Publication: Metaheuristic-assisted complex H-infinity flight control tuning for the Hawkeye unmanned aerial vehicle: A comparative study
dc.contributor.author | Kanokmedhakul, Yodsadej | |
dc.contributor.author | Bureerat, Sujin | |
dc.contributor.author | Panagant, Natee | |
dc.contributor.author | Radpukdee, Thana | |
dc.contributor.author | Pholdee, Nantiwat | |
dc.contributor.author | Yıldız, Ali Rıza | |
dc.contributor.buuauthor | YILDIZ, ALİ RIZA | |
dc.contributor.department | Mühendislik Fakültesi | |
dc.contributor.department | Makine Mühendisliği Bölümü | |
dc.contributor.researcherid | F-7426-2011 | |
dc.date.accessioned | 2025-01-17T08:08:34Z | |
dc.date.available | 2025-01-17T08:08:34Z | |
dc.date.issued | 2024-02-17 | |
dc.description.abstract | Selecting 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.sponsorship | Thailand Research Fund (TRF) - PHD/0153/2561 | |
dc.description.sponsorship | National Research Council of Thailand (NRCT) - N42A650549 | |
dc.identifier.doi | 10.1016/j.eswa.2024.123428 | |
dc.identifier.issn | 0957-4174 | |
dc.identifier.scopus | 2-s2.0-85185394943 | |
dc.identifier.uri | https://doi.org/10.1016/j.eswa.2024.123428 | |
dc.identifier.uri | https://www.sciencedirect.com/science/article/pii/S0957417424002938 | |
dc.identifier.uri | https://hdl.handle.net/11452/49547 | |
dc.identifier.volume | 248 | |
dc.identifier.wos | 001198014500001 | |
dc.indexed.wos | WOS.SCI | |
dc.language.iso | en | |
dc.publisher | Pergamon-Elsevier Science Ltd | |
dc.relation.journal | Expert Systems With Applications | |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi | |
dc.rights | info:eu-repo/semantics/closedAccess | |
dc.subject | Optimization algorithm | |
dc.subject | Uav | |
dc.subject | H-infinity synthesis | |
dc.subject | Evolutionary algorithm | |
dc.subject | Robust and optimum flight control | |
dc.subject | Longitudinal control | |
dc.subject | Computer science | |
dc.subject | Engineering | |
dc.subject | Operations research & management science | |
dc.title | Metaheuristic-assisted complex H-infinity flight control tuning for the Hawkeye unmanned aerial vehicle: A comparative study | |
dc.type | Article | |
dspace.entity.type | Publication | |
local.contributor.department | Mühendislik Fakültesi/Makine Mühendisliği Bölümü | |
local.indexed.at | WOS | |
local.indexed.at | Scopus | |
relation.isAuthorOfPublication | 89fd2b17-cb52-4f92-938d-a741587a848d | |
relation.isAuthorOfPublication.latestForDiscovery | 89fd2b17-cb52-4f92-938d-a741587a848d |