The behavior of a satellite trajectory near the equilibrium points of sun-earth system and its control

In this paper, the behavior of a satellite trajectory near the equilibrium points of the Sun-Earth system is studied. The equations describing the motion of the satellite in the circular restricted three body problem for the Sun-Earth system, are discussed for their ordinary differential equations f...

Full description

Bibliographic Details
Main Authors: Shalby Lina A., Ali Noha A.
Format: Article
Language:English
Published: Serbian Society of Mechanics & Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade 2023-01-01
Series:Theoretical and Applied Mechanics
Subjects:
Online Access:https://doiserbia.nb.rs/img/doi/1450-5584/2023/1450-55842300003S.pdf