Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter

Detalhes bibliográficos
Ano de defesa: 2020
Autor(a) principal: Cunto, Gabriel Giannini de
Orientador(a): Não Informado pela instituição
Banca de defesa: Não Informado pela instituição
Tipo de documento: Dissertação
Tipo de acesso: Acesso aberto
Idioma: eng
Instituição de defesa: Carleton University
Programa de Pós-Graduação: Não Informado pela instituição
Departamento: Não Informado pela instituição
País: Não Informado pela instituição
Palavras-chave em Português:
Link de acesso: https://www.repositorio.mar.mil.br/handle/ripcmb/845435
Resumo: In this work, a Fuzzy Logic Adaptive Control (FLAC) is used to correct an Error-State Kalman Filter (ESKF) and an Unscented Kalman Filter (UKF) in a loosely coupled INS/GNSS system. The FLAC is used to prevent the Kalman Filter (KF) to diverge or to reach to a high bound solution when the Inertial Measurement Unit (IMU) presents a dominant 1/f flicker noise. First, the ESKF and UKF implementation were tuned to achieve the optimal solution when the IMU has only white noise. Secondly, a 1/f flicker noise was applied to the IMU, making both Kalman Filters implementation achieve a suboptimal solution. And thirdly, a FLAC was used to correct both ESKF and UKF when coloured noise is present. The results evidence the influence of coloured noise in the system, which makes both Kalman Filter implementations reach to a large error bound solution. After analyzing the Kalman Filter behaviour with coloured noise, a novel FLAC methodology was defined. The FLAC combines the observation of both the residuals and the states error covariance and apply the correction using the exponential weighted parameter when the error covariance presents a higher than expected value, and a process noise injection when the residuals are broader than expected. The application of the proposed FLAC methodology figures out as the best solution to deal with the coloured noise, leading to a final solution that improves the navigation accuracy for all the states, preserving the stability of the error covariance matrix. Finally, the results for ESKF are compared against the results for the UKF. It was showed that, although both Kalman filter implementations bring equivalent outcomes, the UKF is slightly less sensitive to disturbances.
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spelling Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filterSistemas de navegaçãoFiltro de KalmanCiência, Tecnologia e InovaçãoIn this work, a Fuzzy Logic Adaptive Control (FLAC) is used to correct an Error-State Kalman Filter (ESKF) and an Unscented Kalman Filter (UKF) in a loosely coupled INS/GNSS system. The FLAC is used to prevent the Kalman Filter (KF) to diverge or to reach to a high bound solution when the Inertial Measurement Unit (IMU) presents a dominant 1/f flicker noise. First, the ESKF and UKF implementation were tuned to achieve the optimal solution when the IMU has only white noise. Secondly, a 1/f flicker noise was applied to the IMU, making both Kalman Filters implementation achieve a suboptimal solution. And thirdly, a FLAC was used to correct both ESKF and UKF when coloured noise is present. The results evidence the influence of coloured noise in the system, which makes both Kalman Filter implementations reach to a large error bound solution. After analyzing the Kalman Filter behaviour with coloured noise, a novel FLAC methodology was defined. The FLAC combines the observation of both the residuals and the states error covariance and apply the correction using the exponential weighted parameter when the error covariance presents a higher than expected value, and a process noise injection when the residuals are broader than expected. The application of the proposed FLAC methodology figures out as the best solution to deal with the coloured noise, leading to a final solution that improves the navigation accuracy for all the states, preserving the stability of the error covariance matrix. Finally, the results for ESKF are compared against the results for the UKF. It was showed that, although both Kalman filter implementations bring equivalent outcomes, the UKF is slightly less sensitive to disturbances.Carleton University2022-08-26T19:18:40Z2022-08-26T19:18:40Z2020info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesisapplication/pdfhttps://www.repositorio.mar.mil.br/handle/ripcmb/845435engCunto, Gabriel Giannini deinfo:eu-repo/semantics/openAccessreponame:Repositório Institucional da Produção Científica da Marinha do Brasil (RI-MB)instname:Marinha do Brasil (MB)instacron:MB2023-05-12T13:20:37Zoai:www.repositorio.mar.mil.br:ripcmb/845435Repositório InstitucionalPUBhttps://www.repositorio.mar.mil.br/oai/requestdphdm.repositorio@marinha.mil.bropendoar:2023-05-12T13:20:37Repositório Institucional da Produção Científica da Marinha do Brasil (RI-MB) - Marinha do Brasil (MB)false
dc.title.none.fl_str_mv Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
title Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
spellingShingle Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
Cunto, Gabriel Giannini de
Sistemas de navegação
Filtro de Kalman
Ciência, Tecnologia e Inovação
title_short Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
title_full Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
title_fullStr Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
title_full_unstemmed Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
title_sort Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
author Cunto, Gabriel Giannini de
author_facet Cunto, Gabriel Giannini de
author_role author
dc.contributor.author.fl_str_mv Cunto, Gabriel Giannini de
dc.subject.por.fl_str_mv Sistemas de navegação
Filtro de Kalman
Ciência, Tecnologia e Inovação
topic Sistemas de navegação
Filtro de Kalman
Ciência, Tecnologia e Inovação
description In this work, a Fuzzy Logic Adaptive Control (FLAC) is used to correct an Error-State Kalman Filter (ESKF) and an Unscented Kalman Filter (UKF) in a loosely coupled INS/GNSS system. The FLAC is used to prevent the Kalman Filter (KF) to diverge or to reach to a high bound solution when the Inertial Measurement Unit (IMU) presents a dominant 1/f flicker noise. First, the ESKF and UKF implementation were tuned to achieve the optimal solution when the IMU has only white noise. Secondly, a 1/f flicker noise was applied to the IMU, making both Kalman Filters implementation achieve a suboptimal solution. And thirdly, a FLAC was used to correct both ESKF and UKF when coloured noise is present. The results evidence the influence of coloured noise in the system, which makes both Kalman Filter implementations reach to a large error bound solution. After analyzing the Kalman Filter behaviour with coloured noise, a novel FLAC methodology was defined. The FLAC combines the observation of both the residuals and the states error covariance and apply the correction using the exponential weighted parameter when the error covariance presents a higher than expected value, and a process noise injection when the residuals are broader than expected. The application of the proposed FLAC methodology figures out as the best solution to deal with the coloured noise, leading to a final solution that improves the navigation accuracy for all the states, preserving the stability of the error covariance matrix. Finally, the results for ESKF are compared against the results for the UKF. It was showed that, although both Kalman filter implementations bring equivalent outcomes, the UKF is slightly less sensitive to disturbances.
publishDate 2020
dc.date.none.fl_str_mv 2020
2022-08-26T19:18:40Z
2022-08-26T19:18:40Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/masterThesis
format masterThesis
status_str publishedVersion
dc.identifier.uri.fl_str_mv https://www.repositorio.mar.mil.br/handle/ripcmb/845435
url https://www.repositorio.mar.mil.br/handle/ripcmb/845435
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Carleton University
publisher.none.fl_str_mv Carleton University
dc.source.none.fl_str_mv reponame:Repositório Institucional da Produção Científica da Marinha do Brasil (RI-MB)
instname:Marinha do Brasil (MB)
instacron:MB
instname_str Marinha do Brasil (MB)
instacron_str MB
institution MB
reponame_str Repositório Institucional da Produção Científica da Marinha do Brasil (RI-MB)
collection Repositório Institucional da Produção Científica da Marinha do Brasil (RI-MB)
repository.name.fl_str_mv Repositório Institucional da Produção Científica da Marinha do Brasil (RI-MB) - Marinha do Brasil (MB)
repository.mail.fl_str_mv dphdm.repositorio@marinha.mil.br
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