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Introduction
In this paper, we wish to study the three-dimensional generalisation of the problem studied by Bhatnagar (12,13,14) for the circular case. Since the Hamilton-Jacobi equation for generating a solution takes an unmanageable form for any solution, we have assumed that the third coordinate (3 of the infinitesimal mass is of the 0(μ). It will be interesting to observe that various equations and results worked out by Bhatnagar can be deduced from our results. In Section 2 we have determined the canonical form of the equations of motion, and in Section 3 these equations are regularised by the generalised Levi-Civita's transformation for three dimensions. Eqs (20)–(22) establish the canonical set (l, L, g, G, h, H) and Eq (32) form the basis of the general perturbation theory for the problem under consideration. During the last few years, many mathematician and astronomers have studied different types of periodic orbits in the restricted problem. Some of them are Giacaglia (7), Mayer and Schmidt (17), Markellos (19), Hadjidemetriou (10,11), Bhatnagar and Taqvi (15), Gomez and Noguera (8), Kadrnoska and Hadrava (9), Peridios et al. (21), Ahmad (1), Elipe and Lara (4), Mathlouthi (23), Scuflaire (22), Caranicolas (20), Poddar et al. (5, 6), Abouelmagd and Guirao (2) and Abouelmagd et al. (3). In this work, we have presented an analytical study of the existence of periodic orbits for μ = 0 in the restricted problem of three bodies in a three-dimensional coordinate system when the smaller primary is a triaxial rigid body.
Equations of Motion
The equations of motion in the canonical form of an infinitesimal mass under the gravitational field of two finite and unequal masses and moving in circles are given by
{\dot X_i}\; = \;{{\partial H} \over {\partial pi}};{\dot p_i}\; = \; - {{\partial H} \over {\partial xi}}(i\; = \;1,\;2,\;3)
where the Hamiltonian function H and consequently the energy integral is given by
H\; = \;{1 \over 2}({p_1}^2\; + \;{p_2}^2\; + \;{p_3}^2)\; + \;n\left( {{p_1}{x_2}{\;_ - }\;{p_2}{x_1}} \right)\; - \;{{\left( {1 - \mu \;} \right)} \over {{r_1}}}\; - \;{\mu \over {{r_2}}}\; - \;{\mu \over {2r_2^3}}\; + \;{{3\mu } \over {2r_2^5}}x_2^2\; = \;C
and C is a function of μ = C(μ) = C0 + μ(C1).
\matrix{ {r_1^2\; = \;{{({x_1}\; - \;\mu )}^2}\; + x_2^2\; + \;x_3^2} \cr {r_2^2\; = \;{{\left( {{x_1} - \mu + 1} \right)}^2}\; + \;x_2^2 + x_3^2} \cr {{p_1}\; = \;{x_1} - {x_2}\;} \cr {{p_2} = {{\dot x}_2} + {x_1}} \cr {{p_3} = \;{{\dot x}_3}} \cr }
Mean motion
n = 1 + {3 \over 4}\left( {2{\sigma _1} - {\sigma _2}} \right)
where
{\sigma _1} = {{{a^2} - {c^2}} \over {5{R^2}}}
,
{\sigma _2} = {{{b^2} - {c^2}} \over {5{R^2}}}
, a, b, c = semi-axes of the triaxial rigid body, R = the dimensional distance between the primaries and (x1, x2, x3) are equal to the synodic rectangular dimensionless coordinates of the infinitesimal mass in a uniformly rotating system.
Regularisation of the Solution
We regularise the solution by Levi-Civita's (18) transformation generated by
S = (\mu + \xi _1^2 - \xi _2^2){p_1} + 2{\xi _1}{\xi _2}{p_2} + {\xi _3}{p_3}
Such that
{x_i} = {{\partial s} \over {\partial {p_i}}};{\pi _i} = {{\partial s} \over {{\partial _i}}}(i\; = \;1,\;2,\;3)
where πi is the momenta associated with the new coordinate ξi.
K can be put in the form Ko + μK1, where
{K_o} = {{{\pi ^2}{r_1}} \over {8{\xi ^2}}} + {1 \over 2}\pi _3^2{r_1} + {{{r_1}n} \over 2}({\xi _2}{\pi _1} - {\pi _2}{\xi _1} - 2c_o^\prime) - 1 = - < o\left( {{\rm{say}}} \right)
where
c_0^\prime = {{{c_0}} \over n}
and
{K_1} = {{n{r_1}} \over {2{\xi ^2}}}({\xi _1}{\pi _2} + {\xi _2}{\pi _1}) - {{{r_1}} \over {{r_2}}} - {{{r_1}} \over {2r_2^3}}(2{\sigma _1} - {\sigma _2}) + {{6{r_1}\mu } \over {r_2^5}}({\sigma _1} - {\sigma _2})\xi _1^2\xi _2^2 - {{(c - {c_o})} \over \mu }{r_1} + 1
The form given to k0 ensures that the orbits which are analytically continued from the two-body orbits will belong to the K = 0 manifold. These are the solution to the regularised equation of the restricted problem. Here we have assumed that k0 is negative (5). Thus, the corresponding two-body problem will admit bounded orbits as a solution in rotating coordinates. We can easily show that ||<1.
Generating Solution
To write the Hamilton-Jacobi equation corresponding to the Hamilton k0, we take
{\pi _i} = {{\partial w} \over {{\partial _i}}}(i = 1,2,3)
For generating a solution, we shall choose k0 for our Hamiltonian function. Since τ is not involved in k explicitly, the Hamilton-Jacobi equation corresponding to k0 may be written as
{1 \over 8}\left[ {{{\left( {{{\partial w} \over {\partial {\xi _1}}}} \right)}^2} + {{\left( {{{\partial w} \over {\partial {\xi _2}}}} \right)}^2}} \right]{{{r_1}} \over {{\xi ^2}}} + {1 \over 2}{\left( {{{\partial w} \over {\partial {\xi _3}}}} \right)^2}{r_1} + {{n{r_1}} \over 2}\left\{ {{\xi _2}{{\partial w} \over {\partial {\xi _1}}} - {\xi _1}{{{{\partial w} \over {\partial \xi }}}_2} - 2c_o^\prime} \right\} = \alpha .
where α = 1 − ɛ.
We take ξ3 of the order of μ, then we have
{r_1} = {\xi ^2}\; + 0(\mu )
Putting
{\xi _1} = \;\xi \;{\rm{cos}}\phi ,\;\;\;\;\;{\xi _{2\;\;\;\;}} = {\rm{sin}}\phi Equation (9) may be written as
{1 \over 8}\left[ {{{\left( {{{\partial w} \over {\partial \xi }}} \right)}^2} + {1 \over {{\xi ^2}}}{{\left( {{{\partial w} \over {\partial \phi }}} \right)}^2}} \right] + {1 \over 2}{\xi ^2}{\left( {{{\partial w} \over {\partial {\xi _3}}}} \right)^2} + {1 \over 2}n{\xi ^2}\left[ { - {{\partial w} \over {\partial \phi }} - 2c_0^\prime} \right] = \alpha
Whose solution of Eq. (10) may be written as
W = u\left( \xi \right) + G\phi + \bar H{\xi _3}
where G is an arbitrary parameter and taking ξ2 = z we have
{\left( {{{\partial u} \over {\partial z}}} \right)^2} = {{{{\bar H}^2} - 2n\left( {G + c_0^\prime} \right)} \over {{z^2}}}f\left( z \right)
where
f(z) = {{{G^2}} \over {2n\;\left( {G + c_0^\prime} \right) - {{\bar H}^2}}} - {{2\alpha z} \over {2n\left( {G + c_0^\prime} \right) - {{\bar H}^2}}} - {z^2}
We suppose that
G + c_0^\prime < 0
then the equation f (z) = 0 has two positive roots z1 and z2 and is positive between them. Also
\matrix{ {{z_1} + {z_2} = - {{2\alpha } \over {2n\left( {G + c_0^\prime} \right) - {{\bar H}^2}}} > 0} \cr {{z_1}{z_2} = - {{{G^2}} \over {2n\;\left( {G + c_0^\prime} \right) - {{\bar H}^2}}} > 0} \cr }
The solution of Eq. (12) is
u(Z,G,\alpha ){\left[ {{{\bar H}^2} - 2n\left( {G + c_0^,} \right)} \right]^{{\kern 1pt} 1{\kern 1pt} /{\kern 1pt} 2{\kern 1pt} }}\mathop {\int_{{Z_1}}^{{Z_2}} }{{\sqrt {f\left( z \right)} } \over Z}dz
Let us introduce the parameter a, e, l using the relation
\matrix{ {{Z_1} = a\left( {1 - e} \right),{Z_2} = a\left( {1 + e} \right)} \cr {Z = {Z_1}\mathop {\cos }\nolimits^2 {l \over 2} + {Z_1}\mathop {\sin }\nolimits^2 {l \over 2} = a(1 - e\cos l)} \cr }
where 0≤e≤1. It may be noted that Z = Z1 when l = 0.
These equations form the basis of the general perturbation theory for the problem in question.
The solution described by Eqs (25) or (26) is periodic if l and g have commensurable frequencies, i.e. if
{{{n_l}} \over {{n_g}}} = {{2n(G + C_o^/)} \over L} = {p \over q}
where p and q are integers.
The period of ξiπi is
{{4\pi } \over {{n_l}}}
and
{{4\pi } \over {{n_g}}}
, and therefore, in the case of commensurability the period of solution is
{{4\pi p} \over {{n_l}}}
or
{{4\pi q} \over {{n_g}}}
Conclusion
We have shown that the equations of motion for the problem are regularised by the generalised Levi-Civita's transformation for three dimensions in the neighbourhood of one of the finite masses and the existence of periodic orbits for μ = 0 in the three-dimensional coordinate systems.
Equations (20)–(22) establish the canonical set (l, L, g, G, h, H) and Eq. (32) form the basis of the general perturbation theory for the problem in question. The solution described by Eq. (25) or (26) is periodic if l and g have commensurable frequencies, that is, if
{{{n_l}} \over {{n_g}}} = {{2n(G + C_o^/)} \over L} = {p \over q}({\rm{say}})
where p and q are integers.
The period of ξiπi is
{{4\pi } \over {{n_l}}}
and
{{4\pi } \over {{n_g}}}
, so that in case of commensurability the period of solution is
{{4\pi p} \over {{n_l}}}
or
{{4\pi q} \over {{n_g}}}
.