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卫星用高频微角振动测量敏感器设计、验证与在轨应用

TENG Fei ZHANG Yufei LI Yong ZHANG Peiyong SUN Li LIN Song QIU Jinjuan WANG Qiwei

空间控制技术与应用2025,Vol.51Issue(6):97-107,11.
空间控制技术与应用2025,Vol.51Issue(6):97-107,11.DOI:10.3969/j.issn.1674-1579.2025.06.009

卫星用高频微角振动测量敏感器设计、验证与在轨应用

Design,Testing,and on-Orbit Performance of a Satellite High-Frequency Micro-Angel Vibration Sensor

TENG Fei 1ZHANG Yufei 1LI Yong 1ZHANG Peiyong 1SUN Li 1LIN Song 1QIU Jinjuan 1WANG Qiwei1

作者信息

  • 1. Beijing Institute of Control Engineering,Beijing 100094,China||Laboratory of Space Inertial Technology,Beijing 100090,China
  • 折叠

摘要

Abstract

This paper presents a fiber-optic gyroscope-based high-frequency micro-angular vibration measurement sensor for satellites.To meet the satellite's requirements for high-frequency micro-angular vibration measurement,the design of precision optics,detection circuitry,and overall structural configuration is carried out.Key breakthroughs are achieved in broadband noise suppression technology,adaptive filtering-based staircase wave interference suppression technology,and integrated optoelectronic separation structure design and testing technology.The developed sensor significantly reduces the output noise power spectral density to achieve a high-frequency micro-angular vibration sensor with a detection bandwidth better than 300 Hz.Ground tests and on-orbit application verification have confirmed that the sensor's performance meets the design specifications.

关键词

卫星/高频/微角振动测量/敏感器

Key words

satellite/high-frequency/micro-angle vibration measurement/sensor

分类

航空航天

引用本文复制引用

TENG Fei,ZHANG Yufei,LI Yong,ZHANG Peiyong,SUN Li,LIN Song,QIU Jinjuan,WANG Qiwei..卫星用高频微角振动测量敏感器设计、验证与在轨应用[J].空间控制技术与应用,2025,51(6):97-107,11.

基金项目

国家自然科学基金资助项目(62205016) National Natural Science Foundation of China(62205016) (62205016)

空间控制技术与应用

OA北大核心

1674-1579

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