Effect of gravity gradient on attitude control of a space station
Author:
Affiliation:
1. The Boeing Company, Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28194
Reference6 articles.
1. Gravitational Torque Impulse on a Stabilized Satellite
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1. Flugeigenschaften der drehsymmetrischen Flugkörper bei rückwirkungsfreien Rudern und ohne Flugregelung;Grundzüge der Flugmechanik und Ballistik;1969
2. A two-degree-of-freedom control moment gyro for high-accuracy attitude control.;Journal of Spacecraft and Rockets;1968-01
3. Synthetic fats as part of a closed-loop life support system.;Journal of Spacecraft and Rockets;1967-12
4. An optimum attitude profile to minimize the accumulation of gravity-gradient torque impulse.;Journal of Spacecraft and Rockets;1967-12
5. Control moment gyros in attitude control.;Journal of Spacecraft and Rockets;1966-09
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