Stable Limit Cycles due to Nonlinear Damping in Dual-Spin Spacecraft
- 1 June 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (6), 568-574
- https://doi.org/10.2514/3.59694
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Motion and stability of a dual-spin satellite with nutation dampingJournal of Spacecraft and Rockets, 1970
- Stability of a dual spin satellite with two dampersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Stability of the force-free motions of a dual- spin spacecraft.AIAA Journal, 1969
- Effects of energy dissipation on the attitude stability of dual-spinsatellites.AIAA Journal, 1969
- Optimal attitude control of a dual-spin satellite.Journal of Spacecraft and Rockets, 1968
- Stable rotation states of dual-spin spacecraft.Journal of Spacecraft and Rockets, 1968
- Attitude stability criteria for dual spin spacecraft.Journal of Spacecraft and Rockets, 1967
- Nutational stability of an axisymmetric body containing a rotorJournal of Spacecraft and Rockets, 1964