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master's thesis
Model leta helikoptera
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2010. urn:nbn:hr:235:384411
Zastavnik, Filip
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Institutional repository: Repository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb

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Zastavnik, F. (2010). Model leta helikoptera (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:384411

Zastavnik, Filip. "Model leta helikoptera." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2010. https://urn.nsk.hr/urn:nbn:hr:235:384411

Zastavnik, Filip. "Model leta helikoptera." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2010. https://urn.nsk.hr/urn:nbn:hr:235:384411

Zastavnik, F. (2010). 'Model leta helikoptera', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 17 June 2024, https://urn.nsk.hr/urn:nbn:hr:235:384411

Zastavnik F. Model leta helikoptera [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2010 [cited 2024 June 17] Available at: https://urn.nsk.hr/urn:nbn:hr:235:384411

F. Zastavnik, "Model leta helikoptera", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2010. Available at: https://urn.nsk.hr/urn:nbn:hr:235:384411

Metadata
TitleModel leta helikoptera
Title (english)Helicopter flight real-time simulation with level one model
AuthorFilip Zastavnik
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2010-05-21, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
U ovom radu izrađen je model leta helikoptera. Za dinamiku leta primijenjen je 6DOF model. Za model rotora koristi se analitički matemetički model koji je primjenjen na glavni rotor i, uz neke preinake, na repni rotor. Modelirani su i trup letjelice te vertikalni i horizontalni stabilizator. Cijeli model rađen je unutar MATLAB/Simulink okružja te je napravljeno povezivanje s FlightGear vizualizacijskom aplikacijom za simulaciju u stvarnom vremenu. Najvažnije komponente uspoređene su s podacima iz literature odnosno s drugim, verificiranim, modelima. Primjenjeni 6DOF model je verificiran s postojećim modelom. Model glavnog rotora je uspoređen s rezultatima modela po teoriji elementarnog kraka (BET) u lebdenju i horizontalnom letu. Model repnog rotora uspoređen je u lebdenju. Rezultati analize i usporedbe pokazuju dobra poklapanja. Manja odstupanja su objašnjena i svojstvena su korištenju analitičkog modela rotora.
Keywords
Languagecroatian
URN:NBNurn:nbn:hr:235:384411
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 20:34:13