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dc.contributor.advisorThaler, George J.
dc.contributor.authorMacNamara, M. A. S.
dc.dateMarch 1975
dc.date.accessioned2012-11-20T00:26:21Z
dc.date.available2012-11-20T00:26:21Z
dc.date.issued1975-03
dc.identifier.urihttp://hdl.handle.net/10945/20963
dc.descriptionApproved for public release; distribution is unlimited
dc.description.abstractAn investigation of a method for finding an optimum compensator for use in an autopilot is described. Given a structure with a number of real poles and zeros which is steady-state decoupled, the pole-zero locations are chosen to give a system response as close as possible to a desired response. The desired response can be any one or a combination of system outputs. The computer is used to optimize the pole-zero locations by means of a function minimization program.
dc.description.urihttp://archive.org/details/newparameteropti00macn
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsCopyright is reserved by the copyright owner
dc.subject.lcshAeronauticsen_US
dc.titleA new parameter optimization method applied to autopilot design.en_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentAeronautical Engineering
dc.description.serviceMajor, Canadian Forces
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


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