Implementation Of Flight Control System Based On Kalman And PID Controller For UAV

Abstract Kalman and PID controller are used to design UAV Unmanned Air Vehicles formation flight control system for speed and pitch angle. UAV adjusted the PID parameters to realize control stability of UAV flight. The simulation results will show that Kalman and PID controller have better dynamic performance than the traditional controller in respect of simpler design higher precision easier implement etc. At the same time the control effect will be significantly improved. In addition Kalman 26 PID control is superior in short transition good stability anti-disturbance good control and etc it also fulfills the requirement of real-time and accurate control.