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Design and fabrication of test-bed for testing attitude determination of spin stablilized spacecraft.
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology. (Space Master)
2017 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

 Attitude determination for a spin stabilized satellite is calibrated. A mock spacecraft and a spin simulation test bed are designed and developed. Spin simulation testbed which provides position data is used to acquire true position data. The data from the simulator test bed is used as reference for the sensor data to estimate the error in position of sensor data. Two vector method attitude solutions are used here for attaining the estimated position. Two vectors used for attitude determination are magnetic field vector and sun sensor vector. Calibration of accuracy for sensors is main goal, which is attained by calculating error by comparing the estimated position with true position.

Place, publisher, year, edition, pages
2017. , 99 p.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:ltu:diva-62223OAI: oai:DiVA.org:ltu-62223DiVA: diva2:1077742
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level (120 credits)
Presentation
2017-01-10, 52, JMUW, Wurzburg, 23:07 (English)
Supervisors
Examiners
Available from: 2017-03-07 Created: 2017-02-28 Last updated: 2017-03-07Bibliographically approved

Open Access in DiVA

fulltext(5942 kB)106 downloads
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Type fulltextMimetype application/pdf

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CiteExportLink to record
Permanent link

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Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf