微卫星任务微辐射热计仪器载荷设计

W. F. Payne, J. Gore, T. Pope, L. Phong, Wanping Zheng
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引用次数: 3

摘要

本文介绍了任务和仪器的设计。它比较了微型卫星、地面和空中平台的使用。基于微辐射热计技术的对地观测微卫星任务。探测器是线性阵列,滤波后在5个波段敏感:3个波段在8.5和12.5微米之间,2个波段在3.0和4.5微米之间。预计这颗地球观测卫星将产生有用的数据,如冰架形成/融化、云监测、石油泄漏、森林火灾跟踪和损害评估、京都协议遵守情况监测、城市热华、海洋、陆地和冰的温度,重点是北部沿海水域、北极和亚北极陆地地区。因此,基于卫星的传感器比地面或机载传感器有更多的优势。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Microbolometer instrument payload design for a microsatellite mission
This paper describes the design of the mission and the instrument. It compares the use of microsatellites, ground and air based platforms. An Earth observation microsatellite mission is based on microbolometer technology. The detectors are linear arrays, filtered to be sensitive in five bands: 3 bands between 8.5 and 12.5 microns, and 2 bands between 3.0 and 4.5 microns. It is expected that this Earth observation satellite will produce useful dates like ice-shelf formation/melt, cloud monitoring, oil spills, forest fire tracking and damage assessment, Kyoto Accord compliance monitoring, city heat bloom, temperatures of oceans, land, and ice with the focus on northern coastal waters, Arctic and sub-Arctic land areas. Hence, satellite-based sensors have more advantages over terrestrial or airborne sensors.
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