The unmanned aerial vehicle of the present application includes: a body portion, a battery is installed, the forward direction is set as the x-axis; a plurality of rotors, four or more are provided around the body portion, each rotation axis is aligned in the z-axis direction; an x-axis tilt mechanism portion, the plurality of rotors are tilted with each axis parallel to the x-axis as the center; a y-axis tilt mechanism portion, the plurality of rotors are tilted with each axis parallel to the y-axis as the center; and a first
drive motor portion for driving the y-axis tilt mechanism portion; a second
drive motor portion for driving the x-axis tilt mechanism portion; a control portion, the first rotor, the second rotor, the third rotor, the fourth rotor, the first
drive motor portion and the second drive motor portion are controlled to realize a plurality of flight
modes; and a wing portion, provided on the upper portion of the body portion, formed in the air foil shape to provide lift.