Design of Multi-rotor Control System Basing on Coaxial Propellers

DOI

10.2991/amsm-16.2016.45How to use a DOI?

Keywords

multi-rotor aircraft; coaxial propellers; control system; PID control

Abstract

A kind of UAV with coaxial propellers and multi-rotor is presented and the dynamics model of this UAV is established in this paper, then the control system of the UAV is designed on the basis of PID control algorithm, which includes altitude and atti-tude control module. Simulation results show that the control system can realize effective altitude control and attitude control of the multi-rotor aircraft.

Copyright

© 2016, 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  - Yunqi Zhang
AU  - Yong Xu
AU  - Hangzhou Zhao
PY  - 2016/05
DA  - 2016/05
TI  - Design of Multi-rotor Control System Basing on Coaxial Propellers
BT  - Proceedings of the 2016 International Conference on Applied Mathematics, Simulation and Modelling
PB  - Atlantis Press
SP  - 197
EP  - 200
SN  - 2352-538X
UR  - https://doi.org/10.2991/amsm-16.2016.45
DO  - 10.2991/amsm-16.2016.45
ID  - Zhang2016/05
ER  -