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Decoupled Lateral Directional Flight Control System Design Using Eigenstructure Assignment Method

dc.contributor.advisorBhat, M S
dc.contributor.advisorReddy, B S
dc.contributor.authorDixit, Girish G
dc.date.accessioned2012-11-07T07:08:58Z
dc.date.accessioned2018-07-31T05:15:05Z
dc.date.available2012-11-07T07:08:58Z
dc.date.available2018-07-31T05:15:05Z
dc.date.issued2012-11-07
dc.date.submitted1997
dc.identifier.urihttps://etd.iisc.ac.in/handle/2005/1773
dc.identifier.abstracthttp://etd.iisc.ac.in/static/etd/abstracts/2306/G15051-Abs.pdfen_US
dc.language.isoen_USen_US
dc.relation.ispartofseriesG15051en_US
dc.subjectMilitary Aircraften_US
dc.subjectFlight Controlen_US
dc.subjectMilitary Airplanesen_US
dc.subjectEigenvaluesen_US
dc.subjectEigenvectorsen_US
dc.subjectEigenstructure Assignment Methoden_US
dc.subjectAircraft Lateral Directional Dynamicsen_US
dc.subjectFlight Control System (FCS)en_US
dc.subject.classificationAstronauticsen_US
dc.titleDecoupled Lateral Directional Flight Control System Design Using Eigenstructure Assignment Methoden_US
dc.typeThesisen_US
dc.degree.nameMSc Enggen_US
dc.degree.levelMastersen_US
dc.degree.disciplineFaculty of Engineeringen_US


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