VTOL型無人タンデム翼機の操舵機構

―重心移動型と独立動翼型の比較―

抄録

The tandem wing type aircraft transforming mechanism for VTOL has many examples which equip each wing tip with a tilt type rotor. In this research, It transforms it into VTOL/STOVL by equipping the barycentric position of the airframe with two tilt type rotors. The proposal method can be used though interests of both are counterbalanced as for the comparative result by the scene for which a steady flying characteristic is necessary.