Publisher
American Institute of Aeronautics and Astronautics
Reference37 articles.
1. Aircraft flight controls design using constrained output feedback - An H-infinity loopshaping approach
2. Farret D., Due G., Harcaut J. P., Multi-rate H∞loop shaping control applied to missile autopilot design,AIAAGuidance,Navigation,andControlConference, 6-9August2001, Canada.
3. Smit M. Z., Criig I. K., Robust flight controller design using H∞loop shaping and dynamic inversion techniques,AIAA-98-4132,1998.
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