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Title:Vektorsko vodenje zračne potisne sile togo vpetega pogona : diplomsko delo
Authors:ID Kukovič, Uroš (Author)
ID Sarjaš, Andrej (Mentor) More about this mentor... New window
ID Karner, Timi (Mentor) More about this mentor... New window
Files:.pdf VS_Kukovic_Uros_2023.pdf (23,88 MB)
MD5: 12061BBF7CBBF73533F237F49EDDE410
 
Language:Slovenian
Work type:Bachelor thesis/paper
Typology:2.11 - Undergraduate Thesis
Organization:FERI - Faculty of Electrical Engineering and Computer Science
Abstract:Diplomsko delo obravnava vektorsko vodenje potiska zračnega ventilatorja, ki vpliva na naklon celotnega mehanizma. Vektorsko vodenje se doseže z nagibnim mehanizmom (ang. gimbal) in se uporablja v letalstvu s poudarkom na vojaških bojnih letalih za povečanje okretnosti letalskega plovila. Opisani koncepti se lahko uporabijo tudi kot podlaga za izvedbo vektorskega vodenja raketnega pogona. Diplomsko delo zavzema opis koncepta vektorskega vodenja s primeri 3D modeliranja mehanizma. Nazadnje obsega še sintezo zaprto-zančnega sistema in njegovo implementacijo. Rezultati prikazujejo učinkovitost vektorskega vodenja za povečanje okretnosti letalnega sistema.
Keywords:vektorsko vodenje, zračni potisk, letalstvo, okretnost, zaprto-zančni sistem
Place of publishing:Maribor
Place of performance:Maribor
Publisher:[U. Kukovič]
Year of publishing:2023
Number of pages:1 spletni vir (1 datoteka PDF (XIII, 80 f.))
PID:20.500.12556/DKUM-85167 New window
UDC:629.7.035.7(043.2)
COBISS.SI-ID:170666499 New window
Publication date in DKUM:05.10.2023
Views:514
Downloads:62
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:21.08.2023

Secondary language

Language:English
Title:An air thrust vector control of a rigidly mounted propulsion system
Abstract:The thesis addresses the thrust vector control of an air fan, which affects the inclination of the entire mechanism. Thrust vector control is accomplished by a thrust vectoring mechanism (gimbal) and is used in aviation, especially in military fighter jets for enhancing the maneuverability of the aircraft. The concepts described can also be used as a foundation for designing thrust vector control with rocket propulsion systems. The thesis contains a description of the thrust vector control concept with examples of 3D modeling. Lastly, it includes the design and implementation of a closed-loop system. The results demonstrate the effectiveness of thrust vector control in increasing the maneuverability of the aircraft.
Keywords:thrust vector control, air thrust, aviation, maneuverability, closed-loop system


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