Mathematical modeling and fault tolerant control of uav with wing layout

Abstract

Abstract As the flying wing layout unmanned aerial vehicle (uav) extensive research and task environment increasingly complex, Yu Feiyi layout unmanned aerial vehicle (uav) for fault tolerant control gradually become the main technical means of the flight control, according to the established mathematical model of the flying wing layout of unmanned aerial vehicle (uav) set the actuator failure effect, with adaptive fault-tolerant algorithm, is given for unmanned aerial vehicle (uav) horizontal lateral movement in the MATLAB/simulink, realize the rapid and stable, the control command and response to complete the fault-tolerant control of flying wing uavs.