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首页|期刊导航|空间科学学报|临近空间大气风场星载Fabry-Perot干涉仪设计及仿真结果分析

临近空间大气风场星载Fabry-Perot干涉仪设计及仿真结果分析

孙翼然 王后茂 李鹏达 刘玖 王咏梅 付利平 黄聪 宗位国

空间科学学报2026,Vol.46Issue(2):371-379,9.
空间科学学报2026,Vol.46Issue(2):371-379,9.DOI:10.11728/cjss2026.02.2025-0041

临近空间大气风场星载Fabry-Perot干涉仪设计及仿真结果分析

Design and Simulation Results Analysis of a Spaceborne Fabry-Perot Interferometer for the Near-space Atmospheric Wind Field

孙翼然 1王后茂 2李鹏达 2刘玖 2王咏梅 2付利平 2黄聪 3宗位国3

作者信息

  • 1. 中国科学院国家空间科学中心 北京 100190||中国科学院大学 北京 100049
  • 2. 中国科学院国家空间科学中心 北京 100190
  • 3. 国家卫星气象中心 北京 100081||许健民气象卫星创新中心 北京 100081||中国气象局空间天气重点实验室 北京 100081
  • 折叠

摘要

Abstract

Currently,there are relatively few spaceborne methods for detecting near-space atmospher-ic wind fields,and the Fabry-Perot Interferometer(FPI)is one of the more important and widely used detection techniques.To address the gap in China's space-based FPI wind sensing capabilities,the Na-tional Space Science Center developed a spaceborne FPI wind interferometer.This paper mainly intro-duces this instrument's optical design,structural design,thermal control design,optical simulation,and result analysis.First,the optical design is discussed based on the wideband detection requirements,and the imaging system's image quality is evaluated.Then,based on optical simulation data,wind speed in-version and accuracy analysis of the spaceborne FPI instrument are conducted.The wind speed errors at the 557.7 nm and 762.0 nm bands are-1.722 m·s-1 and-2.3672 m·s-1,respectively,indicating that the spaceborne instrument design meets the wind measurement requirements.Then,the key points of the in-strument's structural design and the thermal control solution for the imaging part are presented,along with a translational filter switching device driven by a trapezoidal lead screw and a micro gear stepping motor or micro linear motor.The paper also explores the relationship between the temperature control accuracy of the instrument's core components(the etalon)and wind measurement errors.A combined active and passive design is adopted to minimize the impact of temperature fluctuations on the results,which is verified with simulation results.

关键词

Fabry-Perot干涉仪(FPI)/临近空间/风速反演/星载仪器

Key words

Fabry-Perot Interferometer(FPI)/Near space/Wind velocity retrieval/Spaceborne instrument

分类

天文与地球科学

引用本文复制引用

孙翼然,王后茂,李鹏达,刘玖,王咏梅,付利平,黄聪,宗位国..临近空间大气风场星载Fabry-Perot干涉仪设计及仿真结果分析[J].空间科学学报,2026,46(2):371-379,9.

基金项目

国家重点研发计划项目资助(2022YFB3901800,2022YFB3901802) (2022YFB3901800,2022YFB3901802)

空间科学学报

0254-6124

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