Article citationsMore>>

Elshaboury, S.M., Abouelmagd, E.I., Kalantonis, V.S. and Perdios, E.A. (2016) The Planar Restricted Three-Body Problem When Both Primaries Are Triaxial Rigid Bodies: Equilibrium Points and Periodic Orbits. Astrophysics and Space Science, 361, 315.
https://doi.org/10.1007/s10509-016-2894-x

has been cited by the following article:

• TITLE: Analysis of Effect of Oblateness of Smaller Primary on the Evolution of Periodic Orbits

  AUTHORS: Niraj Pathak, V. O. Thomas

  KEYWORDS: Restricted Three Body Problem, Low Energy Trajectory Design, Periodic Orbits, Oblateness, Poincare Surface of Section

  JOURNAL NAME: International Journal of Astronomy and Astrophysics, Vol.6 No.4, December 27, 2016

  ABSTRACT: Evolution of periodic orbits in Sun-Mars and Sun-Earth systems are analyzed using Poincare surface of section technique and the effects of oblateness of smaller primary on these orbits are considered. It is observed that oblateness of smaller primary has substantial effect on period, orbit’s shape, size and their position in the phase space.Since these orbits can be used for the design of low energy transfer trajectories, soperturbations due to planetary oblateness has to be understood and should be taken care of during trajectory design. In this paper,detailed stability analysis of periodic orbit having three loops is given forA2= 0.0001.