| 空间飞行器软对接动力学与控制 |
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| 引用本文： | 洪嘉振,石鹏飞.空间飞行器软对接动力学与控制[J].航天控制,1990(2). |
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| 作者姓名： | 洪嘉振 石鹏飞 |
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| 作者单位： | 上海交通大学，上海交通大学 |
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| 摘 要： | 本文提出实现空间飞行器软对接的一种可控的六杆对接装置方案。文中建立了该系统的数学模型,给出了对接口的位置和姿态与控制杆轴向位移的关系,文本还给出一个算例,论证这种软对接方案的可行性。
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| 关 键 词： | 航天器 会合 对接 动力学 动态控制 ~+软对接 |
DYNAMICS AND CONTROL OF SOFT-DOCKING CONCEPT BETWEEN TWO SPACECRAFTS |
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| Hong Jiazhen Shi Pengfei Shanghai Jiao Tong University.DYNAMICS AND CONTROL OF SOFT-DOCKING CONCEPT BETWEEN TWO SPACECRAFTS[J].Aerospace Control,1990(2). |
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| Authors: | Hong Jiazhen Shi Pengfei Shanghai Jiao Tong University |
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| Institution: | Hong Jiazhen Shi Pengfei Shanghai Jiao Tong University |
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| Abstract: | In this paper, a controllable six-rod docking mechamism concept to implement the soft-docking between two spacecrafts is presented, and the mathematical model of the system is established, which gives the relation of position and attitude of docking port to axial displacements of controlled rods. Finally, a calculated example is given to demonstrate feasibility of the soft-docking concept. |
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| Keywords: | Spacecraft Rendezvous Docking Dynamics Dynamic control ~+Soft docking |
| 本文献已被 CNKI 等数据库收录！ |
