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EMI coupling to command lines due to solar array switching strings in spacecraft

机译:由于航天器中的太阳能电池阵列开关串,EMI耦合到命令行

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The satellite as a system consists of various bundles of harness interconnections between subsystems, across the panels. These bundles of harness consist of different types of cables - power lines, data lines, command lines. Power lines from solar array also carry switching currents from the solar array switching circuits. When all these cables are bundled together, it essentially brings out the problem of unintentional electromagnetic energy coupling between the wires. This paper analyzes the amount of coupling in a typical command line placed in close proximity to the power lines carrying switching currents. It is reported that few in-orbit spacecraft on-board anomalies are attributed to spurious commanding due to cable coupling between the command lines and the switching power lines. This analysis considers the different harness configurations of the power lines where such possibilities exist.
机译:作为系统的卫星包括子系统之间的各种线束互连,穿过面板。这些捆绑的线束包括不同类型的电缆 - 电源线,数据线,命令行。来自太阳能阵列的电源线还从太阳能阵列开关电路中携带切换电流。当所有这些电缆都捆绑在一起时,它基本上带出了电线之间无意的电磁能量耦合的问题。本文分析了典型的指令线中的耦合量,其靠近承载切换电流的电力线。据报道,由于指令线和开关电力线之间的电缆耦合,甚至轨道上的轨道航天器的轨道内的异常归因于虚假的指挥。该分析考虑了这些可能性存在的电源线的不同线束配置。

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