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