Optimal Hovering Wing Kinematics of Flapping-Wing Model Using Reinforcement Learning

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dc.contributor.authorYang, Hyeon-Hoko
dc.contributor.authorLee, Sang-Gilko
dc.contributor.authorHan, Yu-Jeongko
dc.contributor.authorHan, Jae-Hungko
dc.date.accessioned2023-01-05T08:02:46Z-
dc.date.available2023-01-05T08:02:46Z-
dc.date.created2023-01-02-
dc.date.created2023-01-02-
dc.date.issued2022-09-07-
dc.identifier.citation33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022-
dc.identifier.urihttp://hdl.handle.net/10203/304054-
dc.description.abstractThe unsteady vortex method is modified to estimate the contribution of leading-edge vortices and was used to simulate the unsteady aerodynamics of the flapping wing model. The reinforcement learning environment to train flapping wing kinematics is established based on a deep neural network. The optimal hovering wing kinematics that leads to maximum lift and lift/drag ratio is found.-
dc.languageEnglish-
dc.publisherInternational Council of the Aeronautical Sciences-
dc.titleOptimal Hovering Wing Kinematics of Flapping-Wing Model Using Reinforcement Learning-
dc.typeConference-
dc.identifier.scopusid2-s2.0-85159687958-
dc.type.rimsCONF-
dc.citation.publicationname33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022-
dc.identifier.conferencecountrySW-
dc.identifier.conferencelocationStockholm-
dc.contributor.localauthorHan, Jae-Hung-
dc.contributor.nonIdAuthorHan, Yu-Jeong-
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AE-Conference Papers(학술회의논문)
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