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https://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 |
DOI: | 10.1177/0959651812455897 |
Published version: | http://dx.doi.org/10.1177/0959651812455897 |
Appears in Collections: | Aurora harvest 4 Electrical and Electronic Engineering publications |
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