Rapid-prototyping and hardware-in-the-loop laboratory platform for development and testing of electro-mechanical actuator controls
To meet the challenges posed by the increasing use of electrical actuation on board next generation aircraft, advanced experimental testing capabilities are required to investigate optimal system design, performance and control. Rapid control-prototyping and hardware-in-the-loop (HiL) techniques pro...
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| Veröffentlicht in: | Journal of engineering (Stevenage, England) England), 2019-06, Vol.2019 (17), p.4133-4137 |
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| container_issue | 17 |
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| container_title | Journal of engineering (Stevenage, England) |
| container_volume | 2019 |
| creator | Hogan, Diarmaid Albiol-Tendillo, Laura Kelleher, Brendan Valdivia-Guerrero, Virgilio Foley, Raymond |
| description | To meet the challenges posed by the increasing use of electrical actuation on board next generation aircraft, advanced experimental testing capabilities are required to investigate optimal system design, performance and control. Rapid control-prototyping and hardware-in-the-loop (HiL) techniques provide the ability to expedite experimental testing, allowing for elements of the system to be validated without requiring fully realised hardware. Previously, this would require large scale laboratory setups, where the entire electrical and mechanical system would have to be designed and built prior to experimental testing. This study presents the development of a laboratory HiL and rapid-prototyping test-bench, capable of investigating the performance of actuator motor control schemes, under a variety of test conditions. Experimental testing is carried out using a laboratory test-bench, demonstrating the performance of landing gear electromechanical actuator controls under power system and load transients. |
| doi_str_mv | 10.1049/joe.2018.8239 |
| format | Article |
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Rapid control-prototyping and hardware-in-the-loop (HiL) techniques provide the ability to expedite experimental testing, allowing for elements of the system to be validated without requiring fully realised hardware. Previously, this would require large scale laboratory setups, where the entire electrical and mechanical system would have to be designed and built prior to experimental testing. This study presents the development of a laboratory HiL and rapid-prototyping test-bench, capable of investigating the performance of actuator motor control schemes, under a variety of test conditions. Experimental testing is carried out using a laboratory test-bench, demonstrating the performance of landing gear electromechanical actuator controls under power system and load transients.</description><subject>actuator motor control schemes</subject><subject>actuators</subject><subject>advanced experimental testing capabilities</subject><subject>aircraft</subject><subject>board next generation aircraft</subject><subject>control engineering computing</subject><subject>control system synthesis</subject><subject>electric actuators</subject><subject>electrical actuation</subject><subject>electro-mechanical actuator controls</subject><subject>electromechanical actuators</subject><subject>entire electrical system</subject><subject>gears</subject><subject>hardware-in-the-loop laboratory platform</subject><subject>hardware-in-the-loop techniques</subject><subject>laboratory HiL</subject><subject>laboratory test-bench</subject><subject>landing gear electromechanical actuator controls</subject><subject>machine control</subject><subject>mechanical system</subject><subject>optimal system design</subject><subject>power system</subject><subject>rapid control-prototyping</subject><subject>rapid-prototyping</subject><subject>scale laboratory setups</subject><subject>test conditions</subject><subject>The 9th International Conference on Power Electronics, Machines and Drives (PEMD 2018)</subject><subject>torque control</subject><issn>2051-3305</issn><issn>2051-3305</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><sourceid>24P</sourceid><sourceid>WIN</sourceid><sourceid>DOA</sourceid><recordid>eNp9kc1P3DAQxSMEUhFw7N1XDt76M4mPLQK6FRISgrM1sSesV944ckzRXvnLm7BVxaVcZkae934j-VXVV85WnCnzbZtwJRhvV62Q5qg6FUxzKiXTxx_mL9XFNG0ZY1wqwRQ_rd4eYAyejjmVVPZjGJ4JDJ5sIPtXyEjDQMsGaUxpJBG6lKGkvCdjhNKnvCNzIR5_Y0zjDofybi44lQWUeoIRXcmJ7tBtYAgOIgFXXhYIcWmYV3E6r056iBNe_O1n1dPN9ePVT3p3f7u--n5HndSypk57KYxpO-2d6qTppa57h52C3inegOO6k8C9rF3HALuOKd0w59u6BSGbRp5V6wPXJ9jaMYcd5L1NEOz7Q8rPFnIJLqKtWyXASSPQa-VNDZ67ttGKm0ahgH5m0QPL5TRNGft_PM7skoed87BLHnbJY9bXB_1riLj_XGwff12LHzeMG1HPxsuDMWCZZS95mL_oP0f-AC_Gnw4</recordid><startdate>201906</startdate><enddate>201906</enddate><creator>Hogan, Diarmaid</creator><creator>Albiol-Tendillo, Laura</creator><creator>Kelleher, Brendan</creator><creator>Valdivia-Guerrero, Virgilio</creator><creator>Foley, Raymond</creator><general>The Institution of Engineering and Technology</general><general>Wiley</general><scope>IDLOA</scope><scope>24P</scope><scope>WIN</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>DOA</scope></search><sort><creationdate>201906</creationdate><title>Rapid-prototyping and hardware-in-the-loop laboratory platform for development and testing of electro-mechanical actuator controls</title><author>Hogan, Diarmaid ; Albiol-Tendillo, Laura ; Kelleher, Brendan ; Valdivia-Guerrero, Virgilio ; Foley, Raymond</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3536-c5d32998b5dc4b39f356fceb4afc417ac15b3a1d36cb0aebb04570cd868a23773</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>actuator motor control schemes</topic><topic>actuators</topic><topic>advanced experimental testing capabilities</topic><topic>aircraft</topic><topic>board next generation aircraft</topic><topic>control engineering computing</topic><topic>control system synthesis</topic><topic>electric actuators</topic><topic>electrical actuation</topic><topic>electro-mechanical actuator controls</topic><topic>electromechanical actuators</topic><topic>entire electrical system</topic><topic>gears</topic><topic>hardware-in-the-loop laboratory platform</topic><topic>hardware-in-the-loop techniques</topic><topic>laboratory HiL</topic><topic>laboratory test-bench</topic><topic>landing gear electromechanical actuator controls</topic><topic>machine control</topic><topic>mechanical system</topic><topic>optimal system design</topic><topic>power system</topic><topic>rapid control-prototyping</topic><topic>rapid-prototyping</topic><topic>scale laboratory setups</topic><topic>test conditions</topic><topic>The 9th International Conference on Power Electronics, Machines and Drives (PEMD 2018)</topic><topic>torque control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hogan, Diarmaid</creatorcontrib><creatorcontrib>Albiol-Tendillo, Laura</creatorcontrib><creatorcontrib>Kelleher, Brendan</creatorcontrib><creatorcontrib>Valdivia-Guerrero, Virgilio</creatorcontrib><creatorcontrib>Foley, Raymond</creatorcontrib><collection>IET Digital Library (Open Access)</collection><collection>Wiley-Blackwell Open Access Titles</collection><collection>Wiley Free Content</collection><collection>CrossRef</collection><collection>DOAJ Directory of Open Access Journals</collection><jtitle>Journal of engineering (Stevenage, England)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hogan, Diarmaid</au><au>Albiol-Tendillo, Laura</au><au>Kelleher, Brendan</au><au>Valdivia-Guerrero, Virgilio</au><au>Foley, Raymond</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Rapid-prototyping and hardware-in-the-loop laboratory platform for development and testing of electro-mechanical actuator controls</atitle><jtitle>Journal of engineering (Stevenage, England)</jtitle><date>2019-06</date><risdate>2019</risdate><volume>2019</volume><issue>17</issue><spage>4133</spage><epage>4137</epage><pages>4133-4137</pages><issn>2051-3305</issn><eissn>2051-3305</eissn><abstract>To meet the challenges posed by the increasing use of electrical actuation on board next generation aircraft, advanced experimental testing capabilities are required to investigate optimal system design, performance and control. Rapid control-prototyping and hardware-in-the-loop (HiL) techniques provide the ability to expedite experimental testing, allowing for elements of the system to be validated without requiring fully realised hardware. Previously, this would require large scale laboratory setups, where the entire electrical and mechanical system would have to be designed and built prior to experimental testing. This study presents the development of a laboratory HiL and rapid-prototyping test-bench, capable of investigating the performance of actuator motor control schemes, under a variety of test conditions. Experimental testing is carried out using a laboratory test-bench, demonstrating the performance of landing gear electromechanical actuator controls under power system and load transients.</abstract><pub>The Institution of Engineering and Technology</pub><doi>10.1049/joe.2018.8239</doi><tpages>5</tpages><oa>free_for_read</oa></addata></record> |
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| subjects | actuator motor control schemes actuators advanced experimental testing capabilities aircraft board next generation aircraft control engineering computing control system synthesis electric actuators electrical actuation electro-mechanical actuator controls electromechanical actuators entire electrical system gears hardware-in-the-loop laboratory platform hardware-in-the-loop techniques laboratory HiL laboratory test-bench landing gear electromechanical actuator controls machine control mechanical system optimal system design power system rapid control-prototyping rapid-prototyping scale laboratory setups test conditions The 9th International Conference on Power Electronics, Machines and Drives (PEMD 2018) torque control |
| title | Rapid-prototyping and hardware-in-the-loop laboratory platform for development and testing of electro-mechanical actuator controls |
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