Title :
LPV control design for pitch-axis missile autopilots
Author :
Wu, Fen ; Packard, Andy ; Balas, Gary
Author_Institution :
Centre for Process Syst. Eng., Imperial Coll. of Sci., Technol. & Med., London, UK
Abstract :
The missile pitch-axis autopilot is designed using linear parameter-varying (LPV) control theory. The controller guarantees quadratic stability and bounded induced L2-norm performance for the missile plant. Our approach is motivated by gain-scheduling methodology and provides a well founded and systematic procedure for high performance missile autopilot design
Keywords :
missile control; stability; stability criteria; LPV control design; bounded induced L2-norm performance; gain-scheduling methodology; linear parameter-varying control; pitch-axis missile autopilots; quadratic stability; Control design; Control system synthesis; Control theory; Design methodology; Educational institutions; Mechanical engineering; Missiles; Open loop systems; Robust control; Robust stability;
Conference_Titel :
Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
Conference_Location :
New Orleans, LA
Print_ISBN :
0-7803-2685-7
DOI :
10.1109/CDC.1995.478672
