Investigation of a fault tolerant and high performance motor drive for critical applications

N. Ertugrul, W. Soong, S. Valtenbergs, H. Chye
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引用次数: 25

Abstract

This paper evaluates a fault-tolerant electric motor drive with redundancy for a potential all-electric aircraft (AEA), and investigates to increase the redundancy against partial or complete motor failures. A flexible motor configuration is proposed to increase the redundancy against motor failures. The paper highlights the importance of effectively simulating the system on computer, and the way in which the ideas and techniques used to simulate the system have been adapted to the physical prototype. The computer modelling section of the paper outlines the steps involved with simulating the complete system using an object orientated programming language, LabVIEW, and some simulation results are provided.
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一种用于关键应用的容错和高性能电机驱动器的研究
本文对潜在全电动飞机的容错冗余电动机驱动进行了评估,并研究了在电动机部分或全部故障时增加冗余的方法。提出了一种灵活的电机配置,以增加电机故障时的冗余。本文强调了在计算机上有效地模拟该系统的重要性,以及如何使用于模拟系统的思想和技术适应于物理原型。论文的计算机建模部分概述了使用面向对象编程语言LabVIEW模拟整个系统所涉及的步骤,并提供了一些仿真结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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