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面向微小卫星的星敏感器研究
引用本文:李赓,王昊,金仲和,王本冬.面向微小卫星的星敏感器研究[J].传感技术学报,2017,30(8).
作者姓名:李赓  王昊  金仲和  王本冬
作者单位:浙江大学航空航天学院,杭州,310027
摘    要:研制了一款新型面向微小卫星的星敏感器,采用商用器件构成以满足微小卫星对小型化的要求.星敏感器由工业镜头、DSP、低功耗CPLD和灰度型CMOS图像传感器组成.为进一步提高测量精度以满足卫星的需求,针对星敏感器的成像模型进行了分析,并用恒星校准的方式补偿了光学参数;对恒星处理算法进行了分析,在图像处理环节特别地采用了中值滤波技术,解决了孤立脉冲噪声对星点提取的影响.基于地球自转的星座跟踪实验表明,所研制的星敏感器样机欧拉角回归标准差为30″,已可实际应用于微小卫星平台.

关 键 词:星敏感器  微小卫星  姿态确定

Research on Star Tracker for Micro-satellites
LI Geng,WANG Hao,JIN Zhonghe,WANG Bendong.Research on Star Tracker for Micro-satellites[J].Journal of Transduction Technology,2017,30(8).
Authors:LI Geng  WANG Hao  JIN Zhonghe  WANG Bendong
Abstract:A new design of star tracker(ST)is proposed.The STisbased on the using of commercial devices,to matchMicro-satellites' compact size.The STconsists of an industrial lens,a DSP processor,a low power CPLD and a grayscale CMOS sensor.To improve the measurement accuracy,theimaging model of the STis analyzed,andthe optical parameters are compensated by in-field star calibration.The algorithm of star photoprocessing is also analyzed,anda median filter is applied to reduce the effect ofimpulse noise during star point extracting.A ST prototype is tested with field experimentsbased on the earth's rotation and constellation tracking,the results show that the prototype's RMSE(Root Mean Square Error)of Euler angleis 30″.The prototype,whichis in compact size and low power consumption,can be exactly applied to Micro-satellites.
Keywords:star tracker  micro-satellite  attitude determination
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