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Title:
Razvoj simulatorja kinematike satelita za zemeljske tirnice
Authors:
ID
Volk, Jernej
(Author)
ID
Strnad, Damjan
(Mentor)
More about this mentor...
ID
Kramberger, Iztok
(Comentor)
Files:
MAG_Volk_Jernej_2024.pdf
(1,74 MB)
MD5: BBCCF408FE9B01A1E0009A20B025EE50
Language:
Slovenian
Work type:
Master's thesis/paper
Typology:
2.09 - Master's Thesis
Organization:
FERI - Faculty of Electrical Engineering and Computer Science
Abstract:
V magistrskem delu opišemo postopek izdelave simulatorja kinematike satelita za zemeljske tirnice. Najprej predstavimo teoretično ozadje simulatorja, kamor spada opis vektorja stanja satelita in njegovega spreminjanja skozi čas. V naslednjem poglavju opišemo cilje in arhitekturo programske opreme ter njeno uporabo. V predzadnjem poglavju predstavimo končen produkt tega dela. Prikažemo in obrazložimo grafe, ki prikazujejo potek simulacije. V zaključku povzamemo glavne ugotovitve in predstavimo možnosti za nadalnje delo.
Keywords:
simulacija
,
satelit
,
vesolje
,
senzor
,
aktuator
Place of publishing:
Maribor
Publisher:
[J. Volk]
Year of publishing:
2024
PID:
20.500.12556/DKUM-90581
UDC:
681.782.8:629.783(043.2)
COBISS.SI-ID:
224473603
Publication date in DKUM:
22.10.2024
Views:
0
Downloads:
35
Metadata:
Categories:
KTFMB - FERI
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:
VOLK, Jernej, 2024,
Razvoj simulatorja kinematike satelita za zemeljske tirnice
[online]. Master’s thesis. Maribor : J. Volk. [Accessed 23 April 2025]. Retrieved from: https://dk.um.si/IzpisGradiva.php?lang=eng&id=90581
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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:
09.09.2024
Secondary language
Language:
English
Title:
Development of a satellite kinematics simulator for Earth orbits
Abstract:
In the master’s thesis, we describe the process of creating a satellite kinematics simulator for Earth orbits. First, we present the theoretical background of the simulator, where we describe the state vector of the satellite and how it changes over time. In the next chapter, we describe the objectives and architecture of the software and its use. In the penultimate chapter we present the final product of this work. We show and explain the graphs that show the course of the simulation. In the conclusion, we summarize the main findings and present the possibilities for further work.
Keywords:
simulation
,
satellite
,
space
,
sensor
,
actuator
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