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Asymmetry in the noise equivalent angle performance of the JWST fine guidance sensor

机译:JWST精细引导传感器的噪声等效角度性能的不对称性

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The James Webb Space Telescope Fine Guidance Sensor makes use of three 2048×2048 five micron cutoff H2RG HgCdTe detectors from Teledyne Imaging Systems. The FGS consists of two Guider channels and a Near-InfraRed Imager and Slitless Spectrograph (NIRISS) channel. We report here on detailed tests results from the Guider channels originating in both instrument level performance testing and from recent Guider performance testing with the FGS integrated into JWST's Integrated Science Instrument Module (ISIM). A key performance parameter is the noise equivalent angle (NEA) or centroiding precision. The JWST requirement flowed down to the Guiders is a NEA of 4 milli-arcseonds, equivalent to approximately 1/20th of a detector pixel. This performance has been achieved in the testing to date. We have noted a systematic asymmetry in the NEA depending on whether the NEA in the row or column direction is considered. This asymmetry depends on guide star brightness and reaches its maximum, where the row NEA is 15% to 20% larger than the column NEA, at the dim end of the Guide star brightness range. We evaluate the detector level characteristics of spatially correlated noise and asymmetric inter-pixel capacitance (IPC) as potential sources of this NEA asymmetry. Modelling is used to estimate the impact on NEA of these potential contributors. These model results are then compared to the Guider test results obtained to date in an effort to isolate the cause of this effect. While asymmetric IPC can induce asymmetric NEA, the required magnitude of IPC is far greater than observed in these detectors. Thus, spatially correlated noise was found to be the most likely cause of the asymmetric NEA.
机译:James Webb Space望远镜精细引导传感器利用来自Teledyne成像系统的三个2048×2048五微米截止H2RG HGCDTE探测器。 FGS由两个导管频道和近红外成像器和无缝光谱仪(NIRISS)通道组成。我们在此报告详细的测试来自源仪表级性能测试的导管通道,以及最近的导线性能测试,使用集成到JWST集成的科学仪器模块(ISIM)中的FGS。关键性能参数是噪声等效角度(NEA)或绝中心精度。流向指导者的JWST要求是4毫安的NEA,相当于探测器像素的大约1/20。该表现在测试到日期之前已经实现。我们已经注意到NEA中的系统不对称,这取决于是否考虑了行或列方向的NEA。该不对称性取决于导恒星亮度并达到其最大值,在导灯亮度范围的暗端处,行nea的最大值为大于柱NEA的15%至20%。我们评估空间相关噪声和不对称间电容(IPC)的检测器电平特征作为该NEA不对称的潜在来源。建模用于估算这些潜在贡献者对NEA的影响。然后将这些模型结果与迄今为止获得的指导试验结果进行比较,以隔离这种效果的原因。虽然不对称IPC可以诱导不对称NEA,但IPC的所需幅度远远大于在这些探测器中观察到的。因此,发现空间相关的噪声是不对称NEA的最可能原因。

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