• DocumentCode
    2365125
  • Title

    A simple controller of minisize quad-rotor vehicle

  • Author

    Hou, Hongning ; Zhuang, Jian ; Xia, Hu ; Wang, Guanwei ; Yu, Dehong

  • Author_Institution
    Sch. of Mech. Eng., Xi´´an Jiaotong Univ., Xi´´an, China
  • fYear
    2010
  • fDate
    4-7 Aug. 2010
  • Firstpage
    1701
  • Lastpage
    1706
  • Abstract
    Based on the analyzing of dynamics, one kind of quad-rotor controller is designed in this research. The quad-rotor is driven by four brushless DC micro-motors, with Mega644 being in rapport with three-axis gyro sensors, three-axis acceleration sensors, altitude pressure sensor, electronic compass and GPS signals, which can at the same time receives PWM wave flight order of the remote control receiver, propels the four non-sense of brushless DC motor speed regulators based on Mega8 single-chip through IIC data bus so as to control the aircraft´s flight attitude and directions.
  • Keywords
    acceleration control; aircraft control; attitude control; brushless DC motors; gyroscopes; height measurement; helicopters; micromotors; pressure sensors; pulse width modulation; GPS signal; IIC data bus; Mega644; Mega8 single-chip; PWM wave flight order; aircraft flight attitude control; altitude pressure sensor; brushless DC micromotor; electronic compass; quad-rotor controller; quad-rotor vehicle; remote control receiver; speed regulator; three-axis acceleration sensor; three-axis gyro sensor; Aerodynamics; Conferences; DC motors; Equations; Mathematical model; Propellers; Sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation (ICMA), 2010 International Conference on
  • Conference_Location
    Xi´an
  • ISSN
    2152-7431
  • Print_ISBN
    978-1-4244-5140-1
  • Electronic_ISBN
    2152-7431
  • Type

    conf

  • DOI
    10.1109/ICMA.2010.5588802
  • Filename
    5588802