Automated Design of Continuously-Adaptive Control: The "Super-Controller" Strategy for Reconfigurable Systems

J. Elder, R. Barron
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引用次数: 13

Abstract

Modern military aircraft undergo rapid and often unpredictable changes in dynamics during flight. Though curent control system design techniques may be adequate to handle the range of flight conditions and maneuvers demanded, further compensation for system malfunctions and/or battle damage has heretofore been extremely difficult - unless one has accepted significant performance penalties at each operating point to obtain a very conservative control solution that can deal with awide range of potential impairments. What is needed is a method for developing simple, robust, high-performance control systems that vary in real time with operating and fault condition changes in the system being controlled; that is, that "reconfigure" rapidly to face rapidly changing conditions. The "super-controller" strategy, outlined here, shows promise of meeting this need. This paper describes the super-controller design technique and preliminary simulation results based upon single and multiple simultaneous effector impairments of a control reconfigurable combat aircraft (CRCA).
连续自适应控制的自动化设计:可重构系统的“超级控制器”策略
现代军用飞机在飞行过程中会经历快速且往往不可预测的动力学变化。虽然目前的控制系统设计技术可能足以处理飞行条件和机动要求的范围,但对系统故障和/或战斗损坏的进一步补偿迄今为止是极其困难的-除非在每个操作点接受重大的性能损失,以获得一个非常保守的控制解决方案,可以处理广泛的潜在损害。我们需要的是一种开发简单、鲁棒、高性能的控制系统的方法,这种控制系统可以随着被控系统的运行和故障条件的变化而实时变化;也就是说,快速“重新配置”以面对快速变化的条件。这里概述的“超级控制器”策略有望满足这一需求。本文介绍了一种控制可重构作战飞机(CRCA)的基于单个和多个同步效应损伤的超级控制器设计技术和初步仿真结果。
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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