Abstract
Several models for estimating sporadic-E intensity from Global Navigation Satellite System (GNSS) radio occultation (RO) observation have previously been developed using a single perturbation or intensity parameter, such as phase-based total electron content (TEC) or the amplitude-based S4 index. Here, we outline two new models that use a combination of phase and amplitude parameters for the L1 and L2 signals. These models show a significant improvement over the baseline models used for comparison. Furthermore, the GNSS-RO parameters are compared with several different ionosonde intensity parameters including the direct foEs and fbEs measurements along with the metallic-ion based foEs and fbEs parameters which account for the background E-region density. Interestingly, the phase-based scintillation index shows the strongest correlation to foEs and fbEs while amplitude-based S4 shows the strongest correlation to foEs and fbEs. While the metallic-ion based foEs and fbEs parameters are physically ideal for GNSS-RO observations, we show difficulties in practical implementation due to the reliance on a background E-region density estimate using a model such as the International Reference Ionosphere (IRI). Ultimately, we provide two improved sporadic-E intensity models that can be used for future GNSS-RO based studies along with a recommendation to compare against the ionosonde-based foEs parameter.
1 Introduction
Sporadic-E (Es) is characterized by an unusually dense plasma at E-region altitudes caused by elevated metallic-ion densities from meteor deposits converged through neutral wind shears (; ; ; ). These enhanced ion layers can significantly affect radio propagation, especially high-frequency (HF) skywaves (; ) and Global Navigation Satellite System (GNSS) signals used for Low Earth Orbit (LEO) satellite position and timing (). Therefore, understanding both the global occurrence rates (; ; ; ) and Es intensities [i.e., peak ion densities; ; ; ] are vital to many aspects of our modern civilization.
While ionosondes provide direct measurements of Es intensities in terms of the peak blanketing frequency, fbEs, and the peak frequency of the ordinary mode return, foEs, ionosondes are inherently land-locked with a sparse distribution throughout the globe (e.g., see Digisonde stations at https://giro.uml.edu/). For this reason, we must use indirect measurements of Es intensities obtained through GNSS radio occultation (RO) to obtain truly global coverage (; ; ; ; ; ). However, the indirect nature of GNSS-RO observations makes it difficult to accurately extract Es parameters, resulting in large uncertainties and ambiguities (; ).
Specifically, many GNSS-RO techniques have been proposed to extract sporadic-E intensities from phase (; ; ) and amplitude (; ) perturbations using direct ionosonde measurements for validation. The phase techniques referenced above rely on total electron content (TEC) calculations using L1 (1,575.41 MHz) and L2 (1,227.60 MHz) phase-based perturbations while the amplitude-based techniques use an L1 scintillation index such as S4 to estimate Es intensities. No technique that we are aware of uses both amplitude and phase information for intensity estimates. Furthermore, phase perturbation techniques will be affected by phase scintillation (σϕ) for stronger Es layers (), and the amplitude scintillation indices have been shown to plateau for stronger layers ().
To further complicate matters, it is unclear which ionosonde-based Es intensity measurement is appropriate for comparison against GNSS-RO observations. Ionosondes provide two commonly used Es intensity parameters: fbEs and foEs. The fbEs typically correspond to more uniform layers that block HF signals from penetrating with frequencies below the fbEs, while the foEs correspond to the peak plasma frequency measured in patchy or cloudy layers (). The GNSS-RO community is generally divided on which parameter to use for comparison, with some using foEs as the validation parameter (; ; ) and others using fbEs (; ). Furthermore, GNSS-RO measurements have been shown to actually measure the metallic-ion density perturbation from the background E-region plasma density, which requires a conversion of foEs/fbEs to foμEs/fbμEs as outlined by . These metallic-ion foμEs and fbμEs parameters are calculated by subtracting the electron density of the background E region from the total ion density derived from foEs or fbEs, such that the metallic-ion density is obtained for the Es layer. No GNSS-RO technique that we are aware of uses these perturbation-based metallic-ion parameters for comparison.
In this study, we develop two improved models for sporadic-E intensity using a combination of L1 and L2 amplitude and phase data in comparison with ionosonde observations. Additionally, we create separate models for foEs, fbEs, foμEs, and fbμEs to determine which parameter shows the strongest agreement with ionosonde observations. The results outlined below show a significant improvement in the Es intensity estimates from GNSS-RO observations, which can be used to refine global empirical models and provide valuable near-real-time information to radio operators.
2 Materials and methods
COSMIC-I 50 Hz atmPhs data obtained from the COSMIC Data Analysis and Archive Center (CDAAC; https://cdaac-www.cosmic.ucar.edu/cdaac/index.html) from 2010 to 2017 are used for GNSS-RO observations. Since GNSS-RO methods do not provide a direct measurement of sporadic-E intensity, a separate dataset must be used for validation. Here, we use ionosonde foEs and fbEs measurements obtained through the Digital Ionogram DataBase (DIDBase; https://giro.uml.edu/didbase/) as the validation data set. Due to the large number of ionograms analyzed in this study, we rely on ionograms automatically scaled by Automatic Real-Time Ionogram Scaler with True height software, version 5 [ARTIST-5; ()]. Most Digisondes incorporated ARTIST-5 around 2010, which is why RO data before 2010 are not included in this comparison. No Confidence Score (CS) threshold was implemented on the automatically scaled ionograms due to the fact that the CS grading criteria is based on standard electron density profiles that deduct points for irregularities like sporadic-E (). Requiring high CS values can unintentionally remove ionograms with reliable sporadic E measurements, which would be detrimental to this analysis.
Uncertainties in ARTIST-5 predictions have recently been quantified by through a comparison with manually scaled ionograms. They found an foEs error bound of [−0.80, 0.35] MHz for the ARTIST-5 estimates minus manually scaled values. This interval contains 95% of the ionograms in the comparison, providing an uncertainty range for the validation dataset used in the present study.
Figure 1 shows example ionograms and the corresponding GNSS-RO amplitude and phase profiles measured with and without sporadic-E present. The amplitude scintillation and phase perturbation caused by the sporadic-E layer is immediately obvious, especially when compared against the measurements without sporadic-E. To limit the spatial and temporal difference between ionosonde and GNSS-RO measurements, RO tangent points must be within 30 min and 50 km of an ionogram that measures sporadic-E. This spatial extent corresponds to half of the 100 km median length of sporadic-E layers as observed by , such that a layer directly over an ionosonde can be observed within a 50 km radius. While reducing the comparison distance causes a reduction in the overall number of concurrent measurements, it allows for more confidence in the fact that both the ionosonde and occultation are measuring the same layer. We also examined larger comparison distances (results not shown), which produced similar results with larger uncertainties caused by measurements of separate Es clouds or RO observations that miss the clouds altogether. All concurrent (within 30 min and 50 km) COSMIC-1 GNSS-RO and DIDBase ionosonde measurements throughout the globe during 2010–2017 are used for this analysis.
FIGURE 1
As a baseline for comparison, two commonly used RO techniques for estimating sporadic-E intensity are included in the results: the S2 amplitude scintillation-based technique from and the total electron content (TEC) based technique from . Note that we use S2 for the amplitude scintillation index here instead of the S4 intensity scintillation index following the definition with COSMIC-1 signal-to-noise-ratio (SNR [V/V]) corresponding to the signal amplitude. The model was selected instead of the updated () S4 model, as we calculate all parameters directly from the CDAAC 50 Hz atmPhs files, while the technique uses scnLv1 files that are calculated in a slightly different manner (see ). After the S2 is calculated using a sliding window of 50 points (one second in time for 50 Hz atmPhs data), the empirical conversion fEs [MHz] = 3.8×S2 + 2.0 is used to calculate the sporadic-E intensity fEs. Throughout this comparison, we use fEs for the GNSS-RO derived intensities instead of foEs, fbEs, etc., as it is unclear which (if any) of the ionosonde specific parameters is measured by RO.
The technique uses the L1 and L2 phases to calculate a TEC, which is then detrended with a Savitzky-Golay () filter using a 25 km window. The detrended TEC is then smoothed using a 1 km Savitzky-Golay filter, and the final TEC perturbation is divided by an effective path length of 176 km for an assumed vertical thickness of 0.6 km () to obtain an electron density for the layer. This technique provides a physically straightforward approach to estimate layer intensities. However, it relies on the assumption of an unknown path length (horizontal length) that can introduce a large uncertainty into the calculations.
In addition to the S2 and TEC calculations discussed above, a variety of scintillation and perturbation parameters are calculated for each RO crossing to examine previously unexplored relationships with sporadic-E intensity. These parameters include the amplitude scintillation index S4, the standard deviation of the nondetrended (measured) excess phase σϕ, and the phase perturbation Δϕ calculated from a 25 km Savitzky-Golay filter used for detrending. All these parameters are calculated for both the L1 and L2 frequencies. A list of the parameters and additional details on the calculations are displayed in Table 1. The size of the sliding windows and the number of detrending iterations (zero or one) for S4, σϕ, and Δϕ were optimized to improve correlations with the ionosonde foEs and fbEs data.
TABLE 1
| Parameter | Units | Calculation details |
|---|---|---|
| L1 S2 | V/V | 50 point sliding window of |
| L1 and L2 S4 | V2/V2 | 121 point sliding window of |
| L1 and L2σϕ | m | 51 point sliding window of |
| L1 and L2 Δϕ | m | ϕ(z) detrended with 25 km SG filter |
| TEC | TECU | TEC(z) detrended with 25 km SG filter; smoothed with 1 km SG filter |
Details on the GNSS-RO scintillation and perturbation parameters calculated from 50 Hz atmPhs observations of sporadic-E. Here, SNR is the signal amplitude, ϕ is the excess phase, z is the altitude, SG stands for Savitzky-Golay, and ⟨ ⟩ denotes the average over the specified window. The S2 and S4 formulas shown here follow for COSMIC-1 SNR representing the signal amplitude.
IRI-2016 () is used to estimate the background E-region ion density required for foμEs and fbμEs calculations. Following the procedure described by , the background E-region ion density at the sporadic-E altitude is estimated by IRI and is subtracted from the foEs (fbEs) to obtain the metallic-ion density, which can be converted to a frequency foμEs (fbμEs). While ionosondes provide the virtual height of the sporadic-E layer, h’Es, the actual height can be estimated by integrating the group index of refraction over altitude to find the actual height corresponding to the measured virtual height [see further description in ]. The actual height is calculated from the IRI electron density profile (EDP), then the background E-region ion density is set to the IRI density at the calculated Es actual height. While this places a strong reliance on IRI predictions for the metallic-ion intensity parameters, we use IRI instead of ionosonde derived EDPs for two reasons: first, blanketing sporadic-E can block the ionosonde returns from the background E-region completely, such that the Digisonde EDP inversion process relies on climatology. Second, to extend this approach to locations without ionosondes in application of the GNSS-RO techniques for global climatology, etc., a model will be required as no local EDP measurements will be available.
The foμEs and fbμEs parameters are derived from metallic-ion density perturbations to the background E-region ionosphere (). Physically, this perturbation is vitally important for quantifying the impacts of Es layers on GNSS-RO signals, as the primary factor in the signal perturbation magnitude is the vertical index of refraction (plasma density) gradient (). The background E-region density gradient is too small to cause significant diffraction in the GNSS-RO signals, while vertically thin sporadic-E layers provide sufficiently large vertical density gradients (see Figure 1). Therefore, the background E-region contribution is insignificant when quantifying the strength of sporadic-E layers for GNSS-RO signal perturbations, and the background densities should be removed to provide the metallic-ion based foμEs and fbμEs parameters. As discussed in Sections 3 and 4, while the physical reasoning behind this conversion makes sense for GNSS-RO applications, the practical implementation is rather difficult.
3 Results
3.1 Relationship between Es intensity parameters
GNSS-RO signals are prone to significant phase perturbations from Es layers, which cause diffraction patterns that are dependent on the vertical thickness and total phase contribution (; ; ). The total phase contribution depends on both the metallic-ion density and the horizontal length of the layer through which the signal crosses. Since the normal E-region varies relatively slowly with altitude (in comparison with Es layers), the phase contribution to the plane-wave GNSS-RO signal is nearly uniform over a small altitude range and does not result in significant perturbations or diffraction. In contrast, the relatively thin vertical thickness of sporadic-E [∼1.5 km; ] acts like a negative lens capable of producing significant perturbations to the RO signals. Therefore, as outlined in , GNSS-RO measurements are sensitive to the metallic-ion density in Es, not to the total ion density that includes the background E-region.
In terms of Es intensity parameters, this metallic-ion density can be estimated from foEs and fbEs through conversion to foμEs and fbμEs, which removes this background E-region contribution. Physically, this argument suggests that the GNSS-RO fEs intensity estimates should only be compared to ionosonde derived foμEs and fbμEs. However, in practice, our reliance on models or low-confidence EDP estimates from ionosondes (because of the presence of sporadic-E) makes it difficult to obtain accurate background E-region densities. This point will be discussed in more detail later, but first we focus on the relationships between these different intensity parameters.
Figure 2 shows the relationships between the different Es intensity parameters. A lower limit of 1 MHz was placed on the foμEs and fbμEs values as the perturbation to GNSS-RO signals would be minor for these weak layers. The different intensity parameters generally show a strong correlation in terms of Spearman’s ρ used throughout this study for potentially nonlinear trends. As expected, the foμEs and fbμEs values are lower than the foEs and fbEs values, with a collection of data points near the 1:1 line corresponding to weak background E-region densities measured at night. Here, night corresponds to a solar zenith angle greater than or equal to 90°, which is roughly 40% of the Es measurements used in this analysis. Calculated linear slopes of 0.8 and 0.6 are found for the foEs to foμEs and fbEs to fbμEs conversions, respectively.
FIGURE 2
For ionosonde measurements with both foEs and fbEs measured, the relationship shows that most fbEs values are close in magnitude to the foEs values. However, there are several ionograms that show strong foEs with weak fbEs. This results in a linear fit with a slope of 0.8 to convert foEs to fbEs.
In an attempt to determine whether fbEs could be used as a proxy for foμEs, the two parameters were compared. From the results, we see that the relationship is relatively weak with a linear fit that results in a slope of 0.6 and an R2 of 0.4. This indicates that fbEs should not be used as an easy-to-obtain proxy for foμEs.
The nontrivial relationships between the different Es intensity parameters make it difficult to choose a single parameter for comparison with GNSS-RO observations. While the metallic-ion parameters are physically more appropriate, the additional uncertainty introduced by model estimates of the background E-region may weaken the overall relationships with RO derived parameters. Therefore, we decided to include all four intensity parameters in our model development to determine which of the parameters is the most practical to use when comparing with GNSS-RO observations.
3.2 GNSS-RO parameters vs. ionosonde intensity parameters
Ionosonde intensity parameters are displayed against the GNSS-RO scintillation and perturbation parameters in Figures 3–6. Thresholds are placed on the GNSS-RO parameters to remove outliers for quality control, and the values for each parameter are displayed in Table 2. These phase-based thresholds were determined from visual inspection of the results, but a future evaluation of the values using simulated profiles may provide an improved approach with a physical basis. For amplitude scintillation, strong signal focusing can result in S4 saturation with indices around 1.5 (
FIGURE 3

Ionosonde derived foEs as a function of GNSS-RO scintillation and perturbation parameters. Note the relatively strong correlation with .
FIGURE 4

Same as Figure 3 but for fbEs. Similar to foEs, there is a relatively strong correlation with .
FIGURE 5

Same as Figure 3 but for foμEs. Note the moderate correlation with S4 and weak correlation with TEC.
FIGURE 6

Same as Figure 3 but for fbμEs. Note the moderate correlations with S4 and .
TABLE 2
| Parameter | Threshold |
|---|---|
| L1 and L2 S4 | 2.0 V2/V2 |
| L1 and L2σϕ | 0.5 m |
| L1 and L2 Δϕ | 0.8 m |
| TEC | 7 TECU |
| Actual Height | 80 km ≤ Altitude ≤135 km |
Thresholds placed on GNSS-RO perturbation and scintillation parameters and Es actual heights to remove outliers for quality control.
For foEs (Figure 3), L1 and L2σϕ show relatively strong correlations with ρ > 0.6. Linear fits also present larger slopes that reach an foEs of 6 MHz for maximum values of L1σϕ, which is not reached for any other parameter. This supports the results of
The results and trends for fbEs are similar to foEs but with stronger correlations (Figure 4). This stronger correlation may be due to the more uniform nature of blanketing Es layers compared to the patchy/cloudy layers (
Unlike foEs, the foμEs estimates show the strongest correlations with S4 (Figure 5). However, the correlations are weaker and there are many low foμEs values for large values of the RO parameter. This is most obvious for TEC, which shows a moderate correlation with foEs, but a weak correlation to foμEs along with a nearly flat linear fit (slope near zero). The collection of low foμEs points is likely due to uncertainties in the background E-region densities introduced by IRI in the foEs to foμEs conversion. These weaker correlations and linear fits highlight the practical challenges of using the metallic-ion parameters. While these metallic-ion parameters are certainly more appropriate for GNSS-RO measurements, the uncertainties introduced by using a model to estimate the background E-region can add unwanted errors to the dataset.
The fbμEs estimates show moderate correlations with S4 and σϕ (Figure 6). However, the correlations are weaker than for fbEs, likely due to the uncertainty added by the IRI estimates, as discussed for foμEs. All of the GNSS-RO scintillation and perturbation parameter correlations with ionosonde derived intensity parameters are statistically significant with p-values ≤0.01. Only the TEC correlation with foμEs provides a p-value of 0.01, while all others are less than 0.01.
3.3 Model development and feature importance
To select an appropriate model for predicting Es intensities (fEs) using GNSS-RO perturbation and scintillation parameters, the Lazy Predict regression package implemented in Python (https://pypi.org/project/lazypredict/; accessed July 2023) was used to test a variety of models on this particular dataset. From Lazy Predict (results not shown), the top performing models for all intensity parameters were Epsilon Support Vector Regression (SVR) and Random Forest, as implemented through scikit-learn (
In addition to the SVR model, a multiple linear regression model (MLR) is developed to provide a simplified approach for relatively easy implementation. Further, the two newer models are compared to previous GNSS-RO based fEs models from the literature. Specifically, the TEC technique described in
A train–test split was implemented using data before 1 January 2015 for training and data after for testing. This results in a roughly 70%–30% split for training–testing. The total number of data points for each ionosonde intensity parameter is displayed in Table 3. Only the training data set is used for model development and tuning.
TABLE 3
| foEs | fbEs | foμEs | fbμEs | |
|---|---|---|---|---|
| Train | 408 | 139 | 290 | 133 |
| Test | 185 | 56 | 135 | 55 |
The number of observations used for training and testing, split by ionosonde intensity parameter.
For model development, a Permutation Feature Importance (PFI) was calculated for each of the model features (GNSS-RO perturbation and scintillation parameters) and ionosonde intensity parameters. PFI shows the decrease in a metric from randomly shuffling the feature of interest. Here, we use a composite metric based on an equal weighting of MAE and R2. The features with the largest decrease are generally the most important features in terms of model performance. As displayed in Figure 7, all ionosonde intensity models except fbEs show the L1 S4 as the most important feature, which supports the heavy reliance on amplitude scintillation in previous GNSS-RO-derived Es intensity estimates [e.g.,
FIGURE 7

Permutation Feature Importance (PFI) for the GNSS-RO scintillation and perturbation parameters in a linear SVR model. The bars correspond to the mean decrease in the MAE–R2 composite metric from randomly shuffling the feature of interest with 1,000 iterations, and the error bars correspond to the standard deviation.
The relative feature importance varies dramatically between the different ionosonde intensity parameters. For example, TEC is the most important for fbEs and is a close second to the L1 S4 for foEs, but it is the least important feature for foμEs and fbμEs. Generally, L2σϕ is important to foEs and fbEs while L2 S4 is important for the metallic-ion (μ) models.
Interestingly, the relative importance of the different features do not match the relative strength of the linear fit R2 and Spearman ρ values displayed in Figures 3–6. For example, the strongest linear fit values for the GNSS-RO parameters to foEs (Figure 3) are from σϕ, while L1 S4 and TEC are the most important features in the SVR model. This is likely due to differences between simple linear regression and SVR, which places different weights and penalties on the data (
For the final SVR and MLR models, we use the top four most important features for each ionosonde intensity parameter to build the final model. Future studies can focus on reducing the number of input variables while maintaining performance, but here we use four parameters for each model for simplicity and consistency. The SVR ϵ and regularization (C) parameters were also tuned to optimize performance using the MAE–R2 composite metric [a description of these SVR parameters can be found in
TABLE 4
| foEs | fbEs | foμEs | fbμEs | |
|---|---|---|---|---|
| ϵ | 0.4 | 0.2 | 0.4 | 0.2 |
| C | 4.3 | 5.9 | 5.1 | 5.1 |
The SVR ϵ and C parameters optimized for each ionosonde intensity parameter.
For reference, the MLR slopes and intercepts are displayed in Table 5 for each ionosonde intensity parameter. While four GNSS-RO perturbation and intensity parameters were used for each model, a couple of parameters have negative slopes, indicating that the number of input parameters can be fine-tuned in future studies to optimize and simplify the models. It must also be noted that the various GNSS-RO parameters are not independent, and the complex mapping from Es characteristics to RO diffraction patterns is not fully understood. This mapping was explored in detail in
TABLE 5
| Intensity | |
|---|---|
| Parameter | MLR Model |
| foEs | fEs = 1.54 × L1S4 + 0.08 × TEC + 4.22 × L2σϕ + 0.15 × L2S4 + 1.75 |
| fbEs | fEs = 0.14 × TEC + 0.47 × L1S4 + 1.57 × L2σϕ + 7.02 × L1σϕ + 1.56 |
| foμEs | fEs = 1.76 × L1S4 + 0.37 × L2S4 + 5.88 × L1Δϕ − 3.47 × L2Δϕ + 1.62 |
| fbμEs | fEs = 1.25 × L1S4 + 0.15 × L2S4 − 1.23 × L2Δϕ + 3.24 × L2σϕ + 1.43 |
GNSS-RO MLR intensity models for each ionosonde intensity parameter. The units and parameter calculation details are displayed in Table 1.
To quantify the statistical significance of the new MLR model, an F-test was performed on the training dataset testing against the null hypothesis that all model parameters are zero. The F-test produced a minimum F-statistic of 22 for the fbμEs model with an associated p-value of 0.001. All other models produced larger F-statistics and lower p-values, indicating a very high significance in the results which allows us to reject the null hypothesis and conclude that the model results are not due to randomness.
3.4 Model performance
GNSS-RO fEs estimates are displayed against the ionosonde intensity parameters in Figures 8–11. Linear fits and uncertainties are calculated using a bootstrapping approach from 10,000 samples with replacement (
FIGURE 8

GNSS-RO fEs estimates versus ionosonde foEs observations. Slope and intercept uncertainties are from the standard errors. Note the improved performance for the MLR and SVR models relative to the baseline S2 and TEC models. The unfilled markers correspond to daytime measurements while the filled markers designate nighttime measurements.
FIGURE 9

GNSS-RO fEs estimates versus ionosonde fbEs observations. The unfilled markers correspond to daytime measurements while the filled markers designate nighttime measurements. Note the relatively large slope for the TEC-based technique.
FIGURE 10

GNSS-RO fEs estimates versus ionosonde-based foμEs observations. The unfilled markers correspond to daytime measurements while the filled markers designate nighttime measurements. Note the nearly flat slope for the TEC-based technique and the weaker performance for the MLR and SVR models relative to Figure 8.
FIGURE 11

GNSS-RO fEs estimates versus ionosonde-based fbμEs observations. The unfilled markers correspond to daytime measurements while the filled markers designate nighttime measurements. Note the low MAE for the MLR and SVR models.
Predictions from the foEs models are displayed in Figure 8. The TEC technique generally underestimates, resulting in a negative R2 value and an MAE of 0.9 MHz. Negative R2 values indicate that the model predictions have a larger sum of squared residuals than a model that simply predicts the average of the observed data, which corresponds to R2 = 0. In other words, the average of the squared residuals is larger than the variance in the observed data, which can indicate a bias in the model as observed here. The S2 approach has a positive but weak R2 with a low slope and a narrow spread of estimates, resulting in an MAE of 0.7 MHz.
Both the MLR and SVR approaches perform similarly, with moderate R2 values and a low MAE of 0.5 MHz. It must be noted that this MAE is within the range of ARTIST-5 foEs error bounds [(−0.80, 0.35) MHz;
Similar behavior is observed for the fbEs estimates (Figure 9), with a general improvement in the fEs estimates by the MLR and SVR models. Interestingly, all of the models perform slightly worse for fbEs than foEs, except for the TEC approach, which shows a slight improvement. This general decrease in performance for fbEs models may be due to the limited number of data points compared to foEs. However, the decrease in MLR and SVR performance is slight, with MAEs increasing from 0.5 to 0.6 MHz. As with foEs, both the MLR and SVR models perform better for daytime measurements.
The metallic-ion based foμEs results are displayed in Figure 10, which show similar performance for the fbEs estimates for all models except for TEC. TEC fEs estimates show a drastic decrease in performance with a nearly flat slope of fEsRO ≈ 0.2 foEsDigi. This poor performance of the TEC model is likely an artifact of the foEs to foμEs conversion that relies on IRI, which introduces an additional uncertainty into the estimates. The large collection of data points with low foμEs and a large spread of TEC values on the left side of the TEC figure is likely caused by overestimates of the background E-region densities, resulting in a cluster of small foμEs values. While this behavior is also observed in the other foμEs models, they are less severe resulting in slopes between 0.4 and 0.5 instead of the TEC slope of 0.2. Unlike foEs and fbEs, the MLR and SVR models for foμEs perform better for nighttime measurements, due to overestimates of the daytime background E-region densities used in the foEs to foμEs conversion.
The fbμEs estimates also show a bias towards lower fbμEs values due to overestimates of the background E-region densities (Figure 11). However, this bias is most obvious in the S2 model, while the TEC model performs significantly better than the TEC foμEs model. The MLR and SVR models have the lowest MAE values of 0.4 MHz of all ionosonde intensity parameters, but the R2 values and slopes are slightly lower than the foEs models. This low MAE is likely the result of lower intensities with a peak fbμEs of approximately 4 MHz, compared to the peak foEs magnitudes above 6 MHz.
4 Discussion
Several interesting results have emerged from this study. First, it appears that while the physical reasoning of the metallic-ion foμEs and fbμEs parameters is appropriate to quantify the EDP enhancement induced by Es (
A second interesting result is the strong correlations of the different ionosonde intensity parameters with respect to the phase scintillation parameter σϕ (Figures 3–6). Many previous studies have used phase-based perturbations (
Finally, while it is no surprise that the newly developed multiple linear regression (MLR) and support vector regression (SVR) models improved intensity estimates for each ionosonde parameter, the relatively low fEsRO to fEsDigi slopes of 0.5 show that these new models still struggle to predict intensities for stronger layers (Figures 8–11). The difficulty in predicting larger fEs values is due to the strong dependence of the models on S4, which is known to saturate for strong layers (
Perhaps the largest obstacle in the quest to develop accurate Es intensity estimates from GNSS-RO observations is the variable nature of the spatial extent and orientation of sporadic-E. Given the cylindrical horizontal shape of the Es layers with wide distributions in both horizontal extent (
In addition, small-scale structures and turbulence caused by Kelvin-Helmholtz instabilities (
These various factors result in an inherent uncertainty to the fEs intensity estimates from GNSS-RO observations, which may be difficult to resolve without the help of additional sensors or multiple GNSS-RO observations with sufficient spatial resolution. Luckily, the current global RO spatial and temporal measurement density allows for high resolution analyses, as recently demonstrated for sporadic-E (
5 Conclusion
Two new models of sporadic-E intensity from GNSS-RO observations were developed and compared with ionosonde observations. The new models were developed using L
1and L
2GNSS-RO measurements through sporadic-E layers within 50 km and 30 min of ionosonde observations, providing concurrent measurements of GNSS-RO phase and amplitude perturbations along with ionosonde intensity parameters foEs and fbEs. Metallic-ion-based fo
μEs and fb
μEs intensity parameters were also calculated using IRI-2016 to remove the background E-region ion density from the ionosonde foEs and fbEs observations, providing estimates of the metallic-ion density perturbations to the slowly varying background ionosphere. The key results are summarized below:
• Multiple linear regression (MLR) and support vector regression (SVR) models demonstrate a drastic increase in performance over the baseline TEC and S2 approaches. This increase in performance is due to the inclusion of both L1 and L2 phase and amplitude perturbation and scintillation indices, instead of only relying on phase (TEC) or amplitude (S2).
• While the new models showed better performance overall, they struggled to predict the strong Es layer intensities, likely due to a heavy reliance on S4 which is known to saturate.
• Comparisons of the various ionosonde intensity parameters (foEs, fbEs, foμEs, and fbμEs) with GNSS-RO perturbation and scintillation parameters showed a strong correlation with phase scintillation σϕ. This σϕ parameter has not been widely implemented in GNSS-RO monitoring of sporadic-E, and here we recommend a closer inspection of the usefulness in future studies.
• Finally, while the metallic-ion-based foμEs and fbμEs parameters are the most physically ideal parameters to compare against GNSS-RO observations, the reliance on modeled background E-region densities makes the practical implementation difficult. The uncertainty introduced by the ionospheric model (here we used IRI-2016) can outweigh the original uncertainties from direct foEs and fbEs measurements. Given the large number of foEs observations relative to fbEs, we recommend comparing GNSS-RO with ionosonde-derived foEs for future development.
Implementation of either the MLR or SVR models outlined here can help improve GNSS-RO-based intensity estimates for global climatologies, morphologies, and radio operations.
Statements
Data availability statement
The raw data supporting the conclusion of this article will be made available by the authors, without undue reservation.
Author contributions
DE: Conceptualization, Formal Analysis, Investigation, Writing–original draft, Writing–review and editing. DW: Conceptualization, Formal Analysis, Investigation, Writing–original draft. NS: Conceptualization, Formal Analysis, Investigation, Writing–original draft. AA: Conceptualization, Formal Analysis, Investigation, Writing–original draft. JE: Conceptualization, Formal Analysis, Investigation, Writing–original draft. KF: Conceptualization, Formal Analysis, Investigation, Writing–original draft. KO: Conceptualization, Formal Analysis, Investigation, Writing–original draft.
Funding
The author(s) declare financial support was received for the research, authorship, and/or publication of this article. This research was funded by the Air Force Office of Scientific Research (AFOSR/RTB1), and NASA’s Living With Star and Sun-Climate research funds to the Goddard Space Flight Center (GSFC) under WBS 936723.02.01.12.48.
Acknowledgments
We would like to thank the Digital Ionogram Database (DIDBase) and the COSMIC Data Analysis and Archive Center (CDAAC) for the use of their data.
Conflict of interest
The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.
Publisher’s note
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Summary
Keywords
sporadic-E, GNSS radio occultation, ionosondes, foEs, fbEs, foμEs, fbμEs
Citation
Emmons DJ, Wu DL, Swarnalingam N, Ali AF, Ellis JA, Fitch KE and Obenberger KS (2023) Improved models for estimating sporadic-E intensity from GNSS radio occultation measurements. Front. Astron. Space Sci. 10:1327979. doi: 10.3389/fspas.2023.1327979
Received
25 October 2023
Accepted
04 December 2023
Published
22 December 2023
Volume
10 - 2023
Edited by
Shun-Rong Zhang, Massachusetts Institute of Technology, United States
Reviewed by
Bingkun Yu, Deep Space Exploration Laboratory, China
Sampad Kumar Panda, K L University, India
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Copyright
© 2023 Emmons, Wu, Swarnalingam, Ali, Ellis, Fitch and Obenberger.
This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.
*Correspondence: Daniel J. Emmons, daniel.emmons@afit.edu
Disclaimer
All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article or claim that may be made by its manufacturer is not guaranteed or endorsed by the publisher.