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Robe’s restricted problem of 2+2 bodies with one of the primaries an oblate body

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Abstract

In this problem, one of the primaries of mass \(m^{*}_{1}\) is a rigid spherical shell filled with a homogeneous incompressible fluid of density ρ1. The smaller primary of mass m2 is an oblate body outside the shell. The third and the fourth bodies (of mass m3 and m4 respectively) are small solid spheres of density ρ3 and ρ4 respectively inside the shell, with the assumption that the mass and the radius of the third and the fourth body are infinitesimal. We assume that m2 is describing a circle around \(m^{*}_{1}\). The masses m3 and m4 mutually attract each other, do not influence the motions of \(m^{*}_{1}\) and m2 but are influenced by them. We also assume that masses m3 and m4 are moving in the plane of motion of mass m2. In the paper, equilibrium solutions of m3 and m4 and their linear stability are analyzed. There are two collinear equilibrium solutions for the system. The non collinear equilibrium solutions exist only when ρ3=ρ4. There exist an infinite number of non collinear equilibrium solutions of the system, provided they lie inside the spherical shell. In a system where the primaries are considered as earth-moon and m3,m4 as submarines, the collinear equilibrium solutions thus obtained are unstable for the mass parameters μ,μ3,μ4 and oblateness factor A. In this particular case there are no non-collinear equilibrium solutions of the system.

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References

  • Rajiv, A., Taqvi, Z.A., Ahmad, I.: Non-linear stability of L4 in the restricted three body problem for radiated axes symmetric primaries with resonances. Bull. Astron. Soc. India 34, 327–356 (2006)

    ADS  Google Scholar 

  • Brouwer, D., Clemence, G.M.: Methods of Celestial Mechanics. Academic Press, New York and London (1961)

    MATH  Google Scholar 

  • Hallan, P.P., Rana, N.: The existence and stability of equilibrium points in the Robe’s restricted problem three-body problem. Celest. Mech. Dyn. Astron. 79, 145–155 (2001a)

    Article  ADS  MathSciNet  Google Scholar 

  • Hallan, P.P., Rana, N.: Effect of perturbation in coriolis and centrifugal forces on the location and stability of the equilibrium point in the Robe’s circular restricted three body problem. Planet. Space Sci. 49, 957–960 (2001b)

    Article  ADS  Google Scholar 

  • Hallan, P.P., Rana, N.: Effect of perturbation in the coriolis and centrifugal forces on the location and stability of the equilibrium points in the Robe’s circular problem with density parameter having arbitrary value. Indian J. Pure Appl. Math. 34(7), 1045–1059 (2003)

    MathSciNet  MATH  Google Scholar 

  • Hallan, P.P., Rana, N.: Effect of oblateness on the location and stability of equilibrium points in Robe’s circular problem. Indian J. Pure Appl. Math. 35(3), 40–43 (2004)

    MathSciNet  MATH  Google Scholar 

  • Hallan, P.P., Mangang, K.B.: Existence and linear stability of equilibrium points in the Robe’s restricted three body problem when the first primary is an oblate spheroid. Planet. Space Sci. 55, 512–516 (2007)

    Article  ADS  Google Scholar 

  • Bhavneet, K., Rajiv, A.: Robe’s problem: its extension to 2+2 bodies. Astrophys. Space Sci. 339, 283–294 (2012)

    Article  Google Scholar 

  • Robe, H.A.G.: A new kind of three body problem. Celest. Mech. Dyn. Astron. 16, 243–351 (1977)

    Google Scholar 

  • Sharma, R.K., Subba Rao, P.V.: Collinear equilibria and their characteristic exponents in the restricted three body problem when the primaries are oblate spheroids. Celest. Mech. 12, 189–201 (1975)

    Article  ADS  Google Scholar 

  • Sharma, R.K., Subba Rao, P.V.: Stationary solutions and their characteristic exponents in the restricted three body problem when the more massive primary is an oblate spheroid. Celest. Mech. 13, 137–149 (1976)

    Article  ADS  MathSciNet  Google Scholar 

  • Sharma, R.K., Subba Rao, P.V.: Effect of oblateness on triangular solutions at critical mass. Astrophys. Space Sci. 60, 247–250 (1979)

    Article  ADS  Google Scholar 

  • Szebehely, V.S.: Theory of Orbits. Academic Press, New York (1967)

    MATH  Google Scholar 

  • Whipple, A.L.: Equilibrium solutions of the restricted problem of 2+2 bodies. Celest. Mech. 33, 271–294 (1984)

    Article  ADS  MathSciNet  Google Scholar 

Download references

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Correspondence to Bhavneet Kaur.

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Aggarwal, R., Kaur, B. Robe’s restricted problem of 2+2 bodies with one of the primaries an oblate body. Astrophys Space Sci 352, 467–479 (2014). https://doi.org/10.1007/s10509-014-1963-2

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