A Method for the Liapunov Stability Analysis of Force-Free Dynamical Systems
Author:
Affiliation:
1. University of Cincinnati, Cincinnati, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49975
Reference6 articles.
1. Stability of the force-free motions of a dual- spin spacecraft.
2. On the high-spin motion of a satellite containing elastic parts.
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1. Spin stability of undamped flexible structures rotating about the minor axis;AIAA Journal;1993-11
2. Optimal control of large space structures governed by a coupled system of ordinary and partial differential equations;Mathematics of Control, Signals, and Systems;1989-03
3. Mathematical modeling and control of large space structures with multiple appendages;Mathematical and Computer Modelling;1988
4. Stabilization of a class of hybrid systems arising in flexible spacecraft;Journal of Optimization Theory and Applications;1986-07
5. Stationary motions of a gyrostat with an elastic annular plate and their stability;Journal of Applied Mathematics and Mechanics;1984-01
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