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Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 1: 65 - 67,71

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.01.017

MISSILES AND GUIDANCE TECHNOLOGY

Research on Launch Dynamics Modeling and Simulating for Surface-to-air Missile

  • CHEN Jinbao ,
  • ZHANG Xiaojin ,
  • ZHANG Guanfei
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Received date: 2009-07-07

  Online published: 2025-05-19

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Abstract

According to the characteristics of launch model, launch dynamics model was founded, and launch movement equations were deduced for missile of tiltable launch. Different slide lengths and launch obliquities were used to simulate and calculate for straight line slides and triangle slides. Movement parameters and laws of the missile were got. The results show that off-slide movement of missile is related to slide lengths and launch obliquities. In addition, subsidence of missile must be considered for triangle slides.

Key words： tiltable slide; launch dynamics; off-slide movement; simulation

Cite this article

CHEN Jinbao , ZHANG Xiaojin , ZHANG Guanfei . Research on Launch Dynamics Modeling and Simulating for Surface-to-air Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(1) : 65 -67,71 . DOI: 10.15892/j.cnki.djzdxb.2010.01.017

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References

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曾颖超, 陆毓峰, 霍秀芳. 战术导弹弹道与姿态动力学[M]. 西安: 西北工业大学出版社, 1991.
[2]
张志涌. 精通 MATLAB6.5 版[M]. 北京: 北京航空航天大学出版社, 2003.
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