Optimization of parallelized power inverters using a direct modelling approach for More Electrical Aircraft
Résumé
This paper presents a new approach to design parallelized power inverters used in More Electrical Aircraft equipment. Dimension-based analytical modelling of building components are described and their use to achieve the optimized design is presented. The results help choosing, among various solutions, which is the optimal (minimizing the global mass) parallelization strategy of two power inverters.
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