Design of Multi-rotor Control System Basing on Coaxial Propellers

被引：0
|
作者：
Zhang, Yunqi [1 ]
Xu, Yong [1 ]
Zhao, Hangzhou [1 ]
机构：
[1] 5 South Zhongguancun St, Beijing, Peoples R China
来源：
PROCEEDINGS OF THE 2016 INTERNATIONAL CONFERENCE ON APPLIED MATHEMATICS, SIMULATION AND MODELLING | 2016年 / 41卷
关键词：
multi-rotor aircraft; coaxial propellers; control system; PID control;
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
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.
引用
收藏
页码：197 / 200
页数：4
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