一种新型大气温度测深装置:系统设计与性能分析

P. Chakraborty, Priyanka Gupta, D. B. Dave, N. Desai, T. Misra
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引用次数: 0

摘要

本文报道了印度空间研究组织(ISRO)研制的毫米波星载大气温度探测装置(TSU)。这是ISRO向毫米波技术迈出的第一步。该传感器有几个新的成就,其中包括探测通道选择的理念,新的温度探测通道分类,同时观测所有通道的两个极化,紧凑的双频扫描格里高利反射天线,自主开发的黑体目标在轨校准,自主开发的毫米波射频前端和预探测自动增益控制方法。该仪器的主要特点是其独特的通道,可以从地表到40公里高度的地球大气剖面,垂直分辨率从近地表不到1公里到30公里高度的±2.5公里。通道主要是50-60 GHz O2吸收光谱中的非谐振频率,提供接近均匀的衰减,因此有更多的通道带宽和更好的温度灵敏度,但它们的加权函数有足够的重叠,以实现所需的垂直分辨率。这些频道与全球所有早期探空任务(如AMSU-A, SSMIS, ATMS等)中飞行的频道不同,频带较少。TSU辐射计已被表征彻底使用巧妙的方法,如低功率有源射频激励与频率扫描。这是一种紧凑、低质量、低功率的仪器,已经配置用于ISRO迷你卫星(IMS-2)总线。硬件性能得到改善的飞行模型正在构建中,并正在探索合适的飞行机会。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A novel atmospheric Temperature Sounding Unit: system design and performance analyses
This paper reports the development of a millimeter-wave space-borne atmospheric Temperature Sounding Unit (TSU) in Indian Space Research Organization (ISRO). This is ISRO’s first leap towards millimeter-wave technology. The sensor has several new accomplishments to its credit which include among others, the philosophy of sounding channel selection, the new assortment of temperature sounding channels, simultaneous observation of both polarizations of all channels, compact dual-band scanning Gregorian reflector antenna, indigenously developed black-body target for in-orbit calibration, in-house developed millimeter-wave RF front-end and pre-detection automatic gain control method. The prime feature of this instrument is its unique set of channels which can profile the earth’s atmosphere from surface to 40 km altitude with vertical resolution ranging from less than a km near surface to ±2.5 km at 30km altitude. The channels are predominantly off-resonant frequencies in the 50―60 GHz O2 absorption spectrum which offer near-uniform attenuation and hence more channel-bandwidth and better temperature sensitivity and yet have adequate overlap of their weighting functions to achieve the desired vertical resolution. These channels are different and have fewer bands from what has been flown in all earlier sounding missions worldwide e.g. AMSU-A, SSMIS, ATMS etc. The TSU radiometer has been characterized thoroughly using ingenious methods such as low-power active RF energizing along with frequency sweep. This is a compact, low-mass, low-power instrument and has been configured for the ISRO mini-satellite (IMS-2) bus. The flight model with improved hardware performance is being built and a suitable opportunity of flying it is being explored.
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