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] |
|
|
|
本文已被:浏览 6825次 下载 5887次 |
共面编队飞行卫星星座的控制 |
文援兰1, 宋以胜2, 文景3 |
(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)
|
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: |
|
The Control of the Satellites Coplanar Formation Flying |
WEN Yuanlan1, SONG Yisheng2, WEN Jing3 |
(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)
|
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 |
|
|
|
|
|