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Optical temperature compensation schemes of spectral modulation sensors for aircraft engine control

机译:飞机发动机控制光谱调制传感器光学温度补偿方案

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temperature compensation schemes for the ratiometric interrogation of spectral modulation sensors for source temperature robustness are presented. We have obtained better than 50 - 100$MUL decrease of the temperature coefficient of the sensitivity using these types of compensation. We have also developed a spectrographic interrogation scheme that provides increased source temperature robustness; this affords a significantly improved accuracy over FADEC temperature ranges as well as temperature coefficient of the sensitivity that is substantially and further reduced. This latter compensation scheme can be integrated in a small E/O package including the detection, analog and digital signal processing. We find that these interrogation schemes can be used within a detector spatially multiplexed architecture.
机译:提出了用于源温度鲁棒性的光谱调制传感器的比例询问的温度补偿方案。使用这些类型的补偿,我们获得了优于50-100 $ MUL的温度系数的降低。我们还开发了一种光谱询问方案,可提供增加的源温度鲁棒性;这提供了对FADEC温度范围的显着提高的精度以及基本上进一步减少的灵敏度的温度系数。后一种补偿方案可以集成在包括检测,模拟和数字信号处理的小型E /​​ O包中。我们发现这些询问方案可以在探测器空间多路复用架构中使用。

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