Liapunov stability analysis of spinning flexible spacecraft.
- 1 April 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (4), 457-466
- https://doi.org/10.2514/3.6774
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Stability of Motion of Force-Free Spinning Satellites with Flexible AppendagesJournal of Spacecraft and Rockets, 1972
- | EQUATORIAL VIBRATIONS OF A LONG FLEXIBLE BOOM ON A SPIN-STABILIZED SATELLITE OF NON-ZERO RADIUSPublished by Elsevier BV ,1972
- A Method for the Liapunov Stability Analysis of Force-Free Dynamical SystemsAIAA Journal, 1971
- A study of the nutational behavior of a flexible spinning satellite using natural frequencies and modes of the rotating structurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,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
- Explanation of the anomalous spin behavior of satellites with long, flexible antennae.Journal of Spacecraft and Rockets, 1967
- Dynamics of an elastic satellite—IInternational Journal of Solids and Structures, 1967
- On the high-spin motion of a satellite containing elastic parts.Journal of Spacecraft and Rockets, 1966
- DYNAMlC STABILITY OF A GRAVITY GRADIENT STABILIZED SATELLITE HAVING LONG FLEXIBLE ANTENNASPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966