摘要
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。
The paper makes a research on energy optimization double-pulse formation reconfiguration on the basis of Hill equation, obtaining the relation between double pulse energy and round satellite＇s initial and final phase gap. 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 for space circle formation reconfiguration.
出处
《装备指挥技术学院学报》
2007年第6期55-58,共4页
Journal of the Academy of Equipment Command & Technology
关键词
空间圆编队
构型调整
二次冲量法
space circle formation
formation reconfiguration
double-pulse method
