Fault Tolerant Brushless DC Motor Drive for Aerospace Applications

Pub Date : 2023-11-01 DOI:10.14429/dsj.73.18898
Harminder Singh Johar, Abhijit Bhattacharya, S. Srinivasa Rao
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Abstract

This article brings out a Fault-tolerant BLDC motor drive for aerospace applications using the redundancy concept. In a way, it brings out a fault-tolerant strategy that can be used to continue the regular operation of a BLDC motor drive even after the occurrence of faults. As BLDC motors are used in critical and dangerous control areas like military services and space vehicles, a fault-tolerant drive is essential to maintain drive operation and provide desirable output. This article compares fault simulation results in the software model of a BLDC motor drive to those of fault simulation results in hardware for three main types of faults. Fault simulation is carried out for three types of faults, viz. inverter device open circuit fault, motor winding open circuit fault, and rotor position sensor (hall sensor) open-circuited fault. Fault tolerance is ensured by introducing a redundant drive (drive-2), which operates the complete drive at the advent of any of the faults mentioned above in the main (healthy) drive-1. A fault-tolerant (redundant) hardware comprising dual stator BLDC motor and redundant controllers is realized and operationalized. Fault simulation is carried out in this hardware, and these results are validated with the results of fault simulation in the MATLAB SIMULINK model. Software and hardware results are comparable and form a basis for developing fault-tolerant electro-mechanical actuation systems for high-reliability, high-cost applications, mainly aerospace.
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航空航天应用的容错无刷直流电机驱动器
本文提出了一种采用冗余概念的航空航天应用容错无刷直流电机驱动器。在某种程度上,提出了一种容错策略,可以使无刷直流电机驱动器在发生故障后继续正常运行。由于无刷直流电机用于军事服务和航天飞行器等关键和危险的控制领域,因此容错驱动器对于保持驱动器运行并提供理想的输出至关重要。本文针对三种主要故障类型,将无刷直流电机驱动软件模型的故障仿真结果与硬件模型的故障仿真结果进行了比较。针对逆变器器件开路故障、电机绕组开路故障、转子位置传感器(霍尔传感器)开路故障三种故障进行故障仿真。通过引入冗余驱动器(驱动器-2)来确保容错性,当主(健康)驱动器1出现上述任何故障时,冗余驱动器(驱动器-2)将运行整个驱动器。实现了由双定子无刷直流电机和冗余控制器组成的容错(冗余)硬件。在该硬件上进行了故障仿真,并与MATLAB SIMULINK模型下的故障仿真结果进行了验证。软件和硬件结果具有可比性,为开发高可靠性、高成本应用(主要是航空航天)的容错机电驱动系统奠定了基础。
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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