Experimental measurement of a UAV propeller's thrust

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dc.authorid0000-0002-0479-6937
dc.contributor.authorKosa, Patrik
dc.contributor.authorKisev, Marian
dc.contributor.authorVacho, Lukas
dc.contributor.authorToth, Ladislav
dc.contributor.authorOlejar, Martin
dc.contributor.authorHarnicarova, Marta
dc.contributor.authorValicek, Jan
dc.contributor.authorTozan, Hakan
dc.date.accessioned2022-01-13T08:28:08Z
dc.date.available2022-01-13T08:28:08Z
dc.date.issued2022
dc.departmentİstanbul Medipol Üniversitesi, Mühendislik ve Doğa Bilimleri Fakültesi, Endüstri Mühendisliği Bölümü
dc.description.abstractAt present, there are several types of propellers in the field of the use of Unmanned Aerial Vehicles (UAVs) with unknown parameters, where it is necessary to provide information about their thrust, current consumption and maximal rotational speed (RPM). Commonly used methods for measurement of a propeller's thrust are mostly based on the usage of a single purpose system, on short measurements without data storage or on inaccurate sensors. The goal of this article is to develop a universal experimental measuring system for more accurate measurement of propeller's parameters (thrust, current consumption, maximal RPM). For more accurate measurement, the battery voltage, temperature and humidity of the environment were also measured. To acquire, measure and store the data safely on a micro SD card, a processing circuit based on an ATmega2560 microcontroller was developed. This innovative approach allowed to analyse the behaviour of the propeller and to measure the dependencies of the RPM on pulse width, of the current on RPM and of the thrust on RPM at different input conditions. The measurements have shown that the dependencies can be approximated by cubic functions. The mathematical description allows predicting the behaviour of the propeller in unmeasurable conditions.
dc.description.sponsorshipVedecka grantova agentura MSVVaS SR a SAV (VEGA) European Commissionen_US
dc.identifier.citationKosa, P., Kisev, M., Vacho, L., Toth, L., Olejar, M., Harnicarova, M. ... Tozan, H. (2022). Experimental measurement of a UAV propeller's thrust. Tehnical Gazette, 29(1), 73-80. https://doi.org/10.17559/TV-20201212185220
dc.identifier.doi10.17559/TV-20201212185220
dc.identifier.endpage80
dc.identifier.issn1330-3651
dc.identifier.issn1848-6339
dc.identifier.issue1
dc.identifier.scopus2-s2.0-85125650785
dc.identifier.scopusqualityQ3
dc.identifier.startpage73
dc.identifier.urihttps://doi.org/10.17559/TV-20201212185220
dc.identifier.urihttps://hdl.handle.net/20.500.12511/8795
dc.identifier.volume29
dc.identifier.wos000739663500011en_US
dc.identifier.wosqualityQ4
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherUniversity of Osijek
dc.relation.ispartofTehnical Gazetteen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectBLDC Motor
dc.subjectPropeller
dc.subjectThrust
dc.subjectUAV
dc.titleExperimental measurement of a UAV propeller's thrust
dc.typeArticle

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