Sensor Fusion INS/GNSS based on Fuzzy Logic Adaptive Error-State Kalman filter and Unscented Kalman filter
| Ano de defesa: | 2020 |
|---|---|
| Autor(a) principal: | |
| Orientador(a): | |
| Banca de defesa: | |
| 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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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 |
| _version_ |
1855762808845631488 |