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MODELING AND ANALYSIS FOR SPACECRAFT DATABASE OF ELECTROMAGNETIC COMPATIBILITY

机译:用于电磁兼容性的航天器数据库的建模与分析

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This paper focuses on system level EMC database modeling of spacecraft. Since there are many electromagnetic interference sources for the sensitive electron devices on the spacecraft, kinds of different EMI sources will be discussed at the beginning. The EMI radiated sources such as strong electromagnetic pulse, various payloads radiated emissions and high-power AC/DC conducted emissions etc will be analyzed in details. After that, as for sensitive devices easily to be interfered by others.types of EMI sources, the EMI estimation formulae will be deduced. Following that, according to deduced EMI estimation formula, the EMI prediction models for sensitive devices will be given out. Because of several of sensitive devices on the spacecraft, different database estimation model should be made according to the allowed EMI safeguard levels. Based on which has been discussed spacecraft database of EMC, the subsystem (equipment) level devices EMC prediction can be simulation under this model. This design methodology can be used in spaceflight project of the various payloads to ensure compliance with the stringent EMI requirements.
机译:本文重点介绍了航天器的系统级EMC数据库建模。由于航天器上的敏感电子器件存在许多电磁干扰源,因此将在开始时讨论各种不同的EMI源。将详细分析EMI辐射源,如强电磁脉冲,各种有效载荷辐射发射和高功率AC / DC进行的排放等。之后,对于容易被他人干扰的敏感装置。EMI源的型号,将推导出EMI估计公式。在此之后,根据推出的EMI估计公式,将发出用于敏感设备的EMI预测模型。由于航天器上的几种敏感设备,应根据允许的EMI保护级别进行不同的数据库估计模型。基于其中已经讨论了EMC的航天器数据库,子系统(设备)级别设备EMC预测可以在此模型下进行仿真。该设计方法可用于各种有效载荷的太空飞行项目,以确保符合严格的EMI要求。

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