Stability analysis of dynamic inversion controllers using time-scale separation
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
2. Michigan, Univ., Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4322
Reference11 articles.
1. W, Hahn, "Stability ofMotion," Springer-Verlag New York Inc. 1967, pp102-115, 271-278.
2. H. K. Khalil, "Nonlinear Systems," Macmillan Publishing Company, 1992, pp.97-122, 136-151.
3. Missile flight control with dynamic inversion and structured singular value synthesis
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