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Switched H2-state-feedback control with application to a fighter aircraft

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journal contribution
posted on 08.05.2019, 13:47 by Emre Kemer, Hasan Başak, Emmanuel Prempain
This paper proposes two different ℋ2-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 ℋ2-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.

History

Citation

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering Institution of Mechanical Engineers, 2019

Author affiliation

/Organisation/COLLEGE OF SCIENCE AND ENGINEERING/Department of Engineering

Version

AM (Accepted Manuscript)

Published in

Proceedings of the Institution of Mechanical Engineers

Publisher

SAGE Publications (UK and US), Professional Engineering Publishing (Institution of Mechanical Engineers)

eissn

2041-3025

Acceptance date

02/04/2019

Copyright date

2019

Available date

08/05/2019

Publisher version

https://journals.sagepub.com/doi/10.1177/0954410019845981

Language

en