PIL simulations of an FWUAV under windy conditions

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dc.authoridBaykara, Cemal/0000-0002-3797-6563
dc.contributor.authorUlker, Hakan
dc.contributor.authorBaykara, Cemal
dc.contributor.authorOzsoy, Can
dc.date.accessioned2024-12-24T19:28:31Z
dc.date.available2024-12-24T19:28:31Z
dc.date.issued2018
dc.departmentSiirt Üniversitesi
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.
dc.identifier.doi10.1108/AEAT-06-2016-0096
dc.identifier.endpage470
dc.identifier.issn1748-8842
dc.identifier.issn1758-4213
dc.identifier.issue2
dc.identifier.scopus2-s2.0-85086760902
dc.identifier.scopusqualityQ2
dc.identifier.startpage461
dc.identifier.urihttps://doi.org/10.1108/AEAT-06-2016-0096
dc.identifier.urihttps://hdl.handle.net/20.500.12604/7098
dc.identifier.volume90
dc.identifier.wosWOS:000427148800024
dc.identifier.wosqualityQ3
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherEmerald Group Publishing Ltd
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_20241222
dc.subjectFlight control
dc.subjectModel predictive control
dc.subjectFixed wing unmanned aerial vehicle
dc.subjectProcessor in the loop
dc.subjectWindy conditions
dc.titlePIL simulations of an FWUAV under windy conditions
dc.typeArticle

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