A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2020; you can also visit the original URL.
The file type is application/pdf.
Spacecraft Orbit Determination and Its Control Strategy
2015
Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials
unpublished
Preserved Fulltext
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