Abstract
The motion properties of the infinitesimal body is studied under the forces due to kerr-like oblate heterogeneous primary, continuation fractional potential for secondary, solar sail, three-body interactions, Coriolis and centrifugal forces in the circular restricted three-body problem. The equations of motion of infinitesimal body are evaluated under the above-said perturbations. Using these equations of motion, we illustrate the locations of equilibrium points, their stability, the periodic orbits and Poincaré surfaces of section. This study will applicable on the motion of the artificial satellite.
Recommended Citation
Sahdev, Shiv K. and ., Abdullah
(2024).
(R2086) Circular Restricted Three-Body Interaction Problem With Various Perturbations,
Applications and Applied Mathematics: An International Journal (AAM), Vol. 19,
Iss.
1, Article 15.
Available at:
https://digitalcommons.pvamu.edu/aam/vol19/iss1/15