Main design parameters and imaging/radiometric performances of the METOP Second Generation conically scanning radiometers

S. Varchetta, S. Pompili, B. Buralli, G. Alberti, G. Pica, M. Santovito, S. D'addio, V. Kangas
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引用次数: 2

Abstract

In the context of MetOp Second Generation (MetOp-SG) phase A/B1 study, Thales Alenia Space is responsible of Microwave Imager (MWI) and Ice Cloud Imager (ICI) instruments. MWI and ICI are conically scanning microwave radiometers, together covering frequency range from 18.7 GHz up to 664 GHz. The on-going study covers all elements of the space segment and instrument architecture and deals with the analysis of the space system requirements and the definition of candidate implementation concepts in order to satisfy the user's needs and requirements. MWI and ICI will fly on a spacecraft in a near circular sun-synchronous, near polar orbit. In order to acquire measurements on a wide swath the instrument will rotates continuously about an axis parallel to the local spacecraft vertical with an active portion of the scan of ~±65 deg centred on the foreword direction of the spacecraft. The Earth scene view is a nearly constant incidence angle of about 53 deg. Challenging Imaging and radiometric requirements are applicable to MWI and ICI instruments and a trade-off has been performed in order to identify and size main system parameters. In the paper a description of the trade-off that was performed will be presented and the results achieved will be described.
METOP第二代锥形扫描辐射计的主要设计参数和成像/辐射性能
在MetOp第二代(MetOp- sg) A/B1期研究的背景下,泰雷兹阿莱尼亚宇航公司负责微波成像仪(MWI)和冰云成像仪(ICI)仪器。MWI和ICI是锥形扫描微波辐射计,频率范围从18.7 GHz到664 GHz。正在进行的研究包括空间部分和仪器结构的所有要素,并分析空间系统要求和确定备选执行概念,以便满足用户的需要和要求。MWI和ICI将在接近圆形太阳同步、近极轨道的航天器上飞行。为了获得宽波段上的测量,仪器将围绕与本地航天器垂直平行的轴连续旋转,扫描的主动部分以航天器的前导方向为中心~±65度。地球场景视图的入射角几乎是恒定的,约为53度。具有挑战性的成像和辐射测量要求适用于MWI和ICI仪器,为了确定和确定主要系统参数,必须进行权衡。在本文中,将介绍所执行的权衡的描述,并描述所取得的结果。
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