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dc.contributor.authorBousquet, Gabriel David Elie Sylvain
dc.contributor.authorTriantafyllou, Michael S
dc.contributor.authorSlotine, Jean-Jacques E
dc.date.accessioned2020-02-14T19:52:53Z
dc.date.available2020-02-14T19:52:53Z
dc.date.issued2017-01
dc.date.submitted2017-01
dc.identifier.isbn9781624104503
dc.identifier.urihttps://hdl.handle.net/1721.1/123819
dc.description.abstractBuilding upon our recent description of dynamic soaring as a succession of small amplitude arcs nearly crosswind, rather than a sequence of half-turns, we formulate an asymptotic expansion for the minimum-wind dynamic soaring cycle when the shear layer between the slow and fast regions has a thin but finite thickness. Our key assumption is that the trajectory remains approximately planar even in finite thickness shears. We obtain an analytical approximation for key flight parameters as a function of the shear layer thickness Δ. In particular we predict that the turn amplitude, maximum climb angle, and cycle altitude scale as Δ [superscript 1=5], Δ[superscript 2=5], and Δ[superscript 3=5], respectively. Our asymptotic expansion is validated against numerical trajectory optimizations and compared with recordings of albatross flights. While the model validity increases with wing loading, it appears to constitute an accurate description down to wing loadings as low as 4kg/m[superscript 2] for oceanic boundary layer soaring, a third that of the wandering albatross.en_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.isversionofhttp://dx.doi.org/10.2514/6.2017-1908en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceElizabeth Soergelen_US
dc.titleDynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solutionen_US
dc.typeArticleen_US
dc.identifier.citationBousquet, Gabriel et al. "Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution." AIAA Guidance, Navigation, and Control Conference 2017, January 2017, Grapevine, Texas, USA, American Institute of Aeronautics and Astronautics, January 2017.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineeringen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Brain and Cognitive Sciencesen_US
dc.relation.journalAIAA Guidance, Navigation, and Control Conference 2017en_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/ConferencePaperen_US
eprint.statushttp://purl.org/eprint/status/NonPeerRevieweden_US
dspace.date.submission2019-07-01T18:54:03Z
mit.metadata.statusComplete


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