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master's thesis
Upravljački sustav bespilotne letjelice Aerosonde
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. urn:nbn:hr:119:066148
Nikolov, Marina
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

Nikolov, M. (2016). Upravljački sustav bespilotne letjelice Aerosonde (Master's thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:066148

Nikolov, Marina. "Upravljački sustav bespilotne letjelice Aerosonde." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:066148

Nikolov, Marina. "Upravljački sustav bespilotne letjelice Aerosonde." Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:066148

Nikolov, M. (2016). 'Upravljački sustav bespilotne letjelice Aerosonde', Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 27 June 2024, https://urn.nsk.hr/urn:nbn:hr:119:066148

Nikolov M. Upravljački sustav bespilotne letjelice Aerosonde [Master's thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2016 [cited 2024 June 27] Available at: https://urn.nsk.hr/urn:nbn:hr:119:066148

M. Nikolov, "Upravljački sustav bespilotne letjelice Aerosonde", Master's thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2016. Available at: https://urn.nsk.hr/urn:nbn:hr:119:066148

Metadata
TitleUpravljački sustav bespilotne letjelice Aerosonde
Title (english)Flight Control System Design for Aerosonde Unmanned Vehicle
AuthorMarina Nikolov
MentorKarolina Krajček Nikolić (mentor)
Committee memberErnest Bazijanac (predsjednik povjerenstva)
Committee memberDavor Franjković (član povjerenstva)
Committee memberDoris Novak (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2016-05-03, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Cilj ovog rada je analiza upravljačkog sustava bespilotne letjelice Aerosonde. Aerosonde je autonomna bespilotna letjelica s iznimnim svojstvima stabilnosti i upravljanja. Pomoću Aerosim Blockset-a određen je nelinearni model letjelice. Nelinearni model je uravnotežen i lineariziran za uzdužno i bočno gibanje. Koristeći linearni model letjelice provedena je analiza dinamičkih karakteristika uzdužnog i bočnog gibanja letjelice. Analizirana su dva sustava upravljanja, sustav upravljanja orijentacijom propinjanja u uzdužnom kanalu upravljanja koristeći linearnu dinamiku uzdužnog gibanja letjelice te sustav bočnog upravljanja i auto stabilizaciju koristeći linearnu dinamiku bočnog gibanja letjelice. Usporedbom stabilnosti i upravljivosti letjelice nakon uvođenja upravljačkog sustava sa stabilnosti i upravljivosti otvorene petlje primjetno je kako upravljački sustav stabilizira letjelicu i omogućava upravljivost.
Abstract (english)
The objective of this paper is design of a flight control system of Aerosonde unmanned aerial vehicle. Aerosonde is autonomous aerial vehicle with great stability and control characteristics. Firstly, the nonlinear 6-degree-of –freedom aircraft is developed using Aerosim Matlab/Simulink Blockset. Before applying flight control algorithm the nonlinear model is trimmed and linearized. Using the linearized aircraft model the analyses of aircraft dynamic characteristics are presented respectively in the longitudinal and lateral-directional senses. Two flight control systems are analyzed. Longitudinal Rate Command Attitude Hold is analyzed using the linear longitudinal dynamics. Lateral-Directional Auto-Stabilizer is analyzed using the linear lateral-directional dynamics. Comparing the stability and control before and after implement of the flight control system it is easy to notice how flight control manage to establish stability and control of aircraft.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:066148
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 on2016-05-06 13:40:27