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Systematic Gain‐Scheduling Control Design: A Missile Autopilot Example
Author(s) -
Wu Fen,
Packard Andy,
Balas Gary
Publication year - 2002
Publication title -
asian journal of control
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.769
H-Index - 53
eISSN - 1934-6093
pISSN - 1561-8625
DOI - 10.1111/j.1934-6093.2002.tb00362.x
Subject(s) - autopilot , missile , control theory (sociology) , gain scheduling , control engineering , engineering , scheduling (production processes) , norm (philosophy) , missile guidance , computer science , control system , control (management) , aerospace engineering , law , operations management , electrical engineering , artificial intelligence , political science
The missile autopilot was designed using linear parameter‐varying (LPV) control techniques. The controller provides exponential stability guarantee and performance bound in terms of induced L 2 norm for the missile plant. The systematic gain‐scheduling approach is motivated by the recent development in LPV control theory and provides a well founded and systematic procedure for high performance missile autopilot design problem.