A dynamic inversion based control law with application to the high angle-of-attack research vehicle
Author:
Affiliation:
1. Honeywell Systems and Research Center, Minneapolis, MN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-3407
Reference57 articles.
1. Problem,"Journal of Aircraft, December 1973.
2. Document SUDAAR 563,July,1987.
3. Minnesota, 1988.
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