FIXED-WING AIRCRAFT CAPABLE OF TAKING OFF AND LANDING VERTICALLY, AND FLIGHT CONTROL METHOD THEREFOR

摘要

The present invention discloses a vertical take-off and landing fixed-wing aircraft and the flight control method thereof, the fixed-wing aircraft comprises a fuselage (10), fixed-wings (11) and a thruster (12) both configured on the fuselage. A storage room (13) is configured inside the fuselage (10), a plurality of openings and their corresponding doors (14) are configured on the fuselage (10), and the openings are connected to the storage room (13). A driving mechanism (30), and a deployable supporting mechanism driven by the driving mechanism (30) are arranged inside the storage room (13), and the outer ends of the deployable supporting mechanism are provided with vertical lifters (40). The fixed-wing aircraft can be in an open state and a closed state, in the open state, the doors (14) open and the vertical lifters (40) spread out outside the storage room (13) through the doors (14), by the act of the deployable supporting mechanism; in the closed state, the vertical lifters (40) are located within the storage room (13) by act of the deployable supporting mechanism while the doors (14) closed. The aircraft may operate in high-speed cruise mode or vertical take-off and landing mode, and can reach a working condition of highest energy efficiency in both modes.