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Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 6: 60 - 62,69

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.06.038

MISSILES AND GUIDANCE TECHNOLOGY

The Simulation Study on Multi-body Launching Dynamics for a Vehicular Missile Launcher

  • GAO Xingdou ,
  • BI Shihua ,
  • CHEN Zhen
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081,China

Received date: 2010-08-23

  Online published: 2025-05-28

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Abstract

In order to study the dynamic response of a vehicular missile launcher during slant launch, the model was introduced into ADAMS by the three-dimensional software Pro/E into; the multi-body system dynamic model of a vehicular missile launcher was built. Dynamic simulation for several launching conditions were conducted, and the vibrational parameter (displacement) of the launching container verge and attitude parameters during launching were eventually acquired. The simulation results show the proposed multi-body dynamic model and simulation method are feasible.

Key words： vehicular missile launcher; launching system; Lagrange equation; multi-body dynamics; simulation

Cite this article

GAO Xingdou , BI Shihua , CHEN Zhen . The Simulation Study on Multi-body Launching Dynamics for a Vehicular Missile Launcher[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(6) : 60 -62,69 . DOI: 10.15892/j.cnki.djzdxb.2010.06.038

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