A Comparative Study of Stability Methods for Flexible Satellites
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Va.
2. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference11 articles.
1. Stability of a spinning body containing elastic parts via Liapunov'sdirect method
2. On the high-spin motion of a satellite containing elastic parts.
3. A Method for the Liapunov Stability Analysis of Force-Free Dynamical Systems
4. Liapunov stability analysis of hybrid dynamical systems with multi-elastic domains†
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