Abstract
New rotor wing type UAV is the aerial vehicle which has a stator wing mechanism to deny the anti-torque by the main rotor. The stator wing is the wing attached under the main rotor. The stator wing causes torque to the body by the downwash of the main rotor and performs attitude control by the torque. This rotor wing type UAV was named SWUM. It perform a horizontal mobility by doing attitude control of an aerial vehicle by control of stator wing angle, not pitch angle control of main rotor bride. The validity of the attitude control by stator wings was confirmed by numerical simulation.
