| | SLO | ENG | Cookies and privacy

Bigger font | Smaller font

Show document Help

Title:Sistem za zaznavo in nadzor orientacije nanosatelita na osnovi magnetnega navora : magistrsko delo
Authors:ID Gonzales, Lorenzo (Author)
ID Kramberger, Iztok (Mentor) More about this mentor... New window
ID Rotovnik, Tomaž (Comentor)
Files:.pdf MAG_Gonzales_Lorenzo_2020.pdf (3,34 MB)
MD5: 81A8B3E73FFB833D970484315952939A
PID: 20.500.12556/dkum/5f400818-40b6-425f-bcc7-07e60f6f1963
 
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 okvirju zaključnega dela je predstavljen sistem za zaznavo in nadzor orientacije nanosatelita primarno razvit za misijo TRISAT-R, ki za orientiranje uporablja magnetne navornike. V sklopu dela so predstavljeni postopki za reguliranje magnetnih vzbujevalnikov tako za umirjanje satelita kot za usmerjanje satelita proti Soncu. Predstavljena je zasnova, načrtovanje in končna sestava sistema skupaj z uporabljenimi algoritmi. Dodatno je predstavljen simulator za propagacijo orbitnih in orientacijskih parametrov, znotraj katerega so primarno preverjeni regulacijski postopki implementirani na sistemu. Na koncu dela pa so predstavljene meritve komponent sistema in njegovo delovanje.
Keywords:nanosatelit, zaznava orientacije, nadzor orientacije, magnetni navornik, vgrajeni sistem
Place of publishing:Maribor
Place of performance:Maribor
Publisher:[L. Gonzales]
Year of publishing:2020
Number of pages:X, 84 f.
PID:20.500.12556/DKUM-77415 New window
UDC:621.398:629.783(043.2)
COBISS.SI-ID:43378435 New window
NUK URN:URN:SI:UM:DK:1WNYB47V
Publication date in DKUM:01.12.2020
Views:1224
Downloads:58
Metadata:XML DC-XML DC-RDF
Categories:KTFMB - FERI
:
Copy citation
  
Average score:(0 votes)
Your score:Voting is allowed only for logged in users.
Share:Bookmark and Share



Hover the mouse pointer over a document title to show the abstract or click on the title to get all document metadata.

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:30.08.2020

Secondary language

Language:English
Title:Magnetorquer-Based attitude determination and control system for nanosatellites
Abstract:In the scope of master thesis, a magnetorquer based attitude determination and control system is presented, which was primarily developed for the TRISAT-R nanosatellite mission. The thesis presents procedures for magnetorquer based regulation intended for satellite detumbling and sun pointing. Design, planning and final assembly of the system is described along with the used control algorithms. Additionally, a simulator with simultaneous orbital and attitude propagation of the satellites parameters is presented and its use for verification of developed regulations used on the described nanosatellite subsystem. Finally, measurements of system components are presented, and functionality of the system is verified.
Keywords:nanosatellite, attitude determination, attitude control, magnetorquer, embedded system


Comments

Leave comment

You must log in to leave a comment.

Comments (0)
0 - 0 / 0
 
There are no comments!

Back
Logos of partners University of Maribor University of Ljubljana University of Primorska University of Nova Gorica