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dc.contributor.advisorThaler, G.J.
dc.contributor.authorNutting, Roger M.
dc.date.accessioned2012-08-29T23:34:18Z
dc.date.available2012-08-29T23:34:18Z
dc.date.issued1965
dc.identifier.urihttps://hdl.handle.net/10945/12804
dc.description.abstractApproved for public release; distribution unlimited.en_US
dc.description.abstractParameter plane techniques were first introduced in an IEEE paper dated November 4, 1964. The paper dealt mainly with the theory of the parameter plane whereby the roots of a polynomial could be determined graphically in terms of two parameters which may appear linearly in any of the coefficients. In this text, parameter plane techniques are applied to the compensation of linear feedback control systems by both graphical and analytical means. Parameter plane equations are extended to include parameter products and three parameters. An attempt is made to show the complementary roles of the parameter plane and root locus. The writer wishes to express his appreciation for the assistance and guidance given him by Dr. G. J. Thaler of the U. S. Naval Postgraduate School in this investigation.en_US
dc.description.urihttp://archive.org/details/parameterplanete1094512804
dc.language.isoen_US
dc.publisherMonterey, California: U.S. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleParameter plane techniques for feedback control systemsen_US
dc.typeThesisen_US
dc.contributor.departmentElectrical 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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