Design of a two-degree-of-freedom helicopter with disturbances in the tail rotor
The design of a two degrees of freedom with an electromechanical mechanism for the generation of disturbances in the tail rotor is presented. The design focuses on a laboratory platform that replicates the dynamics of a helicopter at Pitch and Yaw angles. This platform allows the analysis of the con...
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| creator | Sánchez Meza, Victor Gabriel Lozano Hernández, Yair Gutiérrez Frías, Oscar Octavio Luviano Juárez, Alberto |
| description | The design of a two degrees of freedom with an electromechanical mechanism for the generation of disturbances in the tail rotor is presented. The design focuses on a laboratory platform that replicates the dynamics of a helicopter at Pitch and Yaw angles. This platform allows the analysis of the control schemes in the face of the variation in the incidence in the tail rotor by means of a servomotor.
The included files are:
*Design plans in PDF.
*PDF 3D design file.
*CAD design on the 2022 inventor software.
*Programming files in the simulink environment.
*Videos of the simulation and operation of the mechanism of the disturbance generator in the tail rotor.
*Video of the two degree-of-freedom helicopter operation.
*Programming and interface files on Matlab Simulink for system operation. |
| doi_str_mv | 10.17632/skb34vjtj9 |
| format | Dataset |
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The included files are:
*Design plans in PDF.
*PDF 3D design file.
*CAD design on the 2022 inventor software.
*Programming files in the simulink environment.
*Videos of the simulation and operation of the mechanism of the disturbance generator in the tail rotor.
*Video of the two degree-of-freedom helicopter operation.
*Programming and interface files on Matlab Simulink for system operation.</description><identifier>DOI: 10.17632/skb34vjtj9</identifier><language>eng</language><publisher>Mendeley Data</publisher><subject>Automatic Control ; Helicopter ; Mechanical Design ; Robotics</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><orcidid>0000-0002-2855-3243 ; 0000-0001-8157-3510 ; 0000-0001-8790-4165</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>780,1894</link.rule.ids><linktorsrc>$$Uhttps://commons.datacite.org/doi.org/10.17632/skb34vjtj9$$EView_record_in_DataCite.org$$FView_record_in_$$GDataCite.org$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Sánchez Meza, Victor Gabriel</creatorcontrib><creatorcontrib>Lozano Hernández, Yair</creatorcontrib><creatorcontrib>Gutiérrez Frías, Oscar Octavio</creatorcontrib><creatorcontrib>Luviano Juárez, Alberto</creatorcontrib><title>Design of a two-degree-of-freedom helicopter with disturbances in the tail rotor</title><description>The design of a two degrees of freedom with an electromechanical mechanism for the generation of disturbances in the tail rotor is presented. The design focuses on a laboratory platform that replicates the dynamics of a helicopter at Pitch and Yaw angles. This platform allows the analysis of the control schemes in the face of the variation in the incidence in the tail rotor by means of a servomotor.
The included files are:
*Design plans in PDF.
*PDF 3D design file.
*CAD design on the 2022 inventor software.
*Programming files in the simulink environment.
*Videos of the simulation and operation of the mechanism of the disturbance generator in the tail rotor.
*Video of the two degree-of-freedom helicopter operation.
*Programming and interface files on Matlab Simulink for system operation.</description><subject>Automatic Control</subject><subject>Helicopter</subject><subject>Mechanical Design</subject><subject>Robotics</subject><fulltext>true</fulltext><rsrctype>dataset</rsrctype><creationdate>2024</creationdate><recordtype>dataset</recordtype><sourceid>PQ8</sourceid><recordid>eNqVzi0PwjAQgOEaBAEUf-A8KWyMQNB8BInAN8d63W5s69IeLPx7CCFBox7zilepaZrM0806Wy7i7ZqtHpVU26E67yly0YJ3gCC915aKQKS90-6t9Q2UVHPuO6EAPUsJlqPcwxXbnCJwC1ISCHINwYsPYzVwWEeafB2p2fFw2Z20RcGchUwXuMHwNGliPj_m95P9V78AmOJFRQ</recordid><startdate>20240916</startdate><enddate>20240916</enddate><creator>Sánchez Meza, Victor Gabriel</creator><creator>Lozano Hernández, Yair</creator><creator>Gutiérrez Frías, Oscar Octavio</creator><creator>Luviano Juárez, Alberto</creator><general>Mendeley Data</general><scope>DYCCY</scope><scope>PQ8</scope><orcidid>https://orcid.org/0000-0002-2855-3243</orcidid><orcidid>https://orcid.org/0000-0001-8157-3510</orcidid><orcidid>https://orcid.org/0000-0001-8790-4165</orcidid></search><sort><creationdate>20240916</creationdate><title>Design of a two-degree-of-freedom helicopter with disturbances in the tail rotor</title><author>Sánchez Meza, Victor Gabriel ; Lozano Hernández, Yair ; Gutiérrez Frías, Oscar Octavio ; Luviano Juárez, Alberto</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-datacite_primary_10_17632_skb34vjtj93</frbrgroupid><rsrctype>datasets</rsrctype><prefilter>datasets</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Automatic Control</topic><topic>Helicopter</topic><topic>Mechanical Design</topic><topic>Robotics</topic><toplevel>online_resources</toplevel><creatorcontrib>Sánchez Meza, Victor Gabriel</creatorcontrib><creatorcontrib>Lozano Hernández, Yair</creatorcontrib><creatorcontrib>Gutiérrez Frías, Oscar Octavio</creatorcontrib><creatorcontrib>Luviano Juárez, Alberto</creatorcontrib><collection>DataCite (Open Access)</collection><collection>DataCite</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Sánchez Meza, Victor Gabriel</au><au>Lozano Hernández, Yair</au><au>Gutiérrez Frías, Oscar Octavio</au><au>Luviano Juárez, Alberto</au><format>book</format><genre>unknown</genre><ristype>DATA</ristype><title>Design of a two-degree-of-freedom helicopter with disturbances in the tail rotor</title><date>2024-09-16</date><risdate>2024</risdate><abstract>The design of a two degrees of freedom with an electromechanical mechanism for the generation of disturbances in the tail rotor is presented. The design focuses on a laboratory platform that replicates the dynamics of a helicopter at Pitch and Yaw angles. This platform allows the analysis of the control schemes in the face of the variation in the incidence in the tail rotor by means of a servomotor.
The included files are:
*Design plans in PDF.
*PDF 3D design file.
*CAD design on the 2022 inventor software.
*Programming files in the simulink environment.
*Videos of the simulation and operation of the mechanism of the disturbance generator in the tail rotor.
*Video of the two degree-of-freedom helicopter operation.
*Programming and interface files on Matlab Simulink for system operation.</abstract><pub>Mendeley Data</pub><doi>10.17632/skb34vjtj9</doi><orcidid>https://orcid.org/0000-0002-2855-3243</orcidid><orcidid>https://orcid.org/0000-0001-8157-3510</orcidid><orcidid>https://orcid.org/0000-0001-8790-4165</orcidid><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | DOI: 10.17632/skb34vjtj9 |
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| language | eng |
| recordid | cdi_datacite_primary_10_17632_skb34vjtj9 |
| source | DataCite |
| subjects | Automatic Control Helicopter Mechanical Design Robotics |
| title | Design of a two-degree-of-freedom helicopter with disturbances in the tail rotor |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-25T22%3A28%3A36IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-datacite_PQ8&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.au=S%C3%A1nchez%20Meza,%20Victor%20Gabriel&rft.date=2024-09-16&rft_id=info:doi/10.17632/skb34vjtj9&rft_dat=%3Cdatacite_PQ8%3E10_17632_skb34vjtj9%3C/datacite_PQ8%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |