Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials

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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/).

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Volume Title
Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials
Series
Advances in Engineering Research
Publication Date
July 2015
ISBN
978-94-62520-88-2
ISSN
2352-5401
DOI
10.2991/icimm-15.2015.266How to use a DOI?
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

risenwbib
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  -