By fixing the round satellite s initial and final position s phase and resolving the transfer time,the paper educes a method of pursuing optimization between two space circle formations,presents an optimal simulation result of reconfiguration of space circle formation,and gains general rules.
在Hill方程的基础上研究了空间圆编队构型调整能量最省的双冲量法,得出了该方法所需要的能量和过渡时间、绕飞卫星始末相位差之间的关系,由固定绕飞卫星始末位置相位差求解过渡时间引出全局寻优的方法,给出了空间圆编队构型调整最优能量消耗的仿真结果,给出了空间圆编队构型调整的一般性规律。
