编队飞行队形设计一般化方法

首先 ,在合理的假设条件下 ,基于运动学关系推导了环绕卫星相对参考卫星的相对运动方程 ;然后 ,给出了编队飞行队形设计一般化方法的具体计算公式 ,利用此方法 ,能在参考轨道为圆或椭圆轨道的情况下 ,直接求出编队中所有卫星的轨道参数 ;最后 ,给出了两个编队队形设计的算例

Generalized Method of Formation Flying Configuration Design

At first, based on kinematic relationship, motion equations of surrounding satel lite with respect to reference satellite is deduced under proper assumption. Then, specific formulas of generalized method of microsatellite formation flyin g configuration design are presented. Using this method, orbit elements of a ll the satellites in the formation can be solved directly, on condition that the reference orbit is a circular orbit or an elliptic orbit. At last, two typical examples of formation configuration design are given.