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Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature
This paper investigates the problem of spacecraft relative navigation with respect to an unknown target during the close-proximity operations in the on-orbit service system. The serving spacecraft is equipped with a Time-of-Flight (ToF) camera for object recognition and feature detection. A fast and...
Autores principales: | , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2021
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8708270/ https://www.ncbi.nlm.nih.gov/pubmed/34960586 http://dx.doi.org/10.3390/s21248495 |
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author | Liu, Yue Zhang, Shijie Zhao, Xiangtian |
author_facet | Liu, Yue Zhang, Shijie Zhao, Xiangtian |
author_sort | Liu, Yue |
collection | PubMed |
description | This paper investigates the problem of spacecraft relative navigation with respect to an unknown target during the close-proximity operations in the on-orbit service system. The serving spacecraft is equipped with a Time-of-Flight (ToF) camera for object recognition and feature detection. A fast and robust relative navigation strategy for acquisition is presented without any extra information about the target by using the natural circle features. The architecture of the proposed relative navigation strategy consists of three ingredients. First, a point cloud segmentation method based on the auxiliary gray image is developed for fast extraction of the circle feature point cloud of the target. Secondly, a new parameter fitting method of circle features is proposed including circle feature calculation by two different geometric models and results’ fusion. Finally, a specific definition of the coordinate frame system is introduced to solve the relative pose with respect to the uncooperative target. In order to validate the efficiency of the segmentation, an experimental test is conducted based on real-time image data acquired by the ToF camera. The total time consumption is saved by 94%. In addition, numerical simulations are carried out to evaluate the proposed navigation algorithm. It shows good robustness under the different levels of noises. |
format | Online Article Text |
id | pubmed-8708270 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2021 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-87082702021-12-25 Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature Liu, Yue Zhang, Shijie Zhao, Xiangtian Sensors (Basel) Article This paper investigates the problem of spacecraft relative navigation with respect to an unknown target during the close-proximity operations in the on-orbit service system. The serving spacecraft is equipped with a Time-of-Flight (ToF) camera for object recognition and feature detection. A fast and robust relative navigation strategy for acquisition is presented without any extra information about the target by using the natural circle features. The architecture of the proposed relative navigation strategy consists of three ingredients. First, a point cloud segmentation method based on the auxiliary gray image is developed for fast extraction of the circle feature point cloud of the target. Secondly, a new parameter fitting method of circle features is proposed including circle feature calculation by two different geometric models and results’ fusion. Finally, a specific definition of the coordinate frame system is introduced to solve the relative pose with respect to the uncooperative target. In order to validate the efficiency of the segmentation, an experimental test is conducted based on real-time image data acquired by the ToF camera. The total time consumption is saved by 94%. In addition, numerical simulations are carried out to evaluate the proposed navigation algorithm. It shows good robustness under the different levels of noises. MDPI 2021-12-20 /pmc/articles/PMC8708270/ /pubmed/34960586 http://dx.doi.org/10.3390/s21248495 Text en © 2021 by the authors. https://creativecommons.org/licenses/by/4.0/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 (https://creativecommons.org/licenses/by/4.0/). |
spellingShingle | Article Liu, Yue Zhang, Shijie Zhao, Xiangtian Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature |
title | Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature |
title_full | Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature |
title_fullStr | Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature |
title_full_unstemmed | Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature |
title_short | Relative Pose Determination of Uncooperative Spacecraft Based on Circle Feature |
title_sort | relative pose determination of uncooperative spacecraft based on circle feature |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8708270/ https://www.ncbi.nlm.nih.gov/pubmed/34960586 http://dx.doi.org/10.3390/s21248495 |
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