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A computerized compensator design algorithm with launch vehicle applicationsThis short paper presents a computerized algorithm for the design of compensators for large launch vehicles. The algorithm is applicable to the design of compensators for linear, time-invariant, control systems with a plant possessing a single control input and multioutputs. The achievement of frequency response specifications is cast into a strict constraint mathematical programming format. An improved solution algorithm for solving this type of problem is given, along with the mathematical necessities for application to systems of the above type. A computer program, compensator improvement program (CIP), has been developed and applied to a pragmatic space-industry-related example.
Document ID
19760050341
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mitchell, J. R.
(Mississippi State Univ. Mississippi State, MS, United States)
Mcdaniel, W. L., Jr.
(Mississippi State University Mississippi State, Miss., United States)
Date Acquired
August 8, 2013
Publication Date
June 1, 1976
Publication Information
Publication: IEEE Transactions on Automatic Control
Volume: AC-21
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76A33307
Funding Number(s)
CONTRACT_GRANT: NAS8-21377
Distribution Limits
Public
Copyright
Other

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