Application of Least Mean Square Algorithms to Spacecraft Vibration Compensation
This paper describes the application of the Least Mean Square (LMS) algorithm in tandem with the Filtered-X Least Mean Square algorithm for controlling a science instrument’s line-of-sight pointing. Pointing error is caused by a periodic disturbance and spacecraft vibration. A least mean square algo...
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Veröffentlicht in: | The Journal of the astronautical sciences 1998-01, Vol.46 (1), p.83-90 |
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creator | Woodard, Stanley E. Nagchaudhuri, Abhijit |
description | This paper describes the application of the Least Mean Square (LMS) algorithm in tandem with the Filtered-X Least Mean Square algorithm for controlling a science instrument’s line-of-sight pointing. Pointing error is caused by a periodic disturbance and spacecraft vibration. A least mean square algorithm is used on-orbit to produce the transfer function between the instrument’s servo-mechanism and error sensor. The result is a set of adaptive transversal filter weights tuned to the transfer function. The Filtered-X LMS algorithm, which is an extension of the LMS, tunes a set of transversal filter weights to the transfer function between the disturbance source and the servo-mechanism’s actuation signal. The servo-mechanism’s resulting actuation counters the disturbance response and thus maintains accurate science instrumental pointing. A simulation model of the Upper Atmosphere Research Satellite is used to demonstrate the algorithms. |
doi_str_mv | 10.1007/BF03546194 |
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A simulation model of the Upper Atmosphere Research Satellite is used to demonstrate the algorithms.</description><subject>Actuation</subject><subject>Actuators</subject><subject>Adaptive filters</subject><subject>Algorithms</subject><subject>Computer simulation</subject><subject>Control equipment</subject><subject>Error analysis</subject><subject>Least squares approximations</subject><subject>Mean square values</subject><subject>Servomechanisms</subject><subject>Spacecraft</subject><subject>Spacecraft vibration</subject><subject>Transfer functions</subject><subject>Transversal filters</subject><subject>Upper atmosphere</subject><subject>Vibration control</subject><issn>0021-9142</issn><issn>2195-0571</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1998</creationdate><recordtype>article</recordtype><recordid>eNpdkE9Lw0AUxBdRsFYvfoIFD4IQffsnye6xFqtCRaHqNWy2L5qSZNPdzcFvb2oFwdPw4DePmSHknME1A8hvbhcgUpkxLQ_IhDOdJpDm7JBMADhLNJP8mJyEsAEQDDSbkJdZ3ze1NbF2HXUVXaIJkT6h6ehqOxiPdNZ8OF_HzzbQ6OiqNxatN1Wk73Xp9765a3vsws9xSo4q0wQ8-9UpeVvcvc4fkuXz_eN8tkwslyomolKIVWXXypYouMpQMZYZ1Lgek2pIda7KErThigHmViBwa9NdjfVoUmJKLvd_e--2A4ZYtHWw2DSmQzeEIpeplpxrNpIX_8iNG3w3hiu4FJlkGcgddbWnrHcheKyK3tet8V8Fg2K3bfG3rfgGb79q4g</recordid><startdate>19980101</startdate><enddate>19980101</enddate><creator>Woodard, Stanley E.</creator><creator>Nagchaudhuri, Abhijit</creator><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TC</scope></search><sort><creationdate>19980101</creationdate><title>Application of Least Mean Square Algorithms to Spacecraft Vibration Compensation</title><author>Woodard, Stanley E. ; Nagchaudhuri, Abhijit</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c248t-3f8eeffcd8cbe3286e8116ae9ed021905978bb09a2810e7c3e02cc50021dcd883</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1998</creationdate><topic>Actuation</topic><topic>Actuators</topic><topic>Adaptive filters</topic><topic>Algorithms</topic><topic>Computer simulation</topic><topic>Control equipment</topic><topic>Error analysis</topic><topic>Least squares approximations</topic><topic>Mean square values</topic><topic>Servomechanisms</topic><topic>Spacecraft</topic><topic>Spacecraft vibration</topic><topic>Transfer functions</topic><topic>Transversal filters</topic><topic>Upper atmosphere</topic><topic>Vibration control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Woodard, Stanley E.</creatorcontrib><creatorcontrib>Nagchaudhuri, Abhijit</creatorcontrib><collection>CrossRef</collection><collection>Mechanical Engineering Abstracts</collection><jtitle>The Journal of the astronautical sciences</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Woodard, Stanley E.</au><au>Nagchaudhuri, Abhijit</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Application of Least Mean Square Algorithms to Spacecraft Vibration Compensation</atitle><jtitle>The Journal of the astronautical sciences</jtitle><date>1998-01-01</date><risdate>1998</risdate><volume>46</volume><issue>1</issue><spage>83</spage><epage>90</epage><pages>83-90</pages><issn>0021-9142</issn><eissn>2195-0571</eissn><abstract>This paper describes the application of the Least Mean Square (LMS) algorithm in tandem with the Filtered-X Least Mean Square algorithm for controlling a science instrument’s line-of-sight pointing. 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subjects | Actuation Actuators Adaptive filters Algorithms Computer simulation Control equipment Error analysis Least squares approximations Mean square values Servomechanisms Spacecraft Spacecraft vibration Transfer functions Transversal filters Upper atmosphere Vibration control |
title | Application of Least Mean Square Algorithms to Spacecraft Vibration Compensation |
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