Self-adaptive high-speed aircraft layout based on wingtip deformation

The invention discloses a self-adaptive high-speed aircraft layout based on wingtip deformation. The self-adaptive high-speed aircraft layout comprises a center body, wings, two variable winglet and two one-way Flap rudders located at the rear ends of the lower surfaces of the wings. The center body is mounted on the wings and provides a mounting space for the payload of the aircraft; the wings are used for providing lift force for the aircraft to realize long-distance flight of the aircraft in the atmosphere; the variable winglets are mounted on the two sides of the rear sections of the wingsto provide course static stability for the aircraft in various flight states; and the one-way Flap rudders provide pitching and rolling control capability for the aircraft. According to the invention, different requirements of the aircraft on course stability and agility are met in different flight states; and meanwhile, the aerodynamic efficiency of the aircraft is improved under the condition of ensuring that the aircr