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 H 2/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
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