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dc.contributor.authorSveier, Aksel
dc.contributor.authorSjøberg, Alexander Meyer
dc.contributor.authorEgeland, Olav
dc.date.accessioned2020-01-30T08:43:53Z
dc.date.available2020-01-30T08:43:53Z
dc.date.created2020-01-15T10:29:15Z
dc.date.issued2019
dc.identifier.issn0731-5090
dc.identifier.urihttp://hdl.handle.net/11250/2638766
dc.language.isoengnb_NO
dc.publisherAmerican Institute of Aeronautics and Astronauticsnb_NO
dc.titleApplied Runge–Kutta–Munthe-Kaas Integration for the Quaternion Kinematicsnb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewednb_NO
dc.description.versionacceptedVersionnb_NO
dc.source.journalJournal of Guidance Control and Dynamicsnb_NO
dc.identifier.doi10.2514/1.G004578
dc.identifier.cristin1773434
dc.description.localcode© 2019. This is the authors’ accepted and refereed manuscript to the article.nb_NO
cristin.unitcode194,64,92,0
cristin.unitnameInstitutt for maskinteknikk og produksjon
cristin.ispublishedtrue
cristin.qualitycode1


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