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dc.contributor.advisorKaminer, I.
dc.contributor.authorChristofis, Alexandros.
dc.dateJune 1995
dc.date.accessioned2013-04-29T22:50:31Z
dc.date.available2013-04-29T22:50:31Z
dc.date.issued1995-06
dc.identifier.urihttp://hdl.handle.net/10945/31416
dc.description.abstractThe purpose of this thesis is to investigate using Global Positioning System (GPS) technology, for the guidance of an unmanned air vehicle (UAV) seeking precise navigation. Being fully operationally deployed by now, GPS is the indispensable tool for every application that requires precise positioning. By applying the Differential Positioning Technique, GPS becomes accurate to the point that its position and velocity outputs can be used as inputs to aflight control computer of a UAV. The Archytasen_US
dc.format.extent1 v. (various pagings)en_US
dc.language.isoen_US
dc.publisherMonterey, California. 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. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted.en_US
dc.titleOn design and analysis of a Differential Global Positioning System (DGPS) aided navigation system for an unmanned airborne vehicle [electronic resource]en_US
dc.typeThesisen_US
dc.contributor.departmentAeronautical Engineering
dc.description.funderNAen_US
dc.description.recognitionNAen_US
dc.description.serviceHellenic Navy author.en_US
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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