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一种新的有限时间收敛的末制导律设计

李磊 郭建国 周军 王国庆

火力与指挥控制Issue(12):145-148,4.
火力与指挥控制Issue(12):145-148,4.

一种新的有限时间收敛的末制导律设计

A New Terminal Guidance Law Design with Finite Time Convergence

李磊 1郭建国 1周军 1王国庆2

作者信息

  • 1. 西北工业大学精确制导与控制研究所,西安 710072
  • 2. 中国运载火箭技术研究院研究发展中心,北京 100076
  • 折叠

摘要

Abstract

For the case of a three-dimensional interception, a new nonlinear terminal guidance law with finite time convergence is proposed. Firstly,the basic design rules are given according to the mathematic model of three-dimensional relationship between missile and target. Secondly,a new integral sliding mode is present to avoid the singular problem of traditional terminal sliding mode. A robust terminal guidance law is designed,zeroing the rate of line-of-sight angle and finite time convergence stability of guidance system are strictly proven by Lyapunov stability theory. Finally an illustrative example is given to show that better precision and finite time convergence stability are obtained under the new guidance law for intercepting the target with maneuver than proportional navigation law.

关键词

制导律/有限时间收敛/Terminal滑模/视线角速率

Key words

Guidance law/finite time convergence/terminal sliding mode/rate of line-of-sight angle

分类

军事科技

引用本文复制引用

李磊,郭建国,周军,王国庆..一种新的有限时间收敛的末制导律设计[J].火力与指挥控制,2015,(12):145-148,4.

基金项目

航天科技创新基金资助项目 ()

火力与指挥控制

OA北大核心CSCDCSTPCD

1002-0640

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