Proceedings of the 2017 2nd International Conference on Control, Automation and Artificial Intelligence (CAAI 2017)

Adaptive Fault Tolerant Control of UAV Attitude Control System

Authors
Hangzhou Zhao, Xu Yong, Yunqi Zhang, Yuhao Ding
Corresponding Author
Hangzhou Zhao
Available Online June 2017.
DOI
https://doi.org/10.2991/caai-17.2017.14How to use a DOI?
Keywords
UAV; state feedback; error adjustment; adaptive fault tolerant control
Abstract
In this paper, we design a direct feedback adaptive fault-tolerant controller to cope with the uncertainty and non-modeling of the interference of the four-rotor UAV attitude control system. The controller is stuck in the UAV and the external. Under the condition of uncertainty, the attitude of the UAV can effectively track the state output of the reference system by introducing the feedback of the state and its error.
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Proceedings
2017 2nd International Conference on Control, Automation and Artificial Intelligence (CAAI 2017)
Part of series
Advances in Intelligent Systems Research
Publication Date
June 2017
ISBN
978-94-6252-360-9
ISSN
1951-6851
DOI
https://doi.org/10.2991/caai-17.2017.14How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Hangzhou Zhao
AU  - Xu Yong
AU  - Yunqi Zhang
AU  - Yuhao Ding
PY  - 2017/06
DA  - 2017/06
TI  - Adaptive Fault Tolerant Control of UAV Attitude Control System
BT  - 2017 2nd International Conference on Control, Automation and Artificial Intelligence (CAAI 2017)
PB  - Atlantis Press
SP  - 70
EP  - 76
SN  - 1951-6851
UR  - https://doi.org/10.2991/caai-17.2017.14
DO  - https://doi.org/10.2991/caai-17.2017.14
ID  - Zhao2017/06
ER  -