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Geomagnetism Sensing and Calibration Systems of LING QIAO Satellite: Results Over Three Years of In-Orbit Operation

机译:岭桥卫星的地磁感应和校准系统:结果三年内轨道运行

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Geomagnetism-based attitude determination is a popular method for modern small/macro satellites for availability of small form factor, low power magnetometers and their accuracy in meeting the attitude precision requirements of many space missions. However, it is not an easy work to achieve high attitude precision for small mobile communication satellites by geomagnetism-based attitude sensing due to body magnetic interferences, either generated by high power current loop or complex magnetized field of ferromagnetic materials such as semi-rigid cable. In this work, we present the design and in orbit experiment results in the geomagnetism sensing and calibration systems of LING QIAO experimental mobile communication satellite. The LING QIAO satellite has worked in orbit steadily for more than three years, the in orbit results show an long term attitude control precision of 1° was achieved and short term attitude variation given by the MEMS gyroscope is less than 0.3°.
机译:基于地磁的姿态测定是一种普遍的现代小/宏卫卫星的流行方法,可提供小型系数,低功率磁力计及其在满足许多太空任务的姿态精度要求时的准确性。然而,由于身体磁干扰由于身体磁干扰,通过基于地磁的姿态感测来实现小型移动通信卫星的高姿态精度并不是一项容易的工作,由高功率电流回路或诸如半刚性电缆的铁磁材料的复合磁化领域产生。在这项工作中,我们展示了设计和轨道实验导致凌桥实验移动通信卫星的地磁传感和校准系统。凌巧卫星在轨道上稳步工作了三年以上,轨道结果显示了长期姿态控制精度为1°,由MEMS陀螺仪给出的短期姿态变化小于0.3°。

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