Abstract
The elliptic restricted three-body problem investigates the motion behaviour of the variable mass infinitesimal body under the gravitational forces of the radiated oblate primary and dipole secondary. The equations of motion of the infinitesimal body are determined using Jeans law and Meshcherskii space time transformations. Using the Lindstedt-Poincaré method, we perform the solutions of the equations of motion. With the use of these solutions and the equations of motion, we numerically illustrate the time series, phase spaces, projections and the Halo orbits.
Recommended Citation
Ali, Majhar and ., Abdullah
(2025).
(R2122) Analysis of Halo Orbits in the Elliptical R3BP with Mass Variation,
Applications and Applied Mathematics: An International Journal (AAM), Vol. 20,
Iss.
2, Article 10.
Available at:
https://digitalcommons.pvamu.edu/aam/vol20/iss2/10