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master's thesis
Analiza dinamike četverorotornog helikoptera
2011. urn:nbn:hr:235:021878
Adamić, Tihomir
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Adamić, T. (2011). Analiza dinamike četverorotornog helikoptera (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:021878

Adamić, Tihomir. "Analiza dinamike četverorotornog helikoptera." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2011. https://urn.nsk.hr/urn:nbn:hr:235:021878

Adamić, Tihomir. "Analiza dinamike četverorotornog helikoptera." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2011. https://urn.nsk.hr/urn:nbn:hr:235:021878

Adamić, T. (2011). 'Analiza dinamike četverorotornog helikoptera', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 17 April 2024, https://urn.nsk.hr/urn:nbn:hr:235:021878

Adamić T. Analiza dinamike četverorotornog helikoptera [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2011 [cited 2024 April 17] Available at: https://urn.nsk.hr/urn:nbn:hr:235:021878

T. Adamić, "Analiza dinamike četverorotornog helikoptera", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2011. Available at: https://urn.nsk.hr/urn:nbn:hr:235:021878

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Metadata
TitleAnaliza dinamike četverorotornog helikoptera
Title (english)Analysis of quadrotor helicopter flight dynamics
AuthorTihomir Adamić
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2011-04-01, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
Cilj ovog diplomskog rada je napraviti model četverorotornog helikoptera i provesti numeričku realizaciju leta te letjelice. Prvi dio rada predstavit će taj tip letjelice, njene mogućnosti i primjena. Nakon osnova slijedi konstruiranje odabrane konfiguracije letjelice aplikacijom CatiaV5R18 s ciljem dobivanja inercijskih karakteristika letjelice. U drugom dijelu rada postavljane su jednadžbe za numeričku analizu aerodinamike i dinamike letjelice. Za model rotora koristi se jedan model primijenjen na četiri rotora, dok se aerodinamika trupa zanemaruje. Dinamika letjelice proračunava se Newton Eulerovim jednadžbama, a numerički model i simulacija leta napraviti će se u MATLAB/Simulink okruženju, a rezultati prikazati u posljednjem dijelu. Ovaj model može se koristiti u daljnjem radu pri istraživanju stabilnosti i upravljivosti ovakvog tipa letjelice.
Keywords
Languagecroatian
URN:NBNurn:nbn:hr:235:021878
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2019-05-21 22:20:19