DocumentCode
1137237
Title
Robust control design for aerospace applications
Author
Yedavalli, Rama K.
Author_Institution
Ohio State Univ., Columbus, OH, USA
Volume
25
Issue
3
fYear
1989
fDate
5/1/1989 12:00:00 AM
Firstpage
314
Lastpage
324
Abstract
Time-domain control design for stability robustness of linear systems with structured uncertainty is addressed. Upper bounds on the linear perturbation of an asymptotically stable linear system are obtained, making it possible to maintain stability by using the structural information of the uncertainty. A quantitative measure called the stability robustness index is introduced and used to design controllers for robust stability. The proposed state feedback control design algorithm can be used, for a given set of perturbations, to select the range of control effort for which the system is stability-robust. Conversely it can be used, for a given control effort, to determine the size of the tolerable perturbation. The algorithm is illustrated with examples from aircraft control and large-space-structure control problems
Keywords
aerospace control; aircraft control; control system synthesis; feedback; linear systems; stability; time-domain synthesis; aerospace applications; aircraft control; asymptotically stable linear system; large-space-structure control; linear perturbation; stability robustness; state feedback control design algorithm; structured uncertainty; time domain control; tolerable perturbation; Aerospace control; Asymptotic stability; Control design; Linear systems; Measurement uncertainty; Robust control; Robust stability; State feedback; Time domain analysis; Upper bound;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.30786
Filename
30786
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