Exploitation of inertial coupling in passive gravity-gradient-stabilized satellites
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27665
Reference5 articles.
1. Doolin, B. F. "Gravity torque on an orbiting vehicle," NASA TND-70C1959).
2. The potential energy of a small rigid body in the gravitational field of an oblate spheroid
3. Fishell, R. E. and Mobley, F. F. "A system for passive gravity stabilization of earth satellites/7AIAA Preprint 63-326 (1963).
4. "Vertistat": An Improved Satellite Orientation Device
5. Damping of a Gravitationally Oriented Two-Body Satellite
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1. Two Decades of Spacecraft Attitude Control;Journal of Guidance and Control;1979-01
2. Nontrivial equilibrium and Liapunov stability of flexible damped gravity satellite as a hybrid dynamical system;16th Aerospace Sciences Meeting;1978-01-16
3. Explicit attitude stability criteria for passive, earth-pointing satellites;Journal of Spacecraft and Rockets;1976-03
4. Influence of Thermal Distortion on Gravity Gradient Stabilization;Journal of Spacecraft and Rockets;1975-07
5. Influence of thermal distortion on the anomalous behavior of a gravity gradient satellite;Mechanics and Control of Flight Conference;1974-08-05
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