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Control design for robust stability in linear regulators: Application to aerospace flight controlTime domain stability robustness analysis and design for linear multivariable uncertain systems with bounded uncertainties is the central theme of the research. After reviewing the recently developed upper bounds on the linear elemental (structured), time varying perturbation of an asymptotically stable linear time invariant regulator, it is shown that it is possible to further improve these bounds by employing state transformations. Then introducing a quantitative measure called the stability robustness index, a state feedback conrol design algorithm is presented for a general linear regulator problem and then specialized to the case of modal systems as well as matched systems. The extension of the algorithm to stochastic systems with Kalman filter as the state estimator is presented. Finally an algorithm for robust dynamic compensator design is presented using Parameter Optimization (PO) procedure. Applications in a aircraft control and flexible structure control are presented along with a comparison with other existing methods.
Document ID
19860021793
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yedavalli, R. K.
(Toledo Univ. OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Cybernetics
Report/Patent Number
NAS 1.26:176858
NASA-CR-176858
Report Number: NAS 1.26:176858
Report Number: NASA-CR-176858
Accession Number
86N31265
Funding Number(s)
CONTRACT_GRANT: NAG1-578
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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