| 【文章摘要】 In late years the use of UAV which is suitable for the observation activities in a dangerous area is pushed forw ard.R otary wing type UAV which can perform vertical takeoff and landing and hovering is used. We propose a compact U AV called SW U M which is without tail rotor. We adopt " stator wing" as an anti- torque compensation mechanism instead of a tail rotor.First,the attitude control test around yaw axis was performed using the SW UM prototype on a free rotational table. It was confirmed that the attitude of the vehicle around yaw axis by stator wings was controlled well. We studied a control method for translational motion of this vehicle. The horizontal translational motion will be achieved by tilting the body fone of stator wing.We created the mathematical model of the kinetics of this vehicle,and are performed analysis by the computer simulation. |