Author:
Fu Jingneng,Luo Wen,Zhang Hui
Abstract
Abstract
In the conventional methods of star sensor accuracy evaluation, neither the accuracy calculation formula nor the Monte Carlo method can comprehensively reflect the attitude measurement accuracy of star sensors in real-time. In this paper, a real-time analysis and calculation model for the attitude measurement accuracy of star sensors is proposed. Firstly, the basic attitude measurement model of the star sensor is established through the pinhole imaging model. Moreover, a moving frame of star sensor attitude measurement is established to avoid the defects of attitude representation by the Euler angle in the star sensor accuracy analysis. Then, combined with the error transfer of implicit overdetermined equations proposed in this paper, the error transfers of starspot extraction random error, star catalog random error, and intrinsic parameter system error are provided. Finally, simulation and field experiments are conducted to verify the accuracy of the proposed error analysis theory. The experimental results show that the attitude measurement accuracy of star sensors can be accurately estimated by using single-frame data of guide stars.
Reference14 articles.
1. Stellar attitude determination accuracy with multiple-star-tracking advanced star tracker;Abreu;Proceedings of SPIE - The International Society for Optical Engineering,1993
2. Error analysis of line-of-sight measurement for video satellite;Zhang;Advances in Mechanical Engineering,2017
3. Accuracy performance of star trackers - a tutorial;Liebe;IEEE Transactions on Aerospace Electronic Systems,2002
4. CMOS active pixel sensor specific performance effects on star tracker/imager position accuracy;Hancock,2001