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Stability robustness improvement of direct eigenspace assignment based feedback systems using singular value sensitivitiesA methodology to improve the stability robustness of feedback control systems designed using direct eigenspace assignment techniques is presented. The method consists of considering the sensitivity of the minimum singular value of the return difference transfer matrix at the plant input to small changes in the desired closed-loop eigenvalues and the specified elements of the desired closed-loop eigenvectors. Closed-form expressions for the gradient of the minimum return difference singular value with respect to desired closed-loop eigenvalue and eigenvector parameters are derived. Closed-form expressions for the gradients of the control feedback gains with respect to the specified eigenspace parameters are obtained as an intermediate step. The use of the gradient information to improve the guaranteed gain and phase margins in eigenspace assignment based designs is demonstrated by application to an advanced fighter aircraft.
Document ID
19890018301
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Garg, Sanjay
(Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-182302
NAS 1.26:182302
E-4853
Accession Number
89N27672
Funding Number(s)
PROJECT: RTOP 505-62-01
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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