TY - GEN
T1 - Experimental considerations on an attitude control system with measurement noises for an X4-Flyer
AU - Watanabe, Keigo
AU - Iwabe, Hirotaro
AU - Ouchi, Yusuke
AU - Nagai, Isaku
PY - 2013/11/25
Y1 - 2013/11/25
N2 - 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.
AB - 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.
KW - Aerial robot
KW - Attitude control
KW - Measurement noises
KW - Vibration-proof technique
UR - http://www.scopus.com/inward/record.url?scp=84887939308&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84887939308&partnerID=8YFLogxK
U2 - 10.1109/ICMA.2013.6617999
DO - 10.1109/ICMA.2013.6617999
M3 - Conference contribution
AN - SCOPUS:84887939308
SN - 9781467355582
T3 - 2013 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013
SP - 686
EP - 691
BT - 2013 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013
T2 - 2013 10th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013
Y2 - 4 August 2013 through 7 August 2013
ER -