| 空间交会对接的仿真技术 |
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| 引用本文： | 林来兴.空间交会对接的仿真技术[J].航天控制,1990(4). |
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| 作者姓名： | 林来兴 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 空间交会对接涉及到两个航天器同时要进行多达12个自由度的轨道和姿态控制问题。这不仅在理论上,而且在技术实现上都是相当复杂的。为了确保交会对接的成功并尽量缩短交会对接的时间,必须用实际硬件和星上软件进行整个RVD控制系统的仿真试验。本文主要论述对交会对接仿真技术的要求,仿真方法和关键仿真设备。
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| 关 键 词： | 交会对接 ~+半物理仿真 气浮台 仿真器 |
SIMULATION TECHNOLOGY FOR RENDEZVOUS AND DOCKING IN SPACE |
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| Lin Laixing Beijing Institute of Control Engineering.SIMULATION TECHNOLOGY FOR RENDEZVOUS AND DOCKING IN SPACE[J].Aerospace Control,1990(4). |
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| Authors: | Lin Laixing Beijing Institute of Control Engineering |
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| Institution: | Lin Laixing Beijing Institute of Control Engineering |
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| Abstract: | The rendezvous and docking (RVD) between two spacecrafts in space in-volves both orbit control and attitude control with up to 12 degrees of freedom. It is very com-plex not only in theory but also inimplementation. In order to ensure the success for RVD and minimize the time for RVD, it is necessary f or simulation testing of complete RVD controlsystem with real hardware and onboard software in the loop. This paper primarily discusses the specification of RVD simulation, simulation methodsand critical simulation equipments. |
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| Keywords: | Rendezvous and docking ~+Semi-physical simulation Air-bearing table Simulator |
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