Dynamic Mode Decomposition for Compressive System Identification

Dynamic mode decomposition has emerged as a leading technique to identify spatiotemporal coherent structures from high-dimensional data, benefiting from a strong connection to nonlinear dynamical systems via the Koopman operator. In this work, two recent innovations that extend dynamic mode decompos...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:AIAA journal 2020-02, Vol.58 (2), p.561-574
Hauptverfasser: Bai, Zhe, Kaiser, Eurika, Proctor, Joshua L, Kutz, J. Nathan, Brunton, Steven L
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 574
container_issue 2
container_start_page 561
container_title AIAA journal
container_volume 58
creator Bai, Zhe
Kaiser, Eurika
Proctor, Joshua L
Kutz, J. Nathan
Brunton, Steven L
description Dynamic mode decomposition has emerged as a leading technique to identify spatiotemporal coherent structures from high-dimensional data, benefiting from a strong connection to nonlinear dynamical systems via the Koopman operator. In this work, two recent innovations that extend dynamic mode decomposition to systems with actuation and systems with heavily subsampled measurements are integrated and unified. When combined, these methods yield a novel framework for compressive system identification. It is possible to identify a low-order model from limited input–output data and reconstruct the associated full-state dynamic modes with compressed sensing, adding interpretability to the state of the reduced-order model. Moreover, when full-state data are available, it is possible to dramatically accelerate downstream computations by first compressing the data. This unified framework is demonstrated on two model systems, investigating the effects of sensor noise, different types of measurements (e.g., point sensors, Gaussian random projections, etc.), compression ratios, and different choices of actuation (e.g., localized, broadband, etc.). In the first example, this architecture is explored on a test system with known low-rank dynamics and an artificially inflated state dimension. The second example consists of a real-world engineering application given by the fluid flow past a pitching airfoil at low Reynolds number. This example provides a challenging and realistic test case for the proposed method, and results demonstrate that the dominant coherent structures are well characterized despite actuation and heavily subsampled data.
doi_str_mv 10.2514/1.J057870
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2351631591</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2351631591</sourcerecordid><originalsourceid>FETCH-LOGICAL-a429t-231e77caa0a2a922fdbc235f4a2bd57cbf7c9a42282968c98e20d6af3f21fa6b3</originalsourceid><addsrcrecordid>eNpl0M1KAzEUBeAgCtbqwjcYEAQXU3OTyWRmp7T-VCouVHAX7mQSSHEmNZkW-vamtODC1eXAx7lwCLkEOmECiluYvFAhK0mPyAgE5zmvxNcxGVFKIYdCsFNyFuMyJSYrGJG72bbHzuns1bcmmxntu5WPbnC-z6wP2TTlYGJ0G5O9b-Ngumzemn5w1mncqXNyYvE7movDHZPPx4eP6XO-eHuaT-8XORasHnLGwUipESkyrBmzbaMZF7ZA1rRC6sZKXSfKKlaXla4rw2hbouWWgcWy4WNyte9dBf-zNnFQS78OfXqpUg-UHEQNSd3slQ4-xmCsWgXXYdgqoGo3kAJ1GCjZ671Fh_jX9h_-AvYKY6U</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2351631591</pqid></control><display><type>article</type><title>Dynamic Mode Decomposition for Compressive System Identification</title><source>Alma/SFX Local Collection</source><creator>Bai, Zhe ; Kaiser, Eurika ; Proctor, Joshua L ; Kutz, J. Nathan ; Brunton, Steven L</creator><creatorcontrib>Bai, Zhe ; Kaiser, Eurika ; Proctor, Joshua L ; Kutz, J. Nathan ; Brunton, Steven L</creatorcontrib><description>Dynamic mode decomposition has emerged as a leading technique to identify spatiotemporal coherent structures from high-dimensional data, benefiting from a strong connection to nonlinear dynamical systems via the Koopman operator. In this work, two recent innovations that extend dynamic mode decomposition to systems with actuation and systems with heavily subsampled measurements are integrated and unified. When combined, these methods yield a novel framework for compressive system identification. It is possible to identify a low-order model from limited input–output data and reconstruct the associated full-state dynamic modes with compressed sensing, adding interpretability to the state of the reduced-order model. Moreover, when full-state data are available, it is possible to dramatically accelerate downstream computations by first compressing the data. This unified framework is demonstrated on two model systems, investigating the effects of sensor noise, different types of measurements (e.g., point sensors, Gaussian random projections, etc.), compression ratios, and different choices of actuation (e.g., localized, broadband, etc.). In the first example, this architecture is explored on a test system with known low-rank dynamics and an artificially inflated state dimension. The second example consists of a real-world engineering application given by the fluid flow past a pitching airfoil at low Reynolds number. This example provides a challenging and realistic test case for the proposed method, and results demonstrate that the dominant coherent structures are well characterized despite actuation and heavily subsampled data.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J057870</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Actuation ; Aerodynamics ; Broadband ; Compression ratio ; Computational fluid dynamics ; Data compression ; Decomposition ; Fluid flow ; Identification methods ; Nonlinear systems ; Reduced order models ; Reynolds number ; System identification</subject><ispartof>AIAA journal, 2020-02, Vol.58 (2), p.561-574</ispartof><rights>Copyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at ; employ the ISSN (print) or (online) to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a429t-231e77caa0a2a922fdbc235f4a2bd57cbf7c9a42282968c98e20d6af3f21fa6b3</citedby><cites>FETCH-LOGICAL-a429t-231e77caa0a2a922fdbc235f4a2bd57cbf7c9a42282968c98e20d6af3f21fa6b3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Bai, Zhe</creatorcontrib><creatorcontrib>Kaiser, Eurika</creatorcontrib><creatorcontrib>Proctor, Joshua L</creatorcontrib><creatorcontrib>Kutz, J. Nathan</creatorcontrib><creatorcontrib>Brunton, Steven L</creatorcontrib><title>Dynamic Mode Decomposition for Compressive System Identification</title><title>AIAA journal</title><description>Dynamic mode decomposition has emerged as a leading technique to identify spatiotemporal coherent structures from high-dimensional data, benefiting from a strong connection to nonlinear dynamical systems via the Koopman operator. In this work, two recent innovations that extend dynamic mode decomposition to systems with actuation and systems with heavily subsampled measurements are integrated and unified. When combined, these methods yield a novel framework for compressive system identification. It is possible to identify a low-order model from limited input–output data and reconstruct the associated full-state dynamic modes with compressed sensing, adding interpretability to the state of the reduced-order model. Moreover, when full-state data are available, it is possible to dramatically accelerate downstream computations by first compressing the data. This unified framework is demonstrated on two model systems, investigating the effects of sensor noise, different types of measurements (e.g., point sensors, Gaussian random projections, etc.), compression ratios, and different choices of actuation (e.g., localized, broadband, etc.). In the first example, this architecture is explored on a test system with known low-rank dynamics and an artificially inflated state dimension. The second example consists of a real-world engineering application given by the fluid flow past a pitching airfoil at low Reynolds number. This example provides a challenging and realistic test case for the proposed method, and results demonstrate that the dominant coherent structures are well characterized despite actuation and heavily subsampled data.</description><subject>Actuation</subject><subject>Aerodynamics</subject><subject>Broadband</subject><subject>Compression ratio</subject><subject>Computational fluid dynamics</subject><subject>Data compression</subject><subject>Decomposition</subject><subject>Fluid flow</subject><subject>Identification methods</subject><subject>Nonlinear systems</subject><subject>Reduced order models</subject><subject>Reynolds number</subject><subject>System identification</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNpl0M1KAzEUBeAgCtbqwjcYEAQXU3OTyWRmp7T-VCouVHAX7mQSSHEmNZkW-vamtODC1eXAx7lwCLkEOmECiluYvFAhK0mPyAgE5zmvxNcxGVFKIYdCsFNyFuMyJSYrGJG72bbHzuns1bcmmxntu5WPbnC-z6wP2TTlYGJ0G5O9b-Ngumzemn5w1mncqXNyYvE7movDHZPPx4eP6XO-eHuaT-8XORasHnLGwUipESkyrBmzbaMZF7ZA1rRC6sZKXSfKKlaXla4rw2hbouWWgcWy4WNyte9dBf-zNnFQS78OfXqpUg-UHEQNSd3slQ4-xmCsWgXXYdgqoGo3kAJ1GCjZ671Fh_jX9h_-AvYKY6U</recordid><startdate>20200201</startdate><enddate>20200201</enddate><creator>Bai, Zhe</creator><creator>Kaiser, Eurika</creator><creator>Proctor, Joshua L</creator><creator>Kutz, J. Nathan</creator><creator>Brunton, Steven L</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20200201</creationdate><title>Dynamic Mode Decomposition for Compressive System Identification</title><author>Bai, Zhe ; Kaiser, Eurika ; Proctor, Joshua L ; Kutz, J. Nathan ; Brunton, Steven L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a429t-231e77caa0a2a922fdbc235f4a2bd57cbf7c9a42282968c98e20d6af3f21fa6b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Actuation</topic><topic>Aerodynamics</topic><topic>Broadband</topic><topic>Compression ratio</topic><topic>Computational fluid dynamics</topic><topic>Data compression</topic><topic>Decomposition</topic><topic>Fluid flow</topic><topic>Identification methods</topic><topic>Nonlinear systems</topic><topic>Reduced order models</topic><topic>Reynolds number</topic><topic>System identification</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bai, Zhe</creatorcontrib><creatorcontrib>Kaiser, Eurika</creatorcontrib><creatorcontrib>Proctor, Joshua L</creatorcontrib><creatorcontrib>Kutz, J. Nathan</creatorcontrib><creatorcontrib>Brunton, Steven L</creatorcontrib><collection>CrossRef</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bai, Zhe</au><au>Kaiser, Eurika</au><au>Proctor, Joshua L</au><au>Kutz, J. Nathan</au><au>Brunton, Steven L</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Dynamic Mode Decomposition for Compressive System Identification</atitle><jtitle>AIAA journal</jtitle><date>2020-02-01</date><risdate>2020</risdate><volume>58</volume><issue>2</issue><spage>561</spage><epage>574</epage><pages>561-574</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>Dynamic mode decomposition has emerged as a leading technique to identify spatiotemporal coherent structures from high-dimensional data, benefiting from a strong connection to nonlinear dynamical systems via the Koopman operator. In this work, two recent innovations that extend dynamic mode decomposition to systems with actuation and systems with heavily subsampled measurements are integrated and unified. When combined, these methods yield a novel framework for compressive system identification. It is possible to identify a low-order model from limited input–output data and reconstruct the associated full-state dynamic modes with compressed sensing, adding interpretability to the state of the reduced-order model. Moreover, when full-state data are available, it is possible to dramatically accelerate downstream computations by first compressing the data. This unified framework is demonstrated on two model systems, investigating the effects of sensor noise, different types of measurements (e.g., point sensors, Gaussian random projections, etc.), compression ratios, and different choices of actuation (e.g., localized, broadband, etc.). In the first example, this architecture is explored on a test system with known low-rank dynamics and an artificially inflated state dimension. The second example consists of a real-world engineering application given by the fluid flow past a pitching airfoil at low Reynolds number. This example provides a challenging and realistic test case for the proposed method, and results demonstrate that the dominant coherent structures are well characterized despite actuation and heavily subsampled data.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J057870</doi><tpages>14</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 0001-1452
ispartof AIAA journal, 2020-02, Vol.58 (2), p.561-574
issn 0001-1452
1533-385X
language eng
recordid cdi_proquest_journals_2351631591
source Alma/SFX Local Collection
subjects Actuation
Aerodynamics
Broadband
Compression ratio
Computational fluid dynamics
Data compression
Decomposition
Fluid flow
Identification methods
Nonlinear systems
Reduced order models
Reynolds number
System identification
title Dynamic Mode Decomposition for Compressive System Identification
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-22T00%3A58%3A57IST&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=Dynamic%20Mode%20Decomposition%20for%20Compressive%20System%20Identification&rft.jtitle=AIAA%20journal&rft.au=Bai,%20Zhe&rft.date=2020-02-01&rft.volume=58&rft.issue=2&rft.spage=561&rft.epage=574&rft.pages=561-574&rft.issn=0001-1452&rft.eissn=1533-385X&rft_id=info:doi/10.2514/1.J057870&rft_dat=%3Cproquest_cross%3E2351631591%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=2351631591&rft_id=info:pmid/&rfr_iscdi=true