抄録
The purpose of this study is to develop a wind tunnel experiment system to analyze flight mechanism of flapping Micro Air Vehicles (MAV). This system controls fixed wing MAVs and flapping MAVs in a wind tunnel without a supporting rod and analyzed for stable flight of the MAVs. In order to realize this, we detected position and yaw angle of MAVs in a low speed wind tunnel by a image processing system, which it consist of two CCD (Charge Coupled Device) cameras. Being based on the experimental results obtained in the flight of the fixed wing MAVs by PD control, we have been succeeded in the free flight of the flapping MAVs by controlling rudder, flapping frequency.
