First-order accurate theory of perturbed circular motion

Author:

Bois E.

Publisher

Springer Science and Business Media LLC

Subject

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

Reference14 articles.

1. Bois, E.: 1986, ?First-Order Theory of Satellite Attitude Motion ? Application to HIPPARCOS?,Celestial Mechanics 39, 309?327.

2. Bois, E.: 1988, ?Second-Order Theory of the Rotation of an Artificial Satellite?,Celestial Mechanics 42, 141?168.

3. Bois, E.: 1990, ?Analytical Theory of Perturbed Circular Orbital Motion?,3rd International COGEOS Workshop, Brussels, Belgium, June 90.

4. Bois, E., Exertier, P., and Wytrzyszczak, I.: 1991, ?Algorithmic Formulation for Perturbed Circular Motion?,4th International COGEOS Workshop, Pisa, Italy, June 91.

5. Bois, E. and Kovalevsky, J.: 1990, ?Analytical Model of the Rotation of an Artificial Satellite?,Journal of Guidance, Control and Dynamics 13, No. 4, Publication of the American Institute of Aeronautics and Astronautics, pp. 638?643.

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