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dc.contributor.authorStovner, Bård Nagy
dc.contributor.authorJohansen, Tor Arne
dc.date.accessioned2020-11-09T08:23:55Z
dc.date.available2020-11-09T08:23:55Z
dc.date.created2020-11-06T15:32:57Z
dc.date.issued2020
dc.identifier.isbn978-1-62410-595-1
dc.identifier.urihttps://hdl.handle.net/11250/2686859
dc.description.abstractThis paper considers the estimation of the steady wind component around small fixedwing unmanned aerial vehicles using measurements from a Pitot-static tube and velocity over ground information. A three-stage filter is proposed, which yields globally exponentially stable estimation of the wind velocity and a correction factor on the dynamic pressure measurements from the Pitot-static tube. The suggested filter is compared with an extended Kalman filter and shown to yield identical steady state performance in both simulations and experiments. Additionally, the improved stability with respect to the extended Kalman filter is demonstrated with a choice of suboptimal tuning, for which the extended Kalman filter failed to converge whereas the suggested filter did not.en_US
dc.language.isoengen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.ispartofAIAA Scitech Forum 2020
dc.titleGlobally exponentially stable wind estimation for small fixed-wing UAVs using standard sensorsen_US
dc.typeChapteren_US
dc.description.versionacceptedVersionen_US
dc.identifier.cristin1845729
dc.relation.projectNorges forskningsråd: 223254en_US
dc.relation.projectNorges forskningsråd: 261791en_US
dc.description.localcode© 2020. This chapter is the authors' accepted and refereed chapter accepted for publication in AIAA Scitech Forum 2020. https://doi.org/10.2514/6.2020-1719en_US
cristin.ispublishedtrue
cristin.fulltextpostprint
cristin.qualitycode1


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