@inproceedings{6a88fd0057ae4996b93eef3b45dcf890,
title = "Trajectory planning and control for satellite formation flying maneuver of leaving and joining",
abstract = "With the constraint of collision avoidance, trajectory planning and control for satellite formation flying is presented by which fault satellite leaves the formation and backup satellite joins the formation. For saving the fuel and avoiding collision, the start time of maneuver must be selected carefully. Then sun synchronization orbit satellite formation is simulated. The result of simulation demonstrates validity of control scheme.",
author = "Sun Dong and Zhou Fengqi and Zhou Jun",
year = "2003",
language = "英语",
isbn = "9781563479786",
series = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
booktitle = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
note = "AIAA Guidance, Navigation, and Control Conference and Exhibit 2003 ; Conference date: 11-08-2003 Through 14-08-2003",
}