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dc.contributor.authorAlbrektsen, Sigurd Mørkved
dc.contributor.authorBryne, Torleiv Håland
dc.contributor.authorJohansen, Tor Arne
dc.date.accessioned2019-01-07T10:01:16Z
dc.date.available2019-01-07T10:01:16Z
dc.date.created2018-11-06T09:09:46Z
dc.date.issued2018
dc.identifier.citationIEEE Aerospace Conference. Proceedings. 2018, 2018-March 1-11.nb_NO
dc.identifier.issn1095-323X
dc.identifier.urihttp://hdl.handle.net/11250/2579418
dc.description.abstractTwo of the major challenges with beyond visual line of sight (BVLOS) operations for unmanned aerial vehicles (UAVs) today are navigation and communication. This paper presents a solution that takes on both problems simultaneously, using a phased array radio system (PARS) both for communication and to aid a micro-electro-mechanical inertial navigation system (INS), estimating position, velocity and attitude. The solution is independent of global navigation satellite system (GNSS) for positioning and highly resistant to malicious sources, such as spoofing and jamming. The state estimator presented in this paper fuses range and bearing measurements from the PARS with the measurements from an on-board inertial measurement unit, a magnetometer and a barometer. By aiding the INS with PARS position measurements, magnetometer readings and barometric measurements, drift-free PVA estimates are obtained. The PARS measurements can be used for navigation alongside today's GNSS solutions, or as a redundant backup system running in parallel. To validate the observer, an experiment was carried out with a fixed wing UAV on an approximately 35 minute flight with a maximal distance of 5.35 km from the base station. During this flight a root-mean-square accuracy of 26.3 m compared to a real-time kinematic GNSS solution was achieved.nb_NO
dc.language.isoengnb_NO
dc.publisherInstitute of Electrical and Electronics Engineers (IEEE)nb_NO
dc.titlePhased array radio system aided inertial navigation for unmanned aerial vehiclesnb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewednb_NO
dc.description.versionacceptedVersionnb_NO
dc.source.pagenumber1-11nb_NO
dc.source.volume2018-Marchnb_NO
dc.source.journalIEEE Aerospace Conference. Proceedingsnb_NO
dc.identifier.doi10.1109/AERO.2018.8396433
dc.identifier.cristin1627286
dc.relation.projectNorges forskningsråd: 250725nb_NO
dc.relation.projectNorges forskningsråd: 269480nb_NO
dc.relation.projectNorges forskningsråd: 223254nb_NO
dc.description.localcode© 2018 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.nb_NO
cristin.unitcode194,63,25,0
cristin.unitnameInstitutt for teknisk kybernetikk
cristin.ispublishedtrue
cristin.fulltextpostprint
cristin.qualitycode1


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