Title :
Continuous sliding mode controller with disturbance observer for hypersonic vehicles
Author :
Chaoxu Mu ; Qun Zong ; Bailing Tian ; Wei Xu
Author_Institution :
Tianjin Univ., Tianjin, China
Abstract :
In this paper, a continuous sliding mode controller with disturbance observer is proposed for the tracking control of hypersonic vehicles to suppress the chattering. The finite time disturbance observer is involved to make that the continuous sliding mode controller has the property of disturbance rejection. Due to continuous terms replacing the discontinuous term of traditional sliding mode control, switching modes of velocity and altitude firstly arrive at small regions with respect to disturbance observation errors. Switching modes keep zero and velocity and altitude asymptotically converge to their reference commands after disturbance observation errors disappear. Simulation results have proved the proposed method can guarantee the tracking of velocity and altitude with continuous sliding mode control laws, and also has the fast convergence rate and robustness.
Keywords :
aircraft control; attitude control; control nonlinearities; convergence; observers; space vehicles; variable structure systems; velocity control; altitude switching modes; asymptotic convergence; attitude control; chatter suppression; continuous sliding mode control laws; continuous sliding mode controller; convergence rate; disturbance observation errors; disturbance rejection; finite time disturbance observer; hypersonic vehicles; tracking control; velocity control; velocity switching modes; Atmospheric modeling; Observers; Robustness; Sliding mode control; Switches; Vehicle dynamics; Vehicles; Sliding mode control; chattering suppression; finite time disturbance observer; hypersonic vehicles; robustness;
Journal_Title :
Automatica Sinica, IEEE/CAA Journal of
DOI :
10.1109/JAS.2015.7032905