Title :
The research of bi-elliptic flyaround maneuver
Author :
Hui, Zhao ; Xinglong, Li ; Baoqing, Yang
Author_Institution :
Control & Simulation Center, Harbin Inst. of Technol., Harbin, China
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.
Keywords :
aerospace control; force control; Hill´s equation; bielliptic flyaround formation; coplanar bielliptic flyaround maneuver; future space activities; impulsive thrust control; Aerospace electronics; Equations; Mathematical model; Orbits; Satellites; Simulation; Space vehicles;
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
DOI :
10.1109/ISSCAA.2010.5632537
