R.J. Norman(1), P.L. Dyson(1) and J.A. Bennett(2)
(1) School of Physics
La Trobe University
Bundoora, Victoria 3083
Australia
r.norman@latrobe.edu.au (2) ABSTRACT
Phone +61 3 9479 2637
Monash University
Clayton, Victoria 3168
Australia
Preliminary work by Houminer et al, (1996) proposed that sporadic E clouds or patches could be mapped using Backscatter Sounders (BSS). Their technique has been developed further in this study (see also Norman et al 1998) such that synthesized backscatter ionograms in conjunction with an ionospheric model containing a sporadic E layer are used to map and model different types of Es.
The Quasi-Parabolic Segment (QPS) model (Dyson and Bennett, 1988) is an analytic ionospheric model and is commonly used to represent the Earth’s ionospheric profile. The QPS model, consists of 5 QPS’s, and produces integrable terms when solving for the ray parameters. The 5 QPS’s represent the three ionospheric layers namely the E, F1 and F2 layers. The required inputs of the QPS model are the peak plasma frequencies, the peak heights and the semi-thickness of each of the three ionospheric layers. In this study a further layer is added to the QPS model representing a Es layer. This new analytic ionospheric model is referred throughout this study as the 4 Layer or 4L model. The only added inputs that this model requires are the peak plasma frequency foEs and the height of the peak plasma frequency of the Es layer, hmEs.
The method of mapping Es in this paper is very simple and makes use of the thickness, and maximum operating frequency, of the Es echo traces on the BSI and assumes that the Es behaves as a spherical mirror. The equations determining the distance of the Es cloud from the transmitter/receiver location as well as the peak plasma frequency and the extent of the Es clouds are presented. The effects of patches of Es and some examples of partial reflection from Es are also presented. Two example backscatter ionograms from the Jindalee Stage B data (after Houminer et al 1996) containing Es echo traces are also presented and clearly demonstrate the ease and effectiveness of the modeling and mapping techniques. It should be noted that the effects of beam spreading, multiple hops, antenna patterns and absorption, on the BSI, have been ignored throughout this study.






If hmEs > hmE, a similar approach to that described above can be implemented or a 4 layer ionospheric model using the same criteria as the 3 layer, or QPS model can be used. Using the latter option there will be know valley regions between the layers so if hmE < hmEs < hmF1, and
foEs > foF1 then the F1 layer is ignored and the sporadic E layer fits directly to the F2 layer. Both methods work well, producing realistic results.
foF2 = 4.9 MHz ymF2 = 125.0 km hmF2 = 230.0 km
foF1 = 4.0 MHz ymF1 = 20.0 km hmF1 = 142.6 km
foE = 3.12 MHz ymE = 11.0 km hmE = 102.0 km
foEs = 4.0 MHz ymEs = 1.0 km hmEs = 90.0 km
A very narrow QP layer in Figure 1 represents the sporadic E. This sporadic E layer has a semi-thickness of 1 km, peak height of 90 km and peak plasma frequency of 4 MHz. Figure 2 shows a blow up of the Es. Clearly, a parabolic layer smoothly attached to the rest of the ionospheric profile represents the Es. The valley region between the E and Es consists of two smoothly attached QPS’s.


Figure 2. A magnification of the sporadic E layer in Figure 1.
Figure 3 represents a synthesized BSI determined using the QPS ionospheric model, which produced the profile in Figure 1, without the Es layer.



In this example a QP layer with a semi-thickness of 1 km is used to represent the Es. The semi-thickness in these results has little affect on the Es echo trace. Increasing the semi-thickness of the Es to 10.0 km produces very little change in the shape of the Es echo trace appearing on the BSI. The sporadic E behaves similarly to that of a spherical mirror. The only noticeable difference when increasing the semi-thickness of the Es occurs near the peak operating frequency of the Es echo trace where there is a slight upward bending in the Es echo trace. This upward bending may be of some use in determining the actual thickness of the sporadic E cloud from real BSI’s.
The hmEs can be determined from the BSI by assuming the Es behaves in the manner of a spherical mirror. The synthesized BSI in Figure 4 is used as an example to illustrate the procedure to determine hmEs.
Firstly, the maximum group path from the leading edge of the BSI is determined. In this case the maximum group path is approximately 2250 km.
Secondly, assuming the Es behaves as a good mirror model, then the following equation, which determines the group path,
, for the ray from the transmitter to the base of the Es layer, can be rearranged as follows to produce a simple equation to calculate hmEs.
represents the radius from the centre of the earth to the Es cloud, hmEs
.
Then equation (1) can be rewritten as:-

Depending on the antennas and their location, in practice,
, at best. However, the synthesized BSI in Figure 4 displays ray paths with elevation angle beginning at
. From the BSI in Figure 4,
2150 km.
Then
km which is close to the correct value of 90 km for the peak height of the Es layer used in producing the synthesized BSI in Figure 4. Using a more accurate estimate of
would produce a more accurate value of hmEs. In the following sections, equations for foEs, the length of the Es cloud and the distance the Es cloud is away from the transmitter/receiver location are presented and show that they are in terms of
and not hmEs. This means that a high accuracy in the value of hmEs is not crucial for the modeling and mapping of Es and depending on the desired accuracy in the modeling and mapping required an educated guess of hmEs is in practice normally sufficient.
4.2 Determining foEs from a BSI
The peak plasma frequency should be determined for each of the Es clouds. The equation used to determine the peak plasma frequency of an Es cloud, foEs, is derived as follows:-
At reflection, we know
(2)In order to map Es from a BSI one must determine the distance the transmitter/receiver location is away from the Es cloud. The extent of the Es cloud in the transmitter/receiver also needs to be determined from the BSI. Sometimes more than one Es echo trace is present on the BSI where each echo corresponds to a cloud of Es. It is highly likely that the foEs differ from one cloud to the next. The following procedure should be performed on each cloud separately.
Firstly, calculate the maximum and minimum elevation angles that are reflected from the Es clouds. This is achieved by reading the maximum and minimum group path of the Es echo trace and rearranging equation 1 for a spherical mirror model, as follows:-


where
is the maximum elevation angle of ray paths which transverse the Es cloud,
is the minimum elevation angle of ray paths which transverse the Es cloud,
is the maximum group path of the Es echo read from the BSI,
is the minimum group path of the Es echo read from the BSI,
represents the radius of the earth and
represents the radius from the centre of the earth to the Es cloud, hmEs
.
The extent or length, L, of the Es cloud in the transmitter/receiver direction is given by this simple equation:-
where
and


where
is the angle of incidence at the base of the ionosphere (Es patch). The parameter
is the angle between the transmitter and the Es cloud relative to the centre of the earth, and
are the angles of the ray paths with the lowest and highest elevation angles, which intersect the Es cloud.
The equation below determines the ground distance, D, in kilometers, from the transmitter/receiver location to the position on the ground directly below the edge of the Es cloud nearest the transmitter/receiver location:-

The actual location of the Es cloud in terms of geographic or geomagnetic coordinates can now be readily determined.
6 TESTING THE TECHNIQUE ON REAL BSI’s
Two examples are presented here which clearly demonstrate the ease and effectiveness of the modeling and mapping techniques developed in this study. Figures 6 and 7 show the two Backscatter ionograms from the Jindalee Stage B data (after Houminer et al 1996) which we will attempt to model and map. They are both nighttime cases and clearly show a weak background ionosphere.


Figures 6 and 7. Examples of Jindalee backscatter ionograms with pronounced sporadic E echoes (arrows), (after Houminer et al 1996). Times in UT.
6.1 Example1 Modeling and mapping the BSI in Figure 6
The BSI in Figure 6 shows three distinct Es echo traces at group paths in the range 400-1700 km, indicating three distinct Es clouds were present at this time. The three traces are quite narrow indicating that the patches of Es were relatively small. The three traces extend out to nearly 27 MHz indicating that they are quite dense.
In order to model the Es, one must firstly, measure the maximum operating frequency and the maximum and minimum group paths of each of the Es echo traces on the BSI in Figure 6. The results in Table 1 display these measured values. The maximum operating frequency is used to calculate the maximum plasma frequency of each of the three Es clouds. The maximum and minimum group path measurements are used to calculate the extent of each of the Es clouds. Let Es1 represent the Es cloud closest to the receiver location, represented by the Es echo trace with the smallest group paths. Let Es2 represent the cloud second closest to the receiver and let Es3 represent the Es cloud furthest from the receiver location.
|
Es Cloud |
Max. Frequency [MHz] |
Min. Group Path [km] |
Max. Group Path [km] |
|
Es1 |
25.7 |
350 |
600 |
|
Es2 |
26 |
900 |
1150 |
|
Es3 |
26.5 |
1450 |
1700 |
It is assumed in this case that hmEs for each of the patches is 90 km, again noting that Es generally occurs at altitudes between 90 and 130 km.
Secondly, the maximum and minimum elevation angles that are reflected from the Es clouds and the extent or length, L, of the Es cloud in the direction of the BSI as well as the ground distance, D, in kilometers, from the transmitter/receiver location to the Es cloud are calculated using the equations described earlier, and are presented in Table 2.
The actual location of the Es cloud in terms of geographic or geomagnetic coordinates can be readily determined.
Table 2
|
Es Cloud |
Min. [degree] |
Max. [degree] |
Length of Cloud L [km] |
Distance D [km] |
|
Es1 |
16.2 |
30.2 |
137 |
149 |
|
Es2 |
6.5 |
9.5 |
128 |
438 |
|
Es3 |
2.3 |
3.9 |
127 |
715 |
Thirdly, the peak plasma frequency for each of the Es clouds was calculated using the equations derived earlier, along with and the maximum operating frequencies of the ray paths which were reflected from each of the Es echo traces. The peak plasma frequencies for each of the Es clouds are shown in Table 3.
Table 3
|
Es cloud |
Max. Frequency [MHz] |
foEs [MHz] |
|
Es1 |
25.7 |
8.25 |
|
Es2 |
26 |
5.2 |
|
Es3 |
26.5 |
4.53 |
Then placing these parameters into the new 4L analytic ionospheric ray tracing model, the synthesized BSI in Figure 8 was produced. The Es echo traces, in this BSI, match well to the actual Es echo traces in the BSI shown in Figure 6.
There is very little curvature in the Es echo traces in Figures 6 and 7 indicating very thin Es clouds. Thus, a semi-thickness of 1 km was used in synthesizing the Es clouds.
Figure 8 shows our first attempt at modeling the traces of the BSI in Figure 6, where we have assumed blanketing patches of sporadic E.
Figure 9 shows the synthesized BSI when assuming only partial reflection from the Es clouds. This synthesized BSI matches very well to that shown in Figure 6. In this case it is assumed that all ray paths are only partially reflected from the Es clouds. The method used is designed so that there is about a 20 dB transmission loss for ray paths reflected from (hmEs – 0.2) to hmEs and a 7 dB transmission loss for ray paths reflected from the base of the Es clouds to (hmEs – 0.2). An antenna gain of 10 dB was also included in the synthesized BSI shown in Figure 9.



The BSI in Figure 7 has one well-defined Es echo trace in the 900-1900 km group range. This means that only one large Es cloud is present. The trace appears to have a stronger region of backscatter clutter at a group range of 1600 km. This stronger region is due to a dense patch of ionization within the Es cloud. This can easily be modeled using the technique used previously in modeling the BSI in Figure 6. However, in this section the Es echo trace is modeled as a single spherically stratified Es cloud.
The maximum operating frequency of the ray paths reflected from the Es cloud is 27.5 MHz. The maximum group range is approximately 1700 km. Since we do not have the received angles of arrival of these ray paths, let us assume that the lowest detectable elevation of the antenna array is
. Then hmEs and foEs are determined using equations 1 and 2 and found to be 90 km and 5.0 MHz respectively.
Then placing these parameters into the new 4L analytic ray tracing model, the synthesized BSI shown in Figure 10 resulted. The shape of the Es echo trace in this synthesized BSI matches well with the actual Es echo trace in the BSI shown in Figure 7.
Applying the same conditions of partial reflection, to those that were used in modeling Figure 6, the synthesized BSI in Figure 11 was obtained, which compares reasonably well to the real BSI in Figure 7. Knowing the actual antenna gains would produce even better results.
Not only is it now possible to model the Es, it is also possible to estimate the size and distance from the transmitter/receiver location of the Es clouds.
The new 4L ionospheric model which is simply an extension of the QPS model, in that, another spherically stratified layer is added at the base of the ionosphere to represent Es, produces realistic results.
The equations, determining the distance of the Es cloud from the transmitter/receiver location as well as the peak plasma frequency and the extent of the Es cloud, produce encouraging results. The Es echo traces on the BSI’s compared reasonably well with the synthesized BSI’s, where the synthesized BSI’s were determined using the 4L ionospheric model.
The techniques of both mapping and modeling Es, developed here, are relatively simple, require few input parameters and may be useful in the frequency management system of over-the-horizon radar facilities.
Dyson, P. L., and J. A. Bennett, "A model of the electron concentration in the ionosphere and its application to oblique propagation studies", J. Atmos. Terr. Phys., 50, 251-262, 1988.
Houminer, Z., Russell, C. J., Dyson, P. L., and J. A. Bennett, "Study of sporadic-E clouds by backscatter ionograms", Ann. Geophysicae 14, 1060-1065, 1996.
Norman, R. J., Dyson, P. L., and J. A. Bennett, "Modeling and mapping sporadic E using backscatter ionograms", Report to the Technical Steering Group, Jindalee Project, Telstra Corporation pp. 21, 1998