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
Hauptverfasser: Musolino, Antonino, Raugi, Marco, Rizzo, Rocco, Tucci, Mauro
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container_title IEEE transactions on plasma science
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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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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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