Robust adaptive backstepping tracking control for a flexible air-breathing hypersonic vehicle subject to input constraint
This paper presents a tracking control problem of flexible air-breathing hypersonic vehicle with input constraint and aerodynamic uncertainty. Without ignoring aero-propulsive and elevator-to-lift couplings, a control-oriented model including aerodynamic uncertainty is firstly established. Then a ro...
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Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2015-01, Vol.229 (1), p.10-25 |
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description | This paper presents a tracking control problem of flexible air-breathing hypersonic vehicle with input constraint and aerodynamic uncertainty. Without ignoring aero-propulsive and elevator-to-lift couplings, a control-oriented model including aerodynamic uncertainty is firstly established. Then a robust adaptive backstepping control scheme is designed, in which the control-oriented model does not need to be transformed into linear parameterization formulation. Upper bounds of the uncertain terms do not need to be known in advance, which are estimated online by designing robust adaptive laws. To further consider input constraint, a constrained robust adaptive backstepping controller is proposed to simultaneously handle input constraint and aerodynamic uncertainty. Finally, the compared simulation results show the effectiveness of the designed control strategy. |
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Without ignoring aero-propulsive and elevator-to-lift couplings, a control-oriented model including aerodynamic uncertainty is firstly established. Then a robust adaptive backstepping control scheme is designed, in which the control-oriented model does not need to be transformed into linear parameterization formulation. Upper bounds of the uncertain terms do not need to be known in advance, which are estimated online by designing robust adaptive laws. To further consider input constraint, a constrained robust adaptive backstepping controller is proposed to simultaneously handle input constraint and aerodynamic uncertainty. Finally, the compared simulation results show the effectiveness of the designed control strategy.</description><identifier>ISSN: 0954-4100</identifier><identifier>EISSN: 2041-3025</identifier><identifier>DOI: 10.1177/0954410014525128</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Adaptive control systems ; Aerodynamics ; Aerospace engineering ; Constraints ; Hypersonic vehicles ; Parametrization ; Simulation ; Tracking control ; Uncertainty</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2015-01, Vol.229 (1), p.10-25</ispartof><rights>IMechE 2014 Reprints and permissions: sagepub.co.uk/journalsPermissions.nav</rights><rights>Copyright SAGE PUBLICATIONS, INC. 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Part G, Journal of aerospace engineering</title><description>This paper presents a tracking control problem of flexible air-breathing hypersonic vehicle with input constraint and aerodynamic uncertainty. Without ignoring aero-propulsive and elevator-to-lift couplings, a control-oriented model including aerodynamic uncertainty is firstly established. Then a robust adaptive backstepping control scheme is designed, in which the control-oriented model does not need to be transformed into linear parameterization formulation. Upper bounds of the uncertain terms do not need to be known in advance, which are estimated online by designing robust adaptive laws. To further consider input constraint, a constrained robust adaptive backstepping controller is proposed to simultaneously handle input constraint and aerodynamic uncertainty. Finally, the compared simulation results show the effectiveness of the designed control strategy.</description><subject>Adaptive control systems</subject><subject>Aerodynamics</subject><subject>Aerospace engineering</subject><subject>Constraints</subject><subject>Hypersonic vehicles</subject><subject>Parametrization</subject><subject>Simulation</subject><subject>Tracking control</subject><subject>Uncertainty</subject><issn>0954-4100</issn><issn>2041-3025</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><recordid>eNp1kU1LxDAQhoMouK7ePQa8eKnmo2nToyx-wYIgei5pMt3N2m1qki7uvzdlPYjgXGaG95mXYQahS0puKC3LW1KJPKeE0FwwQZk8QjNGcppxwsQxmk1yNumn6CyEDUkhCj5D-1fXjCFiZdQQ7Q5wo_RHiDAMtl_h6FM3Fdr10bsOt85jhdsOvmzTAVbWZ40HFdcTtN4P4IPrrcY7WFudgDA2G9ARR4dtP4xxMgrJ1fbxHJ20qgtw8ZPn6P3h_m3xlC1fHp8Xd8tM85zFrC0IGFlVqjKKSyFAmrJsC6OaUnJDma4UKwwwTivJDGtMS6XmIKqWFoRxxefo-uA7ePc5Qoj11gYNXad6cGOoaVEQItPd8oRe_UE3bvR92i5ReV4KyUmZKHKgtHcheGjrwdut8vuaknr6Rf33F2kkO4wEtYJfpv_x30UIiqY</recordid><startdate>20150101</startdate><enddate>20150101</enddate><creator>Zong, Q</creator><creator>Wang, F</creator><creator>Su, R</creator><creator>Shao, SK</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></search><sort><creationdate>20150101</creationdate><title>Robust adaptive backstepping tracking control for a flexible air-breathing hypersonic vehicle subject to input constraint</title><author>Zong, Q ; Wang, F ; Su, R ; Shao, SK</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c342t-f60ed899a9da3855e8d77f6dab783d12c9a26de231982d2bdf18c3e59f16023a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Adaptive control systems</topic><topic>Aerodynamics</topic><topic>Aerospace engineering</topic><topic>Constraints</topic><topic>Hypersonic vehicles</topic><topic>Parametrization</topic><topic>Simulation</topic><topic>Tracking control</topic><topic>Uncertainty</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zong, Q</creatorcontrib><creatorcontrib>Wang, F</creatorcontrib><creatorcontrib>Su, R</creatorcontrib><creatorcontrib>Shao, SK</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. 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Without ignoring aero-propulsive and elevator-to-lift couplings, a control-oriented model including aerodynamic uncertainty is firstly established. Then a robust adaptive backstepping control scheme is designed, in which the control-oriented model does not need to be transformed into linear parameterization formulation. Upper bounds of the uncertain terms do not need to be known in advance, which are estimated online by designing robust adaptive laws. To further consider input constraint, a constrained robust adaptive backstepping controller is proposed to simultaneously handle input constraint and aerodynamic uncertainty. Finally, the compared simulation results show the effectiveness of the designed control strategy.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0954410014525128</doi><tpages>16</tpages></addata></record> |
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subjects | Adaptive control systems Aerodynamics Aerospace engineering Constraints Hypersonic vehicles Parametrization Simulation Tracking control Uncertainty |
title | Robust adaptive backstepping tracking control for a flexible air-breathing hypersonic vehicle subject to input constraint |
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