Regional ionospheric modeling using wavelet network model

Mohammed El-Diasty

doi:10.1186/s41445-017-0007-y

Original article
Open Access

Regional ionospheric modeling using wavelet network model

Mohammed El-Diasty^{1, 2}Email author

The Journal of Global Positioning Systems201715:2

https://doi.org/10.1186/s41445-017-0007-y

Received: 16 November 2016
Accepted: 11 May 2017
Published: 22 May 2017

Abstract

A major error component of Global Positioning System (GPS) is the ionospheric delay. Ionopspheric error can be reduced by a dual frequency receiver using a linear combination technique that can not be applied with a single frequecy receiver. However, an accurate ionospheric error modeling for single-frequency receiver is required. Due to the nonlinearity of the ionospheric error, a highly nonlinear wavelet network (WN) method is proposed in this paper. The main objective of the paper is to develop a short-term prediction model based on a short dataset. Therefore, five GPS stations with five days of ionospheric datasets along with time and location were employed to develop the proposed WN-based ionospheric model. Four days of datasets were employed to develop the model and one day of dataset was employed to test the prediction accuracy. To validate the WN-based ionospheric model, a comparison was made between the developed WN-based ionospheric model and the CODE, JPL and IGS Global Ionospheric Map (GIM) models. It is shown that the Root-Mean-Squared (RMS) errors of the developed WN-based ionospheric model are 2.51 TECU, 2.75 TECU and 2.50 TECU (Total Electronic Content Unit) with percentage errors of about 3.4%, 3.8% and 3.4% when compared with the CODE, JPL and IGS GIM models.

Keywords

GPS
Ionospheric delay
Wavelet network
Total electron content (TEC)
GIM model

Introduction

Global Positioning System (GPS) satellites broadcast radio signals in L frequency band and are subject to important distortions while crossing the ionosphere. The ionospheric delay is due to the electron concentration in the ionosphere layers. It varies during the day with the ionisation of the particles hit by sun rays. It is a consequence of the dispersive nature of the medium, which causes sinusoidal waves with different frequencies to travel at slightly different velocities. As a result, the satellite signal is submitted to a group delay and a phase advance of identical amplitudes. The ionospheric delay I is computed as a function of the electron content along the signal trajectory through the ionosphere as follows (Misra and Enge 2006):

$$ I=\frac{40.3* TEC}{f^2} $$

(1)

$$ T E C={\displaystyle \underset{S}{\int }{n}_e(S) dS} $$

(2)

where d is the distance delay (m) in comparison to the propagation in vacuum, TEC is the electron concentration determined along the oblique trajectory (total electron content for the concerned path in el/m2), f is signal frequency (Hz), S is the path from the transmitter to the receiver (m) and n is the electron density (el/m3).

The equation here above only considers the first order effect of ionosphere on signals propagation. The ionospheric delay mathematical representation is actually a limited development. According to the need of precision in the expression of the ionospheric delay the second order effect and the third order effect may be taken into account. The second (1/f³) and third order effect (1/f⁴) are functions of the plasma frequency, the electrons gyrofrequency and the direction of the wave with relation to the magnetic field. In most of the cases only the first order effect is considered to assess the ionospheric delay. In the case of GPS signals, the second order effect is typically of a magnitude of a few centimeters, while the third order effect has a typical magnitude of some millimeters.

All of the GPS errors can be corrected to some extent by implementing model algorithms depending on the applications. A major error component of GPS positioning is the ionospheric delay. However, unlike other GPS errors, ionospheric delay correction is hard and complex to model because the ionosphere shows both spatial and temporal behavior. Ionopspheric error can be reduced by a dual frequency receiver using a linear combination technique that can not be applied for a single frequecy receiver. Operationally for single-frequency receiver, the Klobuchar model is employed to correct for ionospheric error, however, the Klobuchar model permits to correct about 50% of the ionospheric error for mid-latitudes location and average ionospheric environment (Klobuchar, 1975). Therefore, the ionospheric modeling has been investigated for last few decades to develop an accurate ionospheric correction for single-frequency receiver. Currently, GPS analysis centers provide GIMs (Global Ionosphere Maps) on a daily basis. The widely used GPS-derived GIMs are provided by the Center for Orbit Determination in Europe (CODE), the Jet Propulsion Laboratory (JPL) and the International GNSS Service (IGS) with a spatial resolution of 2.5° and 5.0° in latitude and longitude, respectively, and a 2-h temporal resolution (Komjathy 1997; Feltens and Jakowski 2002). However, the Global Ionospheric Map (GIM) models (GIM) models such as CODE, JPL and IGS GIM models cannot reproduce local, short-lasting processes in the ionosphere. In addition, the resolution of these products might not be sufficient to support high quality GPS positioning, especially in the presence of local ionospheric disturbances. The need to produce regional ionosphere models for accurate positioning was investigated by many researchers (Komjathy and Langley, 1996; Hernández-Pajares et al., 1997; Hernandez- Pajares et al. 1999; Liu and Gao, 2003; Wielgosz et al., 2003; Moon, 2004; Leandro and Santos 2007; Sayin et al., 2008; Maruyama, 2007; Liu et al., 2011; Liu et al., 2014; Ohashi et al., 2015 and Razin et al., 2015), where different algorithms were employed for regional ionosphere modeling such as Spherical harmonics, Spline interpolation, Gaussian process, kriging and artificial neural networks. However, due to the nonlinearity of ionosphere physical properties a highly nonlinear model a highly nonlinear wavelet network method is proposed in this paper to model and predict the temporal and spatial variations of ionosphere modeling. The main objective of the paper is to develop a short-term prediction model based on a short dataset. Therefore, five GPS stations with five days of ionospheric datasets along with time and location with 15 min sampling rate are employed to develop the proposed WN-based ionospheric model. Four days of datasets are employed to develop the model and one day of dataset is employed to test the prediction accuracy. Also, a comparison is made between the proposed wavelet network based ionospheric model and the well-established CODE, JPL and the IGS Global Ionospheric Map (GIM) models.

Ionospheric delay estimation

The major range error for GPS measurements is mainly due the deviation of the speed of the signal from its actual light speed because of the presence of free electrons in the ionosphere medium. This medium is extended from 50 km to about 1000 km above the earth surface. The variations of the ionospheric effects are mainly governed by the ionization processes, which is caused by the solar radiation. Hence there is a direct relationship and the state of the ionosphere can be realized by observing the intensity of the solar activity. The physical characteristics of the ionosphere have noticeable diurnal (day and night) variations. During the sun rise, the electron density starts to build up due to the ultraviolet radiations which help to break up gas molecules into ions and free electrons (Leick, 2004; Hofmann-Wellenhof et al., 2008).

Single-frequency receivers can access eight ionospheric coefficients, located in the GPS navigation message to estimate the ionospheric delay based on the Klobuchar model. These coefficients are generated at least once per 6 days but no more than once a day and they are updated by the 5 GPS Ground Control Segment stations. The Klobuchar algorithm is a physical model that considers the changes in latitude, season, solar flux and magnetic activity representing the amplitude change along with the associated diurnal period change of the ionospheric delay. The Klobuchar model permits to correct about 50% of the ionospheric error for mid-latitudes location and average ionospheric environment. Therefore, the ionospheric modeling has been investigated for last few decades to develop an accurate ionospheric correction for single-frequency receiver applications. To develop a regional ionospheric model, the ionospheric error is estimated using dual frequency receivers distributed in the area under consideration as discussed below.

GPS signals are transmitted in two L frequency bands (L1 and L2) and a dual frequency receiver can be used to provide code measurements (P _f1 and P _f2) and carrier-phase measurements (ϕ _f1 and ϕ _f1). The receiver is able to assess the ionospheric delay on f1 using code measurements combination I _P − f1 or using carrier-phase measurements combination I _{ϕ − f1} of identical amplitudes as follows (Hofmann-Wellenhof et al., 2008):

$$ {I}_{P- f1}=\frac{\left({P}_{f1}-{P}_{f2}\right).{f}_2^2}{f_2^2-{f}_1^2} $$

(3)

$$ {I}_{\phi - f1}=\frac{\left({\phi}_{f2}-{\phi}_{f1}\right).{f}_2^2}{f_2^2-{f}_1^2} $$

(4)

The integration of the above code measurements combination and carrier-phase measurements combination along with the ionospheric delay from equation (1) can produce the smoothed value of the TEC as follows:

$$ T E C=\frac{1}{40.3}{\left(\frac{1}{{f_1}^2}-\frac{1}{{f_2}^2}\right)}^{-1}\left(\left({\phi}_{f2}-{\phi}_{f1}\right)-{\left({\phi}_{f2}-{\phi}_{f1}\right)}_0+{\left({P}_1-{P}_2\right)}_0\right)\begin{array}{cc}\hfill \hfill & \hfill \hfill \end{array}\left( el/{m}^2\right) $$

(5)

where (ϕ _f2 − ϕ _f1)₀ and (P ₁ − P ₂)₀ are the initial values of the carrier-phase measurements combination and code measurements combination, respectively, and el is the number of electrons. Fig. 1 shows an example of a noisy and smoothed TEC for one satellite.

Fig. 1
Estimated noisy and smoothed TEC for one satellite

The ionospheric delay is estimated at the ionosphere pierce point (IPP) that is defined as the intersection between the constant ionosphere ellipsoid (350 km above the WGS84 ellipsoid) and the line in view from the receiver antenna reference point to the satellite antenna reference point. Fig. 2 shows he cross-section of main components; Earth, receiver, ionosphere shell, satellite and their spatial relationship. If the elevation angle of a satellite (α) is estimated, the Zenith angle at receiver (z ') and the Zenith angle at IPP (z) can be estimated as follows:

Fig. 2
Ionospheric shell and different angles

$$ z\hbox{'}={90}^{\circ }-\alpha $$

(6)

$$ z={ \sin}^{-1}\left(\frac{R. \sin \left({z}^{\prime}\right)}{R+ h}\right) $$

(7)

It is worth noting that an appropriate cut-off angel is used to ignore those satellites with bad geometry and under horizon level (Hofmann-Wellenhof et al., 2008).

In practice, the ionospheric model is developed using the vertical total electron content (VTEC) that should be estimated at the IPP. Using a simple geometric function, vertical Total Electron Content can be estimated as:

$$ VTEC= T E C\times C o s(z) $$

(8)

where z is the zenith angle at pierce point.

In this paper, the wavelet network model is proposed to model the estimated VTEC form a number of GPS receivers in a regional area and the model was validated by the Global Ionospheric Model (GIM) developed by the CODE analysis center.

Wavelet network model

The wavelet network is an efficient method for data modeling. Zhang and Benveniste (1992) proposed the algorithms of the wavelet network methodology. Afterward, several researchers extended their studies to improve the wavelet network procedure for parameter estimation and learning algorithms (Zhang, 1997). Also, the application of the wavelet network in modeling and prediction has been implemented in several areas of studies such as El-Diasty et. al (2007), Oussar et al. (1998) and Adeli and Samant (2000). It is worth noting that no studies have implemented wavelet networks in regional ionospheric modeling and prediction. A wavelet network is an algorithm connects the neural network with the wavelet decomposition that leads to a wavelet network structure with the highly nonlinear wavelet function. In this research, the tidal height prediction model is developed using wavelet network model with an output ŷ _k computed as:

$$ {\widehat{y}}_k={\displaystyle \sum_{m=1}^{N_m}{c}_i\varPsi \left({a}_m\left({x}_m^k-{b}_m\right)\right)}+ w $$

(9)

where $ {x}_m^k $ is the input neuron, c _i are coefficient variables, a _m are dilation variables, b _m are translation variables, and Ψ is a wavelet function. Fig. 3 shows the wavelet network structure. The wavelet network consists of an input vector of N _m values, a layer of N _i weighted wavelets and an output vector of N _k output neurons. The wavelet network parameters (c _i, a _m, and b _m) can be estimated by a backpropagation-learning method (Haykin 1999; Lekutai, 1997; Zhang and Benveniste, 1992).

Fig. 3
General Wavelet Network Structure (Nm-input, Ni-wavelons, and Nj-outputs). Blue arrows indicate the weights parameters for the connected layers

If N _kis the number of outputs, $ {y}_k^d $ is the desired output values and ŷ _k is the network output estimated from Eqn. (9), then, the wavelet network training objective is to minimize the error function, E (Haykin 1999; Lekutai 1997; Zhang and Benveniste, 1992):

$$ E=\frac{1}{2}{\displaystyle \sum_{k=1}^{N_k}\left({y}_k^d-{\widehat{y}}_k\right)} $$

(10)

The selection of the wavelet function depends on the application. There are several wavelet functions that can be utilized to develop the wavelet network model such as Morlet, Shannon and Mexican hat. We use the Mexican hat in this research to implement the proposed nonlinear regional ionospheric model. The Mexican hat wavelet function for any variable x is:

$$ \varPsi (x)=\left(\kern0.1em {\left\Vert x\right\Vert}^2- p\right)\kern0.5em {e}^{-\frac{{\left\Vert x\right\Vert}^2}{2}}, $$

(11)

where, ‖x‖² = x ^T x, and p is the order of the model (12)

The Mexican hat wavelet function is known as Laplacian operator and represents the second derivative of the Gaussian function (Percival and Walden, 2000). The root-mean-squared (RMS) is commonly used to evaluate the model performance. The RMS error can be computed as:

$$ R M S=\sqrt{\frac{{\left({\displaystyle \sum_{j=1}^{N j}{\displaystyle \sum_{k=1}^{N_k}\left({y}_{k j}^d-{\widehat{y}}_{k j}\right)}}\right)}^2}{N_k.{N}_j}} $$

(13)

The structure of the wavelet network is determined by empirical methods. The number of neurons can be determined by training different architectures with different number of neurons to select the optimal number, based on the lowest RMS error (El-Diasty et al. 2007). It should be noted that the dilation and transition properties of the wavelet function make the wavelet network much more dynamic, flexible, robust, and promising methodology for regional ionospheric modeling and prediction than traditional artificial neural network method.

Methods

The wavelet network method regional ionospheric modeling and prediction was implemented over three major stages as shown in Fig. 4. The implementation of these three stages was performed through; 1) Data preparation stage, 2) Ionospheric modeling and prediction stage and 3) comparison stage. In the first stage, the estimated VTEC for five days long from five RINEX GPS data from the USA CORS network were obtained. In the second stage, a wavelet network model was developed and the well-established CODE, JPL and the IGS Global Ionospheric Map (GIM) models were employed to estimate the VTEC for the regional area under investigation. Then in the third stage, a comparison was made between the developed wavelet network model and the well-established CODE, JPL and the IGS Global Ionospheric Map (GIM) models.

The VTEC were estimated for five days long from five GPS CORS stations in Oklahoma, USA, namely OKTU, OKTE, OKAN, OKMA and OKMU were used to implement the proposed wavelet network model and compare the results with the CODE and JPL GIM models. Fig. 5 shows the geographic location for OKTU, OKTE, OKAN, OKMA and OKMU stations from the CORS map.

Fig. 5
The geographic location for OKTU, OKTE, OKAN, OKMA and OKMU stations from the CORS map

The structure of the wavelet network was built using the Matlab software version 2010. Many wavelet network models were carried out to optimize the structure of the wavelet network using four days of dataset to build the model and one day of dataset to test (prediction mode) the proposed WN-based model. It was found that the wavelet network with the structure [5–90–1] provides the best solution with the lowest root-mean-square (RMS) error. The input layer of five values that represent first input of the day number (one to five), second input of the time of the day (from 0 to 24 in 15 min interval), third input of the latitude of the IPP point (in radians), fourth input of the longitude of the IPP (in radians) and fifth input of the estimated Klobuchar model at same IPP point. The hidden layer of 90 wavelet neurons (wavelons) was employed to model the desired VTEC value.

Results and discussion

In this section, the results of the developed wavelet network model are investigated and a comparison was made between the developed wavelet network based model and the CODE, JPL and the IGS Global Ionospheric Map (GIM) models. It should be noted that the IGS GIM model is a combination of GIM models provided by several analysis centers. All the analysis centers involved may use different approaches to the VTEC derivation from GPS observations, as well as different VTEC representation/modeling techniques. The spatial resolution of the GIM model is 2.5° in latitude and 5.0° in longitude. For comparison purposes, a regional model was extracted from and the CODE, JPL and the IGS GIM models. Fig. 6 shows the estimated IPP positions and the extracted GIM model grid points located in the regional study area.

Fig. 6
The estimated IPP positions and the GIM grid points located in the study area

At the beginning, the estimated VTEC values from the WN-based model, CODE GIM model, JPL GIM model, IGS GIM model and the Klobucher model were investigated. Fig. 7 shows the VTEC values estimated from WN-based model, CODE GIM model, JPL GIM model, IGS GIM model and the Klobucher model in time domain. Then, the VTEC values from the WN-based model, CODE GIM model, JPL GIM model and IGS GIM model were estimated in time and latitude domain. Figs. 8 and 9 show the VTEC values from the WN-based model and IGS GIM model, respectively. It can be seen that the two models show similar diurnal variations in time domain at the same time slots. The other two CODE and JPL GIM models showed similar results as of the IGS GIM model and therefore are not shown in this paper. It should be noted that the gaps in the WN-based model represented the areas with no IPP points during the five days of GPS observations under investigation. Afterwards, the overall performance of the VTEC values from the WN-based model, CODE, JPL and IGS GIM models were investigated. Fig. 10 shows the absolute mean of the VTEC values estimated from the developed WN based model when compared with the CODE, JPL and IGS GIM models. Fig. 11 shows the errors (the difference between the absolute mean of modeled VTEC values) from developed WN based model when compared with the CODE, JPL and IGS GIM models. Tables 1 and 2 illustrate the summary statistical results when the absolute VTEC mean estimated from developed WN based model compared with the ones estimated from CODE, JPL and IGS GIM models for the trained (four days) and the tested (prediction mode for one day) datasets. It can be seen from Tables 1 and 2 that the RMS errors are about 2.51 TECU, 2.75 TECU and 2.50 TECU (Total Electronic Content Unit) when the WN-based model compared with the CODE, JPL and IGS GIM models. It is also shown from Tables 1 and 2, and Fig. 11 that the percentage of the WN-based model error is about 3.4%, 3.8% and 3.4% when WN-based model compared with the CODE, JPL and IGS GIM models and with a maximum absolute error of about 7.17 TECU, 8.17 TECU and 5.74 TECU, respectively. Therefore, in practice the developed WN model can be used for real-time regional ionospheric modeling for accurate GPS positioning with a single frequency GPS receiver and can reduce the ionospheric error with about 96% in average. It is worth noting that the accuracy of the developed short-term WN-based model agrees well with the most recent modeling methods of regional TEC such as spherical cap harmonic analysis model (Liu et al., 2011; Liu et al., 2014), despite the use of short datasets.

Fig. 7
The trained (modeled – four days) and tested (predicted – one day) WN-based VTEC values compared with the CODE GIM model, JPL GIM model, IGS GIM model and the Klobucher model

Fig. 8
The map shows diurnal variations of the WN-based VTEC values (TECU) in a timelatitude domain

Fig. 9
The map shows diurnal variations of the IGS GIM VTEC values (TECU) in a timelatitude domain

Fig. 10
The absolute mean of the WN-based VTEC values compared with the CODE, JPL and IGS GIM models

Fig. 11
The errors (the difference between the absolute mean of modeled VTEC values) from WN-based model when compared with the CODE, JPL and IGS GIM models

Table 1

The summary statistical results when the absolute VTEC mean estimated from wavelet network model is compared with the ones estimated from CODE, JPL and IGS GIM models for training dataset (4 days)

Statistical parameter	WN-based model versus CODE GIM model	WN-based model versus JPL GIM model	WN-based model versus IGS GIM model
Correlation between the WNbased model and GIM model	87.9%	86.7%	87.7%
RMS error between the WNbased model and GIM model	2.51 TECU	2.75 TECU	2.50 TECU
ercentage of error	3.4%	3.8%	3.4%
Absolute VTEC error bias	1.95 TECU	1.90 TECU	1.78 TECU
Absolute VTEC maximum error	7.9 TECU	8.54 TECU	7.3 TECU

Table 2

The summary statistical results when the absolute VTEC mean estimated from wavelet network model is compared with the ones estimated from CODE, JPL and IGS GIM models for testing (prediction) dataset (1 day)

Statistical parameter	WN-based model versus CODE GIM model	WN-based model versus JPL GIM model	WN-based model versus IGS GIM model
Correlation between the WNbased model and GIM model	88.12%	86.5%	88.5%
RMS error between the WNbased model and GIM model	2.50 TECU	2.83 TECU	2.40 TECU
Percentage of error	3.60%	4.2%	3.4%
Absolute VTEC error bias	1.78 TECU	2.03 TECU	1.89 TECU
Absolute VTEC maximum error	7.17 TECU	8.54 TECU	5.78TECU

Conclusion

The main objective of the paper is to develop a short-term prediction model based on a short dataset. An ionospheric model using a wavelet network method was proposed and developed in this paper. GPS data from five stations for five days long were used to implement and validate the proposed model. The wavelet network structure of 5–90–1 gave the best performance solutions (i.e., the minimum RMS), and therefore was used in modeling the VTEC values. It is shown that the Root-Mean-Squared (RMS) errors of the developed WN-based ionospheric model are 2.51 TECU, 2.75 TECU and 2.50 TECU (Total Electronic Content Unit) with percentage errors of about 3.4%, 3.8% and 3.4% when compared with the CODE, JPL and IGS GIM models and with a maximum absolute error of about 7.17 TECU, 8.17 TECU and 5.74 TECU, respectively. Therefore, in practice the developed WN model can be used for real-time regional ionospheric modeling for accurate GPS positioning with a single frequency GPS receiver and can reduce the ionospheric error with about 96% in average.

Declarations

Competing interest

The author declare that they have no competing interests

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Authors’ Affiliations

(1)

Department of Hydrographic Surveying, Faculty of Maritime Studies, King Abdulaziz University, Jeddah, Saudi Arabia

(2)

Engineering Department of Public Works, Faculty of Engineering, Mansoura University, Mansoura, Egypt

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