On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability Analysis
This paper presents the second part of a study aiming at the error state selection in Kalman filters applied to the stationary self-alignment and calibration (SSAC) problem of strapdown inertial navigation systems (SINS). The observability properties of the system are systematically investigated, an...
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doaj-43f31977200b4d7799806d61618a0ca72020-11-24T22:06:32ZengMDPI AGSensors1424-82202017-02-0117343910.3390/s17030439s17030439On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability AnalysisFelipe O. Silva0Elder M. Hemerly1Waldemar C. Leite Filho2Department of Engineering, Federal University of Lavras, Lavras 37200-000, BrazilAeronautics Institute of Technology, Division of Electronic Engineering, São José dos Campos 12228-900, BrazilNational Institute for Space Research, Division of Space Mechanics and Control, São José dos Campos 12227-010, BrazilThis paper presents the second part of a study aiming at the error state selection in Kalman filters applied to the stationary self-alignment and calibration (SSAC) problem of strapdown inertial navigation systems (SINS). The observability properties of the system are systematically investigated, and the number of unobservable modes is established. Through the analytical manipulation of the full SINS error model, the unobservable modes of the system are determined, and the SSAC error states (except the velocity errors) are proven to be individually unobservable. The estimability of the system is determined through the examination of the major diagonal terms of the covariance matrix and their eigenvalues/eigenvectors. Filter order reduction based on observability analysis is shown to be inadequate, and several misconceptions regarding SSAC observability and estimability deficiencies are removed. As the main contributions of this paper, we demonstrate that, except for the position errors, all error states can be minimally estimated in the SSAC problem and, hence, should not be removed from the filter. Corroborating the conclusions of the first part of this study, a 12-state Kalman filter is found to be the optimal error state selection for SSAC purposes. Results from simulated and experimental tests support the outlined conclusions.http://www.mdpi.com/1424-8220/17/3/439SINSalignmentcalibrationerror state selectionobservabilityestimability |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Felipe O. Silva Elder M. Hemerly Waldemar C. Leite Filho |
spellingShingle |
Felipe O. Silva Elder M. Hemerly Waldemar C. Leite Filho On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability Analysis Sensors SINS alignment calibration error state selection observability estimability |
author_facet |
Felipe O. Silva Elder M. Hemerly Waldemar C. Leite Filho |
author_sort |
Felipe O. Silva |
title |
On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability Analysis |
title_short |
On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability Analysis |
title_full |
On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability Analysis |
title_fullStr |
On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability Analysis |
title_full_unstemmed |
On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters—Part II: Observability/Estimability Analysis |
title_sort |
on the error state selection for stationary sins alignment and calibration kalman filters—part ii: observability/estimability analysis |
publisher |
MDPI AG |
series |
Sensors |
issn |
1424-8220 |
publishDate |
2017-02-01 |
description |
This paper presents the second part of a study aiming at the error state selection in Kalman filters applied to the stationary self-alignment and calibration (SSAC) problem of strapdown inertial navigation systems (SINS). The observability properties of the system are systematically investigated, and the number of unobservable modes is established. Through the analytical manipulation of the full SINS error model, the unobservable modes of the system are determined, and the SSAC error states (except the velocity errors) are proven to be individually unobservable. The estimability of the system is determined through the examination of the major diagonal terms of the covariance matrix and their eigenvalues/eigenvectors. Filter order reduction based on observability analysis is shown to be inadequate, and several misconceptions regarding SSAC observability and estimability deficiencies are removed. As the main contributions of this paper, we demonstrate that, except for the position errors, all error states can be minimally estimated in the SSAC problem and, hence, should not be removed from the filter. Corroborating the conclusions of the first part of this study, a 12-state Kalman filter is found to be the optimal error state selection for SSAC purposes. Results from simulated and experimental tests support the outlined conclusions. |
topic |
SINS alignment calibration error state selection observability estimability |
url |
http://www.mdpi.com/1424-8220/17/3/439 |
work_keys_str_mv |
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