Linear-Parameter-Varying/Loop-Shaping H Synthesis for a Missile Autopilot
Author:
Affiliation:
1. Ecole Superieure d’Electricite, F91192 Gif-sur-Yvette, France
2. Aerospatiale, F92320 Chatillon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4821
Reference21 articles.
1. Modern control theory for design of autopilots for bank-to-turn missiles
2. Dynamic scheduling of modern-robust-control autopilot designs for missiles
3. Gain scheduling for H-infinity controllers: a flight control example
4. Gain-scheduled bank-to-turn autopilot design using linear parameter varying transformations
5. Self-scheduled H-infinity control of missile via linear matrix inequalities
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1. Robust gain-scheduled missile autopilot design based on multifrequency extended state observers;Chinese Journal of Aeronautics;2023-12
2. Trajectory tracking using robust gain-scheduling control with a new independent variable;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-09-13
3. Roll-Pitch-Yaw Integrated Robust Autopilot Design for a High Angle-of-Attack Missile;Journal of Guidance, Control, and Dynamics;2009-09
4. Robust Roll-Pitch-Yaw Integrated Autopilot for a High Angle-of-Attack Missile;AIAA Guidance, Navigation and Control Conference and Exhibit;2008-06-15
5. A GENETIC APPROACH TO ANTI-AIR MISSILE CONTROL SYSTEM DESIGN;IFAC Proceedings Volumes;2007
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