Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution

Building 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 bu...

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Main Authors: Bousquet, Gabriel David Elie Sylvain, Triantafyllou, Michael S, Slotine, Jean-Jacques E
Other Authors: Massachusetts Institute of Technology. Department of Mechanical Engineering
Format: Article
Published: American Institute of Aeronautics and Astronautics 2020
Online Access:https://hdl.handle.net/1721.1/123819
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author Bousquet, Gabriel David Elie Sylvain
Triantafyllou, Michael S
Slotine, Jean-Jacques E
author2 Massachusetts Institute of Technology. Department of Mechanical Engineering
author_facet Massachusetts Institute of Technology. Department of Mechanical Engineering
Bousquet, Gabriel David Elie Sylvain
Triantafyllou, Michael S
Slotine, Jean-Jacques E
author_sort Bousquet, Gabriel David Elie Sylvain
collection MIT
description Building 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.
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spelling mit-1721.1/1238192022-09-30T11:27:26Z Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution Bousquet, Gabriel David Elie Sylvain Triantafyllou, Michael S Slotine, Jean-Jacques E Massachusetts Institute of Technology. Department of Mechanical Engineering Massachusetts Institute of Technology. Department of Aeronautics and Astronautics Massachusetts Institute of Technology. Department of Brain and Cognitive Sciences Building 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. 2020-02-14T19:52:53Z 2020-02-14T19:52:53Z 2017-01 2017-01 Article http://purl.org/eprint/type/ConferencePaper 9781624104503 https://hdl.handle.net/1721.1/123819 Bousquet, 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. http://dx.doi.org/10.2514/6.2017-1908 AIAA Guidance, Navigation, and Control Conference 2017 Creative Commons Attribution-Noncommercial-Share Alike http://creativecommons.org/licenses/by-nc-sa/4.0/ application/pdf American Institute of Aeronautics and Astronautics Elizabeth Soergel
spellingShingle Bousquet, Gabriel David Elie Sylvain
Triantafyllou, Michael S
Slotine, Jean-Jacques E
Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution
title Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution
title_full Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution
title_fullStr Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution
title_full_unstemmed Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution
title_short Dynamic Soaring in Finite-Thickness Wind Shears: an Asymptotic Solution
title_sort dynamic soaring in finite thickness wind shears an asymptotic solution
url https://hdl.handle.net/1721.1/123819
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