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Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform
Aerospace, 10 (2023), 6; 1-32. https://doi.org/10.3390/aerospace10060528
Kotarski, Denis; Piljek, Petar; Pranjić, Marko; Kasać, Josip

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Kotarski, D., Piljek, P., Pranjić, M. i Kasać, J. (2023). Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform. Aerospace, 10. (6), 1-32. doi: 10.3390/aerospace10060528

Kotarski, Denis, et al. "Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform." Aerospace, vol. 10, br. 6, 2023, str. 1-32. https://doi.org/10.3390/aerospace10060528

Kotarski, Denis, Petar Piljek, Marko Pranjić i Josip Kasać. "Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform." Aerospace 10, br. 6 (2023): 1-32. https://doi.org/10.3390/aerospace10060528

Kotarski, D., et al. (2023) 'Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform', Aerospace, 10(6), str. 1-32. doi: 10.3390/aerospace10060528

Kotarski D, Piljek P, Pranjić M, Kasać J. Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform. Aerospace [Internet]. 01.06.2023. [pristupljeno 05.07.2024.];10(6):1-32. doi: 10.3390/aerospace10060528

D. Kotarski, P. Piljek, M. Pranjić i J. Kasać, "Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform", Aerospace, vol. 10, br. 6, str. 1-32, Lipanj 2023. [Online]. Dostupno na: https://urn.nsk.hr/urn:nbn:hr:235:385365. [Citirano: 05.07.2024.]

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Podaci o radu
Naslov (engleski)Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform
AutorDenis Kotarski
AutorPetar Piljek
AutorMarko Pranjić
AutorJosip Kasać
Autorova ustanovaVeleučilište u Karlovcu
Autorova ustanovaSveučilište u Zagrebu
Fakultet strojarstva i brodogradnje
Znanstveno / umjetničko
područje, polje i grana		TEHNIČKE ZNANOSTI
Strojarstvo
Sažetak (engleski)
This paper presents a novel concept of a modular multirotor aerial robotic platform that can be used for specific profiles of heavy payload missions. A comprehensive mathematical model of the multirotor unmanned aerial vehicle (UAV) is presented, which is divided into the dynamic model and the control allocation scheme that describes the configuration of the aircraft. The components of the propulsion and energy module are selected, and the characterization of the propulsion units is carried out, as well as a preliminary analysis of the module parameters with regard to the considered payloads from 5 to 50 kg. The main goal is to design a modular aircraft that consists of easy-to-assemble modules and that enables the assembly of different propulsion and energy module configurations. Based on the analysis of system parameters, a modular aerial system is designed and the process of manufacturing using rapid prototyping technologies is presented. Based on the parameters obtained from the aircraft assembly CAD model and the implemented mathematical model, simulations are conducted for the two considered missions in the field of smart agriculture. For the purpose of conducting preliminary experiments, a quadrotor aircraft is built and tested in the case of attitude and remote control.
Jezikengleski
Vrsta publikacijeZnanstveni rad - Izvorni znanstveni rad
Status objaveObjavljen
Vrsta recenzijeRecenziran - međunarodna recenzija
Verzija publikacijeObjavljena verzija rada (izdavačev PDF)
Naslov časopisaAerospace
Brojčani podacivol. 10, br. 6, str. 1-32
e-ISSN2226-4310
DOIhttps://doi.org/10.3390/aerospace10060528
URN:NBNurn:nbn:hr:235:385365
Datum objave publikacije2023-06-01
URL dokumentahttps://www.mdpi.com/2226-4310/10/6/528
Vrsta resursaTekst
Prava pristupaOtvoreni pristup
Uvjeti korištenjaIkona licence Zaštićeno autorskim pravom.
Datum i vrijeme pohrane2024-07-04 16:15:23