Frequency-Weighted Model Predictive Control of Trailing Edge Flaps on a Wind Turbine Blade
This paper presents the load reduction achieved with trailing edge flaps during a full-scale test on a Vestas V27 wind turbine. The trailing edge flap controller is a frequency-weighted linear model predictive control (MPC) where the quadratic cost consists of costs on the zero-phase filtered flapwi...
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| Veröffentlicht in: | IEEE transactions on control systems technology 2013-07, Vol.21 (4), p.1105-1116 |
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| container_title | IEEE transactions on control systems technology |
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| creator | Castaignet, Damien Couchman, Ian Poulsen, Niels Kjolstad Buhl, Thomas Wedel-Heinen, Jens Jakob |
| description | This paper presents the load reduction achieved with trailing edge flaps during a full-scale test on a Vestas V27 wind turbine. The trailing edge flap controller is a frequency-weighted linear model predictive control (MPC) where the quadratic cost consists of costs on the zero-phase filtered flapwise blade root moment and trailing edge flap deflection. Frequency-weighted MPC is chosen for its ability to handle constraints on the trailing edge flaps deflection, and to target at loads with given frequencies only. The controller is first tested in servo-aeroelastic simulations, before being implemented on a Vestas V27 wind turbine. Consistent load reduction is achieved during the full-scale test. An average of 13.8% flapwise blade root fatigue load reduction is measured. |
| doi_str_mv | 10.1109/TCST.2013.2260750 |
| format | Article |
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The trailing edge flap controller is a frequency-weighted linear model predictive control (MPC) where the quadratic cost consists of costs on the zero-phase filtered flapwise blade root moment and trailing edge flap deflection. Frequency-weighted MPC is chosen for its ability to handle constraints on the trailing edge flaps deflection, and to target at loads with given frequencies only. The controller is first tested in servo-aeroelastic simulations, before being implemented on a Vestas V27 wind turbine. Consistent load reduction is achieved during the full-scale test. An average of 13.8% flapwise blade root fatigue load reduction is measured.</description><identifier>ISSN: 1063-6536</identifier><identifier>EISSN: 1558-0865</identifier><identifier>DOI: 10.1109/TCST.2013.2260750</identifier><identifier>CODEN: IETTE2</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Aerodynamics ; Blades ; Deflection ; Fatigue ; Load alleviation ; Load modeling ; Mathematical models ; model predictive control (MPC) ; Predictive control ; Reduction ; Roots ; Rotors ; Trailing edge flaps ; wind energy ; Wind speed ; Wind turbines</subject><ispartof>IEEE transactions on control systems technology, 2013-07, Vol.21 (4), p.1105-1116</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) Jul 2013</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c326t-dd0a3f7b0809266d207974849677099ed419964de7b695fe69d51ab3432cc91e3</citedby><cites>FETCH-LOGICAL-c326t-dd0a3f7b0809266d207974849677099ed419964de7b695fe69d51ab3432cc91e3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/6525363$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,780,784,796,27924,27925,54758</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/6525363$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Castaignet, Damien</creatorcontrib><creatorcontrib>Couchman, Ian</creatorcontrib><creatorcontrib>Poulsen, Niels Kjolstad</creatorcontrib><creatorcontrib>Buhl, Thomas</creatorcontrib><creatorcontrib>Wedel-Heinen, Jens Jakob</creatorcontrib><title>Frequency-Weighted Model Predictive Control of Trailing Edge Flaps on a Wind Turbine Blade</title><title>IEEE transactions on control systems technology</title><addtitle>TCST</addtitle><description>This paper presents the load reduction achieved with trailing edge flaps during a full-scale test on a Vestas V27 wind turbine. The trailing edge flap controller is a frequency-weighted linear model predictive control (MPC) where the quadratic cost consists of costs on the zero-phase filtered flapwise blade root moment and trailing edge flap deflection. Frequency-weighted MPC is chosen for its ability to handle constraints on the trailing edge flaps deflection, and to target at loads with given frequencies only. The controller is first tested in servo-aeroelastic simulations, before being implemented on a Vestas V27 wind turbine. Consistent load reduction is achieved during the full-scale test. An average of 13.8% flapwise blade root fatigue load reduction is measured.</description><subject>Aerodynamics</subject><subject>Blades</subject><subject>Deflection</subject><subject>Fatigue</subject><subject>Load alleviation</subject><subject>Load modeling</subject><subject>Mathematical models</subject><subject>model predictive control (MPC)</subject><subject>Predictive control</subject><subject>Reduction</subject><subject>Roots</subject><subject>Rotors</subject><subject>Trailing edge flaps</subject><subject>wind energy</subject><subject>Wind speed</subject><subject>Wind turbines</subject><issn>1063-6536</issn><issn>1558-0865</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNpdkM9LwzAUx4soOKd_gHgJePHSmR9N0hy1bCooClYGXkLavM6MrplJJ-y_t2PDg6f3Dp_vl_c-SXJJ8IQQrG7L4r2cUEzYhFKBJcdHyYhwnqc4F_x42LFgqeBMnCZnMS4xJhmncpR8zgJ8b6Crt-kc3OKrB4tevIUWvQWwru7dD6DCd33wLfINKoNxresWaGoXgGatWUfkO2TQ3HUWlZtQuQ7QfWssnCcnjWkjXBzmOPmYTcviMX1-fXgq7p7TmlHRp9ZiwxpZ4RwrKoSlWCqZ5ZkSUmKlwGZEKZFZkJVQvAGhLCemYhmjda0IsHFys-9dBz-8Enu9crGGtjUd-E3UJCMyF4oSPqDX_9Cl34RuuE4TtkMyntOBInuqDj7GAI1eB7cyYasJ1jvbemdb72zrg-0hc7XPOAD44wWng3LGfgFFY3kC</recordid><startdate>20130701</startdate><enddate>20130701</enddate><creator>Castaignet, Damien</creator><creator>Couchman, Ian</creator><creator>Poulsen, Niels Kjolstad</creator><creator>Buhl, Thomas</creator><creator>Wedel-Heinen, Jens Jakob</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</general><scope>97E</scope><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>L7M</scope><scope>F28</scope><scope>H8D</scope></search><sort><creationdate>20130701</creationdate><title>Frequency-Weighted Model Predictive Control of Trailing Edge Flaps on a Wind Turbine Blade</title><author>Castaignet, Damien ; Couchman, Ian ; Poulsen, Niels Kjolstad ; Buhl, Thomas ; Wedel-Heinen, Jens Jakob</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c326t-dd0a3f7b0809266d207974849677099ed419964de7b695fe69d51ab3432cc91e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Aerodynamics</topic><topic>Blades</topic><topic>Deflection</topic><topic>Fatigue</topic><topic>Load alleviation</topic><topic>Load modeling</topic><topic>Mathematical models</topic><topic>model predictive control (MPC)</topic><topic>Predictive control</topic><topic>Reduction</topic><topic>Roots</topic><topic>Rotors</topic><topic>Trailing edge flaps</topic><topic>wind energy</topic><topic>Wind speed</topic><topic>Wind turbines</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Castaignet, Damien</creatorcontrib><creatorcontrib>Couchman, Ian</creatorcontrib><creatorcontrib>Poulsen, Niels Kjolstad</creatorcontrib><creatorcontrib>Buhl, Thomas</creatorcontrib><creatorcontrib>Wedel-Heinen, Jens Jakob</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 2005-present</collection><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Xplore (Online service)</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Aerospace Database</collection><jtitle>IEEE transactions on control systems technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Castaignet, Damien</au><au>Couchman, Ian</au><au>Poulsen, Niels Kjolstad</au><au>Buhl, Thomas</au><au>Wedel-Heinen, Jens Jakob</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Frequency-Weighted Model Predictive Control of Trailing Edge Flaps on a Wind Turbine Blade</atitle><jtitle>IEEE transactions on control systems technology</jtitle><stitle>TCST</stitle><date>2013-07-01</date><risdate>2013</risdate><volume>21</volume><issue>4</issue><spage>1105</spage><epage>1116</epage><pages>1105-1116</pages><issn>1063-6536</issn><eissn>1558-0865</eissn><coden>IETTE2</coden><abstract>This paper presents the load reduction achieved with trailing edge flaps during a full-scale test on a Vestas V27 wind turbine. The trailing edge flap controller is a frequency-weighted linear model predictive control (MPC) where the quadratic cost consists of costs on the zero-phase filtered flapwise blade root moment and trailing edge flap deflection. Frequency-weighted MPC is chosen for its ability to handle constraints on the trailing edge flaps deflection, and to target at loads with given frequencies only. The controller is first tested in servo-aeroelastic simulations, before being implemented on a Vestas V27 wind turbine. Consistent load reduction is achieved during the full-scale test. An average of 13.8% flapwise blade root fatigue load reduction is measured.</abstract><cop>New York</cop><pub>IEEE</pub><doi>10.1109/TCST.2013.2260750</doi><tpages>12</tpages></addata></record> |
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| source | IEEE Xplore (Online service) |
| subjects | Aerodynamics Blades Deflection Fatigue Load alleviation Load modeling Mathematical models model predictive control (MPC) Predictive control Reduction Roots Rotors Trailing edge flaps wind energy Wind speed Wind turbines |
| title | Frequency-Weighted Model Predictive Control of Trailing Edge Flaps on a Wind Turbine Blade |
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