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弹箭与制导学报 >

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

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

导弹与制导技术

车载导弹多体发射动力学仿真研究

  • 高星斗 ,
  • 毕世华 ,
  • 陈阵
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  • 北京理工大学宇航学院,北京 100081

高星斗(1984-),男,江西人,博士研究生,研究方向:发射动力学。

收稿日期: 2010-08-23

  网络出版日期: 2025-05-28

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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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摘要

为研究车载导弹倾斜发射过程中动力学响应,利用三维建模软件Pro/E将模型导入ADAMS,建立了车载导弹的多体系统发射动力学模型。对不同工况下的发射过程进行动力学分析,获取了导弹发射阶段发射箱口的振动参量(位移)和姿态参数。仿真结果表明,文中提出的多体动力学模型及仿真方法是可行的。

关键词： 车载导弹; 发射系统; 拉格朗日方程; 多体动力学; 仿真

本文引用格式

高星斗 , 毕世华 , 陈阵 . 车载导弹多体发射动力学仿真研究[J]. 弹箭与制导学报, 2010 , 30(6) : 60 -62,69 . DOI: 10.15892/j.cnki.djzdxb.2010.06.038

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

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参考文献

[1]
柴旭东, 李伯虎, 熊光楞,等. 高层体系结构系统实施技术的初步实践与进一步研究[J]. 系统仿真学报, 2002, 14 (2): 152- 155.
[2]
管红根. 车载炮发射动力学仿真研究[J]. 兵工学报, 2005, 26 (1): 53- 55.
[3]
Timothy J McCoy. Wind turbine ADAMS model linearization including rotational and aerodynamic effects[R]. AIAA 2004-1370, 2004.
[4]
Ahn Kil-Young. A modeling of impact dynamics and its application to impact force prediction[J]. Journal of Mechanical Science and Technology, 2004, 19 (1): 422- 428.
[5]
姚昌仁, 张波. 火箭导弹发射装置设计[M]. 北京: 北京理工大学出版社, 1998: 105- 109.
[6]
陆佑方. 汽车柔性多体系统动力学建模综述[J]. 汽车技术, 1997 (5): 1- 7.
[7]
袁士杰, 吕哲勤. 多刚体系统动力学[M]. 北京: 北京理工大学出版社, 1992: 147- 158.
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