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Title:Stabilizacija fiksno-krilnega UAV-ja s kaskadno PID regulacijo
Authors:ID Pernek, Matjaž (Author)
ID Tič, Vito (Mentor) More about this mentor... New window
ID Šafarič, Riko (Mentor) More about this mentor... New window
ID Fister, Dušan (Comentor)
Files:.pdf MAG_Pernek_Matjaz_2026.pdf (5,61 MB)
MD5: 033832116B9894769770116429AD9481
 
Language:Slovenian
Work type:Master's thesis/paper
Typology:2.09 - Master's Thesis
Organization:FS - Faculty of Mechanical Engineering
Abstract:Magistrsko delo obravnava zasnovo, implementacijo in eksperimentalno verifikacijo sistema za stabilizacijo leta fiksno-krilnega UAV-ja s kaskadno PID-regulacijo. Cilj dela je bil razviti cenovno dostopen krmilnik leta, ki omogoča stabilizacijo po oseh nagiba in valjanja. V okviru dela so bili obravnavani temelji aerodinamike, dinamike leta in regulacije. Razvit je bil lasten krmilnik leta na tiskanem vezju in izdelan mehanski simulator leta. Delovanje sistema je bilo preverjeno z laboratorijskimi testi, zemeljskimi testi in letalskimi preizkusi.
Keywords:Brezpilotno letalo, UAV, zrakoplov, kaskadna regulacija, stabilizacija leta
Place of publishing:Maribor
Year of publishing:2026
PID:20.500.12556/DKUM-99827 New window
Publication date in DKUM:28.09.2026
Views:12
Downloads:1
Metadata:XML DC-XML DC-RDF
Categories:KTFMB - FS
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Licences

License:CC BY-NC-ND 4.0, Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International
Link:http://creativecommons.org/licenses/by-nc-nd/4.0/
Description:The most restrictive Creative Commons license. This only allows people to download and share the work for no commercial gain and for no other purposes.
Licensing start date:27.08.2026

Secondary language

Language:English
Title:Stability of a fixed-wing UAV with a cascade PID regulator
Abstract:The master’s thesis presents the design, implementation, and experimental verification of a flight stabilization system for a fixed-wing UAV using cascade PID control. The objective was to develop a cost-effective flight controller capable of stabilizing the UAV in pitch and roll. The work covers the fundamentals of aerodynamics, flight dynamics, and control theory. A custom flight controller was developed on a printed circuit board and a mechanical Fly Rig simulator was built. The system was verified through laboratory tests, ground tests, and real flight tests.
Keywords:Unmanned aerial vehicle, UAV, plane, cascade regulator, flight stabilization


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