Modeling and Control Design of Quad copter Failsafe System
139 Abstract Quadcopter Unmanned Aerial Vehicle (UAV) has adapt to rapid response and high terrain capability, and now widely be used in reconnaissance, transporting supplies etc. In quad copter control system, with four degrees of freedom, quad copters are difficult to be controlled by non linear system under vibration from structure failure. In this paper, a dynamics model of quad copter control functionis presented. Radial Basis Function Neural Network (RBFNN) based on Proportional Integral Derivative (PID) controller is designed to realize the Adapted and automatically manage Control System (ASAC).Experiment of a quad copter in flight is given to verify the proposed scheme.