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A Sequential Multiplicative Extended Kalman Filter for Attitude Estimation Using Vector Observations

机译:使用载体观测的姿态估计顺序乘法扩展卡尔曼滤波器

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摘要

In this paper, a sequential multiplicative extended Kalman filter (SMEKF) is proposed for attitude estimation using vector observations. In the proposed SMEKF, each of the vector observations is processed sequentially to update the attitude, which can make the measurement model linearization more accurate for the next vector observation. This is the main difference to Murrell’s variation of the MEKF, which does not update the attitude estimate during the sequential procedure. Meanwhile, the covariance is updated after all the vector observations have been processed, which is used to account for the special characteristics of the reset operation necessary for the attitude update. This is the main difference to the traditional sequential EKF, which updates the state covariance at each step of the sequential procedure. The numerical simulation study demonstrates that the proposed SMEKF has more consistent and accurate performance in a wide range of initial estimate errors compared to the MEKF and its traditional sequential forms.
机译:在本文中,提出了一种使用矢量观察的姿态估计的顺序乘法扩展卡尔曼滤波器(SMEKF)。在所提出的SMEKF中,每个向量观测依次处理以更新姿态,这可以使测量模型线性化更准确地用于下一个矢量观察。这是Murrell对MEKF变化的主要区别,这在顺序过程中不会更新姿态估计。同时,在处理所有向量观测后,可以更新协方差,用于考虑态度更新所需的复位操作的特殊特征。这是传统顺序EKF的主要区别,它在顺序过程的每个步骤中更新状态协方差。数值模拟研究表明,与MEKF及其传统的连续形式相比,所提出的SMEKF在广泛的初始估计误差方面具有更一致和准确的性能。

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