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基于莫尔条纹的星光测量技术特性及误差研究

郭放 杜伟峰 郑循江 叶志龙 张徐玮

上海航天(中英文)2025,Vol.42Issue(3):95-103,9.
上海航天(中英文)2025,Vol.42Issue(3):95-103,9.DOI:10.19328/j.cnki.2096-8655.2025.03.012

基于莫尔条纹的星光测量技术特性及误差研究

Technical Characteristics and Error Analysis of Starlight Measurement Based on Moiré Fringes

郭放 1杜伟峰 1郑循江 1叶志龙 1张徐玮1

作者信息

  • 1. 上海航天控制技术研究所,上海 201109||上海市空间智能控制技术重点实验室,上海 201109||空间目标感知全国重点实验室,上海 201109
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摘要

Abstract

To break through the limit of attitude measurement accuracy of traditional star sensors,the interferometric angle measurement technology can be applied to star sensors.Based on the centroid positioning technology,the fringe phase movement can be obtained from the energy of image points,and then the incidence angle can be obtained.In this paper,the imaging mechanism and characteristics of interferometric star sensors are investigated based on Moiré fringes,the influence of the optical structure parameters on the imaging effect and errors are analyzed,and finally methods for reducing the errors are given.It is shown that the grating cannot completely suppress the diffraction light beyond the±1 diffraction order,resulting in multiple sets of image points.Therefore,the grating period and detector distance should be adjusted to move other image points off the screen.Besides,the mismatch between the Moiré fringes and the system aperture will bring segmentation errors.Thus,the deviation between the Moiré fringe period and the system aperture should not exceed 0.5%,and the phase extraction error at this moment should not exceed 2%.Moreover,when the distance between two gratings is not in accordance with the Tabor distance,there will be a phase deviation in the imaging.In view of this,the reference wavelength should be designed according to the target spectra.

关键词

干涉星敏感器/姿态测量精度/泰伯距离/成像机理/莫尔条纹

Key words

interferometric star sensor/attitude measurement/Talbot distance/imaging mechanism/Moiré fringe

分类

信息技术与安全科学

引用本文复制引用

郭放,杜伟峰,郑循江,叶志龙,张徐玮..基于莫尔条纹的星光测量技术特性及误差研究[J].上海航天(中英文),2025,42(3):95-103,9.

基金项目

国家重点研发计划资助课题(2019YFA0706003、2019YFA0706002) (2019YFA0706003、2019YFA0706002)

上海航天(中英文)

2096-8655

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