四発ティルトロータ型VTOLの遷移飛行制御

抄録

We developed a quad tilt rotor type VTOL with fixed wing, which aims to transit to a horizontal flight state, behaving as a quad rotor helicopter during vertical take-off and landing, and as a thrust device by tilting four rotors during level flight. In this experiment, hovering experiment and horizontal flight experiment by rotor inclination were carried out. As a result, it was found that horizontal flight is possible without affecting the pitch axis when the aircraft stabilizes at hovering and tilting the rotor.