| 关于探测器定点在共线平动点附近的控制问题 |
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| 引用本文： | 侯锡云,刘林.关于探测器定点在共线平动点附近的控制问题[J].飞行器测控学报,2005,24(6):29-33. |
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| 作者姓名： | 侯锡云 刘林 |
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| 作者单位： | [1]南京大学天文学系,江苏南京210093 [2]南京大学空间环境与航天动力学研究所,江苏南京210093 |
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| 摘 要： | 对探测器定点在共线平动点附近的轨道控制提出了一种小推力方案,针对日-地（月）系的具体背景给出了数值模拟结果,并对其进行了相应的分析.
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| 关 键 词： | 共线平动点 轨道控制 线性反馈 小推力控制 |
| 收稿时间： | 2005-06-29 |
| 修稿时间： | 2005-07-04 |
On Orbit Control of Spacecraft around Collinear Libration Points |
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| HOU Xi-yun, LIU Lin.On Orbit Control of Spacecraft around Collinear Libration Points[J].Journal of Spacecraft TT&C Technology,2005,24(6):29-33. |
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| Authors: | HOU Xi-yun LIU Lin |
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| Institution: | 1. Astronomy Department, Nanjing University, Nanjing, Jiangsu Province 210093; 2. The Institute of Space Environment and Astrodynamics, Nanjing University, Nanjing, Jiangsu Province 210093 |
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| Abstract: | This paper proposes a low-thrust strategy for orbit control of spacecraft around collinear libration points.Numerical simulation results are given by taking the Sun-Earth+Moon System as an example together with an analysis. |
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| Keywords: | Collinear Libration Point Orbit Control Linear Feedback Low-Thrust Control |
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