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dc.contributor.advisorMcMurrough, Christopher
dc.creatorLOTSPEICH, HAYDEN C
dc.date.accessioned2024-01-31T18:50:54Z
dc.date.available2024-01-31T18:50:54Z
dc.date.created2023-12
dc.date.issued2023-12-18
dc.date.submittedDecember 2023
dc.identifier.urihttp://hdl.handle.net/10106/31973
dc.description.abstractThis project aims to create a testbed for split-cycle flapping wing systems that allows for testing of different motors and ESC protocols to find a suitable set for a flapping wing system. In order for a flapping-wing drone to be able to maneuver, it has to be able to flap its wings at different speeds when flapping forward and flapping backwards. The arching back-and-forth motion is what the output wing would be connected to, so this system is used to calculate the maximum split-cycle time ratio that can be achieved when set up with different motors and ESC protocols.
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.subjectSplit-cycle time ratio
dc.subjectCyclic-averaged speed
dc.titleFeasibility Study of Off-The-Shelf Components on a Split-Cycle Motor and ESC Testbed
dc.typeThesis
dc.date.updated2024-01-31T18:50:54Z
thesis.degree.departmentComputer Science and Engineering
thesis.degree.grantorThe University of Texas at Arlington
thesis.degree.levelMasters
thesis.degree.nameMaster of Science in Computer Science
dc.type.materialtext


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