Nonlinear Tracking Control of an Elastically Supported Flapping Thin Airfoil

Nonlinear Tracking Control of an Elastically Supported Flapping Thin Airfoil

A control law for a self-excited system using state feedback linearization and coordinate transformation is developed. The system consists of an elastically supported hinged thin airfoil, which is subjected to a uniform steady airflow A nonlinear aerodynamic model is used to account for the fluid-so...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of vibration and control 2004-06, Vol.10 (6), p.779-794
Hauptverfasser: Al-Majed, Mohammed I., Alsaif, Khalid A.
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 794
container_issue 6
container_start_page 779
container_title Journal of vibration and control
container_volume 10
creator Al-Majed, Mohammed I.
Alsaif, Khalid A.
description A control law for a self-excited system using state feedback linearization and coordinate transformation is developed. The system consists of an elastically supported hinged thin airfoil, which is subjected to a uniform steady airflow A nonlinear aerodynamic model is used to account for the fluid-solid interaction mnechanism. A chaotic behavior of the open-loop system at certain control parameters is observed experimentally and checked numerically. It is shown that the controllability of the system is guaranteed using a torque source at the leading edge of the airfoil. Furthennore, good tracl4rg of time-varying desired angle of attack is achieved using the developed controller. Finally, a SIMULINK%N model is developed to facilitate time-domain analysis, control design and future real-time control implementations.
doi_str_mv 10.1177/1077546304039430
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_28288343</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_1077546304039430</sage_id><sourcerecordid>28288343</sourcerecordid><originalsourceid>FETCH-LOGICAL-c290t-6f71d2407091c55158b5de8f0cb6c7b0c193fec6c98742918f19ffbcb0d09f7b3</originalsourceid><addsrcrecordid>eNp1kMFLwzAYxYsoOKd3j8GDt-qXNG2S4xibCkMPznNJ02RmZklN2sP-ezsmCANP34P3e4-Pl2W3GB4wZuwRA2MlrQqgUAhawFk2wYzinAhenY96tPODf5ldpbQFAEoxTLLVa_DOei0jWkepvqzfoHnwfQwOBYOkRwsnU2-VdG6P3oeuC7HXLVo62XUHeP1pPZrZaIJ119mFkS7pm987zT6Wi_X8OV-9Pb3MZ6tcEQF9XhmGW0KBgcCqLHHJm7LV3IBqKsUaUFgURqtKCc4oEZgbLIxpVAMtCMOaYprdH3u7GL4Hnfp6Z5PSzkmvw5BqwgnnBS1G8O4E3IYh-vG3mhAMZSmgGiE4QiqGlKI2dRftTsZ9jaE-bFufbjtG8mMkyY3-6_yX_wHtgXfw</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>221055906</pqid></control><display><type>article</type><title>Nonlinear Tracking Control of an Elastically Supported Flapping Thin Airfoil</title><source>Sage Journals</source><creator>Al-Majed, Mohammed I. ; Alsaif, Khalid A.</creator><creatorcontrib>Al-Majed, Mohammed I. ; Alsaif, Khalid A.</creatorcontrib><description>A control law for a self-excited system using state feedback linearization and coordinate transformation is developed. The system consists of an elastically supported hinged thin airfoil, which is subjected to a uniform steady airflow A nonlinear aerodynamic model is used to account for the fluid-solid interaction mnechanism. A chaotic behavior of the open-loop system at certain control parameters is observed experimentally and checked numerically. It is shown that the controllability of the system is guaranteed using a torque source at the leading edge of the airfoil. Furthennore, good tracl4rg of time-varying desired angle of attack is achieved using the developed controller. Finally, a SIMULINK%N model is developed to facilitate time-domain analysis, control design and future real-time control implementations.</description><identifier>ISSN: 1077-5463</identifier><identifier>EISSN: 1741-2986</identifier><identifier>DOI: 10.1177/1077546304039430</identifier><language>eng</language><publisher>Thousand Oaks, CA: SAGE Publications</publisher><subject>Aerodynamics</subject><ispartof>Journal of vibration and control, 2004-06, Vol.10 (6), p.779-794</ispartof><rights>Copyright SAGE PUBLICATIONS, INC. Jun 2004</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c290t-6f71d2407091c55158b5de8f0cb6c7b0c193fec6c98742918f19ffbcb0d09f7b3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/1077546304039430$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/1077546304039430$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,776,780,21800,27903,27904,43600,43601</link.rule.ids></links><search><creatorcontrib>Al-Majed, Mohammed I.</creatorcontrib><creatorcontrib>Alsaif, Khalid A.</creatorcontrib><title>Nonlinear Tracking Control of an Elastically Supported Flapping Thin Airfoil</title><title>Journal of vibration and control</title><description>A control law for a self-excited system using state feedback linearization and coordinate transformation is developed. The system consists of an elastically supported hinged thin airfoil, which is subjected to a uniform steady airflow A nonlinear aerodynamic model is used to account for the fluid-solid interaction mnechanism. A chaotic behavior of the open-loop system at certain control parameters is observed experimentally and checked numerically. It is shown that the controllability of the system is guaranteed using a torque source at the leading edge of the airfoil. Furthennore, good tracl4rg of time-varying desired angle of attack is achieved using the developed controller. Finally, a SIMULINK%N model is developed to facilitate time-domain analysis, control design and future real-time control implementations.</description><subject>Aerodynamics</subject><issn>1077-5463</issn><issn>1741-2986</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2004</creationdate><recordtype>article</recordtype><recordid>eNp1kMFLwzAYxYsoOKd3j8GDt-qXNG2S4xibCkMPznNJ02RmZklN2sP-ezsmCANP34P3e4-Pl2W3GB4wZuwRA2MlrQqgUAhawFk2wYzinAhenY96tPODf5ldpbQFAEoxTLLVa_DOei0jWkepvqzfoHnwfQwOBYOkRwsnU2-VdG6P3oeuC7HXLVo62XUHeP1pPZrZaIJ119mFkS7pm987zT6Wi_X8OV-9Pb3MZ6tcEQF9XhmGW0KBgcCqLHHJm7LV3IBqKsUaUFgURqtKCc4oEZgbLIxpVAMtCMOaYprdH3u7GL4Hnfp6Z5PSzkmvw5BqwgnnBS1G8O4E3IYh-vG3mhAMZSmgGiE4QiqGlKI2dRftTsZ9jaE-bFufbjtG8mMkyY3-6_yX_wHtgXfw</recordid><startdate>200406</startdate><enddate>200406</enddate><creator>Al-Majed, Mohammed I.</creator><creator>Alsaif, Khalid A.</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>JQ2</scope><scope>KR7</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>7U5</scope><scope>H8D</scope></search><sort><creationdate>200406</creationdate><title>Nonlinear Tracking Control of an Elastically Supported Flapping Thin Airfoil</title><author>Al-Majed, Mohammed I. ; Alsaif, Khalid A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c290t-6f71d2407091c55158b5de8f0cb6c7b0c193fec6c98742918f19ffbcb0d09f7b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2004</creationdate><topic>Aerodynamics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Al-Majed, Mohammed I.</creatorcontrib><creatorcontrib>Alsaif, Khalid A.</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics &amp; Communications Abstracts</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</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>Solid State and Superconductivity Abstracts</collection><collection>Aerospace Database</collection><jtitle>Journal of vibration and control</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Al-Majed, Mohammed I.</au><au>Alsaif, Khalid A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Nonlinear Tracking Control of an Elastically Supported Flapping Thin Airfoil</atitle><jtitle>Journal of vibration and control</jtitle><date>2004-06</date><risdate>2004</risdate><volume>10</volume><issue>6</issue><spage>779</spage><epage>794</epage><pages>779-794</pages><issn>1077-5463</issn><eissn>1741-2986</eissn><abstract>A control law for a self-excited system using state feedback linearization and coordinate transformation is developed. The system consists of an elastically supported hinged thin airfoil, which is subjected to a uniform steady airflow A nonlinear aerodynamic model is used to account for the fluid-solid interaction mnechanism. A chaotic behavior of the open-loop system at certain control parameters is observed experimentally and checked numerically. It is shown that the controllability of the system is guaranteed using a torque source at the leading edge of the airfoil. Furthennore, good tracl4rg of time-varying desired angle of attack is achieved using the developed controller. Finally, a SIMULINK%N model is developed to facilitate time-domain analysis, control design and future real-time control implementations.</abstract><cop>Thousand Oaks, CA</cop><pub>SAGE Publications</pub><doi>10.1177/1077546304039430</doi><tpages>16</tpages></addata></record>
fulltext fulltext
identifier ISSN: 1077-5463
ispartof Journal of vibration and control, 2004-06, Vol.10 (6), p.779-794
issn 1077-5463
1741-2986
language eng
recordid cdi_proquest_miscellaneous_28288343
source Sage Journals
subjects Aerodynamics
title Nonlinear Tracking Control of an Elastically Supported Flapping Thin Airfoil
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T20%3A15%3A17IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Nonlinear%20Tracking%20Control%20of%20an%20Elastically%20Supported%20Flapping%20Thin%20Airfoil&rft.jtitle=Journal%20of%20vibration%20and%20control&rft.au=Al-Majed,%20Mohammed%20I.&rft.date=2004-06&rft.volume=10&rft.issue=6&rft.spage=779&rft.epage=794&rft.pages=779-794&rft.issn=1077-5463&rft.eissn=1741-2986&rft_id=info:doi/10.1177/1077546304039430&rft_dat=%3Cproquest_cross%3E28288343%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=221055906&rft_id=info:pmid/&rft_sage_id=10.1177_1077546304039430&rfr_iscdi=true