• 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