Thermally Induced Nutational Body Motion of a Spinning Spacecraft with Flexible Appendages
- 1 April 1975
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (4) , 448-453
- https://doi.org/10.2514/3.49728
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Nonlinear Oscillations in Physical SystemsPublished by Walter de Gruyter GmbH ,1986
- Liapunov stability analysis of spinning flexible spacecraft.AIAA Journal, 1973
- Stability of Motion of Force-Free Spinning Satellites with Flexible AppendagesJournal of Spacecraft and Rockets, 1972
- Liapunov stability of spinning satellites with long flexible appendagesCelestial Mechanics and Dynamical Astronomy, 1971
- Thermally induced vibrations of long thin- walled cylinders of open sectionJournal of Spacecraft and Rockets, 1970
- Thermally induced vibration and flutter of a flexible boom.Journal of Spacecraft and Rockets, 1969
- Explanation of the anomalous spin behavior of satellites with long, flexible antennae.Journal of Spacecraft and Rockets, 1967
- AVERAGING IN SYSTEMS OF ORDINARY DIFFERENTIAL EQUATIONSRussian Mathematical Surveys, 1962