{"title":"Robust Attitude Estimation with Quaternion Left-Invariant EKF and Noise Covariance Tuning","authors":"Yash Pandey, Rahul Bhattacharyya, Yatindra Nath Singh","doi":"arxiv-2409.11496","DOIUrl":null,"url":null,"abstract":"Accurate estimation of noise parameters is critical for optimal filter\nperformance, especially in systems where true noise parameter values are\nunknown or time-varying. This article presents a quaternion left-invariant\nextended Kalman filter (LI-EKF) for attitude estimation, integrated with an\nadaptive noise covariance estimation algorithm. By employing an iterative\nexpectation-maximization (EM) approach, the filter can effectively estimate\nboth process and measurement noise covariances. Extensive simulations\ndemonstrate the superiority of the proposed method in terms of attitude\nestimation accuracy and robustness to initial parameter misspecification. The\nadaptive LI-EKF's ability to adapt to time-varying noise characteristics makes\nit a promising solution for various applications requiring reliable attitude\nestimation, such as aerospace, robotics, and autonomous systems.","PeriodicalId":501175,"journal":{"name":"arXiv - EE - Systems and Control","volume":"92 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-09-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - EE - Systems and Control","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2409.11496","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
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.