Semi-analytical solution for the trapped orbits of satellite near the planet in ER3BP

Author:

Ershkov SergeyORCID,Rachinskaya Alla

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering

Reference35 articles.

1. Cabral, F., Gil, P.: On the Stability of Quasi-Satellite Orbits in the Elliptic Restricted Three-Body Problem. Master Thesis at the Universidade T’ecnica de Lisboa (2011)

2. Arnold, V.: Mathematical Methods of Classical Mechanics. Springer, New York (1978)

3. Lagrange, J.: ’OEuvres’ (M.J.A. Serret, Ed.). Vol. 6, published by Gautier-Villars, Paris (1873)

4. Duboshin G.N.: Nebesnaja mehanika. Osnovnye zadachi i metody. Moscow: “Nauka” (handbook for Celestial Mechanics, in russian) (1968)

5. Szebehely, V.: Theory of Orbits. Yale University, New Haven, Connecticut. Academic Press, New-York and London, The Restricted Problem of Three Bodies (1967)

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