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dc.contributor.authorNaik, Kartik
dc.contributor.authorBeknalkar, Sumedh
dc.contributor.authorReed, James
dc.contributor.authorMazzoleni, Andre
dc.contributor.authorFathy, Hosam
dc.contributor.authorVermillion, Chris
dc.date.accessioned2023-08-16T18:13:57Z
dc.date.available2023-08-16T18:13:57Z
dc.date.copyright11/1/2022 12:00:00 AM
dc.date.issued2022
dc.identifier.issn0022-0434
dc.identifier.otherds_145_01_011005.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291671
dc.description.abstractThis paper presents the formulation and results for a control-aware optimization of the combined geometric and structural design of an energy-harvesting underwater kite. Because kite-based energy-harvesting systems, both airborne and underwater, possess strong coupling between closed-loop flight control, geometric design, and structural design, consideration of all three facets of the design within a single codesign framework is highly desirable. However, while prior literature has addressed one or two attributes of the design at a time, this work constitutes the first comprehensive effort aimed at addressing all three. In particular, focusing on the goals of power maximization and mass minimization, we present a codesign formulation that fuses a geometric optimization tool, structural optimization tool, and closed-loop flight efficiency map. The resulting integrated codesign tool is used to address two mathematical optimization formulations that exhibit subtle differences: a Pareto optimal formulation and a dual-objective formulation that focuses on a weighted power-to-mass ratio as the techno-economic metric of merit. Based on the resulting geometric and structural designs, using a mediumfidelity closed-loop simulation tool, the proposed formulation is shown to achieve more than three times the powerto-mass ratio of a previously published, unoptimized benchmark design.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titlePareto Optimal and Dual-Objective Geometric and Structural Design of an Underwater Kite for Closed-Loop Flight Performance
dc.typeJournal Paper
dc.journal.volume145
dc.journal.issue1
dc.journal.titleJournal of Dynamic Systems, Measurement, and Control
dc.identifier.doi10.1115/1.4055978
dc.journal.fristpage11005-1
dc.journal.lastpage11005-12
dc.page12
dc.treeJournal of Dynamic Systems, Measurement, and Control:;2022:;volume( 145 ):;issue: 001
dc.contenttypeFulltext


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