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Adaptive Observation Error Inflation for Assimilating All-Sky Satellite Radiance

Masashi Minamide Department of Meteorology and Atmospheric Science, and Center for Advanced Data Assimilation and Predictability Techniques, The Pennsylvania State University, University Park, Pennsylvania

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Fuqing Zhang Department of Meteorology and Atmospheric Science, and Center for Advanced Data Assimilation and Predictability Techniques, The Pennsylvania State University, University Park, Pennsylvania

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Abstract

An empirical flow-dependent adaptive observation error inflation (AOEI) method is proposed for assimilating all-sky satellite brightness temperatures through observing system simulation experiments with an ensemble Kalman filter. The AOEI method adaptively inflates the observation error when the absolute difference (innovation) between the observed and simulated brightness temperatures is greater than the square root of the combined variance of the uninflated observational error variance and ensemble-estimated background error variance. This adaptive method is designed to limit erroneous analysis increments where there are large representativeness errors, as is often the case for cloudy-affected radiances, even if the forecast model and the observation operator (the radiative transfer model) are perfect. The promising performance of this newly proposed AOEI method is demonstrated through observing system simulation experiments assimilating all-sky brightness temperatures from GOES-R (now GOES-16) in comparison with experiments using an alternative empirical observation error inflation method proposed by Geer and Bauer. It is found that both inflation methods perform similarly in the accuracy of the analysis and in the containment of potential representativeness errors; both outperform experiments using a constant observation error without inflation. Besides being easier to implement, the empirical AOEI method proposed here also shows some advantage over the Geer–Bauer method in better updating variables at large scales. Large representative errors are likely to be compounded by unavoidable uncertainties in the forecast system and/or nonlinear observation operator (as for the radiative transfer model), in particular in the areas of moist processes, as will be the case for real-data cloudy radiances, which will be further investigated in future studies.

© 2017 American Meteorological Society. For information regarding reuse of this content and general copyright information, consult the AMS Copyright Policy (www.ametsoc.org/PUBSReuseLicenses).

Corresponding author e-mail: Fuqing Zhang, fzhang@psu.edu

Abstract

An empirical flow-dependent adaptive observation error inflation (AOEI) method is proposed for assimilating all-sky satellite brightness temperatures through observing system simulation experiments with an ensemble Kalman filter. The AOEI method adaptively inflates the observation error when the absolute difference (innovation) between the observed and simulated brightness temperatures is greater than the square root of the combined variance of the uninflated observational error variance and ensemble-estimated background error variance. This adaptive method is designed to limit erroneous analysis increments where there are large representativeness errors, as is often the case for cloudy-affected radiances, even if the forecast model and the observation operator (the radiative transfer model) are perfect. The promising performance of this newly proposed AOEI method is demonstrated through observing system simulation experiments assimilating all-sky brightness temperatures from GOES-R (now GOES-16) in comparison with experiments using an alternative empirical observation error inflation method proposed by Geer and Bauer. It is found that both inflation methods perform similarly in the accuracy of the analysis and in the containment of potential representativeness errors; both outperform experiments using a constant observation error without inflation. Besides being easier to implement, the empirical AOEI method proposed here also shows some advantage over the Geer–Bauer method in better updating variables at large scales. Large representative errors are likely to be compounded by unavoidable uncertainties in the forecast system and/or nonlinear observation operator (as for the radiative transfer model), in particular in the areas of moist processes, as will be the case for real-data cloudy radiances, which will be further investigated in future studies.

© 2017 American Meteorological Society. For information regarding reuse of this content and general copyright information, consult the AMS Copyright Policy (www.ametsoc.org/PUBSReuseLicenses).

Corresponding author e-mail: Fuqing Zhang, fzhang@psu.edu

1. Introduction

Assimilation of all-sky satellite-measured observations, including cloud-affected radiance, are still quite limited, though usage of clear-sky satellite observations has been widely spread and has greatly improved the accuracy of numerical weather predictions. Geer and Bauer (2011, hereafter GB11) attributed part of the difficulty in assimilating cloudy-affected microwave radiances to their boundedness and heteroscedasticity, as well as strong nonlinear relationship to atmospheric states. These characteristics can severely degrade the impacts of data assimilation, by causing systematic errors, bias, representative errors, and errors in modeling convective-scale phenomena through forecasting models as well as microscale characteristics of clouds through forwarding models (Pires et al. 2010). Further difficulty in all-sky assimilation lies in the discontinuity between clear- and cloudy-sky radiances. Predicting the exact location of clouds is challenging because of either practical or intrinsic limits of atmospheric predictability (Lorenz 1969, 1982, 1996; Zhang et al. 2002, 2003, 2007). Practical predictability refers to the limit of prediction given the current realistic uncertainties in either the initial conditions or forecast model while intrinsic predictability refers to the fundamental limit in the atmospheric prediction with a nearly perfect model and nearly prefect initial conditions (Lorenz 1996; Melhauser and Zhang 2012; Tao and Zhang 2015; Sun and Zhang 2016). Large departures between the clear-sky surface temperature and cloud-top temperature can occur far more frequently than predicted by assuming Gaussianity in the background and observation error covariance. Many researchers reported that mismatches of the sky type (i.e., clear or cloudy) between the first guesses and observations often leads to a fat-tail distribution in the first-guess departures (e.g., GB11; Tavolato and Isaksen 2015).

Nevertheless, there are great potentials of assimilating cloudy-radiance observations for numerical weather prediction. For example, Otkin (2010, 2012) showed that direct assimilation of infrared cloudy radiances can improve prediction of convective-scale severe storms through strict quality control. Tavolato and Isaksen (2015) assessed the methodology to give relatively smaller weight to the observations with larger first-guess departures, and/or by inflating the observation errors. Though large observation errors may artificially suppress the analysis increments, they showed that the incremental accumulation of those small impacts can be large enough to make a distinguishable improvement from not using the cloudy radiances at all.

GB11 demonstrated that satellite radiance observations have apparent heteroscedasticity, which means that the errors are not universal but vary spatially and among different variables. It is evident that there are more uncertainties in dealing with cloudy radiances than their clear-sky counterparts, but errors might also vary under different atmospheric flow conditions (e.g., clear-sky radiance observation can result in large first-guess departures if the model forecasts a cloudy sky). A common way to estimate observation error variances is to use a statistical relation (Parrish and Derber 1992; Dee 1995):
e1
where is the innovation vector (i.e., the first-guess departure), is the background variance, and is the observation error. Using Eq. (1) and the cloud amount, GB11 formulated climatological observation errors. As an extension of GB11, Okamoto et al. (2014), and Harnisch et al. (2016) proposed the use of a climatological error model for infrared radiances as a function of different cloud-affected parameters.

In this study, we assess the impacts of an adaptive observation error inflation (AOEI) technique for assimilating all-sky satellite brightness temperatures with the ensemble-based data assimilation framework first introduced in Zhang et al. (2016, hereafter ZMC16). Since the inner-core regions of tropical cyclones are mostly covered by clouds, existing studies on assimilation of satellite radiances for tropical cyclones have been mostly focused on the clear-sky observations away from the tropical cyclone cores (e.g., Wang et al. 2015; Zou et al. 2013, 2015). The impacts of AOEI were tested for the matured phase of Hurricane Karl (2010). This article is organized as follows. Model and experimental designs are described in section 2. The AOEI method is formulated and discussed in section 3. The performance of AOEI in comparison with existing methodologies is given in section 4. Conclusions are provided in section 5.

2. Model configuration and experimental design

As in ZMC16, we used the ensemble Kalman filter (EnKF) data assimilation system (Zhang et al. 2009, 2011; Weng and Zhang 2012, 2016) developed at The Pennsylvania State University (PSU), which is built around the Weather Research and Forecasting (WRF) Model (version 3.6.1) (Skamarock et al. 2008) and the Community Radiative Transfer Model (CRTM). This CRTM-integrated framework enables us to directly assimilate multiple channel brightness temperatures with high temporal and spatial resolution into PSU WRF-EnKF. As in ZMC16, there are three two-way nested model domains with grid spacings of 27, 9, and 3 km, respectively (refer to supplemental Fig. 1 of ZMC16 for domain configuration; the finest 3-km domain is shown and examined in all subsequent figures). All the domains used 61 levels with the model top at 50 hPa in a stretched vertical grid. For model physics, we utilized the WRF single-moment 6-class mixed-phase microphysics scheme (WSM6; Hong and Lim 2006), the Yonsei University planetary boundary scheme (Hong et al. 2006), the Tiedtke cumulous parameterization scheme (Tiedtke 1989), and the Rapid Radiative Transfer Model (RRTM) longwave and shortwave radiation schemes (Iacono et al. 2008). Cumulous parameterization was only applied to the coarsest (27 km) domain. Since nearly all convective activities associated with Hurricane Karl was within the finest (3 km) domain, the choice of whether or not using cumulous parameterization on the intermediate resolution (9 km) domain should not affect the results. CRTM is a rapid forward model to calculate brightness temperatures for the satellite data assimilation (Han et al. 2006, 2007; Weng 2007). The simulated brightness temperatures were computed with the successive order of interaction (SOI) forward solver (Heidinger et al. 2006) using the OPTRAN code from CRTM. The standard profiles for the tropical region defaulted in CRTM were used above the model top.

We conducted the perfect-model observing system simulation experiments (OSSEs) with the same 60 initial ensemble perturbations and the reference truth Karl simulation as the perfect-model OSSEs of ZMC16 (see configurations above). Hurricane Karl progressed westward across the Bay of Campeche before making landfall on 17 September. We computed brightness temperatures for hypothetical future GOES-R (now GOES-16) Advanced Baseline Imager [water vapor channels: channels 8, 9, and 10, wavelengths are 6.19, 6.95, and 7.34 μm, respectively; and window channel: channel 14, wavelength is 11.2 μm, refer to Schmit et al. (2005)] every 10 min. Synthetic observations were created by combining those simulated water vapor brightness temperatures (BTs) and assumed Gaussian-distributed universal, constant observation error with a standard deviation of 3 K, which includes both instrumental and representativeness errors. Those synthetic BT observations were thinned with the same channel selection method as employed in ZMC16, which retains for assimilation clear-sky radiances in all three water vapor channels (8, 9, and 10) in the clear-sky region and only the cloudy-sky radiances in channel 8. In addition to BTs, synthetic tropical cyclone minimum sea level pressure (SLP) observations available every hour were derived from the truth simulation with an assumed observation error of 3 hPa. The experiment that assimilated BT with AOEI and minimum SLP is hereafter called AOEI.

Slightly different from ZMC16, which employed a radius of influence of 30 km for hydrometeors and 200 km for other variables, this study utilizes the successive covariance localization (SCL) method proposed by Zhang et al. (2009), which allows better capturing convective-scale structures with a smaller covariance localization radius while updating vortex-scale structure with a larger covariance localization distance. Here the brightness temperatures are assimilated every 12 km by 12 km with a 30-km radius of influence and every 18 km by 18 km with a 300-km radius of influence. No vertical covariance localization is used in this study and ZMC16, while the covariance relaxation method of Zhang et al. (2004) with coefficient = 0.5 is applied. The assimilation was initialized at 2200 UTC 16 September and continued until 0600 UTC 17 September 2010 with brightness temperatures assimilated every 10 min and minimum SLP assimilated every hour. Despite using different radii of influence via SCL, the AOEI experiment performed very similarly to the experiment of ZMC16 that showed great potentials in assimilating all-sky radiance observations. The current study focuses on the methodology and effectiveness of using AOEI.

3. The adaptive observation error inflation (AOEI) algorithm

a. Error distribution

Consistent with the well-established methodology in estimating observation errors (Parrish and Derber 1992; Dee 1995; Desroziers et al. 2005; GB11; Li et al. 2009), the error statistics [Eq. (1)] in the EnKF framework can be modeled as
e2
where is the observation operator (linear or nonlinear) and is the ensemble perturbation vector of model state variables (Evensen 2003). Thus, is the ensemble perturbation vector in the observation space.

Figure 1c shows an example of the spatial distribution of the diagonal term (variance) of the ensemble-estimated forecast error covariances for the simulated brightness temperatures if observed by GOES-16 ABI channel 8 (6.19 μm) for Hurricane Karl at 2200 UTC 16 September (the verifying truth at this same time is shown in Fig. 1a just before the start of the initial EnKF assimilation of brightness temperature). The flow dependency of error distribution can be evidenced from Fig. 1b, which shows the squares of the first-guess departure (or innovation = observation − prior): the regions with larger departures, such as the rainbands in the northwest quadrant of the domain, are corresponding to regions with large background error variances (Fig. 1c). Figure 1d shows that the difference between the observed innovation square () and the summation of observation and forecast error variances () indicating that an optimum statistical relationship in Eq. (2) is likely not satisfied, especially over the cloud-affected areas. As discussed in GB11, such discrepancies that are currently treated in different data assimilation approaches as the observation error may be coming from representativeness errors in either the forecast model and/or from the observation itself. The AOEI method proposed here is trying to mitigate such discrepancies through inflating the observation error as detailed below.

Fig. 1.
Fig. 1.

(a) Simulated brightness temperature from GOES-16 ABI channel 8, (b) the innovation square (), (c) ensemble variance, and (d) the difference between the observed innovation square () and the summation of observation and forecast error variances (), verified at the initial assimilation time at 2200 UTC 16 Sep. Star, circle, square, and triangle markers represent the points shown in Figs. 2 and 8.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

b. Observation error with a nonlinear observation operator

Figure 2 shows the ensemble distribution of the simulated BTs for GOES-16 ABI channel 8 (6.19 μm), column-integrated total hydrometeors, column-integrated total water vapor, and 10-m meridional wind at the selected locations marked in Fig. 1. The thermodynamic variables of hydrometeors and water vapor are more sensitive to the infrared brightness temperature measurements than the 10-m wind speed. The four points (A–D) sampled exemplify for the hurricane outside-of-core, eye, primary rainband, and eyewall regions, respectively. At point A, both the observation and the prior were categorized as in the clear-sky area. The truth is well within one standard deviation from the ensemble mean of BTs and the model state variables at point A (Figs. 2a–d). At the edge of the primary rainband where the ensemble members tend to diverge, the ensemble forecasted BTs in point B displayed a bimodal distribution with one peak typical of (low) cloudy-sky radiance and the other peak typical of (high) clear-sky-regime BT while the ensemble mean is close to the observation (Fig. 2e). Nevertheless, the true amount of water vapor mixing ratio and 10-m meridional wind are away from the range of values simulated by many ensemble members (Figs. 2g,h). Point C represents the hurricane eye (Figs. 2i–l), where the ensemble members are often forecasted as cloudy sky because of the difficulty in precisely capturing the location of the cloud-free (or cloudless) hurricane center in the truth simulation. Correspondingly, many of ensemble members forecasted a much lower BT with a larger amount of hydrometeors than the observation (Fig. 2e). However, though not perfect, the distributions of other model state variables did encompass the truth well approximately within their respective 1σ distribution ranges. Within the eyewall region (point D) where both model and observation tend to simulate strong clouds, the BT was better captured by the ensemble (Fig. 2m) compared to the primary rainband or eye region, but the ensemble distribution of model state variables in the eyewall are not necessarily consistent with BT (Figs. 2n–p). In particular, the true value of hydrometeors was considerably larger than the ensemble mean (Fig. 2n).

Fig. 2.
Fig. 2.

Prior ensemble distributions of the (a),(e),(i),(m) brightness temperature; (b),(f),(j),(n) column-integrated hydrometeors; (c),(g),(k),(o) column-integrated vapor mixing ratio; and (d),(h),(l),(p) the 10-m surface meridional wind. The sky-blue box shows the ensemble distribution, the blue line shows the estimated first-guess distribution based on Gaussian assumption, and the red star shows the verifying truth, for points A, B, C, and D marked in Fig. 1.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

A common practice in treating the inconsistency between the innovation and the prior ensemble spread is to inflate the ensemble covariance. However, the covariance inflation for the prior ensemble state variances may not necessarily inflate properly the ensemble spread in observation space when the observation operators are more nonlinear, which can be further complicated by the rank deficiency due to a limited ensemble size. Because large departures in the observation space do not necessarily correlate with large errors in the model state space, it might be advantageous to treat such uncertainties as part of the observation error for the lack of representativeness, rather than as part of the background error. It is clear that these representative errors may exist even if the forecast model is perfect, without considering errors in either the forecast model (WRF) and/or the radiance forward model (CRTM).

Nonlinearity and rank deficiency can also lead to erroneous analysis increments in a limited-size EnKF data assimilation system. The necessity of dealing with large departures in the observation space can be exemplified in the following thought experiment. Hypothetically, the analysis increments with assimilating one observation through the EnKF update is modeled as follows in a scalar form:
e3
where denotes any variable to be updated whose prior standard deviation is (subscripts and denote analysis and background, respectively), is a BT observation with an assigned random error () of 3 K, and is the simulated observation with the ensemble-estimated standard derivation of . Let be the sea level pressure (SLP) at a model grid point, hypothetically but realistically, be 5 hPa, be 5 K, and the correlation between SLP and BT . If because of the representativeness error there is a mismatch between the cloudy and clear-sky regions for the observed versus simulated BTs (which can be quite common) that leads to a large innovation . Assimilation of this particular observation can result in a SLP analysis increment of 15 hPa. Because of the nonlinearity and sampling error, such innovation and ensemble correlation and the resultant large analysis increment can be highly unrepresentative, which can lead to large imbalance in the EnKF update. The AOEI is designed to limit such representativeness errors in the EnKF analysis increment.

c. Adaptive estimation of observation error variance (AOEI)

More generally, observation error may include instrumental noise and representative error , the latter of which can result from inaccurate interpolation, mismatched scales, and imperfectness in the observation operator (e.g., modeling atmospheric radiative transfer process by CRTM in this study), as well as error due to the nonlinearity of the dynamics and rank deficiency of using a small-size ensemble, that potentially prevent the ensemble (mean and spread) to properly represent the observed phenomena. GB11 reported that the representative error can be much larger than the instrumental noises in satellite BTs. Typical value of instrumental noises is in the order of 1–2 K, while representative errors can be as large as 20 K or bigger.

The empirical AOEI method we proposed can be modeled in the following scalar form for any given BT observation:
e4
where represents the uniform-distributed observation error composed of instrumental noise [refer to Eq. (2), the diagonal term of ] and flow-independent component of representative error ( 3 K in this study). Thus, represents the diagonal term of the flow-dependent in Eq. (2). We set as the empirical lower bound of the observation error since the total observation error variance would not be smaller than that in . With AOEI, the observation error was inflated adaptively when the innovation was too large to be covered by the background variances. The summation of the background and observation error variances will approach the square of the innovation by design, which is a desirable relationship according to Eq. (2).

AOEI is intended to suppress erroneous analysis increments that are induced by the representative and sampling errors, which may also allow gradual transition between clear- and cloudy-sky regions. For example, the large analysis increment in SLP for the hypothetical BT observation in section 3b (with a large first-guess departure) will be limited to only 0.3 hPa with AOEI (instead of 15 hPa without AOEI). This much-reduced analysis increment is likely to maintain better balance, regardless of whether the forecasted sky conditions (clear or cloudy) match with the observation. Although it is expected and unavoidable that sometimes the use of AOEI may artificially suppress the “valid” analysis increments, this disadvantage may be partially compensated by assimilating large volumes of satellite radiance observations that will be available from GOES-16.

d. The alternative Geer–Bauer observation error inflation (GBOEI) method

To further demonstrate the effectiveness of AOEI, we compared the EnKF analysis using the newly proposed technique to those using two other types of observation error representation. The first is to assume observation error was constant ( = 3 K) everywhere including both the clear-air and cloudy/rainy-sky regions with no observation error inflation (hereafter the experiment is referred to as “noOEI”). In the second experiment, the observation error is assumed to be an empirical function of the observed brightness temperature (and thus indirectly clouds) derived from a “climatological” all-sky error distribution using the methodology proposed by GB11 (hereafter the experiment is referred to as “GBOEI”). GB11 argued that heteroscedasticity (i.e., dependence of errors on one or more parameters) of the observation error, which is a part of the representativeness error, can be empirically modeled as a function of cloud amount (which was represented by the horizontally polarized 37-GHz microwave BTs for their study). Their formulation of the observation error used a so-called “symmetric” cloud amount, which is an average of the cloud amount in terms of brightness temperature computed from the observation and the model prior or first guess. The use of symmetric cloud amount will lead to a small observational error where both the observation and the first guess are in clear-sky regime but the observational error increases when either of them is cloud affected.

Here, similar to GB11, we take the BTs of observed and prior simulated BTs to make a symmetric predictor of the cloud-affected radiances for each channel:
e5
where is first-guess (prior) simulated and is observed GOES-16 ABI BT, and is the first-guess (prior)-simulated BT without cloud scattering and cloud emission. We calculated synthetic observations for 1000 times, each with added random observation error, and compared them to the hourly outputs of no-DA (data assimilation) experiment (i.e., 1-day deterministic forecast from the initial ensemble prior mean without any data assimilation) to obtain the error function. The method we adopted here is also similar to that proposed in Okamoto et al. (2014), which defined a parameter to formulate cloud impacts on various channels. They calculated a symmetric difference between the BTs with and without cloud-scattering and cloud-emission calculation, and showed that this parameter can well describe the variations of first-guess departures statistics.
The so-derived climatological error (in standard deviation; absolute value of first-guess departures) modeled as a function of symmetric cloud effects parameter is shown in Figs. 3a, 3c, and 3e. We can see a similar dependence of the observation error on to the dependence on the symmetric cloud amount as shown in Fig. 8 of GB11 and Fig. 7 of Okamoto et al. (2014). A small value of means that both the first-guess prior and the observation are categorized as clear sky, which is generally associated with a smaller observation error. The error peaks at around K and gradually decreases with higher . This pattern is quite reasonable in the sense that the largest errors tend to occur when there is a mismatch of sky types between observation and prior (large first-guess departure), which would fall into the bins for in-between clear and cloudy skies around K. Following GB11 and Okamoto et al. (2014), we prepared a lookup table for the error function , , with the bin size of 2 K in , and total observation error was calculated as follows:
e6
and
e7
where is the default constant observation error variance in the clear-sky region (which is assumed the same as , based on the assumption that the sources of the observation error in the clear-sky region exist uniformly in the domain). For outside the range of the training dataset, we applied the value of at maximum , though the maximum rarely occurred.
Fig. 3.
Fig. 3.

(a),(c),(e) The Geer–Bauer observational error models for the BTs in GOES-16 ABI (a) channel 8, (c) channel 9, and (e) channel 10 used in experiment GBOEI. The standard deviation of first-guess departures is shown by a red solid line, which is modeled as a function of symmetric cloud effect parameter , derived from a 1-day dataset of the no-DA experiment. The gray box shows the number of observations classified into each bin. (b),(d),(f) Innovation statistics, normalized by the summation of background variance and prescribed observation errors using AOEI (blue), GBOEI (red), and noOEI (green), for GOES-16 ABI (b) channel 8, (d) channel 9, and (f) channel 10 (solid line). The dashed line is the targeted perfect Gaussian distribution.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

Figures 3b, 3d, and 3f compare distributions of the first-guess departures among AOEI, GBOEI, and no-OEI computed from each of the 60 ensemble members, all of which are normalized by the square root of the sum of the prior ensemble variance plus the observation errors assumed in each of the respective experiments. Both AOEI and GBOEI approached a more Gaussian-shaped distribution than by no-OEI. GBOEI fits better to the Gaussian distribution for large normalized first-guess departures (with an absolute value greater than 3) while AOEI overall has a better fit for relatively small normalized first-guess departures (approximately −2 to 2).

Figure 4 compares the spatial distribution of inflated observation errors for GOES-16 ABI channel 8 between AOEI and GBOEI at selected times. The observation errors using AOEI are more localized and larger in magnitude in regions with strong, smaller-scale convection such as those to the southeast of Karl (Fig. 4a), on the edge of the rainbands (Figs. 4a,c,e), and to the outer edge of the eyewall (Figs. 4c,e). On the other hand, by design, large values of inflated observation errors are almost everywhere in this model domain for GBOEI except for a few small areas that have clear sky in both the prior estimate and in the observations (e.g., to the northeast corner of the domain). The biggest difference between AOEI and GBOEI lies in the cloudy regions estimated by the prior, where either the innovation is small and/or the ensemble spread is already very large, both of which cases will have inflated observation error by GBOEI but not by AOEI. The inflated observation error structures for GOES-16 ABI channels 8 and 9 are quite similar to channel 8. Results shown in Figs. 3 and 4 suggest that AOEI is likely to be more flow dependent and could be more effective in controlling large innovations than GBOEI, both of which may improve in the innovation–error relationship [Eq. (2)] over the no-OEI approach assuming a constant observation error everywhere.

Fig. 4.
Fig. 4.

The inflated observation error (K) for GOES-16 ABI channel 8 from (a),(c),(e) AOEI and (b),(d),(f) GBOEI, contour shows symmetric cloud effects parameter (contoured every 5 K), verified at (a),(b) 2200 UTC 16 Sep; (c),(d) 0100 UTC 17 Sep; and (e),(f) 0400 UTC 17 Sep.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

4. Potential impacts of AOEI

a. EnKF assimilation of all-sky radiance with different observation error representation

The truth versus posterior-simulated brightness temperatures of GOES-16 ABI channel 14 (11.2 μm), 10-m wind speed, water vapor mixing ratio, and SLP at 0, 3, and 6 h with the EnKF assimilation of the BTs and minimum SLP are shown (see Figs. 68) by applying three different representations of observation error: AOEI, GBOEI, and no-OEI. As an independent verification (i.e., these observations are not assimilated), we utilized simulated BT from channel 14, which is sensitive to cloud distribution. Experiment AOEI is almost the same as the perfect-model experiment, which assimilated both BTs and minimum SLP in ZMC16 except for using the SCL method for radius of influence (refer to section 2 and ZMC16). The impact of assimilating all-sky GOES-16 radiances has been clearly demonstrated in ZMC16 in terms of the accuracy of both the EnKF analysis and forecasts in comparison to experiment that only assimilated minimum SLP but not brightness temperatures. Here we compare the effectiveness and performance of the EnKF using two different observation error inflation methods (AOEI and GBOEI) as well as the one without observation error inflation (no-OEI).

Right after the initial assimilation cycle at 2200 UTC 16 September, the EnKF-analyzed BT field captured well the main characteristics of Hurricane Karl in the truth simulation, including both the primary eyewall and the outer rainbands (Figs. 5a–d). Continuous assimilations of BTs from channels 8–10 further improved the representation of the storm (Figs. 5f–h,j–l) and compared well with the verifying truth: by 0400 UTC 17 September, the EnKF analysis captured well the detailed structures of the clear region of the hurricane eye, the primary rainbands, as well as most of the individual convective clouds in the outer rainbands. While the analyzed BTs are overall similar among all three OSSEs (with flow-dependent adaptive observation error inflation), the analyzed 10-m wind speed and water vapor mixing ratio with AOEI and GBOEI are considerably smaller and more smoothed than no-OEI, though the overall patterns including the maximum in the eyewall and the highly asymmetric secondary maximum associated with the primary rainband are similar (Figs. 6 and 7).

Fig. 5.
Fig. 5.

The simulated brightness temperatures of GOES-16 ABI channel 14 at (a)–(d) 2200 UTC 16 Sep, (e)–(h) 0100 UTC 17 Sep, and (i)–(l) 0400 UTC 17 Sep from the (a),(e),(i) verifying truth; (b),(f),(j) OSSE with AOEI; (c),(g),(k) OSSE with GBOEI; and (d),(h),(l) OSSE with no-OEI.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

Fig. 6.
Fig. 6.

As in Fig. 5, but for the 10-m surface wind speed (color shading) and sea level pressure (contoured every 5 hPa).

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

Fig. 7.
Fig. 7.

As in Fig. 5, but for the vertically integrated water vapor mixing ratio (color shading).

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

b. Vertical error structure with different observation error representations

To further investigate the effectiveness of AOEI, we compare the impacts of using the three different representations of observation error in assimilating of a single cloudy radiance observations from GOES-16 ABI channel 8 on the EnKF analysis. The vertical distributions of the analysis error (at the observation grid) after each assimilation of the observations (points B and C marked in Fig. 1, respectively) that have a relatively large first-guess departure are shown in Fig. 8 as an example. The values for , first-guess departures, prior ensemble standard deviation in observation space, and the inflated observation errors with AOEI and GBOEI are listed in Table 1. Both points were assigned the same observation error according to climatology using GBOEI, while AOEI inflates the observation error differently for these two points given different first-guess departures and different ensemble spreads.

Fig. 8.
Fig. 8.

Vertical distribution of the prior error (gray shading), and posterior error for the EnKF analyses assimilating only one observation on each grid using AOEI (blue), GBOEI (red), and no-OEI (green), compared with different observation error representations at (a)–(c) point B and (d)–(f) point C marked in Fig. 1.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

Table 1.

Values (K) for , first-guess departures, prior ensemble standard deviation, and the inflated observation errors with AOEI and GBOEI as well as for no-OEI.

Table 1.

At point B, because the ensemble spread is comparable to the first-guess departure, its observation error was slightly inflated using AOEI (and remains the same as in no-OEI). A smaller observation error (more accurate) and a larger first-guess departure will lead to larger analysis increments; with GBOEI, the analysis increments are much reduced and the analysis error remained large with the observation error inflation based on the simulation-derived climatology that mimics the approach in GB11 (Figs. 8a–c).

At point C, since the first-guess departure is much larger than the ensemble spread, the observation error is significantly inflated in AOEI, and thus the analysis increments with no-OEI, which are spuriously large for meridional wind, are effectively suppressed. The observation error is also inflated in GBOEI though to a lesser extent and thus the analysis increments remained considerably larger than those in AOEI but significantly smaller than those in no-OEI (Figs. 8d–f). Comparing with the verifying truth, these proof-of-concept single-observation assimilation experiments of the cloudy radiance observations at these two points exemplify the potential advantages of using AOEI over GBOEI and no-OEI given its use of situation-dependent observation error inflation. On the other hand, the impacts of a truly accurate observation and accurate correlation will likely be much reduced if the observation error is artificially inflated.

The relevance of these single-observation assimilation experiments is demonstrated through Fig. 9, which shows the comparison of the vertical distribution of the horizontal domain and temporally averaged root-mean-square error (RMSE) for the EnKF analysis of selected variables for each of the three OSSEs assimilating the all-sky radiances but with different representation of observation error. Overall, the RMSE both with AOEI and GBOEI are noticeably smaller than no-OEI (Figs. 9a–e), except for the hydrometeors, which is more directly connected to observed variables and, thus, is likely to have less representativeness error (Fig. 9f). The RMSEs with AOEI and GBOEI are mostly similar, but AOEI (GBOEI) slightly better analyzed lower (upper) troposphere. Comparison of the cloudy-affected and other indirectly affected variables further supports the potential effectiveness of inflating observation errors to deal with the representativeness error.

Fig. 9.
Fig. 9.

Vertical distribution of the square root of the domain-averaged EnKF analysis errors averaged over all hourly analysis times with AOEI (blue), GBOEI (red), and no-OEI (green) during 2200 UTC 16 Sep–0400 UTC 17 Sep for (a) zonal wind, (b) meridional wind, (c) temperature, (d) vertical wind, (e) mixing ratio, and (f) all hydrometeors.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

c. Temporal error growth with different observation error representations

More quantitatively, Fig. 10 shows the comparison of the time evolutions of the domain-averaged RMSE of the prior estimate and EnKF analysis of selected variables. The difference in RMSEs among three all-sky OSSEs are small for cloud-affected variables (Figs. 10f,h,i) but large for other indirectly affected variables (Figs. 10a–e,g), which is consistent with Figs. 57 that compared brightness temperatures, 10-m wind speed, water vapor mixing ratio, and SLP. The RMSEs of in particular indirectly affected variables with AOEI are slightly smaller than those in GBOEI, possibly by pulling more information from observations through overall smaller observation errors while suppressing potentially “erroneous” analysis increments through larger observation errors in localized area as shown in Fig. 4. Both AOEI and GBOEI are considerably smaller than no-OEI likely by limiting the analysis increments where there are large representative errors. Moreover, at most of the assimilation time, the EnKF updates with AOEI and GBOEI improved all variables from prior to analysis except for water vapor mixing ratio (which is likely due to more small-scale clouds influences and thus more representative error in the RMSE), while those with no-OEI often worsened the analysis of indirectly affected variables over prior, suggesting the accuracy of the sampling correlation between the BT observation and water vapor may be low especially under clouds while there are large representativeness errors in either BTs and/or water vapor fields.

Fig. 10.
Fig. 10.

Temporal evolution of domain-averaged EnKF RMSEs with AOEI (blue), GBOEI (red), no-OEI (green) and simultaneous estimation method (black) for (a) zonal wind, (b) meridional wind, (c) temperature, (d) vertical wind, (e) water vapor mixing ratio, (f) sum of mixing ratio for all hydrometeors, (g) sea level pressure, (h) brightness temperature of GOES-16 ABI channel 14, and (i) brightness temperature of GOES-16 ABI channel 8.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

To further explore the impact of AOEI, we also conducted another experiment using the method proposed by Li et al. (2009) that simultaneously estimates both the observation error and a multiplicative inflation factor. Following Li et al. (2009), the range of inflation factor was set between 0.9 and 1.2. After each assimilation cycle, we estimated the observation error and the inflation factor for BTs, both of which are assumed to be uniform within the entire domain 3 (without any consideration of heteroscedasticity). These estimated values will be applied for the subsequent assimilation cycle. The temporal evolution of RMSEs for this additional experiment are also shown in Fig. 10 as black lines (denoted as “simultaneous_est”). RMSEs with the Li et al.’s simultaneous estimation method were similar to those from the no-OEI experiment, but were noticeably larger than both the AOEI and GBOEI experiments, highlighting the merit of modeling heteroscedasticity and representativeness error by either GBOEI or AOEI.

To demonstrate the influence of small-scale structures and their associated representative error, we conducted two-dimensional (2D) Fourier decomposition on the prior estimate and EnKF analysis of the horizontally detrended selected variables to divide Fig. 10 into scales with 2D horizontal wavelengths larger than 300 km (Fig. 11) and smaller than 300 km (Fig. 12). AOEI showed some advantage over GBOEI in updating cloudy-affected variables at larger scales (Figs. 11f,h,i), possibly because AOEI modeled smaller observation error variance for most of the domain as shown in Fig. 4, while GBOEI better analyzed smaller-scale structures (Figs. 12f,h,i), with relatively smaller observation error variances in the regions where AOEI locally has large observation error inflation. The RMSEs are overall similar among three OSSEs for other indirectly affected variables in large scales (Figs. 11a–e,g), but distinguishably smaller for AOEI and GBOEI compared to no-OEI for indirectly affected variables in small scales (Figs. 12a–e,g), in particular for temperature and the mixing ratio. Moreover, the analysis RMSEs most of the time became larger than the prior for no-OEI, but they are noticeably suppressed for both AOEI and GBOEI. Results shown in Figs. 1012 further suggested the potentials of AOEI to better control the erroneous analysis increments through assimilating brightness temperatures, which are likely due to representative error and sampling issues mainly in small-scale structures. Figure 4 further indicates the potential advantages of AOEI over GBOEI, both of which will lead to much smaller RMSEs than no-OEI for variables that do not directly affect or are not directly affected by the radiance being assimilated.

Fig. 11.
Fig. 11.

As in Fig. 10, but for the horizontal scales larger than 300 km.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

Fig. 12.
Fig. 12.

As in Fig. 10, but for the horizontal scales smaller than 300 km.

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

d. Dynamical imbalance

To further estimate the potential imbalance induced by EnKF data assimilation cycle, Fig. 13 compared the second derivative of surface pressure at each time step during the first 1-h integration of the deterministic forecasts from EnKF analysis mean. The domain root-mean-square (RMS) of grossly represents the gravity wave activity and serves as an indicator of imbalance and adjustment (Greybush et al. 2011; Houtekamer and Mitchell 2005; Poterjoy and Zhang 2014). RMS is largest for no-OEI followed by AOEI and GBOEI, indicating less mass adjustment occurred with AOEI than with no-OEI, and further less with GBOEI, potentially due to inflated observation errors (and thus smaller analysis increments) as shown in Figs. 4b, 4d, and 4f. The comparison of the flow imbalance with these three different representations of observation error further suggests the effectiveness of inflating observation errors to deal with the imbalance with assimilating brightness temperatures, likely by suppressing the influences of unrepresentative observation errors caused by nonlinearity in the observation operator and/or by sampling due to limited ensemble size.

Fig. 13.
Fig. 13.

Root of domain-averaged square of for 1-h deterministic forecasts initialized at every hour during 2200 UTC 16 Sep–0400 UTC 17 Sep initialized from EnKF analysis with AOEI (blue), GBOEI (red), and no-OEI (green).

Citation: Monthly Weather Review 145, 3; 10.1175/MWR-D-16-0257.1

5. Conclusions

An empirical flow-dependent adaptive observation error inflation (AOEI) method is proposed in this study for assimilating all-sky satellite data under the EnKF framework. We assessed the potential usage of ensemble-based flow-dependent covariance structures on the estimation of adaptive observation error. The observation error was inflated if the square of the innovation (first-guess departure) exceeds the summation of background variance and original observation error variance. We have shown that the satellite radiances can have much larger representative error than the instrumental noises, either due to the strong nonlinearity in the observation operator and/or in the sampling error because of limited ensemble size. It can also be due to the strong nonlinearity and variability, and limited predictability, for the moist atmosphere where the radiances are affected by clouds. Those large representative errors are shown to exist even under a perfect-model scenario without any model error. The AOEI method is designed to limit unrepresentative innovations, inaccurate sampling correlation, and the associated large but potentially erroneous analysis increments. The potential impacts of AOEI were investigated through a series of convection-permitting perfect-model observing system simulation experiments using the PSU WRF-EnKF system, in comparison with experiments using an alternative empirical observation error inflation method proposed by Geer and Bauer (2011) as well as the experiments with a constant radiance observation error everywhere. Both methods with observation error inflation have shown to perform similarly and effectively in suppressing potentially large, erroneous analysis increments that will help to mitigate unphysical flow imbalance induced by the EnKF analysis, comparted to experiment using a constant observation error without inflation. There may be some potential advantages of the newly proposed AOEI method over the Geer–Bauer method in better updating some state variables at large scales and in better maintaining flow balance likely because of its flow- and situation-dependent observation error modeling. The AOEI method is also easier and more readily applied in the ensemble data assimilation framework that does not need to have climatological error distribution statistics. Preliminary results using the above methods to assimilate real-world observations (not shown) are also promising, and are consistent with results from the perfect-model OSSEs presented in this study. Future work will further examine the effectiveness of the proposed AOEI method for real-data observations that have more complex sources of errors likely not being sufficiently represented in this study.

One of the key assumptions made in this study is the ability of the ensemble to accurately represent the background uncertainty (spread) and correlations. Since the ensemble spread is also used here to estimate the flow-dependent observation error, an insufficient ensemble spread due to model error, limited ensemble size, and/or filter-divergence, may lead to weighting the observation inappropriately small and the underuse of otherwise more accurate observations. The evaluation of the amount of ensemble spread and correlations, as well as the methodology to improve them would be required in future study that includes, but is not limited to, the adaptive estimation of inflation factor (e.g., Li et al. 2009; Ying and Zhang 2015), variable covariance localization (e.g., Zhang et al. 2009; Zhen and Zhang 2014), more realistic and complicated errors in the forecast and forward models, to make further advances in fully utilized all-sky satellite radiances. More systematic evaluations of the proposed adaptive method, its variants, and sensitivity, in comparison with alternative methods, will be performed in the future for a large number of cases, and for different platforms of satellite measurements.

Acknowledgments

This research is partially supported by NSF Grant 1305798, ONR Grant N000140910526, and NASA Grants NNX16AD84G and NNX15AQ51G. Review comments by two anonymous reviewers were beneficial and greatly appreciated. MM was also supported by Japan’s Funai Overseas Scholarship of the Funai Foundation for Information Technology. We benefited from discussions with Eugene Clothiaux, Yonghui Weng, Michael Ying, Scott Sieron, Jason Otkin, Eugenia Kalnay, Fuzhong Weng, Alan Geer, and many others. Computing was provided by the Texas Advanced Computing Center (TACC). All data presented are stored and can be accessed through the TACC data archive.

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  • Dee, D. P., 1995: Online estimation of error covariance parameters for atmospheric data assimilation. Mon. Wea. Rev., 123, 11281145, doi:10.1175/1520-0493(1995)123<1128:OLEOEC>2.0.CO;2.

    • Crossref
    • Search Google Scholar
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  • Desroziers, G., L. Berre, B. Chapnik, and P. Poli, 2005: Diagnosis of observation, background and analysis-error statistics in observation space. Quart. J. Roy. Meteor. Soc., 131, 33853396, doi:10.1256/qj.05.108.

    • Crossref
    • Search Google Scholar
    • Export Citation
  • Evensen, G., 2003: The ensemble Kalman filter: Theoretical formulation and practical implementation. Ocean Dyn., 53, 343367, doi:10.1007/s10236-003-0036-9.

    • Crossref
    • Search Google Scholar
    • Export Citation
  • Geer, A. J., and P. Bauer, 2011: Observation errors in all-sky data assimilation. Quart. J. Roy. Meteor. Soc., 137, 20242037, doi:10.1002/qj.830.

  • Greybush, S. J., E. Kalnay, T. Miyoshi, K. Ide, and B. R. Hunt, 2011: Balance and ensemble Kalman filter localization techniques. Mon. Wea. Rev., 139, 511522, doi:10.1175/2010MWR3328.1.

    • Crossref
    • Search Google Scholar
    • Export Citation
  • Han, Y., P. van Delst, Q. Liu, F. Weng, B. Yan, R. Treadon, and J. Derber, 2006: JCSDA Community Radiative Transfer Model (CRTM)—Version 1. NOAA Tech. Rep. NESDIS 122, 40 pp. [Available online at http://docs.lib.noaa.gov/noaa_documents/NESDIS/TR_NESDIS/TR_NESDIS_122.pdf.]

  • Han, Y., F. Weng, Q. Liu, and P. van Delst, 2007: A fast radiative transfer model for SSMIS upper atmosphere sounding channels. J. Geophys. Res., 112, D11121, doi:10.1029/2006JD008208.

    • Crossref
    • Search Google Scholar
    • Export Citation
  • Harnisch, F., M. Weissmann, and Á. Periáñez, 2016: Error model for the assimilation of cloud-affected infrared satellite observations in an ensemble data assimilation system. Quart. J. Roy. Meteor. Soc., 142, 17971808, doi:10.1002/qj.2776.

    • Crossref
    • Search Google Scholar
    • Export Citation
  • Heidinger, A., C. O’Dell, R. Bennartz, and T. Greenwald, 2006: The successive-order-of-interaction radiative transfer model. Part I: Model development. J. Appl. Meteor. Climatol., 45, 13881402, doi:10.1175/JAM2387.1.

    • Crossref
    • Search Google Scholar
    • Export Citation
  • Hong, S.-Y., and J. Lim, 2006: The WRF single-moment 6-class microphysics scheme (WSM6). J. Korean Meteor. Soc., 42 (2), 129151.

  • Hong, S.-Y., Y. Noh, and J. Dudhia, 2006: A new vertical diffusion package with an explicit treatment of entrainment processes. Mon. Wea. Rev., 134, 23182341, doi:10.1175/MWR3199.1.

    • Crossref
    • Search Google Scholar
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  • Fig. 1.

    (a) Simulated brightness temperature from GOES-16 ABI channel 8, (b) the innovation square (), (c) ensemble variance, and (d) the difference between the observed innovation square () and the summation of observation and forecast error variances (), verified at the initial assimilation time at 2200 UTC 16 Sep. Star, circle, square, and triangle markers represent the points shown in Figs. 2 and 8.

  • Fig. 2.

    Prior ensemble distributions of the (a),(e),(i),(m) brightness temperature; (b),(f),(j),(n) column-integrated hydrometeors; (c),(g),(k),(o) column-integrated vapor mixing ratio; and (d),(h),(l),(p) the 10-m surface meridional wind. The sky-blue box shows the ensemble distribution, the blue line shows the estimated first-guess distribution based on Gaussian assumption, and the red star shows the verifying truth, for points A, B, C, and D marked in Fig. 1.

  • Fig. 3.

    (a),(c),(e) The Geer–Bauer observational error models for the BTs in GOES-16 ABI (a) channel 8, (c) channel 9, and (e) channel 10 used in experiment GBOEI. The standard deviation of first-guess departures is shown by a red solid line, which is modeled as a function of symmetric cloud effect parameter , derived from a 1-day dataset of the no-DA experiment. The gray box shows the number of observations classified into each bin. (b),(d),(f) Innovation statistics, normalized by the summation of background variance and prescribed observation errors using AOEI (blue), GBOEI (red), and noOEI (green), for GOES-16 ABI (b) channel 8, (d) channel 9, and (f) channel 10 (solid line). The dashed line is the targeted perfect Gaussian distribution.

  • Fig. 4.

    The inflated observation error (K) for GOES-16 ABI channel 8 from (a),(c),(e) AOEI and (b),(d),(f) GBOEI, contour shows symmetric cloud effects parameter (contoured every 5 K), verified at (a),(b) 2200 UTC 16 Sep; (c),(d) 0100 UTC 17 Sep; and (e),(f) 0400 UTC 17 Sep.

  • Fig. 5.

    The simulated brightness temperatures of GOES-16 ABI channel 14 at (a)–(d) 2200 UTC 16 Sep, (e)–(h) 0100 UTC 17 Sep, and (i)–(l) 0400 UTC 17 Sep from the (a),(e),(i) verifying truth; (b),(f),(j) OSSE with AOEI; (c),(g),(k) OSSE with GBOEI; and (d),(h),(l) OSSE with no-OEI.

  • Fig. 6.

    As in Fig. 5, but for the 10-m surface wind speed (color shading) and sea level pressure (contoured every 5 hPa).

  • Fig. 7.

    As in Fig. 5, but for the vertically integrated water vapor mixing ratio (color shading).

  • Fig. 8.

    Vertical distribution of the prior error (gray shading), and posterior error for the EnKF analyses assimilating only one observation on each grid using AOEI (blue), GBOEI (red), and no-OEI (green), compared with different observation error representations at (a)–(c) point B and (d)–(f) point C marked in Fig. 1.

  • Fig. 9.

    Vertical distribution of the square root of the domain-averaged EnKF analysis errors averaged over all hourly analysis times with AOEI (blue), GBOEI (red), and no-OEI (green) during 2200 UTC 16 Sep–0400 UTC 17 Sep for (a) zonal wind, (b) meridional wind, (c) temperature, (d) vertical wind, (e) mixing ratio, and (f) all hydrometeors.

  • Fig. 10.

    Temporal evolution of domain-averaged EnKF RMSEs with AOEI (blue), GBOEI (red), no-OEI (green) and simultaneous estimation method (black) for (a) zonal wind, (b) meridional wind, (c) temperature, (d) vertical wind, (e) water vapor mixing ratio, (f) sum of mixing ratio for all hydrometeors, (g) sea level pressure, (h) brightness temperature of GOES-16 ABI channel 14, and (i) brightness temperature of GOES-16 ABI channel 8.

  • Fig. 11.

    As in Fig. 10, but for the horizontal scales larger than 300 km.

  • Fig. 12.

    As in Fig. 10, but for the horizontal scales smaller than 300 km.

  • Fig. 13.

    Root of domain-averaged square of for 1-h deterministic forecasts initialized at every hour during 2200 UTC 16 Sep–0400 UTC 17 Sep initialized from EnKF analysis with AOEI (blue), GBOEI (red), and no-OEI (green).

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