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dc.contributor.authorAponso, Gayanath
dc.contributor.authorChakravarthy, Animesh
dc.date.accessioned2013-11-18T19:49:41Z
dc.date.available2013-11-18T19:49:41Z
dc.date.issued2013-11-18
dc.date.published2013en_US
dc.description.abstractIn this work, we provide details of the control design of a morphing UAV capable of variable wing sweep. This morphing capability is assumed to be superimposed on a GENMAV (Generic Micro Air Vehicle) configuration originally developed by the Air Force Research Laboratory (AFRL). The nonlinear aerodynamic model for this aircraft is obtained using the Athena-Vortex Lattice (AVL) method with a quasi-steady state assumption.en_US
dc.description.conferenceKansas Unmanned Systems Conference, Manhattan, KS, October 14-16, 2013en_US
dc.identifier.urihttp://hdl.handle.net/2097/16814
dc.language.isoen_USen_US
dc.publisherKansas State Universityen_US
dc.subjectAerodynamicsen_US
dc.subjectMorphingen_US
dc.subjectUnmanned air vehiclesen_US
dc.titleController design for a nonlinear morphing UAVen_US
dc.typeTexten_US

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