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dc.contributor.advisorTitus, Howard A.
dc.contributor.authorCostello, Patrick.
dc.dateMarch 1995
dc.date.accessioned2013-04-29T22:51:20Z
dc.date.available2013-04-29T22:51:20Z
dc.date.issued1995-03
dc.identifier.urihttps://hdl.handle.net/10945/31532
dc.description.abstractProportional Navigation and Command To Line Of Sight missile guidance are explored. A system flow graph is developed for each guidance technique. The block transfer functions are developed and a state space representation of the system is defined. The missile systems are then tested using one two-dimensional engagement and two three-dimensional engagement scenarios. The final three- dimensional scenario introduces measurement noise in order to evaluate the effect of noise on the guidance algorithms. The engagement results are then compared to analyze the miss distance of each type of missile guidance.en_US
dc.description.urihttp://archive.org/details/simulinksimulati1094531532
dc.format.extent81 p.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. Copyright protection is not available for this work in the United States.en_US
dc.titleSimulink simulation of proportional navigation and command to line of sight missile guidanceen_US
dc.typeThesisen_US
dc.contributor.departmentElectrical Engineering
dc.description.funderNAen_US
dc.description.recognitionNAen_US
dc.description.serviceU.S. Navy (U.S.N.) author.en_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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