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dc.contributor.authorGryte, Kristoffer
dc.contributor.authorHansen, Jakob Mahler
dc.contributor.authorJohansen, Tor Arne
dc.contributor.authorFossen, Thor I.
dc.date.accessioned2018-01-04T14:16:38Z
dc.date.available2018-01-04T14:16:38Z
dc.date.created2017-11-01T14:34:15Z
dc.date.issued2017
dc.identifier.citationAIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum. 2017, 1035.nb_NO
dc.identifier.isbn978-1-62410-450-3
dc.identifier.urihttp://hdl.handle.net/11250/2475764
dc.description.abstractTight integration of ultra wideband (UWB) range measurements with real-time kinematic (RTK) aiding of inertial navigation for increased robustness to GNSS dropouts, is achieved using a double-differenced nonlinear observer. A stationary base station provides additional GNSS range measurements, upon which a double-differenced observer is formulated. The results are verified using a simulated unmanned aerial vehicle (UAV) with realistic inertial, GNSS and UWB measurements.nb_NO
dc.language.isoengnb_NO
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)nb_NO
dc.relation.ispartofAIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum
dc.relation.urihttp://folk.ntnu.no/torarnj/AIAA_Gryte_2017.pdf
dc.titleRobust Navigation of UAV using Inertial Sensors Aided by UWB and RTK GPSnb_NO
dc.typeChapternb_NO
dc.description.versionacceptedVersionnb_NO
dc.identifier.doi10.2514/6.2017-1035
dc.identifier.cristin1509861
dc.relation.projectNorges forskningsråd: 223254nb_NO
dc.description.localcode©2017 AIAA. This is the authors' accepted version of the manuscript.nb_NO
cristin.unitcode194,63,25,0
cristin.unitnameInstitutt for teknisk kybernetikk
cristin.ispublishedtrue
cristin.fulltextpostprint
cristin.qualitycode1


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