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U.P.B. Sci. Bull., Series A, Vol. 74, Iss. 2, 2012 ISSN 1223-7027

CLASSICAL MOTION OF A TEST PARTICLE IN THE BERTOTTI-ROBINSON SPACETIME

Gholam Reza Soleimani1, Morteza Yavari2

In this paper, the motion of a test particle in the Bertotti-Robinson space- time by using the Hamilton-Jacobi method is studied. Then, in threading formal- ism, the gravitoelectromagnetism1 acting on this particle in this spacetime is calculated.

Keywords: Bertotti-Robinson spacetime, force, test par- ticle trajectory.

1. Introduction 3 A stationary spacetime (M, gαβ) is a 4-dimensional Lorentzian manifold with a global timelike Killing vector field η. We now assume that there exists a global → R ∂ time function t :M such that η = ∂t . Thus, the quotient space of M by the integral curves of η is a 3-dimensional orbit manifold Σ with projected metric tensor γij to which we refer as space manifold. Hence, this decomposition attempts to decompose spacetime quantities into pieces orthogonal to the given congruence of curves and pieces tangent to the congruence, [3,4]. The threading decomposition leads to the following line element, [4,5]: 2 α β − i 2 − i j ds = gαβdx dx = h(dt gidx ) γijdx dx , (1) where the components of metric are − − g00 = h, g0i = hgi, gij = γij + hgigj, (2) and their inverse are 1 g00 = −g2 + , g0i = −gi, gij = −γij, (3) h 2 i ij in which g = g gi = γ gigj. We now consider a moving test particle of m in a spacetime with the time dependent metric tensor (1). The gravitoelectromagnetism force acting on this particle, as measured by the threading observers, is described

1 Corresponding author, Islamic Azad University, Kashan Branch, Kashan, Iran

2Islamic Azad University, Kashan Branch, Kashan, Iran

3The Greek indices run from 0 to 3 while the Latin indices take the values 1 to 3. 153 154 Gholam Reza Soleimani, Morteza Yavari by the following equation4,5, [6]: ∗d∗p m ∗F = − √ {∗E + ∗v × ∗B + f}, (4) dt 1 − ∗v2 ∗ i i ∗ i m v ∗ 2 ∗ i ∗ j ∗ i v here p = √ such that v = γij v v in which v = √ − ∗ 2 − k 1 v h (1 gkv ) dxi and vi = . Also, the starry total derivative with respect to time is defined as ∗ ∗ dt ∗ d ∂ ∗ i ∗ ∂ 1 ∂ ∗ ∂ = + v ∂i where = √ and ∗i = ∂i = ∂i + g . In equation (4), dt ∂t ∂t h ∂t i ∂t the last term is defined as i − ∗ i ∗ j i ∗ k f = ( λjk v + 2Dk) v , (5)

∗ i 1 il where 3-dimensional starry Christoffel symbols are defined as λ = γ (γ ∗ + jk 2 jl k γkl∗j −γjk∗l) and deformation rates of the reference frame with respect to the observer are represented by the following tensors 1 ∗∂γ 1 ∗∂γij D = ij , Dij = − . (6) ij 2 ∂t 2 ∂t Finally, time dependent gravitoelectromagnetism√ fields are defined in terms of gravo- Φ = ln h and gravomagnetic vector potential g = (g1, g2, g3) as follows6

∗ ∗ ∂g ∗ ∂gi E = − ∇Φ − ; E = −Φ∗ − , (7) ∂t i i ∂t ∗ ∗ i ijk B ∗ B ε √ = ∇ × g ; √ = √ g ∗ . (8) h h 2 γ [k j] For more details about applications of gravitoelectromagnetism fields, see references [7,8].

2. Motion of a test particle in the Bertotti-Robinson spacetime 2.1. Calculation of trajectory At first, we assume that the metric of spacetime is given by the following line element ds2 = e2ν(r)dt2 − e2λ(r)dr2 − dΩ2, (9)

εijk 4The vector C = A × B has components as Ci = √ A B in which γ = det(γ ) and 3- γ j k ij 123 dimensional Levi-Civita tensor εijk is skew-symmetric in any exchange of indices while ε =

ε123 = 1, [5]. 5We use the gravitational units with c=1. ijk 6 ∗ i ε Here, curl of an arbitrary vector in a 3-space with metric γ is defined by ( ∇×A) = √ A ∗ ij 2 γ [k j] while the symbol [ ] represents the anticommutation over indices. Classical motion of a test particle in the Bertotti-Robinson spacetime 155 which is usually assumed to cover all static spherical spacetimes. As is well known, the only static conformally flat spacetime of the form (9) is the Bertotti-Robinson solution which may be written in the following form, [9]: 1 ds2 = (dt2 − dr2 − r2dΩ2). (10) r2 Below, we will calculate the trajectory of a test particle in the Bertotti-Robinson spacetime by using the Hamilton-Jacobi equation, [10-12]. Therefore, this equation is of the form ( ) ( ) ( ) ( ) ∂S 2 ∂S 2 ∂S 2 1 ∂S 2 r − r − − − m2 = 0, (11) ∂t ∂r ∂θ sin θ ∂ϕ where m is the mass of particle. For solving this partial differential equation, we use the method of separation of variables for the Hamilton-Jacobi function as follows S(t, r, θ, ϕ) = −Et + A(r) + B(θ) + Lϕ, (12) where E and L are arbitrary constants and can be identified respectively as energy and angular of test particle along ϕ-direction. With substituting the last relation in the Hamilton-Jacobi equation, the integral expressions for the unknown functions A and B are given by ∫ √ r2 − n2 A = ϵE dr, (13) r ∫ √ B = ϵ c2 − L2 csc2 θ dθ, (14) √ m2 + c2 where n = ϵ while c is the constant of separation and ϵ = ±1 stands for the E sign changing whenever r(or θ) passes through a zero of the integrand, [13]. Now the trajectory of the test particle can be obtained by using the Hamilton-Jacobi method as follows, [10-12]: ∂S ∂S ∂S = constant, = constant, = constant. (15) ∂E ∂L ∂c Consequently, the set of equations (15) change to the following relations (respec- tively) √ 2 2 ∫r = t + n , (16) dθ ϕ = ϵL √ , (17) 2 2 − 2 2 ∫ sin θ∫ c L csc θ dr dθ √ = √ , (18) rE r2 − n2 c2 − L2 csc2 θ we have taken the constants in equations (15) to be zero, without any loss of gener- ality. In continuation, after solving the equation (18), we obtain n sin2 θ = a + ϵb sin(ζ arcsin( )), (19) r 156 Gholam Reza Soleimani, Morteza Yavari

c2+L2 c2−L2 2c where a = 2c2 , b = 2c2 and ζ = nE . Also, from equations (17) and (18), we conclude ∫ dr ϕ = ϵL √ . (20) rE sin2 θ r2 − n2 However, calculations show that the above integral can be solved exactly only for the values ζ = 1, 2. Here, we discuss these two cases as follows:

Case (1) : ζ = 1. It can be shown that the exact solution of the equation (20) is of the form ϵnbe−4iϵϕ + 4n2ae−2iϵϕ + 4ϵn3b r = , (21) ae−4iϵϕ + 4ϵnbe−2iϵϕ + 4n2a √ where i = −1. Let us now restrict our analysis to the following cases: subcase (1) : a = 0. In this case, the equation (21) is transformed to 1 r = n2e2iϵϕ + e−2iϵϕ. (22) 4 ± 1 If we choose n = 2 , then we have the following results 1 r = cos(2ϕ), (23) 2 √ θ = arcsin sec(2ϕ) . (24) Therefore, the trajectories that describe by these equations will be bounded, i.e. the particle can be trapped by the extended object with the Bertotti-Robinson geometry. subcase (2) : b = 0. In this case, the equation (21) is transformed to 1 1 = e2iϵϕ + e−2iϵϕ. (25) r 4n2 ± 1 Like in previous case, if we choose n = 2 , then we have 1 = 2 cos(2ϕ). (26) r From this equation, we can see that the trajectory of particle is bounded and motion π occurs on surface θ = with time period T = π. In these two subcases, the energy 2 4m of particle is7 E = √ which depends on the particle mass. 3 subcase (3) : a = b. π In this case, particle is at rest at point (ϵn, , 0) at time t = 0. 2

7In the next section, we will show that the energy of particle is equal to E. Classical motion of a test particle in the Bertotti-Robinson spacetime 157

Case (2) : ζ = 2. As before, it is easy to show that the following identity is valid, [14]:  √  arcsin(2x 1 − x2) |x| ≤ √1 ,  √ 2 2 arcsin x = π − arcsin(2x 1 − x2) √1 < x ≤ 1, (27)  √ 2 −π − arcsin(2x 1 − x2) −1 ≤ x < − √1 , 2 where x is an arbitrary variable. By considering this identity and applying the equation (16), the solution of equation (20) in terms of t will be (at + ϵnb)c tan ϕ = . (28) nL But for value ζ = 2, we have m = 0. Hence, we ignore the study of this case.

2.2. Calculation of the gravitoelectromagnetism force At first, from the equations (16-18), we can deduce  √  r2 − n2 i = 1,  √ ∗ 2 2 2 vi = ϵ c −L csc θ i = 2, (29)  rE ϵL i = 3. rE sin2 θ With applying this equation and after simplifying, we infer m √ = rE. (30) 1 − ∗v2

Before continuing, we know that the energy of particle,√ as measured by threading observers located at the trajectory, is given by E = √m h , which is a conserved 1−∗v2 quantity during the motion of particle, [3]. As a result, from the equation (30), we conclude that E = E. In the next step, all nonzero components of starry Christoffel symbols are calculated as8 1 ∗λ1 = − , 11 r ∗ 2 − λ33 = sin θ cos θ, (31) ∗ 3 λ23 = cot θ. Also, the nonzero components of deformation tensors are √ 2 − 2 −ϵ r n D11 = 3 , (32) r√ ϵ sin 2θ c2 − L2 csc2 θ D = . (33) 33 2rE

8In our notation (r, θ, ϕ) ≡ (1, 2, 3). 158 Gholam Reza Soleimani, Morteza Yavari

At this stage, from the equations (29-33), we can derive the following expressions   3(r2−n2)  r i = 1, 2 f i = L cot θ i = 2, (34)  r2E2 sin2 θ  √ − 4ϵL cot θ c2−L2 csc2 θ i = 3. r2E2 sin2 θ and   4(2r2 − n2)E i = 1, ∗ ∗ i  d p 4L2 cot θ = 2 i = 2, (35) dt  rE sin θ √  2 2 2 − 8ϵL cot θ c −L csc θ i = 3. rE sin2 θ By considering equations (30), (34), (35) and some calculations, we finally obtain ( √ √ √ ) 2 − 2 − 2 ∗ 2 − 2 3 b L r ϵn −2ϵnbL r n F = (4r n )E, 3 , 2 . (36) (ar + ϵnb) 2 E (ar + ϵnb) To continue our analysis, we are going to determine the potential function corre- sponding to the gravitoelectromagnetism force. For doing this, we can prove that in a 3-space with time dependent metric γij the following identity is valid, [7]: √ ∗ ∗ ∗ ∂ [ ∂ , ∂ ] = h g ∗ . (37) i j [j i] ∂t With the help of this identity and equation (8), we obtain the following relation9 ∗∂Ψ ∗∇ × ∗∇Ψ = ∗B, (38) ∂t where Ψ is an arbitrary scalar function. But the gravitomagnetic fields for the metric (10) are zero, so the above relation changes to

∗∇ × ∗∇Ψ = 0. (39)

On the other hand, by taking the curl of the force, we get  √ √ ( √ ) √ √ − 2 2 2 −  4ϵL b r ϵn a r −n − √ n + 3ϵL b r+ϵn (2ar nϵ(3a+b)) i = 1,  ar+ϵnb ar+ϵnb r r2−n2 2(ar+ϵnb)2  √ √ ( √ ) ∗ ∗ 3 2ϵn2E2 ar+ϵnb r2−n2 2ϵnbL a r2−n2 n2 ∇ × i 2 − − √ ( F) = r Lr3 3 ar+ϵnb 2− 2 i = 2,  r(ar+ϵnb) 2 r r n  √ √  2 − − − 3L √b (2ar nϵ(3a+b)) − 4nE r ϵn i = 3, 2E r−ϵn (ar+ϵnb)3 r2 ≠ 0. (40)

Consequently, by comparing the equations (39) and (40), we cannot define the po- tential function (V) corresponding to the gravitoelectromagnetism force with the following familiar form

∗F = −∗∇V. (41)

9Proof of this identity is simple and have been omitted. Classical motion of a test particle in the Bertotti-Robinson spacetime 159

3. Conclusions In this work, we studied the classical motion of a test particle in the Bertotti- Robinson spacetime. We proved that the particle can be trapped by this gravita- tional field. By determining the gravitoelectromagnetism force, it was shown that the existence of the potential function with the classical definition is impossible.

Acknowledgment This research has been supported in part by the Islamic Azad University-Kashan Branch.

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