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Robust control design for a class of nonlinear uncertain systemswith application to missiles

机译:一类非线性不确定系统的鲁棒控制设计及其在导弹中的应用

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In this paper, we shall extend our study of the“recursive-interlacing” design technique of Kaloust and Qu(1995) to a larger class of nonlinear uncertain systems. Therecursive-interlacing design scheme, also referred to “genericdesign procedure”, is a step by step constructive procedure fordesigning robust control for nonlinear systems with additiveunstructured uncertainties. The design procedure is based on theLyapunov's direct method and includes recursive or back-stepping designsas special cases. Nonlinear system under investigation containsuncertainties that do not satisfy any of the previously developedconditions such as the matching conditions, the conditions of beingequivalently matched, and the generalized matching conditions. A classof third order nonlinear uncertain systems is introduced for whichrobust control is designed using the recursive-interlacing designprocedure. The need for such a design scheme emanates from the fact thata wide range of physical systems such as missiles belong to this classof nonlinear uncertain systems
机译:在本文中,我们将扩展对 Kaloust和Qu的“递归交错”设计技术 (1995年)到一类更大的非线性不确定系统。这 递归交错设计方案,也称为“通用” 设计程序”,是针对 设计具有加性的非线性系统的鲁棒控制 非结构性不确定性。设计程序基于 Lyapunov的直接方法,包括递归或后推设计 作为特殊情况。正在研究的非线性系统包含 不满足任何先前开发的不确定性 匹配条件等条件 等价匹配,以及广义匹配条件。一类 引入三阶非线性不确定系统 使用递归交错设计来设计鲁棒控制 程序。对这样的设计方案的需求源于以下事实: 诸如导弹等各种各样的物理系统都属于此类 非线性不确定系统

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