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弹箭与制导学报 >

2010 , Vol. 30 >Issue 5: 76 - 78

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.05.030

导弹与制导技术

箱式倾斜发射导弹发射扰动研究

  • 赵军民 ,
  • 胡国怀 ,
  • 王琨 ,
  • 潘瑛
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  • 中国兵器工业第203研究所,西安 710065

赵军民(1980-),男,陕西合阳人,工程师,硕士,研究方向:武器系统总体设计及优化、弹道仿真及性能分析。

收稿日期: 2009-08-17

  网络出版日期: 2025-05-28

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The Study on Initial Disturbance of the Slant-launched Missile

  • ZHAO Junmin ,
  • HU Guohuai ,
  • WANG Kun ,
  • PAN Ying
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  • No.203 Research Institute of China Ordanance Industries, Xi'an 710065, China

Received date: 2009-08-17

  Online published: 2025-05-28

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摘要

通过对箱式倾斜发射导弹在发射过程中的受力分析,建立了导弹在半约束运动状态下的发射扰动数学模型,通过Matlab/Simulink进行了数学仿真,仿真结果与实弹飞行测试结果一致,验证了所建立的初始扰动数学模型的正确性与实用性。

关键词： 导弹发射; 半约束; 初始扰动; Matlab/Simulink

本文引用格式

赵军民 , 胡国怀 , 王琨 , 潘瑛 . 箱式倾斜发射导弹发射扰动研究[J]. 弹箭与制导学报, 2010 , 30(5) : 76 -78 . DOI: 10.15892/j.cnki.djzdxb.2010.05.030

Abstract

In this paper, the forces that act on the slant-launch missile during its launch course were analyzed. The model of launch disturbance of missile was established under a half-restriction state. The mathematical simulation was processed using the Matlab/ Simulink toolbox, the result of simulation was accordant with that of live round flight test. The correctness and the practicality of the mathematical model of initial disturbance were validated.

Key words： missile launch; half-restriction; initial disturbance; Matlab/Simulink

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参考文献

[1]
李喜仁. 防空导弹发射装置[M]. 北京: 宇航出版社, 1993.
[2]
薛明旭. 战术导弹发射动力学与仿真[D]. 西安: 西北工业大学, 2004.
[3]
雒朝喜, 焦勇, 董剑. 基于 MATLAB/Simulink 的反坦克导弹系统数字仿真方法研究[J]. 弹箭与制导学报, 2008, 28 (4): 4- 6.
[4]
薛定语, 陈阳泉. 基于MATLAB/Simulink 的系统仿真技术与应用[M]. 北京: 北京清华大学出版社, 2002.
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