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dc.contributor.authorŞahin, Hüseyin
dc.contributor.authorKöse, Oğuz
dc.contributor.authorOktay, Tugrul
dc.date.accessioned2023-02-09T11:57:33Z
dc.date.available2023-02-09T11:57:33Z
dc.date.issued2022en_US
dc.identifier.citationŞahin, H., Kose, O., & Oktay, T. (2022). Simultaneous autonomous system and powerplant design for morphing quadrotors. Aircraft Engineering and Aerospace Technology, 94(8), 1228-1241. doi:10.1108/AEAT-06-2021-0180en_US
dc.identifier.issn17488842
dc.identifier.urihttps://www.emerald.com/insight/content/doi/10.1108/AEAT-06-2021-0180/full/html
dc.identifier.urihttps://hdl.handle.net/20.500.12440/5805
dc.description.abstractPurpose: This study aims to optimize autonomous performance (i.e. both longitudinal and lateral) and endurance of the quadrotor type aerial vehicle simultaneously depending on the autopilot gain coefficients and battery weight. Design/methodology/approach: Quadrotor design processes are critical to performance. Unmanned aerial vehicle durability is an important performance parameter. One of the factors affecting durability is the battery. Battery weight, energy capacity and discharge rate are important design parameters of the battery. In this study, proper autopilot gain coefficients and battery weight are obtained by using a stochastic optimization method named as simultaneous perturbation stochastic approximation (SPSA). Because there is no direct correlation between battery weight and battery energy density, artificial neural network (ANN) is benefited to obtain battery energy density corresponding to resulted battery weight found from SPSA algorithm. By using the SPSA algorithm optimum performance index is obtained, then obtained data is used for longitudinal and lateral autonomous flight simulations. Findings: With SPSA, the best proportional integrator and derivative (PID) coefficients and battery weight, energy efficiency and endurance were obtained in case of morphing. Research limitations/implications: It takes a long time to find the most suitable battery values depending on quadrotor endurance. However, this situation can be overcome with the proposed SPSA. Practical implications: It is very useful to determine quadrotor endurance, PID coefficients and morphing rate using the optimization method. Social implications: Determining quadrotor endurance, PID coefficients and morphing rate using the optimization method provides advantages in terms of time, cost and practicality. Originality/value: The proposed method improves quadrotor endurance. In addition, with the SPSA optimization method and ANN, the parameters required for endurance will be obtained faster and more securely. In addition, the energy density according to the battery weight also contributes to the clean environment and energy efficiency. © 2022, Emerald Publishing Limiteen_US
dc.language.isoengen_US
dc.publisherEmerald Group Holdings Ltd.en_US
dc.relation.ispartofAircraft Engineering and Aerospace Technologyen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectANNen_US
dc.subjectEnduranceen_US
dc.subjectMorphingen_US
dc.subjectOptimizationen_US
dc.subjectPIDen_US
dc.subjectQuadrotoren_US
dc.subjectSPSAen_US
dc.titleSimultaneous autonomous system and powerplant design for morphing quadrotorsen_US
dc.typearticleen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.description.wospublicationidWOS:000772473100001en_US
dc.departmentYüksekokullar, Uygulamalı Bilimler Yüksekokulu, Havacılık Yönetimi Bölümüen_US
dc.authorid0000-0002-8069-8749en_US
dc.identifier.volume94en_US
dc.identifier.issue8en_US
dc.identifier.startpage1228en_US
dc.contributor.institutionauthorKöse, Oğuz
dc.identifier.doi10.1108/AEAT-06-2021-0180en_US
dc.identifier.endpage1241en_US
dc.authorwosidCZZ-3926-2022en_US
dc.authorscopusid57211985357en_US


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