Spacecraft Orbit Determination and Its Control Strategy

Haiyan Xuan, Leibo Song, Peiliang Hao, Hang Ji, Xianwei Li
2015 Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials   unpublished
In this paper, we got the aircraft soft landing trajectory model based on the dynamic model, at the same time, regard saving energy and reducing the economic costs as the main purpose, respectively, we gave the corresponding optimal control strategy for each orbit phase.
doi:10.2991/icimm-15.2015.266 fatcat:4dzuc2kybrcnpl6jym5pqo46dm