Attitude Coordination Control of Spacecraft Formation
In this paper, we study adaptive attitude synchronization of spacecraft formation with switching topology. By introducing a novel adaptive control architecture and by transforming the attitude dynamics into Euler-Lagrange form, decentralized controllers are developed, which allow for parametric unce...
Gespeichert in:
Veröffentlicht in: | Applied Mechanics and Materials 2013-01, Vol.263-266, p.795-802 |
---|---|
Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 802 |
---|---|
container_issue | |
container_start_page | 795 |
container_title | Applied Mechanics and Materials |
container_volume | 263-266 |
creator | Liu, Man Guo Zhang, Ke |
description | In this paper, we study adaptive attitude synchronization of spacecraft formation with switching topology. By introducing a novel adaptive control architecture and by transforming the attitude dynamics into Euler-Lagrange form, decentralized controllers are developed, which allow for parametric uncertainties and unknown external disturbances. Based upon graph theory and Lyapunov stability theory, rigid mathematical analysis on system stability is provided. A distinctive feature of this work is to address the adaptive attitude synchronization with general directed information flow. It is shown that arbitrary desired constant relative orientations within the group or with respect to any external references can be attained. Simulation results are provided to demonstrate the effectiveness of the obtained results. |
doi_str_mv | 10.4028/www.scientific.net/AMM.263-266.795 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_1442799823</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3102387141</sourcerecordid><originalsourceid>FETCH-LOGICAL-c303t-26698a5e37ddb4d93c12cec22ca4192c991205c74bec2cc80559bb407104561a3</originalsourceid><addsrcrecordid>eNqNkMtKAzEUhoMXsNa-w4A7Yaa5X5a1WhVaXKjrkMlkcEo7qUlK8e2btoIuXRzCyTl8_-ED4A7BikIsx7vdroq2c33q2s5WvUvjyWJRYU5KzHklFDsDA8Q5LgWV-ByMlJAEEiEZE5ReHGewVITwK3Ad4xJCThGVA8AmKXVp27hi6n1out6kzve56VPwq8K3xdvGWGeDaVMx82F9nN-Ay9asohv9vEPwMXt8nz6X89enl-lkXtocng6nKWmYI6JpatooYhHOLIytoUhhqxTCkFlB6_xprYSMqbqmUCBIGUeGDMHtibsJ_mvrYtJLvw19jtSIUiyUkpjkrfvTlg0-xuBavQnd2oRvjaA-6NNZn_7Vp7M-nfXprC8X11lfhjycICmYPiZnP_9k_R-zB3O5f6A</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1442799823</pqid></control><display><type>article</type><title>Attitude Coordination Control of Spacecraft Formation</title><source>Scientific.net Journals</source><creator>Liu, Man Guo ; Zhang, Ke</creator><creatorcontrib>Liu, Man Guo ; Zhang, Ke</creatorcontrib><description>In this paper, we study adaptive attitude synchronization of spacecraft formation with switching topology. By introducing a novel adaptive control architecture and by transforming the attitude dynamics into Euler-Lagrange form, decentralized controllers are developed, which allow for parametric uncertainties and unknown external disturbances. Based upon graph theory and Lyapunov stability theory, rigid mathematical analysis on system stability is provided. A distinctive feature of this work is to address the adaptive attitude synchronization with general directed information flow. It is shown that arbitrary desired constant relative orientations within the group or with respect to any external references can be attained. Simulation results are provided to demonstrate the effectiveness of the obtained results.</description><identifier>ISSN: 1660-9336</identifier><identifier>ISSN: 1662-7482</identifier><identifier>ISBN: 9783037855744</identifier><identifier>ISBN: 3037855746</identifier><identifier>EISSN: 1662-7482</identifier><identifier>DOI: 10.4028/www.scientific.net/AMM.263-266.795</identifier><language>eng</language><publisher>Zurich: Trans Tech Publications Ltd</publisher><ispartof>Applied Mechanics and Materials, 2013-01, Vol.263-266, p.795-802</ispartof><rights>2013 Trans Tech Publications Ltd</rights><rights>Copyright Trans Tech Publications Ltd. Dec 2012</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c303t-26698a5e37ddb4d93c12cec22ca4192c991205c74bec2cc80559bb407104561a3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttps://www.scientific.net/Image/TitleCover/2171?width=600</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Liu, Man Guo</creatorcontrib><creatorcontrib>Zhang, Ke</creatorcontrib><title>Attitude Coordination Control of Spacecraft Formation</title><title>Applied Mechanics and Materials</title><description>In this paper, we study adaptive attitude synchronization of spacecraft formation with switching topology. By introducing a novel adaptive control architecture and by transforming the attitude dynamics into Euler-Lagrange form, decentralized controllers are developed, which allow for parametric uncertainties and unknown external disturbances. Based upon graph theory and Lyapunov stability theory, rigid mathematical analysis on system stability is provided. A distinctive feature of this work is to address the adaptive attitude synchronization with general directed information flow. It is shown that arbitrary desired constant relative orientations within the group or with respect to any external references can be attained. Simulation results are provided to demonstrate the effectiveness of the obtained results.</description><issn>1660-9336</issn><issn>1662-7482</issn><issn>1662-7482</issn><isbn>9783037855744</isbn><isbn>3037855746</isbn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNqNkMtKAzEUhoMXsNa-w4A7Yaa5X5a1WhVaXKjrkMlkcEo7qUlK8e2btoIuXRzCyTl8_-ED4A7BikIsx7vdroq2c33q2s5WvUvjyWJRYU5KzHklFDsDA8Q5LgWV-ByMlJAEEiEZE5ReHGewVITwK3Ad4xJCThGVA8AmKXVp27hi6n1out6kzve56VPwq8K3xdvGWGeDaVMx82F9nN-Ay9asohv9vEPwMXt8nz6X89enl-lkXtocng6nKWmYI6JpatooYhHOLIytoUhhqxTCkFlB6_xprYSMqbqmUCBIGUeGDMHtibsJ_mvrYtJLvw19jtSIUiyUkpjkrfvTlg0-xuBavQnd2oRvjaA-6NNZn_7Vp7M-nfXprC8X11lfhjycICmYPiZnP_9k_R-zB3O5f6A</recordid><startdate>20130101</startdate><enddate>20130101</enddate><creator>Liu, Man Guo</creator><creator>Zhang, Ke</creator><general>Trans Tech Publications Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BFMQW</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>FR3</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>KB.</scope><scope>KR7</scope><scope>L6V</scope><scope>M7S</scope><scope>PDBOC</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20130101</creationdate><title>Attitude Coordination Control of Spacecraft Formation</title><author>Liu, Man Guo ; Zhang, Ke</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c303t-26698a5e37ddb4d93c12cec22ca4192c991205c74bec2cc80559bb407104561a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Liu, Man Guo</creatorcontrib><creatorcontrib>Zhang, Ke</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central</collection><collection>Continental Europe Database</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>Engineering Research Database</collection><collection>SciTech Premium Collection</collection><collection>Materials Research Database</collection><collection>Materials Science Database</collection><collection>Civil Engineering Abstracts</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>Materials Science Collection</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>Applied Mechanics and Materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Liu, Man Guo</au><au>Zhang, Ke</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Attitude Coordination Control of Spacecraft Formation</atitle><jtitle>Applied Mechanics and Materials</jtitle><date>2013-01-01</date><risdate>2013</risdate><volume>263-266</volume><spage>795</spage><epage>802</epage><pages>795-802</pages><issn>1660-9336</issn><issn>1662-7482</issn><eissn>1662-7482</eissn><isbn>9783037855744</isbn><isbn>3037855746</isbn><abstract>In this paper, we study adaptive attitude synchronization of spacecraft formation with switching topology. By introducing a novel adaptive control architecture and by transforming the attitude dynamics into Euler-Lagrange form, decentralized controllers are developed, which allow for parametric uncertainties and unknown external disturbances. Based upon graph theory and Lyapunov stability theory, rigid mathematical analysis on system stability is provided. A distinctive feature of this work is to address the adaptive attitude synchronization with general directed information flow. It is shown that arbitrary desired constant relative orientations within the group or with respect to any external references can be attained. Simulation results are provided to demonstrate the effectiveness of the obtained results.</abstract><cop>Zurich</cop><pub>Trans Tech Publications Ltd</pub><doi>10.4028/www.scientific.net/AMM.263-266.795</doi><tpages>8</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1660-9336 |
ispartof | Applied Mechanics and Materials, 2013-01, Vol.263-266, p.795-802 |
issn | 1660-9336 1662-7482 1662-7482 |
language | eng |
recordid | cdi_proquest_journals_1442799823 |
source | Scientific.net Journals |
title | Attitude Coordination Control of Spacecraft Formation |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-06T20%3A47%3A20IST&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=Attitude%20Coordination%20Control%20of%20Spacecraft%20Formation&rft.jtitle=Applied%20Mechanics%20and%20Materials&rft.au=Liu,%20Man%20Guo&rft.date=2013-01-01&rft.volume=263-266&rft.spage=795&rft.epage=802&rft.pages=795-802&rft.issn=1660-9336&rft.eissn=1662-7482&rft.isbn=9783037855744&rft.isbn_list=3037855746&rft_id=info:doi/10.4028/www.scientific.net/AMM.263-266.795&rft_dat=%3Cproquest_cross%3E3102387141%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=1442799823&rft_id=info:pmid/&rfr_iscdi=true |