as the thermodynamic potential
Bof a free bosonic
Green functionGBis formally given by
B=kBTP
q;inln[ G 1
B(q;in)]. At this point, the advantage of using
pair-fluctuation theory becomes evident. For the fermionic degree of freedom, we simply work out the single-particle
Green function G0and the related mean-field thermodynamic potential
0=kBTS0. An example will be provided
lateroninthestudyoftheFulde-Ferrellsuperfluidity. WhileforCooperpairs, wecalculatethevertexfunction andthe
fluctuating thermodynamic potential
. In this way, we may obtain a satisfactory description of strongly-interacting
Fermi systems [59, 60, 62].
In the normal state where the pairing field vanishes, i.e., 0= 0, we may obtain the explicit expression of the
vertex function. In this case, the inverse Green function G 1
0has a diagonal form and can be easily inverted to give
[24]:
G0(K) =
[i!m k VSO(k)] 10
0
i!m+k+VT
SO( k) 1
G0(K) 0
0 ~G0(K)
; (15)
whereK(k;i!m)and!mis the fermionic Matsubara frequency. Here we have introduced the 22particle Green
functionG0(K)and hole Green function ~G0(K), which are related to each other by ~G0(K) = [G0( K)]T. It is
straightforward to show that,
1(Q) =1
U0+kBT
2X
K=(k;i!m)h
G0(K) (i^y)~G0(K Q) (i^y)i
: (16)
The detailed expression of the vertex function depends on the type of SOC. In the study of Rashba SOC, we will give
an example that shows how to calculate the vertex function.
2. Two-particle physics from the particle-particle vertex function
The vertex function can describe the pairing instability of Cooper pairs both on the Fermi surface and in the
vacuum. In the latter case, it describes exactly the two-particle state. The corresponding two-body inverse vertex
function 1
2b(Q)can be obtained from the many-body inverse vertex function by discarding the Fermi distribution
function and by setting chemical potential = 0[64]. One important question concerning the two-body state is
whether there exist bound states. For a given momentum q, the bound state energy E(q)can be determined from
the two-particle vertex function using the following relation ( in!!+i0+) [22, 24]:
Re
1
2b[q;!=E(q)]
= 0: (17)6
A true bound state must satisfy E(q)<2EminwhereEminis the single-particle ground state energy.
It is straightforward but lengthy to calculate the two-particle vertex function for any type of SOC. Here, we quote
only the energy equation obtained using Eq. (17) for the most general form of SOC [34],
VSO
^k
=X
i=x;y;z
i^ki+hi
^i; (18)
whereiis the strength of SOC in the direction i= (x;y;z )andhidenotes the effective Zeeman field. The eigenenergy
E(q)of a two-body eigenstate with momentum qsatisfies the equation:
m
4as=1
VX
k2
6640
B@Ek;q 4E2
k;q(k)2 4hP
i=x;y;ziki(iqi+ 2hi)i2
Ek;qh
E2
k;q P
i=x;y;z(iqi+ 2hi)2i1
CA 1
+1
2k3
775; (19)
whereEk;qE(q) q
2+k q
2 kandk=k2=(2m). We note that, in general, the lowest-energy two-particle
state may occur at a finite momentum q. That is, the two-particle bound state could have a nonzero center-of-mass
momentum. Later, we shall see that this unusual property has nontrivial consequences in the many-body setting.
Another peculiar feature of the two-particle bound state is that the pairs may have an effective mass larger than 2m.
For example, for the bound state with zero center-of-mass momentum q= 0, it would have a quadratic dispersion for
small p,
E(p) =E(0) +p2
x
2Mx+p2
y
2My+p2
z
2Mz: (20)
The effective mass of the bound state Mi(i=x;y;z) can then be determined directly from this dispersion relation.
Another approach to study the two-particle state with SOC , more familiar to most readers, is to use the following
ansatz for the two-particle wave function [21, 23, 65, 66],
j2Bi=1p
CX
kh
"#(k)cy
q
2+k"cy
q
2 k#+ #"(k)cy
q
2+k#cy
q
2 k"+ ""(k)cy
q
2+k"cy
q
2 k"+ ##(k)cy
q
2+k#cy
q
2 k#i
jvaci;
(21)
wherecy
k"andcy
k#are creation field operators of spin-up and spin-down atoms with momentum kandCis the
normalization factor. We note that, in the presence of SOC, the wave function of the two-particle state has both
spin singlet and triplet components. Then, using the Schrödinger equation Hj2B(q)i=E(q)j2B(q)i, we can
straightforwardly derive the equations for coefficients 0appearing in the above two-body wave function and then
the energy equation for E(q). For the general form of SOC, Eq. (18), it leads to exactly the same energy equation
(19) [34].
Each of the two approaches mentioned above has its own advantages. The vertex function approach is useful to
understand the relationship between the two-body physics and the many-body physics. For example, it can be used to
obtain the two-particle bound state in the presence of a Fermi surface. The latter approach of using the two-particle
Schrödinger equation naturally yields the two-particle wave function. Both approaches have been used extensively in
the literature.
3. Many-body T-matrix theory
The functional path-integral approach gives the simplest version of the many-body T-matrix theory, where the bare
Green function has been used in the vertex function. Here, for completeness, we mention briefly another partially
self-consistent T-matrix scheme for a normal spin-orbit coupled Fermi gas, by taking one bare and one fully dressed
Green function in the vertex function [13, 28]. In this scheme, we have the Dyson equation,
G(K) =
G 1
0(K) (K) 1; (22)
where the self-energy is given by
(K) =kBTX
Q=(q;in)t(Q)(i^y)~G0(K Q)(i^y) (23)7
and ~G0(K) [G0( K)]T. Heret(Q)U0=[1 +U0(Q)]is the (scalar) T-matrix with a two-particle propagator
(Q) =kBT
2X
K=(k;i!m)Trh
G(K) (i^y)~G0(K Q) (i^y)i
; (24)
where the trace is taken over the spin degree of freedom only. Note that a fully self-consistent T-matrix theory may
also be obtained by replacing in Eqs. (23) and (24) the bare Green function ~G0(K Q)with the fully dressed Green
function ~G(K Q). We note also that Eqs. (22)-(24) provide a natural generalization of the well-known many-body
T-matrix theory [62], by including the effect of SOC, where the particle or hole Green function, G(K)or~G(K), now
becomes a 22matrix.
In general, the partially self-consistent T-matrix equations are difficult to solve [62]. At a qualitative level, we
may adopt a pseudogap decomposition advanced by the Chicago group [67] and approximate the T-matrixt(Q) =
tsc(Q)+tpg(Q)to be the sum of two parts. Here tsc(Q) = (2
sc=T)(Q)is the contribution from the superfluid with
scbeing the superfluid order parameter, and tpg(Q)represents the contribution from un-condensed pairs which give
rise to a pseudogap
2
pg kBTX
Q6=0tpg(Q): (25)
The full pairing order parameter is given by 2
0= 2
sc+ 2
pg. Accordingly, we have the self-energy (K) = sc(K) +
pg(K), where
sc= 2
sc(iy)~G0(K)(iy) (26)
and
pg= 2
pg(iy)~G0(K)(iy): (27)
We note that, at zero temperature the pseudogap approximation is simply the standard mean-field BCS theory,
in which (K) = 2
0(iy)~G0(K)(iy). Above the superfluid transition, however, it captures the essential physics
of fermionic pairing and therefore should be regarded as an improved theory beyond mean-field. To calculate the
pseudogap pg, we approximate
t 1
pg(Q'0) =Z[in
q+pair];
where the residue Zand the effective dispersion of pairs
q=q2=2Mare to be determined by expanding (Q)
aboutQ= 0in the case that the Cooper pairs condense into a zero-momentum state. The form of tpg(Q)leads to
2
pg(T) =Z 1X
qfB(
q pair);
wherefB(x)1=(ex=kBT 1)is the bosonic distribution function. We finally obtain two coupled equations, the gap
equation 1=U0+(Q= 0) =Zpairand the number equation n=kBTP
KTrG(K), from which the superfluid order
parameter scand the chemical potential can be determined. This pseudogap method has been used to study
the thermodynamics and momentum-resolved rf spectroscopy of interacting Fermi gases with different types of SOC
[13, 28].
4. Bogoliubov-de Gennes equation for trapped Fermi systems
All cold atom experiments are performed with some trapping potentials, VT(r). For such inhomogeneous systems, it
is difficult to directly consider pair fluctuations. In most cases, we focus on the mean-field theory by using the saddle-
point thermodynamic potential Eq. (10) and minimizing it to determine the order parameter 0(r). This amounts to
diagonalizing the 44single-particle Green function G 1
0(r;;r0;0)with the standard Bogoliubov transformation,
=
drX
u(r) (r) +(r) y
(r)
; (28)8
whereis the field operator for Bogoliubov quasiparticle with energy Eand Nambu spinor wave function (r)
[u"(r);u#(r);v"(r);v#(r)]T, which satisfies the following Bogoliubov-de Gennes (BdG) equation,
r2=(2m) +VT(r) +VSO(^k) i0(r) ^y
i
0(r) ^yr2=(2m) + VT(r) VT
SO( ^k)
(r) =E(r): (29)
The BdG Hamiltonian in the above equation includes the pairing gap function 0(r)that should be determined
self-consistently. For this purpose, we may take the inverse Bogoliubov transformation and obtain
(r) =X
u(r)+
(r)y
: (30)
The gap function 0(r) = U0h #(r) "(r)iis then given by,
0(r) = U0
2X
u"(r)v
#(r)f(E) +u#(r)v
"(r)f( E)
; (31)
wheref(E)1=[eE=(kBT)+ 1]is the Fermi distribution function at temperature T. Accordingly, the total density
takes the form,
n(r) =1
2X
h
ju(r)j2f(E) +jv(r)j2f( E)i
: (32)
The chemical potential can be determined using the number equation, N=
drn(r). This BdG approach has
been used to investigate topological superfluids in harmonically trapped spin-orbit coupled Fermi gases in 1D and 2D
[42, 45, 47, 48, 50, 51]. It will be discussed in greater detail in later sections.
It is important to note that, the use of Nambu spinor representation enlarges the Hilbert space of the system. As
a result, there is an intrinsic particle-hole symmetry in the Bogoliubov solutions: For any “particle” solution with
wave function (p)
(r) = [u"(r);u#(r);v"(r);v#(r)]Tand energy E(p)
0, we can always find a partner “hole”
solution with wave function (h)
(r) = [v
"(r);v
#(r);u
"(r);u
#(r)]Tand energy E(h)
= E(p)
0. These two
solutions correspond exactly to the same physical state. To remove this redundancy, we have added an extra factor of
1/2 in the expressions for pairing gap function Eq. (31) and total density Eq. (32). As we shall see, this particle-hole
symmetry is essential to the understanding of the appearance of exotic Majorana fermions - particles that are their
own antiparticles - in topological superfluids.
5. Momentum- or spatially-resolved radio-frequency spectrum
Radio-frequency (rf) spectroscopy, including both momentum-resolved and spatially-resolved rf-spectroscopy, is a
powerful tool to characterize interacting many-body systems. It has been widely used to study fermionic pairing in
a two-component atomic Fermi gas near Feshbach resonances in the BEC-BCS crossover [68–72]. Most recently, it
has also been used to detect new quasiparticles known as repulsive polarons [73, 74], which occur when “impurity”
fermionic particles interact repulsively with a fermionic environment.
The underlying mechanism of rf-spectroscopy is rather simple. The rf field drives transitions between one of the
hyperfine states (say, j#i) and an empty hyperfine state j3iwhich lies above it by an energy !3#. The Hamiltonian
describing this rf-coupling may be written as,
Vrf=V0
drh
y
3(r) #(r) + y
#(r) 3(r)i
; (33)
whereV0is the strength of the rf drive. For a weak rf field, the number of transferred atoms may be calculated using
linear response theory. At this point, it is important to note that a final state effect might be present, which is caused
by the interaction between atoms in the final third state and those in the initial spin-up or spin-down state. This
final state effect is significant for6Li atoms; while for40K atoms, it is not important [19].
For momentum-resolved rf spectroscopy [71], the momentum distribution of the transferred atoms can be obtained
by absorption imaging after a time-of-flight. This gives rise to the information about the single-particle spectral
function of spin-down atoms of the original Fermi system, A##(k;!). In the absence of the final-state effect, the rf
transfer strength (k;!)at a given momentum is given by,
(k;!) =A##(k;k !+!3#)f(k !+!3#): (34)9
Here, we have assumed that the atoms in the third state have the dispersion relation k=k2=(2m)in free space
and have taken the coupling strength V0= 1. Experimentally, we can either measure the momentum-resolved rf
spectroscopy along a particular direction, say, the x-direction, by integrating along the two perpendicular directions
(kx;!)X
ky;kz (k;!); (35)
or after integrating along the remaining direction, obtain the fully integrated rf spectrum (!)P
k (k;!). We
note that, in the extremely weakly interacting BCS and BEC regimes, where the physics is dominated by single-
particle or two-particle physics, respectively, we may use the Fermi golden rule to calculate the momentum-resolved
rf spectroscopy. This will be discussed in greater detail in the relevant subsections. We note also that momentum-
resolved rf spectroscopy is precisely an ultracold atomic analogue of the well-known angle-resolved photoemission
spectroscopy (ARPES) widely used in solid-state experiments.
Alternatively, we may use rf spectroscopy to probe the local information about the original Fermi system. This
was first demonstrated in measuring the pairing gap by using phase-contrast imaging within the local density approx-
imation for a trapped Fermi gas [69]. A more general idea is to use a specifically designed third state, which has a
very flat dispersion relation [75]. This leads to a spatially-resolved rf spectroscopy, which measures precisely the local
density of states of the Fermi system,
(r;!) =1
2X
h
ju(r)j2(! E) +jv(r)j2(!+E)i
: (36)
It could be regarded as a cold-atom scanning tunneling microscopy (STM). As we shall see, the spatially-resolved
rf spectroscopy will provide a useful although indirect measurement of the long-sought Majorana fermion in atomic
topological superfluids.
B. 1D equal-weight Rashba-Dresselhaus spin-orbit coupling
δ
/c173/c175
FIG. 1: Left panel: schematic of the Raman transition that produced the equal-weight Rashba-Dresselhaus SOC. The two
atomic states are labeled as j"iandj#i.is the two-photon Raman detuning. Right panel: schematic of the experimental
setup where a pair of Raman beams counter-propagate along the x-axis. Right figure taken from Ref. [11].
Let us now discuss the two specific types of SOC. One simple scheme to create SOC in cold atoms is through a
Raman transition that couples two hyperfine ground states of the atom, as schematically shown in Fig. 1. The Raman
process is described by the following single-particle Hamiltonian in the first-quantization representation
H0=^ p2
2m+1
2
ei2krx
e i2krx
; (37)
where ^ pis the momentum operator of the atom, 2kr^xis the photon recoil momentum taken to be along the x-axis,
and
arethetwo-photondetuningandthecouplingstrengthoftheRamanbeams, respectively. TheHamiltonianacts
on the Hilbert space expanded by the spin-up and spin-down basis, j"iandj#i. By applying a unitary transformation
with
U=
eikrx0
0e ikrx
; (38)10
the HamiltonianH0can be recast into the following form:
HSO=UyH0U=
^kx+kr^z2
2m+
^k2
y+^k2
z
2m+
2^x+
2^z: (39)
Here, ^k= (^kx;^ky;^kz)denotes the quasi-momentum operator of the atom: When ^kis applied to the transformed wave
function, it gives the atomic quasi-momentum kthat is related to the real momentum pas^p= (^kkr^x)with
for spin-up and down, respectively. From this expression, it is sometimes convenient to regard both
andas the
strengths of effective Zeeman fields.
We note that after a pseudo-spin rotation ( z!x,x! z), Hamiltonian (39) can be cast into the general
form of SOC in Eq. (18) with = (k2
r=m;0;0)andh= (=2;0;
=2). It is clear that the SOC is along a specific
direction. Actually, it is an equal-weight combination of the well-known Rashba and Dresselhaus SOCs in solid-state
physics [56]. For this reason, hereafter we would refer to it as 1D equal-weight Rashba-Dresselhaus SOC. We may
also refer to the detuning as the in-plane Zeeman field since it is aligned along the same direction as the SOC.
Accordingly, we call the coupling strength
as the out-of-plane Zeeman field. As we shall see, depending on and
, the spin-orbit coupled Fermi system can display distinct quantum superfluid phases at low temperatures.
1. Single-particle spectrum
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/s114
/s107
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/s114/s40/s107
/s121 /s61/s48/s44 /s107
/s122/s61/s48/s41/s47 /s69
/s114
/s40/s97/s41/s32 /s32/s61/s32/s48
FIG. 2: Single particle spectrum of a Fermi gas with 1D equal-weight Rashba-Dresselhaus SOC, with (a) or without detuning
(b). In each panel, we increase the coupling strength of the Raman beams from Erto5Er, with a step of Er, as indicated by
the arrows.
The single-particle spectrum can be easily obtained by diagonalizing the Hamiltonian (39), which is given by
Ek=Er+k2
2ms
22
+
kx+
22
; (40)
where we have defined a recoil energy Erk2
r=(2m)and an SOC strength kr=m. The spectrum contains two
branches as shown in Fig. 2. For small
, the lower branch exhibits a double-well structure. The double wells are
symmetric (asymmetric) for = 0(6= 0). For large
, the two wells in the lower branch merge into a single one.
It is important to emphasize that in each branch atoms stay at a mixed spin state with both spin-up and down
components.
The single-particle spectrum can be easily measured by using momentum-resolved rf spectroscopy, as already shown
at Shanxi University and MIT [11, 12]. In this case, the number of transferred atoms can be calculated by using the
Fermi’s golden rule [76]:
(kx;!) =X
i;fjhfjVrfjiij2f(Ei )[! !3# (Ef Ei)]; (41)
where the summation is over all possible initial single-particle states i(with energy Eiand a given wavevector kx)
and final states f(with energy Ef), and the Dirac -function ensures energy conservation during the rf transition. In
practice, the -function is replaced by a function with finite width (e.g., (x)!(
=)(x2+
2) 1where
accounts for11
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/s107
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/s114
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/s47/s69
/s114
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/s114
/s107
/s110/s120/s47/s107
/s114/s48
/s48/s46/s48/s53
/s48/s46/s49
FIG.3: Theoreticalsimulationonmomentum-resolvedrfspectroscopyofaFermigaswith1Dequal-weightRashba-Dresselhaus
SOC.Leftpanel: simulatedexperimentalspectroscopy (kx;!). Rightpanel: thespectroscopy (knxkx+kr;~!=!+k2
x=2m).
Here, theintensityofthecontourplotshowsthenumberoftransferredatoms, increasinglylinearlyfrom0(blue)toitsmaximum
value (red). We have set !3#= 0and used a Lorentzian distribution to replace the Delta function. Figure taken from Ref. [76]
with modification.
the energy resolution of the measurement). The single-particle wave function iis known from the diagonalization of
the Hamiltonian (39) and the transfer element hfjVrfjiiis then easy to determine. The left panel of Fig. 3 shows
the predicted momentum-resolved spectroscopy (kx;!)at= 0and
= 2Er. The chemical potential is tuned
(= 5Er) in such a way that there are significant populations in both energy branches. The simulated spectrum is
not straightforward to understand, because of the final free-particle dispersion relation in the energy conservation in
Eq. (41) and also the recoil momentum shift ( kr) arising from the unitary transformation Eq. (38). Therefore, it is
useful to define
~ (knx;~!)
kx+kr;!+k2
x
2M
; (42)
for which, the energy conservation takes the form [~!+Ei(kx)]. As shown on the right panel of Fig. 3, the single-
particle spectrum is now clearly visible.
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/s114
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/s114
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/s114
/s107
/s110/s120/s47/s107
/s114/s126/s48
/s48/s46/s48/s53
/s48/s46/s49
FIG. 4: Theoretical simulation on momentum-resolved rf spectroscopy of a Fermi gas with 1D equal-weight Rashba-Dresselhaus
SOC and an additional spin-orbit lattice. The left and right panels show (kx;!)and (knxkx+kr;~!=!+k2
x=2m),
respectively. The white lines on the right panel are the calculated energy band structure. The spin-orbit lattice depth is
rf=Erand the other parameters are the same as in Fig. 3. Figure taken from Ref. [76] with modification.
Experimentally, the single-particle properties of the Fermi gas can also be easily tuned, for example, by using
an additional rf field to couple spin-up and down states [12]. After the gauge transformation, it introduces a term
(
=2)[cos(2krx)^x+ sin(2krx)^y]in the spin-orbit Hamiltonian Eq. (39), which behaves like a spin-orbit lattice and
leads to the formation of energy bands. In Fig. 4, we show the simulation of momentum-resolved rf spectroscopy12
under such an rf spin-orbit lattice. The energy band structure is apparent. We refer to Ref. [76] for more details
on the theoretical simulations, in particular the simulations in a harmonic trap. The relevant measurements will be
discussed in greater detail later in the section on experiments.
2. Two-body physics
We now turn to consider the interatomic interaction. The interplay between interatomic interaction and SOC can
lead to a number of intriguing phenomena, even at the two-particle level. Let us first solve numerically the energy
E(q)of the two-particle states by using the general eigenenergy equation Eq. (19). A true bound state must satisfy
E(q)<2Emin, whereEminis the single-particle ground state energy.
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/s114/s97
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/s114/s41/s40/s97/s41
/s48/s46/s48 /s48/s46/s53 /s49/s46/s48 /s49/s46/s53 /s50/s46/s48/s49/s46/s48/s48/s49/s46/s48/s53/s49/s46/s49/s48/s49/s46/s49/s53/s49/s46/s50/s48
/s32/s32
/s32/s49/s47/s40 /s107
/s114/s97
/s115/s41/s32/s32 /s47/s69
/s114/s61/s48/s46/s56
/s32 /s47/s69
/s114/s61/s50/s46/s48
/s32 /s47/s69
/s114/s61/s51/s46/s50/s40/s98/s41
FIG. 5: Energy E(q= 0)(a) and effective mass ratio
=Mx=(2m)(b) of the two-particle ground bound state in the
presence of 1D equal-weight Rashba-Dresselhaus SOC, at zero detuning = 0and at three coupling strengths of Raman beams:
= 0:8Er(solid line), 2Er(dashed line), and 3:2Er(dot-dashed line). The horizontal dotted lines in (a) correspond to the
threshold energies 2Eminwhere the bound states disappear. Figure taken from Ref. [66] with modification.
At zero detuning = 0, the two-particle ground state has zero center-of-mass momentum q= 0[66]. In Fig. 5(a),
we show its energy as a function of the dimensionless interaction parameter 1=(kras). In the presence of 1D equal-
weight Rashba-Dresselhaus SOC, a two-particle bound state occurs on the BEC side with a positive s-wave scattering
lengthas>0. The effective out-of-plane Zeeman field
acts as a pair-breaker and pushes the threshold scattering
length to the BEC limit. In other words, the position of the Feshbach resonance, originally located at as=1, now
shifts to the BEC side with at lower magnetic field strengths [14]. By calculating the dispersion relation E(q)around
q= 0, we are able to determine the effective mass, as shown in Fig. 5(b). It is interesting that the effective mass along
the direction of SOC is greatly altered. It becomes much larger than 2mtowards the threshold scattering length. In
the deep BEC limit, 1=(kras)!1, where two atoms form a tightly bound molecule, the mass is less affected by the
SOC or the effective Zeeman field, as we may anticipate.
0 0.1 0.2 0.3 0.4 0.500.20.40.60.81
1234567x□10
0 0.1 0.2 0.3 0.4 0.500.20.40.60.81
00.20.40.60.81
(a) (b)
/ 2rE/c1002rE/c87
/ 2rE/c100
FIG. 6: Binding energy Eb= 2Emin Eq0and the magnitude of the lowest-energy bound state momentum q0as functions of
and
. The coloring in (a) represents Eb=Er, and that in (b) represents q0=kr. In the upper right corner of both (a) and (b),
there exist no bound states. The scattering length is given by 1=(kras) = 1. Figure taken from Ref. [26] with modifications.13
At nonzero detuning 6= 0, the result shows that the two-particle bound state will have its lowest energy at a finite
center-of-mass momentum q0= (q0;0;0)[26, 30]. Fig. 6 shows the binding energy and the magnitude of q0of the
lowest-energy bound state. That the two-particle ground states possessing a finite momentum implies that the Cooper
pairs, which is a many-body counterpart of two-particle bound state, may acquire finite center-of-mass momentum
and therefore condense into an inhomogeneous superfluid state. This possibility will be addressed in greater detail
later. We note that with the typical parameters, i.e.,
ErandEr,q0is small and less than 1% of the recoil
momentum kr, as shown in Fig. 6(b). However, its magnitude can be significantly enhanced by many-body effect.
For Cooper pairs in the ground state, q0can be tuned to be comparable with kror the Fermi wavevector kF[33].
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/s32
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/s66
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/s69
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/s66/s61/s49/s70 /s40 /s41
/s47/s69
/s66/s40/s98/s41/s32/s48/s46/s53
FIG. 7: (a) Momentum-resolved rf spectroscopy (a) and integrated rf spectroscopy (b) of the two-particle bound state at = 0
and
= 2Er. The energy of rf photon !is measured in units of a binding energy EB1=(ma2
s)and we have set !3#= 0. In
the right panel, the dashed line in the main figure plots the rf line-shape in the absence of SOC: F(!) = (2=)p! EB=!2.
The inset highlights the different contribution from the two final states, as described in the text. Figure taken from Ref. [65]
with modification.
Ideally, momentum-resolved rf-spectroscopy can be used to probe the two-particle bound state discussed above. We
can perform a numerical simulation of the spectroscopy by using again the Fermi’s golden rule. Let us assume that
a bound molecule is initially at rest in the state j2Biwith energy Ei. An rf photon with energy !will break the
molecule and transfer the spin-down atom to the third state j3i. In the case that there is no final-state effect, the
final statejficonsists of a free atom in j3iand a remaining atom in the spin-orbit system. According to the Fermi’s
golden rule, the rf strength (!)of breaking molecules and transferring atoms is proportional to the Franck-Condon
factor [77],
F(!) =jhfjVrfj2Bij2[! !3# (Ef Ei)]: (43)
The integrated Franck-Condon factor satisfies the sum rule,+1
1F(!)d!= 1. A closed expression of F(!)is
derived in Refs. [65] and [66], by carefully analyzing the initial two-particle bound state j2Biand the final state
jfi. Furthermore, by resolving the momentum of transferred atoms, we are able to obtain the momentum-resolved
Franck-Condon factor F(kx;!).
Figs. 7(a) and 7(b) illustrate respectively the momentum-resolved and the integrated rf spectrum of the two-particle
ground state at zero detuning = 0. One can easily resolve two different responses in the spectrum due to two different
final states, as the remaining spin-up atom in the original spin-orbit system can occupy either the upper or the lower
energy branch. Indeed, in the integrated rf spectrum, we can separate clearly the different contributions from the two
final states, as highlighted in the inset. This gives rise to two peaks in the integrated spectrum. We note that the
lower peak exhibits a red shift as the SOC strength increases, due to the decrease of the binding energy. It is also
straightforward to calculate the rf spectrum of the two-particle bound state at nonzero detuning 6= 0(not shown in
the figure). However, the spectrum remains essentially unchanged, due to the fact that the center-of-mass momentum
q0is quite small with typical experimental parameters.
3. Momentum-resolved radio-frequency spectrum of the superfluid phase
Consider now the many-body state. As we mentioned earlier, since the two-particle wave function contains both
spin singlet and triplet components, we anticipate that the superfluid phase at low temperatures would involve both
s-wave pairing and high-partial-wave pairing. Therefore, in general it is an anisotropic superfluid. This is to be
discussed later in detail for 2D Rashba SOC. Here, we are interested in the phase diagram and the experimental probe14
of a 3D Fermi gas with 1D equal-weight Rashba-Dresselhaus SOC. First, let us concentrate on the case with zero
detuning= 0, by using the many-body T-matrix theory within the pseudogap approximation [13].
/s45/s49/s46/s48 /s45/s48/s46/s53 /s48/s46/s48 /s48/s46/s53 /s49/s46/s48/s48/s46/s48/s48/s46/s49/s48/s46/s50/s48/s46/s51/s48/s46/s52
/s48/s46/s48 /s48/s46/s49 /s48/s46/s50 /s48/s46/s51/s48/s46/s48/s48/s46/s50/s48/s46/s52/s48/s46/s54
/s32/s32/s115/s47
/s70
/s84 /s47/s84
/s70
/s84/s42/s32/s61/s32/s50 /s69
/s114
/s32/s32/s84 /s47/s84
/s70
/s49/s47/s40 /s107
/s70/s97
/s115/s41/s115/s117/s112/s101/s114/s102/s108/s117/s105/s100/s84
/s99
FIG. 8: (a) Phase diagram of a spin-orbit coupled Fermi gas at the BEC-BCS crossover at
= 2ErandkF=kr. The
main figure and inset show the superfluid transition temperature and the superfluid order parameter at resonance, respectively,
predicted by using our T-matrix theory (solid line) and the BCS mean-field theory (dashed line). Figure taken from Ref. [13]
with modification.
Focusing on the vicinity of the Feshbach resonance where as!1, in Fig. 8 we show the superfluid transition
temperature Tcand the pair breaking (pseudogap) temperature Tof the spin-orbit coupled Fermi gas at
= 2Er
andkF=kr. The pseudogap temperature is calculated using the standard BCS mean-field theory without taking into
account the preformed pairs (i.e., pg= 0) [57, 67]. We find that the region of superfluid phase is strongly suppressed
by SOC. In particular, at resonance the superfluid transition temperature is about Tc'0:08TF, which is significantly
smaller than the experimentally determined Tc'0:167(13)TFfor a unitary Fermi gas [78]. Thus, it seems to be a
challenge to observe a novel spin-orbit coupled fermionic superfluid in the present experimental scheme.
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/s115/s32/s61/s32
FIG.9: Zero-temperature momentum-resolvedrf-spectroscopyof aspin-orbitcoupled Fermigas acrossthe Feshbach resonance,
at the parameters
= 2ErandkF=kr. Figure taken from Ref. [13] with modification.
In Figs. 9(a)-9(c), we show the zero-temperature momentum-resolved rf spectrum across the resonance. On the
BCS side ( 1=kFas= 0:5), the spectrum is dominated by the response from atoms and shows a characteristic high-
frequency tail at kx<0[11, 12, 76], see for example, the left panel of Fig. 3. We note that the density of the Fermi
cloud, chosen here following the real experimental parameters [11], is low and therefore only the lower energy branch
is occupied at low temperatures. Towards the BEC limit ( 1=kFas= +0:5), the spectrum may be understood from the
picture of well-defined bound pairs and shows a clear two-fold anisotropic distribution, as we already mentioned in
Fig. 7(a) [65]. The spectrum at the resonance is complicated and might be attributed to many-body fermionic pairs.
It is interesting that the response from many-body pairs has a similar tail at high frequency as that from atoms. The
change of the rf spectrum across the resonance is continuous, in accordance with a smooth BEC-BCS crossover.15
4. Fulde-Ferrell superfluidity
The nature of superfluidity can be greatly changed by a nonzero detuning 6= 0. As we discussed earlier in the
two-body part, in this case, the Cooper pairs may carry a nonzero center-of-mass momentum and therefore condense
into an inhomogeneous superfluid state, characterized by the order parameter 0(r) = 0eiqr. This exotic superfluid
has been proposed by Fulde and Ferrell [63], soon after the discovery of the seminal BCS theory. Its existence has
attracted tremendous theoretical and experimental efforts over the past five decades [79]. Remarkably, to date there is
still no conclusive experimental evidence for FF superfluidity. Here, we show that the superfluid phase of a 3D Fermi
gas with 1D equal-weight Rashba-Dresselhaus SOC and finite in-plane effective Zeeman field is precisely the long-
sought FF superfluid [33]. The same issue has also been addressed very recently by Vijay Shenoy [30]. We note that
the FF superfluid can appear in other settings with different types of SOC and dimensionality [29, 31, 32, 34–36, 80].
Theoretically, to determine the FF superfluid state, we solve the BdG equation (29) with VT(r) = 0by using the
following ansatz for quasiparticle wave functions
k(x) =eikx
p
Vh
uk"e+iqx=2;uk#e+iqx=2;vk"e iqx=2;vk#e iqx=2iT
: (44)
The center-of-mass momentum qis assumed to be along the x-direction, inspired from the two-body solution [26].
The mean-field thermodynamic potential
0at temperature Tin Eq. (10) is then given by
0
V=1
2V2
4X
k
k+q=2+k q=2
X
kEk3
5 kBT
VX
kln
1 +e Ek=kBT
2
0
U0; (45)
whereEk(= 1;2;3;4) is the quasiparticle energy. Here, the summation over the quasiparticle energy must be
restricted to Ek0because of an inherent particle-hole symmetry in the Nambu spinor representation. For a
given set of parameters (i.e, the temperature T, interaction strength 1=kFas, etc.), different mean-field phases can
be determined using the self-consistent stationary conditions: @
=@ = 0,@
=@q= 0, as well as the conservation of
total atom number, N= @
=@. At finite temperatures, the ground state has the lowest free energy F=
+N.
In the following, we consider the resonance case with a divergent scattering length 1=kFas= 0and setT= 0:05TF,
whereTFis the Fermi temperature. According to the typical number of atoms in experiments [11, 12], we take the
Fermi wavevector kF=kr.
/s48/s46/s48 /s48/s46/s50 /s48/s46/s52 /s48/s46/s54 /s48/s46/s56 /s49/s46/s48/s45/s48/s46/s56/s52/s45/s48/s46/s56/s50/s45/s48/s46/s56/s48/s45/s48/s46/s55/s56
/s48/s46/s48/s48/s46/s50/s48/s46/s52/s48/s46/s54
/s48/s46/s48/s48/s46/s50/s48/s46/s52/s48/s46/s54/s45/s48/s46/s48/s48/s48/s50/s48/s46/s48/s48/s48/s48/s48/s46/s48/s48/s48/s50
/s48/s46/s48 /s48/s46/s53 /s49/s46/s48/s48/s46/s50/s48/s46/s52/s48/s46/s54
/s32/s32
/s32/s32
/s47/s69
/s70
/s113 /s47/s107
/s70/s32/s70 /s70
/s32/s66/s67/s83
/s32/s78/s111/s114/s109/s97/s108/s70 /s40 /s41/s47/s40 /s78/s69
/s70/s41
/s47/s69
/s70/s40/s98/s41
/s32/s43
/s43/s78/s66/s67/s83
/s47
/s69
/s70/s113/s47/s107/s70/s40/s97/s41
/s109/s102
/s70/s70
/s43
FIG. 10: (a) Landscape of the thermodynamic potential,
mf= [
0(;q)
0(0;0)]=(NEF), at
= 2EFand= 0:68EF.
The chemical potential is fixed to = 0:471EF. The competing ground states include (i) a normal Fermi gas with 0= 0;
(ii) a fully paired BCS superfluid with 06= 0andq= 0; and (iii) a finite momentum paired FF superfluid with 06= 0and
q6= 0. (b) The free energy of different competing states as a function of the detuning at
= 2EF. The inset shows the detuning
dependence of the order parameter and momentum of the FF superfluid state. Figure taken from Ref. [33] with modification.
Ingeneral, foranysetofparameterstherearethreecompetinggroundstatesthatarestableagainstphaseseparation
(i.e.,@2
0=@2
00), as shown in Fig. 10(a): normal gas ( 0= 0), BCS superfluid ( 06= 0andq= 0), and FF
superfluid ( 06= 0andq6= 0). Remarkably, in the presence of spin-orbit coupling the FF superfluid is always more
favorable in energy than the standard BCS pairing state at finite detuning (Fig. 10(b)). It is easy to check that
the superfluid density of the BCS pairing state in the SOC direction becomes negative (i.e., @
0=@q < 0), signaling
the instability towards an FF superfluid. Therefore, experimentally the Fermi gas would always condense into an16
/s48 /s49 /s50 /s51 /s52/s48/s46/s48/s48/s46/s50/s48/s46/s52/s48/s46/s54/s48/s46/s56/s49/s46/s48/s49/s46/s50
/s32/s49/s69/s45/s48/s52
/s48/s46/s48/s49
/s49/s49/s48/s52
/s49/s48/s50
/s49/s70/s117/s108/s100/s101/s45/s70/s101/s114/s114/s101/s108/s108/s32/s115/s117/s112/s101/s114/s102/s108/s117/s105/s100
/s40/s103/s97/s112/s108/s101/s115/s115/s41/s47/s69
/s70
/s47/s69
/s70/s78/s111/s114/s109/s97/s108/s32/s70/s101/s114/s109/s105/s32/s103/s97/s115
/s40/s103/s97/s112/s112/s101/s100/s41
FIG. 11: Phase diagram as a function of and
, atT= 0:05TF. By increasing , the Fermi cloud changes from a FF
superfluid to a normal gas, via first-order (dashed line) and second-order (solid line) transitions at low and high
, respectively.
The FF superfluid can be either gapped or gapless, as separated by the dot-dashed line. The coloring represents the magnitude
of the centre-of-mass momentum of Cooper pairs, q=kF. The BCS superfluid occurs at
= 0or= 0only. Figure taken from
Ref. [33] with modification.
FF superfluid at finite two-photon detuning. In Fig. 11, we report a low-temperature phase diagram that could be
directly observed in current experiments. The FF superfluid occupies the major part of the phase diagram.
/s45/s49 /s48 /s49/s43/s43
/s48/s46/s49
/s40/s99/s41/s32 /s32/s61/s32/s48/s46/s56 /s69
/s70/s32
/s32
/s107
/s120/s47/s107
/s70/s49 /s46 /s48 /s48 /s48 /s69 /s45/s48 /s52
/s48 /s46 /s49 /s48 /s48 /s48 /s49/s48/s45 /s52
/s45/s49 /s48 /s49/s48/s49/s50/s51/s52
/s43/s32
/s32
/s107
/s120/s47/s107
/s70/s47/s69
/s70
/s40/s97/s41/s32 /s32/s61/s32/s48/s43
/s45/s49 /s48 /s49/s43/s43
/s40/s98/s41/s32 /s32/s61/s32/s48/s46/s52 /s69
/s70
/s32
/s107
/s120/s47/s107
/s70
FIG. 12: Logarithmic contour plot of momentum-resolved rf spectroscopy: number of transferred atoms (kx;!)at
= 2EF
and at three detunings: (a) = 0andq= 0, (b)= 0:4EFandq'0:1kF, and (c)= 0:8Eandq'0:6kF. Figure taken from
Ref. [33] with modification.
The experimental probe of an FF superfluid is a long-standing challenge. Here, unique to cold atoms, momentum-
resolved rf spectroscopy may provide a smoking-gun signal of the FF superfluidity. The basic idea is that, since Cooper
pairscarryafinitecenter-of-massmomentum q, thetransferredatomsintherftransitionacquireanoverallmomentum
q=2. As a result, there would be a q=2shift in the measured spectrum. In Fig. 12, we show the momentum-resolved
rf spectrum (kx;!)on a logarithmic scale. As we discussed earlier in the two-body part, there are two contributions
to the spectrum, corresponding to two different final states [65]. These two contributions are well separated in the
frequency domain, with peak positions indicated by the symbols “ +” and “”, respectively. Interestingly, at finite
detuning with a sizable FF momentum q, the peak positions of the two contributions are shifted roughly in opposite
directions by an amount q=2. This provides clear evidence for observing the FF superfluid.17
5. 1D topological superfluidity
Arguably, the most remarkable aspect of SOC is that it provides a feasible routine to realize topological superfluids
[38], which have attracted tremendous interest over the past few years [81]. In addition to providing a new quantum
phaseofmatter, topologicalsuperfluidscanhostexoticquasiparticlesattheirboundaries, knownasMajoranafermions
- particles that are their own antiparticles [82, 83]. Due to their non-Abelian exchange statistics, Majorana fermions
are believed to be the essential quantum bits for topological quantum computation [84]. Therefore, the pursuit for
topological superfluids and Majorana fermions represents one of the most important challenges in fundamental science.
Anumberofsettingshavebeenproposedfortherealizationoftopologicalsuperfluids, includingthefractionalquantum
Hall states at filling = 5=2[85], vortex states of px+ipysuperconductors [86, 87], and surfaces of three-dimensional
(3D) topological insulators in proximity to an s-wave superconductor [88], and one-dimensional (1D) nanowires with
strong spin-orbit coupling coated also on an s-wave superconductor [89]. In the latter setting, indirect evidences of
topological superfluid and Majorana fermions have been reported [90]. Here, we review briefly the possible realizations
of topological superfluids, in the context of a 1D spin-orbit coupled atomic Fermi gas [45, 47, 51, 55], which can be
prepared straightforwardly by loading a 3D spin-orbit Fermi gas into deep 2D optical lattices. Later, we will discuss
2D topological superfluids with Rashba SOC.
/s48 /s49 /s50 /s51 /s52/s48/s46/s48/s48/s46/s53/s49/s46/s48/s49/s46/s53
/s48 /s49 /s50 /s51 /s52/s48/s46/s48/s48/s46/s53/s49/s46/s48/s49/s46/s53
/s113 /s47/s107
/s70/s32 /s32/s32
/s47/s69
/s70/s47/s69
/s70/s32/s61/s32/s48/s46/s54 /s69
/s70
/s32/s32/s69
/s109 /s105/s110/s47/s69
/s70
/s47/s69
/s70/s66/s47/s40/s50 /s41
FIG. 13: Theoretical examination of the topological phase transition at the detuning = 0:6EFandT= 0. The transition
occurs at
'2:46EF, where the energy gap of the system (solid line) close and then open. The Berry phase
Bisand 0
at the topologically trivial and non-trivial regimes (circles). The insets shows the order parameter and momentum of the FF
superfluid, as a function of the Rabi frequency. Figure taken from Ref. [55] with modification.
Consider first a homogeneous 1D Fermi gas with a nonzero detuning 6= 0[55]. In this case, we actually anticipate a
topological inhomogeneous superfluid, where the order parameter also varies in real space. Using the same theoretical
technique as in the previous subsection, we solve the BdG equation (29) in 1D and then minimize the mean-field
thermodynamic potential Eq. (45) to determine the pairing gap 0and the FF momentum q.
In Fig. 13, we show the energy gap as a function of
at= 0:6EFandT= 0. For this result, we use a Fermi
wavevector kF= 0:8krand take a dimensionless interaction parameter
mg1D=(n) = 3, whereg1Dis the strength
of the 1D contact interaction and n= 2kF=is the 1D linear density. Topological phase transition is associated with
a change of the topology of the underlying Fermi surface and therefore is accompanied with closing of the excitation
gap at the transition point. In the main figure this feature is clearly evident. To better characterize the change of
topology, we may calculate the Berry phase defined by [47]
B=i+1
1dk
W
+(k)@kW+(k) +W
(k)@kW (k)
: (46)
HereW(k)[uk"eiqz=2;uk#eiqz=2;vk"e iqz=2;vk#e iqz=2]Tdenotes the wave function of the upper (= +)and
lower (= )branch, respectively. In Fig. 13, the Berry phase is shown by circles. It jumps from to0, right
across the topological phase transition. It is somewhat counter-intuitive that the
B= 0sector corresponds to the
topologically non-trivial superfluid state. It is important to emphasize the inhomogeneous nature of the superfluid.18
Indeed, as shown in the inset, the FF momentum qincreases rapidly across the topological superfluid transition and
reaches about 0:3kFat
= 4EF:
/s48 /s49 /s50 /s51 /s52/s48/s46/s48/s48/s46/s53/s49/s46/s48/s49/s46/s53
/s84/s111/s112/s111/s45/s66/s67/s83/s66/s67/s83/s84/s111/s112/s111/s45/s70/s70
/s32/s32/s47/s69
/s70
/s47/s69
/s70/s70/s70
FIG.14: Zero-temperaturephasediagram. Atopologicallynon-trivialFFsuperfluidappearswhentheRamancouplingstrength
is above a threshold at finite detunings . Depending on the detuning, the transition could be either continuous (solid line)
or of first order (dashed line). The FF superfluid reduces to a BCS superfluid when
= 0or= 0. Figure taken from Ref.
[55] with modification.
InFig. 14, wepresentthezero-temperaturephasediagramforthetopologicalphasetransition. Thecriticalcoupling
strength
cdecreases with the increase of the detuning . At zero detuning,
ccan be determined analytically, since
the expression for the BdG eigenenergy for single-particle excitations (after dropping a constant energy shift Er) is
known [24, 47],
Ek=
2
k+2k2+
2=4 + 2
0q
42
k2k2+
2(2
k+ 2
0)1=2
; (47)
wherek=k2=(2m) and=kr=m. It is easy to see that the excitation gap closes at k= 0for the lower branch
(i.e.,= ), leading to the well-known result [89]
c
2=p
2+ 2: (48)
This criterion for topological superfluids is equivalent to the condition that there are only two Fermi points on the
Fermi surface [39], under which the Fermi system behaves essentially like a 1D weak-coupling p-wave superfluid.
Let us now turn to the experimentally realistic situation with a 1D harmonic trap VT(x) =m!2x2=2and focus on
the case with = 0[45, 47, 51]. The BdG equation (29) can be solved self-consistently by expanding the Nambu
spinor wave function (x)onto the eigenfucntion basis of the harmonic oscillator. In this trapped environment,
Majorana fermions with zero energy are anticipated to emerge at the boundary, if the Fermi gas stays in a topological
superfluid state. The appearance of Majorana fermions can be easily understood from the particle-hole symmetry
obeyed by the BdG equation, which states that every physical state can be described either by a particle state with
a positive energy Eor a hole state with a negative energy E. The Bogoliubov quasiparticle operators associated
with these two states therefore satisfy E= y
E. At the boundary, Eq. (48) could be fulfilled at some points and
give locally the states with E= 0. These states are Majorana fermions, as the associated operators satisfy 0= y
0-
precisely the defining feature of a Majorana fermion [82, 83].
In Fig. 15(a), we present the zero-temperature phase diagram of a trapped 1D Fermi gas at kF= 2krand
=[51]. The transition from BCS superfluid to topological superfluid is now characterized by the appearance of
Majorana fermions, whose energy is precisely zero and therefore the minimum of the quaisparticle spectrum touches
zero, minfjEjg= 0. In the topological superfluid phase, as shown in Fig. 15(b) with
= 2:4EF, the Majorana
fermions may be clearly identified by using spatially-resolved rf spectroscopy. We note that for a trapped Fermi gas
with weak interatomic interaction and/or high density, the upper branch of single-particle spectrum may be populated
at the trap center, leading to four Fermi points on the Fermi surface. This violates Eq. (48). As a result, we may find
a phase-separation phase in which the topological superfluid occurs only at the two wings of the Fermi cloud. This
situation has been discussed in Ref. [45].19
/s48/s46/s56 /s48/s46/s57 /s49/s46/s48 /s49/s46/s49 /s49/s46/s50 /s49/s46/s51 /s49/s46/s52/s48/s46/s48/s48/s46/s49/s48/s46/s50/s48/s46/s51/s48/s46/s52/s48/s46/s53/s48/s46/s54
/s48/s46/s48 /s48/s46/s53 /s49/s46/s48/s45/s48/s46/s53/s48/s46/s48/s48/s46/s53/s32
/s40/s60 /s120/s50
/s62/s41/s49/s47/s50
/s47/s120
/s70/s69 /s47/s69
/s70/s84/s111/s112/s111/s108/s111/s103/s105/s99/s97/s108/s32/s115/s117/s112/s101/s114/s102/s108/s117/s105/s100/s32/s109/s105/s110/s123/s124 /s69 /s124/s125/s47 /s69
/s70
/s47/s40/s50 /s69
/s70/s41/s66/s67/s83/s32/s115/s117/s112/s101/s114/s102/s108/s117/s105/s100
/s40/s97/s41
/s45/s49/s46/s48 /s45/s48/s46/s53 /s48/s46/s48 /s48/s46/s53 /s49/s46/s48/s45/s49/s46/s48/s45/s48/s46/s53/s48/s46/s48/s48/s46/s53/s49/s46/s48
/s40/s98 /s41
/s32/s32/s32
/s32/s47/s69
/s70
/s120 /s47/s120
/s70/s48
/s49
/s50
FIG. 15: (a) Zero-temperature phase diagram of a trapped 1D spin-orbit coupled Fermi gas, determined from the behavior of
the lowest energy in quasiparticle spectrum. The inset shows the energy spectrum at
= 2:4EFas a function of the position
of quasiparticles. A zero-energy quasiparticle (i.e., Majorana fermion) at the trap edge has been highlighted by a big dark
circle. Here, the position of a quasiparticle is approximately characterized by:
x2
=
dxx2P
[u2
(x) +2
(x)].xFis the
Thomas-Fermi radius of the cloud. (b) Linear contour plot of the local density of state at
= 2:4EF. At each trap edge, a
series of edge states, including the zero-energy Majorana fermion mode, are clearly visible. Figure taken from Ref. [51] with
modification.
C. 2D Rashba spin-orbit coupling
Let us now discuss Rashba SOC, which takes the standard form VSO=(^ky^x ^kx^y)[91]. The coupling between
spin and orbital motions occurs along two spatial directions and therefore we shall refer to it as 2D Rashba SOC.
This type of SOC is not realized experimentally yet, although there are several theoretical proposals for its realization
[92, 93]. The superfluid phase with 2D Rashba SOC at low temperatures shares a lot of common features as its
1D counterpart as we reviewed in the previous subsection. Here we focus on some specific features, for example, the
two-particle bound state at sufficiently strong SOC strength - the rashbon [21, 25] - and the related crossover to a BEC
of rashbons. We will also discuss in greater detail the 2D topological superfluid with Rasbha SOC in the presence of
an out-of-plane Zeeman field, since it provides an interesting platform to perform topological quantum computation.
We note that experimentally it is also possible to create a 3D isotropic SOC, VSO=(^kx^x+^ky^y+^kz^z), where
the spin and orbital degree of freedoms are coupled in all three dimensions [94]. We note also that early theoretical
works on a Rashba spin-orbit coupled Fermi gas was reviewed very briefly by Hui Zhai in Ref. [95].
/s45/s52 /s45/s50 /s48 /s50 /s52/s48/s49/s50/s51/s52
/s101/s102/s102/s61/s48/s101/s102/s102/s61/s49/s40 /s41
/s47/s69
/s70/s101/s102/s102/s61/s50
FIG. 16: Left panel: schematic of the single-particle spectrum in the kx kyplane. A energy gap opens at k= 0, due to a
nonzero out-of-plane Zeeman field h. Right panel: density of states of a 3D homogeneous Rashba spin-orbit coupled system at
several SOC strengths, in units of mkF. Right figure taken from Ref. [96] with modification.20
1. Single-particle spectrum
In the presence of an out-of-plane Zeeman field h^z, the single-particle spectrum is given by,
Ek=k2
2mq
2
k2x+k2y
+h2: (49)
The spectrum with a nonzero his illustrated on the left panel of Fig. 16. Compared with the single-particle spectrum
with 1D equal-weight Rashba-Dresselhaus SOC in Fig. 2, it is interesting that the two minima in the lower energy
branch now extend to form a ring structure. At low energy, therefore, we may anticipate that in the momentum space
the particles will be confined along the ring. The effective dimensionality of the system is therefore reduced. Indeed,
it is not difficult to obtain the density of states ( h= 0) [96]:
(!) = (mkF)8
><
>:0;
!< |