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A Closed Loop Research Platform That Enables Dynamic Control Of Wing Gait Patterns In A Vertically Constrained Flapping Wing - Micro Air Vehicle

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Identiferoai:union.ndltd.org:OhioLink/oai:etd.ohiolink.edu:wright1462801627
Date10 May 2016
CreatorsBotha, Hermanus Van Niekerk
PublisherWright State University / OhioLINK
Source SetsOhiolink ETDs
LanguageEnglish
Detected LanguageEnglish
Typetext
Sourcehttp://rave.ohiolink.edu/etdc/view?acc_num=wright1462801627
Rightsunrestricted, This thesis or dissertation is protected by copyright: all rights reserved. It may not be copied or redistributed beyond the terms of applicable copyright laws.

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