Dynamics of gravity-oriented orbiting systems with application to passive stabilization
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2491
Reference11 articles.
1. Attitude Control of Satellites and Space Vehicles
2. Etkin, B , "Attitude stability of articulated gravity-oriented satellites Part 1-General theory and motion in orbital plane," Univ of Toronto, Institute of Aerophysics Rept 89 (1962)
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1. A Control System for Orbiting Tethered-Body Operations;IFAC Proceedings Volumes;1975-08
2. An optimization technique for the transient response of passively stable satellites;Journal of Optimization Theory and Applications;1972-12
3. Use of Fibers in Gravity-Gradient Stabilization Systems;Journal of Spacecraft and Rockets;1971-10
4. Optimal configurations for hinged, two-body satellites.;Journal of Spacecraft and Rockets;1969-09
5. Degree-of-freedom requirements for hinged multibody satellites.;Journal of Spacecraft and Rockets;1969-04
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