Dynamic modeling and simulation of a flexible satellite
A novel dynamic equation of a flexible satellite with flexible appendages is developed based on the coupling deformation field, in which the second-order coupling term of axial displacement caused by that of transverse is included. Lagrangian principle and assumed mode method are used to derive the...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Tagungsbericht |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 1072 |
|---|---|
| container_issue | |
| container_start_page | 1068 |
| container_title | |
| container_volume | |
| creator | Shengjian Bai Xinsheng Huang Yuhao Liu |
| description | A novel dynamic equation of a flexible satellite with flexible appendages is developed based on the coupling deformation field, in which the second-order coupling term of axial displacement caused by that of transverse is included. Lagrangian principle and assumed mode method are used to derive the first-order approximate model of the multibody system. Theoretical analysis and numerical simulations show that the coupling term can have significant effect on the dynamic characteristics of the flexible system undergoing large rigid-body motion and the dynamic stiffening is accounted for. |
| doi_str_mv | 10.1109/ASC-ICSC.2008.4675523 |
| format | Conference Proceeding |
| fullrecord | <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_4675523</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>4675523</ieee_id><sourcerecordid>4675523</sourcerecordid><originalsourceid>FETCH-LOGICAL-i175t-c754605971e4d06ca0968f1de91a8a3c4b4052168b387d504bf488f33b25f2a13</originalsourceid><addsrcrecordid>eNo1j11LwzAYhSMy0M3-AhHyB1rzJm_yJpejfg0GXkyvR9omEklbWSu4f-_AeW4ODxweOIzdgagAhLtf7-pyU-_qSgphKzSktVQXrHBkASUikCV5yZb_YHDBlqctOUHKmCtWTNOnOAW1MmSuGT0cB9-nlvdjF3IaPrgfOj6l_jv7OY0DHyP3PObwk5oc-OTnkHOaww1bRJ-nUJx7xd6fHt_ql3L7-ryp19syAem5bEmjEdoRBOyEab1wxkboggNvvWqxQaElGNsoS50W2ES0NirVSB2lB7Vit3_eFELYfx1S7w_H_fm4-gXcQElV</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Dynamic modeling and simulation of a flexible satellite</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Shengjian Bai ; Xinsheng Huang ; Yuhao Liu</creator><creatorcontrib>Shengjian Bai ; Xinsheng Huang ; Yuhao Liu</creatorcontrib><description>A novel dynamic equation of a flexible satellite with flexible appendages is developed based on the coupling deformation field, in which the second-order coupling term of axial displacement caused by that of transverse is included. Lagrangian principle and assumed mode method are used to derive the first-order approximate model of the multibody system. Theoretical analysis and numerical simulations show that the coupling term can have significant effect on the dynamic characteristics of the flexible system undergoing large rigid-body motion and the dynamic stiffening is accounted for.</description><identifier>ISBN: 1424417864</identifier><identifier>ISBN: 9781424417865</identifier><identifier>EISBN: 9781424417872</identifier><identifier>EISBN: 1424417872</identifier><identifier>DOI: 10.1109/ASC-ICSC.2008.4675523</identifier><identifier>LCCN: 2007907366</identifier><language>eng</language><publisher>IEEE</publisher><subject>Deformable models ; Equations ; Finite element methods ; Flexible structures ; Linear approximation ; Motion analysis ; Nonlinear dynamical systems ; Numerical simulation ; Satellites ; Vehicle dynamics</subject><ispartof>2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing, 2008, p.1068-1072</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/4675523$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2052,27902,54895</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/4675523$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Shengjian Bai</creatorcontrib><creatorcontrib>Xinsheng Huang</creatorcontrib><creatorcontrib>Yuhao Liu</creatorcontrib><title>Dynamic modeling and simulation of a flexible satellite</title><title>2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing</title><addtitle>ASC-ICSC</addtitle><description>A novel dynamic equation of a flexible satellite with flexible appendages is developed based on the coupling deformation field, in which the second-order coupling term of axial displacement caused by that of transverse is included. Lagrangian principle and assumed mode method are used to derive the first-order approximate model of the multibody system. Theoretical analysis and numerical simulations show that the coupling term can have significant effect on the dynamic characteristics of the flexible system undergoing large rigid-body motion and the dynamic stiffening is accounted for.</description><subject>Deformable models</subject><subject>Equations</subject><subject>Finite element methods</subject><subject>Flexible structures</subject><subject>Linear approximation</subject><subject>Motion analysis</subject><subject>Nonlinear dynamical systems</subject><subject>Numerical simulation</subject><subject>Satellites</subject><subject>Vehicle dynamics</subject><isbn>1424417864</isbn><isbn>9781424417865</isbn><isbn>9781424417872</isbn><isbn>1424417872</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2008</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNo1j11LwzAYhSMy0M3-AhHyB1rzJm_yJpejfg0GXkyvR9omEklbWSu4f-_AeW4ODxweOIzdgagAhLtf7-pyU-_qSgphKzSktVQXrHBkASUikCV5yZb_YHDBlqctOUHKmCtWTNOnOAW1MmSuGT0cB9-nlvdjF3IaPrgfOj6l_jv7OY0DHyP3PObwk5oc-OTnkHOaww1bRJ-nUJx7xd6fHt_ql3L7-ryp19syAem5bEmjEdoRBOyEab1wxkboggNvvWqxQaElGNsoS50W2ES0NirVSB2lB7Vit3_eFELYfx1S7w_H_fm4-gXcQElV</recordid><startdate>200810</startdate><enddate>200810</enddate><creator>Shengjian Bai</creator><creator>Xinsheng Huang</creator><creator>Yuhao Liu</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>200810</creationdate><title>Dynamic modeling and simulation of a flexible satellite</title><author>Shengjian Bai ; Xinsheng Huang ; Yuhao Liu</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i175t-c754605971e4d06ca0968f1de91a8a3c4b4052168b387d504bf488f33b25f2a13</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2008</creationdate><topic>Deformable models</topic><topic>Equations</topic><topic>Finite element methods</topic><topic>Flexible structures</topic><topic>Linear approximation</topic><topic>Motion analysis</topic><topic>Nonlinear dynamical systems</topic><topic>Numerical simulation</topic><topic>Satellites</topic><topic>Vehicle dynamics</topic><toplevel>online_resources</toplevel><creatorcontrib>Shengjian Bai</creatorcontrib><creatorcontrib>Xinsheng Huang</creatorcontrib><creatorcontrib>Yuhao Liu</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>Shengjian Bai</au><au>Xinsheng Huang</au><au>Yuhao Liu</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Dynamic modeling and simulation of a flexible satellite</atitle><btitle>2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing</btitle><stitle>ASC-ICSC</stitle><date>2008-10</date><risdate>2008</risdate><spage>1068</spage><epage>1072</epage><pages>1068-1072</pages><isbn>1424417864</isbn><isbn>9781424417865</isbn><eisbn>9781424417872</eisbn><eisbn>1424417872</eisbn><abstract>A novel dynamic equation of a flexible satellite with flexible appendages is developed based on the coupling deformation field, in which the second-order coupling term of axial displacement caused by that of transverse is included. Lagrangian principle and assumed mode method are used to derive the first-order approximate model of the multibody system. Theoretical analysis and numerical simulations show that the coupling term can have significant effect on the dynamic characteristics of the flexible system undergoing large rigid-body motion and the dynamic stiffening is accounted for.</abstract><pub>IEEE</pub><doi>10.1109/ASC-ICSC.2008.4675523</doi><tpages>5</tpages></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | ISBN: 1424417864 |
| ispartof | 2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing, 2008, p.1068-1072 |
| issn | |
| language | eng |
| recordid | cdi_ieee_primary_4675523 |
| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Deformable models Equations Finite element methods Flexible structures Linear approximation Motion analysis Nonlinear dynamical systems Numerical simulation Satellites Vehicle dynamics |
| title | Dynamic modeling and simulation of a flexible satellite |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-02T22%3A18%3A04IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-ieee_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Dynamic%20modeling%20and%20simulation%20of%20a%20flexible%20satellite&rft.btitle=2008%20Asia%20Simulation%20Conference%20-%207th%20International%20Conference%20on%20System%20Simulation%20and%20Scientific%20Computing&rft.au=Shengjian%20Bai&rft.date=2008-10&rft.spage=1068&rft.epage=1072&rft.pages=1068-1072&rft.isbn=1424417864&rft.isbn_list=9781424417865&rft_id=info:doi/10.1109/ASC-ICSC.2008.4675523&rft_dat=%3Cieee_6IE%3E4675523%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&rft.eisbn=9781424417872&rft.eisbn_list=1424417872&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=4675523&rfr_iscdi=true |