Nonlinear missile autopilot design using time-scale separation
Author:
Affiliation:
1. Optimal Synthesis, Palo Alto, CA
2. U.S. Navy, Naval Surface Warfare Center, Dahlgren, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3765
Reference40 articles.
1. Root-mean-square miss distance of proportional navigation missile against sinusoidal target
2. Gain-scheduled missile autopilot design using linear parameter varying transformations
3. Dynamic scheduling of modern-robust-control autopilot designs for missiles
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