LPV control design for pitch-axis missile autopilots

The missile pitch-axis autopilot is designed using linear parameter-varying (LPV) control theory. The controller guarantees quadratic stability and bounded induced L/sub 2/-norm performance for the missile plant. Our approach is motivated by gain-scheduling methodology and provides a well founded an...

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Bibliographic Details
Published inProceedings of 1995 34th IEEE Conference on Decision and Control Vol. 1; pp. 188 - 193 vol.1
Main Authors Fen Wu, Packard, A., Balas, G.
Format Conference Proceeding
LanguageEnglish
Published IEEE Control Systems Society 1995
Subjects
Control design
Control system synthesis
Control theory
Design methodology
Educational institutions
Mechanical engineering
Missiles
Open loop systems
Robust control
Robust stability
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Summary:The missile pitch-axis autopilot is designed using linear parameter-varying (LPV) control theory. The controller guarantees quadratic stability and bounded induced L/sub 2/-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.
ISBN:0780326857
9780780326859
ISSN:0191-2216
DOI:10.1109/CDC.1995.478672