星载微波辐射计定标源辐射亮温计量校准技术方案研究
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作者单位:

1.兰州空间技术物理研究所,甘肃 兰州 730000;2.北京化工大学, 北京 100029;3.国家卫星气象中心,北京 100081;4.上海卫星工程研究所 上海 201109;5.中国空间技术研究院西安分院 陕西 西安710000;6.北京无线电计量测试研究所 北京 100854;7.上海航天测控通信研究所 上海 201109

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基金项目:

甘肃省科技重大专项计划项目(22ZD6GA011)、国家自然科学基金面上项目(62371031)


Research on the metrological calibration technology scheme of brightness temperature for the space-borne microwave radiometer calibration target
Author:
Affiliation:

1.Lanzhou Institute of Physics, Lanzhou 730000, China;2.Beijing University of Chemical Technology, Beijing 100029, China;3.National Satellite Meteorological Center, Beijing 100081,China;4.Shanghai Institute of Satellite Engineering, Shanghai 201100,China;5.China Academy of Space Technology Xi’an, Xi’an;6.710071,China;7.Beijing Institute of Radio Metrology and Measurement, Beijing 100854,China

Fund Project:

Sponsored by the Major Science and Technology Special Project of Gansu Province (22ZD6GA011), and the National Natural Science Foundation of China (62371031).

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    摘要:

    针对星载微波辐射计热定标源的亮温校准应用需求,基于定标源吸波涂层温梯特性和亮温偏差产生机理,结合工程可实施的温度测量方法和实验手段,研究可在轨应用的亮温计量校准技术方案。基于当前定标源高发射率设计和测定技术基本完善的背景,重点研究归纳了定标源涂层温梯特性的测定方法,目标构建在轨可用的,以定标源金属内锥温度测值、定标源辐射口面附近温度测值等多参量输入的亮温校准技术。基于可行的电磁仿真技术、热仿真技术、铂电阻和红外温度测量技术,初步归纳了星载定标源亮温校准技术体系的实现路径,即首先构建考虑均匀背景亮温的亮温校准基本模型,完善从定标源内锥和等效背景亮温到涂层纵向温梯的映射关系;进而构建考虑安装环境的亮温校准应用模型,完善从定标源内锥和辐射口面附近温度测值到定标源亮温偏差的映射关系;最后讨论亮温校准模型的验证和应用。围绕星载定标源亮温校准的研究工作,是进一步提高定标源亮温准确度,乃至发展空间微波辐射测量基准的重要技术基础和参考。

    Abstract:

    Aiming at the application requirements of brightness temperature calibration of the hot calibration target of spaceborne microwave radiometer, and based on the temperature gradient characteristics of the absorbing coating of the calibration target and the mechanism of brightness temperature deviation, combined with practical temperature measurement and experimental methodology, a brightness temperature metrological calibration technology solution applicable for in-orbit use is studied. Given the current background of high emissivity design and determination technology of the calibration target being basically perfected, this work focuses on summarizing the methods for determining the temperature gradient characteristics of the calibration target coating. The goal is to construct an in-orbit available brightness temperature calibration method that uses multiple parameters, such as the measurable temperature values of the metal inner core of the calibration target and that near the radiation aperture of the calibration target. Based on feasible electromagnetic simulation technology, thermal simulation technology, platinum resistance and infrared temperature measurement techniques, the paper preliminarily summarizes the implementation path of the brightness temperature calibration technology system for space-borne calibration targets. This involves first constructing a basic brightness temperature calibration model considering uniform background brightness temperature and improving the mapping relationship from the inner core temperature of the calibration target and the equivalent background brightness temperature to the longitudinal temperature gradient of the coating. Subsequently, an application model for brightness temperature calibration considering the installation environment is constructed, improving the mapping relationship from the temperature measurements of the inner core and that of the radiation aperture area of calibration target to the overall brightness temperature deviation. Finally, the validation and application of the brightness temperature calibration model are discussed. The research on brightness temperature calibration of space-borne calibration source is an important technical basis and reference for further improving the accuracy of brightness temperature of calibration target and even developing space microwave radiation measurement standards.

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  • 收稿日期:2024-12-20
  • 最后修改日期:2025-12-01
  • 录用日期:2025-02-09
  • 在线发布日期: 2025-11-28
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