基于Hill方程的编队卫星群运动分析与轨道设计  

Motion Analysis and Orbit Design of Formation Flying Satellites Based on Hill-Equation

作　　者：张玉锟[1] 戴金海[1] 王石[1] 任萱[1] 

机构地区：[1]国防科技大学航天与材料工程学院,湖南长沙410073

出　　处：《国防科技大学学报》2000年第6期1-5,共5页Journal of National University of Defense Technology

基　　金：国家 8 6 3基金资助项目!(86 3 2 5 2 4)

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 。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.

关 键 词：HiII方程 编队卫星群 绕飞轨道 轨道设计 运动分析 编队飞行 

分 类 号：V412.41[航空宇航科学与技术—航空宇航推进理论与工程]