Missile flight control with dynamic inversion and structured singular value synthesis
Author:
Affiliation:
1. USAF, Armament Directorate, Eglin AFB, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3604
Reference13 articles.
1. Nonlinear inversion flight control for a supermaneuverable aircraft
2. 89-20
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