| 对接机构动力学仿真 |
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| 引用本文： | 时军委,徐峰,胡雪平,肖余之.对接机构动力学仿真[J].上海航天,2011,28(6):17-22,48. |
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| 作者姓名： | 时军委 徐峰 胡雪平 肖余之 |
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| 作者单位： | 1. 上海交通大学机械与动力工程学院,上海,200240
2. 上海市空间飞行器机构重点实验室,上海,201108 |
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| 基金项目： | 上海科学技术委员会资助项目(06DZ22105) |
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| 摘 要： | 以神舟飞船的对接机构为研究对象，介绍了不同研制阶段仿真的任务规划，给出了研究中的对接机构仿真分析的捕获缓冲参数设计、数字样机、对接过程动力学仿真评估、试验验证与模型修正，以及对接动力学试验等。
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| 关 键 词： | 对接机构 动力学仿真 虚拟样机 试验 |
Docking Mechanism Dynamic Simulation |
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| SHI Jun-wei,XU Feng,HU Xue-ping,XIAO Yu-zhi.Docking Mechanism Dynamic Simulation[J].Aerospace Shanghai,2011,28(6):17-22,48. |
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| Authors: | SHI Jun-wei XU Feng HU Xue-ping XIAO Yu-zhi |
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| Institution: | SHI Jun-wei1,2,XU Feng2,HU Xue-ping2,XIAO Yu-zhi2(1.School of Mechanical Engineering,Shanghai Jiao Tong University,Shanghai 200240,China,2.Shanghai Key Laboratory of Spacecraft Mechanism,Shanghai 201108,China) |
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| Abstract: | The mission planning during various research phase was given out while the docking mechanism of Shenzhou spaceship was served as the research target in this paper.The capture and cushion parameter design,digital virtual prototype,verification of docking dynamic simulation,testing and model modification,and docking dynamics test were presented. |
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| Keywords: | Docking mechanism Dynamic simulation Virtual prototype Test |
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