- Tytuł:
- Second Earth Orientation Parameters Prediction Comparison Campaign (2nd EOP PCC): Overview
- Autorzy:
-
Śliwińska, Justyna
Kur, Tomasz
Wińska, Małgorzata
Nastula, Jolanta
Dobslaw, Henryk
Partyka, Aleksander - Powiązania:
- https://bibliotekanauki.pl/articles/2174949.pdf
- Data publikacji:
- 2022
- Wydawca:
- Polska Akademia Nauk. Centrum Badań Kosmicznych PAN
- Tematy:
-
earth orientation parameters
length of day
UT1-UTC
universal time
predictions - Opis:
- Precise positioning and navigation on the Earth’s surface and in space require accurate earth orientation parameters (EOP) data and predictions. In the last few decades, EOP prediction has become a subject of increased attention within the international geodetic community, e.g., space agencies, satellite operators, researchers studying Earth rotation dynamics, and users of navigation systems. Due to this fact, many research centres from around the world have developed dedicated methods for the forecasting of EOP. An assessment of the various EOP prediction capabilities is currently being pursued in the frame of the Second Earth Orientation Parameters Prediction Comparison Campaign (2nd EOP PCC), which began in September 2021 and will be continued until the end of the year 2022. The new campaign was prepared by the EOP PCC Office run by Centrum Badań Kosmicznych Polskiej Akademii Nauk (CBK PAN) in Warsaw, Poland, in cooperation with GeoForschungsZentrum (GFZ) and under the auspices of the International Earth Rotation and Reference Systems Service (IERS). In this paper, we provide an overview of the 2nd EOP PCC five months after its start. We discuss the technical aspects and present statistics about the participants and valid prediction files received so far. Additionally, we present the results of preliminary comparisons of different reference solutions with respect to the official IERS 14 C04 EOP series. Root mean square values for different solutions for polar motion, length of day, and precession-nutation components show discrepancies at the level from 0.04 to 0.36 mas, from 0.01 to 0.10 ms, and from 0.01 to 0.18 mas, respectively.
- Źródło:
-
Artificial Satellites. Journal of Planetary Geodesy; 2022, 57, Special Issue 1; 237--253
2083-6104 - Pojawia się w:
- Artificial Satellites. Journal of Planetary Geodesy
- Dostawca treści:
- Biblioteka Nauki
Artykuł