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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 6: 136 - 139

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.06.048

BALLISIC AND AIRDYNAMICS

The Research on Pulse Parameter Optimization of Terminal Trajectory Correction Projectile Based on Orthogonal Experimental Design Method

  • CAO Yingjun ,
  • FENG Wubin ,
  • BI Xiaomeng ,
  • JI Xiaogang
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  • 1 Beijing Special Vehicle Institute, Beijing 100072, China
    2 Xi'an Military Representatives Bureau of General Armaments Department, Xi'an 710032, China
    3 Military Representatives Office of Army Aviation Division in Xi'an Area, Xi' an 710032, China

Received date: 2012-03-03

  Online published: 2025-05-29

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Abstract

In the case of invariable whole pulse energy, the main pulse parameters including starting control time, pulse number, minimum igniting internal and igniting pulse threshold which affect terminal trajectory correction projectile impact point correction were analyzed in detail. The muti-factor and muti-level combination pulse parameter optimization was studied by using orthogonal experimental design method as mathematics tool. The numerical simulation indicates that the research on pulse parameter optimization of terminal trajectory correction projectile based on orthogonal experimental design method is feasible.

Key words： terminal trajectory correction projectile; pulse parameters; optimization; orthogonal experimental design

Cite this article

CAO Yingjun , FENG Wubin , BI Xiaomeng , JI Xiaogang . The Research on Pulse Parameter Optimization of Terminal Trajectory Correction Projectile Based on Orthogonal Experimental Design Method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(6) : 136 -139 . DOI: 10.15892/j.cnki.djzdxb.2012.06.048

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