Rapid prototyping of advanced control schemes in ASDEX Upgrade
The integration of advanced control schemes is becoming more important as the development of fusion experiments progresses. The ASDEX Upgrade discharge control system (DCS) is designed to be adaptable via configuration, no recompilation is necessary to tailor the behaviour of the control system. In...
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Veröffentlicht in: | Fusion engineering and design 2020-12, Vol.161, p.111958, Article 111958 |
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description | The integration of advanced control schemes is becoming more important as the development of fusion experiments progresses. The ASDEX Upgrade discharge control system (DCS) is designed to be adaptable via configuration, no recompilation is necessary to tailor the behaviour of the control system.
In order to enable advanced control schemes the required information has to be available during the discharge. With the DCS satellite concept the control system can easily be extended by including, e.g. diagnostics, actuators and data processing nodes. In this paper the extension of DCS for rapid prototyping of control schemes is discussed.
To easily add and modify input signals used for advanced control schemes, without the requirement to have expert knowledge of the control system by the experimentalist, a new application process (AP) has been implemented using the C++ Mathematical Expression Toolkit Library (ExprTk), which enables the inclusion of run-time mathematical expressions into DCS. The AP is operated separately from the central DCS as a DCS satellite. This is done to be able to test and validate the calculations without having to make changes to DCS.
For tokamak operation, disruptions pose a major threat especially for large devices such as ITER. Therefore, disruption avoidance is an active field of research and the inclusion of avoidance schemes into DCS as part of exception handling is ongoing. For the case of H-Mode density limit disruptions an avoidance scheme using central heating has been implemented and successfully tested on ASDEX Upgrade, exploiting these new features for rapid development and testing. |
doi_str_mv | 10.1016/j.fusengdes.2020.111958 |
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In order to enable advanced control schemes the required information has to be available during the discharge. With the DCS satellite concept the control system can easily be extended by including, e.g. diagnostics, actuators and data processing nodes. In this paper the extension of DCS for rapid prototyping of control schemes is discussed.
To easily add and modify input signals used for advanced control schemes, without the requirement to have expert knowledge of the control system by the experimentalist, a new application process (AP) has been implemented using the C++ Mathematical Expression Toolkit Library (ExprTk), which enables the inclusion of run-time mathematical expressions into DCS. The AP is operated separately from the central DCS as a DCS satellite. This is done to be able to test and validate the calculations without having to make changes to DCS.
For tokamak operation, disruptions pose a major threat especially for large devices such as ITER. Therefore, disruption avoidance is an active field of research and the inclusion of avoidance schemes into DCS as part of exception handling is ongoing. For the case of H-Mode density limit disruptions an avoidance scheme using central heating has been implemented and successfully tested on ASDEX Upgrade, exploiting these new features for rapid development and testing.</description><identifier>ISSN: 0920-3796</identifier><identifier>EISSN: 1873-7196</identifier><identifier>DOI: 10.1016/j.fusengdes.2020.111958</identifier><language>eng</language><publisher>Amsterdam: Elsevier B.V</publisher><subject>Actuators ; Avoidance ; Central heating ; Control ; Control systems design ; Data processing ; Discharge ; Disruption ; Exception handling ; Mathematical analysis ; Nuclear research ; Prototyping ; Rapid prototyping ; Tokamak ; Toolkits</subject><ispartof>Fusion engineering and design, 2020-12, Vol.161, p.111958, Article 111958</ispartof><rights>2020 Elsevier B.V.</rights><rights>Copyright Elsevier Science Ltd. Dec 2020</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c392t-a9ae032f153d9db487df9c4f0f647964f0173f77d1ab0a70c3c8a96d3eee49423</citedby><cites>FETCH-LOGICAL-c392t-a9ae032f153d9db487df9c4f0f647964f0173f77d1ab0a70c3c8a96d3eee49423</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0920379620305068$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids></links><search><creatorcontrib>Sieglin, B.</creatorcontrib><creatorcontrib>Maraschek, M.</creatorcontrib><creatorcontrib>Kudlacek, O.</creatorcontrib><creatorcontrib>Gude, A.</creatorcontrib><creatorcontrib>Treutterer, W.</creatorcontrib><creatorcontrib>Kölbl, M.</creatorcontrib><creatorcontrib>Lenz, A.</creatorcontrib><creatorcontrib>the ASDEX Upgrade Team, the EUROfusion MST1 Team</creatorcontrib><title>Rapid prototyping of advanced control schemes in ASDEX Upgrade</title><title>Fusion engineering and design</title><description>The integration of advanced control schemes is becoming more important as the development of fusion experiments progresses. The ASDEX Upgrade discharge control system (DCS) is designed to be adaptable via configuration, no recompilation is necessary to tailor the behaviour of the control system.
In order to enable advanced control schemes the required information has to be available during the discharge. With the DCS satellite concept the control system can easily be extended by including, e.g. diagnostics, actuators and data processing nodes. In this paper the extension of DCS for rapid prototyping of control schemes is discussed.
To easily add and modify input signals used for advanced control schemes, without the requirement to have expert knowledge of the control system by the experimentalist, a new application process (AP) has been implemented using the C++ Mathematical Expression Toolkit Library (ExprTk), which enables the inclusion of run-time mathematical expressions into DCS. The AP is operated separately from the central DCS as a DCS satellite. This is done to be able to test and validate the calculations without having to make changes to DCS.
For tokamak operation, disruptions pose a major threat especially for large devices such as ITER. Therefore, disruption avoidance is an active field of research and the inclusion of avoidance schemes into DCS as part of exception handling is ongoing. For the case of H-Mode density limit disruptions an avoidance scheme using central heating has been implemented and successfully tested on ASDEX Upgrade, exploiting these new features for rapid development and testing.</description><subject>Actuators</subject><subject>Avoidance</subject><subject>Central heating</subject><subject>Control</subject><subject>Control systems design</subject><subject>Data processing</subject><subject>Discharge</subject><subject>Disruption</subject><subject>Exception handling</subject><subject>Mathematical analysis</subject><subject>Nuclear research</subject><subject>Prototyping</subject><subject>Rapid prototyping</subject><subject>Tokamak</subject><subject>Toolkits</subject><issn>0920-3796</issn><issn>1873-7196</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNqFkFFLAzEMx4soOKefwYLPN9vr7Xp9EcbcVBgI6sC30rXp7LFdz_Y22Le3x4mvhkBCSP5JfgjdUjKhhJb39cQeIjRbA3GSkzxVKRXT6gyNaMVZxqkoz9GIiJxkjIvyEl3FWBNCefIRenhTrTO4Db7z3al1zRZ7i5U5qkaDwdo3XfA7HPUX7CFi1-DZ--PiE6_bbVAGrtGFVbsIN79xjNbLxcf8OVu9Pr3MZ6tMM5F3mRIKCMstnTIjzKaouLFCF5bYskg3pYRyZjk3VG2I4kQzXSlRGgYAhShyNkZ3g2469PsAsZO1P4QmrZR5wSvaW5G6-NClg48xgJVtcHsVTpIS2cOStfyDJXtYcoCVJmfDJKQnjg6CjNpBj8AF0J003v2r8QPjQXY2</recordid><startdate>202012</startdate><enddate>202012</enddate><creator>Sieglin, B.</creator><creator>Maraschek, M.</creator><creator>Kudlacek, O.</creator><creator>Gude, A.</creator><creator>Treutterer, W.</creator><creator>Kölbl, M.</creator><creator>Lenz, A.</creator><general>Elsevier B.V</general><general>Elsevier Science Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KR7</scope><scope>L7M</scope></search><sort><creationdate>202012</creationdate><title>Rapid prototyping of advanced control schemes in ASDEX Upgrade</title><author>Sieglin, B. ; Maraschek, M. ; Kudlacek, O. ; Gude, A. ; Treutterer, W. ; Kölbl, M. ; Lenz, A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c392t-a9ae032f153d9db487df9c4f0f647964f0173f77d1ab0a70c3c8a96d3eee49423</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Actuators</topic><topic>Avoidance</topic><topic>Central heating</topic><topic>Control</topic><topic>Control systems design</topic><topic>Data processing</topic><topic>Discharge</topic><topic>Disruption</topic><topic>Exception handling</topic><topic>Mathematical analysis</topic><topic>Nuclear research</topic><topic>Prototyping</topic><topic>Rapid prototyping</topic><topic>Tokamak</topic><topic>Toolkits</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sieglin, B.</creatorcontrib><creatorcontrib>Maraschek, M.</creatorcontrib><creatorcontrib>Kudlacek, O.</creatorcontrib><creatorcontrib>Gude, A.</creatorcontrib><creatorcontrib>Treutterer, W.</creatorcontrib><creatorcontrib>Kölbl, M.</creatorcontrib><creatorcontrib>Lenz, A.</creatorcontrib><creatorcontrib>the ASDEX Upgrade Team, the EUROfusion MST1 Team</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Fusion engineering and design</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Sieglin, B.</au><au>Maraschek, M.</au><au>Kudlacek, O.</au><au>Gude, A.</au><au>Treutterer, W.</au><au>Kölbl, M.</au><au>Lenz, A.</au><aucorp>the ASDEX Upgrade Team, the EUROfusion MST1 Team</aucorp><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Rapid prototyping of advanced control schemes in ASDEX Upgrade</atitle><jtitle>Fusion engineering and design</jtitle><date>2020-12</date><risdate>2020</risdate><volume>161</volume><spage>111958</spage><pages>111958-</pages><artnum>111958</artnum><issn>0920-3796</issn><eissn>1873-7196</eissn><abstract>The integration of advanced control schemes is becoming more important as the development of fusion experiments progresses. The ASDEX Upgrade discharge control system (DCS) is designed to be adaptable via configuration, no recompilation is necessary to tailor the behaviour of the control system.
In order to enable advanced control schemes the required information has to be available during the discharge. With the DCS satellite concept the control system can easily be extended by including, e.g. diagnostics, actuators and data processing nodes. In this paper the extension of DCS for rapid prototyping of control schemes is discussed.
To easily add and modify input signals used for advanced control schemes, without the requirement to have expert knowledge of the control system by the experimentalist, a new application process (AP) has been implemented using the C++ Mathematical Expression Toolkit Library (ExprTk), which enables the inclusion of run-time mathematical expressions into DCS. The AP is operated separately from the central DCS as a DCS satellite. This is done to be able to test and validate the calculations without having to make changes to DCS.
For tokamak operation, disruptions pose a major threat especially for large devices such as ITER. Therefore, disruption avoidance is an active field of research and the inclusion of avoidance schemes into DCS as part of exception handling is ongoing. For the case of H-Mode density limit disruptions an avoidance scheme using central heating has been implemented and successfully tested on ASDEX Upgrade, exploiting these new features for rapid development and testing.</abstract><cop>Amsterdam</cop><pub>Elsevier B.V</pub><doi>10.1016/j.fusengdes.2020.111958</doi><oa>free_for_read</oa></addata></record> |
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subjects | Actuators Avoidance Central heating Control Control systems design Data processing Discharge Disruption Exception handling Mathematical analysis Nuclear research Prototyping Rapid prototyping Tokamak Toolkits |
title | Rapid prototyping of advanced control schemes in ASDEX Upgrade |
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