Research on fuzzy PID attitude controller for Multi-rotor UAV
- https://doi.org/10.2991/fmsmt-17.2017.143How to use a DOI?
- Fuzzy PID, Attitude controller, Multi-rotor, UAV
Multi-rotor UAV attitude system has many characteristics such as multi-input multi-output, strong coupling, fast time-varying and non-linearity. Thus, for multi rotor UAV attitude control system, the classic PID has some shortcomings. In this paper, the fuzzy PID controller is established by using fuzzy control and classical PID. The on-line self-tuning of PID parameters is realized. The simulation results show that compared with the classical PID, the fuzzy PID controller has the advantages of high control precision, stronger anti-interference ability and stronger robustness, and is more suitable for multi-rotor UAV attitude control system.
- © 2017, 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 - Shuo Gao AU - Qi Wang AU - Wen Jiang AU - Yan Liu PY - 2017/04 DA - 2017/04 TI - Research on fuzzy PID attitude controller for Multi-rotor UAV BT - Proceedings of the 2017 5th International Conference on Frontiers of Manufacturing Science and Measuring Technology (FMSMT 2017) PB - Atlantis Press SP - 726 EP - 729 SN - 2352-5401 UR - https://doi.org/10.2991/fmsmt-17.2017.143 DO - https://doi.org/10.2991/fmsmt-17.2017.143 ID - Gao2017/04 ER -