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Active Disturbance Rejection Control for Drag-Free Satellites with Saturation-Constrainted Observations
The construction of the active disturbance rejection controller of the gravity satellite drag-free control system is inseparable from the design of the extended state observer to estimate the disturbance of the system. In practical applications, the observation of the relevant information by the sen...
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creator | Yang, Fei Diao, Jing-Dong |
description | The construction of the active disturbance rejection controller of the gravity satellite drag-free control system is inseparable from the design of the extended state observer to estimate the disturbance of the system. In practical applications, the observation of the relevant information by the sensor is subject to saturation constraint. This affects the estimation of the disturbance by the extended state observer, which in turn affects the performance of the drag-free control system. In this paper, the model of drag-free control system is firstly established, and then the set-valued state estimation theory is used to derive the extended state estimation algorithm under the condition of observation subject to saturation constraint, and it is applied to the estimation of the extended state of the gravity satellite drag-free control system based on the observation information of the acceleration sensor. In addition, the estimation results based on the acceleration sensor are combined with the estimation results based on the displacement sensor, which improves the estimation accuracy of the disturbance of the system. Finally, the gravity satellite active disturbance rejection drag-free controller is designed, and the simulation experiment has achieved good results. |
doi_str_mv | 10.23919/ChiCC.2019.8865733 |
format | conference_proceeding |
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In practical applications, the observation of the relevant information by the sensor is subject to saturation constraint. This affects the estimation of the disturbance by the extended state observer, which in turn affects the performance of the drag-free control system. In this paper, the model of drag-free control system is firstly established, and then the set-valued state estimation theory is used to derive the extended state estimation algorithm under the condition of observation subject to saturation constraint, and it is applied to the estimation of the extended state of the gravity satellite drag-free control system based on the observation information of the acceleration sensor. In addition, the estimation results based on the acceleration sensor are combined with the estimation results based on the displacement sensor, which improves the estimation accuracy of the disturbance of the system. Finally, the gravity satellite active disturbance rejection drag-free controller is designed, and the simulation experiment has achieved good results.</description><identifier>EISSN: 2161-2927</identifier><identifier>EISBN: 9789881563972</identifier><identifier>EISBN: 9881563976</identifier><identifier>DOI: 10.23919/ChiCC.2019.8865733</identifier><language>eng</language><publisher>Technical Committee on Control Theory, Chinese Association of Automation</publisher><subject>Acceleration ; active disturbance rejection control ; drag-free ; extended state estimation ; Gravity ; Mathematical model ; Observers ; Satellites ; saturation constraint</subject><ispartof>2019 Chinese Control Conference (CCC), 2019, p.4296-4301</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/8865733$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,27902,54530,54907</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/8865733$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Yang, Fei</creatorcontrib><creatorcontrib>Diao, Jing-Dong</creatorcontrib><title>Active Disturbance Rejection Control for Drag-Free Satellites with Saturation-Constrainted Observations</title><title>2019 Chinese Control Conference (CCC)</title><addtitle>ChiCC</addtitle><description>The construction of the active disturbance rejection controller of the gravity satellite drag-free control system is inseparable from the design of the extended state observer to estimate the disturbance of the system. In practical applications, the observation of the relevant information by the sensor is subject to saturation constraint. This affects the estimation of the disturbance by the extended state observer, which in turn affects the performance of the drag-free control system. In this paper, the model of drag-free control system is firstly established, and then the set-valued state estimation theory is used to derive the extended state estimation algorithm under the condition of observation subject to saturation constraint, and it is applied to the estimation of the extended state of the gravity satellite drag-free control system based on the observation information of the acceleration sensor. In addition, the estimation results based on the acceleration sensor are combined with the estimation results based on the displacement sensor, which improves the estimation accuracy of the disturbance of the system. Finally, the gravity satellite active disturbance rejection drag-free controller is designed, and the simulation experiment has achieved good results.</description><subject>Acceleration</subject><subject>active disturbance rejection control</subject><subject>drag-free</subject><subject>extended state estimation</subject><subject>Gravity</subject><subject>Mathematical model</subject><subject>Observers</subject><subject>Satellites</subject><subject>saturation constraint</subject><issn>2161-2927</issn><isbn>9789881563972</isbn><isbn>9881563976</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2019</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><recordid>eNotkM9OAjEYxKuJiYg8AZe-wK5tP9ptj2QRNSEh8c-ZtN1voWTdNW3B-PaCcprMTH5zGEKmnJUCDDcP9S7UdSkYN6XWSlYAV2RiKm205lKBqcQ1GQmueCGMqG7JXUp7xhQzHEZkO_c5HJEuQsqH6Gzvkb7iHk_p0NN66HMcOtoOkS6i3RbLiEjfbMauCxkT_Q55d_aHaM9AcQJSjjb0GRu6dgnj8a9I9-SmtV3CyUXH5GP5-F4_F6v100s9XxVBMMgFBwuNAcFl610za5nxupLWeweqEbwBa60SXiA4I71qFTDPQTuJwooZkzAm0__dgIibrxg-bfzZXH6BX5vAWac</recordid><startdate>201907</startdate><enddate>201907</enddate><creator>Yang, Fei</creator><creator>Diao, Jing-Dong</creator><general>Technical Committee on Control Theory, Chinese Association of Automation</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>201907</creationdate><title>Active Disturbance Rejection Control for Drag-Free Satellites with Saturation-Constrainted Observations</title><author>Yang, Fei ; Diao, Jing-Dong</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i203t-13a3d93215fcbd4f09c875accb36d21d3aaa62c2e3b95c6f630c138b5e2a24053</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Acceleration</topic><topic>active disturbance rejection control</topic><topic>drag-free</topic><topic>extended state estimation</topic><topic>Gravity</topic><topic>Mathematical model</topic><topic>Observers</topic><topic>Satellites</topic><topic>saturation constraint</topic><toplevel>online_resources</toplevel><creatorcontrib>Yang, Fei</creatorcontrib><creatorcontrib>Diao, Jing-Dong</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Yang, Fei</au><au>Diao, Jing-Dong</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Active Disturbance Rejection Control for Drag-Free Satellites with Saturation-Constrainted Observations</atitle><btitle>2019 Chinese Control Conference (CCC)</btitle><stitle>ChiCC</stitle><date>2019-07</date><risdate>2019</risdate><spage>4296</spage><epage>4301</epage><pages>4296-4301</pages><eissn>2161-2927</eissn><eisbn>9789881563972</eisbn><eisbn>9881563976</eisbn><abstract>The construction of the active disturbance rejection controller of the gravity satellite drag-free control system is inseparable from the design of the extended state observer to estimate the disturbance of the system. In practical applications, the observation of the relevant information by the sensor is subject to saturation constraint. This affects the estimation of the disturbance by the extended state observer, which in turn affects the performance of the drag-free control system. In this paper, the model of drag-free control system is firstly established, and then the set-valued state estimation theory is used to derive the extended state estimation algorithm under the condition of observation subject to saturation constraint, and it is applied to the estimation of the extended state of the gravity satellite drag-free control system based on the observation information of the acceleration sensor. In addition, the estimation results based on the acceleration sensor are combined with the estimation results based on the displacement sensor, which improves the estimation accuracy of the disturbance of the system. Finally, the gravity satellite active disturbance rejection drag-free controller is designed, and the simulation experiment has achieved good results.</abstract><pub>Technical Committee on Control Theory, Chinese Association of Automation</pub><doi>10.23919/ChiCC.2019.8865733</doi><tpages>6</tpages></addata></record> |
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subjects | Acceleration active disturbance rejection control drag-free extended state estimation Gravity Mathematical model Observers Satellites saturation constraint |
title | Active Disturbance Rejection Control for Drag-Free Satellites with Saturation-Constrainted Observations |
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