Electrification is a remarkable trend in the aviation industry; electric machines and power electronics systems have been increasingly embedded in aerospace applications. In this field, the above systems are mainly used in the flight control system, propulsion power system, engine starting/generating system, environmental control system, braking system, and fuel and hydraulic system. The power density, operating efficiency, integration degree, and reliability are critical performance requirements, which contain complex mutual coupling and conflicting requirements that need to be carefully considered. Furthermore, the specific external environment and load characteristics of the aviation applications will unavoidably pose challenges for the design and control of the electric machines and power electronics systems. This special issue aims to collect advanced theoretical and technological research findings in the design and control for electric machines, power converters, drives, and systems in more electric aircraft (MEA). Manuscripts with both theoretical interpretation and practical verification are strongly encouraged. Topics of interest include (but are not limited to):

中文翻译：

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更多电动飞机特刊

电气化是航空业的一个显着趋势；电机和电力电子系统越来越多地嵌入到航空航天应用中。在该领域，上述系统主要应用于飞行控制系统、推进动力系统、发动机启动/发电系统、环境控制系统、制动系统以及燃油和液压系统。功率密度、运行效率、集成度和可靠性是关键的性能要求，其中包含复杂的相互耦合和相互冲突的要求，需要仔细考虑。此外，航空应用的特定外部环境和负载特性将不可避免地对电机和电力电子系统的设计和控制提出挑战。本期特刊旨在收集多电动飞机 (MEA) 中电机、电源转换器、驱动器和系统的设计和控制方面的先进理论和技术研究成果。强烈鼓励既有理论解释又有实践验证的手稿。感兴趣的话题包括（但不限于）：