Guidance and Control of Missile Interceptor using Second-Order Sliding Modes

被引：281

作者：

Shtessel, Yuri B. ^{[1
]}

Shkolnikov, Ilya A. ^{[2
]}

Levant, Arie ^{[3
]}

机构：

[1] Univ Alabama, Dept Elect & Comp Engn, Huntsville, AL 35899 USA

[2] ZI Imaging Corp, Madison, AL 35757 USA

[3] Tel Aviv Univ, Dept Appl Math, IL-69978 Tel Aviv, Israel

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2009年 / 45卷 / 01期

关键词：

HOMING GUIDANCE; SYSTEMS; DESIGN; DIFFERENTIATION;

D O I：

10.1109/TAES.2009.4805267

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A new smooth second-order sliding mode control (SSOSM) is proposed and proved for a system driven by uncertain sufficiently smooth disturbances. The main target application of this technique, the missile interceptor guidance-control system against targets performing evasive maneuvers, is considered to demonstrate benefits of this design for a two-loop integration of guidance and flight control systems. The designed guidance-control system performance is verified via computer simulations using a miniature hypervelocity kinetic energy endo-atmospheric interceptor planar model.

引用

页码：110 / 124

页数：15

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