DocumentCode :
638853
Title :
Experimental considerations on an attitude control system with measurement noises for an X4-Flyer
Author :
Watanabe, K. ; Iwabe, Hirotaro ; Ouchi, Yusuke ; Nagai, Isaku
Author_Institution :
Grad. Sch. of Natural Sci. & Technol., Okayama Univ., Okayama, Japan
fYear :
2013
fDate :
4-7 Aug. 2013
Firstpage :
686
Lastpage :
691
Abstract :
This paper investigates about the influence of sensor noises to the attitude control system of X4-Flyer, where such noises come from vibrations due to the rotation of a rotor. It is pointed out that such measurement noises are serious in the gyroscope sensor which measures an attitude, and then we consider some noise counterplans from hardware and software. The validity of the proposed vibration-proof method or noise processing is verified through actual system experiment.
Keywords :
attitude control; attitude measurement; autonomous aerial vehicles; gyroscopes; helicopters; X4-Flyer; attitude control system; gyroscope sensor; measurement noises; noise processing; vibration-proof method; Accelerometers; Attitude control; Blades; Gyroscopes; Noise; Rotors; Vibrations; Aerial robot; Attitude control; Measurement noises; Vibration-proof technique;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2013 IEEE International Conference on
Conference_Location :
Takamatsu
Print_ISBN :
978-1-4673-5557-5
Type :
conf
DOI :
10.1109/ICMA.2013.6617999
Filename :
6617999
Link To Document :
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