Attitude Dynamics of a Satellite During Deployment of Large Plate-Type Structures
- 1 September 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 5 (5) , 442-447
- https://doi.org/10.2514/3.56192
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- Transient attitude dynamics of satellites with deploying flexible appendagesActa Astronautica, 1978
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- Attitude Dynamics of Satellites with Flexible Appendages- A Brief ReviewJournal of Spacecraft and Rockets, 1974
- Dynamics of spin-stabilized satellites during extension of long flexible boomsJournal of Spacecraft and Rockets, 1971
- Optimization of RAE satellite boom deployment timingJournal of Spacecraft and Rockets, 1970
- Dynamics of deployment of extendible booms from spinning space vehicles.Journal of Spacecraft and Rockets, 1968