Chattering-free variable structure control with application to flight vehicles

Variable structure control (VSC) is a popular robust control method widely used to cope with uncertain system dynamics. Unfortunately, current VSC always comes with "chattering". Eliminating or alleviating such chattering has motivates numerous research efforts, but most proposed methods f...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Liao, X.H., Zhao Sun, Song, Y.D.
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 410
container_issue
container_start_page 406
container_title
container_volume
creator Liao, X.H.
Zhao Sun
Song, Y.D.
description Variable structure control (VSC) is a popular robust control method widely used to cope with uncertain system dynamics. Unfortunately, current VSC always comes with "chattering". Eliminating or alleviating such chattering has motivates numerous research efforts, but most proposed methods for chattering elimination are achieved at the price of control precision and additional heavy computations. In our recent paper (Y. D. Song, et al., March 2004) a novel approach is proposed to completely remove the chattering yet maintain asymptotical system stability. The design philosophy is to directly design the rate of the control (compensating) signal, so that the control input is readily obtained via integration. It is shown that the method can eliminate chattering without sacrificing control precise while at the same time ensuring a bounded and smooth control action. This paper extends the results in (Y. D. Song, et al., March 2004) to a more general higher order nonlinear system. Application of this method to heading direction tracking control of flight vehicles is simulated presented. The results with comparison to traditional VSC and VSC + smoothening are represented
doi_str_mv 10.1109/SSST.2006.1619093
format Conference Proceeding
fullrecord <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_1619093</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>1619093</ieee_id><sourcerecordid>1619093</sourcerecordid><originalsourceid>FETCH-LOGICAL-i90t-4a05691e0d74badc3fc5efd38bce9f027bb4004a705797f735292bc6ae1ba4283</originalsourceid><addsrcrecordid>eNotkMtqwzAUREUfUDfNB5Ru9AN2r16WtSymLwjtItkHSbmKVdzYyEpK_76GBgbmbOYshpB7BhVjYB7X6_Wm4gB1xWpmwIgLUvAZy4YJdUmWRjcwRxiptLoiBYCRJW9Mc0Nup-kL5mXNVUE-2s7mjCke9mVIiPRkU7SuRzrldPT5mJD64ZDT0NOfmDtqx7GP3uY4HGgeaOjjvsv0hF30PU535DrYfsLluRdk8_K8ad_K1efre_u0KqOBXEoLqjYMYaelszsvglcYdqJxHk0Arp2TANJqUNrooIXihjtfW2TOSt6IBXn410ZE3I4pftv0uz0_If4AjRtRvA</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Chattering-free variable structure control with application to flight vehicles</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Liao, X.H. ; Zhao Sun ; Song, Y.D.</creator><creatorcontrib>Liao, X.H. ; Zhao Sun ; Song, Y.D.</creatorcontrib><description>Variable structure control (VSC) is a popular robust control method widely used to cope with uncertain system dynamics. Unfortunately, current VSC always comes with "chattering". Eliminating or alleviating such chattering has motivates numerous research efforts, but most proposed methods for chattering elimination are achieved at the price of control precision and additional heavy computations. In our recent paper (Y. D. Song, et al., March 2004) a novel approach is proposed to completely remove the chattering yet maintain asymptotical system stability. The design philosophy is to directly design the rate of the control (compensating) signal, so that the control input is readily obtained via integration. It is shown that the method can eliminate chattering without sacrificing control precise while at the same time ensuring a bounded and smooth control action. This paper extends the results in (Y. D. Song, et al., March 2004) to a more general higher order nonlinear system. Application of this method to heading direction tracking control of flight vehicles is simulated presented. The results with comparison to traditional VSC and VSC + smoothening are represented</description><identifier>ISSN: 0094-2898</identifier><identifier>ISBN: 9780780394575</identifier><identifier>ISBN: 0780394577</identifier><identifier>EISSN: 2161-8135</identifier><identifier>DOI: 10.1109/SSST.2006.1619093</identifier><language>eng</language><publisher>IEEE</publisher><subject>Asymptotic stability ; Automotive electronics ; Control systems ; NASA ; Nonlinear systems ; Robust control ; Signal design ; Sun ; Switches ; Vehicles</subject><ispartof>2006 Proceeding of the Thirty-Eighth Southeastern Symposium on System Theory, 2006, p.406-410</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/1619093$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2052,4036,4037,27902,54895</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/1619093$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Liao, X.H.</creatorcontrib><creatorcontrib>Zhao Sun</creatorcontrib><creatorcontrib>Song, Y.D.</creatorcontrib><title>Chattering-free variable structure control with application to flight vehicles</title><title>2006 Proceeding of the Thirty-Eighth Southeastern Symposium on System Theory</title><addtitle>SSST</addtitle><description>Variable structure control (VSC) is a popular robust control method widely used to cope with uncertain system dynamics. Unfortunately, current VSC always comes with "chattering". Eliminating or alleviating such chattering has motivates numerous research efforts, but most proposed methods for chattering elimination are achieved at the price of control precision and additional heavy computations. In our recent paper (Y. D. Song, et al., March 2004) a novel approach is proposed to completely remove the chattering yet maintain asymptotical system stability. The design philosophy is to directly design the rate of the control (compensating) signal, so that the control input is readily obtained via integration. It is shown that the method can eliminate chattering without sacrificing control precise while at the same time ensuring a bounded and smooth control action. This paper extends the results in (Y. D. Song, et al., March 2004) to a more general higher order nonlinear system. Application of this method to heading direction tracking control of flight vehicles is simulated presented. The results with comparison to traditional VSC and VSC + smoothening are represented</description><subject>Asymptotic stability</subject><subject>Automotive electronics</subject><subject>Control systems</subject><subject>NASA</subject><subject>Nonlinear systems</subject><subject>Robust control</subject><subject>Signal design</subject><subject>Sun</subject><subject>Switches</subject><subject>Vehicles</subject><issn>0094-2898</issn><issn>2161-8135</issn><isbn>9780780394575</isbn><isbn>0780394577</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2006</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotkMtqwzAUREUfUDfNB5Ru9AN2r16WtSymLwjtItkHSbmKVdzYyEpK_76GBgbmbOYshpB7BhVjYB7X6_Wm4gB1xWpmwIgLUvAZy4YJdUmWRjcwRxiptLoiBYCRJW9Mc0Nup-kL5mXNVUE-2s7mjCke9mVIiPRkU7SuRzrldPT5mJD64ZDT0NOfmDtqx7GP3uY4HGgeaOjjvsv0hF30PU535DrYfsLluRdk8_K8ad_K1efre_u0KqOBXEoLqjYMYaelszsvglcYdqJxHk0Arp2TANJqUNrooIXihjtfW2TOSt6IBXn410ZE3I4pftv0uz0_If4AjRtRvA</recordid><startdate>2006</startdate><enddate>2006</enddate><creator>Liao, X.H.</creator><creator>Zhao Sun</creator><creator>Song, Y.D.</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope></search><sort><creationdate>2006</creationdate><title>Chattering-free variable structure control with application to flight vehicles</title><author>Liao, X.H. ; Zhao Sun ; Song, Y.D.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i90t-4a05691e0d74badc3fc5efd38bce9f027bb4004a705797f735292bc6ae1ba4283</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2006</creationdate><topic>Asymptotic stability</topic><topic>Automotive electronics</topic><topic>Control systems</topic><topic>NASA</topic><topic>Nonlinear systems</topic><topic>Robust control</topic><topic>Signal design</topic><topic>Sun</topic><topic>Switches</topic><topic>Vehicles</topic><toplevel>online_resources</toplevel><creatorcontrib>Liao, X.H.</creatorcontrib><creatorcontrib>Zhao Sun</creatorcontrib><creatorcontrib>Song, Y.D.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Liao, X.H.</au><au>Zhao Sun</au><au>Song, Y.D.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Chattering-free variable structure control with application to flight vehicles</atitle><btitle>2006 Proceeding of the Thirty-Eighth Southeastern Symposium on System Theory</btitle><stitle>SSST</stitle><date>2006</date><risdate>2006</risdate><spage>406</spage><epage>410</epage><pages>406-410</pages><issn>0094-2898</issn><eissn>2161-8135</eissn><isbn>9780780394575</isbn><isbn>0780394577</isbn><abstract>Variable structure control (VSC) is a popular robust control method widely used to cope with uncertain system dynamics. Unfortunately, current VSC always comes with "chattering". Eliminating or alleviating such chattering has motivates numerous research efforts, but most proposed methods for chattering elimination are achieved at the price of control precision and additional heavy computations. In our recent paper (Y. D. Song, et al., March 2004) a novel approach is proposed to completely remove the chattering yet maintain asymptotical system stability. The design philosophy is to directly design the rate of the control (compensating) signal, so that the control input is readily obtained via integration. It is shown that the method can eliminate chattering without sacrificing control precise while at the same time ensuring a bounded and smooth control action. This paper extends the results in (Y. D. Song, et al., March 2004) to a more general higher order nonlinear system. Application of this method to heading direction tracking control of flight vehicles is simulated presented. The results with comparison to traditional VSC and VSC + smoothening are represented</abstract><pub>IEEE</pub><doi>10.1109/SSST.2006.1619093</doi><tpages>5</tpages></addata></record>
fulltext fulltext_linktorsrc
identifier ISSN: 0094-2898
ispartof 2006 Proceeding of the Thirty-Eighth Southeastern Symposium on System Theory, 2006, p.406-410
issn 0094-2898
2161-8135
language eng
recordid cdi_ieee_primary_1619093
source IEEE Electronic Library (IEL) Conference Proceedings
subjects Asymptotic stability
Automotive electronics
Control systems
NASA
Nonlinear systems
Robust control
Signal design
Sun
Switches
Vehicles
title Chattering-free variable structure control with application to flight vehicles
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-15T20%3A11%3A24IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-ieee_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Chattering-free%20variable%20structure%20control%20with%20application%20to%20flight%20vehicles&rft.btitle=2006%20Proceeding%20of%20the%20Thirty-Eighth%20Southeastern%20Symposium%20on%20System%20Theory&rft.au=Liao,%20X.H.&rft.date=2006&rft.spage=406&rft.epage=410&rft.pages=406-410&rft.issn=0094-2898&rft.eissn=2161-8135&rft.isbn=9780780394575&rft.isbn_list=0780394577&rft_id=info:doi/10.1109/SSST.2006.1619093&rft_dat=%3Cieee_6IE%3E1619093%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=1619093&rfr_iscdi=true