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)