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dc.contributor.advisorRekoff, Michael G.
dc.creatorSellers, Donald Franklin
dc.date.accessioned2020-01-08T18:14:57Z
dc.date.available2020-01-08T18:14:57Z
dc.date.created1967
dc.date.issued1966
dc.identifier.urihttps://hdl.handle.net/1969.1/DISSERTATIONS-180919
dc.description.abstractThis report describes the results of a research program to investigate a new type of satellite attitude controller. It is a momentum exchange device and will be referred to as the VMED (Vibrating Momentum Exchange Device). An analytical study was conducted to determine its expected operating characteristics. A single axis unit comprised of the VMED and the associated electronics was designed and constructed. An experimental program involving a closed loop simulation was conducted to verify the concept. The results were generally favorable and demonstrated that the VMED was able to change the angular position of an air bearing table in a controlled manner.en
dc.format.extent84 leaves : illustrationsen
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.subjectElectrical Engineeringen
dc.titleInvestigation of a vibrating momentum exchange deviceen
dc.typeThesisen
thesis.degree.disciplineElectrical Engineeringen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameDoctor of Philosophyen
thesis.degree.levelDoctoralen
dc.contributor.committeeMemberBarnard, Herbert M.
dc.contributor.committeeMemberBasye, Robert E.
dc.type.genredissertationsen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen
dc.publisher.digitalTexas A&M University. Libraries


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