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Robust control design for aerospace applicationsTime-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.
Document ID
19890057686
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Yedavalli, Rama K.
(Ohio State University Columbus, United States)
Date Acquired
August 14, 2013
Publication Date
May 1, 1989
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: 25
ISSN: 0018-9251
Subject Category
Cybernetics
Accession Number
89A45057
Funding Number(s)
CONTRACT_GRANT: F33615-84-K-3606
CONTRACT_GRANT: NAG1-578
Distribution Limits
Public
Copyright
Other

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