Assimilating Radiance Observations

Assimilating radiance observations is more complicated than assimilating conventional observations as radiances are not state variables. We need a observation operator to transform the model variables to brightness temperature. GSI uses the Community Radiative Transfer Model (CRTM, Liu et al. 2008) as an operator of the radiance observations that calculates the brightness temperature simulated by the model in order to compare it with the observations from satellite sensors.

The CRTM radiative transfer model

The CRTM is a fast radiative transfer model that was jointly developed by the NOAA Center for Satellite Applications and Research and the Joint Center for Satellite Data Assimilation (JCSDA). It is a model widely used by the remote sensing community as it is open source and publicly available. In addition, it is used for satellite instrument calibration (Weng et al. 2013; Iacovazzi et al. 2020; Crews et al. 2021), and to generate retrievals from satellite observations (Boukabara et al. 2011; H. Hu et al. 2019; H. Hu and Han 2021). It is also used as an operator of observations as part of the assimilation of satellite radiances (Tong et al. 2020; Barton et al. 2021).

The CRTM is capable of simulating microwave, infrared and visible radiances, under clear and cloudy sky conditions, using atmospheric profiles of pressure, temperature, humidity and other species such as ozone. Recently Cutraro, Galligani, and Skabar (2021) evaluated their use in Argentina with good results in simulating GOES-16 observations.

CRTM is a sensor-oriented radiative transfer model, i.e. it contains pre-calculated parameterizations and coefficient tables specifically for operational sensors. It includes modules that calculate thermal radiation from gaseous absorption, absorption and scattering by aerosols and clouds, and emission and reflection of radiation by the Earth’s surface. The inputs of CRTM include atmospheric state variables, e.g., temperature, water vapor, pressure, and ozone concentration in user-defined layers, and surface state variables and parameters, including emissivity, surface temperature, and wind.

CRTM is capable to simulate satellite observations from the state of the atmosphere. This is necessary during the assimilation process but is also used to verify the accuracy and errors of radiance observations.

The necessary calculations to simulate observations has a very high computational cost as it requires transposing a high dimensional matrix and the minimization of a cost function. This \(K^{*}\) matrix is constructed from the partial derivatives of the radiances with respect to geophysical parameters. CRTM performs these calculations very quickly so it can be used in operational contexts.

To obtain fast results, CRTM applies certain simplifications and approximations when solving the radiative transfer equation. First, it assumes that the Earth’s atmosphere consists of plane-parallel and homogeneous layers in thermodynamic equilibrium and where three-dimensional and polarization effects can be ignored.

In the context of clear skies, it is also assumed that there is no scattering and only the absorption of gases in the atmosphere is considered. In cloudy skies, the scattering generated by clouds is included. In the latter case, the radiative transfer equation cannot be solved analytically and numerical solutions are used.

Specific configuration

The assimilation of radiance observations is controlled with the satinfo file and the GSI namelist. Let’s check the global_satinfo.txt file we get as an example:

!sensor/instr/sat      chan iuse  error  error_cld  ermax   var_b    var_pg  icld_det icloud iaerosol
 amsua_n15               1   1    3.000   20.000    4.500   10.000    0.000     -2      1     -1
 amsua_n15               2   1    2.200   18.000    4.500   10.000    0.000     -2      1     -1
 amsua_n15               3   1    2.000   12.000    4.500   10.000    0.000     -2      1     -1
 amsua_n15               4   1    0.600    3.000    2.500   10.000    0.000     -2      1     -1
 amsua_n15               5   1    0.300    0.500    2.000   10.000    0.000     -2      1     -1
 amsua_n15               6  -1    0.230    0.300    2.000   10.000    0.000     -2      1     -1
 amsua_n15               7   1    0.250    0.250    2.000   10.000    0.000     -2      1     -1
 amsua_n15               8   1    0.275    0.275    2.000   10.000    0.000     -2      1     -1
 amsua_n15               9   1    0.340    0.340    2.000   10.000    0.000     -2      1     -1
 amsua_n15              10   1    0.400    0.400    2.000   10.000    0.000     -2      1     -1
 amsua_n15              11  -1    0.600    0.600    2.500   10.000    0.000     -2      1     -1
 amsua_n15              12   1    1.000    1.000    3.500   10.000    0.000     -2      1     -1
 amsua_n15              13   1    1.500    1.500    4.500   10.000    0.000     -2      1     -1
 amsua_n15              14  -1    2.000    2.000    4.500   10.000    0.000     -2      1     -1
 amsua_n15              15   1    3.500   18.000    4.500   10.000    0.000     -2      1     -1
 hirs3_n17               1  -1    2.000    0.000    4.500   10.000    0.000     -1     -1     -1

The file includes a line for each sensor/satellite and each channel (chan). Usually you will change the iuse and error columns to configure the assimilation of each channel. The options for iuse are:

  • -2 do not use
  • -1 monitor if diagnostics produced
  • 0 monitor and use in QC only
  • 1 use data with complete quality control
  • 2 use data with no airmass bias correction
  • 3 use data with no angle dependent bias correction
  • 4 use data with no bias correction

Defining the observation error is one of the difficult part of the assimilation process, so I usually keep the GFS values to be on the safe side.

To successfully assimilate radiances using the EnKF method it is critical to save in the diag files the vertical location of each radiance observation that is estimated as the model level at which its weight function1 computed by CRTM maximize. It is also important to save the predictors calculated during the bias correction step.

Here is an incomplete list of parameters in the GSI and ENKF namelists.

GSI namelist

Parameter Description Needed value
passive_bc option to turn on bias correction for passive (monitored) channels .true.
use_edges option to exclude radiance data on scan edges .false.
lwrite_predterms option to write out actual predictor terms instead of predicted bias to the radiance diagnostic files .true.
lwrite_peakwt option to write out the approximate pressure of the peak of the weighting function for satellite data to the radiance diagnostic .true.
emiss_bc option to turn on emissivity bias predictor .true.

This namelist will also includes a list with the type of observations and the name of the bufr file for each one (dfile).

ENKF namelist

Parameter Description Needed value
adp_anglebc turn off or on the variational radiance angle bias correction .true.
angord order of polynomial for angle bias correction 4
use_edges logical to use data on scan edges (.true.=to use) .false.
emiss_bc If true, turn on emissivity bias correction .true.
upd_pred bias update indicator for radiance bias correction; 1.0=bias correction coefficients evolve 1

This namelist will also includes a list with the type of observations and the name of each one inside GSI. For example amsua_n15 represent the observations of the AMSU-A sensor on board NOAA-15.

Observation errors and quality control

The preprocessing and quality control of the data is an essential step in the assimilation of radiances and depends on each sensor and channel. This process includes spatial thinning, bias correction, and in clear-sky applications, the detection of cloudy sky observations.

Thinning

During the thinning process the observations to be assimilated are chosen based on their distance to the model grid points, the quality of the observation (based on available data quality information) and the number of available channels (for the same pixel and sensor). The thinning algorithm determines the quality of each observation based on the available information about the channels and their known errors, the type of surface below each pixel (preferring observations over the sea to those over land or snow) and predictors that give information about the quality of the observations (M. Hu et al. 2018). By applying the thinning we avoid incorporating information from smaller scale processes than the model can not represent and to reduce the error correlation of the observations from the same sensor.

The thinning resolution is configured in the GSI namelist:

In this case we have 3 possible mesh size in kilometers: dmesh(1)=120.0, dmesh(2)=60.0, dmesh(3)=10.0. We define which resolution to use for each sensor in the dthin column. Here amsua_n15 will use a thinning of 60 km and abi_g16 a thinning of 10 km.

 &OBS_INPUT
   dmesh(1)=120.0, dmesh(2)=60.0, dmesh(3)=10.0, time_window_max=0.5,ext_sonde=.true.,
 /
OBS_INPUT::
!  dfile          dtype       dplat     dsis                 dval    dthin dsfcalc
   amsuabufr      amsua       n15       amsua_n15           10.0     2     0
   amsuabufr      amsua       n18       amsua_n18           10.0     2     0
   amsuabufr      amsua       n19       amsua_n19           10.0     2     0
   amsuabufr      amsua       metop-a   amsua_metop-a       10.0     2     0
   amsuabufr      amsua       metop-b   amsua_metop-b       10.0     2     0
   airsbufr       amsua       aqua      amsua_aqua           5.0     2     0
   abibufr        abi         g16       abi_g16              1.0     3     0

If the value of dthin is:

  • an integer less than or equal to zero, no thinning is needed
  • an integer larger than zero, this kind of radiance data will be thinned using the mesh size defined as dmesh (dthin).

Bias correction

After the thinning, a bias correction is applied. The bias correction methodology implemented in GSI depends on thermodynamic characteristics of the air and on the scan angle (Zhu et al. 2014). It is computed as a linear polynomial of N predictors \(p_i(x)\), with associated coefficients \(beta_i\). Therefore, the bias-corrected brightness temperature (\(BT_{cb}\)) can be obtained as:

\[\mathrm{\mathit{BT_{cb}} =\mathit{ BT} + \sum_{i = 0}^{N} \beta_i p_i (x)}\]

The polynomial has a constant bias correction term (\(p_0 = 1\)) while the remaining terms and their predictors are the cloud liquid water (CLW) content, the temperature laps rate, the square of the temperature laps rate, and the sensitivity to the surface emissivity to account for the difference between land and sea. The scan angle-dependent bias is modeled as a polynomial of 4\(^\circ\) order (Zhu et al. 2014).

In the GSI system, the coefficients \(\beta_i\) are trained using a variational estimation method that generates the \(\beta_i\) that provides the best fit between the simulation and the observations. The EnKF step also calculate the coefficients for the assimilation.

It is important to evaluate the training of the coefficients and the performance of the bias correction. One way to train the coefficients according to Zhu et al. (2014) is to run the assimilation cycles for a long period of time, updating the coefficients at each cycle. While is possible to start the training with coefficients equal to zero, using the coefficients the GFS generates can help to speed up the process.

To check if the coefficients are correctly trained we can analysed the evolution of the different coefficients for each sensor and channel with time. As an example, here we show the coefficients for AMSU-A on board NOAA-15. Following Zhu et al. (2014), we expected the coefficients to reach a stable range of values after a certain period of time, this is evident for channel 4, 5, 6 and 8 but we see a continuous variation in channels 7 and 9.

Line chart showing the evolution of the coefficients over time for channels 4 to 9 of AMSU-A. For some of the channels the coefficient values are more or lest constant.

Bias correction coefficients as function of time (days) for the training and experiment period. Channels 4 to 9 of AMSU-A on NOAA-15.

Using the resulting coefficients from the training period it is also important to check the impact of the bias correction. An easy way to see this is to calculate the mean difference between the observations and the first-guess (OmB) before and after the correction of the bias for each sensor. In the next figure there is an evident improvement as the mean OmB after the BC is now centered around zero and its standard deviation is smaller. This indicate that the BC correction worked as expected.

Mean difference between observations and first-guess after and before the correction of the bias calculate over a 3 days period for each sensor.

The training of the coefficients requires a lot of computational resources and can be challenging for observations from polar satellites used in regional applications. The reason for this is that the observations are only available 1 or 2 times a day, making the training a slow process. It is important to check that GSI is not penalizing the coefficients when there are no observations available.

The coefficients are saved in the satbias file, a plain text file that looks like this:

    1 amsua_n15                1   0.423099E+00   0.481606E+06   999
        2.680195    0.000000    0.001042    0.004029    0.228152    0.000000    0.000000   -0.009346    3.972107    2.986645
       -4.770297   -1.960179
    2 amsua_n15                2   0.235695E+00   0.519067E+06   999
        1.704236    0.000000    0.010259   14.889464   -3.720292    0.000000    0.000000   -0.011583    3.896762    9.125687
       -4.712555   -1.727947
    3 amsua_n15                3   0.150663E+01   0.593685E+06   999
        1.771621    0.000000    0.009938    0.507936   -0.328143    0.000000    0.000000   -0.013321   -2.458213   -0.946619
       -1.233838    0.234034
    4 amsua_n15                4   0.342465E+01   0.104715E+07   999
       -0.123787    0.000000    0.013865    0.050019   -0.037143    0.000000    0.000000    0.007463   -0.460992   -0.542148
       -0.876047   -0.110968
    5 amsua_n15                5   0.445149E+01   0.112750E+07   999
        0.332174    0.000000    0.007298    0.010457   -0.071543    0.000000    0.000000   -0.009200    0.827698   -0.965067
       -1.350357    0.100073

So, for each sensor and satellite and each channel there are 12 coefficients that are updated in each assimilation cycle. I recommend to save these files to analyses the BC process. Radiance bias correction terms are as follows:

  1. global offset
  2. zenith angle predictor, is not used and set to zero now
  3. cloud liquid water predictor for clear-sky microwave radiance assimilation
  4. square of temperature laps rate predictor
  5. temperature laps rate predictor
  6. cosinusoidal predictor for SSMI/S ascending/descending bias
  7. sinusoidal predictor for SSMI/S
  8. emissivity sensitivity predictor for land/sea differences
  9. fourth order polynomial of angle bias correction
  10. third order polynomial of angle bias correction
  11. second order polynomial of angle bias correction
  12. first order polynomial of angle bias correction

On the other hand the predictors are saved in the diag files (see the Undestanding diag files section).

Cloud detection

The cloud pixel detection methodology depends on the wavelength of the observations. For microwave radiances, potentially cloud-contaminated observations are detected using scattering and Liquid Water Path (LWP) indices calculated from differences between different channels of each sensor (Weston et al. 2019; Zhu et al. 2016). For infrared channels, cloud contaminated observations are detected using the transmittance profile calculated by the CRTM model. In addition, GSI checks the difference between the observations and the simulated brightness temperature to detect cloudy pixels.

A particular case is the ABI observations since the cloud mask (level 2 product) available at the same resolution as the observations is used. This cloud mask is generated by combining information from 8 channels of the ABI sensor from the spatial and temporal point of view.

Other quality controls

The GSI quality control filters out those observations from channels close to the visible range over water surfaces with a zenith angle greater than 60\(^{\circ}\) to reject those observations that could be contaminated by reflection. For infrared and microwave observations it also performs an emissivity check to detect observations contaminated by surface effects. Finally, a gross check is applied, i.e. the difference between the observation and the observation simulated by the model is compared with a predefined threshold depending on the observation error to reject erroneous observations.

References

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Cutraro, Federico, Victoria Sol Galligani, and Yanina García Skabar. 2021. “Evaluation of Synthetic Satellite Images Computed from Radiative Transfer Models over a Region of South America Using WRF and GOES-13/16 Observations.” Quarterly Journal of the Royal Meteorological Society 147 (738): 2988–3003. https://doi.org/10.1002/qj.4111.
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Footnotes

  1. The weight function of each channel corresponds to the change in transmittance with height and its maximum describes the layer of the atmosphere from which the radiation captured by the channel was emitted. Multispectral sensors have good vertical coverage and are capable of capturing from the lower troposphere to the lower stratosphere.↩︎