The NEAR Optimal Two-Impulse Analytical Solution of On-Orbit-Servicing Spacecraft for Fly-Around Orbit Reconfiguration

摘要：

Focusing the optimal two-impulse transfer for flyaround orbit reconfiguration, an near optimal two-impulse analytical algorithm is presented by the CW Equation and its solution. To avoid the singularity aroused from the normal whole solving method by CW equations, the paper calculates the out-of-plane optimal algorithm and in-plane optimal algorithm respectively in the deduction process and then gathers them to obtain the whole solution. Compared with other traditional solutions, the consumed impulse of the analytical solution is very near with that of numerical solution and what’s more, the consumed time is very little VS other algorithms. Thus, it’s suitable for the onboard application of spacecraft. Finally, a simulation is carried out to validate the optimal algorithm.

作者: Feng WANG Xueqin CHEN Ji-he WANG Xi-bin CAO

作者单位: Research Center of Satellite Technology,Harbin Institute of Technology,China

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 790-795

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）