Novel power system architecture and control for 'More Electric Aircraft'

该项目旨在提出一种新的飞机内部电气系统及其控制的概念设计，最大限度地减少传统电力系统的问题，并利用现代控制和技术进步来减少重量/体积和最大限度地提高可靠性。该项目将针对特定的设计，其中包括考虑新颖的电力电子拓扑结构，以实现这些目标。结果将通过仿真、实验和现场测试进行验证。预计该项目中开发的想法将对电动飞机技术以及一般互联能源系统（如直流和交流微电网）产生重大影响。

This project aims to propose a new conceptual design of an internal aircraft electrical system and its control, which minimises the issues of traditional power systems and takes advantage of contemporary control and technology advances to minimise weight/volume and maximise reliability. The project will target a specific design, which includes consideration of novel power electronic topologies, to achieve these goals. The results will be validated through simulation, experiments and field testing. It is anticipated that the ideas developed within this project will have a major impact on More Electric Aircraft technology, as well as on general interconnected energy resource systems, such as DC and AC microgrids.