dc.contributor.author | Gryte, Kristoffer | |
dc.contributor.author | Hansen, Jakob Mahler | |
dc.contributor.author | Johansen, Tor Arne | |
dc.contributor.author | Fossen, Thor I. | |
dc.date.accessioned | 2018-01-04T14:16:38Z | |
dc.date.available | 2018-01-04T14:16:38Z | |
dc.date.created | 2017-11-01T14:34:15Z | |
dc.date.issued | 2017 | |
dc.identifier.citation | AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum. 2017, 1035. | nb_NO |
dc.identifier.isbn | 978-1-62410-450-3 | |
dc.identifier.uri | http://hdl.handle.net/11250/2475764 | |
dc.description.abstract | Tight 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.iso | eng | nb_NO |
dc.publisher | American Institute of Aeronautics and Astronautics (AIAA) | nb_NO |
dc.relation.ispartof | AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum | |
dc.relation.uri | http://folk.ntnu.no/torarnj/AIAA_Gryte_2017.pdf | |
dc.title | Robust Navigation of UAV using Inertial Sensors Aided by UWB and RTK GPS | nb_NO |
dc.type | Chapter | nb_NO |
dc.description.version | acceptedVersion | nb_NO |
dc.identifier.doi | 10.2514/6.2017-1035 | |
dc.identifier.cristin | 1509861 | |
dc.relation.project | Norges forskningsråd: 223254 | nb_NO |
dc.description.localcode | ©2017 AIAA. This is the authors' accepted version of the manuscript. | nb_NO |
cristin.unitcode | 194,63,25,0 | |
cristin.unitname | Institutt for teknisk kybernetikk | |
cristin.ispublished | true | |
cristin.fulltext | postprint | |
cristin.qualitycode | 1 | |