Thermally Induced Nutational Body Motion of a Spinning Spacecraft with Flexible Appendages
Author:
Affiliation:
1. Mitsubishi Electric Corporation, Amagasaki, Hyogo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49728
Reference11 articles.
1. Stability of Motion of Force-Free Spinning Satellites with Flexible Appendages
2. Liapunov stability of spinning satellites with long flexible appendages
3. Liapunov stability analysis of spinning flexible spacecraft.
4. Explanation of the anomalous spin behavior of satellites with long, flexible antennae.
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