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Characterization of multiband imager aboard SELENE: Pre-flight and in-flight radiometric calibration

机译:SELENE上多波段成像仪的特性:飞行前和飞行中辐射度校准

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The Multiband Imager (MI) is a high-resolution, multi-spectral imaging instrument for lunar exploration. It consists of two cameras, VIS and NIR, and is carried on the SELenological and ENgineering Explorer (SELENE), launched on Sep. 14, 2007. During the observation from January 2008 to June 2009, MI acquired about 450,000 scenes of multispectral image. The radiometric properties of the cameras were characterized using the pre-flight data derived in laboratory experiments with a calibrated integrating sphere. Twelve light source sets were used to examine the S/N ratio, linearity, and saturation level of the cameras. The dark field signal is quite stable in both cameras, having a noise level of less than 1 DN (VIS) and 2 DN (NIR). The fluctuation in the light field is also low (2 DN), indicating that the spatial nonuniformity in the camera responses can be removed using a flat field. In order to remove the smear signals due to the frame transfer in the VIS data, we developed an iterate algorithm using all bands in the VIS camera. The S/N ratio, which is critical to the precision of the product, is estimated to exceed 160 for the VIS bands and 400 for the NIR bands under low illumination conditions (5% of lunar surface reflectance). Based on the S/N ratio, the radiometric error due to the noise is calculated to be less than 0.7% for VIS and 0.2% for NIR. The relationship between input and output of the VIS camera is linear with a residual of less than 0.6 DN, corresponding to a radiometric error of 0.3%. The NIR exhibits a non-linear response to the input radiance. A cubic function best fits the pre-flight data with an average residual of 8 DN (corresponds to an error of 0.8%). Validation using in-flight data indicated that the instability of the dark output has not changed, but the level of dark output has slightly changed in the NIR bands (less than 6 DN). The pixel-to-pixel sensitivity variation in the orbit has been changed from that in the pre-flight experiment. The difference between the in-flight data and the pre-flight data ranges within ±2%. There is also a small (less than ±1%) but nonnegligible difference between in-flight data of different cycles in both the VIS and NIR bands, suggesting that the coefficient for spatial ununiformity correction needs to be calculated for each cycle.
机译:多波段成像仪(MI)是用于月球探索的高分辨率,多光谱成像仪。它由VIS和NIR两台摄像机组成,并搭载于2007年9月14日发射的SELenological and Engineering Explorer(SELENE)上。在2008年1月至2009年6月的观测期间,MI采集了约45万个多光谱图像。使用在实验室实验中使用校准的积分球得到的飞行前数据来表征摄像机的辐射特性。使用十二个光源组来检查摄像机的信噪比,线性和饱和度。在两个摄像机中,暗场信号都非常稳定,其噪声水平小于1 DN(VIS)和2 DN(NIR)。光场中的波动也很小(<2 DN),这表明可以使用平坦场消除相机响应中的空间不均匀性。为了消除由于VIS数据中的帧传输而产生的拖尾信号,我们开发了一种使用VIS摄像机中所有波段的迭代算法。对于产品的精度至关重要的信噪比,在低照明条件(月球表面反射率的5%)下,VIS波段的信噪比估计超过160,NIR波段的信噪比超过400。根据信噪比,计算出由于噪声引起的辐射误差对于VIS小于0.7%,对于NIR小于0.2%。 VIS摄像机的输入和输出之间的关系是线性的,其残差小于0.6 DN,对应于0.3%的辐射误差。 NIR对输入辐射表现出非线性响应。三次函数最适合飞行前数据,平均残差为8 DN(对应于0.8%的误差)。使用飞行中数据进行的验证表明,暗输出的不稳定性没有改变,但是在NIR波段(小于6 DN)中暗输出的水平已经略有变化。轨道上像素间的灵敏度变化与飞行前实验相比有所变化。飞行中数据与飞行前数据之间的差异在±2%范围内。在VIS和NIR波段中,不同周期的飞行数据之间也存在很小的差异(小于±1%),但不可忽略,这表明需要为每个周期计算空间不均匀性校正系数。

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