NASA NTRS · 19860043656
An automatic redesign approach for restructurable control systems
Abstract
This 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.
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Looze, D. P., Weiss, J. L., Eterno, J. S., Barrett, N. M.. 1985-01-01. An automatic redesign approach for restructurable control systems. https://ntrs.nasa.gov/citations/19860043656
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