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进入角约束下的载机变结构远距引导

俞吉 周德云 马云红 周灿辉

指挥控制与仿真2013,Vol.35Issue(4):108-111,117,5.
指挥控制与仿真2013,Vol.35Issue(4):108-111,117,5.DOI:10.3969/j.issn.1673-3819.2013.04.026

进入角约束下的载机变结构远距引导

Study on a Long-Distance Navigation Method with Entrance Angle Constraints for Vehicles Based on Variable Structure

俞吉 1周德云 2马云红 3周灿辉3

作者信息

  • 1. 西北工业大学,陕西西安710129
  • 2. 中国电子科技集团公司第二十八研究所,江苏南京210000
  • 折叠

摘要

Abstract

A three-dimensional guidance low based on variable structure has been designed according to the requirement of long-distance navigation,which can lead the attackers to the target with the desired entrance angle self-adaptively.Simulation results show that the attackers can approach the targets quickly even if the targets maneuver acutely with the minor normal acceleration and smoothing trajectory,and can keep its tactical advantages at the ending of navigation.

关键词

远距引导/进入角约束/变结构/制导律

Key words

long-distance navigation/ entrance angle constraint / variable structure/ guidance low

分类

航空航天

引用本文复制引用

俞吉,周德云,马云红,周灿辉..进入角约束下的载机变结构远距引导[J].指挥控制与仿真,2013,35(4):108-111,117,5.

基金项目

航空科学基金(20115553021) (20115553021)

指挥控制与仿真

OACSTPCD

1673-3819

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