Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect

In order to solve the attitude control problem of flexible hypersonic vehicles with consideration of aeroservoelastic effect, uncertainty and external disturbance, a novel moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme is presented in this paper. First, the mea...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2021-09, Vol.235 (12), p.1566-1585
Hauptverfasser: Chen, Erkang, Jing, Wuxing, Gao, Changsheng
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 1585
container_issue 12
container_start_page 1566
container_title Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering
container_volume 235
creator Chen, Erkang
Jing, Wuxing
Gao, Changsheng
description In order to solve the attitude control problem of flexible hypersonic vehicles with consideration of aeroservoelastic effect, uncertainty and external disturbance, a novel moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme is presented in this paper. First, the measurement model considering flexibility is established and the influence of aeroservoelastic effect on system stability is analyzed. Then moving horizon estimator is developed to reconstruct full state information from sensor measurements, while sliding mode disturbance observer and gain adaptation law is proposed to enhance the robustness and attenuate the chattering. Via combining moving horizon estimator, sliding mode disturbance observer, gain adaptation law and baseline hierarchical sliding mode controller, the moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme that is able to achieve the control objective of both precise attitude control and active flexible vibration suppression is developed. Finally, Lyapunov theory is used to prove the stability of the proposed control scheme, and the numerical simulations are carried out, which further verify the effectiveness of the proposed control scheme against aeroservoelastic effect, uncertainty and external disturbance.
doi_str_mv 10.1177/0954410020977553
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2569990473</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_0954410020977553</sage_id><sourcerecordid>2569990473</sourcerecordid><originalsourceid>FETCH-LOGICAL-c309t-282200c79d95f7c5aec3a4019db3ddd4ec9a19990849052f267a1f88f7ffdfe23</originalsourceid><addsrcrecordid>eNp1kE1LAzEQhoMoWKt3jwHP0SS7aTZHKX5BxYuelzSZtCnbzZpsF-vf8A-bpYIgOJc5zPPMJC9Cl4xeMyblDVWiLBmlnCophSiO0ITTkpGCcnGMJuOYjPNTdJbShuYSs2KCvp7D4NsVWYfoP0NLIPV-q_sQiW97WEXdg8Xa6q73A-C1h6ijWXujG5wab7OKt8ECNqHtY2iwCxG7Bj78ssn4voOYQusNHiBLDaQRTN5CHE0NMSSIQ4BG57sGg3Ng-nN04nST4OKnT9Hb_d3r_JEsXh6e5rcLYgqqesIrzik1UlklnDRCgyl0SZmyy8JaW4JRmimlaFUqKrjjM6mZqyonnbMOeDFFV4e9XQzvu_zzehN2sc0nay5mo1nKIlP0QJn82BTB1V3MEcV9zWg9Rl__jT4r5KAkvYLfpf_y301fiAU</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2569990473</pqid></control><display><type>article</type><title>Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect</title><source>SAGE Complete A-Z List</source><creator>Chen, Erkang ; Jing, Wuxing ; Gao, Changsheng</creator><creatorcontrib>Chen, Erkang ; Jing, Wuxing ; Gao, Changsheng</creatorcontrib><description>In order to solve the attitude control problem of flexible hypersonic vehicles with consideration of aeroservoelastic effect, uncertainty and external disturbance, a novel moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme is presented in this paper. First, the measurement model considering flexibility is established and the influence of aeroservoelastic effect on system stability is analyzed. Then moving horizon estimator is developed to reconstruct full state information from sensor measurements, while sliding mode disturbance observer and gain adaptation law is proposed to enhance the robustness and attenuate the chattering. Via combining moving horizon estimator, sliding mode disturbance observer, gain adaptation law and baseline hierarchical sliding mode controller, the moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme that is able to achieve the control objective of both precise attitude control and active flexible vibration suppression is developed. Finally, Lyapunov theory is used to prove the stability of the proposed control scheme, and the numerical simulations are carried out, which further verify the effectiveness of the proposed control scheme against aeroservoelastic effect, uncertainty and external disturbance.</description><identifier>ISSN: 0954-4100</identifier><identifier>EISSN: 2041-3025</identifier><identifier>DOI: 10.1177/0954410020977553</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Active control ; Adaptation ; Adaptive control ; Aeroservoelasticity ; Attitude control ; Control stability ; Disturbance observers ; Hypersonic vehicles ; Mathematical models ; Robustness (mathematics) ; Sliding mode control ; Stability analysis ; Systems stability ; Uncertainty ; Vibration control</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2021-09, Vol.235 (12), p.1566-1585</ispartof><rights>IMechE 2020</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c309t-282200c79d95f7c5aec3a4019db3ddd4ec9a19990849052f267a1f88f7ffdfe23</citedby><cites>FETCH-LOGICAL-c309t-282200c79d95f7c5aec3a4019db3ddd4ec9a19990849052f267a1f88f7ffdfe23</cites><orcidid>0000-0002-7374-2174</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0954410020977553$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0954410020977553$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,776,780,21799,27903,27904,43600,43601</link.rule.ids></links><search><creatorcontrib>Chen, Erkang</creatorcontrib><creatorcontrib>Jing, Wuxing</creatorcontrib><creatorcontrib>Gao, Changsheng</creatorcontrib><title>Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect</title><title>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</title><description>In order to solve the attitude control problem of flexible hypersonic vehicles with consideration of aeroservoelastic effect, uncertainty and external disturbance, a novel moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme is presented in this paper. First, the measurement model considering flexibility is established and the influence of aeroservoelastic effect on system stability is analyzed. Then moving horizon estimator is developed to reconstruct full state information from sensor measurements, while sliding mode disturbance observer and gain adaptation law is proposed to enhance the robustness and attenuate the chattering. Via combining moving horizon estimator, sliding mode disturbance observer, gain adaptation law and baseline hierarchical sliding mode controller, the moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme that is able to achieve the control objective of both precise attitude control and active flexible vibration suppression is developed. Finally, Lyapunov theory is used to prove the stability of the proposed control scheme, and the numerical simulations are carried out, which further verify the effectiveness of the proposed control scheme against aeroservoelastic effect, uncertainty and external disturbance.</description><subject>Active control</subject><subject>Adaptation</subject><subject>Adaptive control</subject><subject>Aeroservoelasticity</subject><subject>Attitude control</subject><subject>Control stability</subject><subject>Disturbance observers</subject><subject>Hypersonic vehicles</subject><subject>Mathematical models</subject><subject>Robustness (mathematics)</subject><subject>Sliding mode control</subject><subject>Stability analysis</subject><subject>Systems stability</subject><subject>Uncertainty</subject><subject>Vibration control</subject><issn>0954-4100</issn><issn>2041-3025</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp1kE1LAzEQhoMoWKt3jwHP0SS7aTZHKX5BxYuelzSZtCnbzZpsF-vf8A-bpYIgOJc5zPPMJC9Cl4xeMyblDVWiLBmlnCophSiO0ITTkpGCcnGMJuOYjPNTdJbShuYSs2KCvp7D4NsVWYfoP0NLIPV-q_sQiW97WEXdg8Xa6q73A-C1h6ijWXujG5wab7OKt8ECNqHtY2iwCxG7Bj78ssn4voOYQusNHiBLDaQRTN5CHE0NMSSIQ4BG57sGg3Ng-nN04nST4OKnT9Hb_d3r_JEsXh6e5rcLYgqqesIrzik1UlklnDRCgyl0SZmyy8JaW4JRmimlaFUqKrjjM6mZqyonnbMOeDFFV4e9XQzvu_zzehN2sc0nay5mo1nKIlP0QJn82BTB1V3MEcV9zWg9Rl__jT4r5KAkvYLfpf_y301fiAU</recordid><startdate>202109</startdate><enddate>202109</enddate><creator>Chen, Erkang</creator><creator>Jing, Wuxing</creator><creator>Gao, Changsheng</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0002-7374-2174</orcidid></search><sort><creationdate>202109</creationdate><title>Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect</title><author>Chen, Erkang ; Jing, Wuxing ; Gao, Changsheng</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c309t-282200c79d95f7c5aec3a4019db3ddd4ec9a19990849052f267a1f88f7ffdfe23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Active control</topic><topic>Adaptation</topic><topic>Adaptive control</topic><topic>Aeroservoelasticity</topic><topic>Attitude control</topic><topic>Control stability</topic><topic>Disturbance observers</topic><topic>Hypersonic vehicles</topic><topic>Mathematical models</topic><topic>Robustness (mathematics)</topic><topic>Sliding mode control</topic><topic>Stability analysis</topic><topic>Systems stability</topic><topic>Uncertainty</topic><topic>Vibration control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Erkang</creatorcontrib><creatorcontrib>Jing, Wuxing</creatorcontrib><creatorcontrib>Gao, Changsheng</creatorcontrib><collection>CrossRef</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology &amp; Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</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>Chen, Erkang</au><au>Jing, Wuxing</au><au>Gao, Changsheng</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect</atitle><jtitle>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</jtitle><date>2021-09</date><risdate>2021</risdate><volume>235</volume><issue>12</issue><spage>1566</spage><epage>1585</epage><pages>1566-1585</pages><issn>0954-4100</issn><eissn>2041-3025</eissn><abstract>In order to solve the attitude control problem of flexible hypersonic vehicles with consideration of aeroservoelastic effect, uncertainty and external disturbance, a novel moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme is presented in this paper. First, the measurement model considering flexibility is established and the influence of aeroservoelastic effect on system stability is analyzed. Then moving horizon estimator is developed to reconstruct full state information from sensor measurements, while sliding mode disturbance observer and gain adaptation law is proposed to enhance the robustness and attenuate the chattering. Via combining moving horizon estimator, sliding mode disturbance observer, gain adaptation law and baseline hierarchical sliding mode controller, the moving-horizon-estimator-integrated adaptive hierarchical sliding mode control scheme that is able to achieve the control objective of both precise attitude control and active flexible vibration suppression is developed. Finally, Lyapunov theory is used to prove the stability of the proposed control scheme, and the numerical simulations are carried out, which further verify the effectiveness of the proposed control scheme against aeroservoelastic effect, uncertainty and external disturbance.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0954410020977553</doi><tpages>20</tpages><orcidid>https://orcid.org/0000-0002-7374-2174</orcidid></addata></record>
fulltext fulltext
identifier ISSN: 0954-4100
ispartof Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2021-09, Vol.235 (12), p.1566-1585
issn 0954-4100
2041-3025
language eng
recordid cdi_proquest_journals_2569990473
source SAGE Complete A-Z List
subjects Active control
Adaptation
Adaptive control
Aeroservoelasticity
Attitude control
Control stability
Disturbance observers
Hypersonic vehicles
Mathematical models
Robustness (mathematics)
Sliding mode control
Stability analysis
Systems stability
Uncertainty
Vibration control
title Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T16%3A00%3A36IST&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=Moving-horizon-estimator-integrated%20adaptive%20hierarchical%20sliding%20mode%20control%20for%20flexible%20hypersonic%20vehicles%20considering%20aeroservoelastic%20effect&rft.jtitle=Proceedings%20of%20the%20Institution%20of%20Mechanical%20Engineers.%20Part%20G,%20Journal%20of%20aerospace%20engineering&rft.au=Chen,%20Erkang&rft.date=2021-09&rft.volume=235&rft.issue=12&rft.spage=1566&rft.epage=1585&rft.pages=1566-1585&rft.issn=0954-4100&rft.eissn=2041-3025&rft_id=info:doi/10.1177/0954410020977553&rft_dat=%3Cproquest_cross%3E2569990473%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=2569990473&rft_id=info:pmid/&rft_sage_id=10.1177_0954410020977553&rfr_iscdi=true