| 星/箭耦合动态响应分析新方法研究 |
| |
| 引用本文： | 邱吉宝,张正平,李海波,韩丽,黄波.星/箭耦合动态响应分析新方法研究[J].强度与环境,2011,38(3):1-9. |
| |
| 作者姓名： | 邱吉宝 张正平 李海波 韩丽 黄波 |
| |
| 作者单位： | 北京强度环境研究所可靠性与环境工程技术重点实验室,北京,100076 |
| |
| 摘 要： | 介绍了采用约束边界模态展开表达式进行星/箭耦合响应分析的方法,导出缩聚在星/箭连接界面处的全箭动力学方程.应用这种方法通过解析推导可以将整个星/箭耦合结构多自由度方程减缩为仅含星/箭连接界面处自由度的方程,形成星/箭耦合响应分析新方法,内部自由度的影响化为固定界面模态有效质量的贡献,它们的贡献累加于界面自由度之上,使动...
|
| 关 键 词： | 星/箭耦合动力学方程 子结构综合 响应分析 模态综合 |
A study of dynamic response analysis new method for coupled satellite/launch vehicle |
| |
| Qiu Jibao,Zhang Zhengping,Li Haibo,Han Li,Huang Bo.A study of dynamic response analysis new method for coupled satellite/launch vehicle[J].Structure & Environment Engineering,2011,38(3):1-9. |
| |
| Authors: | Qiu Jibao Zhang Zhengping Li Haibo Han Li Huang Bo |
| |
| Institution: | Qiu Jibao Zhang Zhengping Li Haibo Han Li Huang Bo(Science and Technology on Reliability and Environment Engineering Laboratory Beijing Institute of Structure and Environment Engineering,Beijing 100076,China) |
| |
| Abstract: | Satellite/launch vehicle coupling response analysis method using expansion expressions with constrained boundary modes is introduced in this paper.Dynamic equation of launch vehicle which condensed in the connection interface of satellite/launch vehicle is derived.Using the method,the equation with multi-DOF of coupled satellite/launch vehicle system can be reduced to an equation involves only DOF from connection interface of satellite/launch vehicle.Subsequently,lead to a new simplified method for coupling... |
| |
| Keywords: | dynamic equation of the coupled satellite/launch vehicle response analysis substructure synthesis mode synthesis |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
