Keywords

1 Introduction

The modeling of mobile communication systems is a frequent topic of study since the last century [1, 2]. However, it is from the perspective of signals and systems that these conventional modeling techniques of mobile communication systems are normally derived from [3]. As a result, these conventional modeling techniques selectively ignore the details of signal propagation and the ambient environment, especially when the networking topology becomes complex [47]. This ambiguity is always efficient in practice, since the electromagnetic nature of signals are too complicated to study and involves Maxwell’s equations [8]. Also, it is rather difficult, when modeling, to measure the ambient environment precisely and take all potential ambient factors into consideration [9]. Admittedly, it is wise to employ conventional modeling techniques when the details can be ignored and when we only need to focus on the signal input/output relation. However, resorting to these modeling techniques de facto degrade modeling precision and shadow the nature of a realistic mobile communication system. Moreover, when the propagation process is required to be analyzed in near field and the velocity of a mobile system is discussed in the order of speed of light levels, these traditional modeling techniques are all stranded and useless [10]. For these special cases, we should view mobile communication systems in terms of electromagnetic theory and build a series of analytical methodologies, especially in certain oversimplified cases where the electromagnetism-based modeling technique can be precise without loss of efficiency. In order to delve into the details of an electromagnetism-based modeling technique of mobile communication systems, we present a case study in this paper which only takes into consideration the direct and single reflected paths between the transmitter and the receiver. By means of this case study, the pros and cons of electromagnetism-based modeling can be revealed and a number of familiar concepts can be reinterpreted through electromagnetic theory. In addition, the nature of signal transmission and reception in free space can be analyzed in depth.

The rest of this paper is organized as follows. In Sect. 2, we present first the fundamentals of signal radiation and propagation which serve as a foundation for further modeling and analysis. Then, the detailed modeling procedure and analysis are provided in Sect. 3. Based on these constructed models, a number of relevant simulations are contacted subsequently and the simulation results are illustrated and discussed in Sect. 4. Finally we conclude this paper in Sect. 5.

2 Fundamentals of Signal Radiation and Propagation

Consider the nature of a wireless radio signal, it is essentially a high-frequency electromagnetic wave and the information contained in the signal is carried by the transmitted electromagnetic field. Three characteristic parameters, i.e. amplitude A, frequency f and phase angle \(\varTheta \), specialize the carried information. Without loss of generality, we might choose a cosine waveform to express the transmitted electromagnetic field and devise its generic form by [11]:

$$\begin{aligned} E(t)=A\cos (2\pi ft+\varTheta ) \end{aligned}$$
(1)
Fig. 1.
figure 1

Free space signal radiation model.

Assume such an electromagnetic field is transmitted from an isotropic antenna with power \(P_t\) as shown in Fig. 1, in which the transmit antenna and the measured point are marked as red and blue points respectively. In the polar coordinate system, each point in free space can be characterized by a vector \(\mathbf {u}=(\theta ,\varphi ,r)\). Assume further that the isotropic antenna is located in the origin and an arbitrary measured point is denoted by \(\mathbf {u}=(\theta ,\varphi ,r)\). Because of the implementation of an isotropic antenna, a set of points over a spherical surface with radius r are mutually equivalent in terms of the field strength. Therefore in this case, the field strength and the received power only depend on the separation distance r between the measured point and the transmitter isotropic antenna. That is, the far field strength is uniformly distributed in free space. Consequently, the three-dimensional space of signal propagation can be reduced to a two-dimensional space. As a result, when the separation distance r is larger than the Fraunhofer distance, the far field power flux density at the measured point can be determined by [12]:

$$\begin{aligned} \varPhi (r)=\frac{P_t}{4\pi r^2} \end{aligned}$$
(2)

It can be proved that the captured effective area of an isotropic received antenna is [12]:

$$\begin{aligned} A_{iso}=\frac{\lambda ^2}{4\pi }=\frac{1}{4\pi }\left( \frac{c}{f}\right) ^2 \end{aligned}$$
(3)

where \(\lambda \) is the wavelength of the received electromagnetic wave, i.e. the signal; c is the speed of light.

Therefore, if an isotropic antenna is employed at the measured point to receive the electromagnetic wave, the received power is:

$$\begin{aligned} P_r(r)=\varPhi (r)A_{iso}=P_t\left( \frac{c}{4\pi f r}\right) ^2 \end{aligned}$$
(4)

From (4), it is clear that the power of the electromagnetic wave decreases as \(r^{-2}\). According to (1) and the relation between the wave amplitude and the power, it is obvious that the wave amplitude decreases as \(r^{-1}\). Therefore, we can determine the received electromagnetic field from the direct propagation path by:

$$\begin{aligned} E_{dr}(t)&=A(r)\cos [2\pi f(t-r/c)+\varTheta ]\nonumber \\&=\frac{A_0\cos [2\pi f(t-r/c)+\varTheta ]}{r} \end{aligned}$$
(5)

where \(A_0\) is termed critical amplitude, which is the amplitude at the Fraunhofer distance \(r_0\); \(r_0\) is the demarcation between near field and far field regions and normally we have \(r_0\gg \lambda \) [13]. In particular, we should note that the phase shift term \(-2\pi fr/c\) presented in this expression is caused by the propagation delay of the electromagnetic field.

Fig. 2.
figure 2

Direct path and single reflected propagation model. (Color figure online)

3 Modeling Procedure and Analysis

Having constructed the fundamental models of the signal radiation and propagation at the far field region of free space, let us now look into a more complicated scenario. Assume an infinitely long, hard and non-transparent plane exists as shown in Fig. 2 and that the distance between the transmit isotropic antenna and the plane is d (\(d>r\)). From the model constructed in Sect. 2, it is easy to derive the reflected wave detected at the measured point:

$$\begin{aligned} E_{rr}(t)=-\frac{A_0\cos [2\pi f(t-(2d-r)/c)+\varTheta ]}{2d-r} \end{aligned}$$
(6)

According to the linearity of the electromagnetic field at the far field region, the superposition of the field strengths from the direct propagation path and the reflected path can be calculated by:

$$\begin{aligned} E_r(t)&=E_{dr}(t)+E_{rr}(t)\nonumber \\&=\frac{A_0\cos [2\pi f(t-r/c)+\varTheta ]}{r}\nonumber \\&-\frac{A_0\cos [2\pi f(t-(2d-r)/c)+\varTheta ]}{2d-r} \end{aligned}$$
(7)

Furthermore, if we assume that the measured point is moving towards the plane at a constant speed v, the propagation process becomes time-varying and the time-varying separation distance can be expressed by \(r=r_1+vt\), where \(r_1\) is the initial separation distance and satisfies the condition \(r_1>r_0\). As a consequence, (7) can be rewritten as:

$$\begin{aligned} E_r(t)&=\frac{A_0\cos [2\pi f(t-(r_1+vt)/c)+\varTheta ]}{r_1+vt}\nonumber \\&-\frac{A_0\cos [2\pi f(t-(2d-r_1-vt)/c)+\varTheta ]}{2d-r_1-vt} \end{aligned}$$
(8)

From (8), because c is a constant as a basic axiom of the special theory of relativity (STR), it thereby cannot be varied by human factors [14]. Therefore, the received resultant field strength of this two-path scenario is determined by \(r_1\), \(A_0\), f, v, t and \(\varTheta \). More generally and precisely, we might replace \(E_r(t)\) by \(E_r(r_1, A_0,f,v,t,\varTheta )\). However, since \(A_0\) is mainly determined by the transmitter power and only serves as a linear scaler of \(E_r(r_1,A_0,f,v,t,\varTheta )\), for brevity, we might suppose it to 1 (normalized). Also, because the phase angle is relative and quite arbitrary, without loss of generality, we may specify it as 0. Analogously, \(r_1\) can also be viewed as a constant for the purpose of simplification.

These three clarified conditions result in an elucidation of the analysis and now the received resultant field strength is only associated with f, v and t. Consequently, the general form of the received resultant field strength \(E_r(f,v,t)\) can be expressed by:

$$\begin{aligned} E_r(f,v,t)&=\frac{\cos [2\pi f(t-(r_1+vt)/c)]}{r_1+vt}\nonumber \\&-\frac{\cos [2\pi f(t-(2d-r_1-vt)/c)]}{2d-r_1-vt} \end{aligned}$$
(9)

By variable control, it is easy to investigate into the effects of these three variables on the received resultant field strength \(E_r(f,v,t)\).

4 Simulation and Discussion

To simulate the time-varying property of the mobile communication system constructed above, we first set \(f=9.6\) GHz and \(v=1\) m/s. Further assume the diameter of the transmit isotropic antenna \(D=0.5\) m. Therefore, in this case, the Fraunhofer distance can be determined by [15]:

$$\begin{aligned} r_0=\frac{2D^2}{\lambda }=\frac{2D^2f}{c}=16\ \mathrm {m} \end{aligned}$$
(10)

From (10), it is reasonable to set \(r_1=100\) m and \(d=200\) m. Having done so, we can simulate the relation between the received resultant field strength \(E_r(f,v,t)\) and the only variable t. The large-scale time variation results are plotted in Fig. 3. From this figure, it is clear that as the moving measured point approaches the reflection plane, these two electromagnetic waves completely cancel each other out and the received resultant field strength \(E_r(f,v,t)\) equalts to \(o[E_r(f,v,0)]\). However, one might argue that the decay of the field strength is caused by the enlarged separation distance \(r=r_1+vt\) over time. This argument is correct to some extent, but it should be noted that only the counteraction of two identical electromagnetic waves caused by ideal reflection can yield \(E_r(f,v,t)=o[E_r(f,v,0)]\). To verify this conjecture, let us remove the reflection plane and re-simulate under the same conditions. The simulation results are illustrated in Fig. 4. From this figure, our conjecture has been validated, and the attenuation as \(r^{-1}\) is trivial in comparison with \(o[E_r(f,v,0)]\).

Fig. 3.
figure 3

Simulation of large-scale time variation, providing \(f=9.6\) GHz, \(v=1\) m/s, \(r_1=100\) m and \(d=200\) m.

To investigate the time-varying property in more detail, we carry out a further small-scale time variation simulation and plot the results in Fig. 5. In this particular case, the impact of the separation attenuation \(r^{-1}\) on \(E_r(f,v,t)\) is supposed to be negligible. In fact, the high-frequency vibration of \(E_r(f,v,t)\) is caused by the displacement of the measured point over time. Once \(t=\arg \left\{ \frac{\cos [2\pi f(t-(r_1+vt)/c)]}{r_1+vt}=\frac{\cos [2\pi f(t-(2d-r_1-vt)/c)]}{2d-r_1-vt}\right\} \), the direct and reflected electromagnetic waves will add destructively and cancel each other out. At this instant in time, the received field strength equals to \(o[E_r(f,v,0)]\) and the received signal is too weak to be precisely detected. Intuitively, the communication reliability will be significantly hindered. On the other hand, the direct wave and the reflected wave can also add constructively causing the received field strength to reach a peak for which the received signal can then be detected with more ease. This vibration phenomenon of \(E_r(f,v,t)\) reflects the nature of multipath fading and the distance from a valley to a peak is defined as the coherence distance [3]:

$$\begin{aligned} \varDelta r_c=\frac{\lambda }{4}=\frac{c}{4f} \end{aligned}$$
(11)

From (11), normally \(\varDelta r_c\) is relatively small compared to the antenna coverage [3]. Hence, multipath fading is also termed small-scale fading, since the amplitude of the received signal varies tempestuously within several meters. On the contrary, the envelope attenuation as \(r^{-1}\) illustrated in Fig. 4 is termed large scale fading, since it will only become significant when the displacement of the measured point is notably larger then the coherence distance \(\varDelta r_c\). Similarly, we can also understand the nomenclature and classification of slow and fast fading.

Fig. 4.
figure 4

Simulation of large-scale time variation, providing \(f=9.6\) GHz, \(v=1\) m/s, \(r_1=100\) m and \(d=\infty \).

Fig. 5.
figure 5

Simulation of small-scale time variation, providing \(f=9.6\) GHz, \(v=1\) m/s, \(r_1=100\) m and \(d=200\) m.

Fig. 6.
figure 6

Simulation of frequency variation, providing \(t=0\), \(v=1\) m/s, \(r_1=100\) m and \(d=200\) m.

Fig. 7.
figure 7

Simulation 3D plot of the relation among v, t and \(E_r(f,v,t)\), providing \(f=9.6\) GHz.

Fig. 8.
figure 8

Simulation contour plot of the relation among v, t and \(E_r(f,v,t)\), providing \(f=9.6\) GHz.

Akin to the variable control strategy as we have used above, we now fix t to 0 and vary carrier frequency f within the region [8.5, 9.6] GHz, The simulation results are presented in Fig. 6. As shown in this figure, the drastic fluctuation shuttling \(o[E_r(f,v,t)]\) back and forth is expected, since the compensation mechanism of two waves can still be activated by the variation of carrier frequency even though the measured point remains motionless. Similarly, the frequency difference between the valley and the peak of \(E_r(f,v,t)\) is fixed and termed coherence bandwidth [3]:

$$\begin{aligned} \varDelta f_c=\frac{1}{2}\left( \frac{2d-r_1}{c}-\frac{r_1}{c}\right) ^2 \end{aligned}$$
(12)

Finally, we set f back to 9.6 GHz again and allow the speed of the measured point v to vary within [0, 100]. Furthermore, in order to prevent the collision between the measured point and the reflection plane, we reset \(d=2000\). The simulation in this case is conducted and the results are illustrated by a 3D plot and a contour in Figs. 7 and 8 respectively. From these figures, several important points can be summarized. Firstly, the effects of speed v and time t are symmetrical and this can be interpreted by the equivalent coherence distance mechanism activated by the variations of v and t. In addition, the impact of the variation of v has a negligible influence on the small-scale fading but an evident impact on the large-scale fading. This is because the small-scale fading mainly depends on the frequency property of the resultant electromagnetic wave, while the Doppler shift (frequency deviation caused by the movement) at the low speed condition (\(v\ll c\)) is trivial compared to the carrier frequency f adopted in this example. The impact of the Doppler shift caused by movement at the speed v can be qualified by Doppler spread [3]:

$$\begin{aligned} D_s(f,v)=|\varDelta f_{dd}(f,v)-\varDelta f_{rd}(f,v)|=\frac{2fv}{c} \end{aligned}$$
(13)

where \(\varDelta f_{dd}(f,v)\) is the Doppler shift of the direct wave and \(\varDelta f_{rd}(f,v)\) is the Doppler shift of the reflected wave.

In this simulation example, \(D_s(f,v) \in [0, 6400] ~\mathrm {Hz}\ll f=9\times 10^{9}\ \mathrm {Hz}\). This result quantitatively explains the reason why Doppler shift can always be ignored in practice when analyzing small-scale fading [12].

5 Conclusion

In conclusion, we have constructed a simplified model of mobile communication systems through the application of electromagnetic theory. Although we have illustrated this model in an oversimplified case where only two-path electromagnetic waves are considered, this paper can still serve as a firm reference for more complicated scenarios. Furthermore, compared to conventional signal system models, the electromagnetic nature of signals and a series of phenomena can be explained and analyzed more extensively by this electromagnetism-based model. However, we can also notice that even for this oversimplified scenario, the electromagnetism-based model is complicated and thus might not be applicable when the ambient environment is complex.