Electromechanical flight stabilization system for CubeSat nanosatellites
Electromechanical flight stabilization system for CubeSat nanosatellites
About this item
Full title
Author / Creator
Publisher
Universidad Nacional de Colombia
Journal title
Language
English
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Publication information
Publisher
Universidad Nacional de Colombia
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Scope and Contents
Contents
The objective of the research was to design and simulate a stabilization system for attitude control of CubeSat nanosatellites in LEO orbit. The electronic system was inside the mechanical system, designed in Proteus. The mechanical system was designed in SolidWorks, then a CubeSat 3U CAD was downloaded for simulation and finally, all CAD designs w...
Alternative Titles
Full title
Electromechanical flight stabilization system for CubeSat nanosatellites
Authors, Artists and Contributors
Author / Creator
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Primary Identifiers
Record Identifier
TN_cdi_doaj_primary_oai_doaj_org_article_7050834d88b74f9082030e8b1074a385
Permalink
https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_7050834d88b74f9082030e8b1074a385
Other Identifiers
ISSN
0012-7353
E-ISSN
2346-2183
DOI
10.15446/dyna.v91n234.115957
