Three-Dimensional Periodic Orbits Around the Collinear Liberation Points in the Restricted Problem When Both the Primaries Are Axis Symmetric Bodies

Authors

  • A. Anurag Jain Department of Applied Science, Ganga Institute of Technology and Management, Kablana, Haryana, India
  • Ekta Katyal Department of Applied Science, Ganga Institute of Technology and Management, Kablana, Haryana, India

Abstract

Three-dimensional periodic orbits around the collinear liberation points in the restricted three body problem has been studied when both the primaries (earth–moon) are axis symmetric bodies with one of their axes as axis of symmetry and equatorial planes coinciding with the plane of motion by taking different values of semi-axes of the axis symmetric bodies(earth-moon). With the help of predictor corrector method, we have computed the initial conditions by taking different values of the semi-axes of the axis symmetric bodies. With these initial conditions, we have drawn three-dimensional periodic orbits in the different cases. Keywords: axis symmetric body, collinear points, periodic orbits, restricted three body

References

Anurag TP. Singh and Sanjay Jain Accepted in GPM Journal of Technology.

Szebehely V. Theory of Orbits, Academic, New York. 1967 [3] Goudas CL. Icarus, 1963; 2: 1–18p. [4] Papadakis KE. Astrophysics and Space Science. 1992; 191: 223–229p. [5] Markellos VV. Celest. Mech and Dyn. Astron. 1993; 9: 365–350p. [6] Olle Merce, Pacha R. Joan. Astron. Astrophy. 1999; 351: 1149–1164p. [7] Perdios EA. Astrophysics and Space Science. 2001; 278: 405–407p [8] Perdios EA, Kanavos SS, Markellos VV. Astrophysic and Space Science. 2004; 262: 75–87p. [9] Kalvouridis T, Mavraganis A, Pangalos C. Astrophysics and Space Science. 2004; 255–259p.

Downloads

Published

2021-01-09

Issue

Vol. 3 No. 2 (2017)

Section

Articles