Control of flexible structures with spillover using an augmented observer
Modern modal control methods for flexible structures have control and observation spillover that can degrade performance and reduce the stability margin of the closed-loop controlled structure. The sensor output is often filtered to reduce observation spillover; however, the filter introduces signal...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 1989-03, Vol.12 (2), p.155-161 |
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creator | CHAIT, YOSSI RADCLIFFE, CLARK J. |
description | Modern modal control methods for flexible structures have control and observation spillover that can degrade performance and reduce the stability margin of the closed-loop controlled structure. The sensor output is often filtered to reduce observation spillover; however, the filter introduces signal distortion and perturbs the closed-loop system eigenvalue locations. This perturbation can reduce the stability margin and jeopardize convergence of a deterministic observer. If the filter equations are not explicitly included in the observer design, then the separation principle between the controller and the observer states no longer holds when present in the unfiltered system. A new method is presented where the observer equations are augmented to include a first-order filter dynamics. The separation principle, controllability, and observability of the unfiltered system are invariant to the filter dynamics in this new method, resulting in no perturbation of controlled system eigenvalue locations. The filter cutoff frequency can be located even within the bandwidth of the system, thereby increasing the filter effectiveness in reducing observation spillover. Spillover-generated errors in closed-loop eigenvalues of these control methods are compared using a numerical example. (Author) |
doi_str_mv | 10.2514/3.20385 |
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The sensor output is often filtered to reduce observation spillover; however, the filter introduces signal distortion and perturbs the closed-loop system eigenvalue locations. This perturbation can reduce the stability margin and jeopardize convergence of a deterministic observer. If the filter equations are not explicitly included in the observer design, then the separation principle between the controller and the observer states no longer holds when present in the unfiltered system. A new method is presented where the observer equations are augmented to include a first-order filter dynamics. The separation principle, controllability, and observability of the unfiltered system are invariant to the filter dynamics in this new method, resulting in no perturbation of controlled system eigenvalue locations. The filter cutoff frequency can be located even within the bandwidth of the system, thereby increasing the filter effectiveness in reducing observation spillover. Spillover-generated errors in closed-loop eigenvalues of these control methods are compared using a numerical example. (Author)</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/3.20385</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>CAE ; Closed loop systems ; Computer aided engineering ; Controllers ; Eigenvalues ; Flexible structures ; Mechanical engineering ; Methods ; Partial differential equations ; Sensors ; stability</subject><ispartof>Journal of guidance, control, and dynamics, 1989-03, Vol.12 (2), p.155-161</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics Mar/Apr 1989</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a377t-2ff52090d5c9b91365d913b3b47c38b7771b65fd9ad579a471138ce663ef94bf3</citedby><cites>FETCH-LOGICAL-a377t-2ff52090d5c9b91365d913b3b47c38b7771b65fd9ad579a471138ce663ef94bf3</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>CHAIT, YOSSI</creatorcontrib><creatorcontrib>RADCLIFFE, CLARK J.</creatorcontrib><title>Control of flexible structures with spillover using an augmented observer</title><title>Journal of guidance, control, and dynamics</title><description>Modern modal control methods for flexible structures have control and observation spillover that can degrade performance and reduce the stability margin of the closed-loop controlled structure. The sensor output is often filtered to reduce observation spillover; however, the filter introduces signal distortion and perturbs the closed-loop system eigenvalue locations. This perturbation can reduce the stability margin and jeopardize convergence of a deterministic observer. If the filter equations are not explicitly included in the observer design, then the separation principle between the controller and the observer states no longer holds when present in the unfiltered system. A new method is presented where the observer equations are augmented to include a first-order filter dynamics. The separation principle, controllability, and observability of the unfiltered system are invariant to the filter dynamics in this new method, resulting in no perturbation of controlled system eigenvalue locations. The filter cutoff frequency can be located even within the bandwidth of the system, thereby increasing the filter effectiveness in reducing observation spillover. Spillover-generated errors in closed-loop eigenvalues of these control methods are compared using a numerical example. (Author)</description><subject>CAE</subject><subject>Closed loop systems</subject><subject>Computer aided engineering</subject><subject>Controllers</subject><subject>Eigenvalues</subject><subject>Flexible structures</subject><subject>Mechanical engineering</subject><subject>Methods</subject><subject>Partial differential equations</subject><subject>Sensors</subject><subject>stability</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1989</creationdate><recordtype>article</recordtype><recordid>eNp9kEtLAzEUhYMoWKv4FwKK4mJqMplMMkspPgoFN7oOmZmkTkknYx5a_73RFgpF3Ny7OB_nnnsAOMdoklNc3JJJjginB2CEKSEZ4bw4BCPECM4oqtAxOPF-iRAmJWYjMJvaPjhroNVQG7XuaqOgDy42ITrl4WcX3qAfOmPsh3Iw-q5fQNlDGRcr1QfVQlt75ZJ2Co60NF6dbfcYvD7cv0yfsvnz42x6N88kYSxkudY0Tzla2lR1lVLQNs2a1AVrCK8ZY7guqW4r2VJWyYJhTHijypIoXRW1JmNwvfEdnH2Pygex6nyjjJG9stELVpSYI85RIq_-JVNdZZVXPIEXe-DSRtenL0ROcIqNECl3hxtnvXdKi8F1K-m-BEY_XoUg4rf6RN5sSNlJufPaymJotdDRmKDWIbGXf7H7lt9O-o6B</recordid><startdate>19890301</startdate><enddate>19890301</enddate><creator>CHAIT, YOSSI</creator><creator>RADCLIFFE, CLARK J.</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><scope>7TC</scope></search><sort><creationdate>19890301</creationdate><title>Control of flexible structures with spillover using an augmented observer</title><author>CHAIT, YOSSI ; RADCLIFFE, CLARK J.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a377t-2ff52090d5c9b91365d913b3b47c38b7771b65fd9ad579a471138ce663ef94bf3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1989</creationdate><topic>CAE</topic><topic>Closed loop systems</topic><topic>Computer aided engineering</topic><topic>Controllers</topic><topic>Eigenvalues</topic><topic>Flexible structures</topic><topic>Mechanical engineering</topic><topic>Methods</topic><topic>Partial differential equations</topic><topic>Sensors</topic><topic>stability</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>CHAIT, YOSSI</creatorcontrib><creatorcontrib>RADCLIFFE, CLARK J.</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><collection>Mechanical Engineering Abstracts</collection><jtitle>Journal of guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>CHAIT, YOSSI</au><au>RADCLIFFE, CLARK J.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Control of flexible structures with spillover using an augmented observer</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>1989-03-01</date><risdate>1989</risdate><volume>12</volume><issue>2</issue><spage>155</spage><epage>161</epage><pages>155-161</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>Modern modal control methods for flexible structures have control and observation spillover that can degrade performance and reduce the stability margin of the closed-loop controlled structure. The sensor output is often filtered to reduce observation spillover; however, the filter introduces signal distortion and perturbs the closed-loop system eigenvalue locations. This perturbation can reduce the stability margin and jeopardize convergence of a deterministic observer. If the filter equations are not explicitly included in the observer design, then the separation principle between the controller and the observer states no longer holds when present in the unfiltered system. A new method is presented where the observer equations are augmented to include a first-order filter dynamics. The separation principle, controllability, and observability of the unfiltered system are invariant to the filter dynamics in this new method, resulting in no perturbation of controlled system eigenvalue locations. The filter cutoff frequency can be located even within the bandwidth of the system, thereby increasing the filter effectiveness in reducing observation spillover. Spillover-generated errors in closed-loop eigenvalues of these control methods are compared using a numerical example. (Author)</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.20385</doi><tpages>7</tpages></addata></record> |
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subjects | CAE Closed loop systems Computer aided engineering Controllers Eigenvalues Flexible structures Mechanical engineering Methods Partial differential equations Sensors stability |
title | Control of flexible structures with spillover using an augmented observer |
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