Reduced-order compensator design for a flexible structure
A low-order controller is designed for an experimental truss structure. The objective is to achieve good disturbance attenuation, while at the same time preserving good stability margin and other robustness properties. The method used is linear quadratic Gaussian (LQG) with frequency dependent weigh...
Gespeichert in:
| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 1990-01, Vol.13 (1), p.46-56 |
|---|---|
| Hauptverfasser: | , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 56 |
|---|---|
| container_issue | 1 |
| container_start_page | 46 |
| container_title | Journal of guidance, control, and dynamics |
| container_volume | 13 |
| creator | OPDENACKER, PH. C. JONCKHEERE, E. A. SAFONOV, M. G. JUANG, J. C. LUKICH, M. S. |
| description | A low-order controller is designed for an experimental truss structure. The objective is to achieve good disturbance attenuation, while at the same time preserving good stability margin and other robustness properties. The method used is linear quadratic Gaussian (LQG) with frequency dependent weights and colored noises for shaping singular-value Bode plots. Controller reduction is accomplished through the open-loop balancing scheme applied to the full-order compensator. A typical design result shows that it is possible to obtain a very low-order design that meets the preceding specification. (Author) |
| doi_str_mv | 10.2514/3.20516 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_aiaa_journals_10_2514_3_20516</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2313796471</sourcerecordid><originalsourceid>FETCH-LOGICAL-a345t-2ac0203190f1f38ad6156dbf9c876b25ca0704bb953f9b68b1b558b0a465e99d3</originalsourceid><addsrcrecordid>eNpt0NtKxDAQBuAgCq6r-AoFRfGia5JpkuZSFk-wIIhehxylS7etSQvr21vtgqBezcB8_Aw_QqcELygjxTUsKGaE76EZYQA5lGWxj2ZYAMkZlvgQHaW0xpgAJ2KG5LN3g_Uub6PzMbPtpvNN0n0bM-dT9dZkYVx1Fmq_rUzts9THwfZD9MfoIOg6-ZPdnKPXu9uX5UO-erp_XN6scg0F63OqLaYYiMSBBCi144RxZ4K0peCGMquxwIUxkkGQhpeGGMZKg3XBmZfSwRxdTLldbN8Hn3q1qZL1da0b3w5JUVaKggs6wrNfcN0OsRl_UxQICMkLQUZ1OSkb25SiD6qL1UbHD0Ww-ipQgfoucJTnk9SV1j9Zf9nVf2x3Vp0LKgx13fttD59WHXqC</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2313796471</pqid></control><display><type>article</type><title>Reduced-order compensator design for a flexible structure</title><source>Alma/SFX Local Collection</source><creator>OPDENACKER, PH. C. ; JONCKHEERE, E. A. ; SAFONOV, M. G. ; JUANG, J. C. ; LUKICH, M. S.</creator><creatorcontrib>OPDENACKER, PH. C. ; JONCKHEERE, E. A. ; SAFONOV, M. G. ; JUANG, J. C. ; LUKICH, M. S.</creatorcontrib><description>A low-order controller is designed for an experimental truss structure. The objective is to achieve good disturbance attenuation, while at the same time preserving good stability margin and other robustness properties. The method used is linear quadratic Gaussian (LQG) with frequency dependent weights and colored noises for shaping singular-value Bode plots. Controller reduction is accomplished through the open-loop balancing scheme applied to the full-order compensator. A typical design result shows that it is possible to obtain a very low-order design that meets the preceding specification. (Author)</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/3.20516</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Aluminum ; Controllers ; Design ; Electrical engineering ; Experiments ; Flexible structures ; Noise ; Sensors</subject><ispartof>Journal of guidance, control, and dynamics, 1990-01, Vol.13 (1), p.46-56</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics Jan/Feb 1990</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a345t-2ac0203190f1f38ad6156dbf9c876b25ca0704bb953f9b68b1b558b0a465e99d3</citedby><cites>FETCH-LOGICAL-a345t-2ac0203190f1f38ad6156dbf9c876b25ca0704bb953f9b68b1b558b0a465e99d3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>OPDENACKER, PH. C.</creatorcontrib><creatorcontrib>JONCKHEERE, E. A.</creatorcontrib><creatorcontrib>SAFONOV, M. G.</creatorcontrib><creatorcontrib>JUANG, J. C.</creatorcontrib><creatorcontrib>LUKICH, M. S.</creatorcontrib><title>Reduced-order compensator design for a flexible structure</title><title>Journal of guidance, control, and dynamics</title><description>A low-order controller is designed for an experimental truss structure. The objective is to achieve good disturbance attenuation, while at the same time preserving good stability margin and other robustness properties. The method used is linear quadratic Gaussian (LQG) with frequency dependent weights and colored noises for shaping singular-value Bode plots. Controller reduction is accomplished through the open-loop balancing scheme applied to the full-order compensator. A typical design result shows that it is possible to obtain a very low-order design that meets the preceding specification. (Author)</description><subject>Aluminum</subject><subject>Controllers</subject><subject>Design</subject><subject>Electrical engineering</subject><subject>Experiments</subject><subject>Flexible structures</subject><subject>Noise</subject><subject>Sensors</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1990</creationdate><recordtype>article</recordtype><recordid>eNpt0NtKxDAQBuAgCq6r-AoFRfGia5JpkuZSFk-wIIhehxylS7etSQvr21vtgqBezcB8_Aw_QqcELygjxTUsKGaE76EZYQA5lGWxj2ZYAMkZlvgQHaW0xpgAJ2KG5LN3g_Uub6PzMbPtpvNN0n0bM-dT9dZkYVx1Fmq_rUzts9THwfZD9MfoIOg6-ZPdnKPXu9uX5UO-erp_XN6scg0F63OqLaYYiMSBBCi144RxZ4K0peCGMquxwIUxkkGQhpeGGMZKg3XBmZfSwRxdTLldbN8Hn3q1qZL1da0b3w5JUVaKggs6wrNfcN0OsRl_UxQICMkLQUZ1OSkb25SiD6qL1UbHD0Ww-ipQgfoucJTnk9SV1j9Zf9nVf2x3Vp0LKgx13fttD59WHXqC</recordid><startdate>199001</startdate><enddate>199001</enddate><creator>OPDENACKER, PH. C.</creator><creator>JONCKHEERE, E. A.</creator><creator>SAFONOV, M. G.</creator><creator>JUANG, J. C.</creator><creator>LUKICH, M. S.</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>199001</creationdate><title>Reduced-order compensator design for a flexible structure</title><author>OPDENACKER, PH. C. ; JONCKHEERE, E. A. ; SAFONOV, M. G. ; JUANG, J. C. ; LUKICH, M. S.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a345t-2ac0203190f1f38ad6156dbf9c876b25ca0704bb953f9b68b1b558b0a465e99d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1990</creationdate><topic>Aluminum</topic><topic>Controllers</topic><topic>Design</topic><topic>Electrical engineering</topic><topic>Experiments</topic><topic>Flexible structures</topic><topic>Noise</topic><topic>Sensors</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>OPDENACKER, PH. C.</creatorcontrib><creatorcontrib>JONCKHEERE, E. A.</creatorcontrib><creatorcontrib>SAFONOV, M. G.</creatorcontrib><creatorcontrib>JUANG, J. C.</creatorcontrib><creatorcontrib>LUKICH, M. S.</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>Aerospace Database</collection><collection>ProQuest Computer Science Collection</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 guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>OPDENACKER, PH. C.</au><au>JONCKHEERE, E. A.</au><au>SAFONOV, M. G.</au><au>JUANG, J. C.</au><au>LUKICH, M. S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Reduced-order compensator design for a flexible structure</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>1990-01</date><risdate>1990</risdate><volume>13</volume><issue>1</issue><spage>46</spage><epage>56</epage><pages>46-56</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>A low-order controller is designed for an experimental truss structure. The objective is to achieve good disturbance attenuation, while at the same time preserving good stability margin and other robustness properties. The method used is linear quadratic Gaussian (LQG) with frequency dependent weights and colored noises for shaping singular-value Bode plots. Controller reduction is accomplished through the open-loop balancing scheme applied to the full-order compensator. A typical design result shows that it is possible to obtain a very low-order design that meets the preceding specification. (Author)</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.20516</doi><tpages>11</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0731-5090 |
| ispartof | Journal of guidance, control, and dynamics, 1990-01, Vol.13 (1), p.46-56 |
| issn | 0731-5090 1533-3884 |
| language | eng |
| recordid | cdi_aiaa_journals_10_2514_3_20516 |
| source | Alma/SFX Local Collection |
| subjects | Aluminum Controllers Design Electrical engineering Experiments Flexible structures Noise Sensors |
| title | Reduced-order compensator design for a flexible structure |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T08%3A38%3A52IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_aiaa_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Reduced-order%20compensator%20design%20for%20a%20flexible%20structure&rft.jtitle=Journal%20of%20guidance,%20control,%20and%20dynamics&rft.au=OPDENACKER,%20PH.%20C.&rft.date=1990-01&rft.volume=13&rft.issue=1&rft.spage=46&rft.epage=56&rft.pages=46-56&rft.issn=0731-5090&rft.eissn=1533-3884&rft_id=info:doi/10.2514/3.20516&rft_dat=%3Cproquest_aiaa_%3E2313796471%3C/proquest_aiaa_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2313796471&rft_id=info:pmid/&rfr_iscdi=true |