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master's thesis
Projektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2023. urn:nbn:hr:235:721814
Perica, Ante
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

Perica, A. (2023). Projektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:721814

Perica, Ante. "Projektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2023. https://urn.nsk.hr/urn:nbn:hr:235:721814

Perica, Ante. "Projektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2023. https://urn.nsk.hr/urn:nbn:hr:235:721814

Perica, A. (2023). 'Projektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 29 November 2024, https://urn.nsk.hr/urn:nbn:hr:235:721814

Perica A. Projektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2023 [cited 2024 November 29] Available at: https://urn.nsk.hr/urn:nbn:hr:235:721814

A. Perica, "Projektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2023. Available at: https://urn.nsk.hr/urn:nbn:hr:235:721814

Metadata
TitleProjektiranje sustava upravljanja autonomne bespilotne letjelice i njegova provjera primjenom simulacije leta
Title (english)Control system design for autonomus unmanned aerial vehicle and its review with flight simulation application
AuthorAnte Perica
MentorMilan Vrdoljak (mentor)
Committee memberIvica Smojver (predsjednik povjerenstva)
Committee memberDarko Ivančević (član povjerenstva)
Committee memberJosip Stepanić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2023-01-25, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Control
Abstract
U ovom diplomskom radu projektirali su se sustavi stabilizacije uzdužnog i bočnog gibanja te sustavi upravljanja smjerom i visinom leta s ciljem postizanja autonomnog leta. Letjelica za koju su sustavi projektirani je konfiguracije letećeg krila nazvana Salus. Na početku rada dani su svi potrebni podaci o letjelici. Zatim su se odredile aerodinamičke značajke na dva različita načina, projektnom metodom i numeričkom metodom. Sljedeći korak bio je izrada lineariziranog modela letjelice, te njegova implementacija u sustave stabilizacije napravljene u programu Simulink. Nakon uspješne implementacije linearnog modela u projektirane sustave stabilizacije, pristupilo se izradi sustava upravljanja letjelice, odnosno navođenja letjelice. Kao posljednji korak su se ti sustavi upravljanja implementirali u 6DOF model leta letjelice i napravljena je simulacija u stvarnom vremenu pomoću programa za vizualizaciju FlightGear. U konačnici su se rezultati dobiveni simulacijom za zadanu putanju leta prikazali pomoću grafova.
Abstract (english)
In this master thesis, longitudinal and lateral motion stabilization systems were designed as well as flight direction and altitude control systems with the aim of achieving autonomous flight. The aircraft for which the systems were designed is a flying wing configuration called the Salus. At the beginning of the thesis, all the necessary information about the aircraft is given. Then, the aerodynamic features were determined in two different ways, the design method and the numerical method. The next step was the creation of a linearized model of the aircraft, and its implementation in the stabilization systems created in the Simulink program. After the successful implementation of the linearized model in the designed stabilization systems, the design of the aircraft control system, i.e. the aircraft's guidance system, began. As a final step, these control systems were implemented in a 6DOF flight model of the aircraft and a real-time simulation was made using the FlightGear visualization program. Finally, the results obtained from the simulation for the given flight path were presented using graphs.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:721814
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 on2023-01-26 11:26:35