Research on aircraft taxiing lateral control based on fuzzy controller

Aircraft anti-skid braking system is modeled, and the traditional anti-skid braking control algorithm is analyzed. A lateral fuzzy controller is designed, based on the original structure of the controller, whose key variable is the reference velocity, Two more inputs of aircraft drift angel and its derivation are introduced to compensate the reference velocities of two wheel braking control loops respectively. The simulation results demonstrate the performance of the lateral fuzzy controller on this principle.