DocumentCode :
2831896
Title :
Obtaining the real time yaw angle using electronic compass in quadrotor systems
Author :
Song, Qiang ; Feng, Jiangtao ; Zhang, Xiaochen ; Xiao, Jizhong
Author_Institution :
Dept. of Autom., Taiyuan Inst. Electr. Eng., Taiyuan, China
fYear :
2012
fDate :
June 30 2012-July 2 2012
Firstpage :
238
Lastpage :
242
Abstract :
This paper discusses the applications of an electronic compass in quadrotor micro aerial vehicles (MAVs). Firstly, the characteristics of the quadrotor and necessity to obtain real time yaw angle for navigation are presented. Secondly, the electronic compass is introduced as a component in quadrotor system. Electronic compass is an important sensor to provide intermediate data towards calculating the yaw value. Thirdly, the system structure of the quadrotor and the method of calculating yaw angles using electronic compasses are illustrated. The hardware design and PID controller of the quadrotor system are also introduced. Finally, the electronic compass calibration, which is an indispensable procedure to increase accuracy, is presented. The experimental results show that our method is effective and robust in calibrating the electronic compass.
Keywords :
aircraft control; compasses; rotors; three-term control; PID controller; calculating yaw angles; electronic compass calibration; hardware design; navigation; quadrotor micro aerial vehicle; quadrotor system; real time yaw angle; yaw value; Accelerometers; Calibration; Compass; Earth; Gyroscopes; Magnetic fields; Robot sensing systems; PID controller; calibration; compass; quadrotor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Science and Engineering (ICSSE), 2012 International Conference on
Conference_Location :
Dalian, Liaoning
Print_ISBN :
978-1-4673-0944-8
Electronic_ISBN :
978-1-4673-0943-1
Type :
conf
DOI :
10.1109/ICSSE.2012.6257183
Filename :
6257183
Link To Document :
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