Optimal Design of EMALS Based on a Double-Sided Tubular Linear Induction Motor
A novel evolutionary algorithm is used for the optimization of the thrust force of the stages of an electromagnetic aircraft launch system, based on a double-sided tubular linear induction motor. A semianalytical model allows for a fast and accurate prediction of all the electromagnetic quantities i...
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Veröffentlicht in: | IEEE transactions on plasma science 2015-05, Vol.43 (5), p.1326-1331 |
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creator | Musolino, Antonino Raugi, Marco Rizzo, Rocco Tucci, Mauro |
description | A novel evolutionary algorithm is used for the optimization of the thrust force of the stages of an electromagnetic aircraft launch system, based on a double-sided tubular linear induction motor. A semianalytical model allows for a fast and accurate prediction of all the electromagnetic quantities in the device, including the thrust force, the back electromotive force, the distribution of the induced current density, and the average magnetic flux density in the teeth. Using the semianalytical formulation, the characterization of the machine is greatly facilitated, so allowing a fast evaluation of the cost function and of the design constraints. |
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A semianalytical model allows for a fast and accurate prediction of all the electromagnetic quantities in the device, including the thrust force, the back electromotive force, the distribution of the induced current density, and the average magnetic flux density in the teeth. Using the semianalytical formulation, the characterization of the machine is greatly facilitated, so allowing a fast evaluation of the cost function and of the design constraints.</description><identifier>ISSN: 0093-3813</identifier><identifier>EISSN: 1939-9375</identifier><identifier>DOI: 10.1109/TPS.2015.2413675</identifier><identifier>CODEN: ITPSBD</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Aircraft ; Current density ; Design optimization ; Electric currents ; Electromagnetic analysis ; Electromagnetics ; Force ; Genetic algorithms ; induction accelerators ; Induction motors ; linear motors ; Optimization ; optimization methods ; Stators ; Vectors</subject><ispartof>IEEE transactions on plasma science, 2015-05, Vol.43 (5), p.1326-1331</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. 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A semianalytical model allows for a fast and accurate prediction of all the electromagnetic quantities in the device, including the thrust force, the back electromotive force, the distribution of the induced current density, and the average magnetic flux density in the teeth. Using the semianalytical formulation, the characterization of the machine is greatly facilitated, so allowing a fast evaluation of the cost function and of the design constraints.</description><subject>Aircraft</subject><subject>Current density</subject><subject>Design optimization</subject><subject>Electric currents</subject><subject>Electromagnetic analysis</subject><subject>Electromagnetics</subject><subject>Force</subject><subject>Genetic algorithms</subject><subject>induction accelerators</subject><subject>Induction motors</subject><subject>linear motors</subject><subject>Optimization</subject><subject>optimization methods</subject><subject>Stators</subject><subject>Vectors</subject><issn>0093-3813</issn><issn>1939-9375</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNo9kM9LwzAUx4MoOKd3wUvAc-dL0jTNcW5TB50TNs8hTVLpmM1M2oP_vRkbnh48Pt_344PQPYEJISCfth-bCQXCJzQnrBD8Ao2IZDKTTPBLNAKQLGMlYdfoJsYdAMk50BF6Xx_69lvv8dzF9qvDvsGL1bTa4GcdncW-wxrP_VDvXbZpbepsh3rY64CrtnOpLDs7mL5N3Mr3Ptyiq0bvo7s71zH6fFlsZ29ZtX5dzqZVZnLB-kyXroYypzVrDNMmr9OpxtFCUENLIxij1DacyZLkAFbnpuaNKKVtnNPGgmVj9Hiaewj-Z3CxVzs_hC6tVKQoaSELInii4ESZ4GMMrlGHkJ4Nv4qAOlpTyZo6WlNnaynycIq0zrl_XICgPBn8A-fZZy8</recordid><startdate>20150501</startdate><enddate>20150501</enddate><creator>Musolino, Antonino</creator><creator>Raugi, Marco</creator><creator>Rizzo, Rocco</creator><creator>Tucci, Mauro</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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subjects | Aircraft Current density Design optimization Electric currents Electromagnetic analysis Electromagnetics Force Genetic algorithms induction accelerators Induction motors linear motors Optimization optimization methods Stators Vectors |
title | Optimal Design of EMALS Based on a Double-Sided Tubular Linear Induction Motor |
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