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

dc.authorid0000-0002-3724-6819en_US
dc.contributor.authorKemer, Emre
dc.contributor.authorBaşak, Hasan
dc.contributor.authorPrempain, Emmanuel
dc.date.accessioned2020-11-19T07:58:14Z
dc.date.available2020-11-19T07:58:14Z
dc.date.issued2019
dc.departmentAÇÜ, Mühendislik Fakültesien_US
dc.description.abstractThis 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.
dc.identifier.citationKemer, E., Başak, H., & Prempain, E. (2019). Switched H 2-state-feedback control with application to a fighter aircraft. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 233(14), 5428-5437.en_US
dc.identifier.doi10.1177/0954410019845981
dc.identifier.endpage5437en_US
dc.identifier.issue14en_US
dc.identifier.scopusqualityQ3
dc.identifier.startpage5428en_US
dc.identifier.urihttps://hdl.handle.net/11494/2474
dc.identifier.volume233en_US
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.institutionauthorBaşak, Hasan
dc.language.isoenen_US
dc.publisherSage Publicationsen_US
dc.relation.ispartofProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectDwell timeen_US
dc.subjectH2−switched controlen_US
dc.subjectSwitched Lyapunov functionsen_US
dc.subjectLongitudinal aircraft dynamicsen_US
dc.subjectLoad factor controlen_US
dc.titleSwitched H-2-state-feedback control with application to a fighter aircraften_US
dc.typeArticle

Dosyalar

Orijinal paket
Listeleniyor 1 - 1 / 1
[ X ]
İsim:
emre.kemer.pdf
Boyut:
780.48 KB
Biçim:
Adobe Portable Document Format
Açıklama:
Lisans paketi
Listeleniyor 1 - 1 / 1
[ X ]
İsim:
license.txt
Boyut:
1.44 KB
Biçim:
Item-specific license agreed upon to submission
Açıklama: