M. Selezneva, A. Proletarsky, K. Neusypin, Zhang Lifei
{"title":"Modification of the Federated Kalman Filter Using the Observability Degree Criterion of State Variables","authors":"M. Selezneva, A. Proletarsky, K. Neusypin, Zhang Lifei","doi":"10.23919/ICINS.2019.8769385","DOIUrl":null,"url":null,"abstract":"The implementation schemes of the federated Kalman filter are considered. It is proposed to increase the accuracy of the federated Kalman filter using a numerical criterion for the observability degree of state variables of the process assessed. The observability degree criterion is used to determine the correction factors of the federated Kalman filter. The effectiveness of the developed modifications of the federated Kalman filter is demonstrated by the example of estimating the errors of the aircraft inertial navigation system.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"99 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ICINS.2019.8769385","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 5
Abstract
The implementation schemes of the federated Kalman filter are considered. It is proposed to increase the accuracy of the federated Kalman filter using a numerical criterion for the observability degree of state variables of the process assessed. The observability degree criterion is used to determine the correction factors of the federated Kalman filter. The effectiveness of the developed modifications of the federated Kalman filter is demonstrated by the example of estimating the errors of the aircraft inertial navigation system.