| 引用本文: | 文援兰,宋以胜,文景.共面编队飞行卫星星座的控制.[J].国防科技大学学报,2004,26(3):24-28.[点击复制] |
| WEN Yuanlan,SONG Yisheng,WEN Jing.The Control of the Satellites Coplanar Formation Flying[J].Journal of National University of Defense Technology,2004,26(3):24-28[点击复制] |
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| 共面编队飞行卫星星座的控制 |
| 文援兰1, 宋以胜2, 文景3 |
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(1.国防科技大学 航天与材料工程学院，湖南 长沙 410073;2.解放军理工大学 工程兵工程学院，江苏 南京 210007;3.株洲工学院，湖南 株洲 412008)
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| 摘要: |
| 共面编队飞行的卫星星座的相对运动轨迹是一个椭圆，但卫星由于受摄动力的影响，其椭圆队形会发生变化。提出了一个简单而又节约燃料的队形保持控制方案，即在Hill轨道坐标系中，通过测量x轴和z轴，利用小推力喷气发动机进行控制，消除椭圆中心的相位漂移和各卫星轨道的不共面。 |
| 关键词: 共面编队飞行 星座 轨道控制 |
| DOI： |
| 投稿日期：2003-10-30 |
| 基金项目: |
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| The Control of the Satellites Coplanar Formation Flying |
| WEN Yuanlan1, SONG Yisheng2, WEN Jing3 |
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(1.College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;2.PLA Univ. of Science and Technology, Nanjing 210007，China;3.Zhuzhou Institute of Technology, Zhuzhou 412008, China)
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| Abstract: |
| The figure of the relative kinematical track of the formation flying will change which is in an ellipse because of the disturbing force from which the satellitessuffer. A simple way of control is developed that saves the fuel, that is, in Hill orbital coordinates, through themeasurement of x-axis and z-axis, the control of the small jet engine will eliminate the phase excursion of the center of the ellipse and the non-coplanarity of the orbit of satellites. |
| Keywords: satellites formation flying constellations orbital control |
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