Robust Attitude Estimation with Quaternion Left-Invariant EKF and Noise Covariance Tuning

Yash Pandey, Rahul Bhattacharyya, Yatindra Nath Singh
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Abstract

Accurate estimation of noise parameters is critical for optimal filter performance, especially in systems where true noise parameter values are unknown or time-varying. This article presents a quaternion left-invariant extended Kalman filter (LI-EKF) for attitude estimation, integrated with an adaptive noise covariance estimation algorithm. By employing an iterative expectation-maximization (EM) approach, the filter can effectively estimate both process and measurement noise covariances. Extensive simulations demonstrate the superiority of the proposed method in terms of attitude estimation accuracy and robustness to initial parameter misspecification. The adaptive LI-EKF's ability to adapt to time-varying noise characteristics makes it a promising solution for various applications requiring reliable attitude estimation, such as aerospace, robotics, and autonomous systems.
利用四元数左变 EKF 和噪声协方差调整进行鲁棒姿态估计
噪声参数的准确估计对于优化滤波器性能至关重要,尤其是在噪声参数真实值未知或随时间变化的系统中。本文介绍了一种用于姿态估计的四元左变下延卡尔曼滤波器(LI-EKF),该滤波器集成了自适应噪声协方差估计算法。通过采用迭代期望最大化(EM)方法,该滤波器可以有效估计过程噪声和测量噪声协方差。大量的仿真证明,所提出的方法在姿态估计的准确性和对初始参数错误指定的鲁棒性方面具有优势。自适应 LI-EKF 能够适应时变噪声特性,这使它在航空航天、机器人和自主系统等需要可靠姿态估计的各种应用中成为一种很有前途的解决方案。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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