The Research of Bi-elliptic Flyaround Maneuver

摘要：

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.

作者: Zhao hui Li Xinglong Yang Baoqing

作者单位: Control and Simulation Center,School of Astronautics,Harbin Institute of Technology Harbin 150080,China

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 265-269

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）