Proceedings of the 2016 International Conference on Artificial Intelligence and Engineering Applications

Attitude Control Method of Spin-Stabilized Satellite Base on Equiangular Precession

Authors
Yonggang Li, Jiping Ren, Libing Guo, Wen Mao, Yi Wang
Corresponding Author
Yonggang Li
Available Online November 2016.
DOI
https://doi.org/10.2991/aiea-16.2016.55How to use a DOI?
Keywords
Spin-stabilized Satellite; Attitude Control; Equiangular Precession; Theory Executing Angular; Executing Times.
Abstract

Attitude control is a basic task of a spin-stabilized satellite control. There are many kinds of attitude control methods, this paper does research for equiangular precession method. The paper first introduced the basic principle of equiangular precession method, and then gave out a detailed calculation method of attitude control quantity, which included theory executing angular, executing times and time delay, finally attitude maneuver process were simulated. The simulation result shows that the computed result of attitude control quantity is correct, the forecasts for control process are essentially the same as practice. The method has been applied to satellite launch mission.

Copyright
© 2016, 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 2016 International Conference on Artificial Intelligence and Engineering Applications
Series
Advances in Computer Science Research
Publication Date
November 2016
ISBN
978-94-6252-270-1
ISSN
2352-538X
DOI
https://doi.org/10.2991/aiea-16.2016.55How to use a DOI?
Copyright
© 2016, 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  - Yonggang Li
AU  - Jiping Ren
AU  - Libing Guo
AU  - Wen Mao
AU  - Yi Wang
PY  - 2016/11
DA  - 2016/11
TI  - Attitude Control Method of Spin-Stabilized Satellite Base on Equiangular Precession
BT  - Proceedings of the 2016 International Conference on Artificial Intelligence and Engineering Applications
PB  - Atlantis Press
SP  - 308
EP  - 313
SN  - 2352-538X
UR  - https://doi.org/10.2991/aiea-16.2016.55
DO  - https://doi.org/10.2991/aiea-16.2016.55
ID  - Li2016/11
ER  -