Closed-Loop Control Strategy for Simulated Smoke Concentration in Aircraft Cargo Compartment Mock-Up
In airworthiness verification flight test on fire smoke detection systems in aircraft cargo compartments, simulated smoke from a smoke generator that can replicate the characteristics of actual fire smoke should be used. In current studies, most of the boundary conditions of smoke generators are adj...
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description | In airworthiness verification flight test on fire smoke detection systems in aircraft cargo compartments, simulated smoke from a smoke generator that can replicate the characteristics of actual fire smoke should be used. In current studies, most of the boundary conditions of smoke generators are adjusted by open-loop control to fulfill the equivalence of the actual fire smoke. However, this method consumes a large amount of resources and has difficulty achieving optimal results from the complex turbulent flow field of smoke in an aircraft cargo compartment. To solve this problem, a computational fluid dynamics (CFD) model was first established to simulate smoke in the full-scale cargo compartment mock-up. Then, a state-space model with the exit parameters of the smoke generator as the input and the smoke concentration in the full-scale cargo compartment mock-up as the state variable was constructed using the data generated by the CFD model. Subsequently, a closed-loop simulated smoke concentration control strategy is proposed. In this strategy, the sensor in the full-scale cargo compartment mock-up collects the simulated smoke concentration signal and feeds it back to the controller. The controller processes the control target and feedback signal in real time. It realizes the automatic closed-loop control of the simulated smoke concentration by automatically adjusting the boundary condition parameters of the smoke generator. In the control law design, the control input constraint and the error between the linear state-space model and the real flow are considered, making the linear state-space model a nonlinear model. Finally, we prove the stability of the control system. The simulation shows that the designed control law can realize the closed-loop control of smoke concentration. The findings of this study can expand the control of simulated smoke flow field in airworthiness verification flight test from open loop to closed loop, and offer a new theoretical approach for smoke simulation technology. |
doi_str_mv | 10.1007/s10694-023-01433-4 |
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In current studies, most of the boundary conditions of smoke generators are adjusted by open-loop control to fulfill the equivalence of the actual fire smoke. However, this method consumes a large amount of resources and has difficulty achieving optimal results from the complex turbulent flow field of smoke in an aircraft cargo compartment. To solve this problem, a computational fluid dynamics (CFD) model was first established to simulate smoke in the full-scale cargo compartment mock-up. Then, a state-space model with the exit parameters of the smoke generator as the input and the smoke concentration in the full-scale cargo compartment mock-up as the state variable was constructed using the data generated by the CFD model. Subsequently, a closed-loop simulated smoke concentration control strategy is proposed. In this strategy, the sensor in the full-scale cargo compartment mock-up collects the simulated smoke concentration signal and feeds it back to the controller. The controller processes the control target and feedback signal in real time. It realizes the automatic closed-loop control of the simulated smoke concentration by automatically adjusting the boundary condition parameters of the smoke generator. In the control law design, the control input constraint and the error between the linear state-space model and the real flow are considered, making the linear state-space model a nonlinear model. Finally, we prove the stability of the control system. The simulation shows that the designed control law can realize the closed-loop control of smoke concentration. The findings of this study can expand the control of simulated smoke flow field in airworthiness verification flight test from open loop to closed loop, and offer a new theoretical approach for smoke simulation technology.</description><identifier>ISSN: 0015-2684</identifier><identifier>EISSN: 1572-8099</identifier><identifier>DOI: 10.1007/s10694-023-01433-4</identifier><language>eng</language><publisher>New York: Springer US</publisher><subject>Aircraft ; Aircraft detection ; Aircraft reliability ; Automatic control ; Boundary conditions ; Cargo aircraft ; Cargo compartments ; Characterization and Evaluation of Materials ; Civil Engineering ; Classical Mechanics ; Closed loops ; Computational fluid dynamics ; Control systems ; Control theory ; Controllers ; Engineering ; Feedback control ; Feedback control systems ; Flight ; Flight tests ; Fluid dynamics ; Fluid flow ; Hydrodynamics ; Mockups ; Parameters ; Physics ; Sensors ; Simulation ; Smoke ; State space models ; Turbulent flow ; Verification</subject><ispartof>Fire technology, 2023-09, Vol.59 (5), p.2263-2297</ispartof><rights>The Author(s), under exclusive licence to Springer Science+Business Media, LLC, part of Springer Nature 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c270t-329a6c4561b69472dc88ae4fdfd3bf43ba21165f0318b6a2b1496076baa10d9a3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s10694-023-01433-4$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s10694-023-01433-4$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>315,781,785,27928,27929,41492,42561,51323</link.rule.ids></links><search><creatorcontrib>Chen, Xiyuan</creatorcontrib><creatorcontrib>Yan, Xiaoshuang</creatorcontrib><creatorcontrib>Yang, Jianzhong</creatorcontrib><title>Closed-Loop Control Strategy for Simulated Smoke Concentration in Aircraft Cargo Compartment Mock-Up</title><title>Fire technology</title><addtitle>Fire Technol</addtitle><description>In airworthiness verification flight test on fire smoke detection systems in aircraft cargo compartments, simulated smoke from a smoke generator that can replicate the characteristics of actual fire smoke should be used. In current studies, most of the boundary conditions of smoke generators are adjusted by open-loop control to fulfill the equivalence of the actual fire smoke. However, this method consumes a large amount of resources and has difficulty achieving optimal results from the complex turbulent flow field of smoke in an aircraft cargo compartment. To solve this problem, a computational fluid dynamics (CFD) model was first established to simulate smoke in the full-scale cargo compartment mock-up. Then, a state-space model with the exit parameters of the smoke generator as the input and the smoke concentration in the full-scale cargo compartment mock-up as the state variable was constructed using the data generated by the CFD model. Subsequently, a closed-loop simulated smoke concentration control strategy is proposed. In this strategy, the sensor in the full-scale cargo compartment mock-up collects the simulated smoke concentration signal and feeds it back to the controller. The controller processes the control target and feedback signal in real time. It realizes the automatic closed-loop control of the simulated smoke concentration by automatically adjusting the boundary condition parameters of the smoke generator. In the control law design, the control input constraint and the error between the linear state-space model and the real flow are considered, making the linear state-space model a nonlinear model. Finally, we prove the stability of the control system. The simulation shows that the designed control law can realize the closed-loop control of smoke concentration. The findings of this study can expand the control of simulated smoke flow field in airworthiness verification flight test from open loop to closed loop, and offer a new theoretical approach for smoke simulation technology.</description><subject>Aircraft</subject><subject>Aircraft detection</subject><subject>Aircraft reliability</subject><subject>Automatic control</subject><subject>Boundary conditions</subject><subject>Cargo aircraft</subject><subject>Cargo compartments</subject><subject>Characterization and Evaluation of Materials</subject><subject>Civil Engineering</subject><subject>Classical Mechanics</subject><subject>Closed loops</subject><subject>Computational fluid dynamics</subject><subject>Control systems</subject><subject>Control theory</subject><subject>Controllers</subject><subject>Engineering</subject><subject>Feedback control</subject><subject>Feedback control systems</subject><subject>Flight</subject><subject>Flight tests</subject><subject>Fluid dynamics</subject><subject>Fluid flow</subject><subject>Hydrodynamics</subject><subject>Mockups</subject><subject>Parameters</subject><subject>Physics</subject><subject>Sensors</subject><subject>Simulation</subject><subject>Smoke</subject><subject>State space models</subject><subject>Turbulent flow</subject><subject>Verification</subject><issn>0015-2684</issn><issn>1572-8099</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>8G5</sourceid><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><sourceid>GNUQQ</sourceid><sourceid>GUQSH</sourceid><sourceid>M2O</sourceid><recordid>eNp9kMtOwzAQRS0EEuXxA6wssTaMH7GTZRXxkopYlK4tJ7GrtEkc7HTRv8clSOxYjUZz7ozmIHRH4YECqMdIQRaCAOMEqOCciDO0oJliJIeiOEcLAJoRJnNxia5i3AFAoSQsUFN2PtqGrLwfcemHKfgOr6dgJrs9YucDXrf9oUttg9e939sTVNvhRLR-wO2Al22og3ETLk3Y-jTvRxOmPjH43dd7shlv0IUzXbS3v_UabZ6fPstXsvp4eSuXK1IzBRPhrDCyFpmkVXpGsabOc2OFa1zDKyd4ZRilMnPAaV5JwyoqCglKVsZQaArDr9H9vHcM_utg46R3_hCGdFKzPCtUJkSmEsVmqg4-xmCdHkPbm3DUFPTJpp5t6mRT_9jUIoX4HIoJHrY2_K3-J_UNZxZ34Q</recordid><startdate>20230901</startdate><enddate>20230901</enddate><creator>Chen, Xiyuan</creator><creator>Yan, 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Control Strategy for Simulated Smoke Concentration in Aircraft Cargo Compartment Mock-Up</title><author>Chen, Xiyuan ; Yan, Xiaoshuang ; Yang, Jianzhong</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c270t-329a6c4561b69472dc88ae4fdfd3bf43ba21165f0318b6a2b1496076baa10d9a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aircraft</topic><topic>Aircraft detection</topic><topic>Aircraft reliability</topic><topic>Automatic control</topic><topic>Boundary conditions</topic><topic>Cargo aircraft</topic><topic>Cargo compartments</topic><topic>Characterization and Evaluation of Materials</topic><topic>Civil Engineering</topic><topic>Classical Mechanics</topic><topic>Closed loops</topic><topic>Computational fluid dynamics</topic><topic>Control systems</topic><topic>Control theory</topic><topic>Controllers</topic><topic>Engineering</topic><topic>Feedback control</topic><topic>Feedback control systems</topic><topic>Flight</topic><topic>Flight tests</topic><topic>Fluid dynamics</topic><topic>Fluid flow</topic><topic>Hydrodynamics</topic><topic>Mockups</topic><topic>Parameters</topic><topic>Physics</topic><topic>Sensors</topic><topic>Simulation</topic><topic>Smoke</topic><topic>State space models</topic><topic>Turbulent flow</topic><topic>Verification</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Xiyuan</creatorcontrib><creatorcontrib>Yan, Xiaoshuang</creatorcontrib><creatorcontrib>Yang, Jianzhong</creatorcontrib><collection>CrossRef</collection><collection>ProQuest Central (Corporate)</collection><collection>Career and Technical Education (ProQuest Database)</collection><collection>Health and Safety Science Abstracts (Full archive)</collection><collection>ABI/INFORM Collection</collection><collection>Health Medical collection</collection><collection>ProQuest Central (purchase 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collection</collection><collection>Environmental Science Collection</collection><collection>ProQuest Central Basic</collection><jtitle>Fire technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chen, Xiyuan</au><au>Yan, Xiaoshuang</au><au>Yang, Jianzhong</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Closed-Loop Control Strategy for Simulated Smoke Concentration in Aircraft Cargo Compartment Mock-Up</atitle><jtitle>Fire technology</jtitle><stitle>Fire Technol</stitle><date>2023-09-01</date><risdate>2023</risdate><volume>59</volume><issue>5</issue><spage>2263</spage><epage>2297</epage><pages>2263-2297</pages><issn>0015-2684</issn><eissn>1572-8099</eissn><abstract>In airworthiness verification flight test on fire smoke detection systems in aircraft cargo compartments, simulated smoke from a smoke generator that can replicate the characteristics of actual fire smoke should be used. In current studies, most of the boundary conditions of smoke generators are adjusted by open-loop control to fulfill the equivalence of the actual fire smoke. However, this method consumes a large amount of resources and has difficulty achieving optimal results from the complex turbulent flow field of smoke in an aircraft cargo compartment. To solve this problem, a computational fluid dynamics (CFD) model was first established to simulate smoke in the full-scale cargo compartment mock-up. Then, a state-space model with the exit parameters of the smoke generator as the input and the smoke concentration in the full-scale cargo compartment mock-up as the state variable was constructed using the data generated by the CFD model. Subsequently, a closed-loop simulated smoke concentration control strategy is proposed. In this strategy, the sensor in the full-scale cargo compartment mock-up collects the simulated smoke concentration signal and feeds it back to the controller. The controller processes the control target and feedback signal in real time. It realizes the automatic closed-loop control of the simulated smoke concentration by automatically adjusting the boundary condition parameters of the smoke generator. In the control law design, the control input constraint and the error between the linear state-space model and the real flow are considered, making the linear state-space model a nonlinear model. Finally, we prove the stability of the control system. The simulation shows that the designed control law can realize the closed-loop control of smoke concentration. The findings of this study can expand the control of simulated smoke flow field in airworthiness verification flight test from open loop to closed loop, and offer a new theoretical approach for smoke simulation technology.</abstract><cop>New York</cop><pub>Springer US</pub><doi>10.1007/s10694-023-01433-4</doi><tpages>35</tpages></addata></record> |
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subjects | Aircraft Aircraft detection Aircraft reliability Automatic control Boundary conditions Cargo aircraft Cargo compartments Characterization and Evaluation of Materials Civil Engineering Classical Mechanics Closed loops Computational fluid dynamics Control systems Control theory Controllers Engineering Feedback control Feedback control systems Flight Flight tests Fluid dynamics Fluid flow Hydrodynamics Mockups Parameters Physics Sensors Simulation Smoke State space models Turbulent flow Verification |
title | Closed-Loop Control Strategy for Simulated Smoke Concentration in Aircraft Cargo Compartment Mock-Up |
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