The invention discloses a coaxial dual-rotor aircraft, and relates to the technical field of aircrafts. The aircraft comprises an aircraft body, a coaxial double-rotor
assembly, a deformable stub wing and a vector thrust
paddle, an
operating system and an aircraft body sensor are arranged on the aircraft body, and the aircraft body sensor is in communication connection with the
operating system. The
fuselage structure of a conventional coaxial rigid double-rotor helicopter is reserved, the
propeller hub without upper rotor control is adopted, compared with a conventional
propeller hub with upper and lower rotor control, the
propeller hub has the advantages that the control structure is simplified, and the structural performance is improved, meanwhile, due to the fact that upper rotor control is omitted, the deformable stub wings and the vector thrust propellers are arranged on the
fuselage, and the structure performance is improved. The deformable stub wings can make up for the possible unbalance of the overall rolling torque of the aircraft when the upper rotor flies forwards at a high speed, the tilting device can drive the thrust paddles to tilt towards the
fuselage relative to the fuselage, and
yaw torque is generated by changing the thrust direction of the thrust paddles, so that the reaction torque of the upper rotor and the lower rotor flies at a high speed is balanced, and the stability of the aircraft is improved. And therefore, the
controllability of
yaw control is ensured.