Multi-propeller tilting aircraft and flight control method therefor

A multi-propeller tilting aircraft, comprises a fuselage body (10), characterized in that, further comprises a left tilt wing (20) fixed on a left side of the fuselage body (10), at least one left front power propeller (21) and at least one left rear power propeller (22) which are respectively fixed on two opposite sides of the left tilt wing (20), a right tilt wing (30) fixed on a right side of the fuselage body (10), at least one right front power propeller (31) and at least one right rear power propeller (32) which are respectively fixed on two opposite sides of the right tilt wing (30), and a tail assembly fixed at the tail of the fuselage body (10);

• the tail assembly comprises a vertical tail (70), a horizontal tail and a horizontal tail rotor (60);
• wherein the left front power propeller (21), the left rear power propeller (22), the right front power propeller (31) and the right rear power propeller (32) implement flight power and attitude control for the vertical takeoff and landing and cruising of the aircraft.