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An automatic redesign approach for restructurable control systemsThis paper presents an approach to the automatic redesign of flight control systems for aircraft that have suffered one or more control element failures. The procedure is based on Linear Quadratic design techniques, and produces a control system that maximizes a measure of feedback system performance subject to a bandwidth constraint.
Document ID
19860043656
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Looze, D. P. (Alphatech, Inc. Burlington, MA, United States)
Weiss, J. L. (Alphatech, Inc. Burlington, MA, United States)
Eterno, J. S. (Alphatech, Inc. Burlington, MA, United States)
Barrett, N. M. (ALPHATECH, Inc. Burlington, MA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Stability And Control
Accession Number
86A28394
Funding Number(s)
CONTRACT_GRANT: NAS1-17411
Distribution Limits
Public
Copyright
Other

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