Stability of a Dual-Spin Spacecraft with a Flexible Momentum Wheel
- 1 September 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (9) , 640-646
- https://doi.org/10.2514/3.61768
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Variable Parameter Nutation Damper for SAS-AJournal of Spacecraft and Rockets, 1971
- Stable Limit Cycles due to Nonlinear Damping in Dual-Spin SpacecraftJournal of Spacecraft and Rockets, 1971
- Motion and stability of a dual-spin satellite with nutation dampingJournal of Spacecraft and Rockets, 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