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An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors

Efficiency and reliability are key issues when a star sensor operates in tracking mode. In the case of high attitude dynamics, the performance of existing attitude tracking algorithms degenerates rapidly. In this paper an extended Kalman filtering-based attitude tracking algorithm is presented. The...

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Detalles Bibliográficos
Autores principales: Li, Jian, Wei, Xinguo, Zhang, Guangjun
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2017
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5580079/
https://www.ncbi.nlm.nih.gov/pubmed/28825684
http://dx.doi.org/10.3390/s17081921
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author Li, Jian
Wei, Xinguo
Zhang, Guangjun
author_facet Li, Jian
Wei, Xinguo
Zhang, Guangjun
author_sort Li, Jian
collection PubMed
description Efficiency and reliability are key issues when a star sensor operates in tracking mode. In the case of high attitude dynamics, the performance of existing attitude tracking algorithms degenerates rapidly. In this paper an extended Kalman filtering-based attitude tracking algorithm is presented. The star sensor is modeled as a nonlinear stochastic system with the state estimate providing the three degree-of-freedom attitude quaternion and angular velocity. The star positions in the star image are predicted and measured to estimate the optimal attitude. Furthermore, all the cataloged stars observed in the sensor field-of-view according the predicted image motion are accessed using a catalog partition table to speed up the tracking, called star mapping. Software simulation and night-sky experiment are performed to validate the efficiency and reliability of the proposed method.
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spelling pubmed-55800792017-09-06 An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors Li, Jian Wei, Xinguo Zhang, Guangjun Sensors (Basel) Article Efficiency and reliability are key issues when a star sensor operates in tracking mode. In the case of high attitude dynamics, the performance of existing attitude tracking algorithms degenerates rapidly. In this paper an extended Kalman filtering-based attitude tracking algorithm is presented. The star sensor is modeled as a nonlinear stochastic system with the state estimate providing the three degree-of-freedom attitude quaternion and angular velocity. The star positions in the star image are predicted and measured to estimate the optimal attitude. Furthermore, all the cataloged stars observed in the sensor field-of-view according the predicted image motion are accessed using a catalog partition table to speed up the tracking, called star mapping. Software simulation and night-sky experiment are performed to validate the efficiency and reliability of the proposed method. MDPI 2017-08-21 /pmc/articles/PMC5580079/ /pubmed/28825684 http://dx.doi.org/10.3390/s17081921 Text en © 2017 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
Li, Jian
Wei, Xinguo
Zhang, Guangjun
An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors
title An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors
title_full An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors
title_fullStr An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors
title_full_unstemmed An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors
title_short An Extended Kalman Filter-Based Attitude Tracking Algorithm for Star Sensors
title_sort extended kalman filter-based attitude tracking algorithm for star sensors
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5580079/
https://www.ncbi.nlm.nih.gov/pubmed/28825684
http://dx.doi.org/10.3390/s17081921
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