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对接机构分系统研制
引用本文:陈宝东,郑云青,邵济明,陈萌.对接机构分系统研制[J].上海航天,2011,28(6):1-6.
作者姓名:陈宝东  郑云青  邵济明  陈萌
作者单位:上海宇航系统工程研究所,上海,201108
基金项目:上海市科学技术委员会资助(10XD1422900)
摘    要:介绍了我国神舟八号飞船和天宫一号目标飞行器对接试验的对接机构分系统的组成、控制时序、设计方案,以及可靠性与安全性。给出了对接机构分系统研制中总体设计、动力学仿真、试验和关键部件研制等关键技术,以及整机特性测试、连接分离试验、热真空对接与分离试验、寿命试验等验证情况。回顾了对接机构分系统的研制过程。

关 键 词:神舟八号飞船  天宫一号目标飞行器  对接机构  控制时序  总体设计  动力学仿真  试验  关键部件  试验验证

Development of Docking Subsystem
CHEN Bao-dong,ZHENG Yun-qing,SHAO Ji-ming,CHEN Meng.Development of Docking Subsystem[J].Aerospace Shanghai,2011,28(6):1-6.
Authors:CHEN Bao-dong  ZHENG Yun-qing  SHAO Ji-ming  CHEN Meng
Institution:CHEN Bao-dong,ZHENG Yun-qing,SHAO Ji-ming,CHEN Meng(Aerospace System Engineering Shanghai,Shanghai 201108,China)
Abstract:The composition,control scheduling,design,and reliability and safety of the docking subsystem of China's Shenzhou-8 spaceship and Tiangong-1 target spacecraft were introduced in this paper.The key technologies of the general design,dynamic simulation,test and important part design in the design of the docking subsystem were given out.The tests,such as the general characteristic test,docking and separating test,docking test system in thermal vacuum,and life test,and test results were presented briefly.The wh...
Keywords:shenzhou-8 spaceship  Tiangong-1 target spacecraft  Docking system  Control scheduling  Design  Dynamic simulation  Test  Key component  Experiment verification  
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