Aircraft control with anti-windup compensation

被引:0
作者
G. A. Leonov
B. R. Andrievskii
N. V. Kuznetsov
A. Yu. Pogromskii
机构
[1] St. Petersburg State University,Institute of Problems of Mechanical Engineering
[2] Russian Academy of Sciences,undefined
[3] University of Jyväskylä,undefined
[4] Eindhoven University of Technology,undefined
来源
Differential Equations | 2012年 / 48卷
关键词
Reference Signal; Linear Matrix Inequality; Harmonic Balance Method; Aircraft Control; Nyquist Curve;
D O I
暂无
中图分类号
学科分类号
摘要
We consider an anti-windup compensation method ensuring the convergence of the closed-loop system for a class of reference signals. An application of the method to an aircraft flight control problem is shown.
引用
收藏
页码:1700 / 1720
页数:20
相关论文
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