Design and development of terminal phase flight control system for an unmanned air vehicle

dc.contributor.guideShanmugam Jen_US
dc.coverage.spatialDesign and development of terminal phase flight control system for an unmanned air vehicleen_US
dc.creator.researcherSenthil kumar Ken_US
dc.date.accessioned2014-12-24T05:51:19Z
dc.date.available2014-12-24T05:51:19Z
dc.date.awarded30/12/2008en_US
dc.date.completed01/12/2008en_US
dc.date.issued2014-12-24
dc.date.registeredn.d.en_US
dc.description.abstractThe ultimate aim of both military and commercial aviation is allweather newlineoperation To achieve this goal it should be possible to land the newlineaircraft without visual reference to the runway This can be accomplished by a newlinelanding system which will guide the aircraft down to a predetermined glide newlineslope and then at a preselected altitude reduce the rate of descent and cause newlinethe aircraft to flare out and touch down with an acceptably low rate of newlinedescent Aircraft has many flight phases but autolanding is a very challenging newlinetask among all aircraft flight phases since aircraft flies at a considerable low newlinealtitude and low speed during landing phase and any failure in this region will newlineresult in more accidents newline newlineen_US
dc.description.noteReference p.251-264en_US
dc.format.accompanyingmaterialNoneen_US
dc.format.dimensions23cmen_US
dc.format.extentxxxvii, 267p.en_US
dc.identifier.urihttp://hdl.handle.net/10603/31658
dc.languageEnglishen_US
dc.publisher.institutionFaculty of Electrical and Electronics Engineeringen_US
dc.publisher.placeChennaien_US
dc.publisher.universityAnna Universityen_US
dc.relationp.251-264en_US
dc.rightsuniversityen_US
dc.source.universityUniversityen_US
dc.subject.keywordair vehicleen_US
dc.subject.keywordelectrical engineeringen_US
dc.subject.keywordflight control systemen_US
dc.titleDesign and development of terminal phase flight control system for an unmanned air vehicleen_US
dc.title.alternativeen_US
dc.type.degreePh.D.en_US

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