attitude determination algorithm

基本解释

A filtering algorithm for high precision attitude determination of a specific satellite is presented based on star-sensors and fiber optic gyroscopes (FOG).
为了满足卫星三轴姿态确定的精度要求，提出了基于状态估计法的星敏感器和光纤陀螺组合的方案，并设计了相应姿态确定算法。
An adaptive extended Kalman filtering algorithm is presented in this paper for attitude determination consisting of a pseudo gyro, a magnetometer and an earth sensor.
以伪陀螺、磁强计与地球敏感器构成的姿态测量系统为基础，设计了自适应扩展卡尔曼滤波算法。
A novel optimal attitude and attitude-rate estimation algorithm is proposed to address the problem of autonomous attitude determination using gravitational filed and geomagnetic field observation.
针对利用地球重力场和磁场矢量观测进行自主姿态测量的应用问题，提出了一种新的最优递推估计算法。
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