Difference between revisions of "Digital Signal Transmission/Error Probability with Intersymbol Interference"

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{{Header
 
{{Header
|Untermenü=Impulsinterferenzen und Entzerrungsverfahren
+
|Untermenü=Intersymbol Interfering and Equalization Methods
 
|Vorherige Seite=Ursachen und Auswirkungen von Impulsinterferenzen
 
|Vorherige Seite=Ursachen und Auswirkungen von Impulsinterferenzen
 
|Nächste Seite=Berücksichtigung von Kanalverzerrungen und Entzerrung
 
|Nächste Seite=Berücksichtigung von Kanalverzerrungen und Entzerrung
 
}}
 
}}
  
== Gaußförmiges Empfangsfilter (1) ==
+
== Gaussian receiver filter==
 
<br>
 
<br>
Zur quantitativen Berücksichtigung der Impulsinterferenzen wird folgende Konfiguration angenommen:
+
We start from the block diagram sketched below.&nbsp; The following configuration is assumed for quantitative consideration of &nbsp;[[Digital_Signal_Transmission/Causes_and_Effects_of_Intersymbol_Interference#Definition_of_the_term_.22Intersymbol_Interference.22|"intersymbol interference"]]:&nbsp;
*Rechteckförmiger NRZ&ndash;Sendegrundimpuls <i>g<sub>s</sub></i>(<i>t</i>) mit der Höhe <i>s</i><sub>0</sub> und der Dauer <i>T</i>,<br>
+
 +
*Rectangular NRZ basic transmission pulse &nbsp;$g_s(t)$&nbsp; with height &nbsp;$s_0$&nbsp; and duration &nbsp;$T$,<br>
  
*Gaußförmiges Empfangsfilter mit der Grenzfrequenz <i>f</i><sub>G</sub>:
+
*Gaussian-shaped receiver filter&nbsp; $H_{\rm G}(f)$&nbsp; with cutoff frequency $f_{\rm G}$:
 
+
:$$H_{\rm E}(f) = H_{\rm G}(f) = {\rm exp}\left [-  \frac{\pi  \cdot f^2}{(2f_{\rm G})^2} \right ] \hspace{0.2cm} \bullet\!\!-\!\!\!-\!\!\!-\!\!\circ
::<math>H_{\rm E}(f) = H_{\rm G}(f) = {\rm exp}\left [-  \frac{\pi  \cdot f^2}{(2f_{\rm G})^2} \right ] \hspace{0.2cm} \bullet\!\!-\!\!\!-\!\!\!-\!\!\circ
 
 
  \hspace{0.2cm}h_{\rm E}(t) = h_{\rm G}(t) = {\rm exp}\left [- \pi  \cdot (2
 
  \hspace{0.2cm}h_{\rm E}(t) = h_{\rm G}(t) = {\rm exp}\left [- \pi  \cdot (2
 
  f_{\rm G} t)^2\right ]
 
  f_{\rm G} t)^2\right ]
   \hspace{0.05cm}.</math>
+
   \hspace{0.05cm},\hspace{0.5cm}\text{note: }\hspace{0.2cm}{\rm exp} [x] = {\rm e}^x.$$
 +
*AWGN channel &nbsp; &rArr; &nbsp; channel frequency response&nbsp;  $H_{\rm K}(f) = 1 $&nbsp; and&nbsp; noise power-spectral density&nbsp; ${\it \Phi}_n(f) = N_0/2$.
  
*AWGN&ndash;Kanal, das heißt, es gilt <i>H</i><sub>K</sub>(<i>f</i>) = 1 und <i>&Phi;<sub>n</sub></i>(<i>f</i>) = <i>N</i><sub>0</sub>/2.<br><br>
 
  
Für das gesamte Kapitel 3.2 wird somit von nachfolgendem Blockschaltbild ausgegangen.<br>
+
<u>Note:</u>&nbsp;
 
+
#We restrict ourselves in this chapter exclusively to&nbsp; '''redundancy-free binary bipolar transmission'''.&nbsp;
[[File:P_ID1372__Dig_T_3_2_S1_version2.png|Blockschaltbild für das Kapitel 3.2|class=fit]]<br>
+
#The ISI influence in multi-level and/or coded transmission will not be discussed until the chapter&nbsp; [[Digital_Signal_Transmission/Intersymbol_Interference_for_Multi-Level_Transmission|"Intersymbol Interference for Multi-Level Transmission"]].
 +
<br>
  
Aufgrund der getroffenen Voraussetzungen gilt für den Detektionsgrundimpuls:
+
Based on the assumptions made here,&nbsp; the following holds for the basic detection pulse:
  
:<math>g_d(t) = g_s(t) \star h_{\rm G}(t) = 2 f_{\rm G} \cdot s_0 \cdot \int_{t-T/2}^{t+T/2}
+
:$$g_d(t) = g_s(t) \star h_{\rm G}(t) = 2 f_{\rm G} \cdot s_0 \cdot \int_{t-T/2}^{t+T/2}
{\rm exp}\left [- \pi  \cdot (2 \cdot
+
{\rm e}^{- \pi  \hspace{0.05cm}\cdot\hspace{0.05cm} (2 \hspace{0.05cm}\cdot\hspace{0.05cm}
  f_{\rm G}\cdot \tau )^2\right ] \,{\rm d} \tau \hspace{0.05cm}.</math>
+
  f_{\rm G}\hspace{0.05cm}\cdot\hspace{0.05cm} \tau )^2} \,{\rm d} \tau \hspace{0.05cm}.$$
  
Die Integration führt zu folgendem Ergebnis:
+
The integration leads to the following equivalent results:
  
:<math>g_d(t) =  s_0 \cdot \left [ {\rm Q} \left (  2 \cdot \sqrt {2 \pi}
+
:$$g_d(t) =  s_0 \cdot \big [ {\rm Q} \left (  2 \cdot \sqrt {2 \pi}
 
\cdot f_{\rm G}\cdot  ( t - {T}/{2})\right )-  {\rm Q} \left (
 
\cdot f_{\rm G}\cdot  ( t - {T}/{2})\right )-  {\rm Q} \left (
 
2 \cdot \sqrt {2 \pi} \cdot f_{\rm G}\cdot ( t + {T}/{2}
 
2 \cdot \sqrt {2 \pi} \cdot f_{\rm G}\cdot ( t + {T}/{2}
)\right ) \right ]\hspace{0.05cm},</math>
+
)\right ) \big ],$$
 
+
:$$g_d(t) = s_0 \cdot\big [ {\rm erfc} \left (  2 \cdot
:<math>g_d(t) = {s_0}/{2} \cdot \left [ {\rm erfc} \left (  2 \cdot
 
 
\sqrt {\pi} \cdot f_{\rm G}\cdot  ( t - {T}/{2})\right )- {\rm
 
\sqrt {\pi} \cdot f_{\rm G}\cdot  ( t - {T}/{2})\right )- {\rm
 
erfc} \left (  2 \cdot \sqrt {\pi} \cdot f_{\rm G}\cdot ( t +
 
erfc} \left (  2 \cdot \sqrt {\pi} \cdot f_{\rm G}\cdot ( t +
{T}/{2} )\right ) \right ]\hspace{0.05cm}.</math>
+
{T}/{2} )\right ) \big ]\hspace{0.05cm}.$$
 +
[[File:EN_Dig_T_3_2_S1.png|right|frame|Block diagram for the chapter&nbsp; "Error Probability with Intersymbol Interference"]]
  
Hierbei sind zwei Varianten der komplementären Gaußschen Fehlerfunktion verwendet, nämlich
+
Here,&nbsp; two variants of the complementary Gaussian error function are used,&nbsp; viz.
  
:<math>\rm Q (\it x) = \frac{\rm 1}{\sqrt{\rm 2\pi}}\int_{\it
+
:$${\rm Q} (x) = \frac{\rm 1}{\sqrt{\rm 2\pi}}\int_{\it
 
x}^{+\infty}\rm e^{\it -u^{\rm 2}/\rm 2}\,d {\it u}
 
x}^{+\infty}\rm e^{\it -u^{\rm 2}/\rm 2}\,d {\it u}
\hspace{0.05cm},\hspace{0.5cm}
+
\hspace{0.05cm},$$
{\rm erfc} (\it x) = \frac{\rm 2}{\sqrt{\rm
+
:$$ {\rm erfc} (\it x) = \frac{\rm 2}{\sqrt{\rm
 
\pi}}\int_{\it x}^{+\infty}\rm e^{\it -u^{\rm 2}}\,d \it u
 
\pi}}\int_{\it x}^{+\infty}\rm e^{\it -u^{\rm 2}}\,d \it u
\hspace{0.05cm}.</math>
+
\hspace{0.05cm}.$$
  
Das Modul [[:File:QFunction.swf|Komplementäre Gaußsche Fehlerfunktion]] liefert die Zahlenwerte von Q(<i>x</i>) und erfc(<i>x</i>).<br>
+
&rArr; &nbsp; The &nbsp;[[Applets:Komplementäre_Gaußsche_Fehlerfunktionen|"Complementary Gaussian Error Functions"]]&nbsp; provides the numerical values of the functions &nbsp;${\rm Q} (x)$&nbsp; and &nbsp;$0.5 \cdot {\rm erfc} (x)$.<br>
  
Die Rauschleistung am Ausgang des gaußförmigen Empfangsfilters <i>H</i><sub>G</sub>(<i>f</i>) ist gleich
+
The noise power at the output of the Gaussian receiver filter &nbsp;$H_{\rm G}(f)$&nbsp; is
 
+
:$$\sigma_d^2 = \frac{N_0}{2} \cdot \int_{-\infty}^{+\infty}
:<math>\sigma_d^2 = \frac{N_0}{2} \cdot \int_{-\infty}^{+\infty}
 
 
|H_{\rm G}(f)|^2 \,{\rm d} f = \frac{N_0\cdot f_{\rm
 
|H_{\rm G}(f)|^2 \,{\rm d} f = \frac{N_0\cdot f_{\rm
G}}{\sqrt{2}}\hspace{0.05cm}.</math>
+
G}}{\sqrt{2}}\hspace{0.05cm}.$$
  
Aus diesen beiden Gleichungen erkennt man bereits:
+
{{BlaueBox|TEXT= 
*Je kleiner die Grenzfrequenz <i>f</i><sub>G</sub> des Gauß&ndash;Tiefpasses ist, desto kleiner ist der Rauscheffektivwert <i>&sigma;<sub>d</sub></i> und umso besser ist demzufolge das Rauschverhalten.<br>
+
$\text{From these equations one can already see:}$&nbsp;
 +
#The smaller the cutoff frequency&nbsp; $f_{\rm G}$&nbsp; of the Gaussian low-pass filter,&nbsp; the smaller the noise rms value &nbsp;$\sigma_d$&nbsp; and consequently the better the noise performance.<br>
 +
#However,&nbsp; a small cutoff frequency leads to a strong deviation of the basic detection pulse &nbsp;$g_d(t)$&nbsp; from the rectangular form and thus to intersymbol interference.}}<br>
  
*Eine kleine Grenzfrequenz führt aber zu einer starken Abweichung des Detektionsgrundimpulses <i>g<sub>d</sub></i>(<i>t</i>) von der Rechteckform und damit zu nicht vernachlässigbaren Impulsinterferenzen.<br><br>
+
{{GraueBox|TEXT= 
 +
$\text{Example 1:}$&nbsp; The left graph shows the basic detection pulse &nbsp;$g_d(t)$&nbsp; at the output of a Gaussian low-pass filter &nbsp;$H_{\rm G}(f)$&nbsp; with the cutoff frequency &nbsp;$f_{\rm G}$&nbsp; when an NRZ rectangular pulse (blue curve) is applied at the input.<br>
  
== Gaußförmiges Empfangsfilter (2) ==
+
[[File:P_ID1373__Dig_T_3_2_S1b_version1.png|right|frame|Basic detection pulse and noise power-spectral density&nbsp; $\rm (PSD)$&nbsp;  with Gaussian receiver filter]]
<br>
+
One can see from this plot:
Die nachfolgend linke Grafik zeigt den Detektionsgrundimpuls <i>g<sub>d</sub></i>(<i>t</i>) am Ausgang eines Gaußtiefpasses mit der Grenzfrequenz <i>f</i><sub>G</sub>, wenn am Eingang ein NRZ&ndash;Rechteckimpuls (blauer Kurvenverlauf) anliegt.<br>
+
*The Gaussian low-pass filter &nbsp;$H_{\rm G}(f)$&nbsp; causes the detection pulse &nbsp;$g_d(t)$&nbsp; to be reduced and broadened compared to the transmitted pulse &nbsp;$g_s(t)$&nbsp; &rArr; &nbsp; "'time dispersion".<br>
  
[[File:P_ID1373__Dig_T_3_2_S1b_version1.png|classs=fit|Grundimpuls und Rauschleistungsdichte bei gaußförmigem Empfangsfilter]]<br>
+
*The pulse deformation is the stronger,&nbsp; the smaller the cutoff frequency &nbsp;$f_{\rm G}$&nbsp; is.&nbsp; For example,&nbsp; with &nbsp;$f_{\rm G} \cdot T = 0.4$&nbsp; (red curve)&nbsp; the pulse maximum is already reduced to &nbsp;$\approx 68\%$.&nbsp;<br>
  
Man erkennt aus dieser Darstellung:
+
*In the limiting case &nbsp;$f_{\rm G} \to \infty$&nbsp; the Gaussian low-pass has no effect &nbsp; &#8658; &nbsp; $g_d(t) = g_s(t)$.&nbsp; However,&nbsp; in this case,&nbsp; there is no noise limitation at all,&nbsp; as can be seen from the right figure.}}
*Der Gaußtiefpass <i>H</i><sub>G</sub>(<i>f</i>) bewirkt, dass der Dektionsimpuls <i>g<sub>d</sub></i>(<i>t</i>) gegenüber dem Sendeimpuls <i>g<sub>s</sub></i>(<i>t</i>) verkleinert und verbreitert wird. Man spricht von <i>Zeitdispersion</i>.<br>
 
  
*Diese Impulsverformung ist umso stärker, je kleiner die Grenzfrequenz <i>f</i><sub>G</sub> ist. Beispielsweise wird mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4 (rote Kurve) das Impulsmaximum bereits auf etwa 68% herabgesetzt.<br>
 
  
*Im Grenzfall <i>f</i><sub>G</sub> &middot; <i>T</i> &#8594; &#8734; hat der Gaußtiefpass keine Wirkung &nbsp;&#8658;&nbsp; <i>g<sub>d</sub></i>(<i>t</i>) = <i>g<sub>s</sub></i>(<i>t</i>). Allerdings ist in diesem Fall keinerlei Rauschbegrenzung wirksam, wie aus dem rechten Bild hervorgeht.<br><br>
+
{{GraueBox|TEXT= 
 +
$\text{Example 2:}$&nbsp; The same preconditions apply as for the last example.&nbsp; The graph shows the detection signal &nbsp;$d(t)$&nbsp; after the Gaussian low-pass&nbsp; $($before the decision$)$&nbsp; for two different cutoff frequencies,&nbsp; namely &nbsp;$f_{\rm G} \cdot T = 0.8$&nbsp; and &nbsp;$f_{\rm G} \cdot T = 0.4$.&nbsp; We want to analyze these images in terms of intersymbol interference.
  
Die Grafik auf der folgenden Seite zeigt das Detektionssignal <i>d</i>(<i>t</i>) nach dem Gaußtiefpass (vor dem Entscheider) für zwei verschiedene Grenzfrequenzen:
+
[[File:Dig_T_3_2_S1c_version2_ret.png|right|frame|Detection signal with Gaussian receiver filter]]
 +
In both diagrams are shown:
 +
*the component &nbsp;$d_{\rm S}(\nu \cdot T)$&nbsp; of the detection signal without considering the noise&nbsp; $($blue circles at the detection times$)$,<br>
 +
*the total detection signal &nbsp;$d(t)$&nbsp; including the noise component (yellow curve),<br>
 +
*the transmitted signal &nbsp;$s(t)$&nbsp; as reference signal (green dotted in the upper graph; equally valid for the lower graph).<br><br>
  
*Der obere Signalverlauf gilt für die (normierte) Grenzfrequenz <i>f</i><sub>E</sub> &middot; <i>T</i> = 0.8.<br>
+
By comparing these images, the following statements can be verified  in terms of Intersymbol Interference&nbsp; $\rm  (ISI)$:
 +
*With the cutoff frequency &nbsp;$f_{\rm G} \cdot T = 0.8$&nbsp; (upper graph),&nbsp; only minor ISI result at the detection times&nbsp; $($at multiples of &nbsp;$T)$.&nbsp; Due to the Gaussian low-pass here primarily the corners of the transmitted signal &nbsp;$s(t)$&nbsp; are rounded.<br>
 +
*In contrast,&nbsp; in the lower image &nbsp;$(f_{\rm G} \cdot T = 0.4)$&nbsp; the ISI effects are clearly visible.&nbsp; At the detection times &nbsp;$(\nu \cdot T)$,&nbsp; the&nbsp;  $($blue$)$&nbsp; signal component &nbsp;$d_{\rm S}(\nu \cdot T)$&nbsp; of the detection signal can assume six different values&nbsp; $($compare grid lines drawn$)$.<br>
 +
*The noise component &nbsp;$d_{\rm N}(t)$ &ndash; recognizable as the difference between yellow curve and blue circles &ndash; is on average larger with $f_{\rm G} \cdot T = 0.8$&nbsp; than with $f_{\rm G} \cdot T = 0.4$.<br>
 +
*This result can be explained by the right graph of &nbsp;$\text{Example 1}$,&nbsp; which shows the PSD of the noise component &nbsp;$d_{\rm N}(t)$:&nbsp;
 +
:$${\it \Phi}_{d{\rm N} }(f) = {N_0}/{2} \cdot \vert H_{\rm G}(f) \vert^2 =
 +
{N_0}/{2} \cdot {\rm exp}\left [-
 +
\frac{2\pi  f^2}{(2f_{\rm G})^2} \right ] .$$
  
*Für den unteren Signalverlauf ist die Grenzfrequenz nur halb so groß: <i>f</i><sub>E</sub> &middot; <i>T</i> = 0.4.<br><br>
+
*The integral over &nbsp;${\it \Phi}_{d{\rm N} }(f)$&nbsp; &ndash; i.e. the noise power &nbsp;$\sigma_d^2$&nbsp; &ndash; is twice as large for &nbsp;$f_{\rm G} \cdot T = 0.8$&nbsp; (purple curve) than with &nbsp;$f_{\rm G} \cdot T = 0.4$&nbsp; (red curve).}}
  
Dargestellt sind in beiden Diagrammen gleichermaßen:
 
*der Anteil <i>d</i><sub>S</sub>(<i>t</i>) ohne Berücksichtigung des Rauschens (blau),<br>
 
*das gesamte Detektionssignal <i>d</i>(<i>t</i>) inklusive der Rauschkomponente (gelb),<br>
 
*das Sendesignal <i>s</i>(<i>t</i>) als Referenzsignal (grün gepunktet).<br><br>
 
  
Leider sind die verschiedenen Signalverläufe dieses Bildschirmabzugs sehr schwer zu erkennen, besonders in der PDF&ndash;Version. Die Bildbeschreibung folgt auf der nächsten Seite.<br>
+
== Definition and statements of the eye diagram==
 
 
== Gaußförmiges Empfangsfilter (3)==
 
 
<br>
 
<br>
Die Grafik zeigt das Detektionssignal <i>d</i>(<i>t</i>) nach dem Gaußtiefpass (also vor dem Entscheider) für zwei verschiedene (normierte) Grenzfrequenzen, nämlich <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8 und <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4.<br>
+
The above mentioned facts can also be explained by the eye diagram.  
 
 
[[File:P ID1384 Dig T 3 2 S1c version2.png|Detektionssignal bei gaußförmigem Empfangsfilter|class=fit]]<br>
 
 
 
Durch einen Vergleich dieser Bilder lassen sich folgende Aussagen verifizieren:
 
*Mit der Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8 (obere Grafik) ergeben sich zu den Detektionszeitpunkten (bei Vielfachen von <i>T</i>) nur geringfügige Impulsinterferenzen. Durch den Gaußtiefpass werden hier in erster Linie die Ecken des Sendesignals <i>s</i>(<i>t</i>) abgerundet.<br>
 
 
 
*Dagegen sind im unteren Bild (<i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4) die Auswirkungen der Impulsinterferenzen deutlich zu erkennen. Zu den Detektionszeitpunkten <i>&nu;</i><i>T</i> kann das blau dargestellte Detektionsnutzsignal <i>d</i><sub>S</sub>(<i>t</i>) sechs verschiedene Werte annehmen (eingezeichnete Rasterlinien).<br>
 
 
 
*Der Rauschanteil <i>d</i><sub>N</sub>(<i>t</i>) &ndash; erkennbar als Differenz zwischen der gelben und der blauen Kurve &ndash; ist mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8 im statistischen Mittel größer als mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4.<br>
 
  
*Dieses Ergebnis kann mit der der rechten Grafik auf der letzten Seite erklärt werden, die das Leistungsdichtespektrum der Rauschkomponente <i>d</i><sub>N</sub>(<i>t</i>) zeigt:
+
{{BlaueBox|TEXT= 
 +
$\text{Definition:}$&nbsp; The &nbsp;'''eye diagram'''&nbsp; (or&nbsp; "eye pattern")&nbsp; is the sum of all superimposed sections of the detection signal&nbsp; $d(t)$,&nbsp; whose duration is an integer multiple of the symbol duration &nbsp;$T$.&nbsp; This diagram has a certain resemblance to an eye, which led to its naming.}}
  
::<math>{\it \Phi}_{d{\rm N}}(f) = {N_0}/{2} \cdot |H_{\rm G}(f)|^2 =
 
{N_0}/{2} \cdot {\rm exp}\left [-
 
\frac{2\pi  f^2}{(2f_{\rm G})^2} \right ] .</math>
 
  
Das Integral über <i>&Phi;</i><sub><i>d</i>N</sub>(<i>f</i>) &ndash; also die Rauschleistung <i>&sigma;<sub>d</sub></i><sup>2</sup> &ndash; ist für
+
{{GraueBox|TEXT= 
<i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8 (violette Kurve) doppelt so groß als mit der kleineren Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4 (rote Kurve).<br>
+
$\text{Example 3:}$&nbsp; We assume a redundancy-free binary bipolar NRZ rectangular signal &nbsp;$s(t)$&nbsp; and the Gaussian low-pass filter with cutoff frequency &nbsp;$f_{\rm G} \cdot T = 0.4$.&nbsp;
 +
[[File:EN_Dig_T_3_2_S2.png|right|frame|On the left:&nbsp; Eye diagram with noise&nbsp; &#8658; &nbsp; signal &nbsp;$d(t)=d_{\rm S}(t) +d_{\rm N}(t)$, <br>on the right:&nbsp; Eye diagram without noise&nbsp; &#8658; &nbsp; signal &nbsp;$d_{\rm S}(t)$|class=fit]]
 +
In the graphic shown are the eye diagrams after the Gaussian low-pass,
 +
*left inclusive the noise component &nbsp; &#8658; &nbsp; signal &nbsp;$d(t)=d_{\rm S}(t) +d_{\rm N}(t)$,
 +
*on the right without taking noise into account &nbsp; &#8658; &nbsp; signal &nbsp;$d_{\rm S}(t)$.
  
== Definition und Aussagen des Augendiagramms==
 
<br>
 
Der oben dargelegte Sachverhalt lässt sich auch am Augendiagramm erklären. Wir gehen von einem redundanzfreien binären bipolaren NRZ&ndash;Rechtecksignal <i>s</i>(<i>t</i>) und dem Gaußtiefpass mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4 aus.  Dargestellt sind die Augendiagramme nach dem Gaußtiefpass, links  mit Berücksichtigung des Rauschens &nbsp;&#8658;&nbsp; Signal <i>d</i>(<i>t</i>) und rechts ohne Berücksichtigung des Rauschens &nbsp;&#8658;&nbsp; Signal <i>d</i><sub>S</sub>(<i>t</i>).<br>
 
  
[[File:P ID1375 Dig T 3 2 S2 version1.png|Augendiagramme mit und ohne Rauschen|class=fit]]<br>
 
  
{{Definition}}''':''' Unter dem Augendiagramm (im Englischen: <i>Eye Pattern</i>) versteht man die Summe aller übereinander gezeichneten Ausschnitte des Detektionssignals, deren Dauer ein ganzzahliges Vielfaches der Symboldauer <i>T</i> ist.{{end}}<br>
+
This representation allows important statements about the quality of a digital transmission system:
  
Dieses Diagramm hat eine gewisse Ähnlichkeit mit einem Auge, was zu seiner Namensgebung geführt hat. Diese Darstellung erlaubt wichtige Aussagen über die Qualität eines digitalen Übertragungssystems:
+
*Only the eye diagram of the signal &nbsp;$d(t)$&nbsp; can be displayed metrologically on an oscilloscope,&nbsp; which is triggered with the clock signal.&nbsp; From this eye diagram&nbsp; $($left graph$)$,&nbsp; for example,&nbsp; the noise rms value &nbsp;$\sigma_d$&nbsp; $($&#8658; &nbsp; noise power &nbsp;$\sigma_d^2)$&nbsp; can be read &ndash; or rather: &nbsp;estimated.<br>
*Nur das Augendiagramm des Signals <i>d</i>(<i>t</i>) kann messtechnisch auf einem Oszilloskop dargestellt werden, das mit dem Taktsignal getriggert wird. Aus diesem Augendiagramm (linke Grafik) kann beispielsweise der Rauscheffektivwert <i>&sigma;<sub>d</sub></i> abgelesen &ndash; besser gesagt: abgeschätzt &ndash; werden.<br>
 
  
*Das Augendiagramm ohne Rauschen (rechte Grafik) bezieht sich auf das Detektionsnutzsignal <i>d</i><sub>S</sub>(<i>t</i>) und kann nur mittels einer Rechnersimulation ermittelt werden. Für ein realisiertes System ist dieses Augendiagramm nicht darstellbar, da der Rauschanteil <i>d</i><sub>N</sub>(<i>t</i>) nicht eliminiert werden kann.<br>
+
*The eye diagram without noise&nbsp; (right graph)&nbsp; refers to the signal component &nbsp;$d_{\rm S}(t)$&nbsp; of the detection signal  and can only be determined by means of a computer simulation.&nbsp; For an implemented system,&nbsp; this eye diagram cannot be displayed,&nbsp; since the noise component &nbsp;$d_{\rm N}(t)$&nbsp; cannot be eliminated.<br>
  
*Bei beiden Diagrammen wurden jeweils 2048 Augenlinien gezeichnet. In der rechten Grafik sind jedoch nur 2<sup>5</sup> = 32 Augenlinien unterscheidbar, da der vorliegende Detektionsgrundimpuls <i>g<sub>d</sub></i>(<i>t</i>) auf den Zeitbereich | <i>t</i> | &#8804; 2<i>T</i> beschränkt ist (siehe frühere Grafik mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4, rote Kurve).<br>
+
*In both diagrams of this example, &nbsp;$2^{11}=2048$&nbsp; eye lines were drawn in each case.&nbsp; In the right graph,&nbsp; however,&nbsp; only &nbsp;$2^5 = 32$&nbsp; eye lines are distinguishable because the present detection pulse &nbsp;$g_d(t)$&nbsp; is limited to the time range &nbsp;$\vert t\vert \le  2T$&nbsp; <br>$($see &nbsp;[[Digital_Signal_Transmission/Error_Probability_with_Intersymbol_Interference#Gaussian_receiver_filter|graph in Example 1]]&nbsp; with &nbsp;$f_{\rm G} \cdot T = 0.4$,&nbsp; red curve$)$.<br>
  
*Die inneren Augenlinien bestimmen die vertikale Augenöffnung <i>ö</i>(<i>T</i><sub>D</sub>). Je kleiner diese ist, desto größer ist der Einfluss von Impulsinterferenzen. Bei einem (impulsinterferenzfreien) Nyquistsystem ist die vertikale Augenöffnung maximal. Normiert auf die Sendeamplitude  gilt hier <i>ö</i>(<i>T</i><sub>D</sub>)/<i>s</i><sub>0</sub> = 2. <br>
+
*The inner eye lines determine the&nbsp; '''vertical eye opening'''&nbsp; $\ddot{o}(T_{\rm D})$.&nbsp; The smaller this is,&nbsp; the greater is the influence of intersymbol interference.&nbsp; For a&nbsp; $($ISI-free$)$&nbsp; Nyquist system the vertical eye opening is maximum.&nbsp; Normalized to the transmitted amplitude, &nbsp;$\ddot{o}(T_{\rm D})/s_0 = 2$&nbsp; is then valid. <br>
  
*Bei symmetrischem Grundimpuls ist der Detektionszeitpunkt <i>T</i><sub>D</sub> = 0 optimal. Mit einem anderen Wert (z.B. <i>T</i><sub>D</sub> = &ndash; <i>T</i>/10) wäre <i>ö</i>(<i>T</i><sub>D</sub>)/<i>s</i><sub>0</sub> etwas kleiner und damit die Fehlerwahrscheinlichkeit deutlich größer. Dieser Fall ist in der Grafik durch die violett&ndash;gestrichelte Vertikale angedeutet.<br>
+
*With symmetrical basic detection pulse,&nbsp; the detection time &nbsp;$T_{\rm D} = 0$&nbsp; is optimal.&nbsp; With a different value&nbsp; $($for example  &nbsp;$T_{\rm D} = -T/10) $, &nbsp; $\ddot{o}(T_{\rm D})$&nbsp; would be somewhat smaller and thus the error probability would be significantly larger.&nbsp; This case is indicated by the purple&ndash;dashed vertical line in the right graph.}}
  
== Mittlere Fehlerwahrscheinlichkeit (1)==
+
== Mean error probability==
 
<br>
 
<br>
Wir gehen wie bei den bisherigen Grafiken im Kapitel 3.2 von folgenden Voraussetzungen aus:
+
As with the previous graphs in this chapter,&nbsp; we assume the following:
*NRZ&ndash;Rechtecke mit Amplitude <i>s</i><sub>0</sub>, AWGN&ndash;Rauschen mit <i>N</i><sub>0</sub>, wobei
+
[[File:P ID1377 Dig T 3 2 S3 version1.png|right|frame|Eye diagram and discrete PDF of the signal component &nbsp;$d_{\rm S}(t)$&nbsp; from &nbsp;$d(t)$|class=fit]]
 
+
*NRZ rectangles with amplitude &nbsp;$s_0$, &nbsp;AWGN noise with power-spectral density &nbsp;$N_0$,&nbsp; where
::<math>10 \cdot {\rm lg}\hspace{0.1cm} \frac{s_0^2 \cdot T}{N_0}\approx
+
:$$10 \cdot {\rm lg}\hspace{0.1cm} \frac{s_0^2 \cdot T}{N_0}\approx
13\,{\rm dB}\hspace{0.3cm}\Rightarrow \hspace{0.3cm}
+
13\,{\rm dB}\hspace{0.3cm} \Rightarrow \hspace{0.3cm}
\frac{N_0}{s_0^2 \cdot T} = 0.05\hspace{0.05cm}.</math>
+
\frac{N_0}{s_0^2 \cdot T} = 0.05\hspace{0.05cm}.$$
 +
*Gaussian receiver filter with cutoff frequency &nbsp;$f_{\rm G} \cdot T = 0.4$:
 +
:$$\sigma_d^2 = \frac{(N_0 /T)\cdot (f_{\rm G}\cdot T)}{\sqrt{2}}= \frac{0.05 \cdot
 +
s_0^2\cdot0.4}{\sqrt{2}}$$
 +
:$$ \Rightarrow \hspace{0.3cm} \sigma_d = \sqrt{0.0141}\cdot s_0
 +
\approx 0.119 \cdot s_0 \hspace{0.05cm}.$$
 +
* Let &nbsp;$g_d(\nu \cdot T) \approx 0$&nbsp; be valid for &nbsp;$|\nu| \ge 2$.&nbsp; The other basic detection pulse values are given as follows:
 +
:$$g_0  =  g_d(t=0) \approx 0.68 \cdot s_0,$$
 +
:$$g_1  =  g_d(t=T) \approx 0.16 \cdot s_0,$$
 +
:$$g_{-1} = g_d(t=-T) \approx
 +
0.16 \cdot s_0\hspace{0.05cm}.$$
  
*Gaußförmiges Empfangsfilter mit Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4:
+
Let us now analyze the possible values for the signal component &nbsp;$d_{\rm S}(t)$&nbsp; at the detection times:
 +
*Of the total &nbsp;$32$&nbsp; eye lines,&nbsp; four lines intersect the ordinate &nbsp;$(t = 0)$&nbsp; at &nbsp;$g_0 + 2 \cdot g_1 = s_0$.&nbsp; These lines belong to the amplitude coefficients&nbsp; "$\text{...}\hspace{0.05cm} +\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} +\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$".&nbsp; &nbsp; Here,&nbsp; the&nbsp; "middle"&nbsp; coefficient &nbsp;$a_{\nu = 0}$&nbsp; is highlighted in italics.<br>
  
::<math>\sigma_d^2 = \frac{(N_0 /T)\cdot (f_{\rm G}\cdot T)}{\sqrt{2}}= \frac{0.05 \cdot
+
*The four eye lines,&nbsp; each representing the coefficients &nbsp;"$\text{...}\hspace{0.05cm} -\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} -\hspace{-0.05cm}1,\hspace{0.05cm} \text{...}$"&nbsp; result in the signal value &nbsp;$d_{\rm S}(T_{\rm D} = 0) =g_0 - 2 \cdot g_1 = 0.36 \cdot s_0$.<br>
s_0^2\cdot0.4}{\sqrt{2}} \hspace{0.3cm} \Rightarrow \hspace{0.3cm} \sigma_d = \sqrt{0.0141}\cdot s_0
 
\approx 0.119 \cdot s_0 \hspace{0.05cm}.</math>
 
  
*Für die Detektionsgrundimpulswerte gilt:
+
*In contrast,&nbsp; the signal value &nbsp;$d_{\rm S}(T_{\rm D} = 0) =g_0 = 0.68 \cdot s_0$&nbsp; occurs twice as often.&nbsp; This goes back either to the coefficients &nbsp;"$\text{...}\hspace{0.05cm} +\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} -\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$"&nbsp; or to  &nbsp;"$\text{...}\hspace{0.05cm} -\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} +\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$".&nbsp; <br>
  
::<math>g_0  =  g_d(t=0) \approx 0.68 \cdot s_0,</math>
+
*For the &nbsp;$16$&nbsp; eye lines which intersect the ordinate &nbsp;$T_{\rm D} = 0$&nbsp; below the decision threshold &nbsp;$E = 0$,&nbsp; exactly mirror-image relations result.<br><br>
::<math> g_1  = g_d(t=T) \approx 0.16 \cdot s_0, \hspace{0.2cm} g_{-1} = g_d(t=-T) \approx
 
0.16 \cdot s_0\hspace{0.05cm}.</math>
 
  
Alle anderen Grundimpulswerte können vernachlässigt werden.<br>
+
The possible values &nbsp;$d_{\rm S}(T_{\rm D})$&nbsp; and their occurrence probabilities can be found in the above graph on the left side in the&nbsp; (discrete)&nbsp; &nbsp;[[Theory_of_Stochastic_Signals/Probability_Density_Function#PDF_definition_for_discrete_random_variables|probability density function]]&nbsp; $\rm (PDF)$&nbsp; of the noise-free detection signal samples:
 
+
:$$f_{d{\rm S}}(d_{\rm S})  =  {1}/{8} \cdot \delta (d_{\rm S}
[[File:P ID1377 Dig T 3 2 S3 version1.png|Augendiagramm und WDF des Nutzsignals|class=fit]]<br>
 
 
 
Analysieren wir nun die möglichen Werte für das Detektionsnutzsignal zu den Detektionszeitpunkten:
 
*Von den insgesamt 32 Augenlinien schneiden vier die Ordinate <i>t</i> = 0 bei <i>g</i><sub>0</sub> + 2 &middot; <i>g</i><sub>1</sub> = <i>s</i><sub>0</sub>. Diese Linien gehören zu den Amplitudenkoeffizienten &bdquo; ... , +1, +1, +1, ... &rdquo;.<br>
 
 
 
*Die vier Augenlinien, die jeweils die Amplitudenkoeffizienten &bdquo; ... , &ndash;1, +1, &ndash;1, ... &rdquo; repräsentieren, ergeben den Detektionsnutzabtastwert <i>d</i><sub>S</sub>(<i>T</i><sub>D</sub> = 0) = <i>g</i><sub>0</sub> &ndash; 2 &middot; <i>g</i><sub>1</sub> = 0.36 &middot; <i>s</i><sub>0</sub>.<br>
 
 
 
*Dagegen tritt der Nutzabtastwert <i>d</i><sub>S</sub>(<i>T</i><sub>D</sub> = 0) = <i>g</i><sub>0</sub> = 0.68 &middot; <i>s</i><sub>0</sub> doppelt so häufig auf. Dieser geht auf die Amplitudenkoeffizienten &bdquo; ... , +1, +1, &ndash;1, ... &rdquo; oder &bdquo; ... , &ndash;1, +1, +1, ... &rdquo; zurück.<br>
 
 
 
*Für die 16 Augenlinien, welche die Ordinate <i>t</i> = 0 unterhalb der Entscheiderschwelle <i>E</i> = 0 schneiden, ergeben sich genau spiegelbildliche Verhältnisse.<br><br>
 
 
 
Die Konsequenzen dieser Analyse werden auf der nächsten Seite beschrieben.<br>
 
 
 
== Mittlere Fehlerwahrscheinlichkeit (2) ==
 
<br>
 
[[File:P ID1377 Dig T 3 2 S3 version1.png|Augendiagramm und WDF des Nutzsignals|class=fit]]<br>
 
 
 
Die möglichen Werte <i>d</i><sub>S</sub>(<i>T</i><sub>D</sub>) und deren Auftrittswahrscheinlichkeiten findet man in obiger Grafik in der Wahrscheinlichkeitsdichtefunktion (WDF) der Detektionsnutzabtastwerte wieder:
 
 
 
:<math>f_{d{\rm S}}(d_{\rm S})  =  {1}/{8} \cdot \delta (d_{\rm S}
 
 
- s_0)+ {1}/{4} \cdot \delta (d_{\rm S} - 0.68 \cdot s_0)+
 
- s_0)+ {1}/{4} \cdot \delta (d_{\rm S} - 0.68 \cdot s_0)+
{1}/{8} \cdot \delta (d_{\rm S} - 0.36 \cdot s_0)+ </math>
+
{1}/{8} \cdot \delta (d_{\rm S} - 0.36 \cdot s_0)+ $$
::::<math> + {1}/{8} \cdot \delta (d_{\rm S} + s_0)+{1}/{4}
+
$$\hspace{2.15cm} + \hspace{0.2cm} {1}/{8} \cdot \delta (d_{\rm S} + s_0)+{1}/{4}
 
\cdot \delta (d_{\rm S} + 0.68 \cdot s_0)+{1}/{8} \cdot
 
\cdot \delta (d_{\rm S} + 0.68 \cdot s_0)+{1}/{8} \cdot
\delta (d_{\rm S} + 0.36 \cdot s_0)\hspace{0.05cm}.</math>
+
\delta (d_{\rm S} + 0.36 \cdot s_0)\hspace{0.05cm}.$$
 
 
Damit kann die (mittlere) Symbolfehlerwahrscheinlichkeit des impulsinterferenzbehafteten Systems angegeben werden. Unter Ausnutzung der Symmetrie erhält man mit <i>&sigma;<sub>d</sub></i>/<i>s</i><sub>0</sub> = 0.119:
 
  
:<math>p_{\rm S}  =  {1}/{4} \cdot {\rm Q} \left( \frac{s_0}{ \sigma_d}
+
Thus,&nbsp; the&nbsp; (average)&nbsp; symbol error probability of the of the ISI-afflicted system can be given.&nbsp; Taking advantage of the symmetry,&nbsp; one obtains with &nbsp;$\sigma_d/s_0 = 0.119$:
 +
:$$p_{\rm S}  =  {1}/{4} \cdot {\rm Q} \left( \frac{s_0}{ \sigma_d}
 
   \right)+ {1}/{2} \cdot {\rm Q} \left( \frac{0.68 \cdot s_0}{ \sigma_d}
 
   \right)+ {1}/{2} \cdot {\rm Q} \left( \frac{0.68 \cdot s_0}{ \sigma_d}
 
   \right)+{1}/{4} \cdot {\rm Q} \left( \frac{0.36 \cdot s_0}{ \sigma_d}
 
   \right)+{1}/{4} \cdot {\rm Q} \left( \frac{0.36 \cdot s_0}{ \sigma_d}
   \right)</math>
+
   \right)$$
::<math>   \approx  {1}/{4} \cdot {\rm Q}(8.40) +{1}/{2} \cdot {\rm Q}(5.71)+ {1}/{4} \cdot {\rm
+
:$$\Rightarrow \hspace{0.3cm}p_{\rm S}   \approx  {1}/{4} \cdot {\rm Q}(8.40) +{1}/{2} \cdot {\rm Q}(5.71)+ {1}/{4} \cdot {\rm
   Q}(3.02)\approx</math>
+
   Q}(3.02)\approx
::<math> \approx {1}/{4} \cdot 2.20 \cdot 10^{-17}+ {1}/{2} \cdot 1.65 \cdot
+
  {1}/{4} \cdot 2.20 \cdot 10^{-17}+ {1}/{2} \cdot 1.65 \cdot
   10^{-9}+ {1}/{4} \cdot 1.26 \cdot 10^{-3} \approx 3.14 \cdot 10^{-4}
+
   10^{-9}+ {1}/{4} \cdot 1.26 \cdot 10^{-3} \approx 3.14 \cdot 10^{-4}
  \hspace{0.05cm}.</math>
+
  \hspace{0.05cm}.$$
  
Anhand dieses Zahlenbeispiels erkennt man, dass
+
<u>Note:</u> &nbsp; For redundancy-free binary bipolar transmission,&nbsp; the bit error probability&nbsp; $p_{\rm B}$&nbsp; is identical to the symbol error probability&nbsp; $p_{\rm S}$.
*bei Vorhandensein von Impulsinterferenzen die (mittlere) Fehlerwahrscheinlichkeit <i>p</i><sub>S</sub> wesentlich durch die inneren Augenlinien bestimmt wird,<br>
 
  
*der Rechenaufwand zur Bestimmung der Fehlerwahrscheinlichkeit <i>p</i><sub>S</sub> sehr groß ist, insbesondere dann, wenn die Impulsinterferenzen von sehr vielen Grundimpulswerten <i>g<sub>&nu;</sub></i> herrühren.<br><br>
+
{{BlaueBox|TEXT= 
 +
$\text{On the basis of this numerical example one recognizes:}$&nbsp;
 +
#In the presence of intersymbol interference,&nbsp; the&nbsp; (average)&nbsp; symbol error probability &nbsp;$p_{\rm S}$&nbsp; is essentially determined by the inner eye lines.<br>
 +
#The computational cost of determining  &nbsp;$p_{\rm S}$&nbsp; can become very large,&nbsp; especially if the ISI comes from very many basic detection pulse values &nbsp;$g_\nu$.&nbsp; }}
  
{{Beispiel}}''':''' Gilt wie hier <i>g</i><sub>2</sub> = <i>g</i><sub>&ndash;2</sub> = ... = 0, so muss zur Berechnung von <i>p</i><sub>S</sub> nur über drei Terme (falls <i>g</i><sub>&ndash;1</sub> = <i>g</i><sub>1</sub>) bzw. über vier Terme (andernfalls) gemittelt werden, wenn die Symmetrie bezüglich der Entscheiderschwelle <i>E</i> = 0 berücksichtigt wird. Sind dagegen die Grundimpulswerte <i>g</i><sub>&ndash;5</sub>, ... , <i>g</i><sub>5</sub> von Null verschieden und <i>E</i> &ne; 0, so ist eine Mittelung über bis zu 2<sup>11</sup> = 2048 Augenlinien erforderlich.{{end}} <br>
 
  
== Ungünstigste Fehlerwahrscheinlichkeit (1)==
+
{{GraueBox|TEXT=
<br>
+
$\text{Example 4:}$&nbsp;
Als eine sehr einfache Näherung für die tatsächliche Fehlerwahrscheinlichkeit <i>p</i><sub>S</sub>
+
*If the pulse values &nbsp;$g_{-5}, \text{...} \ , g_{+5}$&nbsp; are different from zero and &nbsp;$E \ne  0$, an averaging over &nbsp;$2^{11} = 2048$&nbsp;  eye lines is necessary to determine the error probability &nbsp;$p_{\rm S}$.
verwendet man häufig die ungünstigste Fehlerwahrscheinlichkeit (englisch: <i>Worst-Case Error Probability</i>)
+
 
 +
*If,&nbsp; on the other hand,&nbsp; only the pulse values &nbsp;$g_{-1}, \ g_0, \ g_{+1}$&nbsp; are different from zero and,&nbsp; in addition,&nbsp; the symmetry with respect to the threshold &nbsp;$E = 0$&nbsp; is taken into account,&nbsp; the effort is reduced to averaging over four terms.
  
:<math>p_{\rm U} = {\rm Q} \left( \frac{\ddot{o}(T_{\rm D})/2}{ \sigma_d}
+
* If,&nbsp; in addition,&nbsp; the symmetry &nbsp;$g_{-1} = g_{+1}$&nbsp; applies as with the above numerical values,&nbsp; then the symmetry with respect to &nbsp;$T_{\rm D}$&nbsp; can also be exploited and averaging over three terms is sufficient. }} <br>
  \right) \hspace{0.05cm},</math>
 
  
für deren Berechnung stets von den ungünstigsten Symbolfolgen ausgegangen wird. Das bedeutet, dass hier die tatsächliche WDF der Nutzabtastwerte (in der Grafik links eingezeichnet) durch eine vereinfachte WDF mit nur den beiden inneren Diracfunktionen (in der Grafik rechts dargestellt) ersetzt wird.<br>
+
== Worst-case error probability==
 +
<br>
 +
In the past,&nbsp; a variety of approximations for the average error probability have been given, among others:
  
[[File:P ID1379 Dig T 3 2 S4 version1.png|Zusammenhang zwischen mittlerer und ungünstigster Fehlerwahrscheinlichkeit|class=fit]]<br>
+
{{BlaueBox|TEXT= 
 +
$\text{Definition:}$&nbsp; As a very simple approximation for the actual error probability &nbsp;$p_{\rm S}$,&nbsp;
 +
the &nbsp;'''worst-case error probability'''&nbsp; (German:&nbsp; "ungünstigste Fehlerwahrscheinlichkeit" &nbsp; &rArr; &nbsp; subscript:&nbsp; "U")&nbsp; is often used:
 +
[[File:EN_Dig_T_3_2_S4_neu.png|right|frame|"Mean symbol error probability"&nbsp; $p_{\rm S}$&nbsp; vs.&nbsp; "worst-case symbol error probability"&nbsp; $p_{\rm U}$ |class=fit]]
 +
:$$p_{\rm U} = {\rm Q} \left( \frac{\ddot{o}(T_{\rm D})/2}{ \sigma_d}
 +
  \right) \hspace{0.05cm}.$$
  
Für die halbe vertikale Augenöffnung gilt mit den Grundimpulswerten <i>g<sub>&nu;</sub></i> = <i>g<sub>d</sub></i>(<i>T</i><sub>D</sub> + <i>&nu;</i> &middot; <i>T</i>) allgemein:
+
For their calculation,&nbsp; the&nbsp; "worst-case symbol sequences"&nbsp; are always assumed.&nbsp; This means:
  
:<math>{\ddot{o}(T_{\rm D})}/{ 2}= g_0 - \sum_{\nu =
+
*The actual probability density function&nbsp; $\rm (PDF)$&nbsp; of the samples&nbsp;$d_{\rm S}(T_{\rm D})$&nbsp; (left graph: &nbsp;six red Dirac delta functions)&nbsp; is replaced by a simplified PDF with only the inner Dirac delta functions&nbsp; (right graph: &nbsp;two green Diracs).<br>
  1}^{n}|g_{\nu}|- \sum_{\nu = 1}^{v}|g_{-\nu}|
 
  \hspace{0.05cm}.</math>
 
  
Diese Gleichung kann wie folgt interpretiert werden:
+
*For the half vertical eye opening,&nbsp; with the basic detection pulse values &nbsp;$g_\nu = g_d( T_{\rm D}+ \nu \cdot T)$&nbsp; generally holds:
*<i>g</i><sub>0</sub> = <i>g<sub>d</sub></i>(<i>T</i><sub>D</sub>) ist der so genannte Hauptwert des Grundimpulses. Bei Nyquistsystemen gilt stets  <i>ö</i>(<i>T</i><sub>D</sub>)/2 = <i>g</i><sub>0</sub>. Mit Ausnahme von Kapitel 3.6 wird im Folgenden stets <i>T</i><sub>D</sub> = 0 gesetzt.<br>
+
:$$\ddot{o}(T_{\rm D})/{ 2}= g_0 - \sum_{\nu = 1}^{n} \vert g_{\nu} \vert- \sum_{\nu = 1}^{v} \vert g_{-\nu} \vert  \hspace{0.05cm}.$$}}
  
*Die erste Summe beschreibt die Impulsinterferenzen der <i>n</i> Nachläufer vorangegangener Impulse. Stillschweigend vorausgesetzt wird <i>g<sub>&nu;</sub></i> = 0 für <i>&nu;</i> &gt; <i>n</i>.<br>
 
  
*Die zweite Summe berücksichtigt den Einfluss der <i>&upsilon;</i> Vorläufer nachfolgender Impulse unter der Voraussetzung <i>g<sub>&ndash;&nu;</sub></i> = 0 für <i>&nu;</i> &gt; <i>&upsilon;</i>.<br>
+
This equation can be interpreted as follows:
 +
*$g_0 = g_d( T_{\rm D})$&nbsp; is the so-called&nbsp; "main value"&nbsp; of the basic detection pulse.&nbsp; For Nyquist systems &nbsp;$\ddot{o}(T_{\rm D})/{ 2}= g_0$&nbsp; is always valid.&nbsp; In the following&nbsp; (mostly)&nbsp; &nbsp;$T_{\rm D}= 0$&nbsp; is set.<br>
  
*Sind alle Impulsvor&ndash; und &ndash;nachläufer positiv, so lauten die beiden ungünstigsten Symbolfolgen &bdquo;&nbsp;... , &ndash;1, &ndash;1, +1, &ndash;1, &ndash;1, ... &rdquo; und &bdquo; ... , +1, +1, &ndash;1, +1, +1, ... &rdquo;. Dies trifft zum Beispiel für das hier betrachtete gaußförmige Empfangsfilter zu.<br>
+
*The first sum describes the ISI influence of the &nbsp;$n$&nbsp; "trailers"&nbsp; $($German:&nbsp; "Nachläufer"&nbsp; &rArr; &nbsp; variable&nbsp; $n)$&nbsp; of preceding pulses&nbsp; $($sometimes we use the term&nbsp; "postcursor"$)$.&nbsp; Tacitly assumed is &nbsp;$g_\nu = 0$&nbsp; for &nbsp;$\nu  \gt n$.&nbsp; <br>
  
*Sind einige Grundimpulswerte negativ, so wird dies in obiger Gleichung durch die Betragsbildung berücksichtigt. Es ergeben sich dann andere &bdquo;Worst&ndash;case&rdquo;&ndash;Folgen als gerade genannt.<br>
+
*The second sum considers the influence of the &nbsp;$v$&nbsp; "precursors"&nbsp; $($German:&nbsp; "Vorläufer"&nbsp; &rArr; &nbsp; variable&nbsp; $v)$&nbsp; of following pulses under the condition &nbsp;$g_{-\nu} = 0$&nbsp; for &nbsp;$\nu  \gt v$.<br>
  
== Ungünstigste Fehlerwahrscheinlichkeit (2) ==
+
*If all precursors and trailers are positive,&nbsp; the two worst-case symbol sequences are &nbsp;"$\text{...}\hspace{0.05cm} -\hspace{-0.1cm}1,\hspace{0.05cm} -\hspace{-0.05cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} -\hspace{-0.05cm}1,\hspace{0.05cm} -\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$"&nbsp; and &nbsp;"$\text{...}\hspace{0.05cm} +\hspace{-0.1cm}1,\hspace{0.05cm} +\hspace{-0.05cm}1,\hspace{0.05cm} {\it -\hspace{-0.05cm}1},\hspace{0.05cm} +\hspace{-0.05cm}1,\hspace{0.05cm} +\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$"&nbsp; (coefficient &nbsp;$a_{\nu = 0}$&nbsp; is in italics in each case).&nbsp; These specifications apply,&nbsp; for example,&nbsp; to the Gaussian receiver filter considered here.<br>
<br>
 
Die Grafik zeigt die Fehlerwahrscheinlichkeiten in Abhängigkeit des Quotienten <i>E</i><sub>B</sub>/<i>N</i><sub>0</sub>, nämlich
 
*die mittlere Fehlerwahrscheinlichkeit <i>p</i><sub>S</sub> bei gaußförmigem Empfangsfilter (blaue Kreise),<br>
 
*die ungünstigste Fehlerwahrscheinlichkeit <i>p</i><sub>U</sub> bei gaußförmigem Empfangsfilter (blaue Rechtecke),<br>
 
*die Fehlerwahrscheinlichkeit (<i>p</i><sub>S</sub> = <i>p</i><sub>U</sub>) des Optimalempfängers gemäß Kapitel 1.2 (rote Kurve).<br><br>
 
  
Die Energie pro Bit ist dabei gleich <i>E</i><sub>B</sub> = <i>s</i><sub>0</sub><sup>2</sup> &middot; <i>T</i> (NRZ&ndash;Rechteck&ndash;Sendeimpulse).<br>
+
*If some basic detection pulse values&nbsp; $g_{\nu\ne 0}$&nbsp; are negative,&nbsp; this is taken into account in the above equation by the magnitude formation.&nbsp; This results in other "worst&ndash;case" sequences than those just mentioned.<br>
  
[[File:P ID1385 Dig T 3 2 S4b version2.png|Mittlere und ungünstigste Fehlerwahrscheinlichkeit vs. E<sub>B</sub>/N<sub>0</sub>|class=fit]]<br>
 
  
Die linke Grafik gilt für die (normierte) Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4, die rechte für ein breitbandigeres Empfangsfilter mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8. Diese Ergebnisse können wie folgt interpretiert werden:
+
{{GraueBox|TEXT= 
*Die ungünstigste Fehlerwahrscheinlichkeit <i>p</i><sub>U</sub> ist stets eine obere Schranke für die tatsächliche Symbolfehlerwahrscheinlichkeit <i>p</i><sub>S</sub>. Je kleiner der Einfluss der Impulsinterferenzen ist (große Grenzfrequenz), um so näher liegen <i>p</i><sub>S</sub> und <i>p</i><sub>U</sub> zusammen. Beim Optimalempfänger gilt <i>p</i><sub>S</sub> = <i>p</i><sub>U</sub>.<br>
+
$\text{Example 5:}$&nbsp; The graph shows the error probabilities of the AWGN channel as a function of the (logarithmized) quotient &nbsp;$E_{\rm B}/N_0$,&nbsp; namely
  
*Bei gaußförmigem Empfangsfilter mit <i>f</i><sub>G</sub> &middot; <i>T</i> &#8805; 0.3 werden die Impulsinterferenzen allein durch die Nachbarimpulse hervorgerufen (<i>g</i><sub>2</sub> = <i>g</i><sub>3</sub> = ... &asymp; 0), so dass für <i>p</i><sub>S</sub> auch eine untere Schranke angegeben werden kann:
+
*the average error probability &nbsp;$p_{\rm S}$&nbsp; with Gaussian receiver filter&nbsp; (blue circles),<br>
 +
*the worst-case error probability &nbsp;$p_{\rm U}$&nbsp; with Gaussian receiver filter&nbsp; (blue rectangles),<br>
 +
*the smallest possible error probability according to the section&nbsp;[[Digital_Signal_Transmission/Error_Probability_for_Baseband_Transmission#Optimal_binary_receiver_.E2.80.93_.22Matched_Filter.22_realization|"Optimal binary receiver"]]&nbsp; (red curve).<br><br>
  
::<math>{p_{\rm U}}/{ 4} \le p_{\rm S} \le p_{\rm U}
+
Here,&nbsp; the energy per bit is equal to &nbsp;$E_{\rm B} = s_0^2 \cdot T$&nbsp; (redundancy-free binary bipolar transmission,&nbsp; NRZ rectangular transmitted pulses).<br>
  \hspace{0.05cm}.</math>
 
  
*Die starken Impulsinterferenzen eines gaußförmigen Empfangsfilters mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.4 führen dazu, dass gegenüber dem Optimalempfänger ein um 6 dB größeres <i>E</i><sub>B</sub>/<i>N</i><sub>0</sub> aufgewendet werden muss (vierfache Leistung), damit die Fehlerwahrscheinlichkeit den Wert 10<sup>&ndash;8</sup> nicht überschreitet.<br>
+
The left graph is for the&nbsp; (normalized)&nbsp; cutoff frequency &nbsp;$f_{\rm G} \cdot T = 0.4$,&nbsp; the right one for a broader band receiver filter with &nbsp;$f_{\rm G} \cdot T = 0.8$.  
  
*Der horizontale Abstand zwischen der blauen <i>p</i><sub>S</sub>&ndash;Kurve (markiert durch Kreise) und der roten Vergleichskurve ist aber nicht konstant. Bei <i>p</i><sub>S</sub> = 10<sup>&ndash;2</sup> beträgt der Abstand nur 4 dB.<br>
+
[[File:EN_Dig_T_3_2_S4_b_neu.png|right|frame|Mean error probability&nbsp; $p_{\rm S}$&nbsp; and&nbsp; worst-case error probability&nbsp; $p_{\rm U}$&nbsp; as a function of &nbsp;$E_{\rm B}/N_0$|class=fit]]
 +
The results can be interpreted as follows:
 +
*$p_{\rm U}$&nbsp; is always an upper bound for the actual symbol error probability &nbsp;$p_{\rm S}$.&nbsp;  The smaller the influence of the intersymbol interference&nbsp; (large cutoff frequency),&nbsp; the closer &nbsp;$p_{\rm S}$&nbsp; and &nbsp;$p_{\rm U}$&nbsp; are to each other.&nbsp; For the optimal receiver &nbsp;$p_{\rm S} = p_{\rm U}.$
  
*Die rechte Grafik zeigt, dass mit <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8 der Abstand zum Vergleichssystem weniger als 1 dB beträgt. Auf der nächsten Seite wird gezeigt, dass bei einem gaußförmigen Empfangsfilter die (normierte) Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8 näherungsweise das Optimum darstellt.<br>
+
*For a Gaussian receiver filter with &nbsp;$f_{\rm G} \cdot T \ge 0.3$,&nbsp; the ISI are caused by the neighboring pulses alone &nbsp;$(g_2 = g_3 = \text{...} \approx 0)$,&nbsp; so that a lower bound can also be given:&nbsp; ${p_{\rm U} }/{ 4} \le p_{\rm S} \le p_{\rm U}
 +
  \hspace{0.05cm}.$
  
== Optimierung der Grenzfrequenz (1) ==
+
*The strong ISI of a Gaussian receiver filter with &nbsp;$f_{\rm G} \cdot T = 0.4$&nbsp; leads to the fact that compared to the optimal receiver a &nbsp;$6 \ \rm dB$ larger $E_{\rm B}/N_0$&nbsp; must be applied (four times the power), so that the error probability does not exceed the value &nbsp;$10^{-8}$.&nbsp; <br>
<br>
 
Für die Systemoptimierung und den Systemvergleich erweist es sich als zweckmäßig, anstelle von <i>p</i><sub>U</sub> das ungünstigste Signal&ndash;zu&ndash;Rausch&ndash;Leistungsverhältnis  (S/N-Verhältnis) zu verwenden:
 
  
:<math>\rho_{\rm U} = \frac{[\ddot{o}(T_{\rm D})]^2}{ \sigma_d^2}\hspace{0.3cm}\Rightarrow \hspace{0.3cm}
+
*However,&nbsp; the horizontal distance between the blue &nbsp;$p_{\rm S}$ curve&nbsp; (marked by circles)&nbsp; and the red comparison curve is not constant.&nbsp; At &nbsp;$p_{\rm S} = 10^{-2}$&nbsp; the distance is only &nbsp;$4 \ \rm dB$.<br>
  p_{\rm U} = {\rm Q} \left( \sqrt{\rho_{\rm U}}
 
  \right) \hspace{0.05cm}</math>
 
  
Die mittlere Symbolfehlerwahrscheinlichkeit <i>p</i><sub>S</sub> kann formal über die Q&ndash;Funktion ebenfalls durch ein S/N&ndash;Verhältnis ausgedrückt werden:
 
  
:<math>\rho_d = \left[{\rm Q}^{-1} \left( p_{\rm S}
+
The right graph shows that with &nbsp;$f_{\rm G} \cdot T = 0.8$&nbsp; the distance to the comparison system is less than &nbsp;$1 \ \rm dB$.&nbsp; In the next section it is shown that with a Gaussian receiver filter the&nbsp; (normalized)&nbsp; cutoff frequency &nbsp;$f_{\rm G} \cdot T \approx 0.8$&nbsp; is the optimum.}}<br>
  \right)\right]^2 \hspace{0.05cm}.</math>
 
  
Die Grafik zeigt die beiden Größen in logarithmischer Form (10 &middot; lg <i>&rho;<sub>d</sub></i> bzw.  10 &middot; lg <i>&rho;</i><sub>U</sub>) abhängig von der normierten Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> eines gaußförmigen Empfangsfilters, wobei 10 &middot; lg <i>E</i><sub>B</sub>/<i>N</i><sub>0</sub> = 13 dB zugrunde liegt. Zum Vergleich ist als rote horizontale Linie auch das Ergebnis für den Optimalempfänger eingezeichnet. Hier gilt gemäß Kapitel 1.2:
+
== Optimization of the cutoff frequency==
 
 
:<math>\rho_d = \rho_{\rm U} = \frac{2 \cdot E_{\rm B}}{ N_0}\hspace{0.3cm}\Rightarrow \hspace{0.3cm}
 
  10 \cdot {\rm lg}\hspace{0.1cm} \rho_d = 10 \cdot {\rm lg}\hspace{0.1cm} \rho_{\rm U} \approx 16\,{\rm dB}
 
  \hspace{0.05cm}.</math>
 
 
 
Die gelb gefüllten Kreise kennzeichnen 10 &middot; lg <i>&rho;<sub>d</sub></i> und die Quadrate 10 &middot; lg <i>&rho;</i><sub>U</sub>.<br>
 
 
 
[[File:P ID1380 Dig T 3 2 S5 version1.png|SNR in Abhängigkeit der Grenzfrequenz eines Gaußtiefpasses|class=fit]]<br>
 
 
 
Die Bildbeschreibung folgt auf der nächsten Seite.<br>
 
 
 
== Optimierung der Grenzfrequenz (2)==
 
 
<br>
 
<br>
Die Grafik zeigt  die beiden soeben definierten Größen in logarithmischer Darstellung,
+
For system optimization and system comparison, it turns out to be convenient,&nbsp; instead of using the worst-case error probability &nbsp;$p_{\rm U}$&nbsp; to use the&nbsp; "worst&ndash;case signal&ndash;to&ndash;noise power ratio"&nbsp; $\text{(S/N ratio)}$:
*10 &middot; lg <i>&rho;<sub>d</sub></i> &nbsp;&#8658;&nbsp; gelb gefüllte Kreise &nbsp;&#8658;&nbsp; &bdquo;mittleres&rdquo; Detektions&ndash;SNR,<br>
+
[[File:EN_Dig_T_3_2_S5.png|right|frame|SNR as a function of the cutoff frequency of a Gaussian low-pass filter|class=fit]]
  
*10 &middot; lg <i>&rho;</i><sub>U</sub> &nbsp;&#8658;&nbsp; blau umrandete Quadrate  &nbsp;&#8658;&nbsp; ungünstigstes SNR,<br><br>
+
:$$\rho_{\rm U} = [\ddot{o}(T_{\rm D})]^2/ \sigma_d^2.$$
 +
*In the case of Gaussian perturbation, the following relationship exists:
 +
:$$p_{\rm U} = {\rm Q} \left( \sqrt{\rho_{\rm U}}
 +
  \right) \hspace{0.05cm}.$$
 +
*The error probability &nbsp;$p_{\rm S}$&nbsp; can also be formally expressed by a S/N ratio via the Q&ndash;function:
 +
:$$\rho_d = \left[{\rm Q}^{-1} \left( p_{\rm S}
 +
  \right)\right]^2 \hspace{0.05cm}.$$
  
abhängig von der Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> eines gaußförmigen Empfangsfilters für 10 &middot; lg <i>E</i><sub>B</sub>/<i>N</i><sub>0</sub> = 13 dB. Die rote horizontale Linie zeigt das Ergebnis für den Optimalempfänger..<br>
+
The diagram shows the two quantities &nbsp;$\rho_d$&nbsp; and &nbsp;$\rho_{\rm U}$&nbsp; in logarithmic form depending on the normalized cutoff frequency &nbsp;$f_{\rm G} \cdot T$&nbsp; of a Gaussian receiver filter,&nbsp; where &nbsp;$10 \cdot {\rm lg}\hspace{0.1cm} E_{\rm B}/N_0 = 13 \ \rm dB$&nbsp; is the basis.
 +
*The blue circles are for &nbsp;$10 \cdot {\rm lg}\hspace{0.1cm} \rho_d$ &nbsp; &#8658; &nbsp; "mean detection SNR",<br>
  
[[File:P ID1380 Dig T 3 2 S5 version1.png|SNR in Abhängigkeit der Grenzfrequenz eines Gaußtiefpasses|class=fit]]<br>
+
*The blue squares mark &nbsp;$10 \cdot {\rm lg}\hspace{0.1cm} \rho_{\rm U}$ &nbsp; &#8658; &nbsp; "worst-case detection SNR".
  
Man erkennt aus der Grafik:
 
*Das Optimierungskriterium <i>&rho;<sub>d</sub></i> führt näherungsweise zur optimalen Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8. Eine kleinere Grenzfrequenz hat stärkere Impulsinterferenzen zur Folge (kleinere Augenöffnung), eine größere Grenzfrequenz bewirkt einen größeren Rauscheffektivwert <i>&sigma;<sub>d</sub></i>.<br>
 
  
*Ein gaußförmiges Empfangsfilter mit <i>f</i><sub>G</sub> &middot; <i>T</i> &asymp; 0.8 führt zum Störabstand 10 &middot; lg <i>&rho;<sub>d</sub></i> &asymp; 15 dB und damit zur Fehlerwahrscheinlichkeit <i>p</i><sub>S</sub> &asymp; 10<sup>&ndash;8</sup>. Zum Vergleich: Für den optimalen Empfänger (an den Sender angepasste Impulsantwort) ergeben sich 10 &middot; lg <i>&rho;<sub>d</sub></i> &asymp; 16 dB und <i>p</i><sub>S</sub> &asymp; 10<sup>&ndash;10</sup>.<br>
+
For comparison,&nbsp; the result for the &nbsp;[[Digital_Signal_Transmission/Error_Probability_for_Baseband_Transmission#Optimal_binary_receiver_.E2.80.93_.22Matched_Filter.22_realization|"optimal binary receiver"]]&nbsp; is also plotted as a red horizontal line.&nbsp; For this optimum binary system holds:
 +
:$$\rho_d = \rho_{\rm U} = {2 \cdot E_{\rm B}}/{ N_0}\hspace{0.3cm}\Rightarrow \hspace{0.3cm}
 +
  10 \cdot {\rm lg}\hspace{0.1cm} \rho_d = 10 \cdot {\rm lg}\hspace{0.1cm} \rho_{\rm U} \approx 16\,{\rm dB}
 +
  \hspace{0.05cm}.$$
  
*Die Grafik zeigt aber auch, dass das sehr viel einfachere Optimierungskriterien <i>&rho;</i><sub>U</sub> (bzw. <i>p</i><sub>U</sub>) näherungsweise zur gleichen optimalen Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> = 0.8 führt. Für diese Grenzfrequenz erhält man 10 &middot; lg <i>&rho;</i><sub>U</sub> &asymp; 14.7 dB sowie die ungünstigste Fehlerwahrscheinlichkeit <i>p</i><sub>U</sub> &asymp; 3 &middot; 10<sup>&ndash;8</sup>.<br>
+
One can see from the plot:
 
+
#The optimization criterion &nbsp;$\rho_d$&nbsp; leads to the optimal cutoff frequency &nbsp;$f_\text{G, opt} \cdot T = 0.8$.&nbsp; A smaller cutoff frequency results in stronger intersymbol interference&nbsp; $($smaller eye opening$)$,&nbsp; a larger cutoff frequency results in a larger noise power &nbsp;$\sigma_d^2$.<br>
*Ist die Grenzfrequenz <i>f</i><sub>G</sub> &middot; <i>T</i> < 0.27, so ergibt sich für die vertikale Augenöffnung <i>ö</i>(<i>T</i><sub>D</sub>) = 0. Man spricht von einem <i>geschlossenen Auge</i>. Dies hat zur Folge, dass einige ungünstige Impulsfolgen auch dann falsch entschieden würden, wenn überhaupt kein Rauschen vorhanden wäre.<br>
+
#Such a Gaussian receiver filter with &nbsp;$f_\text{G, opt} \cdot T \approx 0.8$&nbsp; leads to the signal-to-noise ratio &nbsp;$10 \cdot {\rm lg}\hspace{0.1cm} \rho_d  \approx 15 \ \rm dB$&nbsp; and thus to the error probability &nbsp;$p_{\rm S} \approx 10^{-8}$.&nbsp; For comparison: &nbsp; With the optimal receiver&nbsp; $($impulse response matched to the transmitter$)$,&nbsp; the results are &nbsp;$10 \cdot {\rm lg}\hspace{0.1cm} \rho_d  \approx 16 \ \rm dB$&nbsp; and &nbsp;$p_{\rm S} \approx 10^{-10}$.<br>
 
+
#However,&nbsp; the graph also shows that the much simpler optimization criterion &nbsp;$ \rho_{\rm U}$&nbsp;  $($or &nbsp;$ p_{\rm U})$&nbsp; leads approximately to the same optimal cutoff frequency &nbsp;$f_\text{G, opt} \cdot T = 0.8$.&nbsp; For this cutoff frequency,&nbsp; we obtain the worst-case SNR  &nbsp;$10 \cdot {\rm lg}\hspace{0.1cm} \rho_{\rm U}  \approx 14.7 \ \rm dB$&nbsp; and the worst-case error probability &nbsp;$p_{\rm U} \approx 3 \cdot 10^{-8}$.<br>
*Weitere Untersuchungen haben gezeigt, dass das Optimierungskriterium <i>&rho;</i><sub>U</sub> auch bei kleinerem <i>E</i><sub>B</sub>/<i>N</i><sub>0</sub>  ausreichend ist. Bei einem verzerrungsfreien Kanal, d.h. <i>H</i><sub>K</sub>(<i>f</i>) = 1, ergibt sich somit die optimale Grenzfrequenz stets zu <i>f</i><sub>G</sub> &middot; <i>T</i> &asymp; 0.8, zumindest bei realitätsnaher Betrachtungsweise.<br><br>
+
#If the cutoff frequency &nbsp;$f_\text{G} \cdot T < 0.27$,&nbsp; the vertical eye opening will always be &nbsp;$\ddot{o}(T_{\rm D}) \equiv 0$.&nbsp; This is called a&nbsp; "closed eye".&nbsp; As a consequence,&nbsp; some worst-case symbol sequences would always be wrongly decided even without noise.&nbsp; A systematic error occurs.<br>
 
+
#Further investigations have shown that the optimization criterion &nbsp;$ \rho_{\rm U}$&nbsp; is sufficient even with smaller &nbsp;$E_{\rm B}/N_0$.&nbsp; Thus,&nbsp; for a distortion-free channel &nbsp; &rArr; &nbsp;  $H_{\rm K}(f) = 1$,&nbsp; the optimal cutoff frequency of the Gaussian low-pass always results in &nbsp;$f_\text{G, opt} \cdot T \approx 0.8$,&nbsp; at least in a realistic approach.<br><br>
Alle Aussagen von Kapitel 3.2 können mit folgendem Interaktionsmodul nachvollzogen werden:<br>
 
[[:File:augendiagramm.swf|Augendiagramm und Augenöffnung]]<br>
 
 
 
 
 
== Next ==
 
[[File:||class=fit]]
 
  
 +
&rArr; &nbsp; All statements of this chapter can be reproduced with the interactive HTML5/JavaScript applet&nbsp; [[Applets:Augendiagramm|"Eye diagram and eye opening"]].
  
 +
==Exercises for the chapter ==
 +
<br>
  
 +
[[Aufgaben:Exercise_3.2:_Eye_Pattern_according_to_Gaussian_Low-Pass|Exercise 3.2: Eye Pattern according to Gaussian Low-Pass]]
  
 +
[[Aufgaben:Exercise_3.2Z:_Optimum_Cut-off_Frequency_for_Gaussian_Low-pass|Exercise 3.2Z: Optimum Cutoff Frequency for Gaussian Low-pass]]
  
  
 
{{Display}}
 
{{Display}}

Latest revision as of 12:15, 10 October 2022

Gaussian receiver filter


We start from the block diagram sketched below.  The following configuration is assumed for quantitative consideration of  "intersymbol interference"

  • Rectangular NRZ basic transmission pulse  $g_s(t)$  with height  $s_0$  and duration  $T$,
  • Gaussian-shaped receiver filter  $H_{\rm G}(f)$  with cutoff frequency $f_{\rm G}$:
$$H_{\rm E}(f) = H_{\rm G}(f) = {\rm exp}\left [- \frac{\pi \cdot f^2}{(2f_{\rm G})^2} \right ] \hspace{0.2cm} \bullet\!\!-\!\!\!-\!\!\!-\!\!\circ \hspace{0.2cm}h_{\rm E}(t) = h_{\rm G}(t) = {\rm exp}\left [- \pi \cdot (2 f_{\rm G} t)^2\right ] \hspace{0.05cm},\hspace{0.5cm}\text{note: }\hspace{0.2cm}{\rm exp} [x] = {\rm e}^x.$$
  • AWGN channel   ⇒   channel frequency response  $H_{\rm K}(f) = 1 $  and  noise power-spectral density  ${\it \Phi}_n(f) = N_0/2$.


Note: 

  1. We restrict ourselves in this chapter exclusively to  redundancy-free binary bipolar transmission
  2. The ISI influence in multi-level and/or coded transmission will not be discussed until the chapter  "Intersymbol Interference for Multi-Level Transmission".


Based on the assumptions made here,  the following holds for the basic detection pulse:

$$g_d(t) = g_s(t) \star h_{\rm G}(t) = 2 f_{\rm G} \cdot s_0 \cdot \int_{t-T/2}^{t+T/2} {\rm e}^{- \pi \hspace{0.05cm}\cdot\hspace{0.05cm} (2 \hspace{0.05cm}\cdot\hspace{0.05cm} f_{\rm G}\hspace{0.05cm}\cdot\hspace{0.05cm} \tau )^2} \,{\rm d} \tau \hspace{0.05cm}.$$

The integration leads to the following equivalent results:

$$g_d(t) = s_0 \cdot \big [ {\rm Q} \left ( 2 \cdot \sqrt {2 \pi} \cdot f_{\rm G}\cdot ( t - {T}/{2})\right )- {\rm Q} \left ( 2 \cdot \sqrt {2 \pi} \cdot f_{\rm G}\cdot ( t + {T}/{2} )\right ) \big ],$$
$$g_d(t) = s_0 \cdot\big [ {\rm erfc} \left ( 2 \cdot \sqrt {\pi} \cdot f_{\rm G}\cdot ( t - {T}/{2})\right )- {\rm erfc} \left ( 2 \cdot \sqrt {\pi} \cdot f_{\rm G}\cdot ( t + {T}/{2} )\right ) \big ]\hspace{0.05cm}.$$
Block diagram for the chapter  "Error Probability with Intersymbol Interference"

Here,  two variants of the complementary Gaussian error function are used,  viz.

$${\rm Q} (x) = \frac{\rm 1}{\sqrt{\rm 2\pi}}\int_{\it x}^{+\infty}\rm e^{\it -u^{\rm 2}/\rm 2}\,d {\it u} \hspace{0.05cm},$$
$$ {\rm erfc} (\it x) = \frac{\rm 2}{\sqrt{\rm \pi}}\int_{\it x}^{+\infty}\rm e^{\it -u^{\rm 2}}\,d \it u \hspace{0.05cm}.$$

⇒   The  "Complementary Gaussian Error Functions"  provides the numerical values of the functions  ${\rm Q} (x)$  and  $0.5 \cdot {\rm erfc} (x)$.

The noise power at the output of the Gaussian receiver filter  $H_{\rm G}(f)$  is

$$\sigma_d^2 = \frac{N_0}{2} \cdot \int_{-\infty}^{+\infty} |H_{\rm G}(f)|^2 \,{\rm d} f = \frac{N_0\cdot f_{\rm G}}{\sqrt{2}}\hspace{0.05cm}.$$

$\text{From these equations one can already see:}$ 

  1. The smaller the cutoff frequency  $f_{\rm G}$  of the Gaussian low-pass filter,  the smaller the noise rms value  $\sigma_d$  and consequently the better the noise performance.
  2. However,  a small cutoff frequency leads to a strong deviation of the basic detection pulse  $g_d(t)$  from the rectangular form and thus to intersymbol interference.


$\text{Example 1:}$  The left graph shows the basic detection pulse  $g_d(t)$  at the output of a Gaussian low-pass filter  $H_{\rm G}(f)$  with the cutoff frequency  $f_{\rm G}$  when an NRZ rectangular pulse (blue curve) is applied at the input.

Basic detection pulse and noise power-spectral density  $\rm (PSD)$  with Gaussian receiver filter

One can see from this plot:

  • The Gaussian low-pass filter  $H_{\rm G}(f)$  causes the detection pulse  $g_d(t)$  to be reduced and broadened compared to the transmitted pulse  $g_s(t)$  ⇒   "'time dispersion".
  • The pulse deformation is the stronger,  the smaller the cutoff frequency  $f_{\rm G}$  is.  For example,  with  $f_{\rm G} \cdot T = 0.4$  (red curve)  the pulse maximum is already reduced to  $\approx 68\%$. 
  • In the limiting case  $f_{\rm G} \to \infty$  the Gaussian low-pass has no effect   ⇒   $g_d(t) = g_s(t)$.  However,  in this case,  there is no noise limitation at all,  as can be seen from the right figure.


$\text{Example 2:}$  The same preconditions apply as for the last example.  The graph shows the detection signal  $d(t)$  after the Gaussian low-pass  $($before the decision$)$  for two different cutoff frequencies,  namely  $f_{\rm G} \cdot T = 0.8$  and  $f_{\rm G} \cdot T = 0.4$.  We want to analyze these images in terms of intersymbol interference.

Detection signal with Gaussian receiver filter

In both diagrams are shown:

  • the component  $d_{\rm S}(\nu \cdot T)$  of the detection signal without considering the noise  $($blue circles at the detection times$)$,
  • the total detection signal  $d(t)$  including the noise component (yellow curve),
  • the transmitted signal  $s(t)$  as reference signal (green dotted in the upper graph; equally valid for the lower graph).

By comparing these images, the following statements can be verified in terms of Intersymbol Interference  $\rm (ISI)$:

  • With the cutoff frequency  $f_{\rm G} \cdot T = 0.8$  (upper graph),  only minor ISI result at the detection times  $($at multiples of  $T)$.  Due to the Gaussian low-pass here primarily the corners of the transmitted signal  $s(t)$  are rounded.
  • In contrast,  in the lower image  $(f_{\rm G} \cdot T = 0.4)$  the ISI effects are clearly visible.  At the detection times  $(\nu \cdot T)$,  the  $($blue$)$  signal component  $d_{\rm S}(\nu \cdot T)$  of the detection signal can assume six different values  $($compare grid lines drawn$)$.
  • The noise component  $d_{\rm N}(t)$ – recognizable as the difference between yellow curve and blue circles – is on average larger with $f_{\rm G} \cdot T = 0.8$  than with $f_{\rm G} \cdot T = 0.4$.
  • This result can be explained by the right graph of  $\text{Example 1}$,  which shows the PSD of the noise component  $d_{\rm N}(t)$: 
$${\it \Phi}_{d{\rm N} }(f) = {N_0}/{2} \cdot \vert H_{\rm G}(f) \vert^2 = {N_0}/{2} \cdot {\rm exp}\left [- \frac{2\pi f^2}{(2f_{\rm G})^2} \right ] .$$
  • The integral over  ${\it \Phi}_{d{\rm N} }(f)$  – i.e. the noise power  $\sigma_d^2$  – is twice as large for  $f_{\rm G} \cdot T = 0.8$  (purple curve) than with  $f_{\rm G} \cdot T = 0.4$  (red curve).


Definition and statements of the eye diagram


The above mentioned facts can also be explained by the eye diagram.

$\text{Definition:}$  The  eye diagram  (or  "eye pattern")  is the sum of all superimposed sections of the detection signal  $d(t)$,  whose duration is an integer multiple of the symbol duration  $T$.  This diagram has a certain resemblance to an eye, which led to its naming.


$\text{Example 3:}$  We assume a redundancy-free binary bipolar NRZ rectangular signal  $s(t)$  and the Gaussian low-pass filter with cutoff frequency  $f_{\rm G} \cdot T = 0.4$. 

On the left:  Eye diagram with noise  ⇒   signal  $d(t)=d_{\rm S}(t) +d_{\rm N}(t)$,
on the right:  Eye diagram without noise  ⇒   signal  $d_{\rm S}(t)$

In the graphic shown are the eye diagrams after the Gaussian low-pass,

  • left inclusive the noise component   ⇒   signal  $d(t)=d_{\rm S}(t) +d_{\rm N}(t)$,
  • on the right without taking noise into account   ⇒   signal  $d_{\rm S}(t)$.


This representation allows important statements about the quality of a digital transmission system:

  • Only the eye diagram of the signal  $d(t)$  can be displayed metrologically on an oscilloscope,  which is triggered with the clock signal.  From this eye diagram  $($left graph$)$,  for example,  the noise rms value  $\sigma_d$  $($⇒   noise power  $\sigma_d^2)$  can be read – or rather:  estimated.
  • The eye diagram without noise  (right graph)  refers to the signal component  $d_{\rm S}(t)$  of the detection signal and can only be determined by means of a computer simulation.  For an implemented system,  this eye diagram cannot be displayed,  since the noise component  $d_{\rm N}(t)$  cannot be eliminated.
  • In both diagrams of this example,  $2^{11}=2048$  eye lines were drawn in each case.  In the right graph,  however,  only  $2^5 = 32$  eye lines are distinguishable because the present detection pulse  $g_d(t)$  is limited to the time range  $\vert t\vert \le 2T$ 
    $($see  graph in Example 1  with  $f_{\rm G} \cdot T = 0.4$,  red curve$)$.
  • The inner eye lines determine the  vertical eye opening  $\ddot{o}(T_{\rm D})$.  The smaller this is,  the greater is the influence of intersymbol interference.  For a  $($ISI-free$)$  Nyquist system the vertical eye opening is maximum.  Normalized to the transmitted amplitude,  $\ddot{o}(T_{\rm D})/s_0 = 2$  is then valid.
  • With symmetrical basic detection pulse,  the detection time  $T_{\rm D} = 0$  is optimal.  With a different value  $($for example  $T_{\rm D} = -T/10) $,   $\ddot{o}(T_{\rm D})$  would be somewhat smaller and thus the error probability would be significantly larger.  This case is indicated by the purple–dashed vertical line in the right graph.

Mean error probability


As with the previous graphs in this chapter,  we assume the following:

Eye diagram and discrete PDF of the signal component  $d_{\rm S}(t)$  from  $d(t)$
  • NRZ rectangles with amplitude  $s_0$,  AWGN noise with power-spectral density  $N_0$,  where
$$10 \cdot {\rm lg}\hspace{0.1cm} \frac{s_0^2 \cdot T}{N_0}\approx 13\,{\rm dB}\hspace{0.3cm} \Rightarrow \hspace{0.3cm} \frac{N_0}{s_0^2 \cdot T} = 0.05\hspace{0.05cm}.$$
  • Gaussian receiver filter with cutoff frequency  $f_{\rm G} \cdot T = 0.4$:
$$\sigma_d^2 = \frac{(N_0 /T)\cdot (f_{\rm G}\cdot T)}{\sqrt{2}}= \frac{0.05 \cdot s_0^2\cdot0.4}{\sqrt{2}}$$
$$ \Rightarrow \hspace{0.3cm} \sigma_d = \sqrt{0.0141}\cdot s_0 \approx 0.119 \cdot s_0 \hspace{0.05cm}.$$
  • Let  $g_d(\nu \cdot T) \approx 0$  be valid for  $|\nu| \ge 2$.  The other basic detection pulse values are given as follows:
$$g_0 = g_d(t=0) \approx 0.68 \cdot s_0,$$
$$g_1 = g_d(t=T) \approx 0.16 \cdot s_0,$$
$$g_{-1} = g_d(t=-T) \approx 0.16 \cdot s_0\hspace{0.05cm}.$$

Let us now analyze the possible values for the signal component  $d_{\rm S}(t)$  at the detection times:

  • Of the total  $32$  eye lines,  four lines intersect the ordinate  $(t = 0)$  at  $g_0 + 2 \cdot g_1 = s_0$.  These lines belong to the amplitude coefficients  "$\text{...}\hspace{0.05cm} +\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} +\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$".    Here,  the  "middle"  coefficient  $a_{\nu = 0}$  is highlighted in italics.
  • The four eye lines,  each representing the coefficients  "$\text{...}\hspace{0.05cm} -\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} -\hspace{-0.05cm}1,\hspace{0.05cm} \text{...}$"  result in the signal value  $d_{\rm S}(T_{\rm D} = 0) =g_0 - 2 \cdot g_1 = 0.36 \cdot s_0$.
  • In contrast,  the signal value  $d_{\rm S}(T_{\rm D} = 0) =g_0 = 0.68 \cdot s_0$  occurs twice as often.  This goes back either to the coefficients  "$\text{...}\hspace{0.05cm} +\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} -\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$"  or to  "$\text{...}\hspace{0.05cm} -\hspace{-0.1cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} +\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$". 
  • For the  $16$  eye lines which intersect the ordinate  $T_{\rm D} = 0$  below the decision threshold  $E = 0$,  exactly mirror-image relations result.

The possible values  $d_{\rm S}(T_{\rm D})$  and their occurrence probabilities can be found in the above graph on the left side in the  (discrete)   probability density function  $\rm (PDF)$  of the noise-free detection signal samples:

$$f_{d{\rm S}}(d_{\rm S}) = {1}/{8} \cdot \delta (d_{\rm S} - s_0)+ {1}/{4} \cdot \delta (d_{\rm S} - 0.68 \cdot s_0)+ {1}/{8} \cdot \delta (d_{\rm S} - 0.36 \cdot s_0)+ $$

$$\hspace{2.15cm} + \hspace{0.2cm} {1}/{8} \cdot \delta (d_{\rm S} + s_0)+{1}/{4} \cdot \delta (d_{\rm S} + 0.68 \cdot s_0)+{1}/{8} \cdot \delta (d_{\rm S} + 0.36 \cdot s_0)\hspace{0.05cm}.$$

Thus,  the  (average)  symbol error probability of the of the ISI-afflicted system can be given.  Taking advantage of the symmetry,  one obtains with  $\sigma_d/s_0 = 0.119$:

$$p_{\rm S} = {1}/{4} \cdot {\rm Q} \left( \frac{s_0}{ \sigma_d} \right)+ {1}/{2} \cdot {\rm Q} \left( \frac{0.68 \cdot s_0}{ \sigma_d} \right)+{1}/{4} \cdot {\rm Q} \left( \frac{0.36 \cdot s_0}{ \sigma_d} \right)$$
$$\Rightarrow \hspace{0.3cm}p_{\rm S} \approx {1}/{4} \cdot {\rm Q}(8.40) +{1}/{2} \cdot {\rm Q}(5.71)+ {1}/{4} \cdot {\rm Q}(3.02)\approx {1}/{4} \cdot 2.20 \cdot 10^{-17}+ {1}/{2} \cdot 1.65 \cdot 10^{-9}+ {1}/{4} \cdot 1.26 \cdot 10^{-3} \approx 3.14 \cdot 10^{-4} \hspace{0.05cm}.$$

Note:   For redundancy-free binary bipolar transmission,  the bit error probability  $p_{\rm B}$  is identical to the symbol error probability  $p_{\rm S}$.

$\text{On the basis of this numerical example one recognizes:}$ 

  1. In the presence of intersymbol interference,  the  (average)  symbol error probability  $p_{\rm S}$  is essentially determined by the inner eye lines.
  2. The computational cost of determining  $p_{\rm S}$  can become very large,  especially if the ISI comes from very many basic detection pulse values  $g_\nu$. 


$\text{Example 4:}$ 

  • If the pulse values  $g_{-5}, \text{...} \ , g_{+5}$  are different from zero and  $E \ne 0$, an averaging over  $2^{11} = 2048$  eye lines is necessary to determine the error probability  $p_{\rm S}$.
  • If,  on the other hand,  only the pulse values  $g_{-1}, \ g_0, \ g_{+1}$  are different from zero and,  in addition,  the symmetry with respect to the threshold  $E = 0$  is taken into account,  the effort is reduced to averaging over four terms.
  • If,  in addition,  the symmetry  $g_{-1} = g_{+1}$  applies as with the above numerical values,  then the symmetry with respect to  $T_{\rm D}$  can also be exploited and averaging over three terms is sufficient.


Worst-case error probability


In the past,  a variety of approximations for the average error probability have been given, among others:

$\text{Definition:}$  As a very simple approximation for the actual error probability  $p_{\rm S}$,  the  worst-case error probability  (German:  "ungünstigste Fehlerwahrscheinlichkeit"   ⇒   subscript:  "U")  is often used:

"Mean symbol error probability"  $p_{\rm S}$  vs.  "worst-case symbol error probability"  $p_{\rm U}$
$$p_{\rm U} = {\rm Q} \left( \frac{\ddot{o}(T_{\rm D})/2}{ \sigma_d} \right) \hspace{0.05cm}.$$

For their calculation,  the  "worst-case symbol sequences"  are always assumed.  This means:

  • The actual probability density function  $\rm (PDF)$  of the samples $d_{\rm S}(T_{\rm D})$  (left graph:  six red Dirac delta functions)  is replaced by a simplified PDF with only the inner Dirac delta functions  (right graph:  two green Diracs).
  • For the half vertical eye opening,  with the basic detection pulse values  $g_\nu = g_d( T_{\rm D}+ \nu \cdot T)$  generally holds:
$$\ddot{o}(T_{\rm D})/{ 2}= g_0 - \sum_{\nu = 1}^{n} \vert g_{\nu} \vert- \sum_{\nu = 1}^{v} \vert g_{-\nu} \vert \hspace{0.05cm}.$$


This equation can be interpreted as follows:

  • $g_0 = g_d( T_{\rm D})$  is the so-called  "main value"  of the basic detection pulse.  For Nyquist systems  $\ddot{o}(T_{\rm D})/{ 2}= g_0$  is always valid.  In the following  (mostly)   $T_{\rm D}= 0$  is set.
  • The first sum describes the ISI influence of the  $n$  "trailers"  $($German:  "Nachläufer"  ⇒   variable  $n)$  of preceding pulses  $($sometimes we use the term  "postcursor"$)$.  Tacitly assumed is  $g_\nu = 0$  for  $\nu \gt n$. 
  • The second sum considers the influence of the  $v$  "precursors"  $($German:  "Vorläufer"  ⇒   variable  $v)$  of following pulses under the condition  $g_{-\nu} = 0$  for  $\nu \gt v$.
  • If all precursors and trailers are positive,  the two worst-case symbol sequences are  "$\text{...}\hspace{0.05cm} -\hspace{-0.1cm}1,\hspace{0.05cm} -\hspace{-0.05cm}1,\hspace{0.05cm} {\it +\hspace{-0.05cm}1},\hspace{0.05cm} -\hspace{-0.05cm}1,\hspace{0.05cm} -\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$"  and  "$\text{...}\hspace{0.05cm} +\hspace{-0.1cm}1,\hspace{0.05cm} +\hspace{-0.05cm}1,\hspace{0.05cm} {\it -\hspace{-0.05cm}1},\hspace{0.05cm} +\hspace{-0.05cm}1,\hspace{0.05cm} +\hspace{-0.05cm}1\hspace{0.05cm} \text{...}$"  (coefficient  $a_{\nu = 0}$  is in italics in each case).  These specifications apply,  for example,  to the Gaussian receiver filter considered here.
  • If some basic detection pulse values  $g_{\nu\ne 0}$  are negative,  this is taken into account in the above equation by the magnitude formation.  This results in other "worst–case" sequences than those just mentioned.


$\text{Example 5:}$  The graph shows the error probabilities of the AWGN channel as a function of the (logarithmized) quotient  $E_{\rm B}/N_0$,  namely

  • the average error probability  $p_{\rm S}$  with Gaussian receiver filter  (blue circles),
  • the worst-case error probability  $p_{\rm U}$  with Gaussian receiver filter  (blue rectangles),
  • the smallest possible error probability according to the section "Optimal binary receiver"  (red curve).

Here,  the energy per bit is equal to  $E_{\rm B} = s_0^2 \cdot T$  (redundancy-free binary bipolar transmission,  NRZ rectangular transmitted pulses).

The left graph is for the  (normalized)  cutoff frequency  $f_{\rm G} \cdot T = 0.4$,  the right one for a broader band receiver filter with  $f_{\rm G} \cdot T = 0.8$.

Mean error probability  $p_{\rm S}$  and  worst-case error probability  $p_{\rm U}$  as a function of  $E_{\rm B}/N_0$

The results can be interpreted as follows:

  • $p_{\rm U}$  is always an upper bound for the actual symbol error probability  $p_{\rm S}$.  The smaller the influence of the intersymbol interference  (large cutoff frequency),  the closer  $p_{\rm S}$  and  $p_{\rm U}$  are to each other.  For the optimal receiver  $p_{\rm S} = p_{\rm U}.$
  • For a Gaussian receiver filter with  $f_{\rm G} \cdot T \ge 0.3$,  the ISI are caused by the neighboring pulses alone  $(g_2 = g_3 = \text{...} \approx 0)$,  so that a lower bound can also be given:  ${p_{\rm U} }/{ 4} \le p_{\rm S} \le p_{\rm U} \hspace{0.05cm}.$
  • The strong ISI of a Gaussian receiver filter with  $f_{\rm G} \cdot T = 0.4$  leads to the fact that compared to the optimal receiver a  $6 \ \rm dB$ larger $E_{\rm B}/N_0$  must be applied (four times the power), so that the error probability does not exceed the value  $10^{-8}$. 
  • However,  the horizontal distance between the blue  $p_{\rm S}$ curve  (marked by circles)  and the red comparison curve is not constant.  At  $p_{\rm S} = 10^{-2}$  the distance is only  $4 \ \rm dB$.


The right graph shows that with  $f_{\rm G} \cdot T = 0.8$  the distance to the comparison system is less than  $1 \ \rm dB$.  In the next section it is shown that with a Gaussian receiver filter the  (normalized)  cutoff frequency  $f_{\rm G} \cdot T \approx 0.8$  is the optimum.


Optimization of the cutoff frequency


For system optimization and system comparison, it turns out to be convenient,  instead of using the worst-case error probability  $p_{\rm U}$  to use the  "worst–case signal–to–noise power ratio"  $\text{(S/N ratio)}$:

SNR as a function of the cutoff frequency of a Gaussian low-pass filter
$$\rho_{\rm U} = [\ddot{o}(T_{\rm D})]^2/ \sigma_d^2.$$
  • In the case of Gaussian perturbation, the following relationship exists:
$$p_{\rm U} = {\rm Q} \left( \sqrt{\rho_{\rm U}} \right) \hspace{0.05cm}.$$
  • The error probability  $p_{\rm S}$  can also be formally expressed by a S/N ratio via the Q–function:
$$\rho_d = \left[{\rm Q}^{-1} \left( p_{\rm S} \right)\right]^2 \hspace{0.05cm}.$$

The diagram shows the two quantities  $\rho_d$  and  $\rho_{\rm U}$  in logarithmic form depending on the normalized cutoff frequency  $f_{\rm G} \cdot T$  of a Gaussian receiver filter,  where  $10 \cdot {\rm lg}\hspace{0.1cm} E_{\rm B}/N_0 = 13 \ \rm dB$  is the basis.

  • The blue circles are for  $10 \cdot {\rm lg}\hspace{0.1cm} \rho_d$   ⇒   "mean detection SNR",
  • The blue squares mark  $10 \cdot {\rm lg}\hspace{0.1cm} \rho_{\rm U}$   ⇒   "worst-case detection SNR".


For comparison,  the result for the  "optimal binary receiver"  is also plotted as a red horizontal line.  For this optimum binary system holds:

$$\rho_d = \rho_{\rm U} = {2 \cdot E_{\rm B}}/{ N_0}\hspace{0.3cm}\Rightarrow \hspace{0.3cm} 10 \cdot {\rm lg}\hspace{0.1cm} \rho_d = 10 \cdot {\rm lg}\hspace{0.1cm} \rho_{\rm U} \approx 16\,{\rm dB} \hspace{0.05cm}.$$

One can see from the plot:

  1. The optimization criterion  $\rho_d$  leads to the optimal cutoff frequency  $f_\text{G, opt} \cdot T = 0.8$.  A smaller cutoff frequency results in stronger intersymbol interference  $($smaller eye opening$)$,  a larger cutoff frequency results in a larger noise power  $\sigma_d^2$.
  2. Such a Gaussian receiver filter with  $f_\text{G, opt} \cdot T \approx 0.8$  leads to the signal-to-noise ratio  $10 \cdot {\rm lg}\hspace{0.1cm} \rho_d \approx 15 \ \rm dB$  and thus to the error probability  $p_{\rm S} \approx 10^{-8}$.  For comparison:   With the optimal receiver  $($impulse response matched to the transmitter$)$,  the results are  $10 \cdot {\rm lg}\hspace{0.1cm} \rho_d \approx 16 \ \rm dB$  and  $p_{\rm S} \approx 10^{-10}$.
  3. However,  the graph also shows that the much simpler optimization criterion  $ \rho_{\rm U}$  $($or  $ p_{\rm U})$  leads approximately to the same optimal cutoff frequency  $f_\text{G, opt} \cdot T = 0.8$.  For this cutoff frequency,  we obtain the worst-case SNR  $10 \cdot {\rm lg}\hspace{0.1cm} \rho_{\rm U} \approx 14.7 \ \rm dB$  and the worst-case error probability  $p_{\rm U} \approx 3 \cdot 10^{-8}$.
  4. If the cutoff frequency  $f_\text{G} \cdot T < 0.27$,  the vertical eye opening will always be  $\ddot{o}(T_{\rm D}) \equiv 0$.  This is called a  "closed eye".  As a consequence,  some worst-case symbol sequences would always be wrongly decided even without noise.  A systematic error occurs.
  5. Further investigations have shown that the optimization criterion  $ \rho_{\rm U}$  is sufficient even with smaller  $E_{\rm B}/N_0$.  Thus,  for a distortion-free channel   ⇒   $H_{\rm K}(f) = 1$,  the optimal cutoff frequency of the Gaussian low-pass always results in  $f_\text{G, opt} \cdot T \approx 0.8$,  at least in a realistic approach.

⇒   All statements of this chapter can be reproduced with the interactive HTML5/JavaScript applet  "Eye diagram and eye opening".

Exercises for the chapter


Exercise 3.2: Eye Pattern according to Gaussian Low-Pass

Exercise 3.2Z: Optimum Cutoff Frequency for Gaussian Low-pass