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dc.contributor.authorKose, Oguz
dc.contributor.authorOktay, Tugrul
dc.date.accessioned2021-11-09T19:48:38Z
dc.date.available2021-11-09T19:48:38Z
dc.date.issued2020
dc.identifier.issn1748-8842
dc.identifier.issn1758-4213
dc.identifier.urihttps://doi.org/10.1108/AEAT-01-2020-0026
dc.identifier.urihttps://hdl.handle.net/20.500.12440/3698
dc.description.abstractPurpose The purpose of this paper is to design a quadrotor with collective morphing using the simultaneous perturbation stochastic approximation (SPSA) optimization algorithm. Design/methodology/approach Quadrotor design is made by using Solidworks drawing program and some mathematical performance relations. Modelling and simulation are performed in Matlab/Simulink program by using the state space model approaches with the parameters mostly taken from Solidworks. Proportional integral derivative (PID) approach is used as control technique. Morphing amount and the best PID coefficients are determined by using SPSA algorithm. Findings By using SPSA algorithm, the amount of morphing and the best PID coefficients are determined, and the quadrotor longitudinal and lateral flights are made most stable via morphing. Research limitations/implications It takes quite a long time to model the quadrotor in Solidworks and Matlab/Simulink with the state space model and using the SPSA algorithm. However, this situation is overcome with the proposed model. Practical implications Optimization with SPSA is very useful in determining the amount of morphing and PID coefficients for quadrotors. Social implications SPSA optimization method is useful in terms of cost, time and practicality. Originality/value It is released to improve performance with morphing, to determine morphing rate with SPSA algorithm and to determine PID coefficients accordingly.en_US
dc.language.isoengen_US
dc.publisherEmerald Group Publishing Ltden_US
dc.relation.ispartofAircraft Engineering and Aerospace Technologyen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectOptimizationen_US
dc.subjectUAVsen_US
dc.subjectQuadrotoren_US
dc.subjectModellingen_US
dc.subjectPIDen_US
dc.subjectCollective morphingen_US
dc.subjectSPSAen_US
dc.titleSimultaneous quadrotor autopilot system and collective morphing system designen_US
dc.typearticleen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.description.wospublicationidWOS:000541533000001en_US
dc.description.scopuspublicationid2-s2.0-85086256496en_US
dc.departmentGümüşhane Üniversitesien_US
dc.authoridOKTAY, TUGRUL / 0000-0003-4860-2230
dc.identifier.volume92en_US
dc.identifier.issue7en_US
dc.identifier.startpage1093en_US
dc.identifier.doi10.1108/AEAT-01-2020-0026
dc.identifier.endpage1100en_US
dc.authorscopusid57211985357
dc.authorscopusid55334339800


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