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ROBUST STAR IDENTIFICATION FOR SPACECRAFT ATTITUDE DETERMINATION

机译:航天器态度决心的强大明星识别

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Accurate attitude information is necessary for advanced space missions. Among existing instruments providing attitude information to spacecraft control systems, star trackers are most accurate for attitude estimation without requiring a priori information. For use of the star tracker data, it is required to identify stars in the field of view (FOV) of a star tracker. Many algorithms for star identification have been developed to determine the correspondence between the imaged stars and the reference stars stored in onboard star catalog. However, few algorithms could realize a robust star identification with the small amount of memory. This paper presents a new algorithm that, by using a defocused onboard star catalog, realizes a robust star identification with the small amount of memory. The robustness of this algorithm is evaluated by the sky simulation. The sky simulation results demonstrate that the proposed algorithm is a robust star identification method with the small amount of memory and suitable for the charge-coupled device (CCD) star tracker with a small FOV.
机译:准确的态度信息是高级空间任务所必需的。在向航天器控制系统提供态度信息的现有仪器中,明星跟踪器最准确地用于姿态估计,而无需先验信息。为了使用星形跟踪器数据,需要识别星际跟踪器的视野(FOV)的恒星。已经开发出许多用于星形识别的算法以确定成像恒星与存储在船上星形目录中的参考恒星之间的对应关系。然而,很少有算法可以实现具有少量内存的强大的星形标识。本文介绍了一种新的算法,通过使用Defocused船上的星星目录,实现了具有少量内存的强大的星形标识。该算法的鲁棒性由天空仿真评估。天空仿真结果表明,该算法是一种具有少量存储器的强大的星形识别方法,适用于具有小FOV的电荷耦合器件(CCD)星跟踪器。

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