Wireless communication systems are designed to recover received signals that are damaged by wireless channel impairments. In classical communication theory, wireless channels were unknown and people think unpredictable noises occur in wireless channels. However, many scientists and engineers investigated wireless channels and developed different types of wireless channel models. They can be categorized as additive white Gaussian noise, jitter, phase shift, path loss, shadowing, multipath fading, interference, and so on. They give the transmitted signals different types of damages. In addition, transmission distance, mobility, geographical feature, weather, antenna position, and signal waveform affect the parameters of wireless channel models. For example, the channel model of short range wireless communications is different from the one of cellular systems. An urban area channel model is different from that of a rural one. A mobile user has more severe frequency offset due to the Doppler effect. Therefore, it is important to understand wireless channels when designing wireless communication systems. In this chapter, we look into wireless channels and their characteristics.
In Chapter 2, we have defined noise as Gaussian distribution due to central limit theorem. When the noise power has a flat power spectral density, we call it white noise and its single-sided power spectral density (Pwn(f) (W/Hz)) can be denoted as follows:
where N0 is constant. This equation means the white noise has an equal power spectral density for all frequency bands. This white noise affects most types of signals independently so that we usually call it Additive White Gaussian Noise (AWGN). If a wireless channel is given, we can calculate capacity of the wireless channel. The channel capacity of single antenna systems for AWGN channel is defined as follows:
Channel capacity, Cawgn, means the amount of information we can send through the given channel. We call this equation Shannon-Hartley theorem [1]. The average received signal power over the channel noise (Pr/N0W) is simply the signal to noise ratio (SNR) and Cawgn/W is simply the normalized channel capacity. Figure 3.1 illustrates their relationship.
In Figure 3.1, we can observe two areas: theoretically impossible area and theoretically possible area. When we want to transmit a signal with data rate, R, it is not possible to communicate reliably in this area (R > Cawgn). The curve represents the limitation of liable transmission under the given channel. When the average received power is large enough (SNR 1), the capacity reaches the saturation point in the power and regards as a linear function in the bandwidth. Therefore, we call this area bandwidth limited regime. The capacity equation can be expressed approximately as follows:
On the contrary, when the average received power is small enough (SNR 1), the capacity reaches the saturation point in the bandwidth and regards as a linear function in the power. Therefore, we call this area power limited regime. The capacity equation can be expressed approximately as follows:
For infinite bandwidth, . (3.3) can be rewritten as follows:
where Eb is a bit energy. We can obtain the following equation:
We call this value (0.694 or −1.6 in dB) Shannon limit. This value means it is not possible to communicate reliably below this value.
An electromagnetic wave propagates from a transmitter to a receiver over the air. During this propagation, the energy of the electromagnetic wave is reduced. Basically, we can express this process as path loss models. One of simple channel models is Friis transmission model [2]. It describes a simple free space channel without obstructions between a transmitter and a receiver. In this model, the electromagnetic waves spread outward in a sphere, and the received power, Pr, is given as follows:
where Pt is the transmitted power, Gt and Gr are the transmitter antenna gain and the receiver antenna gain, respectively, λ is the wavelength, and R is the distance between a transmitter and a receiver. The Friis transmission model is illustrated in Figure 3.2.
The isotropic antenna of the transmitter radiates the Effective Isotropic Radiated Power (EIRP) uniformly. It is represented by
and the antenna of the receiver collects the transmitted power as much as the antenna size (or the effective area) of the receiver. We call it the antenna aperture, Ae. The received power is related to this antenna aperture and the surface area of the sphere, 4πR2. The received power is proportional to Ae/4πR2. Therefore, we can present the received power, Pr, as follows:
The relationship between the receiver antenna gain and effective aperture is
Combining (3.8) and (3.9), we can obtain (3.6). This equation means the received power depends on the square of the distance proportionally because the other parameters are basically given. In practical systems, the received power decreases more quickly due to reflection, diffraction, and scattering. These mechanisms are governed by the Maxwell equations. Reflection is the change in the direction of an electromagnetic wave when it encounters an object. The behavior of the reflection is explained by Fresnel equations. Diffraction is the bending of light when it passes the edge of an object. The behavior of diffraction is explained by Huygen’s principle. Scattering is the production of other small electromagnetic waves when it encounters an object with a rough surface. The process of the scattering is quite complex and some types of scattering are Rayleigh scattering, Mie scattering, Raman scattering, Tyndall scattering, and Brillouin scattering.
Figure 3.3 illustrates the two-ray ground reflection model.
When considering the reflection from ground, we can use the two-ray ground reflection model as follows:
where ht and hr denote the transmitter antenna height and receiver antenna height, respectively. Unlike Friis transmission equation, the received power is affected by the antenna heights. The fourth power of the distance, d4, is included in the equation so that the received power decreases more quickly according to the distance. This equation does not depend on the wavelength.
In practical systems, we use empirical path loss models. The received power of the empirical models is expressed as follows:
where P0 is the power at the reference distance, d0, and γ is the path loss exponent which typically has 2–8 according to carrier frequency, environment, and so on. The path loss is defined as the difference between the transmitted power and the received power as follows:
From Definition 3.2, the path loss of (3.11) is
where PL0 is the path loss at the reference distance d0 (dB). When a propagating electromagnetic wave encounters some obstruction such as wall, building, and tree, reflection, diffraction, and scattering happen and the electromagnetic wave is distorted. We call this effect shadowing or slow fading and use the modified path loss model as follows:
where χ denotes a Gaussian distributed random variable with standard deviation, σ, and represents shadowing effect.
When an electromagnetic wave propagates in the air, reflection happens and it produces some reflected waves as shown in Figure 3.4. Although the receiver wants to have the original signal only, it receives the reflected waves together with the original signal. The reflected signals travel different paths and they have different amplitudes and phase noises. Thus, many signals with different delays and amplitudes arrive at the receiver.
The power delay profile is widely used to analyze multipath wireless channels. It is described by several parameters such as the mean excess delay, maximum excess delay, root mean square (rms) delay spread, and maximum delay spread. Among them, the maximum delay spread, τmax, and the rms delay spread, τrms, are important multipath channel parameters. The maximum delay spread means the total time interval we can receive the reflected signals with high energy. A high value of τmax means a highly dispersive channel. However, the maximum delay spread can be defined in several ways. Therefore, the rms delay spread is more widely used and indicates the rms value of the delay profile. We use this parameter to decide coherence bandwidth. One example of the power delay profile is shown in Figure 3.5.
The multipath channel is modeled as a linear Finite Impulse Response (FIR) filter. The impulse response, h(t, τ), of the multipath channel is
where ai(t) and denote amplitude of a multipath and the Dirac delta function, respectively. N means N different reflected paths. One example is illustrated in Figure 3.6.
We can observe two different reflected paths in the delay profile and represent this using a three-tap FIR filter as shown in Figure 3.7. In this figure, delay, τ1 and τ2, can be implemented by shift-registers and amplitude, a0, a1, and a2, can be implemented by multiplications (or amplifiers).
From the power delay profile, we can analyze the multipath channel.
If a wireless channel is not constant over a transmit bandwidth and severely distorted, it would be very difficult to establish a reliable radio link. Thus, we define the coherence bandwidth (Bc) as follows:
It simply means the range of frequencies we use to send a signal without serious channel distortions. The rms delay spread, τrms, is inversely proportional to the coherence bandwidth as follows:
Therefore, the larger τrms means the wireless channel becomes more frequency selective channel. The more accurate definition of Bc is related to the frequency correlation function. For correlation greater than 0.9 [3],
For correlation greater than 0.5 [3],
When we design a symbol structure of wireless communication systems, the symbol length should be defined according to τrms. For example, if the symbol length is greater than 10 τrms, we assume the wireless communication system does not need to mitigate Inter Symbol Interference (ISI). If it is less than 10 τrms, we must avoid ISI using several techniques such as an equalizer. If it is much less than 10 τrms, a reliable communication is not possible.
Typically, the rms delay spread of cellular systems is less than 8 µs. The urban or mountain area has longer than 8 µs due to more reflections. The rms delay spread of indoor small cells is less than 50 ns.
A wireless channel is varying according to time, movement, environment, and so on. If a wireless channel changes every moment, we will not know wireless channel characteristics and cannot design wireless communication systems. Therefore, we assume a wireless channel is constant during certain time. The coherence time means the certain time. It is defined as follows:
Similar to the power delay profile, the Doppler power spectrum provides statistical information about the coherence time. The Doppler power spectrum is affected by a user mobility while the power delay profile is affected by a multipath. A moving wireless communication device produces the Doppler shift (Δf ). The Doppler shift is expressed as follows:
where v, λ, θ, and c denote the speed of a moving wireless communication device, the wavelength of the carrier electromagnetic wave, the angle of arrival with respect to a direction of the moving wireless device, and the speed of light, respectively. When a receiver moves in the opposite direction of the electromagnetic wave (θ = 0°), the Doppler shift is
When a receiver moves in the same direction of the electromagnetic wave (θ = 180°), the Doppler shift is
When a receiver moves in perpendicular to the electromagnetic wave (θ = 90°), the Doppler shift is
Therefore, the maximum Doppler shift ( fm) means cos θ = 1 and is represented as follows:
and the coherence time (Tc) is inversely proportional to the Doppler spread as follows:
For correlation greater than 0.5 [3],
If the symbol duration is greater than the coherence time, the wireless channel changes during symbol transmission. We call this fast fading. On the other hands, if the symbol duration is less than the coherence time, the wireless channel does not change during symbol transmission. We call this slow fading.
The Rayleigh fading distribution is widely used to model a small-scale fading and describes a statistical time varying model for the propagation of electromagnetic waves. When the time variant channel impulse response in a flat fading channel is given by
where a(t) and φ(t) denote the magnitude and phase rotation, respectively, the probability density function of the Rayleigh distribution is represented by
where σ2 denotes the time average power of the received signal. One example of the Rayleigh fading is illustrated in Figure 3.8.
When there is one strong multipath signal such as a line-of-sight signal, we can use the Rice distribution. It is expressed as follows:
where a0 and I0 denote the peak magnitude of one strong multipath and the modified Bessel function of the first kind. Every natural phenomenon in time domain has corresponding phenomenon in frequency domain. Sometimes we explain the power delay profile in frequency domain through the Fourier transform. The multipath fading results in significant power losses, frequency and phase offsets, and so on. Therefore, a wireless communication system designer should understand fading environments clearly and select suitable mitigation techniques. The diversity techniques are very important techniques to overcome fading channels. Basically, this technique uses the fact that each wireless channel experiences different fading. For example, some part of a signal passing through channel 1 can be damaged seriously but same part of a signal passing through channel 2 may not be damaged. A receiver can recover the transmitted signal through observing multiple signals passing through different channels. More detail will be dealt in Chapter 5. The type of small-scale fading is illustrated in Figure 3.9 where Bs and Ts denote the signal bandwidth and time interval, respectively.
The capacity, Cfreq sel (bits/s/Hz), of the frequency selective fading channel [4] is given by
where is the sub-channel gain and can be found by Lagrangian method as follows:
where λL is the Lagrangian multiplier. We call this power allocation water-filling. One example of the water-filling algorithm is illustrated in Figure 3.10.
In the fast fading channel, we transmit a signal in time interval LTc and have approximately same channel gain for lth coherence time period. Therefore, the average capacity, Cfast (bits/s/Hz), is
When L is large, the capacity is
The outage capacity is used for slow-fading channels because the capacity is a random variable and there is delay limitation. The outage capacity, C0 (bits/s/Hz), is simply defined as the maximum data rate without errors. The outage probability, pout(C0), can be represented as follows:
For example, means the frame error rate is 0.1 with ideal code if the wireless communication system frame has 10 bits/s/Hz spectral efficiency.
The channel model we looked into the previous sections is to provide theoretical backgrounds but it does not include measurement data from real wireless environments. Therefore, many scientists and engineers extensively measure wireless channel parameters in real wireless environments and develop empirical wireless channel models such as Hata model [5], Walfisch-Ikegami model [5], Erceg model [6], ITU model [7], and so on. Among them, the ITU-R recommendation M.1225 is widely used as empirical channel models of cellular systems. Especially, Worldwide Interoperability for Microwave Access (WiMAX) by the Institute of Electrical and Electronics Engineers (IEEE) and Long Term Evolution (LTE) by the 3rd Generation Partnership Project (3GPP) use these models. The wireless channel models are classified into three test environments such as indoor office, pedestrian, and vehicular environment. Their path loss model for the indoor office environment [7] is expressed as follows:
where dindoor and n denote the distance (m) between a transmitter and a receiver and the number of floors, respectively. The path loss model for the pedestrian test environment [5] is
where dpedestrian and f denote the distance (km) between a base station and a mobile station and carrier frequency, respectively. The path loss model for the vehicular test environment [5] is
where dvehicular, hb, and f denotes the distance (km) between a base station and a mobile station, the base station antenna height (m), and carrier frequency, respectively. In addition, they have two different delay spreads: channel A (Low delay spread) and channel B (High delay spread). Their parameters are summarized in Tables 3.1, 3.2, 3.3, and 3.4.
Table 3.1 Parameters for channel impulse response model [5]
Test environment | Channel A | Channel B | ||
rms (ns) | P (%) | rms (ns) | P (%) | |
Indoor office | 35 | 50 | 100 | 45 |
Outdoor to indoor and pedestrian | 45 | 40 | 750 | 55 |
Vehicular—high antenna | 370 | 40 | 4 000 | 55 |
Table 3.2 Indoor office test environment tapped-delay-line parameters [5]
Tap | Channel A | Channel B | Doppler spectrum | ||
Relative delay (ns) | Average power (dB) | Relative delay (ns) | Average power (dB) | ||
1 | 0 | 0 | 0 | 0 | Flat |
2 | 50 | −3.0 | 100 | −3.6 | Flat |
3 | 110 | −10.0 | 200 | −7.2 | Flat |
4 | 170 | −18.0 | 300 | −10.8 | Flat |
5 | 290 | −26.0 | 500 | −18.0 | Flat |
6 | 310 | −32.0 | 700 | −25.2 | Flat |
Table 3.3 Outdoor to indoor and pedestrian test environment tapped-delay-line parameters [5]
Tap | Channel A | Channel B | Doppler spectrum | ||
Relative delay (ns) | Average power (dB) | Relative delay (ns) | Average power (dB) | ||
1 | 0 | 0 | 0 | 0 | Classic |
2 | 110 | −9.7 | 200 | −0.9 | Classic |
3 | 190 | −19.2 | 800 | −4.9 | Classic |
4 | 410 | −22.8 | 1200 | −8.0 | Classic |
5 | — | — | 2300 | −7.8 | Classic |
6 | — | — | 3700 | −23.9 | Classic |
Table 3.4 Vehicular test environment, high antenna, tapped-delay-line parameters [5]
Tap | Channel A | Channel B | Doppler spectrum | ||
Relative delay (ns) | Average power (dB) | Relative delay (ns) | Average power (dB) | ||
1 | 0 | 0.0 | 0 | −2.5 | Classic |
2 | 310 | −1.0 | 300 | 0 | Classic |
3 | 710 | −9.0 | 8 900 | −12.8 | Classic |
4 | 1090 | −10.0 | 12 900 | −10.0 | Classic |
5 | 1730 | −15.0 | 17 100 | −25.2 | Classic |
6 | 2510 | −20.0 | 20 000 | −16.0 | Classic |
Transmission power | 25 W |
Transmitter antenna gain | 10 |
Receiver antenna gain | 15 |
Carrier frequency | 2 GHz |
Distance between transmitter and receiver | 1 km |
Transmission power | 25 W |
Transmitter antenna gain | 1.5 |
Receiver antenna gain | 1 |
Carrier frequency | 1 GHz |
Transmission power | 20 W |
Carrier frequency | 2 GHz |
Transmitter antenna gain | 1.6 |
Receiver antenna gain | 1 |
Transmitter antenna height | 20 m |
Receiver antenna height | 1.5 m |
Find the frequency response of the filter.
Find the frequency response of the filter when L = 1, 3, 5, and 10.
Find the z-transfer function and the phase response.
(i) Find the coherence bandwidth. (ii) Do we need an equalizer when signal bandwidth is 200 kHz? (iii) Find the coherence time when the carrier frequency is 1.8 GHz and a user mobile at a speed of 100 km/h.
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