首页 | 官方网站   微博 | 高级检索  
     

物伞系统动力特性研究
引用本文:程文科,杨小伟,秦子增,张晓今.物伞系统动力特性研究[J].国防科技大学学报,1998,20(4):27-30.
作者姓名:程文科  杨小伟  秦子增  张晓今
作者单位:国防科技大学航天技术系
摘    要:研究了降落伞一物体系统的空间运动。假定降落伞和物体都有6个自由度,两者通过吊带连接起来。推导了物伞系统运动的非线性微分方程,运动方程中没有考虑伞绳和吊带的弹性。用所得数学模型分析了减速伞回收系统的动力特性,给出了仿真计算结果。

关 键 词:降落伞系统,动力学,附加质量
收稿时间:1997/9/29 0:00:00

Analysis of the Dynamic Performance of a Parachute and Payload System
Cheng Wenke,Yang Xiaowei,Qin Zizeng and Zhang Xiaojin.Analysis of the Dynamic Performance of a Parachute and Payload System[J].Journal of National University of Defense Technology,1998,20(4):27-30.
Authors:Cheng Wenke  Yang Xiaowei  Qin Zizeng and Zhang Xiaojin
Affiliation:Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073
Abstract:The three-dimension motion of a parachute and payload system is studied. Both the parachute and payload are assumed to have six degrees of freedom. They are coupled by a riser. The nonlinear differential equations of motion for a parachute-payload system are developed, which model the parachute suspension lines and the riser as inelastic elements. The resulting math model is then applied to analyze the dynamic performance of a drogue parachute recovery system. The simulation results are presented.
Keywords:parachute system  dynamics  added mass  
本文献已被 CNKI 等数据库收录!
点击此处可从《国防科技大学学报》浏览原始摘要信息
点击此处可从《国防科技大学学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司    京ICP备09084417号-23

京公网安备 11010802026262号