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运载火箭多体系统动力学发展及应用
引用本文:石玉红,张宏剑,季宝锋,李雄魁,王辰. 运载火箭多体系统动力学发展及应用[J]. 导弹与航天运载技术, 2017, 0(5). DOI: 10.7654/j.issn.1004-7182.20170503
作者姓名:石玉红  张宏剑  季宝锋  李雄魁  王辰
作者单位:北京宇航系统工程研究所,北京,100076
基金项目:国家自然科学基金项目,中国科协青年人才托举工程
摘    要:从工程实际角度,对运载火箭中的相关多体系统动力学问题进行分析与思考,提出运载火箭研制过程中多体系统动力学学科发展的重要性,并指出多体系统动力学在运载火箭研制方面后续需发展的若干方向,诸如贮箱晃动、分离装置、关节类机构等。建议结合运载火箭大过载、多相耦合的特点,开展针对模型高阶、强非线性相关动力学研究与工程软件研发。

关 键 词:运载火箭  多体系统动力学  非光滑动力学

Development and Application of Multibody System Dynamics in Launch Vehicle
Shi Yu-hong,Zhang Hong-jian,Ji Bao-feng,Li Xiong-kui,Wang Chen. Development and Application of Multibody System Dynamics in Launch Vehicle[J]. Missiles and Space Vehicles, 2017, 0(5). DOI: 10.7654/j.issn.1004-7182.20170503
Authors:Shi Yu-hong  Zhang Hong-jian  Ji Bao-feng  Li Xiong-kui  Wang Chen
Abstract:From the view of engineering practice, this paper concerns the multibody system dynamics in launch vehicle, emphasizes its importance and points out some development directions in this field.,providing some reference to the engineering of launch vehicle,such as tank shaking, separation devices and joint mechanism. It is proposed to combince the characteristics of the launch vehicle's overload and multi-phase coupling to carry out high-order, strong nonlinear dynamics research and engineering software development.
Keywords:Launch vehicle  Multibody system dynamics  Non-smooth dynamics
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