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Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 2: 96 - 100

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.02.021

Research on the Attack Range of the Boost Glide Hypersonic Missile Dive Phase

  • WANG Shaoping 1 ,
  • DONG Shouquan 1 ,
  • CHAO Yulong 2 ,
  • WANG Ze 3
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  • 1 Department of Missile and Shipborne Gun,Dalian Naval Academy,Liaoning Dalian 116018,China
  • 2 No.92896 Unit,Liaoning Dalian 116000,China
  • 3 No.91614 Unit,Liaoning Dalian 116000,China

Received date: 2020-04-28

  Online published: 2025-02-25

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Abstract

As the guidance part of the boost glide hypersonic missile, dive phase attack range directly determines the mission and typical target of the missile. Based on the three degree of freedom trajectory simulation model of the dive phase and an optimal guidance law model satisfying the fall angle constraint, an analysis model of the impact of some factors, such as the dive phase starting height on the boost glide hypersonic missile attack range is established, and the impact of various factors on the missile attack range is analyzed by trajectory translation method. Through simulation analysis, the influence of various factors on the missile attack range is obtained, and it will provide theoretical and methodological guidance for trajectory design of the dive phase and operational capability assessment.

Key words： hypersonic missile; the dive phase; guidance law; attack range

Cite this article

WANG Shaoping , DONG Shouquan , CHAO Yulong , WANG Ze . Research on the Attack Range of the Boost Glide Hypersonic Missile Dive Phase[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(2) : 96 -100 . DOI: 10.15892/j.cnki.djzdxb.2021.02.021

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