Flight control system for quad-rotor aircraft based on improved integral separation PID

DOI

10.2991/icmmita-16.2016.108How to use a DOI?

Keywords

quad-rotor aircraft; PI algorithm; quaternion method; PID control algorithm

Abstract

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.

Copyright

© 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/).

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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  -