Switched H 2-state-feedback control with application to a fighter aircraft

This paper proposes two different H 2 -state-feedback controller synthesis algorithms for uncertain linear, time-varying, switched systems. The synthesis algorithms are based on a dwell-time approach, which makes use of time-varying parameter-dependent Lyapunov functions. The control laws consist of...

Full description

Saved in:
Bibliographic Details
Published in:Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2019-11, Vol.233 (14), p.5428-5437
Main Authors: Kemer, Emre, Başak, Hasan, Prempain, Emmanuel
Format: Article
Language:English
Citations: Items that this one cites
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites cdi_FETCH-LOGICAL-c164t-fca1ed28853181325fa9f97e80e31b3f7ea30ccf7b5921f623e6abbb290b040e3
container_end_page 5437
container_issue 14
container_start_page 5428
container_title Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering
container_volume 233
creator Kemer, Emre
Başak, Hasan
Prempain, Emmanuel
description This paper proposes two different H 2 -state-feedback controller synthesis algorithms for uncertain linear, time-varying, switched systems. The synthesis algorithms are based on a dwell-time approach, which makes use of time-varying parameter-dependent Lyapunov functions. The control laws consist of state-feedback controllers that are switched according to external signals. The proposed synthesis algorithms are then employed to design switched H 2 -state-feedback control laws for the longitudinal dynamics of the ADMIRE fighter benchmark model. The results obtained in simulation show the merits of the proposed approach.
doi_str_mv 10.1177/0954410019845981
format article
fullrecord <record><control><sourceid>sage_cross</sourceid><recordid>TN_cdi_crossref_primary_10_1177_0954410019845981</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_0954410019845981</sage_id><sourcerecordid>10.1177_0954410019845981</sourcerecordid><originalsourceid>FETCH-LOGICAL-c164t-fca1ed28853181325fa9f97e80e31b3f7ea30ccf7b5921f623e6abbb290b040e3</originalsourceid><addsrcrecordid>eNp1kE9LAzEQxYMoWKt3j_kC0Zlks7s5SvEvBQ_qeZmkk3Zr7ZYkIn57t9ST4LvM4f3e8HhCXCJcITbNNThbVQiArq2sa_FITDRUqAxoeywme1vt_VNxlvMaRtnaTMTTy1dfwooX8kFqlQsVVpF54Sm8yzBsSxo2ckRWkna7TR-o9MNWlkGSjP1yVThJ6lNIFMu5OIm0yXzxe6fi7e72dfag5s_3j7ObuQpYV0XFQMgL3bbWYItG20guuoZbYIPexIbJQAix8dZpjLU2XJP3XjvwUI3QVMDhb0hDzoljt0v9B6XvDqHbb9H93WKMqEMk05K79fCZtmPD__kfm-VeOw</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Switched H 2-state-feedback control with application to a fighter aircraft</title><source>IMechE_英国机械工程师协会期刊</source><creator>Kemer, Emre ; Başak, Hasan ; Prempain, Emmanuel</creator><creatorcontrib>Kemer, Emre ; Başak, Hasan ; Prempain, Emmanuel</creatorcontrib><description>This paper proposes two different H 2 -state-feedback controller synthesis algorithms for uncertain linear, time-varying, switched systems. The synthesis algorithms are based on a dwell-time approach, which makes use of time-varying parameter-dependent Lyapunov functions. The control laws consist of state-feedback controllers that are switched according to external signals. The proposed synthesis algorithms are then employed to design switched H 2 -state-feedback control laws for the longitudinal dynamics of the ADMIRE fighter benchmark model. The results obtained in simulation show the merits of the proposed approach.</description><identifier>ISSN: 0954-4100</identifier><identifier>EISSN: 2041-3025</identifier><identifier>DOI: 10.1177/0954410019845981</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><ispartof>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2019-11, Vol.233 (14), p.5428-5437</ispartof><rights>IMechE 2019</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c164t-fca1ed28853181325fa9f97e80e31b3f7ea30ccf7b5921f623e6abbb290b040e3</cites><orcidid>0000-0001-8716-1971</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0954410019845981$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0954410019845981$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,777,781,21894,27905,27906,45040,45428</link.rule.ids></links><search><creatorcontrib>Kemer, Emre</creatorcontrib><creatorcontrib>Başak, Hasan</creatorcontrib><creatorcontrib>Prempain, Emmanuel</creatorcontrib><title>Switched H 2-state-feedback control with application to a fighter aircraft</title><title>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</title><description>This paper proposes two different H 2 -state-feedback controller synthesis algorithms for uncertain linear, time-varying, switched systems. The synthesis algorithms are based on a dwell-time approach, which makes use of time-varying parameter-dependent Lyapunov functions. The control laws consist of state-feedback controllers that are switched according to external signals. The proposed synthesis algorithms are then employed to design switched H 2 -state-feedback control laws for the longitudinal dynamics of the ADMIRE fighter benchmark model. The results obtained in simulation show the merits of the proposed approach.</description><issn>0954-4100</issn><issn>2041-3025</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNp1kE9LAzEQxYMoWKt3j_kC0Zlks7s5SvEvBQ_qeZmkk3Zr7ZYkIn57t9ST4LvM4f3e8HhCXCJcITbNNThbVQiArq2sa_FITDRUqAxoeywme1vt_VNxlvMaRtnaTMTTy1dfwooX8kFqlQsVVpF54Sm8yzBsSxo2ckRWkna7TR-o9MNWlkGSjP1yVThJ6lNIFMu5OIm0yXzxe6fi7e72dfag5s_3j7ObuQpYV0XFQMgL3bbWYItG20guuoZbYIPexIbJQAix8dZpjLU2XJP3XjvwUI3QVMDhb0hDzoljt0v9B6XvDqHbb9H93WKMqEMk05K79fCZtmPD__kfm-VeOw</recordid><startdate>201911</startdate><enddate>201911</enddate><creator>Kemer, Emre</creator><creator>Başak, Hasan</creator><creator>Prempain, Emmanuel</creator><general>SAGE Publications</general><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0001-8716-1971</orcidid></search><sort><creationdate>201911</creationdate><title>Switched H 2-state-feedback control with application to a fighter aircraft</title><author>Kemer, Emre ; Başak, Hasan ; Prempain, Emmanuel</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c164t-fca1ed28853181325fa9f97e80e31b3f7ea30ccf7b5921f623e6abbb290b040e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kemer, Emre</creatorcontrib><creatorcontrib>Başak, Hasan</creatorcontrib><creatorcontrib>Prempain, Emmanuel</creatorcontrib><collection>CrossRef</collection><jtitle>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kemer, Emre</au><au>Başak, Hasan</au><au>Prempain, Emmanuel</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Switched H 2-state-feedback control with application to a fighter aircraft</atitle><jtitle>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</jtitle><date>2019-11</date><risdate>2019</risdate><volume>233</volume><issue>14</issue><spage>5428</spage><epage>5437</epage><pages>5428-5437</pages><issn>0954-4100</issn><eissn>2041-3025</eissn><abstract>This paper proposes two different H 2 -state-feedback controller synthesis algorithms for uncertain linear, time-varying, switched systems. The synthesis algorithms are based on a dwell-time approach, which makes use of time-varying parameter-dependent Lyapunov functions. The control laws consist of state-feedback controllers that are switched according to external signals. The proposed synthesis algorithms are then employed to design switched H 2 -state-feedback control laws for the longitudinal dynamics of the ADMIRE fighter benchmark model. The results obtained in simulation show the merits of the proposed approach.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0954410019845981</doi><tpages>10</tpages><orcidid>https://orcid.org/0000-0001-8716-1971</orcidid></addata></record>
fulltext fulltext
identifier ISSN: 0954-4100
ispartof Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2019-11, Vol.233 (14), p.5428-5437
issn 0954-4100
2041-3025
language eng
recordid cdi_crossref_primary_10_1177_0954410019845981
source IMechE_英国机械工程师协会期刊
title Switched H 2-state-feedback control with application to a fighter aircraft
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-19T19%3A44%3A52IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-sage_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Switched%20H%202-state-feedback%20control%20with%20application%20to%20a%20fighter%20aircraft&rft.jtitle=Proceedings%20of%20the%20Institution%20of%20Mechanical%20Engineers.%20Part%20G,%20Journal%20of%20aerospace%20engineering&rft.au=Kemer,%20Emre&rft.date=2019-11&rft.volume=233&rft.issue=14&rft.spage=5428&rft.epage=5437&rft.pages=5428-5437&rft.issn=0954-4100&rft.eissn=2041-3025&rft_id=info:doi/10.1177/0954410019845981&rft_dat=%3Csage_cross%3E10.1177_0954410019845981%3C/sage_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c164t-fca1ed28853181325fa9f97e80e31b3f7ea30ccf7b5921f623e6abbb290b040e3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rft_sage_id=10.1177_0954410019845981&rfr_iscdi=true