Unsteady Aerodynamics in Model-Based Wind Estimation from Fixed-Wing Aircraft Motion

dc.contributor.authorHalefom, Mekonen H.en
dc.contributor.authorHopwood, Jeremy W.en
dc.contributor.authorWoolsey, Craig A.en
dc.date.accessioned2024-11-06T15:07:08Zen
dc.date.available2024-11-06T15:07:08Zen
dc.date.issued2024-08en
dc.description.abstractThis paper examines the value of incorporating unsteady aerodynamics in a model-based wind estimator for a small, fixed-wing aircraft and presents results of an experimental implementation. An extended Kalman filter is designed for two motion models identified from flight data: one that includes unsteady effects and another that does not. An air data unit with wind vanes and a Kiel probe is used to reconstruct the local wind velocity for validation. Analysis of time histories of the wind estimates and the wind estimate error relative to the reconstructed wind velocity shows that the two model-based estimators perform equally well. The power spectral densities of the reconstructed wind and the estimated wind, computed using either estimator, follow Kolmogorov’s −5/3 law.en
dc.description.sponsorshipThe authors gratefully acknowledge financial support from NASA under grant number 80NSSC20M0162 and the Weather Intelligent Navigation Data and Models for Aviation Planning (WINDMAP) project.en
dc.description.versionAccepted versionen
dc.format.extentpp. 1556-1568en
dc.format.mimetypeapplication/pdfen
dc.identifier.doihttps://doi.org/10.2514/1.G007836en
dc.identifier.issue8en
dc.identifier.orcidWoolsey, Craig A. [0000-0003-3483-7135]en
dc.identifier.urihttps://hdl.handle.net/10919/121557en
dc.identifier.volume47en
dc.language.isoenen
dc.publisherAmerican Institute of Aeronautics and Astronauticsen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.titleUnsteady Aerodynamics in Model-Based Wind Estimation from Fixed-Wing Aircraft Motionen
dc.title.serialJournal of Guidance, Control, and Dynamicsen
dc.typeArticle - Refereeden
dc.type.dcmitypeTexten

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