Attitude stability of a gravity-stabilized gyrostat satellite-Reference-Cited by-同舟云学术

Attitude stability of a gravity-stabilized gyrostat satellite

Published:1970-06 Issue:2 Volume:2 Page:147-165
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Crespo da Silva Marcelo R. M.

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/BF01229493.pdf

Reference16 articles.

1. DeBra, D. B. and Delp, R. H.: 1961, ?Rigid Body Attitude Stability and Natural Frequencies in a Circular Orbit?,Journal of The Astronautical Sciences 8, 1, Spring.

2. DeBra, D. B.: 1962, The Large Attitude Motions and Stability, due to Gravity, of a Satellite with Passive Damping in an Orbit of Arbitrary Eccentricity about an Oblate Body. Ph.D. Dissertation, SUDAER report No. 126, Stanford University.

3. Kane, T. R.: 1965, ?Attitude Stability of Earth Pointing Satellites?,AIAA Journal 3, 4, April.

4. Breakwell, J. V. and Pringle, R., Jr.: 1966, ?Nonlinear Resonances Affecting Gravity Gradient Stability?, inAstrodynamics, Gauthier-Villars, Paris, pp. 305?25.

5. Kane, T. R. and Mingori, D. L.: 1965, ?Effect of a Rotor on the Attitude Stability of a Satellite in a Circular Orbit?,AIAA Journal 3, 5, May.

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