Design of PID controller and fan wing controller for FanWing

FanWing, a concept for embedding cross-flow fan into thick wing lift enhancement and thrust production, is new kind of aircraft. Since the action position after center gravity, rotation produces lift, thrust, an additional pitch-down moment. Although FanWing has achieved great success at air shows, scientists mainly concentrate on optimizing structure to improve characteristics power system dynamic performance but rarely consider control system. There still lot work do theoretical research engineering applications. Thus, present paper will some systems, including two methods: traditional elevator, aileron, rudder method method. The influence moment researched. Based study 3.5 kg proportional integral differential (PID) controllers are designed. proposed controller been compared with PID one. simulations show effectiveness in terms nonlinear simulation.