1. Design and preflight performance of ASTER instrument protoflight model
- Author
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Fujisada, H., Sakuma, F., Ono, A., and Kudoh, M.
- Subjects
United States. Goddard Space Flight Center. Earth Observing System -- Buildings and facilities ,Artificial satellites in remote sensing -- Equipment and supplies ,Radiometers -- Design and construction ,Flight -- Models ,Multispectral photography -- Equipment and supplies ,Business ,Earth sciences ,Electronics and electrical industries - Abstract
The Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER) is an advanced multispectral imager with high spatial, spectral, and radiometric resolution, built to fly on the EOS-AM1 spacecraft along with four other instruments, which will be launched in 1998. The ASTER instrument covers a wide spectral region, from visible to thermal infrared with 14 spectral bands. To meet the wide spectral coverage, optical sensing units of ASTER are separated into three subsystems: visible and near-infrared (VNIR) subsystem, shortwave infrared (SWIR) subsystem, and thermal infrared (TIR) subsystem. ASTER also has an along-track stereoscopic viewing capability using one of the near-infrared bands. To acquire the stereo data, the VNIR subsystem has two telescopes, one for nadir and another for backward viewing. Several new technologies are adopted as design challenges to realize high performance. Excellent observational performances are obtained by a pushbroom VNIR radiometer with a high spatial resolution of 15 m, a pushbroom SWIR radiometer with high spectral resolution, and a whiskbroom-type TIR radiometer with high spatial, spectral, and radiometric resolutions. The preflight performance is evaluated through a protoflight model (PFM). Index Terms - High resolution, multispectral imagers.
- Published
- 1998