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

页码：2518 / 2529

页数：12

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