On the Attitude Dynamics of Spinning Deformable Systems
- 1 June 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (6) , 812-817
- https://doi.org/10.2514/3.60442
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Attitude Stability of a Dual-Spin Satellite with a Large Flexible Solar ArrayJournal of Spacecraft and Rockets, 1973
- A Comparative Study of Stability Methods for Flexible SatellitesAIAA Journal, 1973
- A form of the translational dynamical equations for relative motion in systems of many non-rigid bodiesActa Mechanica, 1972
- Attitude dynamics of a three-axis stabilized satellite with a large flexible solar arrayPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Dynamics of Spinning Bodies Containing Elastic RodsJournal of Spacecraft and Rockets, 1972
- Liapunov stability of spinning satellites with long flexible appendagesCelestial Mechanics and Dynamical Astronomy, 1971
- A Method for the Liapunov Stability Analysis of Force-Free Dynamical SystemsAIAA Journal, 1971
- A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedomAIAA Journal, 1970
- Stability of a spinning body containing elastic parts via Liapunov'sdirect methodAIAA Journal, 1970
- Stability of the force-free motions of a dual- spin spacecraft.AIAA Journal, 1969