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导弹与制导技术

目标机动导致导弹脱靶判别建模与仿真

  • 陈战辉 ,
  • 吴达 ,
  • 刘力 ,
  • 杨永刚
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  • 1 空军工程大学防空反导学院, 陕西三原 713800
    2 中国飞行试验研究院飞行仿真实验室, 西安 710089

陈战辉(1977-),男,陕西武功人,讲师,博士研究生,研究方向:导弹工程和飞行器设计。

收稿日期: 2012-04-13

  网络出版日期: 2025-05-29

基金资助

航空科学基金(20101396008)

The Modeling and Distinguishing Simulation on Target's Maneuver Arose Undershoot of the Missile

  • CHEN Zhanhui ,
  • WU Da ,
  • LIU Li ,
  • YANG Yonggang
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  • 1 The Air Defense and Anti-bullistic Missile Institute, Air Force Engineering University, Shaanxi Sanyuan 713800, China
    2 Flight Simulation Lab of China Flight Test Establishment, Xi'an 710089, China

Received date: 2012-04-13

  Online published: 2025-05-29

摘要

针对目标机动能否逃脱导弹攻击的判断问题,根据比例导引法弹目相对运动方程组分析了目标机动逃脱导弹攻击的条件,推导了目标法向过载与导弹最大需用过载间的关系,建立了目标机动导致比例导引导弹脱靶判别的数学模型,运用该模型对算例进行了仿真与分析,仿真结果符合机动逃脱的运动学一般规律,说明该模型可以用于对抗仿真系统中飞机能否机动逃脱的判据。

本文引用格式

陈战辉 , 吴达 , 刘力 , 杨永刚 . 目标机动导致导弹脱靶判别建模与仿真[J]. 弹箭与制导学报, 2012 , 32(6) : 1 -2,6 . DOI: 10.15892/j.cnki.djzdxb.2012.06.022

Abstract

In view of the issue of whether target maneuver can survive missile attack, according to the movement equation set of the proportional guidance missile, the conditions of target maneuver surviving missile attack was analyzed. The relations between the normal overload of the target and the maximal requisite overload of the missile were deduced, and the model of the missdistance was given. Based on the analysis of the simulation results, the model could be used in counterwork simulation of the battle plane and the missile.

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参考文献

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钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2008: 102- 113.
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