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master's thesis
Linearni model i analiza upravljivosti bespilotne letjelice s kanardima
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. urn:nbn:hr:119:979026
Cvetković, Nikola
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

Cvetković, N. (2017). Linearni model i analiza upravljivosti bespilotne letjelice s kanardima (Master's thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:979026

Cvetković, Nikola. "Linearni model i analiza upravljivosti bespilotne letjelice s kanardima." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:979026

Cvetković, Nikola. "Linearni model i analiza upravljivosti bespilotne letjelice s kanardima." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:979026

Cvetković, N. (2017). 'Linearni model i analiza upravljivosti bespilotne letjelice s kanardima', Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 22 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:979026

Cvetković N. Linearni model i analiza upravljivosti bespilotne letjelice s kanardima [Master's thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2017 [cited 2024 December 22] Available at: https://urn.nsk.hr/urn:nbn:hr:119:979026

N. Cvetković, "Linearni model i analiza upravljivosti bespilotne letjelice s kanardima", Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2017. Available at: https://urn.nsk.hr/urn:nbn:hr:119:979026

Metadata
TitleLinearni model i analiza upravljivosti bespilotne letjelice s kanardima
Title (english)Linear Model and Flying Qualities of an Unmanned Aerial Vehicle with Canard Configurationan Unmanned Aerial Vehicle with Canard Configuration
AuthorNikola Cvetković
MentorKarolina Krajček Nikolić (mentor)
Committee memberAnita Domitrović (predsjednik povjerenstva)
Committee memberDavor Franjković (član povjerenstva)
Committee memberErnest Bazijanac (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2017-09-26, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
U ovom diplomskom radu izračunate su aerodinamičke karakteristike bespilotne letjelice. Dobivene aerodinamičke karakteristike dalje se koriste za statičku analizu stabilnosti, uzdužnu i bočnu. Koristeći podatke iz statičkih analiza i XFLR5 softvera, određuje se linearni model gibanja letjelice. Pomoću linearnog modela letjelice izvršena je dinamička analiza letjelice i analiza odziva sustava na pobudu. Za kraj je određena kvaliteta upravljanja letjelicom prema MIL-F-8785C standardu. Dobiveni rezultati prikazani su analitički i grafički radi lakšeg razumijevanja.
Abstract (english)
Aerodynamic characteristics of an unmanned aerial vehicle are calculated in this thesis. Calculated data is then used for longitudinal and lateral static stability analysis. Data obtained from static analyses and XFLR5 software is then used to determine linear model of an unmanned aerial vehicle. Modal response graphs and dynamic stability analyses were conducted utilizing the linear model of an unmanned aerial vehicle. Finally, control quality was determined according to MIL-F-8785C standard, also by using the linear model of an unmanned aerial vehicle. Results of every analysis are given in mathematical and graphical form for better understanding.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:979026
Study programmeTitle: Aeronautics
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka aeronautike (magistar/magistra inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2017-11-24 14:59:20