Fault-Tolerant Attitude Stabilization for Satellites Without Rate Sensor
A fault-tolerant control approach without rate sensors is presented for the attitude stabilization of a satellite being developed. External disturbances, reaction wheel faults, actuator saturation, and unavailable angular velocity are addressed. A sliding-mode observer is proposed by using attitude...
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| Veröffentlicht in: | IEEE transactions on industrial electronics (1982) 2015-11, Vol.62 (11), p.7191-7202 |
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| container_title | IEEE transactions on industrial electronics (1982) |
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| creator | Xiao, Bing Huo, Mingyi Yang, Xuebo Zhang, Youmin |
| description | A fault-tolerant control approach without rate sensors is presented for the attitude stabilization of a satellite being developed. External disturbances, reaction wheel faults, actuator saturation, and unavailable angular velocity are addressed. A sliding-mode observer is proposed by using attitude feedback only, and the unavailable angular velocity is estimated by this observer in finite time. Using the attitude and the estimated velocity, another sliding-mode observer is proposed to reconstruct actuator faults and disturbances. It is proven that reconstruction with zero observer error is achieved in finite time. With the reconstructed value, a velocity-free controller is then developed to asymptotically stabilize the attitude. Simulation results are also provided to verify the effectiveness of the proposed approach. |
| doi_str_mv | 10.1109/TIE.2015.2432107 |
| format | Article |
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External disturbances, reaction wheel faults, actuator saturation, and unavailable angular velocity are addressed. A sliding-mode observer is proposed by using attitude feedback only, and the unavailable angular velocity is estimated by this observer in finite time. Using the attitude and the estimated velocity, another sliding-mode observer is proposed to reconstruct actuator faults and disturbances. It is proven that reconstruction with zero observer error is achieved in finite time. With the reconstructed value, a velocity-free controller is then developed to asymptotically stabilize the attitude. Simulation results are also provided to verify the effectiveness of the proposed approach.</description><identifier>ISSN: 0278-0046</identifier><identifier>EISSN: 1557-9948</identifier><identifier>DOI: 10.1109/TIE.2015.2432107</identifier><identifier>CODEN: ITIED6</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Actuators ; Angular velocity ; Attitude control ; Attitude stability ; Attitude stabilization ; Disturbances ; fault reconstruction ; Fault tolerance ; fault tolerant control ; Mathematical analysis ; Observers ; Satellites ; Sensors ; sliding mode observer ; Torque ; Wheels</subject><ispartof>IEEE transactions on industrial electronics (1982), 2015-11, Vol.62 (11), p.7191-7202</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) Nov 2015</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c324t-61e8e4fdc3ccabc67fe2e45753f06e2604da2cada20bccae34c69cf9352ec7423</citedby><cites>FETCH-LOGICAL-c324t-61e8e4fdc3ccabc67fe2e45753f06e2604da2cada20bccae34c69cf9352ec7423</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/7105920$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,780,784,796,27924,27925,54758</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/7105920$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Xiao, Bing</creatorcontrib><creatorcontrib>Huo, Mingyi</creatorcontrib><creatorcontrib>Yang, Xuebo</creatorcontrib><creatorcontrib>Zhang, Youmin</creatorcontrib><title>Fault-Tolerant Attitude Stabilization for Satellites Without Rate Sensor</title><title>IEEE transactions on industrial electronics (1982)</title><addtitle>TIE</addtitle><description>A fault-tolerant control approach without rate sensors is presented for the attitude stabilization of a satellite being developed. External disturbances, reaction wheel faults, actuator saturation, and unavailable angular velocity are addressed. A sliding-mode observer is proposed by using attitude feedback only, and the unavailable angular velocity is estimated by this observer in finite time. Using the attitude and the estimated velocity, another sliding-mode observer is proposed to reconstruct actuator faults and disturbances. It is proven that reconstruction with zero observer error is achieved in finite time. With the reconstructed value, a velocity-free controller is then developed to asymptotically stabilize the attitude. Simulation results are also provided to verify the effectiveness of the proposed approach.</description><subject>Actuators</subject><subject>Angular velocity</subject><subject>Attitude control</subject><subject>Attitude stability</subject><subject>Attitude stabilization</subject><subject>Disturbances</subject><subject>fault reconstruction</subject><subject>Fault tolerance</subject><subject>fault tolerant control</subject><subject>Mathematical analysis</subject><subject>Observers</subject><subject>Satellites</subject><subject>Sensors</subject><subject>sliding mode observer</subject><subject>Torque</subject><subject>Wheels</subject><issn>0278-0046</issn><issn>1557-9948</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNpdkE1LAzEQhoMoWD_ugpcFL162Tr42m6NI1YIg2IrHkKazmLJuNMke9Neb0uLBywwMzzu8PIRcUJhSCvpmOZ9NGVA5ZYIzCuqATKiUqtZatIdkAky1NYBojslJShsAKiSVE_J4b8c-18vQY7RDrm5z9nlcY7XIduV7_2OzD0PVhVgtbMa-9xlT9ebzexhz9VJO1QKHFOIZOepsn_B8v0_J6_1sefdYPz0_zO9un2rHmch1Q7FF0a0dd86uXKM6ZCikkryDBlkDYm2Zs2XAqhDIhWu06zSXDJ0SjJ-S693fzxi-RkzZfPjkSjE7YBiToUq1wDVwWtCrf-gmjHEo7QrFNGOSNbpQsKNcDClF7Mxn9B82fhsKZqvWFLVmq9bs1ZbI5S7iEfEPVxSkZsB_AZbidRo</recordid><startdate>201511</startdate><enddate>201511</enddate><creator>Xiao, Bing</creator><creator>Huo, Mingyi</creator><creator>Yang, Xuebo</creator><creator>Zhang, Youmin</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</general><scope>97E</scope><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>8FD</scope><scope>L7M</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope></search><sort><creationdate>201511</creationdate><title>Fault-Tolerant Attitude Stabilization for Satellites Without Rate Sensor</title><author>Xiao, Bing ; Huo, Mingyi ; Yang, Xuebo ; Zhang, Youmin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c324t-61e8e4fdc3ccabc67fe2e45753f06e2604da2cada20bccae34c69cf9352ec7423</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Actuators</topic><topic>Angular velocity</topic><topic>Attitude control</topic><topic>Attitude stability</topic><topic>Attitude stabilization</topic><topic>Disturbances</topic><topic>fault reconstruction</topic><topic>Fault tolerance</topic><topic>fault tolerant control</topic><topic>Mathematical analysis</topic><topic>Observers</topic><topic>Satellites</topic><topic>Sensors</topic><topic>sliding mode observer</topic><topic>Torque</topic><topic>Wheels</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Xiao, Bing</creatorcontrib><creatorcontrib>Huo, Mingyi</creatorcontrib><creatorcontrib>Yang, Xuebo</creatorcontrib><creatorcontrib>Zhang, Youmin</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 2005-present</collection><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Electronic Library (IEL)</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Technology Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><jtitle>IEEE transactions on industrial electronics (1982)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Xiao, Bing</au><au>Huo, Mingyi</au><au>Yang, Xuebo</au><au>Zhang, Youmin</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fault-Tolerant Attitude Stabilization for Satellites Without Rate Sensor</atitle><jtitle>IEEE transactions on industrial electronics (1982)</jtitle><stitle>TIE</stitle><date>2015-11</date><risdate>2015</risdate><volume>62</volume><issue>11</issue><spage>7191</spage><epage>7202</epage><pages>7191-7202</pages><issn>0278-0046</issn><eissn>1557-9948</eissn><coden>ITIED6</coden><abstract>A fault-tolerant control approach without rate sensors is presented for the attitude stabilization of a satellite being developed. External disturbances, reaction wheel faults, actuator saturation, and unavailable angular velocity are addressed. A sliding-mode observer is proposed by using attitude feedback only, and the unavailable angular velocity is estimated by this observer in finite time. Using the attitude and the estimated velocity, another sliding-mode observer is proposed to reconstruct actuator faults and disturbances. It is proven that reconstruction with zero observer error is achieved in finite time. With the reconstructed value, a velocity-free controller is then developed to asymptotically stabilize the attitude. Simulation results are also provided to verify the effectiveness of the proposed approach.</abstract><cop>New York</cop><pub>IEEE</pub><doi>10.1109/TIE.2015.2432107</doi><tpages>12</tpages></addata></record> |
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| ispartof | IEEE transactions on industrial electronics (1982), 2015-11, Vol.62 (11), p.7191-7202 |
| issn | 0278-0046 1557-9948 |
| language | eng |
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| source | IEEE Electronic Library (IEL) |
| subjects | Actuators Angular velocity Attitude control Attitude stability Attitude stabilization Disturbances fault reconstruction Fault tolerance fault tolerant control Mathematical analysis Observers Satellites Sensors sliding mode observer Torque Wheels |
| title | Fault-Tolerant Attitude Stabilization for Satellites Without Rate Sensor |
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