27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS2010-P2.24

ATTITUDE CONTROL OF UAV USING DBD PLASMA ACTUATOR

H. Otsu, Y. Kamada*, Y. Yamagiwa*, T. Ohno**, T. Abe***, T. Ito***
Ryukoku Univ., Japan; *Shizuoka Univ., Japan; **Hirobo ltd., Japan; ***JAXA, Japan

Keywords: dbd plasma actuator, uav

We performed wind tunnel experiments to investigate the applicability of DBD plasma actuator for the attitude control of UAV. As a test model for wind tunnel experiments, a flyable UAV is selected to reproduce the real flight condition.

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