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Application of RTS optimal smoothing algorithm in satellite attitude determination

机译:RTS最优平滑算法在卫星姿态确定中的应用

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In this paper, Rauch-Tung-Striebel(RTS) optimal smoothing algorithm is applied to improving off-line satellite attitude determination accuracy. The measurements are first processed by the forward filter, and then, a separate backward smoothing pass is used for obtaining the smoothing solution. The performances between RTS and extended Kalman filter(EKF) in gyro/star-sensor integrated system are compared. RTS smoother exhibits better accuracy and robustness than EKF under the situation of lower sensors precision, different length of data and larger initial attitude error. The results verify the effectiveness and practicability of RTS smoothing algorithm in satellite attitude determination.
机译:本文采用RAUCH-TUNG-STREBEL(RTS)最优平滑算法应用于提高离线卫星姿态确定精度。首先通过前进滤波器处理测量,然后,使用单独的后向平滑通段来获得平滑解决方案。比较了陀螺/星传感器集成系统中RTS和扩展卡尔曼滤波器(EKF)的性能。在较低的传感器精度,不同的数据和初始姿态误差下,RTS更顺畅比EKF在ekf上表现出更好的准确性和鲁棒性。结果验证了RTS平滑算法在卫星姿态确定中的有效性和实用性。

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