Spaceborne hyperspectral imaging with a static Fourier transform spectrometer
Spaceborne hyperspectral imaging with a static Fourier transform spectrometer
复制标题
使用静态傅里叶变换光谱仪进行星载高光谱成像
DOI:
10.1117/2.1201301.004601
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发表时间:
2013
期刊:
影响因子:
--
通讯作者:
J. Primot
中科院分区:
文献类型:
--
作者:
Y. Ferrec;J. Primot
Hyperspectral imaging views objects by surveying a vast portion of the electromagnetic spectrum, collecting and interpreting dozens to hundreds of discrete frequency bands at a time. Many substances leave distinctive spectral signatures that hyperspectral imaging can detect. For example, geologists can use hyperspectral imaging to find oil and some minerals. Spaceborne hyperspectral imaging has great promise for scientific and military applications, such as environmental monitoring, study of coastal ecosystems, and mapping of urban materials. However, a spatial resolution lower than 10m is needed in most cases.1 Such a resolution is not reached by current spaceborne hyperspectral imagers for civilian Earth observation (see Figure 1). Yet spaceborne panchromatic imagers, which reproduce a scene as it would appear to the human eye, have a resolution better than 1m. This gap is due to the difficulty of reaching high signal-to-noise ratios in hyperspectral imaging. Techniques to refine spectral resolution decrease the number of photons per spectral band. Furthermore, in order to collect the great amount of information provided by both the spectral and the spatial information, the time available to measure each element of a hyperspectral image is reduced compared to a panchromatic image. Time delay and integration technology is impossible, and large focal plane arrays (FPAs) (large in terms of pixels) are needed.2 For these FPAs, the readout time is not negligible, and may even be longer than the integration time, all the more since the finer the spatial resolution, the higher the FPA frame rate. Thus, strategies for increasing the number of photons collected are essential. Three main solutions can be used. The first is to increase the pupil diameter. However, this solution is not adapted to small satellites. A second solution is to use a bus with a forward Figure 1. Current and planned hyperspectral civilian spaceborne hyperspectral imagers. VISNIR: Visible and near-IR. SWIR: Short-wave IR. TIR: Thermal IR.