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机动目标拦截末制导技术研究

董霓 徐俊艳

现代防御技术2017,Vol.45Issue(6):5-10,6.
现代防御技术2017,Vol.45Issue(6):5-10,6.DOI:10.3969/j.issn.1009-086x.2017.06.002

机动目标拦截末制导技术研究

Terminal Guidance Law Based on Maneuvering Targets

董霓 1徐俊艳2

作者信息

  • 1. 北京电子工程总体研究所,北京100854
  • 2. 航天系统仿真重点实验室,北京100854
  • 折叠

摘要

Abstract

A nonlinear system guidance law which is also called nonlinear sliding mode guidance law with strong robustness is chosen for studying,which could take advantage in intercepting process of maneuvering targets with respect to maneuvering acceleration.To analyze the accuracy of whole research,simulation results are presented to demonstrate that the performance of the terminal control and guidance laws designed can satisfy the request of maneuvering target interception.

关键词

机动目标/拦截/末制导/视线转率/滑模变结构/制导律

Key words

maneuverable target/interception/terminal guidance/line of sight conversion efficiency/sliding variable structure/guidance law

分类

军事科技

引用本文复制引用

董霓,徐俊艳..机动目标拦截末制导技术研究[J].现代防御技术,2017,45(6):5-10,6.

现代防御技术

OACSTPCD

1009-086X

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