The research of bi-elliptic flyaround maneuver

Zhao Hui, Liu Xinglong, Yang Baoqing
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Abstract

The flyaround maneuvers have a broad application prospects in the future space activities. In this paper, a coplanar bi-elliptic flyaround maneuver by impulsive thrust control is discussed; the necessary conditions of the bi-elliptic flyaround formation are deduced based on the Hill's equation. Simulation results verify the superiority of the bi-elliptic flyaround maneuver compared with the natural flyaround maneuver.
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双椭圆绕飞机动的研究
绕飞机动在未来空间活动中具有广阔的应用前景。讨论了脉冲推力控制下的共面双椭圆绕飞机动问题;在希尔方程的基础上,推导了双椭圆绕飞编队形成的必要条件。仿真结果验证了双椭圆绕飞机动与自然绕飞机动相比的优越性。
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