A Laboratory Prototype Tandem Helicopter With Two Degrees of Freedom
Unmanned aircraft have had a great impact on society, their applications in various fields are increasing day by day, so it becomes necessary to propose, develop or validate new designs and concepts that help minimize operating errors or improve the safety of aircraft. One way to understand the oper...
Gespeichert in:
| Veröffentlicht in: | IEEE access 2021, Vol.9, p.39618-39625 |
|---|---|
| Hauptverfasser: | , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 39625 |
|---|---|
| container_issue | |
| container_start_page | 39618 |
| container_title | IEEE access |
| container_volume | 9 |
| creator | Pena, Jacobo Marcos Allende Paredes, Salvador Antonio Rodriguez Martinez, Jorge Salvador Valdez Aguilar-Molina, Yehoshua |
| description | Unmanned aircraft have had a great impact on society, their applications in various fields are increasing day by day, so it becomes necessary to propose, develop or validate new designs and concepts that help minimize operating errors or improve the safety of aircraft. One way to understand the operating principle of these unmanned aircraft is through laboratory prototypes or test benches; these prototypes allow experimentation and testing in controlled environments to minimize errors in their operation. This article presents a novel configuration for a laboratory prototype of a tandem-rotor helicopter with two degrees of freedom (DOF), and the dynamic modeling, control, signal filtering, and implementation of the control and filtering system using a microcontroller and a low-cost prototype made with easily accessible materials. This is to promote education, research, and technological development in this area of engineering. |
| doi_str_mv | 10.1109/ACCESS.2021.3064568 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_ieee_</sourceid><recordid>TN_cdi_ieee_primary_9373313</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>9373313</ieee_id><doaj_id>oai_doaj_org_article_700ed585058742479774ebb31a07c8ce</doaj_id><sourcerecordid>2503499945</sourcerecordid><originalsourceid>FETCH-LOGICAL-c408t-b52c4ad6cb3342fd46c1af6f6cf2c60ddd5f2c9814aad23780890d2235f539b3</originalsourceid><addsrcrecordid>eNpNUF1LAzEQPERB0f6CvgR8bk2y-Xws9aNCQaEHPoZcsqdX2qbmTqT_3qtXxH3ZYZiZXaYoxoxOGaP2bjafP6xWU045mwJVQipzVlxxpuwEJKjzf_iyGLXtmvZjekrqq-J-Rpa-Stl3KR_Ia05d6g57JKXfRdySBW6akPYdZvLWdB-k_E7kHt8zYktSTR57ENP2prio_abF0WlfF-XjQzlfTJYvT8_z2XISBDXdpJI8CB9VqAAEr6NQgfla1SrUPCgaY5Q9sIYJ7yMHbaixNHIOspZgK7gunofYmPza7XOz9fngkm_cL5Hyu_O5a8IGnaYUozSSSqMFF9pqLbCqgHmqgwnYZ90OWfucPr-w7dw6feVd_73jkoKw1grZq2BQhZzaNmP9d5VRdyzfDeW7Y_nuVH7vGg-uBhH_HBY0AAP4ASfJfng</addsrcrecordid><sourcetype>Open Website</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2503499945</pqid></control><display><type>article</type><title>A Laboratory Prototype Tandem Helicopter With Two Degrees of Freedom</title><source>IEEE Open Access Journals</source><source>DOAJ Directory of Open Access Journals</source><source>EZB-FREE-00999 freely available EZB journals</source><creator>Pena, Jacobo Marcos Allende ; Paredes, Salvador Antonio Rodriguez ; Martinez, Jorge Salvador Valdez ; Aguilar-Molina, Yehoshua</creator><creatorcontrib>Pena, Jacobo Marcos Allende ; Paredes, Salvador Antonio Rodriguez ; Martinez, Jorge Salvador Valdez ; Aguilar-Molina, Yehoshua</creatorcontrib><description>Unmanned aircraft have had a great impact on society, their applications in various fields are increasing day by day, so it becomes necessary to propose, develop or validate new designs and concepts that help minimize operating errors or improve the safety of aircraft. One way to understand the operating principle of these unmanned aircraft is through laboratory prototypes or test benches; these prototypes allow experimentation and testing in controlled environments to minimize errors in their operation. This article presents a novel configuration for a laboratory prototype of a tandem-rotor helicopter with two degrees of freedom (DOF), and the dynamic modeling, control, signal filtering, and implementation of the control and filtering system using a microcontroller and a low-cost prototype made with easily accessible materials. This is to promote education, research, and technological development in this area of engineering.</description><identifier>ISSN: 2169-3536</identifier><identifier>EISSN: 2169-3536</identifier><identifier>DOI: 10.1109/ACCESS.2021.3064568</identifier><identifier>CODEN: IAECCG</identifier><language>eng</language><publisher>Piscataway: IEEE</publisher><subject>Aircraft ; Aircraft safety ; Atmospheric modeling ; control ; Control systems ; Degrees of freedom ; Dynamic models ; Experimentation ; Filtering ; Filtration ; Helicopters ; implementation ; Laboratories ; Mathematical model ; microcontroller ; Microcontrollers ; Prototypes ; Rotors ; signal filtering ; Tandem rotor helicopters ; Tandem-rotor helicopter 2DOF ; Unmanned aerial vehicles ; Unmanned aircraft</subject><ispartof>IEEE access, 2021, Vol.9, p.39618-39625</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2021</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c408t-b52c4ad6cb3342fd46c1af6f6cf2c60ddd5f2c9814aad23780890d2235f539b3</citedby><cites>FETCH-LOGICAL-c408t-b52c4ad6cb3342fd46c1af6f6cf2c60ddd5f2c9814aad23780890d2235f539b3</cites><orcidid>0000-0003-1227-0449</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/9373313$$EHTML$$P50$$Gieee$$Hfree_for_read</linktohtml><link.rule.ids>314,780,784,864,2102,4024,27633,27923,27924,27925,54933</link.rule.ids></links><search><creatorcontrib>Pena, Jacobo Marcos Allende</creatorcontrib><creatorcontrib>Paredes, Salvador Antonio Rodriguez</creatorcontrib><creatorcontrib>Martinez, Jorge Salvador Valdez</creatorcontrib><creatorcontrib>Aguilar-Molina, Yehoshua</creatorcontrib><title>A Laboratory Prototype Tandem Helicopter With Two Degrees of Freedom</title><title>IEEE access</title><addtitle>Access</addtitle><description>Unmanned aircraft have had a great impact on society, their applications in various fields are increasing day by day, so it becomes necessary to propose, develop or validate new designs and concepts that help minimize operating errors or improve the safety of aircraft. One way to understand the operating principle of these unmanned aircraft is through laboratory prototypes or test benches; these prototypes allow experimentation and testing in controlled environments to minimize errors in their operation. This article presents a novel configuration for a laboratory prototype of a tandem-rotor helicopter with two degrees of freedom (DOF), and the dynamic modeling, control, signal filtering, and implementation of the control and filtering system using a microcontroller and a low-cost prototype made with easily accessible materials. This is to promote education, research, and technological development in this area of engineering.</description><subject>Aircraft</subject><subject>Aircraft safety</subject><subject>Atmospheric modeling</subject><subject>control</subject><subject>Control systems</subject><subject>Degrees of freedom</subject><subject>Dynamic models</subject><subject>Experimentation</subject><subject>Filtering</subject><subject>Filtration</subject><subject>Helicopters</subject><subject>implementation</subject><subject>Laboratories</subject><subject>Mathematical model</subject><subject>microcontroller</subject><subject>Microcontrollers</subject><subject>Prototypes</subject><subject>Rotors</subject><subject>signal filtering</subject><subject>Tandem rotor helicopters</subject><subject>Tandem-rotor helicopter 2DOF</subject><subject>Unmanned aerial vehicles</subject><subject>Unmanned aircraft</subject><issn>2169-3536</issn><issn>2169-3536</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>ESBDL</sourceid><sourceid>RIE</sourceid><sourceid>DOA</sourceid><recordid>eNpNUF1LAzEQPERB0f6CvgR8bk2y-Xws9aNCQaEHPoZcsqdX2qbmTqT_3qtXxH3ZYZiZXaYoxoxOGaP2bjafP6xWU045mwJVQipzVlxxpuwEJKjzf_iyGLXtmvZjekrqq-J-Rpa-Stl3KR_Ia05d6g57JKXfRdySBW6akPYdZvLWdB-k_E7kHt8zYktSTR57ENP2prio_abF0WlfF-XjQzlfTJYvT8_z2XISBDXdpJI8CB9VqAAEr6NQgfla1SrUPCgaY5Q9sIYJ7yMHbaixNHIOspZgK7gunofYmPza7XOz9fngkm_cL5Hyu_O5a8IGnaYUozSSSqMFF9pqLbCqgHmqgwnYZ90OWfucPr-w7dw6feVd_73jkoKw1grZq2BQhZzaNmP9d5VRdyzfDeW7Y_nuVH7vGg-uBhH_HBY0AAP4ASfJfng</recordid><startdate>2021</startdate><enddate>2021</enddate><creator>Pena, Jacobo Marcos Allende</creator><creator>Paredes, Salvador Antonio Rodriguez</creator><creator>Martinez, Jorge Salvador Valdez</creator><creator>Aguilar-Molina, Yehoshua</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</general><scope>97E</scope><scope>ESBDL</scope><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>DOA</scope><orcidid>https://orcid.org/0000-0003-1227-0449</orcidid></search><sort><creationdate>2021</creationdate><title>A Laboratory Prototype Tandem Helicopter With Two Degrees of Freedom</title><author>Pena, Jacobo Marcos Allende ; Paredes, Salvador Antonio Rodriguez ; Martinez, Jorge Salvador Valdez ; Aguilar-Molina, Yehoshua</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c408t-b52c4ad6cb3342fd46c1af6f6cf2c60ddd5f2c9814aad23780890d2235f539b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Aircraft</topic><topic>Aircraft safety</topic><topic>Atmospheric modeling</topic><topic>control</topic><topic>Control systems</topic><topic>Degrees of freedom</topic><topic>Dynamic models</topic><topic>Experimentation</topic><topic>Filtering</topic><topic>Filtration</topic><topic>Helicopters</topic><topic>implementation</topic><topic>Laboratories</topic><topic>Mathematical model</topic><topic>microcontroller</topic><topic>Microcontrollers</topic><topic>Prototypes</topic><topic>Rotors</topic><topic>signal filtering</topic><topic>Tandem rotor helicopters</topic><topic>Tandem-rotor helicopter 2DOF</topic><topic>Unmanned aerial vehicles</topic><topic>Unmanned aircraft</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Pena, Jacobo Marcos Allende</creatorcontrib><creatorcontrib>Paredes, Salvador Antonio Rodriguez</creatorcontrib><creatorcontrib>Martinez, Jorge Salvador Valdez</creatorcontrib><creatorcontrib>Aguilar-Molina, Yehoshua</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 2005-present</collection><collection>IEEE Open Access Journals</collection><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Electronic Library (IEL)</collection><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>DOAJ Directory of Open Access Journals</collection><jtitle>IEEE access</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Pena, Jacobo Marcos Allende</au><au>Paredes, Salvador Antonio Rodriguez</au><au>Martinez, Jorge Salvador Valdez</au><au>Aguilar-Molina, Yehoshua</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A Laboratory Prototype Tandem Helicopter With Two Degrees of Freedom</atitle><jtitle>IEEE access</jtitle><stitle>Access</stitle><date>2021</date><risdate>2021</risdate><volume>9</volume><spage>39618</spage><epage>39625</epage><pages>39618-39625</pages><issn>2169-3536</issn><eissn>2169-3536</eissn><coden>IAECCG</coden><abstract>Unmanned aircraft have had a great impact on society, their applications in various fields are increasing day by day, so it becomes necessary to propose, develop or validate new designs and concepts that help minimize operating errors or improve the safety of aircraft. One way to understand the operating principle of these unmanned aircraft is through laboratory prototypes or test benches; these prototypes allow experimentation and testing in controlled environments to minimize errors in their operation. This article presents a novel configuration for a laboratory prototype of a tandem-rotor helicopter with two degrees of freedom (DOF), and the dynamic modeling, control, signal filtering, and implementation of the control and filtering system using a microcontroller and a low-cost prototype made with easily accessible materials. This is to promote education, research, and technological development in this area of engineering.</abstract><cop>Piscataway</cop><pub>IEEE</pub><doi>10.1109/ACCESS.2021.3064568</doi><tpages>8</tpages><orcidid>https://orcid.org/0000-0003-1227-0449</orcidid><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 2169-3536 |
| ispartof | IEEE access, 2021, Vol.9, p.39618-39625 |
| issn | 2169-3536 2169-3536 |
| language | eng |
| recordid | cdi_ieee_primary_9373313 |
| source | IEEE Open Access Journals; DOAJ Directory of Open Access Journals; EZB-FREE-00999 freely available EZB journals |
| subjects | Aircraft Aircraft safety Atmospheric modeling control Control systems Degrees of freedom Dynamic models Experimentation Filtering Filtration Helicopters implementation Laboratories Mathematical model microcontroller Microcontrollers Prototypes Rotors signal filtering Tandem rotor helicopters Tandem-rotor helicopter 2DOF Unmanned aerial vehicles Unmanned aircraft |
| title | A Laboratory Prototype Tandem Helicopter With Two Degrees of Freedom |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-05T20%3A40%3A50IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_ieee_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20Laboratory%20Prototype%20Tandem%20Helicopter%20With%20Two%20Degrees%20of%20Freedom&rft.jtitle=IEEE%20access&rft.au=Pena,%20Jacobo%20Marcos%20Allende&rft.date=2021&rft.volume=9&rft.spage=39618&rft.epage=39625&rft.pages=39618-39625&rft.issn=2169-3536&rft.eissn=2169-3536&rft.coden=IAECCG&rft_id=info:doi/10.1109/ACCESS.2021.3064568&rft_dat=%3Cproquest_ieee_%3E2503499945%3C/proquest_ieee_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2503499945&rft_id=info:pmid/&rft_ieee_id=9373313&rft_doaj_id=oai_doaj_org_article_700ed585058742479774ebb31a07c8ce&rfr_iscdi=true |