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...
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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 |
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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 |
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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. 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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 & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & 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> |
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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 |
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