Please use this identifier to cite or link to this item: http://hdl.handle.net/2440/80383
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Type: Journal article
Title: Control design for a hypersonic aircraft using a switched linear parameter-varying system approach
Author: Lu, Q.
Zhang, L.
Shi, P.
Karimi, H.
Citation: Proceedings of the Institution of Mechanical Engineers Part I-Journal of Systems and Control Engineering, 2013; 227(1):85-95
Publisher: Professional Engineering Publishing Ltd
Issue Date: 2013
ISSN: 0959-6518
2041-3041
Statement of
Responsibility: 
Qiugang Lu, Lixian Zhang, Peng Shi and Hamid Reza Karimi
Abstract: This paper is concerned with the control problem of an air-breathing hypersonic aircraft using a switched linear-parameter-varying systems approach. The rigid non-linear longitudinal model of a generic hypersonic aircraft is adopted with the aim of verifying the design methodology of the developed controller and switching logic. By linearizing the non-linear model of the hypersonic aircraft at trim points and dividing the velocity range into several parts, a switched linear parameter-varying model for the underlying system is derived. With the aid of multiple Lyapunov-like functions technique, controllers that ensure the tracking of given commands of the closed-loop system are designed under mode-independent and mode-dependent switching logic, respectively. Simulation results for the generic hypersonic aircraft show the effectiveness of the proposed method and the advantages of the mode-dependent switching logic.
Keywords: Average dwell time; hypersonic vehicle; mode-dependent average dwell time; switched linear parameter-varying system
Rights: © IMechE 2012
RMID: 0020131253
DOI: 10.1177/0959651812455897
Appears in Collections:Electrical and Electronic Engineering publications

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