(μ-Mu)-Iteration Technique: Application to attitude control of satellite with large flexible appendages
This paper addresses the problem of increasing robustness, with respect to real parameter variations, for a satellite with large flexible appendages. A first control law is designed using, for example, a classical frequency-domain method. Subsequently, robustness is improved iteratively, using the (...
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| creator | Chiappa, C. Bodineau, G. Boulade, S. Beugnon, C. |
| description | This paper addresses the problem of increasing robustness, with respect to real parameter variations, for a satellite with large flexible appendages. A first control law is designed using, for example, a classical frequency-domain method. Subsequently, robustness is improved iteratively, using the (μ-Mu)-iteration technique, which is based on alternating between real μ-analysis and modal Multi-model design. |
| doi_str_mv | 10.1109/CDC.2005.1582228 |
| format | Conference Proceeding |
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Subsequently, robustness is improved iteratively, using the (μ-Mu)-iteration technique, which is based on alternating between real μ-analysis and modal Multi-model design.</description><subject>Artificial satellites</subject><subject>Centralized control</subject><subject>Damping</subject><subject>Flexible structures</subject><subject>Mars</subject><subject>Radar antennas</subject><subject>Robust control</subject><subject>Space vehicles</subject><subject>Uncertainty</subject><subject>Vehicle dynamics</subject><issn>0191-2216</issn><isbn>9780780395671</isbn><isbn>0780395670</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2005</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotkE9LAzEUxAMqWGvvgpcc9bD1vaTZbLzJ-q9Q8VLPJZt9aSNxd91NUb-bn8HPZKGFgYE5_JgZxi4Qpohgbsr7cioA1BRVIYQojtjE6AJ2kkblGo_ZCNBgJgTmp-xsGN4BoIA8H7HN1d9v9rK9zuaJeptC2_AluU0TPrd0y--6Lga3j1PLbUohbWvirm1S30beej7YRDGGRPwrpA2Ptl8T95G-QxWJ266jprZrGs7ZibdxoMnBx-zt8WFZPmeL16d5ebfI3K55yoyr66qQEo0gLWYKC-0k1TNCb7WqkMA4ne_WGbDgjCKJ1lTezjQpT17LMbvccwMRrbo-fNj-Z3U4Rv4DqYZY2w</recordid><startdate>2005</startdate><enddate>2005</enddate><creator>Chiappa, C.</creator><creator>Bodineau, G.</creator><creator>Boulade, S.</creator><creator>Beugnon, C.</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope></search><sort><creationdate>2005</creationdate><title>(μ-Mu)-Iteration Technique: Application to attitude control of satellite with large flexible appendages</title><author>Chiappa, C. ; Bodineau, G. ; Boulade, S. ; Beugnon, C.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c222t-9cddb833192e7245187c3ed4e1fa75b1e09c7697890a0c95e31a9bfa47e5fef73</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2005</creationdate><topic>Artificial satellites</topic><topic>Centralized control</topic><topic>Damping</topic><topic>Flexible structures</topic><topic>Mars</topic><topic>Radar antennas</topic><topic>Robust control</topic><topic>Space vehicles</topic><topic>Uncertainty</topic><topic>Vehicle dynamics</topic><toplevel>online_resources</toplevel><creatorcontrib>Chiappa, C.</creatorcontrib><creatorcontrib>Bodineau, G.</creatorcontrib><creatorcontrib>Boulade, S.</creatorcontrib><creatorcontrib>Beugnon, C.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Chiappa, C.</au><au>Bodineau, G.</au><au>Boulade, S.</au><au>Beugnon, C.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>(μ-Mu)-Iteration Technique: Application to attitude control of satellite with large flexible appendages</atitle><btitle>Proceedings of the 44th IEEE Conference on Decision and Control</btitle><stitle>CDC</stitle><date>2005</date><risdate>2005</risdate><spage>641</spage><epage>646</epage><pages>641-646</pages><issn>0191-2216</issn><isbn>9780780395671</isbn><isbn>0780395670</isbn><abstract>This paper addresses the problem of increasing robustness, with respect to real parameter variations, for a satellite with large flexible appendages. A first control law is designed using, for example, a classical frequency-domain method. Subsequently, robustness is improved iteratively, using the (μ-Mu)-iteration technique, which is based on alternating between real μ-analysis and modal Multi-model design.</abstract><pub>IEEE</pub><doi>10.1109/CDC.2005.1582228</doi><tpages>6</tpages></addata></record> |
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| ispartof | Proceedings of the 44th IEEE Conference on Decision and Control, 2005, p.641-646 |
| issn | 0191-2216 |
| language | eng |
| recordid | cdi_ieee_primary_1582228 |
| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Artificial satellites Centralized control Damping Flexible structures Mars Radar antennas Robust control Space vehicles Uncertainty Vehicle dynamics |
| title | (μ-Mu)-Iteration Technique: Application to attitude control of satellite with large flexible appendages |
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