Issue |
J. Space Weather Space Clim.
Volume 8, 2018
Developing New Space Weather Tools: Transitioning fundamental science to operational prediction systems
|
|
---|---|---|
Article Number | A39 | |
Number of page(s) | 21 | |
DOI | https://doi.org/10.1051/swsc/2018025 | |
Published online | 24 August 2018 |
Research Article
An operational solar wind prediction system transitioning fundamental science to operations
1
National Space Science Center, Chinese Academy of Sciences, Beijing, PR China
2
School of Earth and Space Sciences, University of Science and Technology of China, Hefei, Anhui, PR China
3
School of Astronomy and Space Sciences, University of Chinese Academy of Sciences, Beijing, PR China
* Corresponding author: wangjingjing@nssc.ac.cn
Received:
5
June
2017
Accepted:
29
June
2018
We present in this paper an operational solar wind prediction system. The system is an outcome of the collaborative efforts between scientists in research communities and forecasters at Space Environment Prediction Center (SEPC) in China. This system is mainly composed of three modules: (1) a photospheric magnetic field extrapolation module, along with the Wang-Sheeley-Arge (WSA) empirical method, to obtain the background solar wind speed and the magnetic field strength on the source surface; (2) a modified Hakamada-Akasofu-Fry (HAF) kinematic module for simulating the propagation of solar wind structures in the interplanetary space; and (3) a coronal mass ejection (CME) detection module, which derives CME parameters using the ice-cream cone model based on coronagraph images. By bridging the gap between fundamental science and operational requirements, our system is finally capable of predicting solar wind conditions near Earth, especially the arrival times of the co-rotating interaction regions (CIRs) and CMEs. Our test against historical solar wind data from 2007 to 2016 shows that the hit rate (HR) of the high-speed enhancements (HSEs) is 0.60 and the false alarm rate (FAR) is 0.30. The mean error (ME) and the mean absolute error (MAE) of the maximum speed for the same period are −73.9 km s−1 and 101.2 km s−1, respectively. Meanwhile, the ME and MAE of the arrival time of the maximum speed are 0.15 days and 1.27 days, respectively. There are 25 CMEs simulated and the MAE of the arrival time is 18.0 h.
Key words: Forecasting / Solar Wind / Coronal Mass Ejection (CME) / Space weather
© J. Wang et al., Published by EDP Sciences 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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