DocumentCode
622584
Title
Super-twisting sliding mode control based on Lyapunov analysis for the cursing flight of hypersonic vehicles
Author
Chaoxu Mu ; Changyin Sun ; Chengshan Qian ; Ruimin Zhang
Author_Institution
Dept. of Electr. Eng. & Autom., Tianjin Univ., Tianjin, China
fYear
2013
fDate
12-14 June 2013
Firstpage
522
Lastpage
527
Abstract
In this paper, the tracking control for air-breathing hypersonic vehicles in cruising flight is studied, where the super-twisting algorithm is utilized to design a continuous controller. The nonlinear transformation is used to clarify a control-oriented model for hypersonic vehicles. A second order sliding mode controller based on the super-twisting algorithm is designed for the tracking of velocity and altitude, and Lyapunov approach is involved to analyze the stability of closed loop system, which also demonstrates that sliding mode surfaces converge in a finite time. The super-twisting sliding mode control has the ability to reduce chattering and also is robust against varying parameters. Simulations are shown to validate that the proposed method has reduced chattering efficiently and the robustness has been also guaranteed.
Keywords
Lyapunov methods; aerospace control; aircraft; closed loop systems; control system synthesis; nonlinear control systems; variable structure systems; Lyapunov analysis; Lyapunov approach; air breathing hypersonic vehicles; closed loop system; continuous controller design; cursing flight; hypersonic vehicles; nonlinear transformation; stability analysis; super twisting sliding mode control; super-twisting algorithm; Aerodynamics; Atmospheric modeling; Lyapunov methods; Robustness; Sliding mode control; Vehicle dynamics; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation (ICCA), 2013 10th IEEE International Conference on
Conference_Location
Hangzhou
ISSN
1948-3449
Print_ISBN
978-1-4673-4707-5
Type
conf
DOI
10.1109/ICCA.2013.6565017
Filename
6565017
Link To Document