Flight control system for quad-rotor aircraft based on improved integral separation PID
Hongpeng Tian, Lei Li
Available Online January 2017.
- 10.2991/icmmita-16.2016.108How to use a DOI?
- quad-rotor aircraft; PI algorithm; quaternion method; PID control algorithm
Quad-rotor aircraft can be widely used in military and civilian fields, and it is drawing a great deal of attention. Combining with PI algorithm and quaternion method, this article resolves the aircraft flight attitude and complete aircraft attitude control with improved integral separation PID control algorithm. At last, conventional PID controller, integral separation controller and improved integral separation controller are simulated in the environment of MATLAB and compared with each other. The result shows that the response rate of improved integral separation PID is faster than the conventional integral separation algorithm and the overshoot volume is also lower.
- © 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 - Hongpeng Tian AU - Lei Li PY - 2017/01 DA - 2017/01 TI - Flight control system for quad-rotor aircraft based on improved integral separation PID BT - Proceedings of the 2016 4th International Conference on Machinery, Materials and Information Technology Applications PB - Atlantis Press SP - 582 EP - 586 SN - 2352-538X UR - https://doi.org/10.2991/icmmita-16.2016.108 DO - 10.2991/icmmita-16.2016.108 ID - Tian2017/01 ER -