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一种基于直接天文观测的星敏感器精度测量方法。

An accuracy measurement method for star trackers based on direct astronomic observation.

作者信息

Sun Ting, Xing Fei, Wang Xiaochu, You Zheng, Chu Daping

机构信息

Department of Precision Instrument, Tsinghua University, Beijing, China.

State Key Laboratory of Precision Measurement Technology and Instruments, Tsinghua University, Beijing, China.

出版信息

Sci Rep. 2016 Mar 7;6:22593. doi: 10.1038/srep22593.

Abstract

Star tracker is one of the most promising optical attitude measurement devices and it is widely used in spacecraft for its high accuracy. However, how to realize and verify such an accuracy remains a crucial but unsolved issue until now. The authenticity of the accuracy measurement method of a star tracker will eventually determine the satellite performance. A new and robust accuracy measurement method for a star tracker based on the direct astronomical observation is proposed here. In comparison with the conventional method with simulated stars, this method utilizes real navigation stars as observation targets which makes the measurement results more authoritative and authentic. Transformations between different coordinate systems are conducted on the account of the precision movements of the Earth, and the error curves of directional vectors are obtained along the three axes. Based on error analysis and accuracy definitions, a three-axis accuracy evaluation criterion has been proposed in this paper, which could determine pointing and rolling accuracy of a star tracker directly. Experimental measurements confirm that this method is effective and convenient to implement. Such a measurement environment is close to the in-orbit conditions and it can satisfy the stringent requirement for high-accuracy star trackers.

摘要

星敏感器是最具前景的光学姿态测量装置之一,因其高精度而在航天器中得到广泛应用。然而,如何实现并验证这种精度至今仍是一个关键但尚未解决的问题。星敏感器精度测量方法的真实性最终将决定卫星的性能。本文提出了一种基于直接天文观测的新型且稳健的星敏感器精度测量方法。与使用模拟星的传统方法相比,该方法利用真实导航星作为观测目标,这使得测量结果更具权威性和真实性。考虑到地球的精确运动,进行不同坐标系之间的转换,并沿三个轴获得方向矢量的误差曲线。基于误差分析和精度定义,本文提出了一种三轴精度评估准则,该准则可直接确定星敏感器的指向和滚动精度。实验测量证实该方法有效且易于实施。这样的测量环境接近在轨条件,能够满足对高精度星敏感器的严格要求。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a753/4984851/0ac4cc84829a/srep22593-f1.jpg

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