Proceedings of the 2018 International Conference on Advanced Control, Automation and Artificial Intelligence (ACAAI 2018)

Research on Attitude Algorithm of Aircraft Based on Quaternion

Authors
Junru Chen
Corresponding Author
Junru Chen
Available Online March 2018.
DOI
https://doi.org/10.2991/acaai-18.2018.46How to use a DOI?
Keywords
quaternion; coordinate system; attitude angle
Abstract

In this paper, the quaternion method is used to get the accurate aircraft attitude. It is introduced coordinate system and attitude angle establishment, attitude angle acquisition and data fusion algorithm in detail. Experiments show that the algorithm effectively suppresses the gyroscope deviation and improves the accuracy of the attitude angle.

Copyright
© 2018, 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 2018 International Conference on Advanced Control, Automation and Artificial Intelligence (ACAAI 2018)
Series
Advances in Intelligent Systems Research
Publication Date
March 2018
ISBN
978-94-6252-483-5
ISSN
1951-6851
DOI
https://doi.org/10.2991/acaai-18.2018.46How to use a DOI?
Copyright
© 2018, 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  - Junru Chen
PY  - 2018/03
DA  - 2018/03
TI  - Research on Attitude Algorithm of Aircraft Based on Quaternion
BT  - Proceedings of the 2018 International Conference on Advanced Control, Automation and Artificial Intelligence (ACAAI 2018)
PB  - Atlantis Press
SP  - 196
EP  - 199
SN  - 1951-6851
UR  - https://doi.org/10.2991/acaai-18.2018.46
DO  - https://doi.org/10.2991/acaai-18.2018.46
ID  - Chen2018/03
ER  -