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
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