Switched H 2-state-feedback control with application to a fighter aircraft

This paper proposes two different H 2 -state-feedback controller synthesis algorithms for uncertain linear, time-varying, switched systems. The synthesis algorithms are based on a dwell-time approach, which makes use of time-varying parameter-dependent Lyapunov functions. The control laws consist of...

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Bibliographic Details
Published in:Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2019-11, Vol.233 (14), p.5428-5437
Main Authors: Kemer, Emre, Başak, Hasan, Prempain, Emmanuel
Format: Article
Language:English
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Summary:This paper proposes two different H 2 -state-feedback controller synthesis algorithms for uncertain linear, time-varying, switched systems. The synthesis algorithms are based on a dwell-time approach, which makes use of time-varying parameter-dependent Lyapunov functions. The control laws consist of state-feedback controllers that are switched according to external signals. The proposed synthesis algorithms are then employed to design switched H 2 -state-feedback control laws for the longitudinal dynamics of the ADMIRE fighter benchmark model. The results obtained in simulation show the merits of the proposed approach.
ISSN:0954-4100
2041-3025
DOI:10.1177/0954410019845981