Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle

Detalhes bibliográficos
Autor(a) principal: Lane, P.
Data de Publicação: 2020
Outros Autores: Throneberry, G., Fernandez, I., Hassanalian, M., Vasconcellos, R. [UNESP], Abdelkefi, A.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.3390/drones4030039
http://hdl.handle.net/11449/199371
Resumo: Throughout the last decade, there has been an increased demand for intricate flapping-wing drones with different capabilities than larger drones. The design of flapping-wing drones is focused on endurance and stability, as these are two of the main challenges of these systems. Researchers have recently been turning towards bioinspiration as a way to enhance aerodynamic performance. In this work, the propulsion system of a flapping-wing micro air vehicle is investigated to identify the limitations and drawbacks of specific designs. Each system has a tandem wing configuration inspired by a dragonfly, with wing shapes inspired by a bumblebee. For the design of this flapping-wing, a sizing process is carried out. A number of actuation mechanisms are considered, and two different mechanisms are designed and integrated into a flapping-wing system and compared to one another. The second system is tested using a thrust stand to investigate the impact of wing configurations on aerodynamic force production and the trend of force production from varying flapping frequency. Results present the optimal wing configuration of those tested and that an angle of attack of two degrees yields the greatest force production. A tethered flight test is conducted to examine the stability and aerodynamic capabilities of the drone, and challenges of flapping-wing systems and solutions that can lead to successful flight are presented. Key challenges to the successful design of these systems are weight management, force production, and stability and control.
id UNSP_0d1932a1968677a2117c75c8aad114bd
oai_identifier_str oai:repositorio.unesp.br:11449/199371
network_acronym_str UNSP
network_name_str Repositório Institucional da UNESP
repository_id_str 2946
spelling Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicleBioinspirationFlapping wing systemManufacturingTestingThroughout the last decade, there has been an increased demand for intricate flapping-wing drones with different capabilities than larger drones. The design of flapping-wing drones is focused on endurance and stability, as these are two of the main challenges of these systems. Researchers have recently been turning towards bioinspiration as a way to enhance aerodynamic performance. In this work, the propulsion system of a flapping-wing micro air vehicle is investigated to identify the limitations and drawbacks of specific designs. Each system has a tandem wing configuration inspired by a dragonfly, with wing shapes inspired by a bumblebee. For the design of this flapping-wing, a sizing process is carried out. A number of actuation mechanisms are considered, and two different mechanisms are designed and integrated into a flapping-wing system and compared to one another. The second system is tested using a thrust stand to investigate the impact of wing configurations on aerodynamic force production and the trend of force production from varying flapping frequency. Results present the optimal wing configuration of those tested and that an angle of attack of two degrees yields the greatest force production. A tethered flight test is conducted to examine the stability and aerodynamic capabilities of the drone, and challenges of flapping-wing systems and solutions that can lead to successful flight are presented. Key challenges to the successful design of these systems are weight management, force production, and stability and control.Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)Department of Mechanical and Aerospace Engineering New Mexico State UniversityDepartment of Mechanical Engineering New Mexico Institute of Mining and TechnologyDepartment of Aeronautical Engineering São Paulo State University (Unesp), Campus of São João da Boa VistaDepartment of Aeronautical Engineering São Paulo State University (Unesp), Campus of São João da Boa VistaCNPq: 311082/2016-5CAPES: 88881.302889/2018-01New Mexico State UniversityNew Mexico Institute of Mining and TechnologyUniversidade Estadual Paulista (Unesp)Lane, P.Throneberry, G.Fernandez, I.Hassanalian, M.Vasconcellos, R. [UNESP]Abdelkefi, A.2020-12-12T01:38:00Z2020-12-12T01:38:00Z2020-09-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article1-18http://dx.doi.org/10.3390/drones4030039Drones, v. 4, n. 3, p. 1-18, 2020.2504-446Xhttp://hdl.handle.net/11449/19937110.3390/drones40300392-s2.0-85090631317Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengDronesinfo:eu-repo/semantics/openAccess2021-10-22T17:57:53Zoai:repositorio.unesp.br:11449/199371Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462021-10-22T17:57:53Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
title Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
spellingShingle Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
Lane, P.
Bioinspiration
Flapping wing system
Manufacturing
Testing
title_short Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
title_full Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
title_fullStr Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
title_full_unstemmed Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
title_sort Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
author Lane, P.
author_facet Lane, P.
Throneberry, G.
Fernandez, I.
Hassanalian, M.
Vasconcellos, R. [UNESP]
Abdelkefi, A.
author_role author
author2 Throneberry, G.
Fernandez, I.
Hassanalian, M.
Vasconcellos, R. [UNESP]
Abdelkefi, A.
author2_role author
author
author
author
author
dc.contributor.none.fl_str_mv New Mexico State University
New Mexico Institute of Mining and Technology
Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Lane, P.
Throneberry, G.
Fernandez, I.
Hassanalian, M.
Vasconcellos, R. [UNESP]
Abdelkefi, A.
dc.subject.por.fl_str_mv Bioinspiration
Flapping wing system
Manufacturing
Testing
topic Bioinspiration
Flapping wing system
Manufacturing
Testing
description Throughout the last decade, there has been an increased demand for intricate flapping-wing drones with different capabilities than larger drones. The design of flapping-wing drones is focused on endurance and stability, as these are two of the main challenges of these systems. Researchers have recently been turning towards bioinspiration as a way to enhance aerodynamic performance. In this work, the propulsion system of a flapping-wing micro air vehicle is investigated to identify the limitations and drawbacks of specific designs. Each system has a tandem wing configuration inspired by a dragonfly, with wing shapes inspired by a bumblebee. For the design of this flapping-wing, a sizing process is carried out. A number of actuation mechanisms are considered, and two different mechanisms are designed and integrated into a flapping-wing system and compared to one another. The second system is tested using a thrust stand to investigate the impact of wing configurations on aerodynamic force production and the trend of force production from varying flapping frequency. Results present the optimal wing configuration of those tested and that an angle of attack of two degrees yields the greatest force production. A tethered flight test is conducted to examine the stability and aerodynamic capabilities of the drone, and challenges of flapping-wing systems and solutions that can lead to successful flight are presented. Key challenges to the successful design of these systems are weight management, force production, and stability and control.
publishDate 2020
dc.date.none.fl_str_mv 2020-12-12T01:38:00Z
2020-12-12T01:38:00Z
2020-09-01
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.3390/drones4030039
Drones, v. 4, n. 3, p. 1-18, 2020.
2504-446X
http://hdl.handle.net/11449/199371
10.3390/drones4030039
2-s2.0-85090631317
url http://dx.doi.org/10.3390/drones4030039
http://hdl.handle.net/11449/199371
identifier_str_mv Drones, v. 4, n. 3, p. 1-18, 2020.
2504-446X
10.3390/drones4030039
2-s2.0-85090631317
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Drones
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 1-18
dc.source.none.fl_str_mv Scopus
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv
_version_ 1803650024406515712