Airplane capable of performing fixed wing flight and vertical take-off and landing based on three-axle flight control panel

An airplane capable of performing fixed wing flight and vertical take-off and landing based on a three-axle flight control panel is characterized in the airplane structure and the airplane control connection manner. In the aspect of structure, the airplane is characterized in that front inclination/rotation power capsules are symmetrically arranged on two sides of each wing of the airplane, a rear inclination/rotation power capsule is arranged at the rear part of an airplane body. In the aspect of airplane control connection manner, the airplane is characterized by adopting an innovative connection manner based on a simple three-axle flight control panel, so that the airplane can complete fixed wing flight and vertical take-off and landing under the control of the three-axle flight control panel. The airplane provided by the invention can complete double flight modes including fixed wing flight and vertical take-off and has good maneuverability and high flight efficiency, which is very important for improving the survival rate of the airplane in a war. In addition, the airplane based on the conventional three-axle control panel is convenient and reliable in the control manner and is suitable for mass production.