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B.4 Spin geodesic precession

The spin precession can be evaluated using the following equation:
ij dM-A- −2 [i j] −2 [ij] dτ = − 2ε vAP A − 2ε R A . (227 )
Evaluating the surface integrals in ij R A and i Q A (appearing through the momentum-velocity relation), we have up to 2 ε
( ) ( ) -d- M ij1 + 2v[1iDj1] = ε2m2- 2n[1i2M j1]kvk1 − 4v[i1M j1]knk12 − 4n [i12M j1]kvk2 + 4v[2iM j1]knk12 dτ r12 26m2- k [i j]k + ε r3 n12n12I1 12 ( ) + ε22m2- nk ni Zk[jl]l− nk nj Zk [il]l+ nk ni Zj [kl]l− nk ni Zj [kl]l r312 12 12 1 12 12 1 12 12 1 12 12 1 + 𝒪 (ε3). (228 )
Note that there is no monopole-monopole coupling.

In our formalism, the above form is sufficient since we use M iAj, not the spin vector siA. To transform the above equation into the usual form, we take a “crude” method; we shall treat one star, say, the star 1 as if it felt only the gravitational field of the companion star. Motivated by the formalism on extended bodies by Dixon [69], we introduce the intrinsic spin four-vector 𝒮Aμ and the intrinsic spin tensor ℳ μν A as

2ε−6 ∫ ℳ μAν = √---- d3Σ ρσ[AμΛνN]ρ, (229 ) − g ℬA 1- ρσ α 𝒮Aμ = 2εαρσμℳ A u A, (230 )
where εαρσμ is the totally anti-symmetric symbol with ε0123 = 1. 3 d Σα is the proper volume element satisfying d3Σ [αuA β] = 0. ℬA is a three-sphere surrounding star A whose normal is uA α and whose radius is εRA. σμA is the spacelike four-vector satisfying gμνσAμu μA = 0. The four-momentum is normalized as gμνuμuν = ε−2 A A. The above definitions imply the spin supplementary condition
μ μ μν 𝒮Aμu A = 0, or equivalently, 𝒟 A = − ℳ A uAμ = 0, (231 )
where 𝒟 μ A is the intrinsic dipole moment. Now we construct a coordinate transformation from the near zone μ i x = (τ,x ) to the Fermi normal coordinates ˆρ ˆi σA = (ˆτ ,σ ) (see e.g. Section 40.7 in [122Jump To The Next Citation Point]),
ˆρ ˆρ μ σA = eAμx , (232 ) ˆτ 1-2 2 2m2- e1τ = 1 + 2ε v1 − ε r , (233 ) ˆτ 2 12 e1i = −( ε v1i, ) (234 ) ˆı 2m2 i 1 2 i e1j = 1 + ε --- δj + -ε v1v1j. (235 ) r12 2
Then we express the intrinsic spin tensor in the Fermi normal coordinates in terms of the moments in the near zone. Using d3Σ α = − uAα(1 + ε2m2 ∕r12 − ε2v2∕2 ) 1, we have
[( 1 2m ) 1 ] ℳ ˆıˆτ1 = 1 + -ε2v21 − ε2---2 δij − -ε2vi1vj1 Dj1 − ε2M i1kvk1 + 𝒪 (ε3), (236 ) 2 r12 2 ˆıˆj ij 2 k [i j]k 3 ℳ 1 = M 1 + ε v1v1M 1 + 𝒪 (ε ). (237 )
Now defining the intrinsic center of mass by setting 𝒟 μA = ℳ ˆıτAˆ= 0, we obtain
i 2 ik k D A = ε M 1 v1. (238 )
Notice that this relation provides the spin-orbit coupling force in the previous form (see Appendix B.1; thus we get di = 𝒟i A A in the present treatment). Using Equation (228View Equation), we finally obtain the spin geodesic equation in the usual form (we omit the quadrupole and ijkl Z 1 term for simplicity),
[( ) ] d ⃗𝒮1 2m2 3 3 ---- = ε -2- 2⃗v2 − -⃗v1 × ⃗n12 × 𝒮⃗1 + 𝒪 (ε ), (239 ) dτ r12 2
where ⃗𝒮1 is the spatial part of the intrinsic spin four-vector ˆˆ 𝒮1ˆi = εijkℳ j1k∕2. Equation (239View Equation) is the geodesic precession equation, or called the de Sitter-Fokker precession (see e.g. Section 40.7 in [122] and [36145]).
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