Light and small flying-wing manned aircraft with short takeoff and landing capacity

The invention designs a light and small flying-wing aircraft with a short takeoff and landing (STOL) capacity. With the integrated design of aircraft body, aircraft wings and a cockpit, the low-resistance cruise advantage of flying-wings is fully utilized, and vector forces before the center of gravity are adopted by the flying-wings and are matched with the design of a leading edge flap and a trail edge flap, thereby realizing the STOL capacity of the flying-wing aircraft. Compared with the light and small aircraft of the same type, the light and small flying-wing aircraft provided by the invention has superior comprehensive performance.