Exercise 2.5Z: Multi-Path Scenario

Mobilfunk–Szenario mit drei Pfaden

In Task 2.5 a delay–Doppler–function was given. From this, we will calculate and interpret the other system functions. The given scatter function $s(\tau_0, f_{\rm D})$ was

$s(\tau_0, f_{\rm D}) =\frac{1}{\sqrt{2}} \cdot \delta (\tau_0) \cdot \delta (f_{\rm D} - 100\,{\rm Hz}) \ - \$

$\hspace{1.5cm} \ - \ \hspace{-0.2cm} \frac{1}{2} \cdot \delta (\tau_0 \hspace{-0.05cm}- \hspace{-0.05cm}1\,{\rm \mu s}) \cdot \delta (f_{\rm D} \hspace{-0.05cm}- \hspace{-0.05cm}50\,{\rm Hz}) \ - \frac{1}{2} \cdot \delta (\tau_0 \hspace{-0.05cm}- \hspace{-0.05cm}1\,{\rm \mu s}) \cdot \delta (f_{\rm D}\hspace{-0.05cm} + \hspace{-0.05cm}50\,{\rm Hz}) \hspace{0.05cm}.$

Note: In our learning tutorial, $s(\tau_0, \hspace{0.05cm} f_{\rm D})$ is also identified with $\eta_{\rm VD}(\tau_0, \hspace{0.05cm}f_{\rm D})$ .

Here we have replaced the delay variable $\tau$ with $\tau_0$ . The new variable $\tau_0$ describes the difference between the delay of a path and the delay $\tau_1$ of the main path. The main path is thus identified in the above equation by $\tau_0 = 0$ .

Now, we try to find a mobile radio scenario in which this scatter function would actually occur. The basic structure is sketched above as a top view, and the following hold:

A single frequency is transmitted $f_{\rm S} = 2 \ \rm GHz$ .
The mobile receiver $\rm (E)$ is represented here by a yellow dot. It is not known whether the vehicle is stationary, moving towards the transmitter $\rm (S)$ or moving away from it.
The signal reaches the receiver via a main path (red) and two secondary paths (blue and green). Reflections from the obstacles cause phase shifts of $\pi$ .
${\rm S}_2$ and ${\rm S}_3$ are to be understood here as fictitious transmitters from whose position the angles of incidence $\alpha_2$ and $\alpha_3$ of the secondary paths can be determined.
Let the signal frequency be $f_{\rm S}$ , the angle of incidence $\alpha$ , the velocity $v$ and the velocity of light $c = 3 \cdot 10^8 \ \rm m/s$ . Then, the Doppler frequency is

$f_{\rm D}= {v}/{c} \cdot f_{\rm S} \cdot \cos(\alpha) \hspace{0.05cm}.$

The damping factors $k_1$ , $k_2$ and $k_3$ are inversely proportional to the path lengths $d_1$ , $d_2$ and $d_3$ . This corresponds to the path loss exponent $\gamma = 2$ .
This means: The signal power decreases quadratically with distance $d$ and accordingly the signal amplitude decreases linearly with $d$ .

Notes:

This task belongs to chapter Das GWSSUS–Kanalmodell.
We focus especially on the path-loss model and the Doppler effect.

Questionnaire

Sample solution

Musterlösung

(1) The Doppler frequency is positive for

$\tau_0$ . This means that the receiver is moving towards the transmitter ⇒ statement 2.

(2) The equation for the Doppler frequency is general or for the angle $\alpha = 0$ .

$f_{\rm D}= \frac{v}{c} \cdot f_{\rm S} \cdot \cos(\alpha) \hspace{0.05cm},\hspace{0.3cm}\alpha = 0 \hspace{0.05cm}{\rm :} \hspace{0.15cm}f_{\rm D}= \frac{v}{c} \cdot f_{\rm S}\hspace{0.05cm}.$

This is what you get for speed:

$$v = \frac{f_{\rm D}}}{f_{\rm S} \cdot c = \frac{10^2\,{\rm Hz}}}{2 \cdot 10^9\,{\rm Hz}} \cdot 3 \cdot 10^8\,{\rm m/s} = 15\,{\rm m/s} \hspace{0.1cm} \underline {= 54 \,{\rm km/h} \hspace{0.05cm}.$$

(3) Correct are the solutions 1 and 4:

The Doppler frequency $f_{\rm D} = 50 \ \rm Hz$ comes from the blue path, because the receiver somehow moves towards the virtual transmitter ${\rm S}_2$ (at the reflection point), although not in a direct direction.
The angle $\alpha_2$ between the direction of movement and the connecting line ${\rm S_2 – E}$ is $60^\circ$ :

$\cos(\alpha_2) = \frac{f_{\rm D}}}{f_{\rm S}} \cdot \frac{c}{v} = \frac{50 \,{\rm Hz}\cdot 3 \cdot 10^8\,{\rm m/s}}}{2 \cdot 10^9\,{\rm Hz}\cdot 15\,{\rm m/s}} = 0.5 \hspace{0.3cm} \Rightarrow \hspace{0.3cm} \alpha_2 \hspace{0.1cm} \underline {= 60^{\circ} } \hspace{0.05cm}.$

(4) Correct are the statements 1 and 3:

From $f_{\rm D} = \, –50 \ \rm Hz$ follows $\alpha_3 = \alpha_2 ± \pi$ , so $\alpha_3 \ \underline {= 240^\circ}$ .

(5) All statements are correct:

The two Dirac functions at $± 50 \ \ \rm Hz$ have the same running time. For both durations $\tau_3 = \tau_2 = \tau_1 + \tau_0$ is valid.
From the same transit time, however, also follows $d_3 = d_2$ and with the same length also the same damping factors.

(6) The runtime difference is $\tau_0 = 1 \ \rm µ s$ , as shown in the equation for $s(\tau_0, f_{\rm D})$ .

This gives the difference in length:

$\Delta d = \tau_0 \cdot c = 10^{–6} {\rm s} \cdot 3 \cdot 10^8 \ \rm m/s \ \ \underline {= 300 \ \ \rm m}.$

(7) The path loss exponent was assumed to be $\gamma = 2$ for this task.

Then $k_1 = K/d_1$ and $k_2 = K/d_2$ .

The minus sign takes into account the $180^\circ$ –phase rotation on the secondary paths.
From the weights of the Dirac functions one can read $k_1 = \sqrt{0.5}$ and $k_2 = -0.5$ . From this follows:

$\frac{\2}{d_1} = \frac{k_1}{-k_2} = \frac{1/\sqrt{2}}{0.5} = \sqrt{2} \hspace{0.15cm} \underline {= 1,414} \hspace{0.05cm}.$

The constant $K$ is only an auxiliary variable that does not need to be considered further.

(8) Aus $d_2/d_1 = 2^{-0.5}$ and $\Delta d = d_2 \, - d_1 = 300 \ \rm m$ finally follows:

$\sqrt{2} \cdot d_1 - d_1 = 300\,{\rm m} \hspace{0.3cm} \Rightarrow \hspace{0.3cm} d_1 = \frac{300\,{\rm m}}}{\sqrt{2} - 1} \hspace{0.15cm} \underline {= 724\,{\rm m}} \hspace{0.3cm} \Rightarrow \hspace{0.3cm} d_2 = \sqrt{2} \cdot d_1 \hspace{0.15cm} \underline {= 1024\,{\rm m}} \hspace{0.05cm}.$

	This Dirac comes from the blue path.
	This Dirac comes from the green path.
	The angle is $30^\circ$ .
	The angle is $60^\circ$ .

	The receiver is standing.
	The receiver moves directly towards the transmitter.
	The receiver moves away in the opposite direction to the transmitter.

	For this, $\tau_0 = 1 \ \ \rm µ s$ and $f_{\rm D} = \, –50 \ \ \rm Hz$ .
	The angle $\alpha_3$ (see graphic) is $60^\circ$ .
	The angle $\alpha_3$ is $240^\circ$ .

	It applies $d_3 = d_2$ .
	It is $k_3 = k_2$ .
	It is $\tau_3 = \tau_2$ .