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首页> 外文期刊>Space Science Reviews >Far ultraviolet imaging from the IMAGE spacecraft. 2. Wideband FUV imaging [Review]
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Far ultraviolet imaging from the IMAGE spacecraft. 2. Wideband FUV imaging [Review]

机译:来自IMAGE航天器的远紫外成像。 2.宽带FUV成像[评论]

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The Far Ultraviolet Wideband Imaging Camera (WIC) complements the magnetospheric images taken by the IMAGE satellite instruments with simultaneous global maps of the terrestrial aurora. Thus, a primary requirement of WIC is to image the total intensity of the aurora in wavelength regions most representative of the auroral source and least contaminated by dayglow, have sufficient field of view to cover the entire polar region from spacecraft apogee and have resolution that is sufficient to resolve auroras on a scale of 1 to 2 latitude degrees. The instrument is sensitive in the spectral region from 140-190 nm. The WIC is mounted on the rotating IMAGE spacecraft viewing radially outward and has a field of view of 17 degrees in the direction parallel to the spacecraft spin axis. Its field of view is 30 degrees in the direction perpendicular to the spin axis, although only a 17 degrees x17 degrees image of the Earth is recorded. The optics was an all-reflective, inverted Cassegrain Burch camera using concentric optics with a small convex primary and a large concave secondary mirror. The mirrors were coated by a special multi-layer coating, which has low reflectivity in the visible and near UV region. The detector consists of a MCP-intensified CCD. The MCP is curved to accommodate the focal surface of the concentric optics. The phosphor of the image intensifier is deposited on a concave fiberoptic window, which is then coupled to the CCD with a fiberoptic taper. The camera head operates in a fast frame transfer mode with the CCD being read approximately 30 full frames (512x256 pixel) per second with an exposure time of 0.033 s. The image motion due to the satellite spin is minimal during such a short exposure. Each image is electronically distortion corrected using the look up table scheme. An offset is added to each memory address that is proportional to the image shift due to satellite rotation, and the charge signal is digitally summed in memory. On orbit, approximately 300 frames will be added to produce one WIC image in memory. The advantage of the electronic motion compensation and distortion correction is that it is extremely flexible, permitting several kinds of corrections including motions parallel and perpendicular to the predicted axis of rotation. The instrument was calibrated by applying ultraviolet light through a vacuum monochromator and measuring the absolute responsivity of the instrument. To obtain the data for the distortion look up table, the camera was turned through various angles and the input angles corresponding to a pixel matrix were recorded. It was found that the spectral response peaked at 150 nm and fell off in either direction. The equivalent aperture of the camera, including mirror reflectivities and effective photocathode quantum efficiency, is about 0.04 cm(2). Thus, a 100 Rayleigh aurora is expected to produce 23 equivalent counts per pixel per 10 s exposure at the peak of instrument response. [References: 6]
机译:远紫外线宽带成像相机(WIC)通过IMAGE卫星仪器拍摄的磁层图像与地球极光的同时全球地图相辅相成。因此,WIC的主要要求是在最能代表极光源且受日光污染最少的波长区域中成像极光的总强度,并具有足够的视场以覆盖航天器顶点的整个极区,且分辨率为足以解析1至2纬度的极光。该仪器在140-190 nm的光谱范围内敏感。 WIC安装在旋转的IMAGE航天器上,径向向外观察,并在与航天器旋转轴平行的方向上具有17度的视野。尽管仅记录了17度x17度的地球图像,但其视场在垂直于自旋轴的方向上为30度。光学元件是全反射,倒置的Cassegrain Burch相机,使用同心光学元件,具有小的凸面主镜和大凹面副镜。镜面涂有特殊的多层涂层,该涂层在可见光和近紫外线区域具有低反射率。检测器由MCP增强的CCD组成。 MCP弯曲以容纳同心光学器件的焦面。图像增强器的荧光粉沉积在凹形的光纤窗口上,然后通过光纤锥度将其耦合到CCD。摄像头以快速帧传输模式运行,CCD每秒以大约0.033 s的曝光时间每秒读取约30个全帧(512x256像素)。在如此短的曝光期间,由于卫星自旋而引起的图像运动极小。使用查找表方案对每个图像进行电子失真校正。将偏移量添加到每个存储地址,该偏移量与由于卫星旋转而引起的图像偏移成比例,并且电荷信号被数字求和到内存中。在轨道上,将添加大约300帧以在内存中生成一张WIC图像。电子运动补偿和失真校正的优势在于它非常灵活,可以进行多种校正,包括与预测的旋转轴平行和垂直的运动。通过通过真空单色仪施加紫外光并测量仪器的绝对响应度来校准仪器。为了获得用于畸变查找表的数据,将照相机旋转各种角度,并记录与像素矩阵相对应的输入角度。发现光谱响应在150nm处达到峰值并在任一方向上下降。相机的等效孔径,包括镜面反射率和有效的光电阴极量子效率,约为0.04 cm(2)。因此,在仪器响应的峰值处,每100 s曝光,每100像素瑞利极光将产生23个等效计数。 [参考:6]

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