ENHANCED ROBUSTNESS IN INTEGRATED STRUCTURAL CONTROL-SYSTEMS DESIGN

被引：11

作者：

GRANDHI, RV ^{[1
]}

HAQ, I ^{[1
]}

机构：

[1] USAF,WRIGHT AERONAUT LABS,WRIGHT PATTERSON AFB,OH 45433

来源：

AIAA JOURNAL | 1991年 / 29卷 / 07期

关键词：

D O I：

10.2514/3.10719

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper addresses maximizing the robustness of an integrated structural/control system for increasing the stability margin under parametric uncertainties. The robustness limit is defined for a linear time-invariant system consisting of structured perturbations. The optimization problem has considered the closed-loop eigenvalues, damping parameter, and robustness as design constraints. Effects of increasing the stability robustness of a closed-loop system are demonstrated on two structural optimization examples.

引用

页码：1168 / 1173

页数：6

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