Title :
Research on aircraft taxiing lateral control based on fuzzy controller
Author :
Li, Yang ; Jiao, Zongxia ; Shang, Yaoxing
Author_Institution :
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
Abstract :
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.
Keywords :
aircraft control; braking; fuzzy control; aircraft antiskid braking system; aircraft taxiing lateral control; lateral fuzzy controller; reference velocity; two wheel braking control loops; Aerospace control; Aircraft; Atmospheric modeling; Control systems; Friction; Mathematical model; Wheels; anti-skid braking system; fuzzy control; lateral control; reference velocity;
Conference_Titel :
Fluid Power and Mechatronics (FPM), 2011 International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-8451-5
DOI :
10.1109/FPM.2011.6045830
