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Journal of Projectiles, Rockets, Missiles and Guidance >

2018 , Vol. 38 >Issue 1: 165 - 168

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2018.01.038

Simulation and Study on the Dynamics of a Vehicle Missile Launcher

  • LI Min ,
  • WANG Xuezhi ,
  • LI Chao
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  • Air and Missile Defense College, Air force Engineering University, Xi'an 710051, China

Received date: 2017-05-08

  Online published: 2025-05-28

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Abstract

The vibration response of launcher is an important factor that affects the launching accuracy of missile. In this paper, by using ADAMS dynamics simulation software and ANSYS finite element analysis software, the rigid-flexible coupling model based on a missile launcher was established and verified, and the vibration response analysis was carried out. Through the comparison and analysis of the factors affecting the subsidence of launcher, it is concluded that the subsidence can be reduced by increasing the stiffness of the frame and chassis.

Key words： rigid-flexible coupling; vibration response; subsidence

Cite this article

LI Min , WANG Xuezhi , LI Chao . Simulation and Study on the Dynamics of a Vehicle Missile Launcher[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018 , 38(1) : 165 -168 . DOI: 10.15892/j.cnki.djzdxb.2018.01.038

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