Guidance law implementation with performance recovery using an extended high-gain observer

被引：31

作者：

Ma, Kemao ^{[1
]}

Khalil, Hassan K. ^{[2
]}

Yao, Yu ^{[1
]}

机构：

[1] Harbin Inst Technol, Sch Astronaut, Control & Simulat Ctr, Harbin 150080, Peoples R China

[2] Michigan State Univ, Dept Elect & Comp Engn, E Lansing, MI 48823 USA

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2013年 / 24卷 / 01期

基金：

美国国家科学基金会; 中国国家自然科学基金;

关键词：

Guidance law; Target maneuver; High-gain observer; Performance recovery; PARTIAL STABILITY; HOMING MISSILE; STABILIZATION;

D O I：

10.1016/j.ast.2011.11.005

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input-multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance. (C) 2011 Elsevier Masson SAS. All rights reserved.

引用

页码：177 / 186

页数：10

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