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Invariant Momentum-tracking Kalman Filter for attitude estimation

机译:不变动量跟踪卡尔曼滤波器用于姿态估计

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摘要

This paper presents the development, simulation and experimental testing of a non-linear Kalman filter for attitude estimation. This non-linear filter is able to conserve the invariants of the Kalman filter, i.e., the expectations on state estimates and their covariances, by operating in the Lie algebra of SO(3) and along the trajectory of evolving angular momentum. The main feature of this novel discrete-time filter is that the linearization of the Gaussian uncertainty around these permanent trajectories leads to a locally optimal Kalman gain matrix. Results confirm that this Invariant Momentum-tracking Kalman Filter (IMKF) out-performs state-of-the-art approaches such as the Extended Kalman Filter (EKF), and Invariant Extended Kalman Filter (IEKF). At very-low sampling rates, EKFs suffer from divergence as the uncertainty propagation is corrupted by the underlying system approximations. The IMKF suffers no such problems according to the theoretical developments and results reported here.
机译:本文介绍了用于姿态估计的非线性卡尔曼滤波器的开发,仿真和实验测试。通过在SO(3)的李代数中以及沿着角动量的变化轨迹进行运算,该非线性滤波器能够保留卡尔曼滤波器的不变性,即对状态估计及其协方差的期望。这种新颖的离散时间滤波器的主要特征是,围绕这些永久轨迹的高斯不确定性的线性化导致了局部最优的卡尔曼增益矩阵。结果证实,该不变动量跟踪卡尔曼滤波器(IMKF)优于最新方法,例如扩展卡尔曼滤波器(EKF)和不变扩展卡尔曼滤波器(IEKF)。在非常低的采样率下,EKF会发散,因为不确定性传播会受到基础系统近似的破坏。根据理论发展和此处报告的结果,IMKF不会遇到此类问题。

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