Second-order theory of the rotation of an artificial satellite-Reference-Cited by-同舟云学术

Second-order theory of the rotation of an artificial satellite

Published:1987-03 Issue:1-4 Volume:42 Page:141-168
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Bois Eric

Publisher

Springer Science and Business Media LLC

Subject

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

Link

http://link.springer.com/content/pdf/10.1007/BF01232953.pdf

Reference5 articles.

1. Bois, E., 1986, ?First-order theory of satellite attitude motion-Application to HIPPARCOS?,Celest. Mech. 39, 309?327.

2. Bois, E., 1987, ?Théorie Analytique de la Rotation d'un Satellite Artificiel-Application à HIPPARCOS?, Thèse de Doctorat, Observatoire de Paris.

3. Donati, F., Canuto, E., Fassino, B. and Belforte, P., 1986, ?High accuracy on-ground attitude reconstitution for the ESA astrometry HIPPARCOS mission?,Manuscripta Geodaetica 11, 119.

4. Kovalevsky, J., 1982,The satellite HIPPARCOS, Proceedings of an International Colloquium on the scientific aspects of the HIPPARCOS mission, held at Strasbourg, ESA-SP-177, p. 15?20.

5. Kovalevsky, J. and Bois, E., 1986, ?Attitude determination of the HIPPARCOS satellite?,Space Dynamics and Celestial Mechanics, p. 345?354.

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