Effects of Radiating Oblate Spheroid and Triaxial Rigid Body in the Restricted Three Body Problem

Authors

  • S. Dewangan  Shri Shankaracharya Engineering College,Bhilai, Durg, Chhattisgarh, India
  • Poonam Duggad  Shri Shankaracharya Group of Institutions,Bhilai, India

Keywords:

Restricted Problem; Libration Points; Rigid Body; Oblate Spheroid; Periodic orbits.

Abstract

This paper deals with finding stationary solutions and periodic orbits of the planar restricted three body problem, when the smaller primary is a triaxial rigid body with one of the axes as the axis of symmetry and the bigger primary an oblate spheroidand the source of radiationwith equatorial plane of the primaries coinciding with the plane of the motion. It is further observed that the collinear points are unstable, while the triangular equilibrium points are stable for the range of mass parameter (the critical mass parameter). It is also observed that the triangular equilibrium points have long or short periodic elliptical orbits in the same range of µ

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International Journal of Scientific Research in Science, Engineering and Technology

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Published

2018-02-28

Issue

Volume 4, Issue 6, January-February-2018

Section

Research Articles

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This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

[1]
S. Dewangan, Poonam Duggad "Effects of Radiating Oblate Spheroid and Triaxial Rigid Body in the Restricted Three Body Problem" International Journal of Scientific Research in Science, Engineering and Technology (IJSRSET), Print ISSN : 2395-1990, Online ISSN : 2394-4099, Volume 4, Issue 6, pp.81-89, January-February-2018.