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Wing-gust encounters lead to unsteady flow physics and non-uniform flow velocity distribution along the wing. In this work, we develop a low-order aerodynamic framework to capture these effects, and design a closed-loop controller to mitigate the effect of the gust on the wing.

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This page is a summary of: Lift Regulation During Transverse Gust Encounters Using a Modified Goman–Khrabrov Model, AIAA Journal, September 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059127.
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