DocumentCode :
3467858
Title :
Generalized singular robust control design
Author :
Juang, J.C. ; Lin, C.F. ; Cloutier, J.R. ; Evers, J.H.
Author_Institution :
American GNC Corp., Chatsworth, CA, USA
fYear :
1991
fDate :
11-13 Dec 1991
Firstpage :
2995
Abstract :
A generalized singular robust control approach for missile autopilot design is described. This approach unifies the generalized singular linear quadratic linear quadratic Gaussian, and worst-case H control design methods using the generalized Hamiltonian formulation and structure algorithm. Extensions of this method to multiple-criterion autopilot design problems are also discussed. The approach considered provides a constructive algorithm to design a multiple-criterion controller and offers new insights into the relationship between multiple H2/H and multiple H /H designs
Keywords :
aerospace control; control system synthesis; missiles; optimal control; LQG control; aerospace control; generalized Hamiltonian formulation; generalized singular robust control; missile autopilot; multiple-criterion autopilot; singular linear quadratic control; worst-case H control; Aerodynamics; Algorithm design and analysis; Control design; Drag; Force control; Missiles; Observability; Robust control; Robust stability; Robustness; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1991., Proceedings of the 30th IEEE Conference on
Conference_Location :
Brighton
Print_ISBN :
0-7803-0450-0
Type :
conf
DOI :
10.1109/CDC.1991.261096
Filename :
261096
Link To Document :
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