Two attitude determination systems are discussed for three-axis stabilization satellite. One uses gyros and magnetometer, and the other uses gyros and star sensor.
针对三轴稳定卫星的姿态估计问题,本文研究了“陀螺+磁强计”、“陀螺+星敏感器”两种姿态确定方案。
参考来源 - UKF和EKF在卫星姿态确定中的应用研究·2,447,543篇论文数据,部分数据来源于NoteExpress
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