基于星跟踪器高精度测量的星载卫星偏航转向律修正

2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics Pub Date : 2010-06-08 DOI:10.1109/ISSCAA.2010.5633474

Sun Yingmei, Chen Junli, Wan Xiangcheng, Zhang Jiu Ling, Wang Yun

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引用次数: 0

摘要

本文给出了偏航转向律在卫星工程中应用的成功实例。另外，在合成孔径雷达卫星中，可以在轨道上获得偏航转向律的理论参数并对其进行优化，从而得到期望的多普勒质心。

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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The correction of spaceborne satellite's yaw steering law based on the star tracker high-precision measurement

This paper presents a successful example of how the yaw steering law used in the satellite project. Otherwise in the synthetic aperture radar satellite, the theoretic parameter of the yaw steering law can be obtained and optimized on the track, then the expected Doppler centroid will be gotten.

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2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

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