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The AMDAR data used in this paper are received by the National Meteorological Information Center through a Global Telecommunication System from the International Exchange Station via China Integrated Meteorological Information Service System (CIMISS)- national integrated meteorological information sharing platform. The amount of data collected from aircraft has been increasing in recent years. By the end of December 2019, the CIMISS database had recorded 1 million daily observations from aircraft. Fig. 1 shows the global distribution of AMDAR data at 12UTC on August 12, 2019.
AMDAR data are mainly distributed on the routes to and from the United States, Western Europe, East Asia, Australia, and South Africa. 64% of the data are from routes with length of less than 8000 meters, 21% from routes with length of 8000~10000 meters and 15% from routes with length of 10000 meters or more. Most of the data on these routes are from altitudes above 10, 000 meters (Fig. 1), about 36% of the total data. There are no aircraft data south of 60° S, and the vertical distribution is from the ground to 200 hPa. In terms of observation frequency, the climbing stage is observed every 35 seconds, the cruise stage is observed every 3 minutes, and the descent stage is observed every 60 seconds.
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The ERA5 reanalysis made available by the ECMWF is a new reanalysis product at a high resolution replacing ERA-Interim (EI) since September 1, 2019 (Hans et al. [27]). The ERA5 has a horizontal resolution of ~0.25° and higher temporal (hourly analysis) output resolution. Besides the higher temporal and spatial resolution compared to EI, the ERA5 has a higher number of vertical levels (137 versus 60 in EI). In this paper, ERA5 temperature reanalysis data are used as the reference field. ERA5 data are interpolated from 0.25 degrees to 1-degree spatial resolution.
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The difference between the ERA5 and temperature observations is used to calculate the bias and standard deviation. The statistical period corresponded to August 1-31, 2019. The method of the AMDAR blacklist design used in this paper is based on: (a) NCEP data quality monitoring statistical report (https://www.nco.ncep.noaa.gov/pmb/qap/amdar/). For each aircraft, based on the difference between observed values of the AMDAR temperature data and ERA5 reanalysis, the bias and standard deviation are computed and compared with the given threshold of data quality monitoring. The NCEP quality monitoring evaluation indexes included gross error, bias, standard deviation and root mean square error (RMSE) (Table 1); (b) Pre-quality controls for the AMDAR temperature observations, mainly including internal consistency checks, extreme value checks, time consistency and space consistency checks (Table 2).
Pressure level Sample number Gross error Bias Std RMSE >700 hPa >=30 150℃ 3℃ 3℃ 4℃ 300-700 hPa >=50 100℃ 2℃ 2℃ 3℃ < =300 hPa >=50 10℃ 2℃ 2℃ 3℃ Table 1. Threshold setting of AMDAR blacklist.
QC Suspicious number Extremum check NS>30 Internal consistency NS>30 Time consistency NS>30 Spatial consistency NS>30 Table 2. Pre-quality control of AMDAR.
The bias is calculated as:
$$ {\rm{Bia}}{{\rm{s}}_i} = \frac{1}{N}\sum\limits_{j = 1}^N {({O_{ij}} - {B_{ij}})} $$ (1) where Biasi is the average difference between the temperature observations of the aircraft with the ith identification number and ERA5 in the statistical period, Oij is the jth observation of the aircraft with the i identification number in the statistical period, and Bij is the interpolation of ERA5 reanalysis in the same time window corresponding to the observation position of the ith identification number. N is the total number of observation records of the i th aircraft during the statistical period. Stdi is the standard deviation of the temperature of the ith aircraft, and RMSEi is the RMSE between the observation and the reference field.
The standard deviation is calculated as:
$$ {\rm{St}}{{\rm{d}}_i} = \sqrt {\frac{1}{N}\sum\limits_{j = 1}^N {{{({\rm{Bia}}{{\rm{s}}_i} - {\rm{mean}}({\rm{Bia}}{{\rm{s}}_i}))}^2}} } $$ (2) The RMSE is calculated as:
$$ {\rm{RMS}}{{\rm{E}}_i} = \sqrt {\frac{1}{N}\sum\limits_{j = 1}^N {{{({O_{ij}} - {B_{ij}})}^2}} } $$ (3) When the sample number of observations for each aircraft is greater than the given number, the bias, standard deviation and RMSE are calculated.
AMDAR blacklist rules are formulated as follows:
(1) The ith aircraft will be blacklisted if its STDi or RMSEi are greater than the threshold in Table 1, or
(2) When the monthly count of failed inspections of the ith aircraft in any check (indicated by NS) is greater than 30, it will enter the blacklist.
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In this paper, we use the global CMA-GFS numerical weather forecast model independently developed and applied by the Chinese Meteorological Administration (Xue et al. [28]). This model has a horizontal resolution of 0.25°, 87 vertical layers, and the top layer reaches 0.1hPa. The assimilation system is the four-dimensional variational assimilation (Zhang et al. [29]), and the analysis variables are non-equilibrium dimensionless pressure, flow function, non-equilibrium velocity potential and specific humidity. The assimilation data include sounding, ground report, ship, AMDAR, and NOAA15, 18, 19, Metop-A, B and Fengyun series 3 and 4 (FY3, 4). Two groups of experiments are designed to research the influence of blacklisted data on the analysis and forecast. Experiment 1 (Exp1) is used as the control experiment to assimilate all the data described above including all the AMDAR data, and Experiment 2 (Exp2) is used as the influence experiment to assimilate the above data and the AMDAR data after blacklist screening. The experiment period is from September 1 to September 30, 2019. The forecast period is 00UTC per day, with a 10-day forecast. The Globe is divided into four study areas: the Northern Hemisphere (20-90 degrees north), the Southern Hemisphere (20-90 degrees south), the tropics (20 degrees south to 20 degrees north), and East Asia (70-145 degrees east and 15-65 degrees north).