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Title:Samodejno pristajanje raketnega sistema z ventilatorskim pogonom in vektorskim usmerjanjem potiska : magistrsko delo
Authors:ID Kukovič, Uroš (Author)
ID Sarjaš, Andrej (Mentor) More about this mentor... New window
Files:.pdf MAG_Kukovic_Uros_2026.pdf (4,16 MB)
MD5: C8192E62D5CEBCA3E7ABABDD97FF99A7
 
Language:Slovenian
Work type:Master's thesis/paper
Typology:2.09 - Master's Thesis
Organization:FERI - Faculty of Electrical Engineering and Computer Science
Abstract:Magistrsko delo predstavlja razvoj in preizkus raketnega sistema za samodejno navpično pristajanje z uporabo električnega ventilatorskega pogona (EDF) in vektorskega usmerjanja potiska. Vključuje pregled obstoječih tehnologij, teorijo regulacije in praktično izdelavo prototipa. Poudarek je na načrtovanju mehanskih sklopov in implementaciji algoritmov za stabilizacijo. Sistem temelji na kaskadni arhitekturi regulatorjev. Rezultat je delujoč prototip, sposoben samodejnega lebdenja in kontroliranega pristanka. Delo prispeva k razvoju cenovno dostopnih raziskovalnih platform za testiranje tehnologij navpičnega pristajanja.
Keywords:navpično pristajanje, vektorsko usmerjanje potiska, kaskadna regulacija, stabilizacijski algoritmi, električni ventilatorski pogon
Place of publishing:Maribor
Place of performance:Maribor
Publisher:[U. Kukovič]
Year of publishing:2026
Number of pages:1 spletni vir (1 datoteka PDF (XII, 98 str.))
PID:20.500.12556/DKUM-97606 New window
UDC:681.51:629.76.077(043.2)
COBISS.SI-ID:278521603 New window
Publication date in DKUM:08.05.2026
Views:157
Downloads:27
Metadata:XML DC-XML DC-RDF
Categories:KTFMB - FERI
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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:24.03.2026

Secondary language

Language:English
Title:Autonomous landing of a rocket system using an electric ducted fan and thrust vector control
Abstract:The master's thesis presents the development and testing of a rocket system for autonomous vertical landing using an electric ducted fan (EDF) propulsion system and thrust vector control. It includes a review of existing technologies, control theory and the practical construction of a prototype. The focus is on the design of mechanical assemblies and the implementation of stabilization algorithms. The system is based on a cascaded controller architecture. The result is a functioning prototype capable of autonomous hovering and controlled landing. The thesis contributes to the development of cost-effective research platforms for testing vertical landing technologies.
Keywords:vertical landing, thrust vector control, cascaded control, stabilization algorithms, electric ducted fan


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