Strategies for the control of a satellite with thruster misalignment

dc.contributor.advisorTreurnicht, J.
dc.contributor.authorVan Daalen, Corne E.en_ZA
dc.contributor.otherUniversity of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering.
dc.date.accessioned2006-11-16T06:27:45Zen_ZA
dc.date.accessioned2010-06-01T08:45:39Z
dc.date.available2006-11-16T06:27:45Zen_ZA
dc.date.available2010-06-01T08:45:39Z
dc.date.issued2006-03en_ZA
dc.descriptionThesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2006.
dc.description.abstractThis project investigates two problems related to satellites that contain cold gas thrusters and reaction wheels. The first problem concerns the estimation of the thruster force response to a pulse command. An optimal data integration method is developed and implemented to estimate the thruster force output from a number of noisy sensors. The second problem occurs when the output force vector of a thruster mounted on a satellite is misaligned with the centre of mass with the satellite. As a result a disturbance torque is generated on the satellite during thruster operation.en_ZA
dc.format.extent2339796 bytesen_ZA
dc.format.mimetypeapplication/pdfen_ZA
dc.identifier.urihttp://hdl.handle.net/10019.1/2306
dc.language.isoen_ZAen_ZA
dc.publisherStellenbosch : University of Stellenbosch
dc.rights.holderUniversity of Stellenbosch
dc.subjectArtificial satellites -- Control systemsen_ZA
dc.subjectArtificial satellites -- Propulsion systemsen_ZA
dc.subjectDissertations -- Electronic engineeringen_ZA
dc.subjectTheses -- Electronic engineeringen_ZA
dc.subject.otherElectrical and Electronic Engineeringen_ZA
dc.titleStrategies for the control of a satellite with thruster misalignmenten_ZA
dc.typeThesisen_ZA
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