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dc.contributor.advisorFossen, Thor Inge
dc.contributor.authorFurseth, Jostein
dc.date.accessioned2019-09-11T11:43:54Z
dc.date.created2015-06-22
dc.date.issued2015
dc.identifierntnudaim:12722
dc.identifier.urihttp://hdl.handle.net/11250/2616137
dc.description.abstractA simulator for the complete vehicle dynamics, as well as a flight control system, have been implemented in MATLAB/Simulink. The simulator enables easier development and testing of the control system, and provides valuable estimates of the total system performance. A physical prototype for concept validation is under development.en
dc.languageeng
dc.publisherNTNU
dc.subjectKybernetikk og robotikken
dc.titleModeling and Control of VTOL Flying Wing with Thrust Vectoringen
dc.typeMaster thesisen
dc.source.pagenumber141
dc.contributor.departmentNorges teknisk-naturvitenskapelige universitet, Fakultet for informasjonsteknologi og elektroteknikk,Institutt for teknisk kybernetikknb_NO
dc.date.embargoenddate10000-01-01


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