Difference between revisions of "Linear and Time Invariant Systems/Inverse Laplace Transform"

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{{Header
 
{{Header
|Untermenü=Beschreibung kausaler realisierbarer Systeme
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|Untermenü=Description of Causal Realizable Systems
|Vorherige Seite=Laplace–Transformation und p–Übertragungsfunktion
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|Vorherige Seite=Laplace_Transform_and_p-Transfer_Function
|Nächste Seite=Einige Ergebnisse der Leitungstheorie
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|Nächste Seite=Some_Results_from_Transmission_Line_Theory
 
}}
 
}}
==Ersatzschaltbild eines kurzen Leitungsabschnitts (1)==
+
==Problem formulation and prerequisites==
Zur Herleitung der Leitungsgleichungen wird zunächst ein sehr kurzer Leitungsabschnitt der Länge $dx$ betrachtet, so dass sich die Werte für Spannung und Strom am Leitungsanfang $(U$ bzw. $I$ bei $x)$ und am Leitungsende $(U + dU$ sowie $I + dI$ bei $x + dx)$ nur geringfügig unterscheiden. Die Grafik zeigt das zugrundeliegende Modell.
+
<br>
 +
{{BlaueBox|TEXT=
 +
$\text{Task:}$&nbsp; This chapter deals with the following problem:
 +
*The&nbsp; $p$–spectral function&nbsp; $Y_{\rm L}(p)$&nbsp;  is given in&nbsp; &raquo;pole-zero notation&laquo;.
 +
*The&nbsp; &raquo;'''inverse Laplace transform'''&laquo;, i.e. the associated time function&nbsp; $y(t)$&nbsp; is searched-for,&nbsp; where the following notation should hold:
 +
:$$y(t) = {\rm L}^{-1}\{Y_{\rm L}(p)\}\hspace{0.05cm} , \hspace{0.3cm}{\rm briefly}\hspace{0.3cm}
 +
y(t) \quad \circ\!\!-\!\!\!-^{\hspace{-0.25cm}\rm L}\!\!\!-\!\!\bullet\quad Y_{\rm L}(p)\hspace{0.05cm} .$$}}
  
[[File:P_ID1792__LZI_T_4_1_S1_neu.png | Ersatzschaltbild eines kurzen Leitungsabschnitts]]
+
[[File:EN_LZI_T_3_3_S1.png |right|frame|Prerequisites for the chapter "Inverse Laplace Transform"]]
  
  
Anders ausgedrückt: Die Leitungslänge $dx$ sei sehr klein gegenüber der Wellenlänge der sich entlang der Leitung ausbreitenden elektromagnetischen Welle, die sich ergibt, da
+
The graph summarizes the prerequisites for this task.
*mit dem Strom ein magnetisches Feld verbunden ist,
 
*die Spannung zwischen den Leitern ein elektrisches Feld bewirkt.  
 
  
 +
*$H_{\rm L}(p)$&nbsp; describes the transfer function of the causal system and &nbsp;$Y_{\rm L}(p)$&nbsp; specifies the Laplace transform of the output signal &nbsp;$y(t)$&nbsp; considering the input signal &nbsp;$x(t)$&nbsp;. &nbsp;$Y_{\rm L}(p)$&nbsp; is characterized by &nbsp;$N$&nbsp; poles,&nbsp; by &nbsp;$Z ≤ N$&nbsp; zeros and by the constant &nbsp;$K.$
 +
 +
*Poles and zeros exhibit the properties mentioned in the&nbsp; [[Linear_and_Time_Invariant_Systems/Laplace_Transform_and_p-Transfer_Function#Properties_of_poles_and_zeros|&raquo;last chapter&laquo;]]:&nbsp; Poles are only allowed in the left &nbsp;$p$–half plane or on the imaginary axis;&nbsp; zeros are also allowed in the right &nbsp;$p$–half plane.
 +
 +
*All&nbsp; &raquo;singularities&laquo;&nbsp; – this is the generic term for poles and zeros – are either real or exist as pairs of conjugate-complex singularities.&nbsp; Multiple poles and zeros are also allowed.
 +
 +
*With the input &nbsp;$x(t) = δ(t)$ &nbsp; &rArr; &nbsp;  $X_{\rm L}(p) = 1$  &nbsp; &rArr; &nbsp;  $Y_{\rm L}(p) = H_{\rm L}(p)$, the output signal &nbsp;$y(t)$&nbsp; then describes the [[Linear_and_Time_Invariant_Systems/System_Description_in_Time_Domain#Impulse_response|&raquo;impulse response&laquo;]]  &nbsp;$h(t)$&nbsp; of the transmission system.&nbsp; For this purpose,&nbsp; only the singularities drawn in green in the graph may be used for computation.
  
Alle infinitesimalen „Bauelemente” im oben skizzierten Ersatzschaltbild sind bei homogenen Leitungen ortsunabhängig:
+
*A unit jump  function &nbsp;$x(t) = γ(t)$ &nbsp; &rArr; &nbsp;  $ X_{\rm L} = 1/p$&nbsp; at the input causes the output signal &nbsp;$y(t)$&nbsp; to be equal to the &nbsp;[[Linear_and_Time_Invariant_Systems/System_Description_in_Time_Domain#Step_response|&raquo;step response&laquo;]] &nbsp; $σ(t)$ of $H_{\rm L}(p)$&nbsp;.&nbsp; In addition to the singularities of &nbsp;$H_{\rm L}(p)$,&nbsp; the pole&nbsp; $($shown in red in the graph$)$&nbsp; at &nbsp;$p = 0$&nbsp; must now also be taken into account for computation.
*Die Induktivität des betrachteten Leitungsabschnitts beträgt $L' · dx$, wobei man die auf die Länge $dx$ bezogene Größe als '''Induktivitätsbelag''' bezeichnet.  
+
*Ebenso ist der '''Kapazitätsbelag''' $C'$ eine infinitesimal kleine Größe, der ebenso wie $L'$ nur relativ wenig von der Frequenz abhängt.  
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*Possible as input &nbsp;$x(t)$&nbsp; are only signals for which &nbsp;$X_{ \rm L}(p)$&nbsp; can be expressed in pole-zero notation&nbsp;  (see the &nbsp;[[Linear_and_Time_Invariant_Systems/Laplace_Transform_and_p-Transfer_Function#Some_important_Laplace_correspondences|$\text{table}$]]&nbsp; in the chapter &raquo;Laplace Transform and $p$–Transfer Function&raquo;$)$,&nbsp; for example a cosine or sine signal switched on at time &nbsp;$t = 0$&nbsp;.
*Der '''Ableitungsbelag''' $G'$ berücksichtigt die Verluste des Dielektrikums zwischen den Drähten. Er nimmt etwa proportional mit der Frequenz zu.
+
*Den weitaus größten Einfluss auf die Signalübertragung hat der Widerstandsbelag $R'$, der für hohe Frequenzen aufgrund des dann dominanten Skineffekts  nahezu proportional mit der Wurzel der Frequenz ansteigt.
+
*So,&nbsp; a rectangular signal &nbsp;$x(t)\ \  ⇒ \ \ X_{\rm L}(p) = (1 - {\rm e}^{\hspace{0.05cm}p\hspace{0.05cm}\cdot \hspace{0.05cm} T})/p$&nbsp; is not possible in the approach described here.&nbsp; However, the rectangular response &nbsp;$y(t)$&nbsp; can be computed indirectly as the difference of two step responses.
  
==Ersatzschaltbild eines kurzen Leitungsabschnitts (2)==
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==Some results of function theory==
Aus den Maschen– und Knotengleichungen des Leitungsabschnitts ergeben sich mit $ω = 2πf$ die beiden Differenzengleichungen
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<br>
$$ \begin{align*} U  & =  I \cdot (R' + {\rm j}  \cdot \omega  L') \cdot {\rm d}x + (U + {\rm d}U)\hspace{0.05cm},\\ I  & =  (U + {\rm d}U) \cdot (G' + {\rm j}  \cdot \omega  C') \cdot {\rm d}x + (I + {\rm d}I)\hspace{0.05cm} \end{align*}$$.
+
In contrast to the&nbsp; [[Signal_Representation/Fourier_Transform_and_Its_Inverse#The_first_Fourier_integral|&raquo;Fourier integrals&laquo;]],&nbsp; which differ only slightly in the two directions of transformation,&nbsp; for&nbsp; &raquo;Laplace&laquo;&nbsp; the computation of &nbsp;$y(t)$&nbsp; from &nbsp;$Y_{\rm L}(p)$ – that is the inverse transformation – is
Für einen sehr kurzen Leitungsabschnitt (infinitesimal kleines $dx$) und bei Vernachlässigung der kleinen Größen zweiter Ordnung (zum Beispiel $dU · dx$) kann man nun zwei Differentialquotienten bilden, deren gemeinsame Betrachtung zu einer linearen Differentialgleichung zweiter Ordnung führt:
+
*much more difficult than computing &nbsp;$Y_{\rm L}(p)$&nbsp; from &nbsp;$y(t)$,
$$\frac{ {\rm  d}U}{ {\rm  d}x}  =  - (R' + {\rm j}  \cdot \omega  L')  \cdot I,\hspace{0.5cm} \frac{ {\rm  d}I}{ {\rm  d}x}  =  - (G' + {\rm j}  \cdot \omega  C')
+
   
\cdot U$$
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*unresolvable or solvable only very laboriously by elementary means.
$$\Rightarrow \hspace{0.3cm}\frac{{\rm d}^2U}{{\rm  d}x^2}  =  (R' + {\rm j}  \cdot \omega  L') \cdot  (G' + {\rm j}  \cdot \omega  C')
 
  \cdot U\hspace{0.05cm}.$$
 
Die Lösung dieser Differentialgleichung lautet:
 
$$U(x)  =  U_{\rightarrow}(x=0) \cdot  {\rm e}^{-\hspace{0.02cm}\gamma \hspace{0.03cm} \cdot \hspace{0.05cm}x}  + U_{\leftarrow}(x=0) \cdot  {\rm e}^{\gamma \hspace{0.03cm} \cdot \hspace{0.05cm}x}  \hspace{0.05cm}.$$
 
  
  
Der Spannungsverlauf hängt außer vom Ort $x$ auch von der Frequenz $f$ ab, was hier nicht explizit vermerkt ist. Formelmäßig erfasst wird diese Frequenzabhängigkeit durch das Übertragungsmaß
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{{BlaueBox|TEXT= 
$$\gamma(f) =  \sqrt{(R' + {\rm j}   \cdot 2\pi f \cdot L')  \cdot  (G' + {\rm j} \cdot 2\pi f \cdot  C')} = \alpha (f) + {\rm j}   \cdot \beta (f)\hspace{0.05cm}.$$
+
$\text{Definition:}$&nbsp;
 +
In general, the following holds for the&nbsp; &raquo;'''inverse Laplace transform'''&laquo;:
 +
:$$y(t) = {\rm L}^{-1}\{Y_{\rm L}(p)\}= \lim_{\beta \hspace{0.05cm}\rightarrow \hspace{0.05cm}\infty} \hspace{0.15cm} \frac{1}{ {\rm j} \cdot 2 \pi}\cdot     \int_{ \alpha - {\rm j} \hspace{0.05cm}\cdot \hspace{0.05cm}2 \pi \beta } ^{\alpha+{\rm j} \hspace{0.05cm}\cdot \hspace{0.05cm}2 \pi \beta}  Y_{\rm L}(p) \hspace{0.05cm}\cdot \hspace{0.05cm} {\rm e}^{\hspace{0.05cm}p \hspace{0.05cm}\cdot \hspace{0.05cm} t}\hspace{0.1cm}{\rm
 +
d}p \hspace{0.05cm} .$$
 +
#The integration is parallel to the imaginary axis.
 +
#The real part &nbsp;$α$&nbsp; is to be chosen such that all poles are located to the left of the integration path.}}
  
  
Die beiden letzten Gleichungen beschreiben gemeinsam den Spannungsverlauf entlang der Leitung, der sich aus der Überlagerung einer in positiver $x$–Richtung laufenden Welle $U_→(x)$ und der Welle $U_←(x)$ in Gegenrichtung zusammensetzt.  
+
The left graph illustrates this line integral along the red dotted vertical &nbsp;${\rm Re}\{p\}= α$.&nbsp; This integral is solvable using &nbsp;[https://en.wikipedia.org/wiki/Jordan%27s_lemma &raquo;Jordan's lemma of complex analysis&laquo;].&nbsp; In this tutorial only a very short and simple summary of the approach is depicted:
 +
[[File:EN_LZI_T_3_3_S2.png |right|frame|Line integral together with left and right circular integral]]
 +
 +
#The line integral can be divided into two circular integrals so that all poles are located in the left circular integral while the right circular integral may only contain zeros.
 +
#According to the theory of functions, the right circular integral yields the time function &nbsp;$y(t)$&nbsp; for negative times.&nbsp;
 +
#Due to causality, &nbsp;$y(t < 0)$&nbsp; must be identical to zero,&nbsp; but according to the fundamentals of function theorem this is only true if there are no poles in the right &nbsp;$p$–half-plane.
 +
#In contrast,&nbsp; the integral over the left semicircle yields the time function for &nbsp;$t ≥ 0$.&nbsp;
 +
#This encloses all poles and can be computed using the&nbsp; &raquo;'''residue theorem'''&laquo;&nbsp; in a&nbsp; $($relatively$)$&nbsp; simple way,&nbsp; as it will be shown in the next sections.
 +
<br clear=all>
 +
==Formulation of the residue theorem==
 +
<br>
 +
It is further assumed that the transfer function &nbsp;$Y_{\rm L}(p)$&nbsp; can be expressed in pole-zero notation  by
 +
*the constant factor&nbsp; $K$,
 +
*the &nbsp;$Z$&nbsp; &raquo;zeros&laquo; &nbsp;$p_{{\rm o}i}$&nbsp; $(i = 1$, ... , $Z)$&nbsp; and
 +
*the &nbsp;$N$&nbsp; &raquo;poles&laquo; &nbsp;$p_{{\rm x}i}$&nbsp; $(i = 1$, ... , $N$).  
  
Der Realteil $α(f)$ des komplexen Übertragungsmaßes $γ(f)$ dämpft die sich ausbreitende Welle und wird daher Dämpfungsmaß genannt. Diese stets gerade Funktion  $⇒  α(–f) = α(f)$ ergibt sich aus obiger $γ(f)$–Gleichung wie folgt:
 
$$\alpha(f)  =  \sqrt{\frac {1}{2}\cdot \left (R' G' - \omega^2 \cdot L'  C'\right)+ \frac {1}{2}\sqrt{(R'^2 + \omega^2 \cdot L'^2) \cdot (G'^2 + \omega^2 \cdot C'^2)}} \bigg |_{\omega \hspace{0.05cm}= \hspace{0.05cm}2\pi f}.$$
 
Der ungerade Imaginärteil  $⇒  β(– f) = – β(f)$ heißt Phasenmaß und beschreibt die Phasendrehung der Welle entlang der Leitung:
 
$$\beta(f)  =  \sqrt{\frac {1}{2}\cdot \left (-R' G' + \omega^2 \cdot L'  C'\right)+ \frac {1}{2}\sqrt{(R'^2 + \omega^2 \cdot L'^2) \cdot (G'^2 + \omega^2 \cdot C'^2)}} \bigg |_{\omega \hspace{0.05cm}= \hspace{0.05cm}2\pi f}.$$
 
  
==Wellenwiderstand und Reflexionen (1)==
+
We also assume &nbsp;$Z < N$.&nbsp; The number of&nbsp; &raquo;distinguishable poles&laquo;&nbsp; is denoted by &nbsp;$I$.&nbsp; Multiple poles are counted only once to determine &nbsp;$I$.&nbsp; Thus,&nbsp; the following holds for the&nbsp; [[Linear_and_Time_Invariant_Systems/Inverse_Laplace_Transform#Some_results_of_function_theory|$\text{sketch}$]]&nbsp; in the last section considering the  double pole: &nbsp; 
Betrachten wir nun eine homogene Leitung der Länge $l$, an dessen Eingang eine harmonische Schwingung $U_0(f)$ mit variabler Frequenz $f$ angelegt wird. Der Sender besitzt den Innenwiderstand $Z_1$, der Empfänger den Eingangswiderstand $Z_2$, der gleichzeitig den Abschlusswiderstand der Leitung bildet. Wir gehen vereinfachend davon aus, dass $Z_1$ und $Z_2$ reelle Widerstände sind.
+
:$$N = 5,\hspace{0.3cm} I = 4.$$
  
[[File:P_ID1793__LZI_T_4_1_S2a_neu.png | Leitung der Länge l mit Beschaltung]]
+
{{BlaueBox|TEXT= 
 +
$\text{Residue Theorem:}$&nbsp;
 +
Considering the above conditions,&nbsp; the&nbsp; &raquo;'''inverse Laplace transform'''&laquo;&nbsp; of &nbsp;$Y_{\rm L}(p)$&nbsp; for times&nbsp; $t ≥ 0$&nbsp; is obtained as the sum of&nbsp; $I$&nbsp; natural oscillations of the poles,&nbsp; which are called the&nbsp; &raquo;residuals&laquo;&nbsp; – abbreviated as&nbsp; $\rm Res$:
 +
:$$y(t) = \sum_{i=1}^{I}{\rm Res} \bigg \vert _{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}_i}} \hspace{-0.7cm}\{Y_{\rm L}(p)\cdot  {\rm e}^{p \hspace{0.05cm}t}\} \hspace{0.05cm} .$$
  
Strom und Spannung von hinlaufender und rücklaufender Welle sind jeweils über den Wellenwiderstand $Z_W(f)$ miteinander verknüpft:
+
Since&nbsp; $Y_{\rm L}(p)$&nbsp; is only specifiable for causal signals, &nbsp;$y(t < 0) = 0$&nbsp; always holds for negative times.  
$$I_{\rightarrow}(x, f) = \frac{U_{\rightarrow}(x, f)}{Z_{\rm W}(f)}\hspace{0.05cm}, \hspace{0.5cm} I_{\leftarrow}(x, f) = \frac{U_{\leftarrow}(x, f)}{Z_{\rm W}(f)}\hspace{0.05cm}.$$
 
Für den Wellenwiderstand gilt dabei:
 
$$Z_{\rm W}(f)  =  \sqrt{\frac {R' + {\rm j}  \cdot \omega  L'}{G' + {\rm j}  \cdot \omega  C'}} \hspace{0.1cm}\bigg |_{\omega \hspace{0.05cm}= \hspace{0.05cm}2\pi f}.$$
 
  
 +
*In general,&nbsp; the following holds for a pole of multiplicity &nbsp;$l$&nbsp;:
 +
:$${\rm Res} \bigg \vert _{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{-0.7cm}\{Y_{\rm L}(p)\cdot {\rm e}^{p t}\}= \frac{1}{(l-1)!}\cdot \frac{ {\rm d}^{\hspace{0.05cm}l-1} }{ {\rm d}p^{\hspace{0.05cm}l-1} }\hspace{0.15cm} \left \{Y_{\rm L}(p)\cdot (p - p_{ {\rm x}_i})^{\hspace{0.05cm}l}\cdot  {\rm e}^{p \hspace{0.05cm}t}\right\} \bigg \vert_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{0.05cm} .$$
 +
*The following is obtained out of it with &nbsp;$l = 1$&nbsp; for a simple pole as a special case:
 +
:$${\rm Res} \bigg\vert_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{-0.7cm}\{Y_{\rm L}(p)\cdot {\rm e}^{p t}\}= Y_{\rm L}(p)\cdot (p - p_{ {\rm x}_i} )\cdot  {\rm e}^{p \hspace{0.05cm}t} \bigg \vert _{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{0.05cm} .$$}}
  
Die in positiver x–Richtung laufende Welle wird durch die Wechselspannungsquelle am Leitungsanfang (also bei $x =$ 0) erzeugt. Die rücklaufende Welle entsteht erst durch Reflektion der Vorwärtswelle am Leitungsende $(x = l)$. An dieser Stelle wird durch den Abschlusswiderstand $Z_2$ ein festes Verhältnis zwischen Spannung und Strom entsprechend $U_2(f) = Z_2 · I_2(f)$ erzwungen.
 
  
Die rücklaufende Welle entsteht bei Fehlanpassung durch Reflexion am Leitungsende:
+
In the next sections,&nbsp; the&nbsp; &raquo;residue theorem&laquo;&nbsp; is illustrated by three detailed examples corresponding to the three constellations in&nbsp; [[Linear_and_Time_Invariant_Systems/Laplace_Transform_and_p-Transfer_Function#Properties_of_poles_and_zeros|$\text{Example 3}$]]&nbsp; of chapter&nbsp; &raquo;Laplace transform and p-transfer function&laquo;:
$$U_{\leftarrow}(x = l) = {U_{\rightarrow}(x = l)}\cdot \frac{Z_2 -Z_{\rm W}(f)}{Z_2 + Z_{\rm W}(f)}\hspace{0.05cm}.$$
+
*So,&nbsp; we consider again the two-port network with an inductance &nbsp;$L = 25 \ \rm &micro;H$&nbsp; in the longitudinal branch as well as the the series connection of an ohmic resistance&nbsp; $R = 50 \ \rm Ω$&nbsp; and a capacitance&nbsp; $C$&nbsp; in the transverse branch.
  
Man erkennt aus dieser Gleichung, dass nur für $Z_2 = Z_W(f)$ keine rücklaufende Welle entsteht. Eine solche Widerstandanpassung wird in der Nachrichtentechnik stets angestrebt. Allerdings ist diese Anpassung wegen der Frequenzabhängigkeit des Wellenwiderstandes bei festem Abschluss $Z_2$ nicht über einen größeren Frequenzbereich möglich.  
+
*For the latter,&nbsp; we consider three different values,&nbsp; namely &nbsp;$C = 62.5 \ \rm nF$, &nbsp;$C = 8 \ \rm nF$&nbsp; and &nbsp;$C = 40 \ \rm nF$.  
  
Nachfolgend werden diese Gleichungen an einem Beispiel erläutert.
+
*The following is always assumed: &nbsp;$x(t) = δ(t) \; ⇒  \; X_{\rm L}(p) = 1$ &nbsp; &rArr; &nbsp; $Y_{\rm L}(p) = H_{\rm L}(p)$  &nbsp; &rArr; &nbsp; the output signal&nbsp; $y(t)$&nbsp; is equal to the impulse response &nbsp;$h(t)$.
  
==Wellenwiderstand und Reflexionen (2)==
+
==Aperiodically decaying impulse response==
{{Beispiel}}
+
<br>
Wir betrachten den Fall, dass sich der Abschlusswiderstand $Z_2$ der Leitung (gleichzeitig der Eingangswiderstand des nachfolgenden Empfängers) vom Wellenwiderstand $Z_W(f)$ unterscheidet. Die Fehlanpassung am Leitungsanfang lassen wir außer Betracht.
+
The following is obtained for the&nbsp; $p$&ndash;transfer function computed in the section &nbsp;[[Linear_and_Time_Invariant_Systems/Laplace_Transform_and_p-Transfer_Function#Pole-zero_representation_of_circuits|&raquo;pole-zero representation of circuits&laquo;]]&nbsp; with the capacitance &nbsp;$C = 62.5 \ \rm nF$.&nbsp; The other numerical values are given in the graph below:
 +
[[File: EN_LZI_T_3_3_S3a.png|right|frame|Aperiodically decaying impulse response]]
  
[[File:P_ID2844__LZI_T_4_1_S2c_neu.png | Modell zur Beschreibung der Wellenreflexion]]
+
:$$H_{\rm L}(p)= K \cdot \frac {p - p_{\rm o }} {(p - p_{\rm x 1})(p - p_{\rm x 2})}= 2 \cdot \frac {p + 0.32 }
 +
{(p +0.4)(p +1.6 )} \hspace{0.05cm} .$$
  
Die untere Grafik aus [Han08]  soll deutlich machen, wie sich die resultierende Welle $U(x)$ – als durchgezogene Kurve dargestellt – von der hinlaufenden Welle $U_→(x)$ unterscheidet.
+
Note the normalization of &nbsp;$p$, &nbsp;$K$ and also of all poles and zeros by the factor &nbsp;${\rm 10^6} · 1/\rm s$.
  
[[File:P_ID2840__LZI_T_4_1_S2b_V2.png | Hinlaufende, rücklaufende und resultierende Welle]]
+
&rArr; &nbsp; The impulse response is composed of &nbsp;$I = N = 2$&nbsp; natural oscillations. For $t < 0$,&nbsp; these are equal to zero.
 +
*The residual of the pole at &nbsp;$p_{{\rm x}1} =\  –0.4$&nbsp; yields the following time function:
 +
:$$h_1(t)  =  {\rm Res} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}1}} \hspace{-0.7cm}\{H_{\rm L}(p)\cdot {\rm e}^{p t}\}= H_{\rm L}(p)\cdot (p - p_{{\rm x}1})\cdot {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}1}}$$
 +
: $$\Rightarrow \hspace{0.3cm}h_1(t)  =  2 \cdot \frac {p + 0.32 } {p +0.4}\cdot  {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}-0.4}= - \frac {2 } {15}\cdot  {\rm e}^{-0.4 \hspace{0.05cm} t} \hspace{0.05cm}. $$
 +
*In the same way, the residual of the second pole at &nbsp;$p_{{\rm x}2} = \ –1.6$&nbsp; can be computed:
 +
:$$h_2(t)  =  {\rm Res} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}2}} \hspace{-0.7cm}\{H_{\rm L}(p)\cdot {\rm e}^{p t}\}= H_{\rm L}(p)\cdot (p - p_{{\rm x}2})\cdot  {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}2}}$$
 +
:$$\Rightarrow \hspace{0.3cm}h_2(t)  =  2 \cdot \frac {p + 0.32 } {p +1.6}\cdot  {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}-1.6}=  \frac {32 } {15}\cdot  {\rm e}^{-1.6 \hspace{0.05cm} t} \hspace{0.05cm}. $$
  
*Rot markiert ist die hinlaufende Welle $U_→(x)$, die ausgehend vom Sender  $⇒  U_→(x =$ 0) sich längs der Leitung abschwächt. $U_→(x = l)$ bezeichnet die Welle am Leitungsende.  
+
The graph shows &nbsp;$h_1(t)$&nbsp; and &nbsp;$h_2(t)$&nbsp; as well as the sum signal &nbsp;$h(t)$.  
*Aufgrund der Fehlanpassung kommt es zur rücklaufenden Welle (Reflexion) $U_←(x)$ vom Leitungsende zum Sender, in der Grafik grün markiert. Für diese gilt am Ausgangspunkt $x = l$:
+
#The normalization factor &nbsp;$1/T = 10^6 · \rm 1/s$&nbsp; is taken into account here so that the time is normalized to &nbsp;$T = 1 \ \rm &micro; s$&nbsp;.
$$U_{\leftarrow}(x = l) = {U_{\rightarrow}(x = l)}\cdot \frac{Z_2 -Z_{\rm W}(f)}{Z_2 + Z_{\rm W}(f)}\hspace{0.05cm}.$$
+
#For &nbsp;$t =0$,&nbsp; $T \cdot h(t=0) = {32 }/ {15} -{2 }/ {15}= 2 \hspace{0.05cm}$&nbsp; is obtained as a result.  
*Die resultierende (blaue) Welle $U(x)$ ergibt sich aus der phasenrichtigen Addition dieser beiden für sich allein nicht sichtbaren Anteile. Mit zunehmendem $x$ wird $U(x)$ ebenso wie $U_→(x)$ wegen der Leitungsdämpfung kleiner. Auch die rücklaufende Welle $U_←(x)$ wird mit zunehmender Länge gedämpft, allerdings von rechts nach links.
+
#For times &nbsp;$t > 2 \ \rm &micro; s$,&nbsp; the impulse response is negative&nbsp; $($although only slightly and difficult to see in the graph$)$.
{{end}}
 
  
==Verlustlose und verlustarme Leitungen==
 
Für sehr kurze Koaxialleitungen, wie sie für Verbindungen von HF–Messgeräten im Labor verwendet werden, kann von $R' = G' ≈$ 0 ausgegangen werden. Man spricht dann von einer verlustlosen Leitung. Für eine solche vereinfachen sich die obigen Gleichungen zu
 
$$\alpha(f)  = 0\hspace{0.05cm}, \hspace{0.3cm}\beta(f)  =  2\pi \cdot f \cdot \sqrt{L' \cdot C' }\hspace{0.05cm}, \hspace{0.3cm} Z_{\rm W}(f) = \sqrt{{L'}/{ C'} }\hspace{0.05cm}.$$
 
  
Sind $L'$ und $C'$ im betrachteten Frequenzbereich konstant, so ist der (reelle) Wellenwiderstand $Z_W(f)$ ebenfalls frequenzunabhängig und das Phasenmaß $β(f)$ proportional zur Frequenz. Das bedeutet, dass eine verlustlose Leitung stets verzerrungsfrei ist. Das Ausgangssignal weist gegenüber dem Eingangssignal lediglich eine Laufzeit auf. Üblich sind Wellenwiderstände von 50 Ω, 75 Ω und 150 Ω.  
+
==Attenuated-oscillatory impulse response==
 +
<br>
 +
The component values &nbsp;$R = 50 \ \rm Ω$, &nbsp;$L = 25 \ \rm &micro; H$&nbsp; and &nbsp;$C = 8 \ \rm nF$ result in two conjugate complex poles at &nbsp;$p_{{\rm x}1} = \ –1 + {\rm j} · 2$&nbsp; and &nbsp;$p_{{\rm x}2} = \ –1 - {\rm j} · 2$.&nbsp;
 +
[[File:EN_LZI_T_3_3_S3b.png|right|frame| Attenuated-oscillatory impulse response]]
 +
 +
*The zero is located at &nbsp;$p_{\rm o} = \ –2.5$.
 +
 +
*$K = 2$&nbsp; holds
  
Betrachten wir nun nochmals die Formel für das Dämpfungsmaß, also die Dämpfungsfunktion pro Länge,
+
*All numerical values are to be multiplied by factor &nbsp;$1/T$&nbsp; $(T = 1\ \rm &micro; s$).
$$\alpha(f)  = {{\rm a}(f)}/{ l} \hspace{0.05cm},$$
 
wenn die Leitung etwas länger ist, aber noch nicht als lang bezeichnet werden kann. Man spricht in diesem Fall von einer verlustarmen Leitung.  
 
  
Die vorne angegebene Formel für das Dämpfungsmaß soll nun für den nicht ganz der Wirklichkeit entsprechenden Fall konstanter Leitungsbeläge ausgewertet werden. Oberhalb einer '''charakteristischen Frequenz''' $f_∗$, die von $R', L', G'$ und $C'$ abhängt, kann $R'$ als sehr klein gegenüber $ωL'$ und $G'$ als sehr klein gegenüber $ωC'$ angenommen werden. Damit ergibt sich die Näherungsformel
 
$$\alpha_{_{{\rm I}}}(f)  = \frac{1}{2} \cdot \left [R' \cdot \sqrt{\frac{C'}{ L'} } + G' \cdot \sqrt{\frac{L'}{ C'} }\right ] \hspace{0.05cm},$$
 
die in der Literatur häufig als '''schwache Dämpfung''' bezeichnet wird.
 
  
Für kleine Frequenzen $(f < f_∗)$ ist dagegen $R' >> ωL'$ und $G' >> ωC'$ zu berücksichtigen und man erhält eine zweite obere Schranke, die man oft als '''starke Dämpfung''' bezeichnet:
+
Applying the residue theorem to this configuration then it is obtained:
  
[[File:P_ID1795__LZI_T_4_1_S3_kleiner_neu.png | Dämpfungsmaß α(f) und Schranken | rechts]]
+
:$$h_1(t) =  K \cdot \frac {p_{\rm x 1} - p_{\rm o }} {p_{\rm x 1} - p_{\rm x 2}} \cdot  {\rm e}^{\hspace{0.05cm}p_{\rm x 1} \cdot \hspace{0.05cm}t} $$
 +
:$$\Rightarrow \hspace{0.3cm}h_1(t) =    2 \cdot \frac {-1 + {\rm j}\cdot 2 +2.5} {(-1 + {\rm j}\cdot 2) - (-1 - {\rm j}\cdot 2)}\cdot  {\rm e}^{\hspace{0.05cm}p_{\rm x 1}
 +
\cdot\hspace{0.05cm}t}$$
 +
:$$\Rightarrow \hspace{0.3cm}h_1(t) =  2 \cdot \frac {1.5 + {\rm j}\cdot 2} {{\rm j}\cdot 4}\cdot  {\rm e}^{\hspace{0.05cm}p_{\rm x 1} \cdot\hspace{0.05cm}t}= (1 - {\rm j}\cdot 0.75)\cdot {\rm
 +
e}^{-t}\cdot {\rm  e}^{\hspace{0.03cm}{\rm j}\hspace{0.05cm}\cdot \hspace{0.05cm} 2t} \hspace{0.05cm} ,$$
  
$$\alpha_{_{{\rm II}}}(f)  =  \sqrt{\omega  \cdot \frac{R' \hspace{0.05cm} C'}{ 2} }\hspace{0.1cm} \bigg |_{\omega \hspace{0.05cm}= \hspace{0.05cm}2\pi f}\hspace{0.05cm}.$$
+
:$$ h_2(t) =  K \cdot \frac {p_{\rm x 2} - p_{\rm o }} {p_{\rm x 2} - p_{\rm x 1}}\cdot {\rm e}^{\hspace{0.05cm}p_{\rm x 2} \hspace{0.03cm}\cdot \hspace{0.05cm}t} $$
Die Grafik zeigt das Dämpfungsmaß $α(f)$ bei konstanten Leitungsbelägen nach der exakten, aber komplizierten Formel und die beiden Schranken $α_I(f)$ und $α_{II}(f)$.
+
:$$\Rightarrow \hspace{0.3cm} h_2(t) = 2 \cdot \frac {-1 - {\rm j}\cdot 2 +2.5} {(-1 - {\rm j}\cdot 2) - (-1 + {\rm j}\cdot 2)}\cdot  {\rm e}^{\hspace{0.05cm}p_{\rm x 2} \hspace{0.03cm}\cdot\hspace{0.05cm}t} $$
 +
:$$\Rightarrow \hspace{0.3cm}h_2(t) =2 \cdot \frac {1.5 - {\rm j}\cdot 2} {-{\rm j}\cdot 4}\cdot  {\rm e}^{\hspace{0.05cm}p_{\rm x 2} \hspace{0.03cm}\cdot\hspace{0.05cm}t}= (1 + {\rm j}\cdot 0.75)\cdot {\rm e}^{-t}\cdot {\rm  e}^{\hspace{0.03cm}-{\rm j}\hspace{0.05cm}\cdot \hspace{0.05cm} 2t} \hspace{0.05cm} . $$
  
Man erkennt aus dieser Darstellung:  
+
Using&nbsp; [[Signal_Representation/Calculating_With_Complex_Numbers#Representation_by_magnitude_and_phase|&raquo;Euler's theorem&laquo;]]&nbsp; the following is obtained for the sum signal:
*Sowohl $α_I(f)$ als auch $α_{II}(f)$ sind obere Schranken für $α(f)$.  
+
:$$h(t) =  h_1(t) + h_2(t)\hspace{0.3cm}
*Die charakteristische Frequenz $f_∗$ ist der Schnittpunkt von $α_I(f)$ und $α_{II}(f)$.  
+
\Rightarrow \hspace{0.3cm}h(t) = {\rm  e}^{-t}\cdot \big [ (1 - {\rm j}\cdot 0.75)\cdot (\cos() + {\rm j}\cdot \sin())+
*Für $f >> f_∗$ gilt $α(f) ≈ α_I(f)$, für $f << f_∗$ dagegen $α(f) ≈ α_{II}(f)$.  
+
+ (1 + {\rm j}\cdot 0.75)\cdot (\cos() - {\rm j}\cdot \sin())\big ]$$
   
+
:$$\Rightarrow \hspace{0.3cm}h(t) ={\rm  e}^{-t}\cdot \big [ 2\cdot \cos(2t) + 1.5 \cdot \sin(2t)\big ]\hspace{0.05cm} . $$
 +
 
 +
The graph shows the attenuated-oscillatory impulse response &nbsp;$h(t)$&nbsp; attenuated by &nbsp;${\rm e}^{–t}$&nbsp; for this pole–zero configuration.
 +
 
 +
 
 +
==Critically attenuated case==
 +
<br>
 +
With &nbsp;$R = 50 \ \rm Ω$, &nbsp;$L = 25 \ \rm &micro; H$&nbsp; and&nbsp; &nbsp;$C = 40 \ \rm nF$&nbsp; we get the so-called&nbsp; &raquo;critically attenuated case&laquo;:
 +
:$$H_{\rm L}(p)= K \cdot \frac {p - p_{\rm o }} {(p - p_{\rm x })^2}= 2 \cdot \frac {p + 0.5 } {(p +1)^2}  \hspace{0.05cm} .$$
 +
 
 +
The capacitance &nbsp;$C = 40 \ \rm nF$&nbsp; is the smallest possible value for which there are just real pole places.&nbsp; These coincide,&nbsp; that &nbsp;$p_{\rm x} = \ -1$&nbsp; is a double pole place.&nbsp; The time function is thus according to the residue theorem with &nbsp;$l = 2$:
 +
:$$h(t) = {\rm Res} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x} } } \hspace{-0.7cm}\{H_{\rm L}(p)\cdot {\rm e}^{p t}\}= \frac{ {\rm d} }{ {\rm d}p}\hspace{0.15cm}
 +
\left \{H_{\rm L}(p)\cdot (p - p_{ {\rm x} })^2\cdot {\rm e}^{p \hspace{0.05cm}t}\right\} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x} } } = K \cdot \frac{ {\rm d} }{ {\rm d}p}\hspace{0.15cm}\left \{ (p - p_{ {\rm o} })\cdot {\rm e}^{p \hspace{0.05cm}t}\right\}  \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x} } } \hspace{0.05cm} .$$
 +
 
 +
[[File:EN_LZI_T_3_3_S3c.png |right|frame| Impulse response and step response of the critically attenuated case]]
 +
Using the&nbsp; &raquo;product rule&laquo;&nbsp; of differential calculus,&nbsp; this gives:
 +
:$$h(t) = K \cdot \left [ {\rm e}^{p \hspace{0.05cm}t} + (p - p_{ {\rm o} })\cdot t \cdot {\rm e}^{p \hspace{0.05cm}t} \right ] \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}-1} = {\rm  e}^{-t}\cdot \left ( 2 - t \right)
 +
\hspace{0.05cm} .$$
 +
 
 +
The graph shows this impulse response&nbsp; $($green curve$)$&nbsp; in normalized representation.&nbsp; It differs only slightly from the one with two different poles at&nbsp; $-0.4$&nbsp; and&nbsp; $-1.6$&nbsp;.
 +
 
 +
The signal drawn in red &nbsp; &rArr; &nbsp; $y(t) = 1 - {\rm e}^{-t} + t \cdot {\rm e}^{-t}$&nbsp; results when a step function&nbsp; $\gamma(t)$&nbsp; is considered at the input &nbsp; &rArr; &nbsp; &raquo;step response&laquo;.  
 +
 
 +
To calculate the step response &nbsp;$\sigma(t) = y(t)$&nbsp; one can alternatively
 +
*consider the additional red pole at &nbsp;$p = 0$ &nbsp; in the residual calculation,&nbsp;
 +
 
 +
*or form the integral over the impulse response &nbsp;$h(t)$.
 +
 
 +
 
 +
==Partial fraction decomposition==
 +
<br>
 +
Prerequisite for the application of the residue theorem is that there are less zeros than poles &nbsp; &rArr; &nbsp; $Z$&nbsp; must always be smaller than &nbsp;$N$&nbsp;.
 +
 
 +
*If,&nbsp; on the other hand,&nbsp; as in the case of a high-pass filter &nbsp;$Z = N$,&nbsp; then the limit of the p&ndash;transfer function&nbsp; $H_{\rm L}(p)$&nbsp; for large &nbsp;$p$&nbsp; is not equal to zero,
 +
 
 +
*If the associated time signal &nbsp;$y(t)$&nbsp; also contains &nbsp;[[Signal_Representation/Direct_Current_Signal_-_Limit_Case_of_a_Periodic_Signal#Dirac_.28delta.29_function_in_frequency_domain|&raquo;Dirac delta functions&laquo;]],&nbsp;  the residue theorem fails and a&nbsp; [https://en.wikipedia.org/wiki/Partial_fraction_decomposition&nbsp; &raquo;'''partial fraction decomposition'''&laquo;]&nbsp; must be performed.
 +
 
 +
 
 +
The procedure is to be clarified exemplarily for a high-pass of first order.
 +
 
 +
{{GraueBox|TEXT= 
 +
$\text{Example 1:}$&nbsp;
 +
The&nbsp; $p$-transfer function of a&nbsp; &raquo;first-order RC high-pass filter&laquo;&nbsp; can be transformed by splitting off a constant as follows:
 +
[[File:EN_LZI_T_3_3_S5_v2.png |right|frame| Impulse response of low-pass&nbsp; $($blue$)$&nbsp; and high-pass&nbsp; $($red$)$]]
 +
:$$\frac{p}{p + RC} = 1- \frac{RC}{p + RC}\hspace{0.05cm} .$$
 +
Thus,&nbsp; the high-pass impulse response is:
 +
:$$h_{\rm HP}(t) = \delta(t) - h_{\rm TP}(t) \hspace{0.05cm} .$$
 +
 
 +
The graph shows
 +
*as blue curve the impulse response &nbsp;$h_{\rm TP}(t)$&nbsp; of the equivalent low-pass,
 +
 
 +
*as red curve the high&ndash;pass impulse response &nbsp;$h_{\rm HP}(t)$.
 +
 
 +
 
 +
&rArr; &nbsp; The Dirac delta function is the Laplace transform of the constant value&nbsp; $1$,&nbsp; <br>while the second function to be subtracted gives the impulse response of the equivalent low-pass filter,&nbsp; which is given by the residue theorem with &nbsp;
 +
:$$Z = 0,\hspace{0.2cm} N =1,\hspace{0.2cm} K = RC.$$ }}
 +
 
 +
 
 +
 
 +
==Exercises for the chapter==
  
 +
[[Aufgaben:Exercise_3.5:_Circuit_with_R,_L_and_C|Exercise 3.5: Circuit with R, L and C]]
  
 +
[[Aufgaben:Exercise_3.5Z:_Application_of_the_Residue_Theorem|Exercise 3.5Z: Application of the Residue Theorem]]
  
 +
[[Aufgaben:Exercise_3.6:_Transient_Behavior|Exercise 3.6: Transient Behavior]]
  
 +
[[Aufgaben:Exercise_3.6Z:_Two_Imaginary_Poles|Exercise 3.6Z: Two Imaginary Poles]]
  
 +
[[Aufgaben:Exercise_3.7:_Impulse_Response_of_a_High-Pass_Filter|Exercise 3.7: Impulse Response of a High-Pass Filter]]
  
 +
[[Aufgaben:Exercise_3.7Z:_Partial_Fraction_Decomposition|Exercise 3.7Z: Partial Fraction Decomposition]]
  
  
 
{{Display}}
 
{{Display}}

Latest revision as of 17:03, 21 November 2023

Problem formulation and prerequisites


$\text{Task:}$  This chapter deals with the following problem:

  • The  $p$–spectral function  $Y_{\rm L}(p)$  is given in  »pole-zero notation«.
  • The  »inverse Laplace transform«, i.e. the associated time function  $y(t)$  is searched-for,  where the following notation should hold:
$$y(t) = {\rm L}^{-1}\{Y_{\rm L}(p)\}\hspace{0.05cm} , \hspace{0.3cm}{\rm briefly}\hspace{0.3cm} y(t) \quad \circ\!\!-\!\!\!-^{\hspace{-0.25cm}\rm L}\!\!\!-\!\!\bullet\quad Y_{\rm L}(p)\hspace{0.05cm} .$$
Prerequisites for the chapter "Inverse Laplace Transform"


The graph summarizes the prerequisites for this task.

  • $H_{\rm L}(p)$  describes the transfer function of the causal system and  $Y_{\rm L}(p)$  specifies the Laplace transform of the output signal  $y(t)$  considering the input signal  $x(t)$ .  $Y_{\rm L}(p)$  is characterized by  $N$  poles,  by  $Z ≤ N$  zeros and by the constant  $K.$
  • Poles and zeros exhibit the properties mentioned in the  »last chapter«:  Poles are only allowed in the left  $p$–half plane or on the imaginary axis;  zeros are also allowed in the right  $p$–half plane.
  • All  »singularities«  – this is the generic term for poles and zeros – are either real or exist as pairs of conjugate-complex singularities.  Multiple poles and zeros are also allowed.
  • With the input  $x(t) = δ(t)$   ⇒   $X_{\rm L}(p) = 1$   ⇒   $Y_{\rm L}(p) = H_{\rm L}(p)$, the output signal  $y(t)$  then describes the »impulse response«  $h(t)$  of the transmission system.  For this purpose,  only the singularities drawn in green in the graph may be used for computation.
  • A unit jump function  $x(t) = γ(t)$   ⇒   $ X_{\rm L} = 1/p$  at the input causes the output signal  $y(t)$  to be equal to the  »step response«   $σ(t)$ of $H_{\rm L}(p)$ .  In addition to the singularities of  $H_{\rm L}(p)$,  the pole  $($shown in red in the graph$)$  at  $p = 0$  must now also be taken into account for computation.
  • Possible as input  $x(t)$  are only signals for which  $X_{ \rm L}(p)$  can be expressed in pole-zero notation  (see the  $\text{table}$  in the chapter »Laplace Transform and $p$–Transfer Function»$)$,  for example a cosine or sine signal switched on at time  $t = 0$ .
  • So,  a rectangular signal  $x(t)\ \ ⇒ \ \ X_{\rm L}(p) = (1 - {\rm e}^{\hspace{0.05cm}p\hspace{0.05cm}\cdot \hspace{0.05cm} T})/p$  is not possible in the approach described here.  However, the rectangular response  $y(t)$  can be computed indirectly as the difference of two step responses.

Some results of function theory


In contrast to the  »Fourier integrals«,  which differ only slightly in the two directions of transformation,  for  »Laplace«  the computation of  $y(t)$  from  $Y_{\rm L}(p)$ – that is the inverse transformation – is

  • much more difficult than computing  $Y_{\rm L}(p)$  from  $y(t)$,
  • unresolvable or solvable only very laboriously by elementary means.


$\text{Definition:}$  In general, the following holds for the  »inverse Laplace transform«:

$$y(t) = {\rm L}^{-1}\{Y_{\rm L}(p)\}= \lim_{\beta \hspace{0.05cm}\rightarrow \hspace{0.05cm}\infty} \hspace{0.15cm} \frac{1}{ {\rm j} \cdot 2 \pi}\cdot \int_{ \alpha - {\rm j} \hspace{0.05cm}\cdot \hspace{0.05cm}2 \pi \beta } ^{\alpha+{\rm j} \hspace{0.05cm}\cdot \hspace{0.05cm}2 \pi \beta} Y_{\rm L}(p) \hspace{0.05cm}\cdot \hspace{0.05cm} {\rm e}^{\hspace{0.05cm}p \hspace{0.05cm}\cdot \hspace{0.05cm} t}\hspace{0.1cm}{\rm d}p \hspace{0.05cm} .$$
  1. The integration is parallel to the imaginary axis.
  2. The real part  $α$  is to be chosen such that all poles are located to the left of the integration path.


The left graph illustrates this line integral along the red dotted vertical  ${\rm Re}\{p\}= α$.  This integral is solvable using  »Jordan's lemma of complex analysis«.  In this tutorial only a very short and simple summary of the approach is depicted:

Line integral together with left and right circular integral
  1. The line integral can be divided into two circular integrals so that all poles are located in the left circular integral while the right circular integral may only contain zeros.
  2. According to the theory of functions, the right circular integral yields the time function  $y(t)$  for negative times. 
  3. Due to causality,  $y(t < 0)$  must be identical to zero,  but according to the fundamentals of function theorem this is only true if there are no poles in the right  $p$–half-plane.
  4. In contrast,  the integral over the left semicircle yields the time function for  $t ≥ 0$. 
  5. This encloses all poles and can be computed using the  »residue theorem«  in a  $($relatively$)$  simple way,  as it will be shown in the next sections.


Formulation of the residue theorem


It is further assumed that the transfer function  $Y_{\rm L}(p)$  can be expressed in pole-zero notation by

  • the constant factor  $K$,
  • the  $Z$  »zeros«  $p_{{\rm o}i}$  $(i = 1$, ... , $Z)$  and
  • the  $N$  »poles«  $p_{{\rm x}i}$  $(i = 1$, ... , $N$).


We also assume  $Z < N$.  The number of  »distinguishable poles«  is denoted by  $I$.  Multiple poles are counted only once to determine  $I$.  Thus,  the following holds for the  $\text{sketch}$  in the last section considering the double pole:  

$$N = 5,\hspace{0.3cm} I = 4.$$

$\text{Residue Theorem:}$  Considering the above conditions,  the  »inverse Laplace transform«  of  $Y_{\rm L}(p)$  for times  $t ≥ 0$  is obtained as the sum of  $I$  natural oscillations of the poles,  which are called the  »residuals«  – abbreviated as  $\rm Res$:

$$y(t) = \sum_{i=1}^{I}{\rm Res} \bigg \vert _{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}_i}} \hspace{-0.7cm}\{Y_{\rm L}(p)\cdot {\rm e}^{p \hspace{0.05cm}t}\} \hspace{0.05cm} .$$

Since  $Y_{\rm L}(p)$  is only specifiable for causal signals,  $y(t < 0) = 0$  always holds for negative times.

  • In general,  the following holds for a pole of multiplicity  $l$ :
$${\rm Res} \bigg \vert _{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{-0.7cm}\{Y_{\rm L}(p)\cdot {\rm e}^{p t}\}= \frac{1}{(l-1)!}\cdot \frac{ {\rm d}^{\hspace{0.05cm}l-1} }{ {\rm d}p^{\hspace{0.05cm}l-1} }\hspace{0.15cm} \left \{Y_{\rm L}(p)\cdot (p - p_{ {\rm x}_i})^{\hspace{0.05cm}l}\cdot {\rm e}^{p \hspace{0.05cm}t}\right\} \bigg \vert_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{0.05cm} .$$
  • The following is obtained out of it with  $l = 1$  for a simple pole as a special case:
$${\rm Res} \bigg\vert_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{-0.7cm}\{Y_{\rm L}(p)\cdot {\rm e}^{p t}\}= Y_{\rm L}(p)\cdot (p - p_{ {\rm x}_i} )\cdot {\rm e}^{p \hspace{0.05cm}t} \bigg \vert _{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x}_i} } \hspace{0.05cm} .$$


In the next sections,  the  »residue theorem«  is illustrated by three detailed examples corresponding to the three constellations in  $\text{Example 3}$  of chapter  »Laplace transform and p-transfer function«:

  • So,  we consider again the two-port network with an inductance  $L = 25 \ \rm µH$  in the longitudinal branch as well as the the series connection of an ohmic resistance  $R = 50 \ \rm Ω$  and a capacitance  $C$  in the transverse branch.
  • For the latter,  we consider three different values,  namely  $C = 62.5 \ \rm nF$,  $C = 8 \ \rm nF$  and  $C = 40 \ \rm nF$.
  • The following is always assumed:  $x(t) = δ(t) \; ⇒ \; X_{\rm L}(p) = 1$   ⇒   $Y_{\rm L}(p) = H_{\rm L}(p)$   ⇒   the output signal  $y(t)$  is equal to the impulse response  $h(t)$.

Aperiodically decaying impulse response


The following is obtained for the  $p$–transfer function computed in the section  »pole-zero representation of circuits«  with the capacitance  $C = 62.5 \ \rm nF$.  The other numerical values are given in the graph below:

Aperiodically decaying impulse response
$$H_{\rm L}(p)= K \cdot \frac {p - p_{\rm o }} {(p - p_{\rm x 1})(p - p_{\rm x 2})}= 2 \cdot \frac {p + 0.32 } {(p +0.4)(p +1.6 )} \hspace{0.05cm} .$$

Note the normalization of  $p$,  $K$ and also of all poles and zeros by the factor  ${\rm 10^6} · 1/\rm s$.

⇒   The impulse response is composed of  $I = N = 2$  natural oscillations. For $t < 0$,  these are equal to zero.

  • The residual of the pole at  $p_{{\rm x}1} =\ –0.4$  yields the following time function:
$$h_1(t) = {\rm Res} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}1}} \hspace{-0.7cm}\{H_{\rm L}(p)\cdot {\rm e}^{p t}\}= H_{\rm L}(p)\cdot (p - p_{{\rm x}1})\cdot {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}1}}$$
$$\Rightarrow \hspace{0.3cm}h_1(t) = 2 \cdot \frac {p + 0.32 } {p +0.4}\cdot {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}-0.4}= - \frac {2 } {15}\cdot {\rm e}^{-0.4 \hspace{0.05cm} t} \hspace{0.05cm}. $$
  • In the same way, the residual of the second pole at  $p_{{\rm x}2} = \ –1.6$  can be computed:
$$h_2(t) = {\rm Res} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}2}} \hspace{-0.7cm}\{H_{\rm L}(p)\cdot {\rm e}^{p t}\}= H_{\rm L}(p)\cdot (p - p_{{\rm x}2})\cdot {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{{\rm x}2}}$$
$$\Rightarrow \hspace{0.3cm}h_2(t) = 2 \cdot \frac {p + 0.32 } {p +1.6}\cdot {\rm e}^{p \hspace{0.05cm}t} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}-1.6}= \frac {32 } {15}\cdot {\rm e}^{-1.6 \hspace{0.05cm} t} \hspace{0.05cm}. $$

The graph shows  $h_1(t)$  and  $h_2(t)$  as well as the sum signal  $h(t)$.

  1. The normalization factor  $1/T = 10^6 · \rm 1/s$  is taken into account here so that the time is normalized to  $T = 1 \ \rm µ s$ .
  2. For  $t =0$,  $T \cdot h(t=0) = {32 }/ {15} -{2 }/ {15}= 2 \hspace{0.05cm}$  is obtained as a result.
  3. For times  $t > 2 \ \rm µ s$,  the impulse response is negative  $($although only slightly and difficult to see in the graph$)$.


Attenuated-oscillatory impulse response


The component values  $R = 50 \ \rm Ω$,  $L = 25 \ \rm µ H$  and  $C = 8 \ \rm nF$ result in two conjugate complex poles at  $p_{{\rm x}1} = \ –1 + {\rm j} · 2$  and  $p_{{\rm x}2} = \ –1 - {\rm j} · 2$. 

Attenuated-oscillatory impulse response
  • The zero is located at  $p_{\rm o} = \ –2.5$.
  • $K = 2$  holds
  • All numerical values are to be multiplied by factor  $1/T$  $(T = 1\ \rm µ s$).


Applying the residue theorem to this configuration then it is obtained:

$$h_1(t) = K \cdot \frac {p_{\rm x 1} - p_{\rm o }} {p_{\rm x 1} - p_{\rm x 2}} \cdot {\rm e}^{\hspace{0.05cm}p_{\rm x 1} \cdot \hspace{0.05cm}t} $$
$$\Rightarrow \hspace{0.3cm}h_1(t) = 2 \cdot \frac {-1 + {\rm j}\cdot 2 +2.5} {(-1 + {\rm j}\cdot 2) - (-1 - {\rm j}\cdot 2)}\cdot {\rm e}^{\hspace{0.05cm}p_{\rm x 1} \cdot\hspace{0.05cm}t}$$
$$\Rightarrow \hspace{0.3cm}h_1(t) = 2 \cdot \frac {1.5 + {\rm j}\cdot 2} {{\rm j}\cdot 4}\cdot {\rm e}^{\hspace{0.05cm}p_{\rm x 1} \cdot\hspace{0.05cm}t}= (1 - {\rm j}\cdot 0.75)\cdot {\rm e}^{-t}\cdot {\rm e}^{\hspace{0.03cm}{\rm j}\hspace{0.05cm}\cdot \hspace{0.05cm} 2t} \hspace{0.05cm} ,$$
$$ h_2(t) = K \cdot \frac {p_{\rm x 2} - p_{\rm o }} {p_{\rm x 2} - p_{\rm x 1}}\cdot {\rm e}^{\hspace{0.05cm}p_{\rm x 2} \hspace{0.03cm}\cdot \hspace{0.05cm}t} $$
$$\Rightarrow \hspace{0.3cm} h_2(t) = 2 \cdot \frac {-1 - {\rm j}\cdot 2 +2.5} {(-1 - {\rm j}\cdot 2) - (-1 + {\rm j}\cdot 2)}\cdot {\rm e}^{\hspace{0.05cm}p_{\rm x 2} \hspace{0.03cm}\cdot\hspace{0.05cm}t} $$
$$\Rightarrow \hspace{0.3cm}h_2(t) =2 \cdot \frac {1.5 - {\rm j}\cdot 2} {-{\rm j}\cdot 4}\cdot {\rm e}^{\hspace{0.05cm}p_{\rm x 2} \hspace{0.03cm}\cdot\hspace{0.05cm}t}= (1 + {\rm j}\cdot 0.75)\cdot {\rm e}^{-t}\cdot {\rm e}^{\hspace{0.03cm}-{\rm j}\hspace{0.05cm}\cdot \hspace{0.05cm} 2t} \hspace{0.05cm} . $$

Using  »Euler's theorem«  the following is obtained for the sum signal:

$$h(t) = h_1(t) + h_2(t)\hspace{0.3cm} \Rightarrow \hspace{0.3cm}h(t) = {\rm e}^{-t}\cdot \big [ (1 - {\rm j}\cdot 0.75)\cdot (\cos() + {\rm j}\cdot \sin())+ + (1 + {\rm j}\cdot 0.75)\cdot (\cos() - {\rm j}\cdot \sin())\big ]$$
$$\Rightarrow \hspace{0.3cm}h(t) ={\rm e}^{-t}\cdot \big [ 2\cdot \cos(2t) + 1.5 \cdot \sin(2t)\big ]\hspace{0.05cm} . $$

The graph shows the attenuated-oscillatory impulse response  $h(t)$  attenuated by  ${\rm e}^{–t}$  for this pole–zero configuration.


Critically attenuated case


With  $R = 50 \ \rm Ω$,  $L = 25 \ \rm µ H$  and   $C = 40 \ \rm nF$  we get the so-called  »critically attenuated case«:

$$H_{\rm L}(p)= K \cdot \frac {p - p_{\rm o }} {(p - p_{\rm x })^2}= 2 \cdot \frac {p + 0.5 } {(p +1)^2} \hspace{0.05cm} .$$

The capacitance  $C = 40 \ \rm nF$  is the smallest possible value for which there are just real pole places.  These coincide,  that  $p_{\rm x} = \ -1$  is a double pole place.  The time function is thus according to the residue theorem with  $l = 2$:

$$h(t) = {\rm Res} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x} } } \hspace{-0.7cm}\{H_{\rm L}(p)\cdot {\rm e}^{p t}\}= \frac{ {\rm d} }{ {\rm d}p}\hspace{0.15cm} \left \{H_{\rm L}(p)\cdot (p - p_{ {\rm x} })^2\cdot {\rm e}^{p \hspace{0.05cm}t}\right\} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x} } } = K \cdot \frac{ {\rm d} }{ {\rm d}p}\hspace{0.15cm}\left \{ (p - p_{ {\rm o} })\cdot {\rm e}^{p \hspace{0.05cm}t}\right\} \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}p_{ {\rm x} } } \hspace{0.05cm} .$$
Impulse response and step response of the critically attenuated case

Using the  »product rule«  of differential calculus,  this gives:

$$h(t) = K \cdot \left [ {\rm e}^{p \hspace{0.05cm}t} + (p - p_{ {\rm o} })\cdot t \cdot {\rm e}^{p \hspace{0.05cm}t} \right ] \bigg |_{p \hspace{0.05cm}= \hspace{0.05cm}-1} = {\rm e}^{-t}\cdot \left ( 2 - t \right) \hspace{0.05cm} .$$

The graph shows this impulse response  $($green curve$)$  in normalized representation.  It differs only slightly from the one with two different poles at  $-0.4$  and  $-1.6$ .

The signal drawn in red   ⇒   $y(t) = 1 - {\rm e}^{-t} + t \cdot {\rm e}^{-t}$  results when a step function  $\gamma(t)$  is considered at the input   ⇒   »step response«.

To calculate the step response  $\sigma(t) = y(t)$  one can alternatively

  • consider the additional red pole at  $p = 0$   in the residual calculation, 
  • or form the integral over the impulse response  $h(t)$.


Partial fraction decomposition


Prerequisite for the application of the residue theorem is that there are less zeros than poles   ⇒   $Z$  must always be smaller than  $N$ .

  • If,  on the other hand,  as in the case of a high-pass filter  $Z = N$,  then the limit of the p–transfer function  $H_{\rm L}(p)$  for large  $p$  is not equal to zero,


The procedure is to be clarified exemplarily for a high-pass of first order.

$\text{Example 1:}$  The  $p$-transfer function of a  »first-order RC high-pass filter«  can be transformed by splitting off a constant as follows:

Impulse response of low-pass  $($blue$)$  and high-pass  $($red$)$
$$\frac{p}{p + RC} = 1- \frac{RC}{p + RC}\hspace{0.05cm} .$$

Thus,  the high-pass impulse response is:

$$h_{\rm HP}(t) = \delta(t) - h_{\rm TP}(t) \hspace{0.05cm} .$$

The graph shows

  • as blue curve the impulse response  $h_{\rm TP}(t)$  of the equivalent low-pass,
  • as red curve the high–pass impulse response  $h_{\rm HP}(t)$.


⇒   The Dirac delta function is the Laplace transform of the constant value  $1$, 
while the second function to be subtracted gives the impulse response of the equivalent low-pass filter,  which is given by the residue theorem with  

$$Z = 0,\hspace{0.2cm} N =1,\hspace{0.2cm} K = RC.$$


Exercises for the chapter

Exercise 3.5: Circuit with R, L and C

Exercise 3.5Z: Application of the Residue Theorem

Exercise 3.6: Transient Behavior

Exercise 3.6Z: Two Imaginary Poles

Exercise 3.7: Impulse Response of a High-Pass Filter

Exercise 3.7Z: Partial Fraction Decomposition