一种可重构控制系统设计方法

The 23rd IEEE Conference on Decision and Control Pub Date : 1984-12-01 DOI:10.1109/CDC.1984.272266

D. Looze, S. Krolewski, J. Weiss, J. Eterno, S. Gully

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引用次数: 12

摘要

本文提出了一种针对一个或多个控制元件失效的飞机飞行控制系统的自动再设计方法。该程序是基于线性二次设计技术，并产生一个控制系统，最大限度地衡量反馈系统的性能受制于带宽限制。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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An approach to restructurable control system design

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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The 23rd IEEE Conference on Decision and Control

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