Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach
This study proposes a novel fault accommodation scheme for the strong coupled attitude system of the hypersonic reentry vehicle (HRV) with both actuator drift and loss of efficiency. A general coupling/fault/uncertainty effect-triggered control concept is first introduced for the HRV attitude tracki...
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| Veröffentlicht in: | Nonlinear dynamics 2021-02, Vol.103 (3), p.2605-2625 |
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| container_title | Nonlinear dynamics |
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| creator | Chang, Jing Guo, Zongyi Cieslak, Jérôme Henry, David |
| description | This study proposes a novel fault accommodation scheme for the strong coupled attitude system of the hypersonic reentry vehicle (HRV) with both actuator drift and loss of efficiency. A general coupling/fault/uncertainty effect-triggered control concept is first introduced for the HRV attitude tracking system to improve its robustness and dynamic performance, which can be derived easily via Lyapunov stability. The design of such a control approach is based on an improved adaptive disturbance observer (ADO) to estimate the lumped uncertainties and actuator faults. The proposed scheme can achieve graceful degradation in tracking performance for the fault-tolerant control system by eliminating the detrimental uncertainty and actuator fault while keeping the beneficial uncertainty and actuator fault. A detailed design procedure has been presented with consideration of the implementation problem. Simulation results obtained on the HRV have demonstrated the effectiveness of the approach proposed. |
| doi_str_mv | 10.1007/s11071-021-06237-1 |
| format | Article |
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A general coupling/fault/uncertainty effect-triggered control concept is first introduced for the HRV attitude tracking system to improve its robustness and dynamic performance, which can be derived easily via Lyapunov stability. The design of such a control approach is based on an improved adaptive disturbance observer (ADO) to estimate the lumped uncertainties and actuator faults. The proposed scheme can achieve graceful degradation in tracking performance for the fault-tolerant control system by eliminating the detrimental uncertainty and actuator fault while keeping the beneficial uncertainty and actuator fault. A detailed design procedure has been presented with consideration of the implementation problem. Simulation results obtained on the HRV have demonstrated the effectiveness of the approach proposed.</description><identifier>ISSN: 0924-090X</identifier><identifier>EISSN: 1573-269X</identifier><identifier>DOI: 10.1007/s11071-021-06237-1</identifier><language>eng</language><publisher>Dordrecht: Springer Netherlands</publisher><subject>Accommodation ; Actuators ; Adaptive control ; Automatic Control Engineering ; Automotive Engineering ; Classical Mechanics ; Computer Science ; Control ; Control stability ; Disturbance observers ; Dynamic stability ; Dynamical Systems ; Engineering ; Fault tolerance ; Hypersonic reentry ; Mechanical Engineering ; Original Paper ; Reentry ; Reentry vehicles ; Tracking systems ; Uncertainty ; Vibration</subject><ispartof>Nonlinear dynamics, 2021-02, Vol.103 (3), p.2605-2625</ispartof><rights>The Author(s), under exclusive licence to Springer Nature B.V. part of Springer Nature 2021</rights><rights>The Author(s), under exclusive licence to Springer Nature B.V. part of Springer Nature 2021.</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c353t-7b2d5bf3933ed7dc9f9bbe58825454f9642993a81d26acbfc28c118207c3e6053</citedby><cites>FETCH-LOGICAL-c353t-7b2d5bf3933ed7dc9f9bbe58825454f9642993a81d26acbfc28c118207c3e6053</cites><orcidid>0000-0001-6837-9924 ; 0000-0002-7166-1880 ; 0000-0001-7169-7704</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s11071-021-06237-1$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s11071-021-06237-1$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>230,314,776,780,881,27901,27902,41464,42533,51294</link.rule.ids><backlink>$$Uhttps://hal.science/hal-03111260$$DView record in HAL$$Hfree_for_read</backlink></links><search><creatorcontrib>Chang, Jing</creatorcontrib><creatorcontrib>Guo, Zongyi</creatorcontrib><creatorcontrib>Cieslak, Jérôme</creatorcontrib><creatorcontrib>Henry, David</creatorcontrib><title>Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach</title><title>Nonlinear dynamics</title><addtitle>Nonlinear Dyn</addtitle><description>This study proposes a novel fault accommodation scheme for the strong coupled attitude system of the hypersonic reentry vehicle (HRV) with both actuator drift and loss of efficiency. A general coupling/fault/uncertainty effect-triggered control concept is first introduced for the HRV attitude tracking system to improve its robustness and dynamic performance, which can be derived easily via Lyapunov stability. The design of such a control approach is based on an improved adaptive disturbance observer (ADO) to estimate the lumped uncertainties and actuator faults. The proposed scheme can achieve graceful degradation in tracking performance for the fault-tolerant control system by eliminating the detrimental uncertainty and actuator fault while keeping the beneficial uncertainty and actuator fault. A detailed design procedure has been presented with consideration of the implementation problem. Simulation results obtained on the HRV have demonstrated the effectiveness of the approach proposed.</description><subject>Accommodation</subject><subject>Actuators</subject><subject>Adaptive control</subject><subject>Automatic Control Engineering</subject><subject>Automotive Engineering</subject><subject>Classical Mechanics</subject><subject>Computer Science</subject><subject>Control</subject><subject>Control stability</subject><subject>Disturbance observers</subject><subject>Dynamic stability</subject><subject>Dynamical Systems</subject><subject>Engineering</subject><subject>Fault tolerance</subject><subject>Hypersonic reentry</subject><subject>Mechanical Engineering</subject><subject>Original Paper</subject><subject>Reentry</subject><subject>Reentry vehicles</subject><subject>Tracking systems</subject><subject>Uncertainty</subject><subject>Vibration</subject><issn>0924-090X</issn><issn>1573-269X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNp9kEFLwzAYhoMoOKd_wFPAk4fql6RtGm9jqBMGgijsFtI0XTu6ZibpYP_ezIrePIQPwvO-vDwIXRO4IwD83hMCnCRA48sp4wk5QROScZbQXKxO0QQETRMQsDpHF95vAIBRKCbIvNly8AHXaugCVlrb7dZWKrS2xz44Fcz6gG2NQ2OwM6YP7oD3pml1Zx6wwlXrw-BK1WuDjQ_tNgaS4Nr12jhTYbXbOat0c4nOatV5c_Vzp-jj6fF9vkiWr88v89ky0SxjIeElrbKyZoIxU_FKi1qUpcmKgmZpltYiT6kQTBWkornSZa1poQkpKHDNTA4Zm6LbsbdRndy5OMcdpFWtXMyW8vgHjBBCc9iTyN6MbJz4OcTxcmMH18d5kqaCM54xlkeKjpR21ntn6t9aAvKoXo7qZVQvv9XLYzUbQz7CfVTxV_1P6gseXYcj</recordid><startdate>20210201</startdate><enddate>20210201</enddate><creator>Chang, Jing</creator><creator>Guo, Zongyi</creator><creator>Cieslak, Jérôme</creator><creator>Henry, David</creator><general>Springer Netherlands</general><general>Springer Nature B.V</general><general>Springer Verlag</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M7S</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope><scope>1XC</scope><orcidid>https://orcid.org/0000-0001-6837-9924</orcidid><orcidid>https://orcid.org/0000-0002-7166-1880</orcidid><orcidid>https://orcid.org/0000-0001-7169-7704</orcidid></search><sort><creationdate>20210201</creationdate><title>Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach</title><author>Chang, Jing ; Guo, Zongyi ; Cieslak, Jérôme ; Henry, David</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c353t-7b2d5bf3933ed7dc9f9bbe58825454f9642993a81d26acbfc28c118207c3e6053</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Accommodation</topic><topic>Actuators</topic><topic>Adaptive control</topic><topic>Automatic Control Engineering</topic><topic>Automotive Engineering</topic><topic>Classical Mechanics</topic><topic>Computer Science</topic><topic>Control</topic><topic>Control stability</topic><topic>Disturbance observers</topic><topic>Dynamic stability</topic><topic>Dynamical Systems</topic><topic>Engineering</topic><topic>Fault tolerance</topic><topic>Hypersonic reentry</topic><topic>Mechanical Engineering</topic><topic>Original Paper</topic><topic>Reentry</topic><topic>Reentry vehicles</topic><topic>Tracking systems</topic><topic>Uncertainty</topic><topic>Vibration</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chang, Jing</creatorcontrib><creatorcontrib>Guo, Zongyi</creatorcontrib><creatorcontrib>Cieslak, Jérôme</creatorcontrib><creatorcontrib>Henry, David</creatorcontrib><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><collection>Hyper Article en Ligne (HAL)</collection><jtitle>Nonlinear dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chang, Jing</au><au>Guo, Zongyi</au><au>Cieslak, Jérôme</au><au>Henry, David</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach</atitle><jtitle>Nonlinear dynamics</jtitle><stitle>Nonlinear Dyn</stitle><date>2021-02-01</date><risdate>2021</risdate><volume>103</volume><issue>3</issue><spage>2605</spage><epage>2625</epage><pages>2605-2625</pages><issn>0924-090X</issn><eissn>1573-269X</eissn><abstract>This study proposes a novel fault accommodation scheme for the strong coupled attitude system of the hypersonic reentry vehicle (HRV) with both actuator drift and loss of efficiency. A general coupling/fault/uncertainty effect-triggered control concept is first introduced for the HRV attitude tracking system to improve its robustness and dynamic performance, which can be derived easily via Lyapunov stability. The design of such a control approach is based on an improved adaptive disturbance observer (ADO) to estimate the lumped uncertainties and actuator faults. The proposed scheme can achieve graceful degradation in tracking performance for the fault-tolerant control system by eliminating the detrimental uncertainty and actuator fault while keeping the beneficial uncertainty and actuator fault. A detailed design procedure has been presented with consideration of the implementation problem. 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| ispartof | Nonlinear dynamics, 2021-02, Vol.103 (3), p.2605-2625 |
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| source | Springer Nature - Complete Springer Journals |
| subjects | Accommodation Actuators Adaptive control Automatic Control Engineering Automotive Engineering Classical Mechanics Computer Science Control Control stability Disturbance observers Dynamic stability Dynamical Systems Engineering Fault tolerance Hypersonic reentry Mechanical Engineering Original Paper Reentry Reentry vehicles Tracking systems Uncertainty Vibration |
| title | Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach |
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