Dynamic Model of Soft Ferrites for Avionic Applications

H. Rimal
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引用次数: 2

Abstract

A simplified dynamic model to represent the behaviour of soft ferrites at higher frequency is necessary in many applications including avionics. We have tried to address this issue by using a circuital model. The model represents frequency dependence of hysteresis in ferrite material using the parallel combination of static hysteresis model and passive electrical elements. The static hysteresis model such as preisach model represents the magnetic core behaviour, whereas the passive electrical elements represent the broadening of hysteresis loops with the increase in frequency. The parameters of the model are identified using pattern search algorithm, and the model is tested for the frequency upto one Megahertz. Comparison between the results obtained from simulation and measurements for N30 Manganese Zinc ferrite using sinusoidal excitation are presented in the paper. The model is applicable to predict the performance of ferrite core inductors that are used to mitigate the lightning indirect effects in avionic equipments.
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航空电子用软铁氧体动力学模型
在包括航空电子在内的许多应用中,需要一个简化的动态模型来表示软铁氧体在高频下的行为。我们试图通过使用电路模型来解决这个问题。该模型采用静态磁滞模型与无源电元件并行结合的方法,描述了铁氧体材料磁滞的频率依赖性。静态迟滞模型(如预激模型)代表磁芯行为,而无源电元件则代表迟滞环随频率增加而展宽。利用模式搜索算法对模型的参数进行了识别,并对该模型进行了高达1兆赫的频率测试。本文对N30锰锌铁氧体用正弦激励的仿真结果与实测结果进行了比较。该模型可用于预测航空电子设备中用于减轻雷电间接影响的铁氧体铁芯电感的性能。
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