Spacecraft Orbit Determination and Its Control Strategy
Authors
Haiyan Xuan, Leibo Song, Peiliang Hao, Hang Ji, Xianwei Li
Corresponding Author
Haiyan Xuan
Available Online July 2015.
- DOI
- 10.2991/icimm-15.2015.266How to use a DOI?
- Keywords
- Orbit determination; soft landing; dynamics; control strategy.
- Abstract
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.
- Copyright
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Haiyan Xuan AU - Leibo Song AU - Peiliang Hao AU - Hang Ji AU - Xianwei Li PY - 2015/07 DA - 2015/07 TI - Spacecraft Orbit Determination and Its Control Strategy BT - Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials PB - Atlantis Press SP - 1462 EP - 1465 SN - 2352-5401 UR - https://doi.org/10.2991/icimm-15.2015.266 DO - 10.2991/icimm-15.2015.266 ID - Xuan2015/07 ER -