Control moment gyro actuator for small satellite applications

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dc.contributor.advisorSteyn, W. H.
dc.contributor.authorBerner, Reimeren_ZA
dc.contributor.otherUniversity of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering.
dc.date.accessioned2006-11-01T06:00:00Zen_ZA
dc.date.accessioned2010-06-01T08:41:24Z
dc.date.available2006-11-01T06:00:00Zen_ZA
dc.date.available2010-06-01T08:41:24Z
dc.date.issued2005-03en_ZA
dc.descriptionThesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005.
dc.description.abstractThe aim of the thesis is to design a Control Moment Gyro (CMG) actuator which can be used in small satellite applications. The hardware and software of the CMG has to be designed according to specifications given. A satellite fitted with these CMGs has to be able to do a 30 degree rotation within 10 seconds.en_ZA
dc.format.extent2558800 bytesen_ZA
dc.format.mimetypeapplication/pdfen_ZA
dc.identifier.urihttp://hdl.handle.net/10019.1/2144
dc.language.isoenen_ZA
dc.publisherStellenbosch : University of Stellenbosch
dc.rights.holderUniversity of Stellenbosch
dc.subjectActuatorsen_ZA
dc.subjectArtificial satellites -- Automatic controlen_ZA
dc.subjectArtificial satellites -- Control systemsen_ZA
dc.subjectDissertations -- Electronic engineeringen_ZA
dc.subjectTheses -- Electronic engineeringen_ZA
dc.subject.otherElectrical and Electronic Engineeringen_ZA
dc.titleControl moment gyro actuator for small satellite applicationsen_ZA
dc.typeThesisen_ZA
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