prikaz prve stranice dokumenta Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona
Embargo period 2026-12-06
master's thesis
Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. urn:nbn:hr:235:659120
Rožić, Patrik
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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

Cite this document

Rožić, P. (2024). Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:659120

Rožić, Patrik. "Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:659120

Rožić, Patrik. "Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:659120

Rožić, P. (2024). 'Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 17 January 2025, https://urn.nsk.hr/urn:nbn:hr:235:659120

Rožić P. Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2024 [cited 2025 January 17] Available at: https://urn.nsk.hr/urn:nbn:hr:235:659120

P. Rožić, "Implementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2024. Available at: https://urn.nsk.hr/urn:nbn:hr:235:659120

Metadata
TitleImplementacija fly-by-wire sustava upravljanja na simulatoru leta modernog borbenog aviona
Title (english)Implementation of fly-by-wire flight controls on flight simulator for modern fighter airplane
AuthorPatrik Rožić
MentorMilan Vrdoljak (mentor)
MentorMarijan Andrić (komentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2024-12-06, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
U diplomskom radu prikazan je razvoj i izrada fly-by-wire (FBW) upravljačke palice koja koristi silu za određivanje zadanih komandi, za razliku od konvencionalnih palica koje mjere pomak. Opisan je proces kalibracije palice te prilagodba postojećeg Simulink model leta kako bi se palica mogla koristiti. Za procjenu primjenjivosti nove FBW palice, proveden je eksperiment s dvije skupine ispitanika koji je uključivao dva zadatka. Prvi zadatak sastojao se od praćenja zadanog kuta propinjanja, dok je u drugom zadatku potrebno pratiti zadani smjer leta. Izvedba je analizirana na dva načina. Objektivno, mjerenjem varijance pogreške od zadanih vrijednosti i mjerenjem broja ekstrema u signalu palice te subjektivno ispunjavanjem NASA-TLX upitnika i ocjenom upravljivosti prema Cooper-Harper ljestvici za ocjenu upravljivosti. Na kraju je prikazana usporedba ostvarenih varijanci pogreške s novom FBW palicom i konvencionalnom upravljačkom palicom.
Abstract (english)
The topic of this master’s thesis is the development and creation of a fly-by-wire (FBW) control stick that uses force to determine input commands, unlike conventional control sticks that measure displacement. The calibration process of the stick is described, as well as the adaptation of an existing Simulink flight simulation model to enable its use. To evaluate the applicability of the new FBW control stick, an experiment was conducted with two groups of participants, involving two tasks. The first task consisted of tracking a specified pitch angle, while the second required tracking a specified flight direction. Performance was analyzed in two ways. Objectively, by measuring the variance of error from predefined values and counting the number of extrema in the control stick signal and subjectively, through the completion of the NASA-TLX questionnaire and maneuverability assessment using the Cooper-Harper rating scale. Finally, a comparison of the error variance achieved with the new FBW control stick and the conventional control stick is shown.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:659120
Study programmeTitle: Aeronautical Engineering
Study programme type: university
Study level: graduate
Academic / professional title: sveučilišni/a magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (sveučilišni/a magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsEmbargoed access
Embargo expiration date: 2026-12-06
Terms of useLicence In copyright icon
Created on2024-11-29 15:18:54