Integral sliding mode control of a quadrotor with fractional order reaching dynamics

We consider integral sliding mode control with a fractional order reaching law in this paper. The reaching law approach is followed and stability of the sliding manifold is shown graphically. We choose a quadrotor-type unmanned aerial vehicle (UAV) to validate the design. The attitude dynamics of th...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Transactions of the Institute of Measurement and Control 2011-12, Vol.33 (8), p.985-1003
1. Verfasser: Efe, Mehmet Önder
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 1003
container_issue 8
container_start_page 985
container_title Transactions of the Institute of Measurement and Control
container_volume 33
creator Efe, Mehmet Önder
description We consider integral sliding mode control with a fractional order reaching law in this paper. The reaching law approach is followed and stability of the sliding manifold is shown graphically. We choose a quadrotor-type unmanned aerial vehicle (UAV) to validate the design. The attitude dynamics of the vehicle is controlled by the proposed scheme and it is seen that the proposed form of the control system gives much better results compared with its integer order counterpart. The contribution of the study is to report a highly robust control scheme utilizing the fractional order differintegration operators.
doi_str_mv 10.1177/0142331210377227
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1010904927</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_0142331210377227</sage_id><sourcerecordid>1010904927</sourcerecordid><originalsourceid>FETCH-LOGICAL-c341t-e99b626f9118173b2f3e750e13c61c7b0462dc293d02aa8b54f51dc535c32ac63</originalsourceid><addsrcrecordid>eNp1kM9LwzAYhoMoOKd3j8GTl-r3JWmzHGX4YzDwMs8lTdKuo222pEX239syQRh4-g7v87zwvYTcIzwhSvkMKBjnyBC4lIzJCzJDIWUCPFOXZDbFyZRfk5sYdwAgRCZmZLPqelcF3dDY1LbuKtp666jxXR98Q31JNT0M2gbf-0C_635Ly6BNX_tudHywLtDgtNlOqj12uq1NvCVXpW6iu_u9c_L19rpZfiTrz_fV8mWdGC6wT5xSRcayUiEuUPKCldzJFBxyk6GRBYiMWcMUt8C0XhSpKFO0JuWp4UybjM_J46l3H_xhcLHP2zoa1zS6c36IOQKCAqGYHNGHM3TnhzD-EHOFjIEYW0cITpAJPsbgynwf6laH49iUTyvn5yuPSnJSoq7cX-e__A9m3nsG</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>912204535</pqid></control><display><type>article</type><title>Integral sliding mode control of a quadrotor with fractional order reaching dynamics</title><source>SAGE Complete A-Z List</source><creator>Efe, Mehmet Önder</creator><creatorcontrib>Efe, Mehmet Önder</creatorcontrib><description>We consider integral sliding mode control with a fractional order reaching law in this paper. The reaching law approach is followed and stability of the sliding manifold is shown graphically. We choose a quadrotor-type unmanned aerial vehicle (UAV) to validate the design. The attitude dynamics of the vehicle is controlled by the proposed scheme and it is seen that the proposed form of the control system gives much better results compared with its integer order counterpart. The contribution of the study is to report a highly robust control scheme utilizing the fractional order differintegration operators.</description><identifier>ISSN: 0142-3312</identifier><identifier>EISSN: 1477-0369</identifier><identifier>DOI: 10.1177/0142331210377227</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Control systems ; Design engineering ; Dynamical systems ; Dynamics ; Electrical engineering ; Integrals ; Law ; Sliding mode control ; Unmanned aerial vehicles</subject><ispartof>Transactions of the Institute of Measurement and Control, 2011-12, Vol.33 (8), p.985-1003</ispartof><rights>2010 The Institute of Measurement and Control</rights><rights>SAGE Publications © Dec 2011</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c341t-e99b626f9118173b2f3e750e13c61c7b0462dc293d02aa8b54f51dc535c32ac63</citedby><cites>FETCH-LOGICAL-c341t-e99b626f9118173b2f3e750e13c61c7b0462dc293d02aa8b54f51dc535c32ac63</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0142331210377227$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0142331210377227$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,778,782,21802,27907,27908,43604,43605</link.rule.ids></links><search><creatorcontrib>Efe, Mehmet Önder</creatorcontrib><title>Integral sliding mode control of a quadrotor with fractional order reaching dynamics</title><title>Transactions of the Institute of Measurement and Control</title><description>We consider integral sliding mode control with a fractional order reaching law in this paper. The reaching law approach is followed and stability of the sliding manifold is shown graphically. We choose a quadrotor-type unmanned aerial vehicle (UAV) to validate the design. The attitude dynamics of the vehicle is controlled by the proposed scheme and it is seen that the proposed form of the control system gives much better results compared with its integer order counterpart. The contribution of the study is to report a highly robust control scheme utilizing the fractional order differintegration operators.</description><subject>Control systems</subject><subject>Design engineering</subject><subject>Dynamical systems</subject><subject>Dynamics</subject><subject>Electrical engineering</subject><subject>Integrals</subject><subject>Law</subject><subject>Sliding mode control</subject><subject>Unmanned aerial vehicles</subject><issn>0142-3312</issn><issn>1477-0369</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><sourceid>GNUQQ</sourceid><recordid>eNp1kM9LwzAYhoMoOKd3j8GTl-r3JWmzHGX4YzDwMs8lTdKuo222pEX239syQRh4-g7v87zwvYTcIzwhSvkMKBjnyBC4lIzJCzJDIWUCPFOXZDbFyZRfk5sYdwAgRCZmZLPqelcF3dDY1LbuKtp666jxXR98Q31JNT0M2gbf-0C_635Ly6BNX_tudHywLtDgtNlOqj12uq1NvCVXpW6iu_u9c_L19rpZfiTrz_fV8mWdGC6wT5xSRcayUiEuUPKCldzJFBxyk6GRBYiMWcMUt8C0XhSpKFO0JuWp4UybjM_J46l3H_xhcLHP2zoa1zS6c36IOQKCAqGYHNGHM3TnhzD-EHOFjIEYW0cITpAJPsbgynwf6laH49iUTyvn5yuPSnJSoq7cX-e__A9m3nsG</recordid><startdate>20111201</startdate><enddate>20111201</enddate><creator>Efe, Mehmet Önder</creator><general>SAGE Publications</general><general>Sage Publications Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>3V.</scope><scope>7SP</scope><scope>7U5</scope><scope>7XB</scope><scope>88I</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>F28</scope><scope>FR3</scope><scope>GNUQQ</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>L7M</scope><scope>M2P</scope><scope>M7S</scope><scope>P5Z</scope><scope>P62</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope><scope>Q9U</scope><scope>S0W</scope><scope>H8D</scope></search><sort><creationdate>20111201</creationdate><title>Integral sliding mode control of a quadrotor with fractional order reaching dynamics</title><author>Efe, Mehmet Önder</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c341t-e99b626f9118173b2f3e750e13c61c7b0462dc293d02aa8b54f51dc535c32ac63</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Control systems</topic><topic>Design engineering</topic><topic>Dynamical systems</topic><topic>Dynamics</topic><topic>Electrical engineering</topic><topic>Integrals</topic><topic>Law</topic><topic>Sliding mode control</topic><topic>Unmanned aerial vehicles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Efe, Mehmet Önder</creatorcontrib><collection>CrossRef</collection><collection>ProQuest Central (Corporate)</collection><collection>Electronics &amp; Communications Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Science Database (Alumni Edition)</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>Materials Science &amp; Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies &amp; Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection (ProQuest)</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>ANTE: Abstracts in New Technology &amp; Engineering</collection><collection>Engineering Research Database</collection><collection>ProQuest Central Student</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Science Database (ProQuest)</collection><collection>Engineering Database</collection><collection>Advanced Technologies &amp; Aerospace Database</collection><collection>ProQuest Advanced Technologies &amp; Aerospace Collection</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><collection>ProQuest Central Basic</collection><collection>DELNET Engineering &amp; Technology Collection</collection><collection>Aerospace Database</collection><jtitle>Transactions of the Institute of Measurement and Control</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Efe, Mehmet Önder</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Integral sliding mode control of a quadrotor with fractional order reaching dynamics</atitle><jtitle>Transactions of the Institute of Measurement and Control</jtitle><date>2011-12-01</date><risdate>2011</risdate><volume>33</volume><issue>8</issue><spage>985</spage><epage>1003</epage><pages>985-1003</pages><issn>0142-3312</issn><eissn>1477-0369</eissn><abstract>We consider integral sliding mode control with a fractional order reaching law in this paper. The reaching law approach is followed and stability of the sliding manifold is shown graphically. We choose a quadrotor-type unmanned aerial vehicle (UAV) to validate the design. The attitude dynamics of the vehicle is controlled by the proposed scheme and it is seen that the proposed form of the control system gives much better results compared with its integer order counterpart. The contribution of the study is to report a highly robust control scheme utilizing the fractional order differintegration operators.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0142331210377227</doi><tpages>19</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0142-3312
ispartof Transactions of the Institute of Measurement and Control, 2011-12, Vol.33 (8), p.985-1003
issn 0142-3312
1477-0369
language eng
recordid cdi_proquest_miscellaneous_1010904927
source SAGE Complete A-Z List
subjects Control systems
Design engineering
Dynamical systems
Dynamics
Electrical engineering
Integrals
Law
Sliding mode control
Unmanned aerial vehicles
title Integral sliding mode control of a quadrotor with fractional order reaching dynamics
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T17%3A16%3A20IST&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=Integral%20sliding%20mode%20control%20of%20a%20quadrotor%20with%20fractional%20order%20reaching%20dynamics&rft.jtitle=Transactions%20of%20the%20Institute%20of%20Measurement%20and%20Control&rft.au=Efe,%20Mehmet%20%C3%96nder&rft.date=2011-12-01&rft.volume=33&rft.issue=8&rft.spage=985&rft.epage=1003&rft.pages=985-1003&rft.issn=0142-3312&rft.eissn=1477-0369&rft_id=info:doi/10.1177/0142331210377227&rft_dat=%3Cproquest_cross%3E1010904927%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=912204535&rft_id=info:pmid/&rft_sage_id=10.1177_0142331210377227&rfr_iscdi=true