| 引用本文: | 张玉锟,戴金海,王石,等.基于Hill方程的编队卫星群运动分析与轨道设计.[J].国防科技大学学报,2000,22(6):1-5.[点击复制] |
| ZHANG Yukun,DAI Jinhai,WANG Shi,et al.Motion Analysis and Orbit Design of Formation Flying Satellites Based on Hill-Equation[J].Journal of National University of Defense Technology,2000,22(6):1-5[点击复制] |
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| 基于Hill方程的编队卫星群运动分析与轨道设计 |
| 张玉锟, 戴金海, 王石, 任萱 |
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(国防科技大学 航天与材料工程学院, 湖南 长沙 410073)
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| 摘要: |
| 从Hill方程出发，研究了绕飞轨道的性质及编队卫星群的轨道设计方法。从三方面对绕飞轨道进行了描述：坐标平面投影，与坐标平面的夹角，绕飞轨道根数。编队卫星群的轨道设计分两步进行：先求基本环绕卫星的轨道根数；再求其它环绕卫星的轨道根数。仿真结果表明，此方法适用于编队飞行的初步设计。 |
| 关键词: Hill方程 编队卫星群 绕飞轨道 轨道设计 |
| DOI： |
| 投稿日期：2000-05-15 |
| 基金项目:国家863基金资助项目(863-2-5-2.4) |
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| Motion Analysis and Orbit Design of Formation Flying Satellites Based on Hill-Equation |
| ZHANG Yukun, DAI Jinhai, WANG Shi, REN Xun |
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(College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China)
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| Abstract: |
| In this paper, based on the Hill-equation, the property of the flying-around orbit and the orbit design method of formation flying satellites are studied. The flying-around orbit is described in three respects: the coordinate-plane projection, the angle with the coordinate-plane, flying-around orbit elements. The orbit design of formation flying satellites is done in two steps: first the basic surrounding satellite, then the other surrounding satellites. Numerical results show that this method is suitable for the preliminary design of formation flying. |
| Keywords: Hill-equation formation flying satellites flying-around orbit orbit design |
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