A Model-Based Multi-Objective Optimization for High Efficiency and High Power Density Motor Drive Inverters for Aircraft Applications
Authors:
- 1 July 2018
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 36-42
Abstract
This paper proposes a multi-objective design optimization methodology for power-electronics inverters with more electric aircraft applications, which orients the optimum design point of both passive components and semiconductors between power density and efficiency of the inverter system based on semi-physical mathematical models and multi-level sub-optimization models. This algorithm is demonstrated by designing a 25 kW 2-level motor-drive inverter and showing superior performances than state-of-arts products.Keywords
This publication has 6 references indexed in Scilit:
- The More Electric Aircraft: Technology and challengesIEEE Electrification Magazine, 2014
- Overview of Electric Motor Technologies Used for More Electric Aircraft (MEA)IEEE Transactions on Industrial Electronics, 2011
- Moving towards a more electric aircraftIEEE Aerospace and Electronic Systems Magazine, 2007
- Using transformer parasitics for resonant converters - a review of the calculation of the stray capacitance of transformers2005
- Comparative Evaluation of Three-Phase High-Power-Factor AC–DC Converter Concepts for Application in Future More Electric AircraftIEEE Transactions on Industrial Electronics, 2005
- Electrical power technology for the more electric aircraft2002