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Reduction the secular solution to periodic solution in the generalized restricted three-body problem

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Abstract

The aim of the present work is to find the secular solution around the triangular equilibrium points and reduce it to the periodic solution in the frame work of the generalized restricted thee-body problem. This model is generalized in sense that both the primaries are oblate and radiating as well as the gravitational potential from a belt. We show that the linearized equation of motion of the infinitesimal body around the triangular equilibrium points has a secular solution when the value of mass ratio equals the critical mass value. Moreover, we reduce this solution to periodic solution, as well as some numerical and graphical investigations for the effects of the perturbed forces are introduced. This model can be used to examine the existence of a dust particle near the triangular points of an oblate and radiating binary stars system surrounded by a belt.

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References

  • Abouelmagd, E.I.: Existence and stability of triangular points in the restricted three-body problem with numerical applications. Astrophys. Space Sci. 342, 45–53 (2012)

    Article  ADS  Google Scholar 

  • Abouelmagd, E.I.: The effect of photogravitational force and oblateness in the perturbed restricted three-body problem. Astrophys. Space Sci. 346, 51–69 (2013a)

    Article  ADS  MATH  Google Scholar 

  • Abouelmagd, E.I.: Stability of the triangular points under combined effects of radiation and oblateness in the restricted three-body problem. Earth Moon Planets 110, 143–155 (2013b)

    Article  ADS  Google Scholar 

  • Abouelmagd, E.I., El-Shaboury, S.M.: Periodic orbits under combined effects of oblateness and radiation in the restricted problem of three bodies. Astrophys. Space Sci. 341, 331–341 (2012)

    Article  ADS  Google Scholar 

  • Abouelmagd, E.I., Sharaf, M.A.: The motion around the libration points in the restricted three-body problem with the effect of radiation and oblateness. Astrophys. Space Sci. 344, 321–332 (2013)

    Article  ADS  MATH  Google Scholar 

  • Abouelmagd, E.I., Asiri, H.M., Sharaf, M.A.: The effect of oblateness in the perturbed restricted three-body problem. Meccanica 48, 2479–2490 (2013)

    Article  MathSciNet  Google Scholar 

  • Beevi, A.S., Sharma, R.K.: Oblateness effect of Saturn on periodic orbits in the Saturn-Titan restricted three-body problem. Astrophys. Space Sci. 340, 245–261 (2012)

    Article  ADS  Google Scholar 

  • Elipe, A., Lara, M.: Periodic orbits in the restricted three body problem with radiation pressure. Celest. Mech. Dyn. Astron. 68, 1–11 (1997)

    Article  ADS  MATH  MathSciNet  Google Scholar 

  • Hou, X.Y., Liu, L.: On quasi-periodic motions around the collinear libration points in the real Earth–Moon system. Celest. Mech. Dyn. Astron. 110, 71–98 (2011)

    Article  ADS  MATH  MathSciNet  Google Scholar 

  • Ishwar, B., Elipe, A.: Secular solutions at triangular equilibrium point in the generalized photogravitational restricted three body problem. Astrophys. Space Sci. 277, 437–446 (2001)

    Article  ADS  MATH  Google Scholar 

  • Mittal, A., Ahmad, I., Bhatnagar, K.B.: Periodic orbits generated by Lagrangian solution of the restricted three body problem when one of the primaries is an oblate body. Astrophys. Space Sci. 319, 63–73 (2009)

    Article  ADS  MATH  Google Scholar 

  • Miyamoto, M., Nagai, R.: Three-dimensional models for the distribution of mass in galaxies. Publ. Astron. Soc. Jpn. 27, 533–543 (1975)

    ADS  Google Scholar 

  • Papadakis, K.E.: Families of asymmetric periodic orbits in the restrict three-body problem. Earth Moon Planets 103, 25–42 (2008)

    Article  ADS  MATH  Google Scholar 

  • Perdios, E.A.: Parameter values for stable low-inclination periodic motion in the restricted three-body problem with oblateness. Astrophys. Space Sci. 278, 405–407 (2001)

    Article  ADS  Google Scholar 

  • Sharma, R.K., The linear stability of libration points of the photogravitational restricted three-body problem when the smaller primary is an oblate spheroid. Astrophys. Space Sci. 135, 271–281 (1987)

    Article  ADS  MATH  Google Scholar 

  • Shibayama, M., Yagasaki, K.: Families of symmetric relative periodic orbits originating from the circular Euler solution in the isosceles three-body Problem. Celest. Mech. Dyn. Astron. 110, 53–70 (2011)

    Article  ADS  MATH  MathSciNet  Google Scholar 

  • Singh, J., Begha, J.M.: Periodic orbits in the generalized perturbed restricted three-body problem. Astrophys. Space Sci. 332, 319–324 (2011)

    Article  ADS  MATH  Google Scholar 

  • Singh, J., Taura, J.J.: Motion in the generalized restricted three-body problem. Astrophys. Space Sci. 343, 95–106 (2013)

    Article  ADS  Google Scholar 

  • Tsirrogiannis, G.A., Douskos, C.N.E., Perdios, E.A.: Computation of the Lyapunov orbits in the photogravitational RTBP with oblateness. Astrophys. Space Sci. 305, 389–398 (2006)

    Article  ADS  Google Scholar 

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Acknowledgements

The authors (especially the first author) wish to express their gratitude to referees for their useful suggestions and criticism which improved the presentation of the paper.

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Correspondence to Elbaz I. Abouelmagd.

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Abouelmagd, E.I., Awad, M.E., Elzayat, E.M.A. et al. Reduction the secular solution to periodic solution in the generalized restricted three-body problem. Astrophys Space Sci 350, 495–505 (2014). https://doi.org/10.1007/s10509-013-1756-z

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  • DOI: https://doi.org/10.1007/s10509-013-1756-z

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