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Preliminary demonstration of a robust controller design methodAlternative computational procedures for obtaining a feedback control law which yields a control signal based on measurable quantitites are evaluated. The three methods evaluated are: (1) the standard linear quadratic regulator design model; (2) minimization of the norm of the feedback matrix, k via nonlinear programming subject to the constraint that the closed loop eigenvalues be in a specified domain in the complex plane; and (3) maximize the angles between the closed loop eigenvectors in combination with minimizing the norm of K also via the constrained nonlinear programming. The third or robust design method was chosen to yield a closed loop system whose eigenvalues are insensitive to small changes in the A and B matrices. The relationship between orthogonality of closed loop eigenvectors and the sensitivity of closed loop eigenvalues is described. Computer programs are described.
Document ID
19810011295
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, L. R.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 15, 1980
Subject Category
Cybernetics
Report/Patent Number
NASA-CR-164010
VPI-AERO-120
Report Number: NASA-CR-164010
Report Number: VPI-AERO-120
Accession Number
81N19822
Funding Number(s)
CONTRACT_GRANT: NAG1-80
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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