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：
中国国家自然科学基金; 美国国家科学基金会;
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
收藏
页码：177 / 186
页数：10
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