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Journal of Projectiles, Rockets, Missiles and Guidance >

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

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

MISSILES AND GUIDANCE TECHNOLOGY

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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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

Cite this article

ZHAO Junmin , HU Guohuai , WANG Kun , PAN Ying . The Study on Initial Disturbance of the Slant-launched Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(5) : 76 -78 . DOI: 10.15892/j.cnki.djzdxb.2010.05.030

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