Abstract
A real-time correlation method for space objects using radar observations is proposed in this paper. According to the orbit prediction error characteristics of space objects, an error model is established in the satellite-based coordinate system, and the correlation threshold is calculated based on the Hill equation and the inner accuracy of orbital elements. In order to meet the requirements of engineering application, the double decision is used to improve the efficiency. The simulation results verify the feasibility and effectiveness of the method.
Original language | English |
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Title of host publication | 2019 2nd International Conference on Electronics Technology, ICET 2019 |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 263-268 |
Number of pages | 6 |
ISBN (Electronic) | 9781728116181 |
DOIs | |
Publication status | Published - May 2019 |
Event | 2nd IEEE International Conference on Electronics Technology, ICET 2019 - Chengdu, China Duration: 10 May 2019 → 13 May 2019 |
Publication series
Name | 2019 2nd International Conference on Electronics Technology, ICET 2019 |
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Conference
Conference | 2nd IEEE International Conference on Electronics Technology, ICET 2019 |
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Country/Territory | China |
City | Chengdu |
Period | 10/05/19 → 13/05/19 |
Keywords
- Double decision
- Real-time correlation
- Satellite-based coordinate system
- Space objects
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Dong, S., Chen, D., Yang, P., & Zhang, Y. (2019). A real-time correlation method for space objects in satellite-based coordinate system. In 2019 2nd International Conference on Electronics Technology, ICET 2019 (pp. 263-268). Article 8839380 (2019 2nd International Conference on Electronics Technology, ICET 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ELTECH.2019.8839380