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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 6: 33 - 36

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.06.017

MISSILES AND GUIDANCE TECHNOLOGY

The Research on Computing Method for Firing Data of Boost-glide Aerocraft

  • LIU Jun ,
  • CHEN Kejun ,
  • XIE Yu ,
  • TANG Guojian
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  • College of Aerospace and Material Engineering, National University. of Defense Technology, Changsha 410073, China

Received date: 2012-03-28

  Online published: 2025-05-29

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Abstract

The computing method for firing data of boost-glide aerocraft was investigated. In the paper, based on analysis of the impact of firing data on aerocraft trajectory, a delamination tactic of computing was proposed. The underdetermined equations of basic firing data of boost-glide aerocraft were divided into several groups of determined equation, then the computing method for basic firing data of boost-glide aerocraft was designed with the Newton iterative algorithm of simulation of target practice. Finally, the feasibility of this approach was proven by an example.

Key words： boost-glide aerocraft; firing data; tactic of computing; Newton iterative; simulation of target practice

Cite this article

LIU Jun , CHEN Kejun , XIE Yu , TANG Guojian . The Research on Computing Method for Firing Data of Boost-glide Aerocraft[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(6) : 33 -36 . DOI: 10.15892/j.cnki.djzdxb.2012.06.017

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