基于Hill方程的编队卫星群运动分析与轨道设计

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

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

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.