DocumentCode :
582076
Title :
Adaptive exponential time-varying sliding mode control for hypersonic cruise vehicles
Author :
Liang Wang ; Xiangdong Liu ; Binglong Cong ; Zhen Chen
Author_Institution :
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
fYear :
2012
fDate :
25-27 July 2012
Firstpage :
3160
Lastpage :
3165
Abstract :
This paper describes the design of an adaptive exponential time-varying sliding mode control (AETVSMC) with strong robustness for hypersonic cruise vehicles subject to parametric uncertainties on the inertial and aerodynamic coefficients. An adaptation scheme is adopted to deal with unknown but bounded system uncertainties. Thus, the selection of switching gains can be obtained on-line and the upper bounds of the model uncertainties are not required to be known in advance. Stability analysis of the closed-loop system is derived based on the Lyapunov theory. Finally, simulation results demonstrate the effectiveness and robustness of the proposed approach.
Keywords :
Lyapunov methods; adaptive control; aerodynamics; aircraft control; closed loop systems; control system synthesis; robust control; time-varying systems; uncertain systems; variable structure systems; AETVSMC; Lyapunov theory; adaptation scheme; adaptive exponential time-varying sliding mode control design; aerodynamic coefficients; closed-loop system; hypersonic cruise vehicles; inertial coefficients; model uncertainties; parametric uncertainties; robustness; stability analysis; switching gain selection; system uncertainties; Adaptation models; Aerodynamics; Robustness; Switches; Uncertainty; Vehicles; Adaptive; Exponential time-varying sliding mode; Hypersonic vehicle; Robustness;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2012 31st Chinese
Conference_Location :
Hefei
ISSN :
1934-1768
Print_ISBN :
978-1-4673-2581-3
Type :
conf
Filename :
6390465
Link To Document :
بازگشت