The Flight Control of Micro Quad-Rotor UAV Based on PID

被引：0

作者：

Mou, Yihong ^{[1
]}

Zhang, Qingyong ^{[1
]}

Liu, Shilin ^{[1
]}

Liang, Ketian ^{[1
]}

机构：

[1] Wuhan Univ Technol, Sch Automat, Wuhan 430070, Peoples R China

来源：

2016 31ST YOUTH ACADEMIC ANNUAL CONFERENCE OF CHINESE ASSOCIATION OF AUTOMATION (YAC) | 2016年

关键词：

micro quad-rotor UAV; flight control; quaternion; PID controls; android mobile phone;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Attitude estimation is the key part of the flight control system of micro quad-rotor UAV. To begin with, quaternion and complementary filter Attitude algorithm is designed to reduce the operation quantity of attitude estimation. And then using the PID control algorithm work out the attitude control. Finally, use the android mobile phone via Bluetooth control the flight status of UAV, The simulation results demonstrate that the PID control system is well to maintain stable flight of the aircraft.

引用

页码：353 / 356

页数：4