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

DOI10.2298/TAM220816003SOpenAlexW4362684099MaRDI QIDQ6119877

Unnamed Author, Unnamed Author

Publication date: 20 February 2024

Published in: Theoretical and Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2298/tam220816003s

zbMATH Keywords

stabilitychaosLagrange pointscircular restricted three body problem

Mathematics Subject Classification ID

Three-body problems (70F07)

Cites Work

• On the stability of artificial equilibrium points in the circular restricted three-body problem
• Solar sail dynamics in the three-body problem: Homoclinic paths of points and orbits
• Dynamics in the center manifold of the collinear points of the restricted three-body problem
• Minimum fuel-consumption stabilization of a spacecraft at the Lagrangian points
• Solar sail periodic orbits in the elliptic restricted three-body problem

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