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跳伞着陆冲击的多体系统仿真分析方法
引用本文:张俊,徐元铭,安瑞卿.跳伞着陆冲击的多体系统仿真分析方法[J].航空计算技术,2006,36(6):50-53,58.
作者姓名:张俊  徐元铭  安瑞卿
作者单位:1. 北京航空航天大学,航空科学与工程学院,北京,100083
2. 空军航空医学研究所,北京,100036
摘    要:探讨跳伞着陆冲击过程中人体模型的多刚体系统动力学建模方法,介绍多刚体系统理论中Kane方法的基本原理,用Kane方法建立跳伞着陆冲击的二维人体模型,模拟人体在跳伞着陆冲击载荷作用下的运动学特征,计算出人体各段承受的着陆冲击力,并与相关试验结果进行比较,论证了Kane方法用于跳伞着陆冲击仿真分析的可行性.

关 键 词:多刚体系统动力学  Kane方法  人体模型  跳伞着陆冲击
文章编号:1671-654X(2006)06-0050-04
修稿时间:2006年7月3日

Two-dimension Human Body Dynamics Model of Parachuting landing Impact Based on Kane Method
ZHANG Jun,XU Yuan-ming,AN Rui-qing.Two-dimension Human Body Dynamics Model of Parachuting landing Impact Based on Kane Method[J].Aeronautical Computer Technique,2006,36(6):50-53,58.
Authors:ZHANG Jun  XU Yuan-ming  AN Rui-qing
Abstract:A multi-rigid body dynamic modeling of human body in parachuting landing is studied in this paper.The Kane method is applied to build a two-dimensional human body dynamics model in parachuting landing impact phase.The simulation of kinetic features of human body under the impact load during the parachuting landing is performed by Matlab.The landing impact forces of body segments is then computed and the results are compared with the experiment data.The feasibility of such Kane-based method for impact simulation of parachuting landing is evaluated according to the results and modeling.
Keywords:multi-rigid system dynamics  Kane-Method  human body model  parachuting landing impact
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