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弹箭与制导学报 >

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

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

弹道与气动力技术

基于正交试验设计的末修弹脉冲参数优化研究

  • 曹营军 ,
  • 冯武斌 ,
  • 毕晓蒙 ,
  • 纪晓罡
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  • 1 北京特种车辆研究所,北京 100072
    2 总装西安军事代表局,西安 710032
    3 总参陆航驻西安地区军事代表室,西安 710032

曹营军(1972-),男,河北灵寿人,工程师,博士,研究方向:坦克武器论证,飞行器制导与控制。

收稿日期: 2012-03-03

  网络出版日期: 2025-05-29

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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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摘要

在总脉冲量恒定的前提下,对影响末段弹道修正弹落点修正效果的主要脉冲参数(包括启控时间、总脉冲数、最小点火时间间隔、点火阈值)进行了详细分析。以正交试验设计为数学工具,对多因素、多水平组合的脉冲参数优化进行了深入研究。数值仿真表明,基于正交试验设计的末段弹道修正弹脉冲参数优化是可行的。

关键词： 末修弹; 脉冲参数; 优化; 正交试验设计

本文引用格式

曹营军 , 冯武斌 , 毕晓蒙 , 纪晓罡 . 基于正交试验设计的末修弹脉冲参数优化研究[J]. 弹箭与制导学报, 2012 , 32(6) : 136 -139 . DOI: 10.15892/j.cnki.djzdxb.2012.06.048

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

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参考文献

[1]
Thanat Jitpraphai, Bradley Burchett, Mark Costell.A comparision of different guidance schemes for a direct fire Rocket with a pulse jet control mechanism,AIAA - 2001 - 4326[R]. 2001.
[2]
王涛. 脉冲式弹道修正弹的修正方法研究[D]. 南京: 南京理工大学, 2005.
[3]
肖顺旺, 安志勇, 李升才,等. 基于不同导引律的脉冲修正弹广义弹道偏差研究[J]. 弹箭与制导学报, 2010, 30 (2): 205- 207.
[4]
曹营军. 基于脉冲控制的修正弹制导与控制技术研究[D]. 北京: 北京理工大学, 2008.
[5]
余锦华, 杨维权. 多元统计分析与应用[M]. 广州: 中山大学出版社, 2005.
[6]
杨德. 试验设计与分析[M]. 北京: 中国农业出版社, 2002.
[7]
钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学, 2000.
[8]
薛定宇, 陈阳泉. 基于MATLAB/Simulink的系统仿真技术与应用[M]. 北京: 清华大学出版社, 2002.
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