DocumentCode :
1804514
Title :
Feedback linearization and guaranteed cost control of uncertain nonlinear systems and its application to an air-breathing hypersonic flight vehicle
Author :
Rehman, Obaid Ur ; Petersen, Ian R.
Author_Institution :
Univ. of New South Wales at the Australian Defence Force Acad., Canberra, ACT, Australia
fYear :
2011
fDate :
15-18 May 2011
Firstpage :
688
Lastpage :
693
Abstract :
This paper presents some recent work on designing a nonlinear robust control system for an uncertain nonlinear system. In this research a new approach to uncertainty modeling is presented. The method uses the feedback linearization approach to linearize the nominal nonlinear dynamics of the uncertain nonlinear system and linearizes the nonlinear uncertainties at an arbitrary point using the mean value theorem. This approach gives a multi-input multi-output (MIMO) linear uncertain system model with unstructured uncertainty. A guaranteed cost controller is then designed for the linearized MIMO model which stabilizes the original uncertain nonlinear system. In order to demonstrate the procedure and effectiveness of the proposed method, it is applied to a velocity and altitude tracking control problem of an air-breathing hypersonic flight vehicle.
Keywords :
MIMO systems; attitude control; control system synthesis; cost optimal control; feedback; linearisation techniques; nonlinear control systems; robust control; uncertain systems; velocity control; air-breathing hypersonic flight vehicle; altitude tracking control; feedback linearization approach; guaranteed cost control; mean value theorem; multiinput multioutput linear uncertain system model; nonlinear robust control system; uncertain nonlinear systems; uncertainty modeling; velocity control; Control systems; Mathematical model; Nonlinear systems; Stability analysis; Uncertain systems; Uncertainty; Upper bound;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ASCC), 2011 8th Asian
Conference_Location :
Kaohsiung
Print_ISBN :
978-1-61284-487-9
Electronic_ISBN :
978-89-956056-4-6
Type :
conf
Filename :
5899155
Link To Document :
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