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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 6: 1 - 2,6

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.06.022

MISSILES AND GUIDANCE TECHNOLOGY

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

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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.

Key words： target maneuver; proportional guidance; missdistance determination; modeling

Cite this article

CHEN Zhanhui , WU Da , LIU Li , YANG Yonggang . The Modeling and Distinguishing Simulation on Target's Maneuver Arose Undershoot of the Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(6) : 1 -2,6 . DOI: 10.15892/j.cnki.djzdxb.2012.06.022

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