| 空间交会最终平移段控制策略 |
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| 引用本文： | 朱仁璋,尹艳,汤溢.空间交会最终平移段控制策略[J].中国空间科学技术,2005,25(4):31-38. |
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| 作者姓名： | 朱仁璋 尹艳 汤溢 |
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| 作者单位： | 1. 北京航空航天大学,北京,100083
2. 中国空间技术研究院,北京,100086 |
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| 摘 要： | 提出空间交会最终平移段的控制方法，选取追踪航天器的相对位置与姿态角作为控制变量，同步控制追踪航天器的质心运动与姿态运动，修正制导机动执行偏差的影响，使目标航天器保持在光学导航视场范围之内，且满足对接操作对追踪航天器状态的要求。
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| 关 键 词： | 最终平移段 交会敏感器 控制 航天器 控制策略 空间交会 平移 目标航天器 控制变量 相对位置 |
| 收稿时间： | 2004-05-24 |
| 修稿时间： | 2004-05-242004-09-07 |
The Control Strategy for the Final Translation of Space Rendezvous |
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| Zhu Renzhang,Yin Yan,Tang Yi.The Control Strategy for the Final Translation of Space Rendezvous[J].Chinese Space Science and Technology,2005,25(4):31-38. |
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| Authors: | Zhu Renzhang Yin Yan Tang Yi |
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| Abstract: | The control strategy for the final translation of space rendezvous is investigated in this paper. A main aim is keeping the target vehicle in the view field of RLS. The attitude angle and the relative position coordinations of the chaser are taken as controlled variables. The lateral boundary is set according to the limited value of the azimuth angle and elevation angle of the target as well as the attitude of the chaser. The velocity increments of control maneuvers are divided into several levels. |
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| Keywords: | Final approach Rendezvous Sensor Control Spacecraft |
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