PIL simulations of an FWUAV under windy conditions

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dc.contributor.authorUlker, Hakan
dc.contributor.authorBaykara, Cemal
dc.contributor.authorOzsoy, Can
dc.date.accessioned2024-03-13T10:35:37Z
dc.date.available2024-03-13T10:35:37Z
dc.date.issued2018
dc.departmentİstanbul Beykent Üniversitesien_US
dc.description.abstractPurpose A fixed wing unmanned aerial vehicle (FWUAV) is targeted to perform processor in the loop (PIL) simulations for the flight scenarios such as straight and level, level climb, level turn, climbing turn and level steady heading sideslip under windy conditions such as steady wind (SW) and wind gust (WG) in a desired and controlled manner. Design/methodology/approach The constrained multi-input-multi-output (MIMO) lateral and longitudinal linear models-based model predictive controllers (MPCs) which are proposed in a previous study (Ulker et al., 2017) are tested in the PIL simulations under specified windy conditions. BeagleBone Black Rev C is used as a target hardware or processor in the PIL simulations. Findings The results of the PIL simulations show that the MPCs proposed in the previous study can achieve satisfactory performance and flying qualities for the all flight scenarios handled in this paper under windy conditions. Practical implications The MPCs proposed in the previous study can be easily implemented in the real world to a low-cost and small-sized board like BeagleBone Black Rev C which is used in this paper. Originality/value The proposed MPCs in the previous study which are capable of providing more flexibility in terms of tracking complex trajectories are showed to be able to be implemented to real system by means of PIL simulations under the changeable windy conditions which are difficult for performance tests.en_US
dc.identifier.doi10.1108/AEAT-06-2016-0096
dc.identifier.endpage470en_US
dc.identifier.issn1748-8842
dc.identifier.issn1758-4213
dc.identifier.issue2en_US
dc.identifier.scopus2-s2.0-85086760902en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage461en_US
dc.identifier.urihttps://doi.org/10.1108/AEAT-06-2016-0096
dc.identifier.urihttps://hdl.handle.net/20.500.12662/4520
dc.identifier.volume90en_US
dc.identifier.wosWOS:000427148800024en_US
dc.identifier.wosqualityQ3en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherEmerald Group Publishing Ltden_US
dc.relation.ispartofAircraft Engineering And Aerospace Technologyen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectFlight controlen_US
dc.subjectModel predictive controlen_US
dc.subjectFixed wing unmanned aerial vehicleen_US
dc.subjectProcessor in the loopen_US
dc.subjectWindy conditionsen_US
dc.titlePIL simulations of an FWUAV under windy conditionsen_US
dc.typeArticleen_US

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