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11institutetext: Center for Cosmology and Astrophysics, Alikhanian National Laboratory and Yerevan State University, Yerevan, Armenia 22institutetext: SIA, Sapienza Universita di Roma, Rome, Italy

Lense-Thirring precession and gravito-gyromagnetic ratio

A. Stepanian 11    Sh. Khlghatyan 11    V.G. Gurzadyan 1122
(Received: date / Revised version: date)
Abstract

The geodesics of bound spherical orbits i.e. of orbits performing Lense-Thirring precession, are obtained in the case of the Λ\Lambda-term within gravito-electromagnetic formalism. It is shown that the presence of the Λ\Lambda-term in the equations of gravity leads to both relativistic and non-relativistic corrections in the equations of motion. The contribution of the Λ\Lambda-term in the Lense-Thirring precession is interpreted as an additional relativistic correction and the gravito-gyromagnetic ratio is defined.

pacs:
98.80.-kCosmology

1 Introduction

The Lense-Thirring (LT) effect is one of essential predictions of General Relativity (GR) C1 ; C2 which enabled accurate measurements in conditions of the Earth gravity by means of laser ranging satellites C3 ; C4 ; C5 . The potential observability of L-T precession is among the features attributed to the accretion disks of galactic nuclei and binary stars, e.g. Dyda .

LT precession has been efficiently treated within the gravito-electromagnetism (GEM) (or gravitomagnetism) formalism, see GEM ; GEM1 ; GEM2 ; M1 ; M2 and refs therein. This approach will be used below, as enabling to reveal explicitly the contributions of the relevant terms in the equations of motion.

We will be interested in the role of the Λ\Lambda-term in the LT effect. This issue has to be considered within the importance of consideration of modified gravity models to describe the observational data on the dark energy and dark matter. Namely, we will use the following metric for the spherically symmetric solution of field equations

g00=12Gmc2rΛr23;grr=(12Gmc2rΛr23)1,g_{00}=1-\frac{2Gm}{c^{2}r}-\frac{\Lambda r^{2}}{3}\,;\qquad g_{rr}=\left(1-\frac{2Gm}{c^{2}r}-\frac{\Lambda r^{2}}{3}\right)^{-1}\,, (1)

known as Schwarzschild-de Sitter metric Rind . This metric is arising also as weak-field limit of GR in view of the Newton’s theorem on the “sphere-point” equivalency G ; GS1 ; GS2 ; GKS . Then, the cosmological constant, Λ\Lambda can be attributed as a fundamental constant GS3 , which is present in both relativistic and non-relativistic equations of gravity. Within McCrea-Milne cosmology it enables one to consider e.g. the observed galactic flow in the vicinity of the Local Group RG ; GS4 .

The appearance of Λ\Lambda in the above relations can be given a clear group-theoretical background. Namely, for three different vacuum solutions for GR equations the isometry groups are defined depending on the sign of Λ\Lambda, the stabilizer group of the maximally symmetric Lorentzian 4D-geometries is the Lorentz group O(1,3). Then, for all of these Lorentzian geometries the group O(1,3) of orthogonal transformations defines a spherical symmetry in Lorentzian sense at each point; for details see GS1 .

The numerical value of Λ\Lambda is too small i.e. Λ=1.11×1052\Lambda=1.11\times 10^{-52} m2m^{-2}Pl and certainly the possibility to observe/detect the role of the Λ\Lambda-term in Eq.(1) looks non-trivial for now, as previously had appeared so, but now directly observed the black hole’s shadow in the center of M87 galaxy and of the gravitational waves. Particularly, the gravitational lensing can provide one of the possibilities to detect a discrepancy between GR and Λ\Lambda-gravity GSlens . Up to now, different constraints for Λ\Lambda are obtained Con1 ; Con2 ; Con3 ; L ; SK , with no inconsistency with the above mentioned numerical value for the cosmological constant.

In this paper, for the first time we merge the LT effect, GEM and the Λ\Lambda-gravity. We start with the geodesic equations in a time-varying LT system based on M1 ; M2 , and then move to the interpretation of the nature of additional Λ\Lambda-term appeared in the LT precession in the context of GEM.

2 Spherical orbits

In the context of Λ\Lambda-gravity, the metric of time-depending angular momentum of a central mass is given by following relation

ds2=c2(12Φc2)dt24c(𝐀d𝐱)dt+(1+2Φc2)δijdxidxj,ds^{2}=-c^{2}\left(1-2\frac{\Phi}{c^{2}}\right)dt^{2}-\frac{4}{c}(\mathbf{A}\cdot d\mathbf{x})dt+\left(1+2\frac{\Phi}{c^{2}}\right)\delta_{ij}dx^{i}dx^{j}, (2)

where in the same analogy with standard GEM

Φ=GMr+Λc2r26,𝐀=Gc𝐉(t)×𝐱r3,\Phi=\frac{GM}{r}+\frac{\Lambda c^{2}r^{2}}{6},\quad\mathbf{A}=\frac{G}{c}\frac{\mathbf{J}(t)\times\mathbf{x}}{r^{3}},\quad (3)

are the gravitoelectric and gravitomagnetic potentials, respectively. Meantime, r=|𝐱|r=|\mathbf{x}| and 𝐉(t)\mathbf{J}(t) linear time-dependent angular momentum of central mass

𝐉(t)=(J0+J1t)𝐳^.\mathbf{J}(t)=(J_{0}+J_{1}t)\hat{\mathbf{z}}.

Considering the geodesics duμdτ+Γμuρρσuσ=0\frac{du^{\mu}}{d\tau}+\Gamma^{\mu}{}_{\rho\sigma}u^{\rho}u^{\sigma}=0, we will have

c2Γ00μ\displaystyle c^{2}\Gamma^{0}{}_{0\mu} =Φ,μ,\displaystyle=-\Phi_{,\mu},
c2Γ0ij\displaystyle c^{2}\Gamma^{0}{}_{ij} =2A(i,j)+δijΦ,0,\displaystyle=2A_{(i,j)}+\delta_{ij}\Phi_{,0},
c2Γi00\displaystyle c^{2}\Gamma^{i}{}_{00} =Φ,i2Ai,0,\displaystyle=-\Phi_{,i}-2A_{i,0},
c2Γi0j\displaystyle c^{2}\Gamma^{i}{}_{0j} =δijΦ,0+2A[i,j],\displaystyle=\delta_{ij}\Phi_{,0}+2A_{[i,j]},
c2Γijk\displaystyle c^{2}\Gamma^{i}{}_{jk} =δijΦ,k+δikΦ,jδjkΦ,i.\displaystyle=\delta_{ij}\Phi_{,k}+\delta_{ik}\Phi_{,j}-\delta_{jk}\Phi_{,i}.

From GEM point of view, the equation of motion can be regarded as the equation of motion for a charge due to the “Lorentz force”. It will take the following form

d𝐯dt+GM𝐱r3Λc2𝐱3=(GMc2r3Λ3)[4(𝐱𝐯)𝐯v2𝐱]+2Gc2𝐉˙×𝐱r32c𝐯×𝐁6GJ(t)c4r5[𝐉^(𝐱×𝐯)](𝐱𝐯)𝐯,\frac{d{\mathbf{v}}}{dt}+\frac{GM{\mathbf{x}}}{r^{3}}-\frac{\Lambda c^{2}{\mathbf{x}}}{3}=\left(\frac{GM}{c^{2}r^{3}}-\frac{\Lambda}{3}\right)[4({\mathbf{x}}\cdot{\mathbf{v}}){\mathbf{v}}-v^{2}{\mathbf{x}}]+\frac{2G}{c^{2}}\frac{\dot{\mathbf{J}}\times{\mathbf{x}}}{r^{3}}-\frac{2}{c}{\mathbf{v}}\times{\mathbf{B}}-\frac{6GJ(t)}{c^{4}r^{5}}[\hat{\mathbf{J}}\cdot({\mathbf{x}}\times{\mathbf{v}})]({\mathbf{x}}\cdot{\mathbf{v}}){\mathbf{v}}, (4)

where

𝐁=×𝐀=G(J0+J1t)cr5(3z𝐱r2𝐳^).\mathbf{B}=\mathbf{\nabla}\times\mathbf{A}=\frac{G(J_{0}+J_{1}t)}{cr^{5}}(3z\mathbf{x}-r^{2}\hat{\mathbf{z}}).

The equation of motion includes the linear post-Newtonian contributions. However, in order to fully understand the motion of the test particle we have to include the following non-linear gravitoelectric term 4G2M2c2r4𝐱\frac{4G^{2}M^{2}}{c^{2}r^{4}}\mathbf{x} too.

In spherical coordinates (r,θ,ϕ)(r,\theta,\phi) the Eq.(4) will be written as

r¨rθ˙2rϕ˙2sin2θ+GMr2Λc2r3=GMc2r2(4r˙2v2+4GMr)Λr3(4r˙2v2)+2GJ(t)c2r2ϕ˙sin2θ,\displaystyle\ddot{r}-r\dot{\theta}^{2}-r\dot{\phi}^{2}\sin^{2}\theta+\frac{GM}{r^{2}}-\frac{\Lambda c^{2}r}{3}=\frac{GM}{c^{2}r^{2}}\left(4\dot{r}^{2}-v^{2}+\frac{4GM}{r}\right)-\frac{\Lambda r}{3}(4\dot{r}^{2}-v^{2})+\frac{2GJ(t)}{c^{2}r^{2}}\dot{\phi}\sin^{2}\theta, (5)
rθ¨+2r˙θ˙rϕ˙2sinθcosθ=(4GMc2r4Λr23)r˙θ˙4GJ(t)c2r2ϕ˙sinθcosθ,\displaystyle r\ddot{\theta}+2\dot{r}\dot{\theta}-r\dot{\phi}^{2}\sin\theta\cos\theta=\left(\frac{4GM}{c^{2}r}-\frac{4\Lambda r^{2}}{3}\right)\dot{r}\dot{\theta}-\frac{4GJ(t)}{c^{2}r^{2}}\dot{\phi}\sin\theta\cos\theta, (6)
rϕ¨sinθ+2r˙ϕ˙sinθ+2rθ˙ϕ˙cosθ=(4GMc2r4Λr23)r˙ϕ˙sinθ+2GJ˙c2r2sinθ2GJ(t)c2r3(r˙sinθ2rθ˙cosθ).\displaystyle r\ddot{\phi}\sin\theta+2\dot{r}\dot{\phi}\sin\theta+2r\dot{\theta}\dot{\phi}\cos\theta=\left(\frac{4GM}{c^{2}r}-\frac{4\Lambda r^{2}}{3}\right)\dot{r}\dot{\phi}\sin\theta+\frac{2G\dot{J}}{c^{2}r^{2}}\sin\theta-\frac{2GJ(t)}{c^{2}r^{3}}(\dot{r}\sin\theta-2r\dot{\theta}\cos\theta).

The Eq.(2) can be rewritten as

ddt[r2ϕ˙sin2θ2GJ(t)c2rsin2θ]=(4GMrc24Λr43)r˙ϕ˙sin2θ.\frac{d}{dt}\left[r^{2}\dot{\phi}\sin^{2}\theta-\frac{2GJ(t)}{c^{2}r}\sin^{2}\theta\right]=\left(\frac{4GMr}{c^{2}}-\frac{4\Lambda r^{4}}{3}\right)\dot{r}\dot{\phi}\sin^{2}\theta. (8)

Consequently, we get the integral of the motion if the right-hand side of Eq.(8) vanishes. Considering spherical orbits (φ,ϑ,ρ)(\varphi,\vartheta,\rho), i.e. the circular orbits with frame dragging, we obtain

φ˙=Csin2ϑ+2GJ(t)c2ρ3.\dot{\varphi}=\frac{C}{\sin^{2}\vartheta}+\frac{2GJ(t)}{c^{2}\rho^{3}}. (9)

Therefore, the Eqs.(5, 6) will be written as

ϑ˙2+C2sin2ϑ\displaystyle\dot{\vartheta}^{2}+\frac{C^{2}}{\sin^{2}\vartheta} =GMρ3(13GMc2ρΛρ23)6GJ(t)c2ρ3CΛc23(1+GMc2ρΛρ23)\displaystyle=\frac{GM}{\rho^{3}}\left(1-\frac{3GM}{c^{2}\rho}-\frac{\Lambda\rho^{2}}{3}\right)-\frac{6GJ(t)}{c^{2}\rho^{3}}C-\frac{\Lambda c^{2}}{3}\left(1+\frac{GM}{c^{2}\rho}-\frac{\Lambda\rho^{2}}{3}\right) (10)
ϑ¨C2cosϑsin3ϑ\displaystyle\ddot{\vartheta}-\frac{C^{2}\cos\vartheta}{\sin^{3}\vartheta} =0.\displaystyle=0. (11)

These equations will be compatible only if J˙=0\dot{J}=0. Thus by setting J=J0J=J_{0}, we define the positive constant Ω\Omega such that

Ω2=GMρ3(13GMc2ρΛρ23)6GJ0c2ρ3CΛc23(1+GMc2ρΛρ23).\Omega^{2}=\frac{GM}{\rho^{3}}\left(1-\frac{3GM}{c^{2}\rho}-\frac{\Lambda\rho^{2}}{3}\right)-\frac{6GJ_{0}}{c^{2}\rho^{3}}C-\frac{\Lambda c^{2}}{3}\left(1+\frac{GM}{c^{2}\rho}-\frac{\Lambda\rho^{2}}{3}\right). (12)

It should be noticed that due to the incorporation of Λ\Lambda in the equations of gravity, according to Eq.(1), changes/modifies the notion of Ω\Omega which was introduced in M1 . Namely, as stated above we have both relativistic as well as non-relativistic corrections which are appeared due to the presence of Λ\Lambda term. First, according to Eq.(1), the standard Newtonian dynamics is written as

v2=GMrΛc2r23.v^{2}=\frac{GM}{r}-\frac{\Lambda c^{2}r^{2}}{3}. (13)

The second corrections is pure relativistic which can be observed in Eq.(4). Indeed, in contrast to the left-hand side of Eq.(4) the Λ3\frac{\Lambda}{3} term on the right-hand side is a pure relativistic effect and has no classical analogue.

In this sense, although we have newly modified Ω\Omega term, comparing to the results of M1 the nature of the solutions do not change. Thus, for the motion in ϑ\vartheta we get

(dcosϑdt)2=(Ω2C2)Ω2cos2ϑ.\left(\frac{d\cos\vartheta}{dt}\right)^{2}=(\Omega^{2}-C^{2})-\Omega^{2}\cos^{2}\vartheta. (14)

The above equation has solution once Ω2C2\Omega^{2}\geq C^{2}. Thus, we have

cosϑ=αsin(Ωt+β),C2=Ω2(1α2),\cos\vartheta=\alpha\sin(\Omega t+\beta),\quad C^{2}=\Omega^{2}(1-\alpha^{2}), (15)

where β\beta is a constant. Accordingly, in the same analogy with M1 , if we take C=ΩcosiC=\Omega\cos i, the solution of the Eq.(9) may be written as

φ(t)=2GJ0tc2ρ3+tan1[cositan(Ωt+β)]+φ0,\varphi(t)=\frac{2GJ_{0}t}{c^{2}\rho^{3}}+\tan^{-1}[\cos i\tan(\Omega t+\beta)]+\varphi_{0}, (16)

where, φ0\varphi_{0} is an integration constant and ii is the inclination angle.

As a result we can state that the above considered spherical orbits can be characterized as circular orbits in the post-Newtonian gravitational field of Λ\Lambda-gravity, which undergo LT precession due to the presence of a constant angular momentum of the source. Consequently, we can find the modified Keplerian frequency

ωΛ=GMr3Λc23\omega_{\Lambda}=\frac{GM}{r^{3}}-\frac{\Lambda c^{2}}{3} (17)

and the frequency ω\omega as follows

Ω=ω3GJ0c2ρ3C,\Omega=\omega-\frac{3GJ_{0}}{c^{2}\rho^{3}}C, (18)

the form for ω\omega is obtained from the relation E.(12)

ω=GMρ3(13GMc2ρΛρ23)Λc23(1+GMc2ρΛρ23).\omega=\frac{GM}{\rho^{3}}\left(1-\frac{3GM}{c^{2}\rho}-\frac{\Lambda\rho^{2}}{3}\right)-\frac{\Lambda c^{2}}{3}\left(1+\frac{GM}{c^{2}\rho}-\frac{\Lambda\rho^{2}}{3}\right).

Thus, in comparison with the results of M1 , both definitions of constants Ω\Omega and ω\omega are changed accordingly. Namely, for both of them we get relativistic and non-relativistic corrections due to the presence of Λ\Lambda term. However, since these corrections enter into the equations of motion as a combination of constants, we can conclude that apart from the numerical corrections, the nature of the analysis regarding the spherical orbits does not change.

3 Perturbed orbits

Turning to the perturbation analysis, we can state that in case of

J=J0+J1tJ=J_{0}+J_{1}t

the perturbation (f(t),g(t),h(t))(f(t),g(t),h(t)) which is written as

r=ρ(1+f(t)),θ=ϑ+g(t),ϕ=φ+h(t),r=\rho(1+f(t)),\quad\theta=\vartheta+g(t),\quad\phi=\varphi+h(t), (19)

will lead to the instability if the spherical orbits, causing inward (when J1cosi<0J_{1}\cos i<0) and outward (when J1cosi>0J_{1}\cos i>0) spiral orbits.

Considering the physics of orbital mechanics and the possible modifications of pure Keplerian motion, it is essential to mention the relativistic shift of the precession, too. Namely, it is a deviation from the precession predicted by Newtonian gravity which occurs due to GR effects and is equal to

ΔϕGR=6πGMc2a(1e2),\Delta\phi_{GR}=6\pi\frac{GM}{c^{2}a(1-e^{2})}, (20)

where aa and ee are the semi-major axis and the eccentricity of the orbit, respectively. Accordingly, if we consider the Λ\Lambda-term in the equations, besides the ΔϕGR\Delta\phi_{GR} we get an additional shift

ΔϕΛ=πc2Λa3GM1e2.\Delta\phi_{\Lambda}=\frac{\pi c^{2}\Lambda a^{3}}{GM}\sqrt{1-e^{2}}. (21)

It can be shown that, this additional shift is of pure relativistic origin and cannot be reduced to any non-relativistic effect Br ; Mash . Moreover, in the absence of central object of mass MM, the Λ\Lambda-term in Eqs.(1),(2) will have no effect on the orbital precession, and, of course, for real astrophysical systems the ΔϕΛ\Delta\phi_{\Lambda} numerically is essentially smaller than ΔϕGR\Delta\phi_{GR}.

Finally, it is worth mentioning that besides the above derivation, we can have another relation where right-hand side of Eq.(8) vanishes generally,

rcrit3=3GMc2Λ,r^{3}_{crit}=\frac{3GM}{c^{2}\Lambda}, (22)

which is the distance where the gravitational repulsion of Λ\Lambda-term in Eq.(1) completely balances the gravitational attraction of Newtonian term. It should be stressed that although in this case, the test particle located at rcritr_{crit} does not feel any force from the central object it cannot be considered as a free particle. Indeed, this is a unique feature which is taken place in the context of Λ\Lambda-gravity. The reason lies on the fact that while the net force over the test particle with mass mm vanishes, the gravitational potential is non-zero i.e.

Φ=GMrΛc2r26|rcrit=Λc2rcrit22,F=mΦ=GMmr2+Λc2rm3|rcrit=0.\Phi=-\frac{GM}{r}-\frac{\Lambda c^{2}r^{2}}{6}|_{r_{crit}}=-\frac{\Lambda c^{2}r_{crit}^{2}}{2},\quad F=-m\nabla\Phi=-\frac{GMm}{r^{2}}+\frac{\Lambda c^{2}rm}{3}|_{r_{crit}}=0. (23)

4 GEM interpretation

In this section we intend to generalize the standard “GEM” interpretation in such way that it incorporates the Λ\Lambda term. Namely, the GEM is an approaches which tries to find an analogy between the Maxwell field equations and those of GR written at relevant approximation GEM . Thus, in the context of Λ\Lambda-gravity the GEM equations will be written as

𝐄=4πGρΛc2,\nabla\cdot\mathbf{E}=4\pi G\rho-\Lambda c^{2}, (24)
×𝐄=𝐁t,\nabla\times\mathbf{E}=-\frac{\partial\mathbf{B}}{\partial t}, (25)
𝐁=0,\nabla\cdot\mathbf{B}=0, (26)
×𝐁=μ𝐉+𝐄t,\nabla\times\mathbf{B}=\mu\mathbf{J}+\frac{\partial\mathbf{E}}{\partial t}, (27)

where Λ\Lambda-term in the first equation can be regarded as the additional “vacuum density” which is equal to Λc24πG\frac{-\Lambda c^{2}}{4\pi G}. Considering the fact that the vacuum density is just a combination of constants, we can state that it won’t change anything in the continuity equation

dρdt+𝐉=0.\frac{d\rho}{dt}+\nabla\cdot\mathbf{J}=0. (28)

Meantime, in the context of GEM the LT precession is interpreted as the Larmor precession which is written as

Ω=γ𝐁,\Omega=\gamma\mathbf{B}, (29)

where γ\gamma is the gyromagnetic ratio and 𝐁\mathbf{B} is the magnetic field. Accordingly, for LT precession, the gravitomagnetic field will be written as

𝐁=G𝐉c2r3,\quad\mathbf{B}=\frac{G\mathbf{J}}{c^{2}r^{3}}, (30)

By turning to Λ\Lambda-gravity it can be shown that the LT precession is written as

2GJc2r3+ΛJ3M.\frac{2GJ}{c^{2}r^{3}}+\frac{\Lambda J}{3M}. (31)

Considering the fact that, the gravitomagnetic field is produced by gravito-current i.e. the rotation, it is not correct to consider the ΛJ3M\frac{\Lambda J}{3M} as a correction to the magnetic field. Here the key point is that the second term in Eq.(31) can be interpreted as the correction over the gravito-gyromagnetic ratio

γ=2(1+MΛM),\gamma=2\left(1+\frac{M_{\Lambda}}{M}\right), (32)

where MΛM_{\Lambda} is the “effective mass” of the vacuum with a density Λc28πG\frac{\Lambda c^{2}}{8\pi G}. It can be checked that this correction is purely relativistic in its nature. Namely, comparing both Eq.(1) and Eq.(24), it becomes clear that while the presence of Λ\Lambda in the relativistic equations is regarded as the contribution of vacuum with density equal to Λc28πG\frac{\Lambda c^{2}}{8\pi G}, in the non-relativistic limit, where we are dealing with gravitational force, this correction changes to the notion of vacuum with density equal to Λc24πG\frac{-\Lambda c^{2}}{4\pi G}. Speaking in other words, one can conclude that while the Λ\Lambda term can contribute to the gravitational potential as an additional term, for those equations where instead of potential we are dealing with the notion of “gravitational fields” or “gravitational force” the contribution of Λ\Lambda becomes subtractive. Thus, by checking the presence of Λ\Lambda term in Eq.(31) we can state that this correction should be a relativistic correction with no classical analogue. Considering the Eq.(32) and continuing the analogue in electromagnetism in the GEM spirit, we can state that such correction is similar to the electron’s g-factor geg_{e} in the context of relativistic quantum mechanics

ge=2(1+α2π+),α=14πϵe2c1137.g_{e}=2(1+\frac{\alpha}{2\pi}+...),\quad\alpha=\frac{1}{4\pi\epsilon}\frac{e^{2}}{\hbar c}\approx\frac{1}{137}. (33)

However, the main difference between Eq(32) and above relation is that while in Eq.(33) the second term is constant, the MΛM\frac{M_{\Lambda}}{M} is variable. Namely, its value becomes larger as the radius increases. Moreover, it can be shown at some distance its contribution will be equal to the first term i.e.

r3=6GMc2Λ,r^{3}=\frac{6GM}{c^{2}\Lambda}, (34)

which is twice the rcritr_{crit} in Eq.(22). Consequently, we can state that at radii larger than rr in Eq.(34) the dominant term such causes the LT precession is the Λ\Lambda term. However, it should be recalled that even in such cases, the presence of a central rotating body with mass MM and angular momentum JJ is the necessary condition. Indeed, this statement once again shows that the nature of Λ\Lambda-term is purely relativistic and confirms the fact the in contrast to other similar precessions e.g. the geodetic precession, for LT precession the rotation of the central object is essential.

5 Conclusions

In this paper we studied the geodesics of spherical bound orbits, i.e. the circular orbits with frame dragging, in the context of Λ\Lambda-gravity within the gravito-electromagnetic formalism. We have derived the equations in the same analogy with the equations of motion for a charged particle experiencing the Lorenz force. Consequently, we have shown that the Λ\Lambda-term enters both the relativistic as well as non-relativistic corrections to the original equations. Furthermore, by considering the LT precession, we have given a new interpretation of GEM within which the Λ\Lambda is included. Namely, we have shown that, from the GEM point of view, the additional Λ\Lambda term in LT can be regarded as a relativistic correction to the gravito-gyromagnetic ratio.

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