Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/7817
Full metadata record
DC FieldValueLanguage
dc.contributor.authorTanyer, İlker-
dc.contributor.authorTatlıcıoğlu, Enver-
dc.contributor.authorZergeroǧlu, Erkan-
dc.date.accessioned2020-07-18T03:35:12Z-
dc.date.available2020-07-18T03:35:12Z-
dc.date.issued2020-
dc.identifier.issn0826-8185-
dc.identifier.issn1925-7090-
dc.identifier.urihttps://doi.org/10.2316/J.2020.206-0074-
dc.identifier.urihttps://hdl.handle.net/11147/7817-
dc.description.abstractOutput tracking control of an aircraft subject to uncertainties in the dynamic model and additive state-dependent nonlinear disturbancelike terms is aimed. Uncertainties in the aircraft dynamic model yield an uncertain input gain matrix, which is neither positive definite nor symmetric and an uncertain term in the error dynamics. To deal with the uncertain input gain matrix, a decomposition method is utilized to put error dynamics in a form where an uncertain positive definite matrix multiplies the auxiliary error but this results in the control input to be pre-multiplied first with a unity upper triangular matrix which is uncertain and then with a known diagonal matrix. A novel controller composed of a neural network compensation term and an integral of signum of error is designed. A novel Lyapunov type stability analysis is utilized to prove global asymptotic tracking of output of a reference model. Extensive numerical simulations are presented to demonstrate the efficacy of the proposed controller where robustness to variation of initial states and a comparison with a robust controller are also shown. © 2020 Acta Press. All rights reserved.en_US
dc.language.isoenen_US
dc.publisherACTA Pressen_US
dc.relation.ispartofInternational Journal of Robotics and Automationen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectAircraft controlen_US
dc.subjectLyapunoven_US
dc.subjectNeural networksen_US
dc.subjectRobust controlen_US
dc.subjectUncertain systemsen_US
dc.titleNeural network based robust control of an aircraften_US
dc.typeArticleen_US
dc.institutionauthorTatlıcıoğlu, Enver-
dc.institutionauthorTanyer, İlker-
dc.institutionauthorZergeroǧlu, Erkan-
dc.departmentİzmir Institute of Technology. Electrical and Electronics Engineeringen_US
dc.identifier.volume35en_US
dc.identifier.issue1en_US
dc.identifier.startpage13en_US
dc.identifier.endpage22en_US
dc.identifier.wosWOS:000550619400002en_US
dc.identifier.scopus2-s2.0-85080873640en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.identifier.doi10.2316/J.2020.206-0074-
dc.relation.doi10.2316/J.2020.206-0074en_US
dc.coverage.doi10.2316/J.2020.206-0074en_US
dc.identifier.wosqualityQ4-
dc.identifier.scopusqualityQ3-
item.languageiso639-1en-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.cerifentitytypePublications-
item.grantfulltextnone-
item.fulltextNo Fulltext-
item.openairetypeArticle-
crisitem.author.dept03.05. Department of Electrical and Electronics Engineering-
Appears in Collections:Electrical - Electronic Engineering / Elektrik - Elektronik Mühendisliği
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection
Show simple item record



CORE Recommender

SCOPUSTM   
Citations

5
checked on Feb 17, 2024

WEB OF SCIENCETM
Citations

4
checked on Jan 27, 2024

Page view(s)

138
checked on Feb 26, 2024

Google ScholarTM

Check




Altmetric


Items in GCRIS Repository are protected by copyright, with all rights reserved, unless otherwise indicated.