Title :
A discrete model reference sliding mode controller with a disturbance compensator and its application to flight simulator
Author :
Cai Chao ; Wang Wei-hong ; Zhang Wu-long
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fDate :
May 31 2014-June 2 2014
Abstract :
As for parameters fluctuating, uncertainties caused by external disturbance and friction, the nonlinearity of the flight simulator turntable servo system, a discrete model reference sliding mode control theme combining with adaptive method and decoupled disturbance compensator is presented, and the globally asymptotically stability of the system is proved. The simulation results verified that the proposed control method can restrain the uncertainties and external disturbance of the flight simulator servo system efficiently assuring the dynamic tracking performance and strong robustness at a long range frequency.
Keywords :
adaptive control; aerospace simulation; asymptotic stability; compensation; control nonlinearities; discrete systems; robust control; servomechanisms; uncertain systems; variable structure systems; adaptive method; decoupled disturbance compensator; discrete model reference sliding mode controller; dynamic tracking performance; external disturbance; flight simulator turntable servo system; friction; global asymptotic stability; nonlinearity; robustness; uncertainties; Adaptation models; Mathematical model; Robustness; Servomotors; Sliding mode control; Vectors; Discrete Control System; Disturbance Compensator; Flight Simulator; Model Reference Control; Sliding Mode Control;
Conference_Titel :
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location :
Changsha
Print_ISBN :
978-1-4799-3707-3
DOI :
10.1109/CCDC.2014.6852772