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dc.contributor.authorTaamallah, S.en_US
dc.date.accessioned2013-11-11T09:11:54Z
dc.date.available2013-11-11T09:11:54Z
dc.date.issued2010en_US
dc.identifier.otherNLR-TP-2010-286-PT-1en_US
dc.identifier.urihttp://hdl.handle.net/10921/909
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2010-286-PT-1en_US
dc.subject.otherUnmanned aircraft systems (UAS)en_US
dc.subject.otherHelicoptersen_US
dc.titleA Flight Dynamics Helicopter UAV Model For A Single Pitch-Lag-Flap Main Rotor: Modeling & Simulationsen_US


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