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
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