Modeling and analysis of a viscoelastic micro-vibration isolation and mitigation platform for spacecraft
A new viscoelastic micro-vibration isolation and mitigation platform is proposed to reduce disturbances generated by flywheels on board spacecraft. Firstly, property tests on the high-damping viscoelastic material used in the micro-vibration isolation and mitigation element are conducted. Experiment...
Gespeichert in:
| Veröffentlicht in: | Journal of vibration and control 2018-09, Vol.24 (18), p.4337-4352 |
|---|---|
| Hauptverfasser: | , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 4352 |
|---|---|
| container_issue | 18 |
| container_start_page | 4337 |
| container_title | Journal of vibration and control |
| container_volume | 24 |
| creator | Xu, Chao Xu, Zhao-Dong Huang, Xing-Huai Xu, Ye-Shou Ge, Teng |
| description | A new viscoelastic micro-vibration isolation and mitigation platform is proposed to reduce disturbances generated by flywheels on board spacecraft. Firstly, property tests on the high-damping viscoelastic material used in the micro-vibration isolation and mitigation element are conducted. Experimental results show that the developed viscoelastic material has better energy dissipation capability under micro-vibration conditions. A mathematic model is employed to describe the dynamic properties of the high-damping viscoelastic material and is used to model the isolation and mitigation element. Secondly, a viscoelastic micro-vibration isolation and mitigation platform, which consists of four elements, is proposed and the analytical model of the coupled system that consists of the platform with flywheel is established. Finally, the isolation and mitigation performances of this micro-vibration isolation and mitigation platform are analyzed and discussed. The results show that the isolation and mitigation platform can effectively reduce the micro-vibration disturbances induced by the flywheel. |
| doi_str_mv | 10.1177/1077546317724321 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2098318138</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_1077546317724321</sage_id><sourcerecordid>2098318138</sourcerecordid><originalsourceid>FETCH-LOGICAL-c309t-dedfa698ebb81626e7e361973d4b5e720894f1318b835a1eb91f3233652d3fd73</originalsourceid><addsrcrecordid>eNp1UE1LxDAQDaLgunr3GPAczSRtPo6y-AUrXvRc0jZZs7SbmnQX9t-bUkEQPMzMm5n3HswgdA30FkDKO6BSloXgGbOCMzhBC5AFEKaVOM04r8m0P0cXKW0ppUUBdIE-X0NrO7_bYLNrc5jumHzCwWGDDz41wXYmjb7BvW9iIAdfRzP6sMM-hW5Gk7D3o9_M7ZDHLsQe54TTYBrbROPGS3TmTJfs1U9doo_Hh_fVM1m_Pb2s7tek4VSPpLWtM0IrW9cKBBNWWi5AS94WdWklo0oXDjioWvHSgK01OM44FyVruWslX6Kb2XeI4Wtv01htwz7mu1LFqFZZCVxlFp1Z-aiUonXVEH1v4rECWk3_rP7-M0vILElmY39N_-V_A_4Adcw</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2098318138</pqid></control><display><type>article</type><title>Modeling and analysis of a viscoelastic micro-vibration isolation and mitigation platform for spacecraft</title><source>SAGE Complete</source><creator>Xu, Chao ; Xu, Zhao-Dong ; Huang, Xing-Huai ; Xu, Ye-Shou ; Ge, Teng</creator><creatorcontrib>Xu, Chao ; Xu, Zhao-Dong ; Huang, Xing-Huai ; Xu, Ye-Shou ; Ge, Teng</creatorcontrib><description>A new viscoelastic micro-vibration isolation and mitigation platform is proposed to reduce disturbances generated by flywheels on board spacecraft. Firstly, property tests on the high-damping viscoelastic material used in the micro-vibration isolation and mitigation element are conducted. Experimental results show that the developed viscoelastic material has better energy dissipation capability under micro-vibration conditions. A mathematic model is employed to describe the dynamic properties of the high-damping viscoelastic material and is used to model the isolation and mitigation element. Secondly, a viscoelastic micro-vibration isolation and mitigation platform, which consists of four elements, is proposed and the analytical model of the coupled system that consists of the platform with flywheel is established. Finally, the isolation and mitigation performances of this micro-vibration isolation and mitigation platform are analyzed and discussed. The results show that the isolation and mitigation platform can effectively reduce the micro-vibration disturbances induced by the flywheel.</description><identifier>ISSN: 1077-5463</identifier><identifier>EISSN: 1741-2986</identifier><identifier>DOI: 10.1177/1077546317724321</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Damping ; Disturbances ; Energy dissipation ; Flywheels ; Mathematical models ; Mitigation ; Spacecraft ; Vibration ; Vibration analysis ; Viscoelasticity</subject><ispartof>Journal of vibration and control, 2018-09, Vol.24 (18), p.4337-4352</ispartof><rights>The Author(s) 2017</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c309t-dedfa698ebb81626e7e361973d4b5e720894f1318b835a1eb91f3233652d3fd73</citedby><cites>FETCH-LOGICAL-c309t-dedfa698ebb81626e7e361973d4b5e720894f1318b835a1eb91f3233652d3fd73</cites><orcidid>0000-0003-0544-8253</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/1077546317724321$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/1077546317724321$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,776,780,21798,27901,27902,43597,43598</link.rule.ids></links><search><creatorcontrib>Xu, Chao</creatorcontrib><creatorcontrib>Xu, Zhao-Dong</creatorcontrib><creatorcontrib>Huang, Xing-Huai</creatorcontrib><creatorcontrib>Xu, Ye-Shou</creatorcontrib><creatorcontrib>Ge, Teng</creatorcontrib><title>Modeling and analysis of a viscoelastic micro-vibration isolation and mitigation platform for spacecraft</title><title>Journal of vibration and control</title><description>A new viscoelastic micro-vibration isolation and mitigation platform is proposed to reduce disturbances generated by flywheels on board spacecraft. Firstly, property tests on the high-damping viscoelastic material used in the micro-vibration isolation and mitigation element are conducted. Experimental results show that the developed viscoelastic material has better energy dissipation capability under micro-vibration conditions. A mathematic model is employed to describe the dynamic properties of the high-damping viscoelastic material and is used to model the isolation and mitigation element. Secondly, a viscoelastic micro-vibration isolation and mitigation platform, which consists of four elements, is proposed and the analytical model of the coupled system that consists of the platform with flywheel is established. Finally, the isolation and mitigation performances of this micro-vibration isolation and mitigation platform are analyzed and discussed. The results show that the isolation and mitigation platform can effectively reduce the micro-vibration disturbances induced by the flywheel.</description><subject>Damping</subject><subject>Disturbances</subject><subject>Energy dissipation</subject><subject>Flywheels</subject><subject>Mathematical models</subject><subject>Mitigation</subject><subject>Spacecraft</subject><subject>Vibration</subject><subject>Vibration analysis</subject><subject>Viscoelasticity</subject><issn>1077-5463</issn><issn>1741-2986</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNp1UE1LxDAQDaLgunr3GPAczSRtPo6y-AUrXvRc0jZZs7SbmnQX9t-bUkEQPMzMm5n3HswgdA30FkDKO6BSloXgGbOCMzhBC5AFEKaVOM04r8m0P0cXKW0ppUUBdIE-X0NrO7_bYLNrc5jumHzCwWGDDz41wXYmjb7BvW9iIAdfRzP6sMM-hW5Gk7D3o9_M7ZDHLsQe54TTYBrbROPGS3TmTJfs1U9doo_Hh_fVM1m_Pb2s7tek4VSPpLWtM0IrW9cKBBNWWi5AS94WdWklo0oXDjioWvHSgK01OM44FyVruWslX6Kb2XeI4Wtv01htwz7mu1LFqFZZCVxlFp1Z-aiUonXVEH1v4rECWk3_rP7-M0vILElmY39N_-V_A_4Adcw</recordid><startdate>201809</startdate><enddate>201809</enddate><creator>Xu, Chao</creator><creator>Xu, Zhao-Dong</creator><creator>Huang, Xing-Huai</creator><creator>Xu, Ye-Shou</creator><creator>Ge, Teng</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>JQ2</scope><scope>KR7</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0003-0544-8253</orcidid></search><sort><creationdate>201809</creationdate><title>Modeling and analysis of a viscoelastic micro-vibration isolation and mitigation platform for spacecraft</title><author>Xu, Chao ; Xu, Zhao-Dong ; Huang, Xing-Huai ; Xu, Ye-Shou ; Ge, Teng</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c309t-dedfa698ebb81626e7e361973d4b5e720894f1318b835a1eb91f3233652d3fd73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Damping</topic><topic>Disturbances</topic><topic>Energy dissipation</topic><topic>Flywheels</topic><topic>Mathematical models</topic><topic>Mitigation</topic><topic>Spacecraft</topic><topic>Vibration</topic><topic>Vibration analysis</topic><topic>Viscoelasticity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Xu, Chao</creatorcontrib><creatorcontrib>Xu, Zhao-Dong</creatorcontrib><creatorcontrib>Huang, Xing-Huai</creatorcontrib><creatorcontrib>Xu, Ye-Shou</creatorcontrib><creatorcontrib>Ge, Teng</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Journal of vibration and control</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Xu, Chao</au><au>Xu, Zhao-Dong</au><au>Huang, Xing-Huai</au><au>Xu, Ye-Shou</au><au>Ge, Teng</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Modeling and analysis of a viscoelastic micro-vibration isolation and mitigation platform for spacecraft</atitle><jtitle>Journal of vibration and control</jtitle><date>2018-09</date><risdate>2018</risdate><volume>24</volume><issue>18</issue><spage>4337</spage><epage>4352</epage><pages>4337-4352</pages><issn>1077-5463</issn><eissn>1741-2986</eissn><abstract>A new viscoelastic micro-vibration isolation and mitigation platform is proposed to reduce disturbances generated by flywheels on board spacecraft. Firstly, property tests on the high-damping viscoelastic material used in the micro-vibration isolation and mitigation element are conducted. Experimental results show that the developed viscoelastic material has better energy dissipation capability under micro-vibration conditions. A mathematic model is employed to describe the dynamic properties of the high-damping viscoelastic material and is used to model the isolation and mitigation element. Secondly, a viscoelastic micro-vibration isolation and mitigation platform, which consists of four elements, is proposed and the analytical model of the coupled system that consists of the platform with flywheel is established. Finally, the isolation and mitigation performances of this micro-vibration isolation and mitigation platform are analyzed and discussed. The results show that the isolation and mitigation platform can effectively reduce the micro-vibration disturbances induced by the flywheel.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/1077546317724321</doi><tpages>16</tpages><orcidid>https://orcid.org/0000-0003-0544-8253</orcidid></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1077-5463 |
| ispartof | Journal of vibration and control, 2018-09, Vol.24 (18), p.4337-4352 |
| issn | 1077-5463 1741-2986 |
| language | eng |
| recordid | cdi_proquest_journals_2098318138 |
| source | SAGE Complete |
| subjects | Damping Disturbances Energy dissipation Flywheels Mathematical models Mitigation Spacecraft Vibration Vibration analysis Viscoelasticity |
| title | Modeling and analysis of a viscoelastic micro-vibration isolation and mitigation platform for spacecraft |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-08T02%3A58%3A30IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Modeling%20and%20analysis%20of%20a%20viscoelastic%20micro-vibration%20isolation%20and%20mitigation%20platform%20for%20spacecraft&rft.jtitle=Journal%20of%20vibration%20and%20control&rft.au=Xu,%20Chao&rft.date=2018-09&rft.volume=24&rft.issue=18&rft.spage=4337&rft.epage=4352&rft.pages=4337-4352&rft.issn=1077-5463&rft.eissn=1741-2986&rft_id=info:doi/10.1177/1077546317724321&rft_dat=%3Cproquest_cross%3E2098318138%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2098318138&rft_id=info:pmid/&rft_sage_id=10.1177_1077546317724321&rfr_iscdi=true |