Optimal Low-Thrust Trajectory Design and Robust Tracking Control for Spacecraft Rendezvous

摘要：

　　In this work,a low-thrust,fixed time,fuel-optimal constrained terminal approach direction rendezvous strategy is presented for spacecraft near elliptic orbit accounting for nonlinear differential gravity.There are two aspects in the approach presented: generating a optimal trajectory and tracing that trajectory.

关键词： Spacecraft Rendezvous Energy Minimization Trajectory Robust Tracking Control

作者: ZHANG Song HOU Mingshan WANG Dong ZHOU Tao

作者单位: School of Automation, Northwestern Polytechnical University, Xi’an 710029, China

会议类型: 国际会议

会议名称: the 32nd Chinese Control Conference(第三十二届中国控制会议)

会议地点: 西安

会议语种:英文

页码: 4885-4888

在线出版日期: 2013-07-01（万方平台首次上网日期，不代表论文的发表时间）