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Multi-objective Thermal Optimization of Dual-input Aeronautic Static Inverter Based on MOEA/D

YAN Jie GE Hongjuan WANG Yongshuai LI Huang

南京航空航天大学学报：英文版2022，Vol.39Issue(S01)：P.65-72,8.

南京航空航天大学学报：英文版2022，Vol.39Issue(S01)：P.65-72,8.DOI:10.16356/j.1005-1120.2022.S.009

Multi-objective Thermal Optimization of Dual-input Aeronautic Static Inverter Based on MOEA/D

YAN Jie ¹GE Hongjuan ¹WANG Yongshuai ²LI Huang¹

作者信息

1. College of Civil Aviation,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,P.R.China
2. College of Automation,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,P.R.China
折叠

摘要

关键词

aeronautic static inverter/thermal optimization/heat sink/MOEA/D/fuzzy set theory

分类

航空航天

引用本文复制引用

YAN Jie,GE Hongjuan,WANG Yongshuai,LI Huang..Multi-objective Thermal Optimization of Dual-input Aeronautic Static Inverter Based on MOEA/D[J].南京航空航天大学学报：英文版,2022,39(S01):P.65-72,8.

基金项目

supported by the National Natural Science Foundation of China(Nos.U1933115,U2133203) （Nos.U1933115,U2133203）

南京航空航天大学学报：英文版

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ISSN：1005-1120

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