The invention discloses a sweepforward canard flying wing aerodynamic layout unmanned aerial vehicle, and the unmanned aerial vehicle comprises a vehicle body, main wings, edge strip wings, full-motion canard wings and full-motion vertical tail wings, wherein the main wings, the edge strip wings, the full-motion canard wings and the full-motion vertical tail wings are connected with the vehicle body, and the full-motion canard wings and the full-motion vertical tail wings are arranged at the front end of the vehicle body; the main wings and the edging wings are arranged at the rear end of thefuselage and are of an integrated structure; the flying wing aerodynamic layout, the canard aerodynamic layout and the sweepforward wing aerodynamic layout are fused, so the flying performance of thefixed-wing aircraft is well improved, the contradiction between sweepforward wing aerodynamic divergence and structural quality is solved, the problems that the maximum lift coefficient Clmax of the flying wing layout is too small and the pitching maneuverability is poor are solved, and the problem that a canard layout structure is complex is solved; the maneuvering performance, the loading capacity, the low-speed performance and the like of the canard layout structure are greatly improved, and compared with a conventional aerodynamic layout fixed-wing unmanned aerial vehicle, the effective load of the canard layout structure is increased by 20%, the take-off and landing distance is shortened by 35%, the maximum flight speed is increased by 5%, and the minimum flight speed is reduced by 30%.