Research on Attitude Algorithm of Aircraft Based on Quaternion
- 10.2991/acaai-18.2018.46How to use a DOI?
- quaternion; coordinate system; attitude angle
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.
- © 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 - 10.2991/acaai-18.2018.46 ID - Chen2018/03 ER -