基于ADAMS的内装式空射运载火箭分离过程动力学分析*

张久星; 张登成; 朱和铨; 张艳华

doi:10.15892/j.cnki.djzdxb.2011.02.039

弹箭与制导学报 >

2011 , Vol. 31 >Issue 2: 153 - 156

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.02.039

弹道与气动力技术

基于ADAMS的内装式空射运载火箭分离过程动力学分析*

张久星 ,
张登成 ,
朱和铨 ,
张艳华

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空军工程大学工程学院,西安 710038

张久星(1985-),男,河北唐山人,硕士研究生,研究方向:飞行力学和飞行仿真。

收稿日期: 2010-05-22

网络出版日期: 2025-05-30

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Dynamic Analysis of Internally Carried Air-launched Launch Vehicle Separation from Aircraft Based on ADAMS

ZHANG Jiuxing ,
ZHANG Dengcheng ,
ZHU Hequan ,
ZHANG Yanhua

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The Engineering Institute, Air Force Engineering University, Xi'an 710038, China

Received date: 2010-05-22

Online published: 2025-05-30

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摘要

为初步论证内装式空中发射运载火箭总体方案,利用动力学仿真软件ADAMS和实体建模软件Solidworks联合建立了载机、运载火箭、稳定伞等样机的实体模型;对分离过程中三者的受力情况进行了详细分析,并建立了动力学仿真所需要的动力学方程;对样机进行动力学仿真,验证样机建立正确合理,从而为空气动力仿真提供了一种新的方法。

关键词： ADAMS; 动力学仿真; 飞行力学; 空中发射; 运载火箭; 物伞系统

本文引用格式

张久星 , 张登成 , 朱和铨 , 张艳华 . 基于ADAMS的内装式空射运载火箭分离过程动力学分析*[J]. 弹箭与制导学报, 2011 , 31(2) : 153 -156 . DOI: 10.15892/j.cnki.djzdxb.2011.02.039

Abstract

In order to verify the total project of internally carried air-launched launch vehicle, the physical models of the cargo, launch vehicle and parachute based on ADAMS and Solidworks were built. The dynamic equation for the dynamic simulation was built according to the detailed dynamic analysis of the three in the process of separation. The simulation model is proved correctly according to the dynamic simulation; it provides a new reference method for air dynamic simulation.

Key words： ADAMS; dynamic analysis; flight dynamics; air launch; launch vehicle; parachute and payload system

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参考文献

[1]	Marti Sarigul-Klijn,Nesrin Sarigul-Klijn. Trade studies for air launching a small launch vehicle from a cargo aircraft, AIAA 2005-0621[R].2005.
[2]	何民.内装式空射运载火箭初始弹道稳定方法研究[D].西安:西北工业大学,2010.
[3]	张登成,闫杰,张久星.内装式空射运载火箭与载机分离研究[J].弹箭与制导学报,2009,29(5):158-161.
[4]	王利荣.降落伞理论与应用[M].北京:宇航出版社,1997.

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