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Design and Simulation Results Analysis of a Spaceborne Fabry-Perot Interferometer for the Near-space Atmospheric Wind Field
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Yiran SUN1, 2, Houmao WANG1, Pengda LI1, Jiu LIU1, Yongmei WANG1, Liping FU1, Cong HUANG3, 4, 5, Weiguo ZONG3, 4, 5
Chinese Journal of Space Science | 2026, 46(2) : 371 - 379
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Chinese Journal of Space Science | 2026, 46(2): 371-379
Research Article
Design and Simulation Results Analysis of a Spaceborne Fabry-Perot Interferometer for the Near-space Atmospheric Wind Field
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Yiran SUN1, 2, Houmao WANG1, Pengda LI1, Jiu LIU1, Yongmei WANG1, Liping FU1, Cong HUANG3, 4, 5, Weiguo ZONG3, 4, 5
Affiliations
  • 1National Space Science Center, Chinese Academy of Sciences, Beijing 100190
  • 2University of Chinese Academy of Sciences, Beijing 100049
  • 3National Satellite Meteorological Center, Beijing 100081
  • 4Xu Jianmin Meteorological Satellite Innovation Center, Beijing 100081
  • 5Key Laboratory of Space Weather, China Meteorological Administration, Beijing 100081
Published: 2026-03-15 doi: 10.11728/cjss2026.02.2025-0041
Outline
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Currently, there are relatively few spaceborne methods for detecting near-space atmospheric 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 National Space Science Center developed a spaceborne FPI wind interferometer. This paper mainly introduces 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 inversion 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 instrument’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.

Fabry-Perot Interferometer (FPI)  /  Near space  /  Wind velocity retrieval  /  Spaceborne instrument
Yiran SUN, Houmao WANG, Pengda LI, Jiu LIU, Yongmei WANG, Liping FU, Cong HUANG, Weiguo ZONG. Design and Simulation Results Analysis of a Spaceborne Fabry-Perot Interferometer for the Near-space Atmospheric Wind Field[J]. Chinese Journal of Space Science, 2026 , 46 (2) : 371 -379 . DOI: 10.11728/cjss2026.02.2025-0041
Year 2026 volume 46 Issue 2
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Article Info
doi: 10.11728/cjss2026.02.2025-0041
  • Receive Date:2025-03-18
  • Online Date:2026-07-08
  • Published:2026-03-15
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History
  • Received:2025-03-18
  • Revised:2025-04-14
Affiliations
    1National Space Science Center, Chinese Academy of Sciences, Beijing 100190
    2University of Chinese Academy of Sciences, Beijing 100049
    3National Satellite Meteorological Center, Beijing 100081
    4Xu Jianmin Meteorological Satellite Innovation Center, Beijing 100081
    5Key Laboratory of Space Weather, China Meteorological Administration, Beijing 100081
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小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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