Guidance Laws Based on Input-to-State Stability and High-Gain Observers

被引：45
|
作者：
Yan, Han [1 ]
Ji, Hai-Bo [1 ]
机构：
[1] Univ Sci & Technol China, Dept Automat, Hefei 230026, Peoples R China
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2012年 / 48卷 / 03期
基金：
中国国家自然科学基金;
关键词：
OUTPUT-FEEDBACK STABILIZATION; VARIABLE-STRUCTURE CONTROL; CONTROL LOOP DYNAMICS; PROPORTIONAL NAVIGATION; NONLINEAR-SYSTEMS; HOMING MISSILE;
D O I：
10.1109/TAES.2012.6237606
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A novel three-dimensional guidance law based on input-to-state stability (ISS) and high-gain observers for interception of maneuvering targets is proposed. The ISS method is introduced to design a guidance law to achieve robust tracking of a maneuvering target. Since in practice the line-of-sight (LOS) rate is difficult for a pursuer to measure accurately, a high-gain observer is utilized to estimate it. Stability analysis as well as simulation results show that the presented approach is effective.
引用
收藏
页码：2518 / 2529
页数：12
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