Gravity-gradient stabilization of gyrostat satellites with rotor axes in principal planes-Reference-Cited by-同舟云学术

Gravity-gradient stabilization of gyrostat satellites with rotor axes in principal planes

Published:1971-06 Issue:2 Volume:3 Page:169-188
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Longman Richard W.

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/BF01228031.pdf

Reference11 articles.

1. Anchev, A. A.: 1966, ?Flywheel Stabilization of Relative Equilibrium of a Satellite?,Kosm. Issl. 4, 192?202.

2. Likins, P. W. and Roberson, R. E.: 1966, ?Uniqueness of Equilibrium Attitudes for Earth-Pointing Satellites?,J. Astronaut. Sci. 13, 87?88.

3. Longman, R. W.: 1969a, ?A Generalized Approach to Gravity-Gradient Stabilization of Gyrostat Satellites?, The RAND Corporation, RM-5921-PR.

4. Longman, R. W.: 1969b, ?The Equilibria of Orbiting Gyrostats with Internal Angular Momenta Along Principal Axes?, Proceedings of the Symposium on Gravity Gradient Attitude Stabilization, Aerospace Corporation Report No. TR-0066(5143)-1 (Air Force Report No. SAMSO-TR-69-307). Also available as RAND Corporation P-3916, Aug. 1968.

5. Longman, R. W. and Roberson, R. E.: 1969, General Solution for the Equilibria of Orbiting Gyrostats Subject to Gravitational Torques?,J. Astronaut. Sci. 16, 49?58.

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