Finally, main methods and characteristics of flying-wing UAV's control system design are analyzed based on nonlinear simulation results and some advice for improvement is presented.

Then it is convenient to construct a nonlinear simulation circuit and experiment with it, and the circuit can be a substitution of the nonlinear dynamic high-pressure measurement system.

Simulation results show that nonlinear state PI SVC controller cooperating with the excitation system of generator can improve dynamic stability of power system effectively.