An undercarriage, a middle large rotor and a middle large motor are connected to the lower portion of a
fuselage body and sequentially connected to the top of a middle small
tower, and the right front portion, the left front portion, the left rear portion and the right rear portion of the
fuselage body are correspondingly connected with a right front
fuselage arm, a left front fuselage arm, a left rear fuselage arm, a right rear fuselage arm and a power
assembly. The connecting line of the rotating centers of the rotors of the four power assemblies is square or rectangular, the rotating directions of the rotors of the power assemblies at the same opposite angles are the same, the rotating directions of the rotors of the power assemblies at different opposite angles are opposite, and the rotating faces of the two rotors opposite to the middle large rotor in rotating direction incline around the axes of the respective arms. The included angle between the rotating surfaces of the two rotors and the horizontal plane is an
acute angle beta, the rotating surfaces of the two rotors with the same rotating direction as the middle large rotor incline around respective arm axes, the included angle between the rotating surfaces of the two rotors and the horizontal plane is an
acute angle theta, beta is larger than theta, the reaction torque and the horizontal component torque of the rotors jointly drive the aircraft to steer, and the aircraft has the advantages of being long in endurance time, large in load and high in wind resistance. And a universal flight platform is formed.