Attitude Stability of a Dual-Spin Satellite with a Large Flexible Solar Array
- 1 February 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 10 (2) , 126-132
- https://doi.org/10.2514/3.61857
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
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- Stability of a dual spin satellite with two dampersJournal of Spacecraft and Rockets, 1971
- Influence of flexible appendages on dual-spin spacecraft dynamics and controlJournal of Spacecraft and Rockets, 1970
- Stability of a spinning body containing elastic parts via Liapunov'sdirect methodAIAA Journal, 1970
- Oriented flexible rolled-up solar arrayPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Dynamics of Spin-Stabilized Flexible Satellites of Crossed-Dipole ConfigurationPublished by Springer Nature ,1970
- Effects of energy dissipation on the attitude stability of dual-spinsatellites.AIAA Journal, 1969
- Attitude stability criteria for dual spin spacecraft.Journal of Spacecraft and Rockets, 1967
- On the high-spin motion of a satellite containing elastic parts.Journal of Spacecraft and Rockets, 1966
- Rotation of Artificial Earth SatellitesNature, 1958