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undergraduate thesis
Projektiranje male bespilotne letjelice s fiksnim krilima
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. urn:nbn:hr:119:009314
Ribić, David
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Institutional repository: Faculty of Transport and Traffic Sciences

Cite this document

Ribić, D. (2016). Projektiranje male bespilotne letjelice s fiksnim krilima (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:009314

Ribić, David. "Projektiranje male bespilotne letjelice s fiksnim krilima." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:009314

Ribić, David. "Projektiranje male bespilotne letjelice s fiksnim krilima." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:009314

Ribić, D. (2016). 'Projektiranje male bespilotne letjelice s fiksnim krilima', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 22 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:009314

Ribić D. Projektiranje male bespilotne letjelice s fiksnim krilima [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2016 [cited 2024 December 22] Available at: https://urn.nsk.hr/urn:nbn:hr:119:009314

D. Ribić, "Projektiranje male bespilotne letjelice s fiksnim krilima", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2016. Available at: https://urn.nsk.hr/urn:nbn:hr:119:009314

Metadata
TitleProjektiranje male bespilotne letjelice s fiksnim krilima
Title (english)Design of a Small Fixed Wing Unmanned Aerial Vehicle
AuthorDavid Ribić
MentorKarolina Krajček Nikolić (mentor)
Committee memberAnita Domitrović (predsjednik povjerenstva)
Committee memberDavor Franjković (član povjerenstva)
Committee memberŽeljko Marušić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2016-09-13, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Construction and Design
Abstract
U radu je opisan postupak izrade bespilotne letjelice. Cilj je projektiranje bespilotne letjelice i provođenje računske potvrde o njezinim performansama. Ovaj pristup omogućava studentima upoznavanje s osnovama gradnje letjelice te rješavanje konstruktivnih i aerodinamičkih problema tijekom izrade. Za izradu letjelice korištena je kompozitna struktura koja je zahtjevnija s obzirom na proces proizvodnje. Proces započinje s idejom koja se dokazuje proračunom aerodinamičkih karakteristika i osnovnih performansi zrakoplova uz testiranje prototipa. Model letjelice upravljan je preko radio frekvencijskog uređaja. Za pogon letjelice korišten je elektro-ventilatorski motor koji može imati sustav naknadnoga izgaranja zapaljivog plina te servomotori za upravljanje komandnim površinama. Dobivene performanse su zadovoljavajuće uz maksimalnu brzinu horizontalnoga leta od 25 m/s jer da letjelica ima malu i slabu pogonsku grupu. Izračunate performanse uspoređene su s rezultatima dobivenim testiranjem slobodno letećeg modela pri čemu je bitno uzeti u obzir faktor točnosti izrade modela.
Abstract (english)
In this paper is a description on how to make an unmaned aircraft vehicle. The goal of this project is to design and mathematically verify a model plane performance. This allows for students to familiarize with basics of building an aircraft and resolving structural and aerodynamic problems. Composite materials are used for the structure, this tipe of material is most complex due to it's manufacturing process. In building a plane, the proces begins with an idea wich is matemathically tested. After that follows the free flying model test wich is used for canceling all problem for the build of the finall product. The aircraft is controlled via remote controll. The powerplant is an electric ducted fan motor with possible afterburning butane gas to increase thrust. The performance of this aircraft are relatively good with a maximum speed of 25 m/s since it's a small aircraft with a small and weak powerplant. After geting the mathematicall performance they are compared with real performance given in the flight of the aircraft.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:009314
Study programmeTitle: Aeronautics
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2016-09-19 10:35:59