Advanced actuators for the control of large space structures
The objective of this research was to develop advanced six-degree-of-freedom actuators employing magnetic suspensions suitable for the control of structural vibrations in large space structures. The advanced actuators consist of a magnetically suspended mass that has three-degrees-of-freedom in both...
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creator | Downer, James Hockney, Richard Johnson, Bruce Misovec, Kathleen |
description | The objective of this research was to develop advanced six-degree-of-freedom actuators employing magnetic suspensions suitable for the control of structural vibrations in large space structures. The advanced actuators consist of a magnetically suspended mass that has three-degrees-of-freedom in both translation and rotation. The most promising of these actuators featured a rotating suspended mass providing structural control torques in a manner similar to a control moment gyro (CMG). These actuators employ large-angle-magnetic suspensions that allow gimballing of the suspended mass without mechanical gimbals. Design definitions and sizing algorithms for these CMG type as well as angular reaction mass actuators based on multi-degree-of-freedom magnetic suspensions were developed. The performance of these actuators was analytically compared with conventional reaction mass actuators for a simple space structure model. |
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The advanced actuators consist of a magnetically suspended mass that has three-degrees-of-freedom in both translation and rotation. The most promising of these actuators featured a rotating suspended mass providing structural control torques in a manner similar to a control moment gyro (CMG). These actuators employ large-angle-magnetic suspensions that allow gimballing of the suspended mass without mechanical gimbals. Design definitions and sizing algorithms for these CMG type as well as angular reaction mass actuators based on multi-degree-of-freedom magnetic suspensions were developed. The performance of these actuators was analytically compared with conventional reaction mass actuators for a simple space structure model.</description><language>eng</language><publisher>Legacy CDMS</publisher><subject>Spacecraft Design, Testing And Performance</subject><creationdate>1993</creationdate><rights>Copyright Determination: GOV_PUBLIC_USE_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,776,796</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/19930018383$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Downer, James</creatorcontrib><creatorcontrib>Hockney, Richard</creatorcontrib><creatorcontrib>Johnson, Bruce</creatorcontrib><creatorcontrib>Misovec, Kathleen</creatorcontrib><title>Advanced actuators for the control of large space structures</title><description>The objective of this research was to develop advanced six-degree-of-freedom actuators employing magnetic suspensions suitable for the control of structural vibrations in large space structures. The advanced actuators consist of a magnetically suspended mass that has three-degrees-of-freedom in both translation and rotation. The most promising of these actuators featured a rotating suspended mass providing structural control torques in a manner similar to a control moment gyro (CMG). These actuators employ large-angle-magnetic suspensions that allow gimballing of the suspended mass without mechanical gimbals. Design definitions and sizing algorithms for these CMG type as well as angular reaction mass actuators based on multi-degree-of-freedom magnetic suspensions were developed. The performance of these actuators was analytically compared with conventional reaction mass actuators for a simple space structure model.</description><subject>Spacecraft Design, Testing And Performance</subject><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>1993</creationdate><recordtype>conference_proceeding</recordtype><sourceid>CYI</sourceid><recordid>eNrjZLBxTClLzEtOTVFITC4pTSzJLypWSMsvUijJSFVIzs8rKcrPUchPU8hJLEpPVSguSEwGkiVFpUC1RanFPAysaYk5xam8UJqbQcbNNcTZQzcvsTgxHqi5ON7Q0tLYwMDQwtjC2JiANAD1hivw</recordid><startdate>19930101</startdate><enddate>19930101</enddate><creator>Downer, James</creator><creator>Hockney, Richard</creator><creator>Johnson, Bruce</creator><creator>Misovec, Kathleen</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>19930101</creationdate><title>Advanced actuators for the control of large space structures</title><author>Downer, James ; Hockney, Richard ; Johnson, Bruce ; Misovec, Kathleen</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_199300183833</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>1993</creationdate><topic>Spacecraft Design, Testing And Performance</topic><toplevel>online_resources</toplevel><creatorcontrib>Downer, James</creatorcontrib><creatorcontrib>Hockney, Richard</creatorcontrib><creatorcontrib>Johnson, Bruce</creatorcontrib><creatorcontrib>Misovec, Kathleen</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Downer, James</au><au>Hockney, Richard</au><au>Johnson, Bruce</au><au>Misovec, Kathleen</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Advanced actuators for the control of large space structures</atitle><date>1993-01-01</date><risdate>1993</risdate><abstract>The objective of this research was to develop advanced six-degree-of-freedom actuators employing magnetic suspensions suitable for the control of structural vibrations in large space structures. The advanced actuators consist of a magnetically suspended mass that has three-degrees-of-freedom in both translation and rotation. The most promising of these actuators featured a rotating suspended mass providing structural control torques in a manner similar to a control moment gyro (CMG). These actuators employ large-angle-magnetic suspensions that allow gimballing of the suspended mass without mechanical gimbals. Design definitions and sizing algorithms for these CMG type as well as angular reaction mass actuators based on multi-degree-of-freedom magnetic suspensions were developed. The performance of these actuators was analytically compared with conventional reaction mass actuators for a simple space structure model.</abstract><cop>Legacy CDMS</cop><oa>free_for_read</oa></addata></record> |
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subjects | Spacecraft Design, Testing And Performance |
title | Advanced actuators for the control of large space structures |
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