Return to search

Control moment gyro actuator for small satellite applications

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005. / The 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.

Identiferoai:union.ndltd.org:netd.ac.za/oai:union.ndltd.org:sun/oai:scholar.sun.ac.za:10019.1/2144
Date03 1900
CreatorsBerner, Reimer
ContributorsSteyn, W. H., University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering.
PublisherStellenbosch : University of Stellenbosch
Source SetsSouth African National ETD Portal
LanguageEnglish
Detected LanguageEnglish
TypeThesis
Format2558800 bytes, application/pdf
RightsUniversity of Stellenbosch

Page generated in 0.0022 seconds