prikaz prve stranice dokumenta Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors
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Scientific paper - Original scientific paper
Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors
Applied Sciences, 11 (2021), 18; 1-18. https://doi.org/10.3390/app11188786
Kotarski, Denis; Piljek, Petar; Kasać, Josip; Majetić, Dubravko

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Kotarski, D., Piljek, P., Kasać, J. & Majetić, D. (2021). Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors. Applied Sciences, 11. (18), 1-18. doi: 10.3390/app11188786

Kotarski, Denis, et al. "Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors." Applied Sciences, vol. 11, no. 18, 2021, pp. 1-18. https://doi.org/10.3390/app11188786

Kotarski, Denis, Petar Piljek, Josip Kasać and Dubravko Majetić. "Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors." Applied Sciences 11, no. 18 (2021): 1-18. https://doi.org/10.3390/app11188786

Kotarski, D., et al. (2021) 'Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors', Applied Sciences, 11(18), pp. 1-18. doi: 10.3390/app11188786

Kotarski D, Piljek P, Kasać J, Majetić D. Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors. Applied Sciences [Internet]. 2021 September 21 [cited 2024 October 01];11(18):1-18. doi: 10.3390/app11188786

D. Kotarski, P. Piljek, J. Kasać and D. Majetić, "Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors", Applied Sciences, vol. 11, no. 18, pp. 1-18, September 2021. [Online]. Available at: https://urn.nsk.hr/urn:nbn:hr:235:070114. [Accessed: 01 October 2024]

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Title (english)Performance Analysis of Fully Actuated Multirotor Unmanned Aerial Vehicle Configurations with Passively Tilted Rotors
AuthorDenis Kotarski
AuthorPetar Piljek
AuthorJosip Kasać
AuthorDubravko Majetić
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 (croatian)
Unmanned aerial vehicles (UAVs) nowadays represent an interesting tool capable of performing various missions. The multirotor type of UAV is proven to be a potential solution in missions that require precise movements, such as environmental objects manipulation. In this paper, a procedure for the performance analysis of fully actuated multirotor UAV configurations is proposed. For this purpose, a configuration is described by a control allocation scheme and implemented in the software package which enables the analysis and control implementation of a real system. The parameter analysis of the passively tilted multirotor configurations is performed based on the characteristics of the electric propulsion units, and the allocation of propulsion forces is graphically shown. The results of the proposed procedure provide an insight into the capabilities of configurations and can ultimately be used to select the propulsion system components and parameters according to the requirements and constraints associated with the specific mission profile. An experimental aircraft was built, and custom firmware was created, which enable us to experimentally prove the feasibility of fully actuated and passively tilted configurations.
Languagecroatian
Publication typeScientific paper - Original scientific paper
Publication statusPublished
Peer reviewPeer review - international
Publication versionPublished version
Journal titleApplied Sciences
Numberingvol. 11, no. 18, pp. 1-18, 8786
e-ISSN2076-3417
DOIhttps://doi.org/10.3390/app11188786
URN:NBNurn:nbn:hr:235:070114
Publication2021-09-21
Document URLhttps://www.mdpi.com/2076-3417/11/18/8786
Type of resourceText
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2024-07-04 16:24:05