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dc.contributor.advisorThaler, George J.
dc.contributor.authorBeck, Walter R.
dc.contributor.authorStuart, Donald B.
dc.date1962
dc.date.accessioned2013-01-23T21:58:51Z
dc.date.available2013-01-23T21:58:51Z
dc.date.issued1962
dc.identifier.urihttp://hdl.handle.net/10945/26367
dc.descriptionApproved for public release; distribution is unlimiteden_US
dc.description.abstractSince the advent of power electrical machinery, the problem of improved voltage regulation has always been a dominate factor. Recently, the Bendix Corporation has designed a new aircraft voltage regulator using transistorized components. This regulator was considered to be a non-linear degenerative feedback unit. Using the well defined procedures of servo analysis, dynamic and frequency response tests were taken of the regulator and the regulator-generator system. These tests were evaluated with a view toward developing a regulator describing function and a system function. The writers wish to express their appreciation for the assistance and time given them by Doctor George J. Thaler, of the U.S. Naval Postgraduate School in the experimental research of this paper.en_US
dc.description.urihttp://www.archive.org/details/analysisoftransi00beck
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.titleAn analysis of a transistorized aircraft voltage regulatoren_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentDepartment of Electrical Engineering
dc.description.serviceLieutenant, United States Navyen_US
etd.thesisdegree.nameM.S. in Electrical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineElectrical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


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