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自适应二阶滑模制导律

花文华 陈兴林

现代防御技术2011,Vol.39Issue(6):121-125,143,6.
现代防御技术2011,Vol.39Issue(6):121-125,143,6.DOI:10.3969/j.issn.1009-086x.2011.06.023

自适应二阶滑模制导律

Self-Adaptive Second Order Sliding-Mode Guidance Law

花文华 1陈兴林1

作者信息

  • 1. 哈尔滨工业大学航天学院,黑龙江哈尔滨 150001
  • 折叠

摘要

Abstract

Conventional guidance laws designed based on Lyapunov theorems can not ensure the finite time convergence of guidance system. A novel second-order sliding-mode control approach with finite time convergence is presented by using sliding-mode control theory and is used in a maneuvering target interception scenario for a guidance law design. The first part of this guidance law features similar structure of proportional navigation with time-varying effective navigation ratio, so that the line-of-sight rate tends to zero. The extension part of this guidance law features line-of-sight ( LoS) shaping, finite time convergence of sliding mode surface and robustness to the variation of interception missile and target velocities. The simulations with nonlinear motion model are carried out for two typical target maneuvers. The results show that this guidance law can intercept the target effectively and can verify the above features.

关键词

滑模制导/自适应控制/有限时间收敛/视线成型

Key words

sliding-mode guidance/ adaptive control/ finite time convergence/ line-of-sight (LoS) shaping

分类

军事科技

引用本文复制引用

花文华,陈兴林..自适应二阶滑模制导律[J].现代防御技术,2011,39(6):121-125,143,6.

基金项目

黑龙江省科技攻关计划(GZ06A 104) (GZ06A 104)

现代防御技术

OA北大核心CSTPCD

1009-086X

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