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--> --> --> -->2.1. Data selection and quality control
The selected area is centered at the Nanjing radar site with a 150-km radius. Since the time of one volume scan of the GR is about 6 min, the GR volume scan is acquired beginning within a 6-min window centered on the TRMM PR overpass time, along with its corresponding spaceborne radar data.The level II algorithm of the PR profile (2A25), which includes ground clutter filtering, attenuation and beam filling correction, is applied to the TRMM PR reflectivity data. This relies on the output of 1C21 and 1B21 to separate the surface clutter ranges from the clutter-free ranges (Kozu et al., 2001; Wang et al., 2015). The clutter identification routine used in 1B21 may not be perfect, and some surface clutter may occasionally be misidentified as rain echo in 2A25, but this problem is usually confined to mountain regions. Moreover, only the data at a height above 1 km are used, which may further minimize the contamination from the remaining ground clutter. The TRMM PR attenuation correction is processed with a Hitschfeld-Bordan iterative scheme and surface reference technique (Iguchi et al., 2000; Meneghini et al., 2004), and the beam filling correction is also performed in the 2A25 product (Iguchi et al., 2000; Kozu et al., 2001). TRMM PR operates at 13.8 GHz (Ku band) and has a low sensitivity threshold of 18 dBZ. It scans 17° to either side of nadir at intervals of 0.7° in the cross-track direction, which gives a swath width of 214 km (246 km after boost) at the Earth's surface, with a horizontal resolution of about 4.3 km (5 km after boost) at nadir. The TRMM PR pulse duration is 1.67 μs, which gives a vertical resolution of about 0.25 km.
For this case study, the GR data from ground Doppler radar at Longwang Mountain (32.1908°N, 118.6969°E) in Nanjing city, China, are adopted. Nanjing radar operates at the S band with a VCP21 mode. The current reflectivity product operates at a 1-km range resolution and 1° azimuthal resolution, with a minimum detectable reflectivity of -7.5 dBZ at 50 km. Before fusing the GR data, quality control is performed on the Nanjing GR reflectivity data, including removing electronic interference, anomalous propagations and ground clutter, and system bias correction. The NCAR SOLO II algorithm is used to remove the anomalous propagations and ground clutter, and the system bias correction is addressed in section 2.3.
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2.2. Gridding and matching
For the subsequent data fusion, the TRMM PR and GR reflectivity data should be interpolated in a common coordinate system. The spatial matchup scheme is based on the grid matching method provided in the literature related to comparisons of PR and GR (Anagnostou et al., 2001; Liao and Meneghini, 2009; Wang and Wolff, 2009). The gridded GR data in a 3D Cartesian coordinate system are interpolated from the GR spherical coordinate system centered at the GR using a cubic linear interpolation algorithm, with a vertical resolution of about 1 km to a height of 20 km and a horizontal resolution of about 1 km to a horizontal extent of 150 km. Thus, 3D gridded data for Nanjing GR are obtained with a resolution of about 1 km × 1 km × 1 km.The TRMM PR data are also resampled into Cartesian coordinates. During 3D gridding, the displacement or parallax of PR samples is corrected with the method described in (Wang and Wolff, 2009). After displacement correction, the resolution of resampled TRMM PR in a 3D grid is about 4 km × 4 km × 0.25 km.
A case study for Nanjing GR on 27 May 2008 is performed, and the orbit number is 59995. The overpass time of PR at Nanjing GR is 0456:41 UTC, and the beginning time of the corresponding GR volume scan is 0453:00 UTC. Figure 1a shows the GR CAPPI (Constant Altitude Plan Position Indicator) data at 3 km height with a resolution of 1 km × 1 km. Figure 1b shows the PR data at 3 km height in Cartesian coordinates with a resolution of 4 km × 4 km. For the following NN training, the input GR data should be downsampled to the same resolution as the PR horizontal resolution. The downsampled GR reflectivity is shown in Figure. 1c with a horizontal resolution 4 km × 4 km using an average filter of size 4× 4 on a horizontal plane.
It can be seen that the radar echoes from TRMM PR are basically consistent with those from GR in Fig. 1. Figure 2 is a scatter plot of TRMM PR and gridded GR reflectivity at 3 km height in Figs. 1b and c. The correlation coefficient of downsampled GR data and original TRMM PR data is 0.79, indicating relatively high coherence, but the mean difference (PR minus GR) is about 2.9 dB. Many factors, like differences in radar sensitivities, sample volumes, viewing angles, attenuation and different radar wavelengths, may influence the reflectivity difference of TRMM PR and GR, but the GR system calibration bias may bring about the difference between TRMM PR and GR (Anagnostou et al., 2001).
Figure1. (a) Gridded Nanjing GR with horizontal resolution of 1 km × 1 km; (b) TRMM PR with horizontal resolution of 4 km × 4 km; and (c) gridded Nanjing GR downsampled by a factor of 4 at a height of 3 km.
Figure2. Scatterplot of TRMM PR and GR reflectivity. The data are the common data from 3 km CAPPI in Figs. 1b and c. The straight line is the regression line, and the sample points, the correlation coefficients, and the mean error between TRMM PR and GR reflectivity are shown in the inset text.
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2.3. GR calibration bias correction
For NN fusion processing, the GR reflectivity data and TRMM PR data are assumed as unbiased estimates in a global sense, and hence the system calibration bias should be corrected if it exists. With considerable long-term certainty and stability, the TRMM PR has served as a reference to calibrate GRs and to detect inconsistencies between adjacent GRs (Anagnostou et al., 2001; Bolen and Chandrasekar, 2000; Wang and Wolff, 2009). In (Zhu et al., 2016), 245 TRMM PR and Nanjing GR matchup cases for the period 2008-13 were adopted and compared using statistical analysis methods to determine the calibration biases of Nanjing GR. The results showed that Nanjing GR presents a "three-stage" feature, and the mean deviation of TRMM PR and Nanjing GR in stage 1 from January 2008 to March 2010 was about 1.2 dB, the mean deviation in stage 2 from March 2010 to May 2013 was about 4.2 dB, and the mean deviation in stage 3 from May 2013 to October 2013 was approximately 1.5 dB. In this study, a bias adjustment of 1.2 dB is applied to GR for the case in Figure. 1.2
2.4. Conversion from Ku to S band
For TRMM PR at Ku band, some large particles may fall into the Mie scattering region, and the radar reflectivity factors at S and Ku bands can be significantly different (Liao and Meneghini, 2009; Wen et al., 2011; Cao et al., 2013). This Mie scattering effect can be estimated using a raindrop size distribution model. Based on the gamma particle size distribution modeling in the ice region, melting layer, and raining region, (Cao et al., 2013) derived the empirical relations between Ku and S band reflectivity in different regions. Since the proposed algorithm is mainly for convective precipitation, here we divide the precipitation into snow and rain regions according to the height of the freezing level in the 2A23 product of TRMM PR, and the melting region is not calculated separately: \begin{equation} \begin{array}{rcl} Z_{\rm s}\!-\!Z_{\rm Ku}&=&0.0478+0.0123Z_{\rm Ku}\!-\!3.504\times 10^{-4}Z_{\rm Ku}^2\\ &&-3.3\times 10^{-5}Z_{\rm Ku}^3+4.27\times 10^{-7}Z_{\rm Ku}^4\\ &&{\rm (for\ rain)}\\ Z_{\rm s}\!-\!Z_{\rm Ku}&=&0.174+0.0135Z_{\rm Ku}\!-\!1.38\times 10^{-3}Z_{\rm Ku}^2\\ &&+4.74\times 10^{-5}Z_{\rm Ku}^3\\ &&{\rm (for\ snow)} \end{array} \ \ (1)\end{equation} where Z s and Z Ku are expressed in dBZ units. From the relations in Eq. (1), a Ku band reflectivity can be conveniently converted to an S band reflectivity. Based on Eq. (1), it can be seen that the difference between Z s and Z Ku is small when Z s<35 dBZ, and about 2 dB or more when Z s>35 dBZ.-->
3.1. Fusion with NN
NNs have been exploited in weather radar applications like precipitation forecasting, rainfall rate estimation, wind prediction, and so on (Orlandini and Morlini, 2000; Sarma et al., 2008; Wang et al., 2015). A new NN approach is developed where multiple NNs are trained using the 0.25 km vertical resolution TRMM PR data at different heights as outputs of training NNs, and gridded GR data with 1 km vertical resolution at different heights as inputs. Different from conventional NN methods, the goal of this study is to gain a 3D high resolution radar echo structure, and hence the 3D gridded radar reflectivity data with different resolution are used as inputs and outputs for training NNs, respectively.The vertical range of the 3D reflectivity data is from 1 km to 20 km, and thus the number of layers is 20 for the GR data with a vertical resolution of 1 km, and the number of layers is 77 for the TRMM PR data with a vertical resolution of 0.25 km. For one NN, we use TRMM PR data at four adjacent heights as outputs, and GR data at 4 heights nearest to the output heights as inputs. In this way, 19 neural networks are trained with 20 layers of GR data and 77 layers of TRMM PR data. The specific structure setting for the Kth neural network is shown in Fig. 4. In Fig. 4, the input of the Kth training NN is 2D GR data at four heights of K-1 km, K km, K+1 km and K+2 km, and the corresponding output is TRMM PR data at four heights of K km, K+0.25 km, K+0.5 km and K+0.75 km, where K=2-18. Here, the first and the 19th NN are excluded. The inputs of the first NN are GR data at heights of 1 km, 2 km, 3 km and 4 km, and the corresponding outputs are TRMM PR data at heights of 1 km, 1.25 km, 1.5 km and 1.75 km. For the 19th neural network, the inputs are GR data at heights of 17 km, 18 km, 19 km and 20 km, and the outputs are TRMM PR data at heights of 19 km, 19.25 km, 19.5 km, 19.75 km and 20 km. Besides, for matching to the horizontal resolution of TRMM PR data, original GR data are converted to 4 km × 4 km by smoothing and downsampling by a factor of 4, using an average filter of size 4× 4. After 19 NNs are trained, the trained NN parameters are applied to the original 2D GR data, and the output data with a high vertical resolution of 0.25 km and horizontal resolution of 1 km × 1 km can be generated.
Figure4. Flow chart of the Kth NN fusion, where K=2-18. The upper part is the NN training part, and the lower dashed box part applies the trained NN parameters to retrieve high vertical resolution reflectivity data with inputs of original GR data. A total of 19 NNs are modeled for training 20 layers of GR data with a vertical resolution of 1 km and 77 layers of TRMM PR data with a vertical resolution of 1 km. The inputs of the first and 19th NN are GR data at heights of 1 km, 2 km, 3 km and 4 km, and heights of 17 km, 18 km, 19 km and 20 km, respectively.
The upper part of Fig. 4 is the NN training part, and the application part uses the trained NN parameters to retrieve high vertical resolution reflectivity data with an input of high horizontal resolution GR data. The inner structure of the Kth training NN is shown in Fig. 5.
Figure5. Inner structure of the training NN. Three layers are included in the training NN, which are the input layer, hidden layer and output layer. The W and b in the hidden layer and output layer are the weighting matrix and adjusting factor, respectively. The outputs of the hidden layer are calculated with a logistic sigmoid activation function, and the outputs of the output layer are calculated with a linear activation function.
The types of NN used in Fig. 5 are back-propagation feed-forward NNs. In the following, the fundamental algorithm of the back-propagation NN is simply reviewed. After normalization of input data, the data in the hidden layer are updated with weighting, and the outputs of the hidden layer O h are calculated with a logistic sigmoid activation function, \begin{eqnarray} {O}_{\rm h}&=&f({W}_{\rm ih}{X}+{b}_{\rm ih})\ \ (2)\\ f(a)&=&\dfrac{1}{1+\exp(-a)} , \ \ (3)\end{eqnarray} where X is the input matrix; W ih and b ih are the weighting matrix and adjusting factor for the hidden layer. The output layer calculates the final output O p using the outputs of the hidden layer and a trained matrix W ho and adjusted factor b ho with a linear activation function, \begin{equation} \label{eq1} {O}_{\rm p}={W}_{\rm ho}{O}_{\rm h}+{b}_{\rm ho} . \ \ (4)\end{equation} For weighting matrices and adjusting factors in the hidden and output layer, they are updated according to Levenberg-Marquardt optimization, \begin{eqnarray} \label{eq2} {W}_{\rm ho}^{(l+1)}&=&{W}_{\rm ho}^{(l)}+\Delta{W}_{\rm ho} ,\ \ (5) \\ \label{eq3} \Delta{W}_{\rm ho}&=&[{\it J}^{\rm T}({W}_{\rm ho}){\it J}({W}_{\rm ho})+\eta{I}]^{-1}{\rm J}^{\rm T}({W}_{ho}){\it E}({W}_{\rm ho}) , \ \ (6)\end{eqnarray} where l represents the lth iteration, T indicates transposition, η is the learning rate, I is the identity matrix, and J(W ho) is the Jacobian matrix of E(W ho). E(W ho) is the vector of the mean-square error of the output O p and target output Y, \begin{equation} \label{eq4} {\it E}({W}_{\rm ho})=\dfrac{1}{2}\sum_1^n\|{O}_{\rm p}-{Y}\|^2 , \ \ (7) \end{equation} where n is number of nodes of the output layer. From Fig. 4, it is seen that n is 4. Also, we can see that the size of the input matrix X is 4× M and the size of the output matrix Y is 4× M, where M is the data samples (matched GR and PR data) in one training set. It should be noted that only commonly available data in the matched area of the four input height layers of the GR data and output TRMM PR data are used during NN training. The weighting matrices of the hidden layer (W ih) and adjusting factors (b) are updated similarly to that of W ho. Finally, the global error of the network is calculated with \begin{equation} \label{eq5} e=\dfrac{1}{2M}\sum_1^M\sum_1^n({O}_{\rm p}-{Y})^2 . \ \ (8)\end{equation} If the error e reaches setting precision or learning times larger than the setting maximum number of iterations or error e no longer converges, the algorithm stops. If not, the next iteration starts until one of the aforementioned conditions has been satisfied. The trained results of the weighting matrices and adjusting factors are saved for the application of the trained NN.
Figure 6a is a plot of MSE (mean square error) variation of the training process for the third NN. The input data are 2D gridded GR at heights of 2 km, 3 km, 4 km and 5 km, and the corresponding output is 2D TRMM PR data at heights of 3 km, 3.25 km, 3.5 km and 3.75 km. The MSE converges to 0.025284 dB2 at the 21st iteration. For this NN training, the number of hidden layer nodes is set as nine.
Figure6. (a) Performance variation of the training process for the third NN. The MSE converges to 0.025284 dB2 at the 21st iteration. (b) Rain type classification, where plus signs represent convective precipitation and dots stratiform precipitation. (c) Convergent global MSE (dB2) of 19 trained NNs. (d) Number of samples for convective and stratiform precipitation of 19 training NNs. Since different types of precipitation may vary distinctly, the matched available training pairs are separated into stratiform (black line) and convective types (red line). The precipitation types are determined according to the rain type classification in the TRMM PR 2A23 products.
The performance or the generalization ability of NN training is dependent on many factors, such as the issue complexity, the data samples and the number of hidden layer nodes. The first two factors are difficult to change for a given case, and the optimum number of hidden layer nodes is also usually difficult to determine. Generally, some empirical formulas for obtaining hidden layer nodes are used, like (Shi et al., 2009) \begin{equation} L=\sqrt{mn}\ or\ L=2^*m+1\ or\ L=\sqrt{m+n}+\alpha , \ \ (9)\end{equation} where m is number of input nodes, n is the number of output nodes, L is the number of hidden layer nodes, and α is a number between 1 and 10. Equation (9) is just empirical formulas, which has certain limitations because it ignores the size of training samples and complexity of the issue. In practical applications, we can use the trial and error method by testing the range of the formulas in Eq. (9) to obtain a relatively optimal number for each NN. For four input nodes and four output nodes in Fig. 5, the number of hidden layer nodes we can try is 4-12. Besides, the optimum number of hidden layer nodes may be determined by optimization algorithms like a genetic algorithm or a particle swarm optimization algorithm. Since different types of precipitation may vary distinctly, the matched available training pairs are separated into stratiform and convective types according to the parameter "rainType" in the TRMM PR 2A23 product, and the rain type classification is shown in Fig. 6b. Figure 6c is the global MSE of 19 trained NNs with relatively optimal hidden layer nodes determined by the trial and error method, and Fig. 6d is the number of samples of convective and stratiform rain for 19 NNs. From Fig. 6c it is apparent that the performance of training NN reduces with the increase in height, and the performance of convective rain is superior to that of stratiform rain at higher heights. Since the case in this study is a thunderstorm event primarily featuring convective rain, the number of stratiform precipitation samples that can be seen from Fig. 6d decreases sharply (the number falls back into single digits) at higher heights, which makes the performance of stratiform rain become very poor at heights above 9 km.
Of note is that the small training dataset potentially limits the usefulness of the NN approach. In the NN training, the critical minimal data samples are generally required to be at least twice the number of NN weights (Shi et al., 2009). In the case of Fig. 6b, the numbers of convective and stratiform data samples for the 10th NN are 59 and 10 respectively, and so the samples are not enough for training even if precipitation data are not separated into different types. Hence, the NNs greater than the 10th (10-19 NNs) are regarded as unfit for NN training. The high-resolution reflectivity of 10-19 NNs is obtained with interpolation and simple linear fusion. Firstly, GR data above 10 km height are processed with linear interpolation in the vertical direction to produce a 0.25 km height resolution. Then, TRMM PR data above 10 km height are processed with nearest neighbor interpolation in the horizontal direction to produce a 1 km × 1 km horizontal resolution. Finally, the high-resolution fusion data at the Nth (N>10 for this case) height are obtained with \begin{equation} \label{eq6} f_{{\rm PRGR}_N}=f_{{\rm GR}_N}\frac{\bar{f}_{{\rm PR}_N}}{\bar{f}_{{\rm GR}_N}} , \ \ (10)\end{equation} where f GRN and f PRN are the reflectivity of GR and TRMM PR at the Nth height, respectively; N is from 10 to 20 with a spacing of 0.25; and \(\bar{f}_\rm PR_N\) and \(\bar{f}_\rm GR_N\) represent averaging over the common echoes of the Nth height GR and TRMM PR data, respectively.
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3.2. Weak echoes interpolation
The minimum detectable reflectivity of TRMM PR is about 18 dBZ, and data less than this minimum are excluded from the NN training, so weak echoes less than 18 dBZ cannot be obtained with the NN method. The echoes less than 18 dBZ may be used to estimate the height of the storm top and, most importantly, they are utilized to estimate the rainfall amount. So, the weak echoes should be taken into account for the 3D fusion of TRMM PR and GR data. The field below 18 dBZ in the final 3D high-resolution fusion reflectivity data is generated with linear interpolation in the vertical direction of the corresponding GR data.2
3.3. GR blind areas compensation
Nanjing GR scans in the VCP 21 mode, and the highest elevation angle is 19.5°. Limited by the scanning elevation angles, significant data voids exist above the highest beam, i.e., the GR blind area or the "cone of silence". The area of the "cone of silence" increases with height. When the storm is at 20 km horizontal distance from the radar, the radar can only detect the precipitation below the height of about 7.1 km, and the characteristic echo parameters of most convective precipitation will be underestimated.After GR data are processed with NN fusion, the remaining GR blind area echoes are obtained by merging upsampled TRMM PR data and coincident surrounding pixels of high-resolution NN fused data in a selected window. For a given pixel in a blind area, the optimum weight can be determined by the available data and the distance between the center pixel and neighboring pixels from the merging window (Mahani and Khanbilvardi, 2009). The window size is varied according to the size of the GR blind area and the number of surrounding reflectivity pixels.
The merging method is to adjust the TRMM PR reflectivity data for any given pixel in the blind area based on an appropriate weight with respect to the available TRMM PR and NN-fused reflectivity of its neighboring pixels. The weight factor wi is calculated by \begin{equation} \begin{array}{rcl} w_i&=&\dfrac{r_o^2-r_i^2}{r_o^2+r_i^2},r_i<r_o\\[3mm] r_i^2&=&(x_i-x_o)^2+(y_i-y_o)^2 , \end{array} \ \ (11)\end{equation} where ri is the distance between the center pixel (o) and the observation pixel (i); ro is the maximum distance from the center; and (x,y) are the grid pixel coordinates. The merged reflectivity for the center pixel (f PRGRo) is obtained by \begin{equation} \label{eq7} f_{{\rm PRGR}_o}=f_{{\rm PR}_o}+\frac{\sum_{i=1}^n{w_i(f_{{\rm PRGR}_i}-f_{{\rm PR}_i})}}{\sum_{i=1}^n{w_i}} , \ \ (12)\end{equation} where f PRGRi and f PRi are the reflectivity of the NN-fused data (PRGR NN) and TRMM PR for the observation pixel (i) inside the window, respectively; and n is the number of pixels observed with both PRGR and TRMM PR inside the window.
The same data shown in Fig. 1 are used here to illustrate the results of blind area compensation. Figure 7a shows the PRGR NN at 3 km height with a blind area of about 16× 16 pixels, and Fig. 7b shows the TRMM PR data upsampled by a factor of 4 with nearest neighborhood interpolation for matching with the fused data, PRGR NN. Figure 7c shows the merging result by simply substituting the blind area data with the corresponding TRMM PR data in Fig. 7b. Merging Fig. 7a and Fig. 7b with the distance weighting-based approach, we get the merging result shown in Fig. 7d with a window size of 5× 5 pixels. Comparing Fig. 7c with Fig. 7d, it can be seen that the merging result with the distance weighting-based approach in Fig. 7d is more consistent with the surrounding original data in Fig. 7a than the TRMM PR data substitution in Fig. 7c. That is because the merging approach retains more details on the reflectivity structures of PRGR NN by allowing more contributions from near-range observations.
Figure7. (a) Reflectivity data at 3 km height after NN fusion as described in section 3.1. (b) TRMM PR reflectivity data at 3 km height with a horizontal resolution of 1 km × 1 km using the nearest neighbor method. (c) Merged reflectivity images by compensating blind areas with TRMM PR data substitution. (d) Merged reflectivity images by compensating blind areas with the distance weighting-based approach with a window size of 5× 5 pixels. For better revealing the compensation results, the images are enlarged around the blind areas.
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3.4. Combination
3D high-resolution reflectivity data over GR regions larger than PR's sensitivity can be obtained using NN fusion. For data below PR's sensitivity, the high-resolution data are generated with linear interpolation in the vertical direction of the corresponding GR data. By merging upsampled TRMM PR data at each height with coincident surrounding pixels of PRGR NN data in a selected window, high-resolution data over GR blind areas can be obtained. For convenience, the fused 3D high-resolution reflectivity data are denoted as PRGR data; the fused data without blind areas compensation is denoted as PRGR NN.Figure8. (a) Original GR reflectivity data; (b) upsampled TRMM PR data (horizontal resolution: 1 km × 1 km) with the nearest neighbor method, and (c) fused high-resolution reflectivity data (PRGR) at 3 km height. (d) Reflectivity profiles along the dashed line in (c), where the red line denotes the TRMM PR data, the black line GR data, and the green line PRGR data.
The fused high-resolution results are shown in Figs. 8-10. Figure 8a shows the 3-km CAPPI of the original GR reflectivity data, and Fig. 8c shows the fused 3D high-resolution PRGR data at 3-km height. For validating the performance of the fused result, the horizontal section of PRGR is compared with GR and TRMM PR data at each grid point with the same resolution, and original TRMM PR data are upsampled by a factor of 4 with the nearest neighborhood method shown in Fig. 8b. It can be seen that the echo structure of the fused product, PRGR, is close to the GR data, and the impact of TRMM PR on the magnitude of the PRGR field can be found in the central region of the domain in Fig. 8c. Compared with upsampled TRMM PR, the fused product, PRGR, recovers more small scale features and produces a fused reflectivity image with a more detailed structure. Besides, the weak echoes below PR's sensitivity and the echoes within the cone of silence are included in the fusion product, which makes the echo structure more complete. A 1D reflectivity dataset shown in Fig. 8d, which is obtained along the horizontal dashed line in Fig. 8c, better demonstrates the performance of the PRGR data. It can be seen that the red line denoting TRMM PR data is smoother due to its coarse horizontal resolution, and the fused data preserve the fine structure of GR while taking into account information from the TRMM PR observation.
Figure9. Vertical cross section of reflectivity data along the black solid line in Fig. 8a for (a) original GR, (b) GR with vertical linear interpolation (GR interp), (c) TRMM PR, and (d) fused data with compensation of the cone of silence (PRGR). Vertical profiles of reflectivity in Figs. 10a-d along the black solid line (e) and along the black dashed line (f), where the black line denotes the vertical profile of GR data in (a), the green line denotes the vertical profile of GR interp in (b), the red line denotes the vertical profile of TRMM PR data in (c), and the blue line represents the vertical profile of PRGR data in (d).
Statistical comparisons of reflectivity data in Fig. 8 are shown in Table 1, where correlation coefficients (Corr. Coeff), mean errors (Mean) and root-mean-square errors (RMSEs) between TRMM PR data and GR, fused PRGR data and TRMM PR, and fused PRGR data and GR, are compared. The data pairs selected in the comparisons are in the area where both TRMM PR and GR data are available; hence, PRGR data used are mainly data with NN fusion, and Table 1 mainly quantitatively reflects the performance of the fused product with the NN fusion method. For matching to GR and PRGR data, the TRMM PR data used are the upsampled data in the horizontal direction with the nearest neighborhood method. The results in Table 1 show that the generated PRGR data at horizontal planes are more correlated to GR, showing a high correlation coefficient, which means that the horizontal structure of PRGR is more similar to that of GR. The mean error and RMSE of PRGR to TRMM PR is much smaller than that of the original GR to TRMM PR, which indicates the magnitude of PRGR with NN fusion incorporates the characteristics of TRMM PR.
The images in Figs. 9a-d and Figs. 10a-d are vertical cross sections of the reflectivity along the black solid line and dashed line in Fig. 8a, where Fig. 9 represents the convective precipitation and Fig. 10 represents the stratiform precipitation. Due to the coarse vertical resolution of GR, strong discontinuity in the vertical direction can be observed in
Figure10. Vertical cross section of reflectivity data along the black dashed line in Fig. 8a for (a) original GR, (b) GR with vertical linear interpolation (GR interp), (c) TRMM PR, and (d) fused data (PRGR). Vertical profiles of reflectivity in Figs. 10a-d along the black solid line (e) and along the black dashed line (f), where the black line denotes the vertical profile of GR data in (a), the green line denotes the vertical profile of GR interp in (b), the red line denotes the vertical profile of TRMM PR data in (c), and the blue line represents the vertical profile of PRGR data in (d).
Fig. 9a and Fig. 10a. After linear interpolation, the vertical cross sections of GR in Figs. 9b and 10b are similar to those in Figs. 9a and 10a but smoother. Clearer vertical structures are seen in Figs. 9c and 10c of TRMM PR data, and the bright band can be observed near 4-4.5 km altitude in Fig. 10c. The fused products in Figs. 9d and 10d are more inclined to the TRMM PR data, but the magnitude and the horizontal distribution involves few characteristics of GR. For the convective precipitation in Fig. 9, many echoes above 8 km altitude are missed around the radar center in Figs. 9a and b due to the cone of silence, especially at the range (20 km, 40 km), which may make the echo top underestimated. With the distance weighting-based approach, the void area around the radar center above the height of 8 km is filled by the compensation, but the compensated echoes in Fig. 9d are more consistent with the original TRMM PR data, and a slight discontinuity exists between the echoes in the cone of silence and neighboring PRGR echoes. This is mainly because the available PRGR NN data become increasingly less with the increase in echo height and the blind region.
For better demonstrating the vertical structure of the fused product, the vertical profiles are shown in Figs. 9e and f and Figs. 10e and f. The vertical profiles in Figs. 9e and f are generated from the vertical cross sections of the convective precipitation in Figs. 9a-d along the black solid and dashed lines in Fig. 9a. The two images of vertical profiles correspond to the two heavy rain centers of the convective precipitation band, respectively. From Figs. 9e and f it is apparent that the vertical profiles of TRMM PR and PRGR can better display the detailed features of the vertical variation of reflectivity, and the vertical variation of GR and GR interp reflectivity are more gentle. Because the vertical cross sections of GR and GR interp are produced by interpolating the measured reflectivity data with different elevations, some fine structures are smoothed out in the vertical profiles of GR and GR interp. For example, in Fig. 9f, the vertical variation of TRMM PR and PRGR from about 5 km to 10 km altitude is more significant than that of GR and GR interp, and more turning points like a point at about 6 km altitude exist in the vertical profiles of TRMM PR and PRGR, which indicates a finer vertical structure of TRMM PR and PRGR. In Fig. 9e, the maximum reflectivity is distributed at about 2.5-3.5 km altitude in the vertical profiles of TRMM PR and PRGR, and the reflectivity decreases above and under the maximum region. However, the vertical profiles of GR or GR interp present monotonous reduction with increasing height and the maximum is near the surface.
The vertical profiles in Figs. 10e and f are generated from the vertical cross sections in the stratiform region of Figs. 10a-d along the black solid and dashed lines in Fig. 10a. Notably, the vertical structure of stratiform rain is apparently different from that of convective rain in Fig. 9. A clear bright band characteristic is seen in the vertical profiles of TRMM PR and PRGR in Figs. 10e and f, which indicates the melting layer. The maximum is at about 4-4.5 km, which corresponds to the bright band height (parameter "BBheight") of about 4.3 km in the 2A25 product. However, the feature of the bright band is not obvious in the vertical profiles of GR and GR interp, and gentler structures are presented in Figs. 10e and f. Moreover, the maximum in the vertical profiles of GR and GR interp in Fig. 10f appears at about 2.75 km altitude, which is quite different from the brightness height in the TRMM PR profile, and cannot properly represent the characteristics of stratiform precipitation. Overall, the vertical structure of the fused product, PRGR, is closer to that of TRMM PR, inheriting the advantage of high vertical resolution from TRMM PR, and can demonstrate the vertical variation characteristics of precipitation well.