Adaptive Fault Tolerant Control of UAV Attitude Control System
Hangzhou Zhao, Xu Yong, Yunqi Zhang, Yuhao Ding
Available Online June 2017.
- https://doi.org/10.2991/caai-17.2017.14How to use a DOI?
- UAV; state feedback; error adjustment; adaptive fault tolerant control
- 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.
- 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 -