Publication:
Metaheuristic-assisted complex H-infinity flight control tuning for the Hawkeye unmanned aerial vehicle: A comparative study

dc.contributor.authorKanokmedhakul, Yodsadej
dc.contributor.authorBureerat, Sujin
dc.contributor.authorPanagant, Natee
dc.contributor.authorRadpukdee, Thana
dc.contributor.authorPholdee, Nantiwat
dc.contributor.authorYıldız, Ali Rıza
dc.contributor.buuauthorYILDIZ, ALİ RIZA
dc.contributor.departmentMühendislik Fakültesi
dc.contributor.departmentMakine Mühendisliği Bölümü
dc.contributor.researcheridF-7426-2011
dc.date.accessioned2025-01-17T08:08:34Z
dc.date.available2025-01-17T08:08:34Z
dc.date.issued2024-02-17
dc.description.abstractSelecting weighting factors for H-infinity controller requires tones of knowledge and experience without guaranteeing obtaining the best results. This paper proposes novel idea for H-infinity controller synthesis using metaheuristics (MHs). The optimisation problem for the H-infinity controller synthesis is posed to find the weighting factors to optimise the control performance subject to stability and control handling constraints. A number of established MHs are used to solve the problem while their performance are investigated. The results indicate that the Artificial Hummingbird Algorithm and Grey Wolf Optimizer is the most efficient algorithm for the optimisation problem of H-infinity flight control design. Based on this study, the performance of several MHs on solving the H-infinity flight control design are examined while the optimum weighting factors for H-infinity flight controller are obtained. This paper is said to be a based line of studying in easy and efficient way for Hinfinity controller synthesis using MHs.
dc.description.sponsorshipThailand Research Fund (TRF) - PHD/0153/2561
dc.description.sponsorshipNational Research Council of Thailand (NRCT) - N42A650549
dc.identifier.doi10.1016/j.eswa.2024.123428
dc.identifier.issn0957-4174
dc.identifier.scopus2-s2.0-85185394943
dc.identifier.urihttps://doi.org/10.1016/j.eswa.2024.123428
dc.identifier.urihttps://www.sciencedirect.com/science/article/pii/S0957417424002938
dc.identifier.urihttps://hdl.handle.net/11452/49547
dc.identifier.volume248
dc.identifier.wos001198014500001
dc.indexed.wosWOS.SCI
dc.language.isoen
dc.publisherPergamon-Elsevier Science Ltd
dc.relation.journalExpert Systems With Applications
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectOptimization algorithm
dc.subjectUav
dc.subjectH-infinity synthesis
dc.subjectEvolutionary algorithm
dc.subjectRobust and optimum flight control
dc.subjectLongitudinal control
dc.subjectComputer science
dc.subjectEngineering
dc.subjectOperations research & management science
dc.titleMetaheuristic-assisted complex H-infinity flight control tuning for the Hawkeye unmanned aerial vehicle: A comparative study
dc.typeArticle
dspace.entity.typePublication
local.contributor.departmentMühendislik Fakültesi/Makine Mühendisliği Bölümü
local.indexed.atWOS
local.indexed.atScopus
relation.isAuthorOfPublication89fd2b17-cb52-4f92-938d-a741587a848d
relation.isAuthorOfPublication.latestForDiscovery89fd2b17-cb52-4f92-938d-a741587a848d

Files