Return to search

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

No description available.
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.

Page generated in 0.0015 seconds