Star Identification Algorithm Based on Dynamic Distance Ratio Matching

A star tracker is a widely used celestial sensor in astronomical navigation systems, which calculates the spacecraft’s high-precision attitude by observing stars in space to obtain several star vectors. Existing star identification algorithms typically require the selection of a specific anchor star (e.g., the nearest neighbor star), using the line connecting the target star and the anchor star as the rotational reference axis to achieve rotation invariance in the star identification algorithm. However, this approach makes the entire identification algorithm overly dependent on the anchor star, resulting in insufficient identification accuracy in cases of excessive positional noise or a high number of false stars. In this paper, we adopt the angles between any neighboring stars and the distances ratio between neighboring stars and the observed star as the initial matching criteria. We then calculate the matching with each navigation star using the accumulated angle in the counterclockwise direction based on this criterion. The navigation star with the highest matching is identified. Unlike other identification algorithms that require selecting the nearest neighbor star which can be easily affected by interference as the rotational reference axis, our method effectively achieves rotation invariance in star identification by leveraging angle information. Therefore, it exhibits better tolerance to positional noise, magnitude noise, and false stars, particularly demonstrating higher robustness against focal length variations.

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Publication Details

Journal
Remote Sensing
Published
2024-12-27
DOI
https://doi.org/10.3390/rs17010062
Citations
3
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
3.90

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article

Star Identification Algorithm Based on Dynamic Distance Ratio Matching

Hua Xing Zhu, Yu Xu, Rui Zhang, Shufan Wu et al.
3 citations
Remote Sensing
Inertial Sensor and Navigation
3.90
article

Star Identification Algorithm Based on Dynamic Distance Ratio Matching

Hua Xing Zhu, Yu Xu, Rui Zhang, Shufan Wu, Chenguang Shi, Ya Dai, Sixiang Shan, Liyan Ben, Wang Zhou
article en
3 citations

Abstract

A star tracker is a widely used celestial sensor in astronomical navigation systems, which calculates the spacecraft’s high-precision attitude by observing stars in space to obtain several star vectors. Existing star identification algorithms typically require the selection of a specific anchor star (e.g., the nearest neighbor star), using the line connecting the target star and the anchor star as the rotational reference axis to achieve rotation invariance in the star identification algorithm. However, this approach makes the entire identification algorithm overly dependent on the anchor star, resulting in insufficient identification accuracy in cases of excessive positional noise or a high number of false stars. In this paper, we adopt the angles between any neighboring stars and the distances ratio between neighboring stars and the observed star as the initial matching criteria. We then calculate the matching with each navigation star using the accumulated angle in the counterclockwise direction based on this criterion. The navigation star with the highest matching is identified. Unlike other identification algorithms that require selecting the nearest neighbor star which can be easily affected by interference as the rotational reference axis, our method effectively achieves rotation invariance in star identification by leveraging angle information. Therefore, it exhibits better tolerance to positional noise, magnitude noise, and false stars, particularly demonstrating higher robustness against focal length variations.

Remote SensingVol. 17(1)
Shanghai Jiao Tong University (CN), Shanghai Micro Satellite Engineering Center (CN), Beihang University (CN), Nanjing University of Aeronautics and Astronautics (CN)
Shanghai Jiao Tong University
Openalex Percentile: Top 6%
Inertial Sensor and Navigation
3.90
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