Active Pixel Digital Sun Sensor for Satellites

Muhammad Awais Arshad, Ali Nasir, M. Gulzar, Mansoor Fayyaz, Jawad Khalid Qureshi, Amer Saeed
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引用次数: 1

Abstract

Satellites use sun sensors as a reliable source of attitude determination during sunlit conditions while in orbit around the earth. This work elucidates the design and development of high precision and wide field of view digital sun sensor for space applications. Sun sensor employs active pixel image sensor along with processing techniques of feature extraction and image correlation. Software algorithm exploits the distinctive features of Active Pixel imaging Sensor (APS), in comparison to CCD based image sensor, for computationally efficient algorithm design. Sunlight falling on the sun sensor produces an image of the sun on image sensor. Software algorithm processes this image for noise removal, feature extraction, centroid analysis and sun vector calculations. Digital sun sensor, presented here, achieves 0.018 pixels (3σ) centroid accuracy with 120°×120°field of view.
卫星有源像素数字太阳敏感器
卫星在绕地球轨道运行时,利用太阳传感器作为确定姿态的可靠来源。本文阐述了高精度、大视场空间数字式太阳敏感器的设计与研制。太阳敏感器采用有源像素图像传感器,采用特征提取和图像相关处理技术。软件算法利用主动像素成像传感器(APS)的特点,与基于CCD的图像传感器相比,计算效率高的算法设计。落在太阳传感器上的太阳光在图像传感器上产生太阳的图像。软件算法处理该图像进行去噪、特征提取、质心分析和太阳矢量计算。数字式太阳敏感器在120°×120°视场下,质心精度达到0.018像素(3σ)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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