Attitude dynamics of a rigid body on a Keplerian orbit: A simplification

Author:

Arribas Mercedes,Elipe Antonio

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modeling and Simulation

Reference9 articles.

1. Andoyer, H.: 1923,Course de Mécanique Céleste. Gauthier-Villars. Paris.

2. Chernous'ko, F.L.: 1963, On the motion of a satellite about its center of mass under the action of gravitational moments,Prikladnaya Mathematic Mechanica 27, 474?483.

3. Cochran, J.: 1972, Effects of gravity-gradient torque on the motion of a triaxial satellite,Celestial Mechanics 6, 131?152.

4. Deprit A. and Miller B.: 1989, Simplify or perish. Proceedings of the 109th Colloquium of the International Astronomical Union: Applications of Computer Technology to Dynamical Astronomy,Celestial Mechanics 45, 189?200.

5. Hughes, P.C.: 1986,Spacecraft Attitude Dynamics John Wiley and sons. New York.

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