A Star Tracker for Cubesats - Implementation and Analysis

Wen Chen, Shau-Shiun Jan
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Abstract

A star tracker employs images of stars taken by a satellite-based camera to estimate its attitude and angular velocity in space. A star tracker is a flexible attitude sensor, which meets the requirements of a CubeSat. The objective of this paper is to develop an arc-minute accurate star tracker algorithm for CubeSats, and to analyze the results using a software-in-the-loop simulation. The algorithm is divided into three main parts: centroiding, Lost-in-Space (LIS) mode, and tracking mode. The weight sum method is used in centroiding, the voting method and quaternion-estimator (QUEST) method are used in the LIS mode, and the extended Kalman Filter (EKF) and catalog partitioning are used in tracking. Stars images are simulated to verify the algorithm. We evaluate centroid accuracy under different noise levels and star magnitudes, and the results have sub-pixel accuracy. In addition, we show the performance of LIS algorithm. With an appropriate voting tolerance, over 80% of the stars are correctly matched, the attitude estimations have arc-minute accuracy, and the matching results have over a 95% success rate. Also, the performance of the tracking algorithm is showed. The tracking results are successful, and the attitude estimation from the EKF has arc-minute accuracy.
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一种用于立方体卫星的星跟踪器——实现与分析
恒星跟踪器利用卫星相机拍摄的恒星图像来估计其在太空中的姿态和角速度。星跟踪器是一种满足立方体卫星要求的柔性姿态传感器。本文的目标是开发一种用于立方体卫星的弧分精确星跟踪算法,并使用软件在环仿真对结果进行分析。该算法分为三个主要部分:质心、空间丢失(LIS)模式和跟踪模式。质心定位采用权值和法,LIS模式采用投票法和四元数估计法,跟踪采用扩展卡尔曼滤波(EKF)和目录划分。通过星图仿真验证了算法的有效性。我们评估了不同噪声水平和星等下的质心精度,结果具有亚像素精度。此外,我们还展示了LIS算法的性能。在适当的投票容差下,匹配正确率达到80%以上,姿态估计精度达到弧分,匹配成功率达到95%以上。最后,给出了该跟踪算法的性能。结果表明,基于EKF的姿态估计具有弧分精度。
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