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Flight control application of new stability robustness bounds for linear uncertain systemsThis paper addresses the issue of obtaining bounds on the real parameter perturbations of a linear state-space model for robust stability. Based on Kronecker algebra, new, easily computable sufficient bounds are derived that are much less conservative than the existing bounds since the technique is meant for only real parameter perturbations (in contrast to specializing complex variation case to real parameter case). The proposed theory is illustrated with application to several flight control examples.
Document ID
19940034151
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Yedavalli, Rama K.
(Ohio State Univ. Columbus, United States)
Date Acquired
August 16, 2013
Publication Date
December 1, 1993
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 16
Issue: 6
ISSN: 0731-5090
Subject Category
Cybernetics
Accession Number
94A10806
Funding Number(s)
CONTRACT_GRANT: NAG1-1164
Distribution Limits
Public
Copyright
Other

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