Multicopter with passively-adjusting tiltwing

A multicopter comprising:

• a fuselage, a fuselage first thruster, a wing (1), and a first tiltwing thruster (2) statically connected to the wing (1) forming a passively-adjusting tiltwing (3),
• wherein a bearing mechanically couples the tiltwing and the fuselage said tiltwing freely rotatable relative to the fuselage within a predetermined angular range around a tiltwing axis (4),
• said tiltwing having i) a mass centroid, ii) an area centroid, iii) a mass centroid torque distance being the distance between the mass centroid and the tiltwing axis, iv) an area centroid torque distance being the distance between the area centroid and the tiltwing axis, and v) a tiltwing centroid ratio said centroid ratio being the mass centroid torque distance divided by the area centroid torque distance,
• wherein the value of the tiltwing centroid ratio is between 0.2 and 5,
• wherein aerodynamic and gravitational forces produce torques about the tiltwing axis said torques comprising a positive tiltwing center of gravity force torque, a negative impacting air aerodynamic force torque, and a third positive torque, and
• wherein thrust of the fuselage first thruster relative to thrust of the first tiltwing thruster controls the pitch of the fuselage.