Simulink Models for flapping wing systems via slider crank and direct drive

DOI

Those MATLAB files include the mathematical model for a flapping wing aerial vehicle via a direct-drive mechanism and slider crank mechanism. They allow for estimating the powers, forces, and efficiencies of each system. 

Identifier
DOI https://doi.org/10.5522/04/22595950.v1
Related Identifier HasPart https://ndownloader.figshare.com/files/40119955
Related Identifier HasPart https://ndownloader.figshare.com/files/40119958
Related Identifier HasPart https://ndownloader.figshare.com/files/40119961
Related Identifier HasPart https://ndownloader.figshare.com/files/40119964
Related Identifier HasPart https://ndownloader.figshare.com/files/40119988
Metadata Access https://api.figshare.com/v2/oai?verb=GetRecord&metadataPrefix=oai_datacite&identifier=oai:figshare.com:article/22595950
Provenance
Creator Park, Moonsoo; Abolfathi, Ali
Publisher University College London UCL
Contributor Figshare
Publication Year 2023
Rights https://creativecommons.org/licenses/by-nc/4.0/
OpenAccess true
Contact researchdatarepository(at)ucl.ac.uk
Representation
Language English
Resource Type Software
Discipline Other