prikaz prve stranice dokumenta Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform
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Scientific paper - Original scientific paper
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. & 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, no. 6, 2023, pp. 1-32. https://doi.org/10.3390/aerospace10060528

Kotarski, Denis, Petar Piljek, Marko Pranjić and Josip Kasać. "Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform." Aerospace 10, no. 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), pp. 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]. 2023 June 01 [cited 2024 July 06];10(6):1-32. doi: 10.3390/aerospace10060528

D. Kotarski, P. Piljek, M. Pranjić and J. Kasać, "Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform", Aerospace, vol. 10, no. 6, pp. 1-32, June 2023. [Online]. Available at: https://urn.nsk.hr/urn:nbn:hr:235:385365. [Accessed: 06 July 2024]

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Metadata
Title (english)Concept of a Modular Multirotor Heavy Lift Unmanned Aerial Vehicle Platform
AuthorDenis Kotarski
AuthorPetar Piljek
AuthorMarko Pranjić
AuthorJosip Kasać
Author's institutionKarlovac University of Applied Sciences
Author's institutionUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract (english)
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.
Languageenglish
Publication typeScientific paper - Original scientific paper
Publication statusPublished
Peer reviewPeer review - international
Publication versionPublished version
Journal titleAerospace
Numberingvol. 10, no. 6, pp. 1-32
e-ISSN2226-4310
DOIhttps://doi.org/10.3390/aerospace10060528
URN:NBNurn:nbn:hr:235:385365
Publication2023-06-01
Document URLhttps://www.mdpi.com/2226-4310/10/6/528
Type of resourceText
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2024-07-04 16:15:23