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DOI:
飞控与探测:2022,(5):01-05
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H波段折反式星敏感器光学系统设计
(1.哈尔滨工业大学空间光学工程研究中心;2.上海航天控制技术研究所)
Optical System Design of H-Band Catadioptric Star Tracker
(1.Research Center for Space Optical Engineering, Harbin Institute of Technology;2.Shanghai Aerospace Control Technology Institute, Shanghai)
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中文摘要: 面向短波红外星敏感器在机载平台、弹载平台以及舰载平台的应用需求,设计了H波段折反式星敏感器光学系统。该折反式镜头总长为232mm、焦距为704.3mm、全视场为2°、F数为3.9、探测极限星等为6。结果表明:调制传递函数值接近衍射极限,在奈奎斯特采样频率处大于0.5;各视场径向能量趋于一致,弥散斑可覆盖2~3像元;相对畸变小于0.1%,满足指标要求。本文可为近地空间短波红外星敏感器的工程应用提供理论基础与技术支持。
中文关键词: 星敏感器  H波段  折反式  光学设计  近地空间
Abstract:The optical system of the H-band catadioptric star tracker is designed for application on airborne, missile, and ship-borne platforms. The total length of the catadioptric lens is 232mm, the focal length is 704.3mm, the whole field of view is 2°, the F-number is 3.9, and the detection limit magnitude is 6. The results show that the value of the modulation transfer function is close to the diffraction limit and is more significant than 0.5 at Nyquist frequency. The radial energy of each field of view is consistent, and the dispersing speckle can cover 2~3 pixels. The relative distortion is less than 0.1%, which meets the index. This paper can provide a theoretical basis and technical support for the engineering application of short wavelength infrared star trackers in near-earth space.
文章编号:20220501     中图分类号:V11    文献标志码:A
基金项目:国家自然科学基金(61705220)
引用文本:
汪洪源,王秉文,毛晓楠.H波段折反式星敏感器光学系统设计[J].飞控与探测,2022,(5):01-05.