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Reaction wheels for picosatellites
2009 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

Picosatellite is the name given to the category of satellites that ranges from 0.1 to 1 kg mass. A popular standardized format is the CubeSat which is a cubed shaped satellite measuring 10 cm on its sides. The objective of this thesis is to analyze the requirements for a wheel based ADCS (Attitude Determination and Control System) for a picosatellite using as much as possible COTS (commercial off the shelf) components and suggest a design to be used in the near future by the University's own CubeSat program. Results are obtained by testing and simulations.

Place, publisher, year, edition, pages
2009.
Keyword [en]
Technology, Attitude Control, Small Satellite, Cubesat, Picosatellite, COTS, ADCS, Reaction Wheel.
Keyword [sv]
Teknik
Identifiers
URN: urn:nbn:se:ltu:diva-44986ISRN: LTU-PB-EX--09/013--SELocal ID: 2bbd1025-4f82-445d-8cce-782201220427OAI: oai:DiVA.org:ltu-44986DiVA: diva2:1018265
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level
Examiners
Note
Validerat; 20101217 (root)Available from: 2016-10-04 Created: 2016-10-04Bibliographically approved

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CiteExportLink to record
Permanent link

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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