Solved Problems · Set 32

Circuit Analysis in the s-Domain

Part 3 · Frequency Response — Set 31 transformed differential equations that were simply handed over. Here the circuit is transformed instead, so that stored energy becomes a source on the diagram and every method of Part 1 applies unchanged.

Prof. Mithun Mondal 20 solved · 12 practice · 3 challenge GATE · ESE · University

Set 32 — Circuit Analysis in the s-Domain

Set 31 established the transform and its theorems, but every problem there began from a differential equation or a transform that had already been written down. Getting from a circuit diagram to that equation was still the classical business of applying KVL, differentiating, and tracking initial conditions by hand. This set removes that step entirely. Each element is replaced by an impedance in \(s\)\(R\), \(sL\), \(1/sC\) — and any stored energy becomes an ordinary independent source drawn onto the diagram. What remains is a resistive network with slightly unusual element values, and every technique of Part 1 applies to it without a single modification.

Textbook Chapter 17 · 20 solved · 12 practice · 3 challenge · 12 MCQs

i Method Recap
  • Transformed impedances — the whole method in one row of a table:

    Element\(\mathbf{Z}(s)\)\(\mathbf{Y}(s)\)
    Resistor\(R\)\(1/R\)
    Inductor\(sL\)\(1/sL\)
    Capacitor\(1/sC\)\(sC\)
  • Stored energy becomes a source:

    ElementThévenin formNorton form
    Inductor, \(i(0^-)\)\(sL\) + series \(Li(0^-)\)\(sL\) ∥ current \(i(0^-)/s\)
    Capacitor, \(v(0^-)\)\(1/sC\) + series \(v(0^-)/s\)\(1/sC\) ∥ current \(Cv(0^-)\)
  • Then every Part 1 method applies unchanged: KVL and KCL, series–parallel reduction, mesh and nodal analysis, source transformation, Thévenin and Norton, superposition, maximum power transfer.

  • Reading the endpoints from element behaviour rather than algebra:

    LimitInductorCapacitor
    \(s \to \infty\) (\(t \to 0^+\))Open circuitShort circuit
    \(s \to 0\) (\(t \to \infty\))Short circuitOpen circuit

    subject to any stored-energy sources, which do not vanish in either limit.

  • Network functions: \(H(s) = \) output over input, defined with zero initial conditions. Poles come from the denominator — the network's own natural frequencies.

  • Convention: capital letters for transformed quantities (\(I(s)\), \(V(s)\)), lower case for time functions. All initial conditions are the \(0^-\) values.

VideoWalkthrough
Problem 1CoreTransformed Elements

Derive the \(s\)-domain impedance of each passive element, and explain why the result makes every Part 1 technique available.

Solution

Transform each element law, taking zero initial conditions for now:

\[ \text{Resistor: } v = Ri \;\longrightarrow\; V(s) = RI(s) \]
\[ \text{Inductor: } v = L\frac{di}{dt} \;\longrightarrow\; V(s) = sLI(s) \]
\[ \text{Capacitor: } i = C\frac{dv}{dt} \;\longrightarrow\; I(s) = sCV(s) \;\Longrightarrow\; V(s) = \frac{I(s)}{sC} \]

Each is now \(V = \mathbf{Z}I\)Ohm's law with a complex-valued coefficient. The calculus has vanished.

The impedance table:

Element\(\mathbf{Z}(s)\)At \(s = j\omega\)Set 20 form
Resistor\(R\)\(R\)\(R\)
Inductor\(sL\)\(j\omega L\)\(j\omega L\) ✓
Capacitor\(1/sC\)\(1/j\omega C\)\(-j/\omega C\) ✓

Setting \(s = j\omega\) recovers Set 20's phasor impedances exactly. The \(s\)-domain impedance is the more general object; the phasor impedance is its restriction to the imaginary axis, valid under the stability condition of Set 31, Problem 16.

Why every Part 1 method transfers. The techniques of Sets 3 to 12 relied on exactly three facts:

FactStill true in \(s\)?
KVL: voltages round a loop sum to zeroYes — transform is linear
KCL: currents at a node sum to zeroYes — same reason
Each element obeys \(V = \mathbf{Z}I\)Yes — just derived

Nothing else was ever used. Mesh analysis, nodal analysis, Thévenin, Norton, superposition and source transformation therefore all carry over verbatim — Problem 19 audits this claim properly.

Combination rules are unchanged:

\[ \mathbf{Z}_{\text{series}} = \sum\mathbf{Z}_k, \qquad \frac{1}{\mathbf{Z}_{\text{parallel}}} = \sum\frac{1}{\mathbf{Z}_k} \]

A series \(RLC\) branch, for instance:

\[ \mathbf{Z}(s) = R+sL+\frac{1}{sC} = \frac{s^2LC+sRC+1}{sC} \]

A ratio of polynomials — every impedance of a lumped network is rational in \(s\), which is why every response is a sum of exponentials (Set 31, Problem 14).

Reading the limiting behaviour straight off the impedances:

\(s \to \infty\)\(s \to 0\)
\(sL\)\(\to\infty\)open\(\to0\)short
\(1/sC\)\(\to0\)short\(\to\infty\)open

By the initial and final value theorems these correspond to \(t\to0^+\) and \(t\to\infty\)the familiar rules of Set 18, now derived from impedance rather than remembered. Problem 14 uses this as a checking method.

Once the elements are transformed, the circuit is resistive. That single sentence is the content of this set: differential equations, initial conditions and transient analysis all collapse into a network problem of exactly the kind solved in Part 1, with polynomials in \(s\) in place of numbers.
Answer\(\mathbf{Z}_R = R\), \(\mathbf{Z}_L = sL\), \(\mathbf{Z}_C = 1/sC\). Since KVL, KCL and \(V = \mathbf{Z}I\) all hold, every technique of Part 1 applies unchanged.
Problem 2Exam levelInitial Conditions as Sources

Derive both the Thévenin and Norton models for an inductor and a capacitor with stored energy, and show the two are equivalent.

Solution

The inductor, from the differentiation theorem (Set 31, Problem 5):

\[ v = L\frac{di}{dt} \;\longrightarrow\; V(s) = sLI(s) - Li(0^-) \]

Read as a KVL statement: an impedance \(sL\) in series with a voltage source of value \(Li(0^-)\), oriented to oppose the assumed current direction. Note the source is a constant in \(s\), hence an impulse in time.

The Norton form follows by rearranging for \(I\):

\[ I(s) = \frac{V(s)}{sL}+\frac{i(0^-)}{s} \]

Admittance \(1/sL\) in parallel with a current source \(i(0^-)/s\) — a step of current in the time domain, which is the more intuitive picture: the inductor was already carrying that current.

Check they are equivalent by source transformation (Set 8):

\[ I_N = \frac{V_{Th}}{\mathbf{Z}} = \frac{Li(0^-)}{sL} = \frac{i(0^-)}{s}\;\checkmark \]

The capacitor, from the integration theorem (Set 31, Problem 6):

\[ V(s) = \frac{I(s)}{sC}+\frac{v(0^-)}{s} \qquad\text{(Thévenin)} \]
\[ I(s) = sCV(s)-Cv(0^-) \qquad\text{(Norton)} \]

Check: \(I_N = V_{Th}/\mathbf{Z} = [v(0^-)/s](sC) = Cv(0^-)\) ✓.

The complete table, which is all one needs to draw a transformed circuit:

ElementImpedanceSeries sourceParallel source
Resistor\(R\)
Inductor\(sL\)\(Li(0^-)\) (impulse)\(i(0^-)/s\) (step)
Capacitor\(1/sC\)\(v(0^-)/s\) (step)\(Cv(0^-)\) (impulse)

Note the pleasing duality: the inductor's series source is an impulse and its parallel source a step; the capacitor's are the other way round. Sets 8 and 18's dualities, appearing once more.

Which form to use — the same reasoning as Set 8:

AnalysisPreferred formWhy
MeshThévenin (series)Voltage sources go straight into KVL
NodalNorton (parallel)Current sources go straight into KCL

Getting the polarity right is the one place errors creep in. The safe procedure:

StepAction
1Fix a reference direction for \(i\) through the element
2Write the transformed law with that sign convention
3Draw the source to match the equation, not intuition
4Check with the initial value theorem

Step 4 is decisive: if the initial value comes out as \(-i(0^-)\), a source is reversed. Problem 4 demonstrates the check in use.

Stored energy is indistinguishable from a source. A charged capacitor and a battery behind an impedance produce identical terminal behaviour, which is why the transformed circuit needs no special machinery for initial conditions — they are drawn on the diagram like any other source and then forgotten about.
AnswerInductor: \(sL\) with series \(Li(0^-)\) or parallel \(i(0^-)/s\). Capacitor: \(1/sC\) with series \(v(0^-)/s\) or parallel \(Cv(0^-)\). The pairs are related by source transformation.
Problem 3CoreThe Running Circuit, at Rest

A series \(RLC\) circuit has \(R = 5\ \Omega\), \(L = 1\) H, \(C = \tfrac16\) F, initially at rest. A 10 V step is applied at \(t = 0\). Find \(i(t)\) and \(v_C(t)\).

Solution

1Transform the circuit. With no stored energy there are no extra sources:

\[ \mathbf{Z}(s) = R+sL+\frac{1}{sC} = 5+s+\frac{6}{s} = \frac{s^2+5s+6}{s} \]
\[ = \frac{(s+2)(s+3)}{s} \]

The natural frequencies are already visible — at \(-2\) and \(-3\), before any response has been computed. They are the zeros of the impedance.

2Apply Ohm's law:

\[ I(s) = \frac{V(s)}{\mathbf{Z}(s)} = \frac{10/s}{(s+2)(s+3)/s} = \frac{10}{(s+2)(s+3)} \]

The \(s\) cancels. The pole at the origin from the step is removed by the capacitor's zero — physically, no DC current flows through a capacitor, so there is no steady-state term.

3Invert by partial fractions:

\[ I(s) = \frac{10}{s+2}-\frac{10}{s+3} \]
\[ \boxed{\;i(t) = 10\left(e^{-2t}-e^{-3t}\right)\ \text{A}\;} \]

4The capacitor voltage, from \(V_C = I/sC\):

\[ V_C(s) = \frac{6}{s}\cdot\frac{10}{(s+2)(s+3)} = \frac{60}{s(s+2)(s+3)} \]
\[ = \frac{10}{s}-\frac{30}{s+2}+\frac{20}{s+3} \]
\[ \boxed{\;v_C(t) = 10-30e^{-2t}+20e^{-3t}\ \text{V}\;} \]

Check every endpoint:

QuantityAt \(t=0\)ExpectedAt \(t=\infty\)Expected
\(i\)\(10-10 = 0\)0 — inductor blocks ✓00 — capacitor blocks ✓
\(v_C\)\(10-30+20 = 0\)0 — uncharged ✓1010 — full source ✓

All four correct with no extra work — the initial and final conditions were never imposed, they simply emerged.

The current peak, by differentiating:

\[ \frac{di}{dt} = 0 \;\Longrightarrow\; -20e^{-2t}+30e^{-3t} = 0 \;\Longrightarrow\; t = \ln\tfrac32 = 0.4055\ \text{s} \]
\[ i_{\max} = 10\left(e^{-0.811}-e^{-1.216}\right) = 1.481\ \text{A} \]

Well below \(V/R = 2\) A, because the capacitor begins charging before the inductor has finished building current.

Four lines from circuit to answer, and both initial conditions checked for free. Compare Set 19, where a second-order transient required classifying the damping, writing the appropriate general solution, and solving two simultaneous equations for the constants. Here the damping case is simply whether the denominator factors over the reals.
Answer\(i(t) = 10(e^{-2t}-e^{-3t})\) A, peaking at 1.481 A at \(t = \ln 1.5 = 0.406\) s; \(v_C(t) = 10-30e^{-2t}+20e^{-3t}\) V.
Problem 4Exam levelThe Same Circuit, Energised

Repeat Problem 3 with \(i(0^-) = 2\) A and \(v_C(0^-) = 4\) V, and verify by KVL.

Solution

1Draw the transformed circuit with both stored-energy sources in Thévenin form, since this is a single loop:

ElementImpedanceSeries sourceSense
Source\(10/s\)Drives current
\(R\)5
\(L\)\(s\)\(Li(0^-) = 2\)Aids — current already flowing
\(C\)\(6/s\)\(v_C(0^-)/s = 4/s\)Opposes — charge already present

The signs are the crux. The inductor source pushes current in the direction it was already flowing; the capacitor's existing voltage opposes further charging.

2Apply KVL round the single loop:

\[ I(s)\left(5+s+\frac{6}{s}\right) = \frac{10}{s}+2-\frac{4}{s} \]
\[ I(s)\cdot\frac{(s+2)(s+3)}{s} = \frac{6}{s}+2 = \frac{2s+6}{s} = \frac{2(s+3)}{s} \]

3Solve — and something remarkable happens:

\[ I(s) = \frac{2(s+3)}{(s+2)(s+3)} = \frac{2}{s+2} \]
\[ \boxed{\;i(t) = 2e^{-2t}\ \text{A}\;} \]

The \((s+3)\) factor cancelled. A second-order circuit has produced a purely first-order current — the natural mode at \(s = -3\) is entirely absent. This is not an arithmetic accident, and Problem 13 explains it.

4The capacitor voltage:

\[ V_C(s) = \frac{I(s)}{sC}+\frac{v_C(0^-)}{s} = \frac{6}{s}\cdot\frac{2}{s+2}+\frac{4}{s} \]
\[ = \frac{12}{s(s+2)}+\frac{4}{s} = \frac{6}{s}-\frac{6}{s+2}+\frac{4}{s} \]
\[ \boxed{\;v_C(t) = 10-6e^{-2t}\ \text{V}\;} \]

Also purely first-order, and note the initial-condition term \(4/s\) had to be added back\(I/sC\) alone gives only the voltage change.

Verify by KVL in the time domain, the strongest available check:

TermExpression
\(v_R = 5i\)\(10e^{-2t}\)
\(v_L = L\,di/dt\)\(-4e^{-2t}\)
\(v_C\)\(10-6e^{-2t}\)
Sum\(10e^{-2t}-4e^{-2t}+10-6e^{-2t} = \mathbf{10}\) ✓

The exponentials cancel exactly, leaving the source voltage. KVL holds at every instant, confirming both the solution and the source polarities of step 1.

Endpoint checks:

\[ i(0^+) = \lim_{s\to\infty}sI(s) = \lim_{s\to\infty}\frac{2s}{s+2} = 2\ \text{A}\;\checkmark \]
\[ v_C(\infty) = \lim_{s\to0}sV_C(s) = 10\ \text{V}\;\checkmark \]

Both match the given data and physical expectation. Had a source been reversed, \(i(0^+)\) would have come out as \(-2\) A — which is precisely why the check is worth two lines.

The initial conditions never appeared as boundary conditions — they were sources in the KVL equation from the first line. That is the practical difference between this method and Set 19's, and it becomes decisive in circuits with several stored-energy elements, where the classical route needs simultaneous equations for the constants.
Answer\(i(t) = 2e^{-2t}\) A and \(v_C(t) = 10-6e^{-2t}\) V — both first-order, because the \((s+3)\) factor cancelled. KVL confirms the sum is exactly 10 V at all times.
Problem 5Exam levelMesh Analysis in s

A 10 V step drives mesh 1 through \(R_1 = 1\ \Omega\); a 1 H inductor is shared between the meshes; mesh 2 contains \(R_2 = 2\ \Omega\) and \(C = \tfrac12\) F. Find both mesh currents, starting from rest.

Solution

Write the impedance matrix exactly as in Set 4, but with polynomials:

\[ \begin{bmatrix}1+s & -s\\ -s & s+2+\dfrac{2}{s}\end{bmatrix} \begin{bmatrix}I_1\\ I_2\end{bmatrix} = \begin{bmatrix}10/s\\ 0\end{bmatrix} \]
EntryValueComposition
\(Z_{11}\)\(1+s\)\(R_1\) plus the shared \(sL\)
\(Z_{22}\)\(s+2+2/s\)Shared \(sL\), \(R_2\), \(1/sC\)
\(Z_{12} = Z_{21}\)\(-s\)Shared branch, negated

The matrix is symmetric, as it must be for a network of passive bilateral elements — the same check applied in Set 26, Problem 8.

Solve by Cramer's rule. The determinant:

\[ \Delta = (1+s)\left(s+2+\frac{2}{s}\right)-s^2 = \frac{3s^2+4s+2}{s} \]
\[ I_1(s) = \frac{10\left(s^2+2s+2\right)}{s\left(3s^2+4s+2\right)}, \qquad I_2(s) = \frac{10s}{3s^2+4s+2} \]

The natural frequencies are the roots of the common denominator:

\[ 3s^2+4s+2 = 0 \;\Longrightarrow\; s = \frac{-4\pm\sqrt{16-24}}{6} = -\frac{2}{3}\pm j\frac{\sqrt2}{3} \]

Underdamped — both mesh currents will oscillate at \(\sqrt2/3 = 0.471\) rad/s while decaying with \(\tau = 1.5\) s. The natural frequencies belong to the network, not to either mesh, which is why the same pair appears in both currents.

Check the endpoints without inverting:

QuantityFVTPhysical reasoning
\(i_1(\infty)\)\(\dfrac{10(2)}{2} = 10\) AInductor shorts, capacitor blocks; so \(10/R_1 = 10\) A ✓
\(i_2(\infty)\)0Capacitor blocks DC ✓

At DC the inductor short-circuits mesh 2's contribution and the capacitor blocks it, so all the current flows round mesh 1 through \(R_1\) and the inductor. The \(s\)-domain result agrees with elementary reasoning.

Where the initial conditions would go. Had the inductor carried \(i_L(0^-)\), its Thévenin source \(Li_L(0^-)\) would appear in both mesh equations — with opposite signs, since the branch is shared:

\[ \text{RHS} = \begin{bmatrix}10/s + Li_L(0^-)\\ -Li_L(0^-)\end{bmatrix} \]

Exactly the treatment a shared voltage source would receive in Set 4. No new rule is needed.

What carried over from Set 4, item by item:

Set 4 ruleStill valid?
Diagonal = sum of impedances round the mesh
Off-diagonal = negative of the shared impedance
Matrix symmetric for passive networks
RHS = net driving voltage round the mesh✓ — now including IC sources
Supermesh for current sources✓ — Set 6's method unchanged
Mesh analysis in the \(s\)-domain is mesh analysis. The entries are polynomials rather than numbers and the arithmetic is heavier, but not one rule has changed — which means a second-order transient with two loops is no harder to set up than a DC resistive network.
Answer\(I_1 = 10(s^2+2s+2)/[s(3s^2+4s+2)]\), \(I_2 = 10s/(3s^2+4s+2)\). Natural frequencies \(-\frac23 \pm j\frac{\sqrt2}{3}\), common to both. \(i_1(\infty) = 10\) A, \(i_2(\infty) = 0\).
Problem 6Exam levelNodal Analysis in s

A 4 A current step drives a parallel combination of \(R = 2\ \Omega\), \(L = 1\) H and \(C = \tfrac18\) F, initially at rest. Find \(v(t)\) and explain where the current ends up.

Solution

Write KCL at the single node — the admittance form is natural here:

\[ \mathbf{Y}(s) = \frac{1}{R}+sC+\frac{1}{sL} = \frac{1}{2}+\frac{s}{8}+\frac{1}{s} \]
\[ = \frac{s^2+4s+8}{8s} \]

Note that the natural frequencies come from the numerator of \(\mathbf{Y}\), whereas in Problem 3's series circuit they came from the numerator of \(\mathbf{Z}\). Duality again.

Solve:

\[ V(s) = \frac{I(s)}{\mathbf{Y}(s)} = \frac{4/s}{\left(s^2+4s+8\right)/8s} = \frac{32}{s^2+4s+8} \]

Complete the square (Set 31, Problem 4):

\[ s^2+4s+8 = (s+2)^2+2^2 \;\Longrightarrow\; V(s) = 16\cdot\frac{2}{(s+2)^2+2^2} \]
\[ \boxed{\;v(t) = 16e^{-2t}\sin2t\ \text{V}\;} \]

Check both endpoints:

EndpointValueReason
\(v(0^+)\)0Capacitor is a short at \(t=0^+\) ✓
\(v(\infty)\)0Inductor is a short at DC ✓

A common trap is to expect \(v(\infty) = IR = 8\) V. That would be right for a resistor alone, but the inductor short-circuits it at DC. The final voltage is zero, and the interesting question is where the 4 A goes.

Follow the current. The inductor current is \((1/L)\int v\,dt\), i.e. \(V(s)/sL\):

\[ I_L(s) = \frac{32}{s\left(s^2+4s+8\right)} \;\Longrightarrow\; i_L(t) = 4-4\sqrt2\,e^{-2t}\sin\left(2t+45°\right) \]
BranchCurrent as \(t\to\infty\)
Inductor4 A — all of it
Resistor\(v/R = 0\)
Capacitor0

The inductor takes the entire source current and holds it with no voltage across it — a perfect DC short. This is the dual of Problem 3's capacitor holding the entire source voltage with no current through it.

Reading the damping. Comparing with the standard form of Set 29:

\[ s^2+2\alpha s+\omega_0^2 \;\Longrightarrow\; \alpha = 2, \qquad \omega_0 = \sqrt8 = 2.828\ \text{rad/s} \]
\[ \zeta = \frac{\alpha}{\omega_0} = 0.7071, \qquad \omega_d = \sqrt{\omega_0^2-\alpha^2} = 2\ \text{rad/s} \]

\(\zeta = 1/\sqrt2\) exactly — a second-order Butterworth (Set 30, Problem 5). The damping ratio is read from the same denominator that gave the poles, so no separate classification step is needed.

For a parallel circuit, use \(\mathbf{Y}\), not \(\mathbf{Z}\). Computing \(\mathbf{Z} = 1/\mathbf{Y}\) first and then dividing would work, but inverting a three-term sum is needless labour. The rule from Set 5 stands:

TopologyUseNatural frequencies from
SeriesImpedances, mesh analysisNumerator of \(\mathbf{Z}\)
ParallelAdmittances, nodal analysisNumerator of \(\mathbf{Y}\)
The final state is decided by what the elements become at \(s = 0\), not by the resistor. An inductor in parallel always wins the DC argument, just as a capacitor in series always wins it — which is why "the voltage settles to \(IR\)" is wrong here and would be right if the inductor were absent.
Answer\(v(t) = 16e^{-2t}\sin2t\) V, with \(v(\infty) = 0\) — not \(IR\). All 4 A ends up in the inductor: \(i_L(t) = 4-4\sqrt2e^{-2t}\sin(2t+45°)\). Here \(\zeta = 0.707\).
Problem 7CoreThree Damping Cases

With \(L = 1\) H and \(C = \tfrac16\) F fixed and a 10 V step applied, find \(i(t)\) for \(R = 5\), \(2\sqrt6\) and 2 Ω, and show that all three come from one denominator.

Solution

One expression covers all three cases:

\[ I(s) = \frac{10/s}{s+R+6/s} = \frac{10}{s^2+Rs+6} \]

Only \(R\) changes. The damping case is decided entirely by whether \(s^2+Rs+6\) has real, repeated or complex roots — i.e. by the sign of \(R^2-24\).

aOverdamped, \(R = 5\ \Omega\). Discriminant \(25-24 = 1 > 0\):

\[ s^2+5s+6 = (s+2)(s+3) \;\Longrightarrow\; i(t) = 10\left(e^{-2t}-e^{-3t}\right) \]

Two distinct real poles, two exponentials, no oscillation — Problem 3's result.

bCritically damped, \(R = 2\sqrt6 = 4.899\ \Omega\). Discriminant zero:

\[ s^2+2\sqrt6s+6 = \left(s+\sqrt6\right)^2 \;\Longrightarrow\; I(s) = \frac{10}{\left(s+\sqrt6\right)^2} \]
\[ i(t) = 10t\,e^{-\sqrt6t} \]

The \(t\) factor is a repeated pole — Set 31, Problem 10. Nothing special had to be done: the partial-fraction rule for a double pole produced it automatically.

cUnderdamped, \(R = 2\ \Omega\). Discriminant \(4-24 = -20 < 0\):

\[ s^2+2s+6 = (s+1)^2+5 \;\Longrightarrow\; I(s) = \frac{10}{(s+1)^2+\left(\sqrt5\right)^2} \]
\[ i(t) = \frac{10}{\sqrt5}e^{-t}\sin\sqrt5t = 2\sqrt5\,e^{-t}\sin\sqrt5t \]

Poles at \(-1\pm j\sqrt5\): decay rate 1, ringing at \(\sqrt5 = 2.236\) rad/s.

The three cases side by side:

\(R\) (Ω)\(\zeta\)Poles\(i(t)\)
51.021\(-2, -3\)\(10(e^{-2t}-e^{-3t})\)
\(2\sqrt6\)1.000\(-\sqrt6\) (double)\(10te^{-\sqrt6t}\)
20.408\(-1\pm j\sqrt5\)\(2\sqrt5e^{-t}\sin\sqrt5t\)

using \(\zeta = R/(2\sqrt{L/C}) = R/(2\sqrt6)\). The natural frequency \(\omega_0 = \sqrt6 = 2.449\) rad/s is the same in all three — only the damping differs, which is Set 29's reading of pole geometry.

What has been avoided. Set 19 required identifying the case first, then selecting the matching general solution:

Set 19 approach\(s\)-domain approach
Compute \(\alpha\) and \(\omega_0\), compareWrite \(I(s)\) once
Choose from three solution formsFactor or complete the square
Apply two initial conditionsAlready included

The three "cases" are three ways a quadratic can factor, not three physical situations requiring different theory.

One expression, one denominator, three algebraic outcomes. The overdamped, critical and underdamped classification is a statement about a discriminant — and the \(s\)-domain method never needs to know which case applies until the moment of factoring.
AnswerAll from \(I(s) = 10/(s^2+Rs+6)\): \(R=5\) gives \(10(e^{-2t}-e^{-3t})\); \(R=2\sqrt6\) gives \(10te^{-\sqrt6t}\); \(R=2\) gives \(2\sqrt5e^{-t}\sin\sqrt5t\).
Problem 8Exam levelThévenin in s

Find the \(s\)-domain Thévenin equivalent of a 10 V step behind \(R_1 = 4\ \Omega\) with \(C = \tfrac12\) F shunting the output, and explain what \(\mathbf{Z}_{Th}(s)\) means physically.

Solution

The open-circuit voltage, by the divider rule of Set 3:

\[ V_{Th}(s) = \frac{10}{s}\cdot\frac{1/sC}{R_1+1/sC} = \frac{10}{s}\cdot\frac{2/s}{4+2/s} \]
\[ = \frac{10}{s(2s+1)} \]

The Thévenin impedance, with the source killed (short-circuited, as in Set 9):

\[ \mathbf{Z}_{Th}(s) = R_1\parallel\frac{1}{sC} = \frac{4\cdot(2/s)}{4+2/s} = \frac{4}{2s+1} \]

Not a resistance but a function of \(s\) — which is the whole difference from Part 1. It still behaves exactly as a Thévenin impedance should.

What it means, read at the two extremes:

Limit\(\mathbf{Z}_{Th}\)Interpretation
\(s\to0\)4 ΩAt DC the capacitor is open, leaving \(R_1\)
\(s\to\infty\)0Instantaneously the capacitor is a short

So the equivalent source has zero output impedance the instant a load is connected, rising to 4 Ω once everything settles — a fair description of a capacitor's stiffening effect on a supply, and a result no purely resistive equivalent could express.

Test it. Connect a load \(R_L = 4\ \Omega\) and find \(v_L(t)\):

\[ V_L(s) = V_{Th}\cdot\frac{R_L}{R_L+\mathbf{Z}_{Th}} = \frac{10}{s(2s+1)}\cdot\frac{4}{4+\dfrac{4}{2s+1}} \]
\[ = \frac{10}{s(2s+1)}\cdot\frac{2s+1}{2s+2} = \frac{10}{s(2s+2)} = \frac{5}{s(s+1)} \]
\[ v_L(t) = 5\left(1-e^{-t}\right)\ \text{V} \]

Check directly: the loaded circuit is a 10 V step behind 4 Ω charging \(C = \tfrac12\) F in parallel with 4 Ω. Final value \(10 \times 4/8 = 5\) V ✓; time constant \((4\parallel4)C = 2 \times 0.5 = 1\) s ✓.

The theorems that carry over, all of Part 1's:

Theorem\(s\)-domain form
Thévenin\(V_{Th}(s)\) in series with \(\mathbf{Z}_{Th}(s)\)
Norton\(I_N(s) = V_{Th}/\mathbf{Z}_{Th}\) in parallel
Maximum power transfer\(\mathbf{Z}_L = \mathbf{Z}_{Th}^*\) at each \(s = j\omega\) — Set 24
ReciprocityUnchanged for bilateral networks

The one requiring care is maximum power transfer, which is inherently a steady-state, single-frequency idea — it needs \(s = j\omega\) and the conjugate, so it does not generalise to arbitrary \(s\).

With stored energy present, the initial-condition sources are simply additional sources when finding \(V_{Th}\) — and are killed like any other source when finding \(\mathbf{Z}_{Th}\). Voltage sources short, current sources open, including the IC sources.

A Thévenin equivalent in \(s\) compresses an entire network's dynamics into two functions. The impedance is no longer a number but a description of how the source's stiffness varies with timescale — and it does so with the same two-element diagram that served in Part 1.
Answer\(V_{Th}(s) = 10/[s(2s+1)]\) and \(\mathbf{Z}_{Th}(s) = 4/(2s+1)\) — rising from 0 instantaneously to 4 Ω at DC. Loading with 4 Ω gives \(v_L = 5(1-e^{-t})\) V.
Problem 9ChallengeSuperposition in s

Use superposition to re-solve Problem 4, treating the applied source and each initial condition as a separate contribution, and comment on what the decomposition reveals.

Solution

Three sources act on the transformed circuit of Problem 4:

SourceValueOrigin
\(V_a\)\(10/s\)Applied step
\(V_b\)\(+2\)Inductor, \(Li(0^-)\)
\(V_c\)\(-4/s\)Capacitor, opposing

Since the loop impedance is the same in every case, each contribution is that source divided by \(\mathbf{Z}(s) = (s+2)(s+3)/s\).

Contribution of each:

\[ I_a = \frac{10/s}{(s+2)(s+3)/s} = \frac{10}{(s+2)(s+3)} \;\Longrightarrow\; 10e^{-2t}-10e^{-3t} \]
\[ I_b = \frac{2}{(s+2)(s+3)/s} = \frac{2s}{(s+2)(s+3)} \;\Longrightarrow\; -4e^{-2t}+6e^{-3t} \]
\[ I_c = \frac{-4/s}{(s+2)(s+3)/s} = \frac{-4}{(s+2)(s+3)} \;\Longrightarrow\; -4e^{-2t}+4e^{-3t} \]

Sum the three:

Contribution\(e^{-2t}\) coefficient\(e^{-3t}\) coefficient
Applied source+10−10
Inductor IC−4+6
Capacitor IC−4+4
Total+20
\[ i(t) = 2e^{-2t}\ \text{A}\;\checkmark \]

Matching Problem 4 exactly.

What the decomposition reveals. The \(e^{-3t}\) column is the interesting one: \(-10+6+4 = 0\). Each source individually excites the \(s = -3\) mode; their contributions cancel exactly.

The pole–zero cancellation of Problem 4 was not a single source failing to excite a mode — it was three sources exciting it in amounts that sum to zero. Problem 13 shows this is a designable condition.

Zero-state and zero-input, in Set 31, Problem 19's language:

GroupingTermsResult
Zero-state (applied source alone)\(I_a\)\(10e^{-2t}-10e^{-3t}\)
Zero-input (ICs alone)\(I_b+I_c\)\(-8e^{-2t}+10e^{-3t}\)

The zero-state response is precisely Problem 3's answer — the same circuit starting from rest. Superposition therefore says: a circuit with stored energy behaves as the at-rest circuit plus a source-free discharge.

When superposition is worth using here. For a single loop it is more work than direct KVL, but it earns its place when:

SituationBenefit
Several sources at different frequenciesEach handled separately — Set 11
Only the IC contribution is wantedKill the applied source
Diagnosing which source excites a modeExactly the table above
One source changes, others fixedRecompute one term
Superposition works on initial conditions because they are genuinely sources. Nothing distinguishes the inductor's \(Li(0^-)\) from an applied battery, so the principle of Set 11 applies to them without qualification — and the resulting table shows exactly which source is responsible for which natural mode.
AnswerContributions \(10e^{-2t}-10e^{-3t}\), \(-4e^{-2t}+6e^{-3t}\) and \(-4e^{-2t}+4e^{-3t}\) sum to \(2e^{-2t}\). The \(e^{-3t}\) terms cancel: all three sources excite that mode, in amounts totalling zero.
Problem 10CoreTransfer Function from a Circuit

Derive the transfer function of the running \(RLC\) circuit taken across the capacitor, and relate it to the standard second-order form of Sets 29 and 30.

Solution

Definition. A transfer function is defined with zero initial conditions:

\[ H(s) = \frac{V_{\text{out}}(s)}{V_{\text{in}}(s)}\bigg|_{\text{ICs}=0} \]

This restriction is essential. With stored energy present the output is not proportional to the input, so no single ratio describes the circuit — the IC contribution of Problem 9 would be there regardless of the input.

Apply the divider rule — the circuit is a single loop, so this is one line:

\[ H(s) = \frac{1/sC}{R+sL+1/sC} \]

Multiply top and bottom by \(s/L\):

\[ \boxed{\;H(s) = \frac{1/LC}{s^2+\dfrac{R}{L}s+\dfrac{1}{LC}}\;} \]

Compare with the standard form of Set 29:

\[ H(s) = \frac{\omega_0^2}{s^2+\dfrac{\omega_0}{Q}s+\omega_0^2} \]
ParameterCircuit expressionRunning values
\(\omega_0\)\(1/\sqrt{LC}\)\(\sqrt6 = 2.449\) rad/s
\(Q\)\(\dfrac{1}{R}\sqrt{\dfrac{L}{C}}\)\(\sqrt6/5 = 0.490\)
\(\zeta = 1/2Q\)\(\dfrac{R}{2}\sqrt{\dfrac{C}{L}}\)1.021

Set 29's \(Q\) formulas, derived rather than quoted. With \(R = 5\) the circuit is slightly overdamped, consistent with the real poles found in Problem 3.

Substituting the running values:

\[ H(s) = \frac{6}{s^2+5s+6} = \frac{6}{(s+2)(s+3)} \]
FeatureValueMeaning
Poles\(-2, -3\)Natural frequencies
ZerosNone finiteTwo at infinity
\(H(0)\)\(6/6 = 1\)Unity DC gain — capacitor takes the full source
\(H(\infty)\)0Low-pass, rolling off at \(-40\) dB/dec

The output terminals decide the filter type. Same circuit, three different transfer functions:

Output across\(H(s)\)Type
Capacitor\(\dfrac{1/LC}{D(s)}\)Low-pass
Inductor\(\dfrac{s^2}{D(s)}\)High-pass — double zero at origin
Resistor\(\dfrac{(R/L)s}{D(s)}\)Band-pass — one zero at origin

with \(D(s) = s^2+(R/L)s+1/LC\) throughout. The poles are a property of the network; the zeros are a property of where you measure. This is the single most useful structural fact in the set, and Problem 18 develops it.

Sanity check the band-pass claim via element behaviour:

FrequencyElements\(v_R\)
\(s\to0\)Capacitor open0 — no current
\(s = j\omega_0\)\(L\) and \(C\) cancelMaximum — full source across \(R\)
\(s\to\infty\)Inductor open0 — no current

Zero at both ends, peak in the middle — a band-pass, exactly as Set 29 described series resonance.

Three filters share one denominator, differing only in numerator. Set 30 chose pole positions to shape a response; here the same poles serve low-pass, high-pass and band-pass duty depending only on which pair of terminals is called the output — which is why the zeros, not the poles, determine the filter type.
Answer\(H(s) = (1/LC)/[s^2+(R/L)s+1/LC] = 6/[(s+2)(s+3)]\), giving \(\omega_0 = \sqrt6\) and \(Q = \frac1R\sqrt{L/C} = 0.490\). Taking the output across \(L\) or \(R\) instead gives high-pass or band-pass with the same poles.
Problem 11CoreImpulse and Step Response

Find the impulse and step responses of the running circuit's low-pass transfer function, and show how each is obtained from the other.

Solution

The impulse response is \(\mathcal{L}^{-1}\{H(s)\}\), since \(\mathcal{L}\{\delta\} = 1\):

\[ H(s) = \frac{6}{(s+2)(s+3)} = \frac{6}{s+2}-\frac{6}{s+3} \]
\[ \boxed{\;h(t) = 6\left(e^{-2t}-e^{-3t}\right)\ \text{V}\;} \]

Check: \(h(0) = 0\) ✓ — an impulse of voltage cannot instantaneously change the capacitor voltage, because the series inductor limits the current.

The step response is \(\mathcal{L}^{-1}\{H(s)/s\}\):

\[ \frac{H(s)}{s} = \frac{6}{s(s+2)(s+3)} = \frac{1}{s}-\frac{3}{s+2}+\frac{2}{s+3} \]
\[ \boxed{\;a(t) = 1-3e^{-2t}+2e^{-3t}\;} \]

This is Problem 3's \(v_C(t)\) divided by 10 — as it must be, since that was the response to a 10 V step.

The two are related by calculus, in either direction:

\[ a(t) = \int_0^th(\tau)\,d\tau, \qquad h(t) = \frac{da}{dt} \]

Verify by differentiating:

\[ \frac{da}{dt} = 6e^{-2t}-6e^{-3t} = h(t)\;\checkmark \]

In the \(s\)-domain this is just the factor \(1/s\) of Set 31, Problem 6 — integration in time is division by \(s\), and the step is the integral of the impulse.

Useful checks on both:

CheckValueMeaning
\(\displaystyle\int_0^\infty h\,dt\)\(6/2-6/3 = 1\)\(= H(0)\), the DC gain ✓
\(a(\infty)\)1Same quantity ✓
\(a(0)\)\(1-3+2 = 0\)Capacitor starts uncharged ✓
\(h\) peak0.889 at \(t = 0.406\) sSteepest point of \(a(t)\)

The area under the impulse response equals the DC gain. This follows directly from \(H(0) = \int_0^\infty h\,e^{0}dt\) and is one of the quickest sanity checks available.

Why the impulse response is the fundamental one. By the convolution theorem (Set 31, Problem 12), \(h(t)\) determines the response to every input:

\[ v_{\text{out}}(t) = \int_0^th(\tau)v_{\text{in}}(t-\tau)\,d\tau \]

In practice, though, the step response is what gets measured — an impulse is hard to generate and the resulting signal is small. Measure the step response, differentiate to get \(h\), transform to get \(H\).

Rise time, using Set 28, Problem 19:

\[ a(t) = 0.1 \ \text{at} \ t = 0.218\ \text{s}; \qquad a(t) = 0.9 \ \text{at} \ t = 1.631\ \text{s} \]
\[ t_r = 1.413\ \text{s} \]

With the dominant pole at \(-2\), a first-order circuit of the same time constant would give \(2.2\tau = 1.1\) s. The true rise time is 28% longer, because the second pole at \(-3\) adds its own lag. A dominant-pole estimate is optimistic about the rise even when it is accurate about the tail (Set 31, Problem 14) — the extra poles cannot speed anything up.

Impulse response, step response and transfer function are three descriptions of one thing. Differentiate, integrate, or transform to move between them — and the choice of which to use is decided by what is easiest to measure, not by what is mathematically primary.
Answer\(h(t) = 6(e^{-2t}-e^{-3t})\) and \(a(t) = 1-3e^{-2t}+2e^{-3t}\), with \(h = da/dt\). The area under \(h\) is 1, equal to \(H(0)\).
Problem 12Exam levelSwitched Circuits

A 10 V source is applied to an \(RC\) circuit (\(\tau = 1\) s) at \(t=0\) and removed at \(t=2\) s. Solve it in two ways — stage by stage, and in one shot — and compare.

Solution

aThe stage-by-stage method, as in Set 18.

Stage 1 \((0 \le t < 2)\) — charging from zero:

\[ v_C(t) = 10\left(1-e^{-t}\right) \]
\[ v_C(2) = 10\left(1-e^{-2}\right) = 8.6466\ \text{V} \]

Stage 2 \((t \ge 2)\) — this value becomes the new initial condition, and the source is now zero:

\[ v_C(t) = 8.6466\,e^{-(t-2)} \]

Correct, but note what was required: solve, evaluate at the switching instant, restart the problem. With three or four switching events this bookkeeping becomes the dominant labour and the main source of error.

bThe one-shot method, using the delay theorem (Set 31, Problem 7). Describe the whole input as a single function:

\[ v_{\text{in}}(t) = 10\left[u(t)-u(t-2)\right] \;\Longrightarrow\; V_{\text{in}}(s) = \frac{10}{s}\left(1-e^{-2s}\right) \]
\[ V_C(s) = \frac{10\left(1-e^{-2s}\right)}{s(1+s)} \]

Invert the exponential-free part first:

\[ \mathcal{L}^{-1}\left\{\frac{10}{s(1+s)}\right\} = 10\left(1-e^{-t}\right) \equiv g(t) \]

Then apply the delay theorem to the second piece:

\[ \boxed{\;v_C(t) = g(t)\,u(t)-g(t-2)\,u(t-2)\;} \]

One expression, valid for all \(t\). The switching instant never had to be treated as a separate problem.

Verify the two agree:

\(t\) (s)Stage methodOne-shot
2.08.64668.6466
2.55.24455.2445
3.03.18093.1809
4.01.17021.1702
5.00.43050.4305

Identical to four decimals. The delay theorem has absorbed the stage-two initial condition automatically\(-g(t-2)\) encodes exactly the discharge from whatever level had been reached.

Why the second stage decays from 8.65 V and not 10 V. The pulse lasts only \(2\tau\), so the capacitor reaches \(1-e^{-2} = 86.5\%\) of the source:

Pulse widthPeak reached
\(0.5\tau\)39.3%
\(\tau\)63.2%
\(2\tau\)86.5%
\(5\tau\)99.3%

When each method wins:

SituationBetter method
One switching event, simple circuitStage by stage — more intuitive
Several switching eventsDelay theorem
Periodic switchingPeriodic transform — Set 31, Problem 17
The circuit itself changes at the switchStage by stage — \(H(s)\) is different in each stage

The last row is the real limitation. The delay theorem handles a changing input to a fixed network. If the switch alters the topology, each configuration has its own \(H(s)\) and the stages must be solved separately, carrying the state across.

A switched source is not a sequence of problems but one problem with an unusual input. Writing the input as a sum of delayed steps converts every switching instant into an exponential factor — and the initial condition for each stage then emerges from the algebra instead of being computed by hand.
Answer\(v_C(t) = g(t)u(t)-g(t-2)u(t-2)\) with \(g(t) = 10(1-e^{-t})\). Peak 8.6466 V at \(t=2\) s, then decaying — identical to the two-stage result at every point.
Problem 13ChallengeExciting One Mode

Explain the pole–zero cancellation of Problem 4, find the general condition for it, and find the initial conditions that would silence the other mode instead.

Solution

Write the current with general initial conditions. For the running circuit with source \(V_0u(t)\):

\[ I(s) = \frac{\dfrac{V_0}{s}+Li_0-\dfrac{v_0}{s}}{\dfrac{(s+2)(s+3)}{s}} = \frac{Li_0\,s+\left(V_0-v_0\right)}{(s+2)(s+3)} \]

The numerator is a first-order polynomial in \(s\) whose coefficients are set entirely by the initial conditions and the source.

Locate its zero:

\[ Li_0\,s+\left(V_0-v_0\right) = 0 \;\Longrightarrow\; s_z = -\frac{V_0-v_0}{Li_0} \]

The initial conditions place a zero. If that zero lands on a pole, the corresponding natural mode is cancelled and never appears in the response.

The condition for silencing each mode. With \(L = 1\), \(V_0 = 10\), \(v_0 = 4\):

\[ s_z = -\frac{6}{i_0} \]
To cancelNeed \(s_z =\)Required \(i_0\)Resulting \(i(t)\)
Pole at \(-3\)\(-3\)2 A\(2e^{-2t}\)
Pole at \(-2\)\(-2\)3 A\(3e^{-3t}\)

Problem 4 used \(i_0 = 2\) A, so it silenced the fast mode. With \(i_0 = 3\) A instead, the response is \(3e^{-3t}\) — a purely fast decay from a second-order circuit.

Verify the second case from scratch:

\[ I(s) = \frac{3s+6}{(s+2)(s+3)} = \frac{3(s+2)}{(s+2)(s+3)} = \frac{3}{s+3} \]
\[ i(t) = 3e^{-3t}\ \text{A} \]

Check: \(i(0^+) = 3\) A ✓, matching the stated initial current.

What this means physically. A natural mode is a particular pattern of energy exchange between \(L\) and \(C\):

SituationResult
Initial state matches one mode's patternOnly that mode is excited
Initial state is a general oneBoth modes appear
Initial state is orthogonal to a modeThat mode stays silent

The special initial conditions are eigenvector-like: they set the circuit going in a state that decays without changing shape. Every other starting state is a mixture of the two.

A caution — this is cancellation, not removal. The pole is still there:

QuestionAnswer
Is the circuit still second order?Yes — two energy-storage elements
Does \(H(s)\) still have both poles?Yes\(H\) is IC-independent
Would a different input excite the mode?Yes
Is the mode gone?No — merely unexcited

The cancellation is a property of this particular excitation, not of the network. Perturb the initial current by 1% and the \(e^{-3t}\) term reappears in proportion.

Where this matters in practice. The same mathematics appears whenever a zero is placed on a pole:

ApplicationUse
Control compensatorsA lead network's zero cancels a slow plant pole
Input shapingCommand profiles chosen to leave a resonance unexcited
Ringing suppressionPre-charging a node so the transient never starts

All are fragile in the same way: cancellation requires exact matching, and component tolerance or drift resurrects the mode — Set 30, Challenge C3's lesson in a different guise.

Initial conditions do not merely scale the response, they place a zero. A second-order circuit can be made to behave as first-order by choosing the stored energy to match one natural mode exactly — but the missing mode is dormant rather than absent, and the smallest mismatch brings it back.
AnswerThe ICs place a zero at \(s_z = -(V_0-v_0)/Li_0\). With \(i_0 = 2\) A it lands on \(-3\), giving \(i = 2e^{-2t}\); with \(i_0 = 3\) A it lands on \(-2\), giving \(i = 3e^{-3t}\). The mode is unexcited, not removed.
Problem 14CoreEndpoints from the Circuit

Show how to obtain \(t = 0^+\) and \(t = \infty\) values by inspecting the circuit rather than the algebra, and use it as a check on Problems 3, 4 and 6.

Solution

The correspondence. The initial and final value theorems relate \(s\) limits to \(t\) limits, and the impedances have simple limits:

Element\(s\to\infty\)\(t\to0^+\)\(s\to0\)\(t\to\infty\)
Resistor \(R\)\(R\)\(R\)
Inductor \(sL\)OpenShort
Capacitor \(1/sC\)ShortOpen

These are Set 18's rules, now derived. An inductor opposes sudden current change (open at \(t=0^+\)) but passes DC freely (short at \(t=\infty\)); the capacitor does the reverse.

The important qualification. These apply to elements with no stored energy. With initial conditions:

Element at \(t=0^+\)Model
Inductor with \(i(0^-)\)Current source of \(i(0^-)\)
Capacitor with \(v(0^-)\)Voltage source of \(v(0^-)\)

The uncharged cases are the special instances with source value zero — an inductor carrying no current is an open circuit, and an uncharged capacitor is a short.

Apply to Problem 3 (at rest, 10 V step):

InstantCircuit becomesPredictionAlgebra gave
\(t=0^+\)\(L\) open\(i=0\), \(v_C=0\)0, 0 ✓
\(t=\infty\)\(C\) open\(i=0\), \(v_C=10\)0, 10 ✓

Apply to Problem 4 (energised):

InstantCircuit becomesPredictionAlgebra gave
\(t=0^+\)\(L\) → 2 A source; \(C\) → 4 V source\(i=2\), \(v_C=4\)2, 4 ✓
\(t=\infty\)\(C\) open\(i=0\), \(v_C=10\)0, 10 ✓

Note the final values are the same in Problems 3 and 4. Initial conditions affect how a circuit gets there, never where it ends up — the final state is set by the sources and the topology alone.

Apply to Problem 6 (parallel, 4 A step) — the case that catches people out:

InstantReasoningResult
\(t=0^+\)\(C\) shorts the node\(v=0\) ✓
\(t=\infty\)\(L\) shorts the node\(v=0\) ✓, all current in \(L\)

Two seconds of inspection would have prevented the natural but wrong guess that \(v(\infty) = IR = 8\) V.

Use it as a working discipline:

StepAction
1Before solving, sketch the \(t=0^+\) and \(t=\infty\) circuits
2Read off both endpoint values
3Solve in the \(s\)-domain
4Confirm the answer hits both

Doing step 1 first matters. Predictions made after seeing the answer tend to agree with it.

Two degenerate circuits, drawn in seconds, verify both ends of an answer that took several minutes to compute. The endpoints are where sign errors and reversed initial-condition sources announce themselves, and they cost almost nothing to check.
AnswerAt \(t=0^+\): \(L\) open (or a current source \(i(0^-)\)), \(C\) short (or a voltage source \(v(0^-)\)). At \(t=\infty\): \(L\) short, \(C\) open. All three problems check out.
Problem 15Exam levelCoupled Inductors

Write the \(s\)-domain equations for coupled inductors, including initial currents, and find the reflected impedance.

Solution

The time-domain equations, from Set 26, with the sign set by the dot convention:

\[ v_1 = L_1\frac{di_1}{dt} \pm M\frac{di_2}{dt}, \qquad v_2 = \pm M\frac{di_1}{dt}+L_2\frac{di_2}{dt} \]

Transforming term by term:

\[ V_1 = sL_1I_1 \pm sMI_2 - \left[L_1i_1(0^-) \pm Mi_2(0^-)\right] \]
\[ V_2 = \pm sMI_1+sL_2I_2 - \left[\pm Mi_1(0^-)+L_2i_2(0^-)\right] \]

The mutual term brings its own initial-condition source. A current in coil 2 contributes flux linkage to coil 1, so it appears in coil 1's initial-condition term — an effect with no counterpart in uncoupled circuits.

In matrix form, the transformed circuit is

\[ \begin{bmatrix}V_1\\V_2\end{bmatrix} = \begin{bmatrix}sL_1 & \pm sM\\ \pm sM & sL_2\end{bmatrix} \begin{bmatrix}I_1\\I_2\end{bmatrix} - \begin{bmatrix}L_1i_1(0^-) \pm Mi_2(0^-)\\ \pm Mi_1(0^-)+L_2i_2(0^-)\end{bmatrix} \]

The impedance matrix is symmetric, as Set 26, Problem 8 required — and the check applies just as forcefully here. An asymmetric off-diagonal pair means an error, since \(M_{12} = M_{21}\) for any passive coupled network.

Reflected impedance. With a load \(\mathbf{Z}_L\) on the secondary and no initial energy, the secondary loop gives

\[ 0 = \pm sMI_1+\left(sL_2+\mathbf{Z}_L\right)I_2 \;\Longrightarrow\; I_2 = \frac{\mp sMI_1}{sL_2+\mathbf{Z}_L} \]

Substituting into the primary equation:

\[ \boxed{\;\mathbf{Z}_{\text{in}}(s) = sL_1+\frac{\left(sM\right)^2}{sL_2+\mathbf{Z}_L}\;} \]

The sign of \(M\) has disappeared — it is squared. Set 26 found the same: the dot convention affects individual voltages but never the input impedance, because the coupling is traversed twice.

A worked case. Take \(L_1 = L_2 = 1\) H, \(M = 0.5\) H, \(\mathbf{Z}_L = 1\ \Omega\):

\[ \mathbf{Z}_{\text{in}}(s) = s+\frac{0.25s^2}{s+1} = \frac{s^2+s+0.25s^2}{s+1} = \frac{1.25s^2+s}{s+1} \]
Limit\(\mathbf{Z}_{\text{in}}\)Interpretation
\(s\to0\)0Both inductors short at DC
\(s\to\infty\)\(1.25s\)Behaves as \(L_1+M^2/L_2 = 1.25\) H

At high frequency the secondary current is limited by \(sL_2\) rather than \(\mathbf{Z}_L\), so the reflected term becomes the constant \(M^2/L_2\). Note this makes the effective inductance larger, because the reflected impedance adds here.

The T-equivalent of Set 26 transfers unchanged:

ArmImpedance
Primary series\(s(L_1-M)\)
Shunt\(sM\)
Secondary series\(s(L_2-M)\)

This removes the coupling entirely, leaving three ordinary inductors — after which mesh and nodal analysis apply without any special treatment of the mutual term. Usually the easier route for a circuit with more than two meshes.

Coupling adds nothing new to the \(s\)-domain method — only off-diagonal entries and their initial-condition sources. Every result of Set 26 carries over by writing \(s\) for \(j\omega\), and gains the transient behaviour that the phasor treatment could not reach.
AnswerImpedance matrix \(\begin{bmatrix}sL_1 & \pm sM\\ \pm sM & sL_2\end{bmatrix}\) with IC sources \(L_1i_1(0^-)\pm Mi_2(0^-)\) and its dual. Reflected impedance \((sM)^2/(sL_2+\mathbf{Z}_L)\), independent of the dot convention.
Problem 16Exam levelOp-Amp Circuits

Derive the transfer functions of the inverting op-amp integrator and first-order low-pass in the \(s\)-domain, and design one for a 159 Hz cut-off with a gain of 10.

Solution

The general inverting configuration. With an ideal op-amp the inverting input is a virtual earth, so Set 12's result applies with impedances in place of resistances:

\[ H(s) = -\frac{\mathbf{Z}_f(s)}{\mathbf{Z}_i(s)} \]

One formula covers every inverting op-amp circuit. Choosing \(\mathbf{Z}_f\) and \(\mathbf{Z}_i\) is the whole design problem.

aThe integrator — feedback capacitor, input resistor:

\[ H(s) = -\frac{1/sC_f}{R_i} = -\frac{1}{sR_iC_f} \]

A pole at the origin, gain falling at \(-20\) dB/dec — the ideal integrator of Set 28, Problem 4. But the pole is exactly on the imaginary axis, which by Set 31, Problem 15 is marginally stable: any DC input, or the op-amp's own input offset, integrates without limit until the output saturates.

bThe practical version puts \(R_f\) across the capacitor to bound the DC gain:

\[ \mathbf{Z}_f = R_f\parallel\frac{1}{sC_f} = \frac{R_f}{1+sR_fC_f} \]
\[ \boxed{\;H(s) = -\frac{R_f/R_i}{1+sR_fC_f}\;} \]
FeatureValue
DC gain\(-R_f/R_i\)
Pole\(s = -1/R_fC_f\)
Behaviour above the poleIntegrates
Behaviour below the poleConstant gain

The pole has moved off the axis into the left half-plane, which is exactly what makes the circuit usable. It is a first-order low-pass that happens to integrate at high frequencies.

cThe design. For gain 10 and \(f_c = 159\) Hz:

\[ \frac{R_f}{R_i} = 10; \qquad \omega_c = \frac{1}{R_fC_f} = 2\pi(159) = 1000\ \text{rad/s} \]

Choose \(R_f = 100\) kΩ (a convenient value that keeps currents small):

\[ R_i = 10\ \text{k}\Omega, \qquad C_f = \frac{1}{(10^5)(10^3)} = 10\ \text{nF} \]
\[ H(s) = \frac{-10\,000}{s+1000} \]

Check: \(H(0) = -10\) ✓, pole at \(-1000\) rad/s \(= 159.2\) Hz ✓.

Swapping the elements gives the differentiator — input capacitor, feedback resistor:

\[ H(s) = -\frac{R_f}{R_i+1/sC_i} = -\frac{sR_fC_i}{1+sR_iC_i} \]

A zero at the origin and a pole at \(-1/R_iC_i\)a high-pass. The series \(R_i\) is essential: without it the gain would rise indefinitely with frequency, amplifying noise and inviting instability. Every practical differentiator is band-limited.

What the ideal op-amp assumption costs. A real device has finite gain-bandwidth product, adding a pole of its own:

AssumptionConsequence when it fails
Infinite open-loop gainDC gain slightly below \(-R_f/R_i\)
Infinite bandwidthExtra pole — the design becomes second order
Zero output impedanceLoading interacts with \(\mathbf{Z}_f\)

The second is the one that bites. It is also what limits Set 30's Sallen–Key sections at high \(Q\) — the amplifier's own pole conspires with the intended ones.

Active circuits need no new theory in the \(s\)-domain — only \(H = -\mathbf{Z}_f/\mathbf{Z}_i\). The op-amp's real contribution is that it lets a designer place poles using resistors and capacitors alone, which is what made Set 30's inductorless filters possible.
Answer\(H = -\mathbf{Z}_f/\mathbf{Z}_i\). Integrator: \(-1/sR_iC_f\), marginally stable. Practical version: \(-(R_f/R_i)/(1+sR_fC_f)\). Design: \(R_f = 100\) kΩ, \(R_i = 10\) kΩ, \(C_f = 10\) nF gives \(-10\,000/(s+1000)\).
Problem 17CoreNetwork Functions

Classify the network functions of a two-port, and distinguish driving-point from transfer functions using the running circuit.

Solution

A network function is any ratio of a transformed response to a transformed excitation, with zero initial conditions. They divide into two families:

FamilyMeasuredExamples
Driving-pointAt the same pair of terminals\(\mathbf{Z}(s)\), \(\mathbf{Y}(s)\)
TransferAt a different pair\(V_2/V_1\), \(I_2/I_1\), \(V_2/I_1\), \(I_2/V_1\)

The four transfer types are voltage gain, current gain, transfer impedance and transfer admittance. All are dimensionally distinct and none should be called simply "the transfer function" without saying which.

The driving-point impedance of the running circuit, seen from the source:

\[ \mathbf{Z}(s) = \frac{(s+2)(s+3)}{s} \]
FeatureLocationPhysical meaning
Zeros of \(\mathbf{Z}\)\(-2, -3\)Natural frequencies — current flows with no applied voltage
Pole of \(\mathbf{Z}\)\(0\)Capacitor blocks DC — infinite impedance

A zero of a driving-point impedance is a short-circuit natural frequency. At \(s = -2\) the loop can sustain a current of the form \(e^{-2t}\) with the terminals shorted — which is precisely what Problems 4 and 13 observed.

The admittance is the reciprocal, so poles and zeros exchange:

\[ \mathbf{Y}(s) = \frac{s}{(s+2)(s+3)} \]

Its poles are now at \(-2\) and \(-3\). This is why Problem 6's parallel circuit took its natural frequencies from the numerator of \(\mathbf{Y}\) while Problem 3's series circuit took them from the numerator of \(\mathbf{Z}\)the same physical frequencies, appearing in whichever function the topology makes convenient.

Properties of driving-point functions of passive networks, which act as strong checks:

PropertyReason
Poles and zeros in the closed LHPPassive networks cannot generate energy
Poles and zeros alternate on the axis for \(LC\) networksFoster's reactance theorem
\(\text{Re}\,\mathbf{Z}(j\omega) \ge 0\) for all \(\omega\)A passive network absorbs power
Degrees of numerator and denominator differ by at most 1Element behaviour at \(s\to\infty\)

A function satisfying all of these is called positive real, and it is exactly the condition for a rational function to be realisable as a passive network — the foundation of network synthesis.

Transfer functions are less constrained. Their zeros may sit anywhere, including the right half-plane:

PolesZeros
Driving-pointClosed LHPClosed LHP
TransferClosed LHPAnywhere

Right-half-plane zeros give the non-minimum-phase behaviour of Set 28, Challenge C3 — extra phase lag with no magnitude penalty, and an initial undershoot in the step response. A passive network can have them; a passive driving-point impedance cannot.

Why the poles are shared. Every network function of a given network has the same denominator, because it comes from the same determinant:

\[ \text{any function} = \frac{\text{cofactor}}{\Delta(s)} \]

as Problem 5's mesh determinant showed. Poles belong to the network; zeros belong to the particular input–output pair chosen. Problem 18 turns this into a design observation.

One network, many functions, one set of poles. Which function is quoted depends entirely on what is being driven and what is being measured — and confusing a driving-point impedance with a transfer impedance is a real error, since only the former is constrained to be positive real.
AnswerDriving-point functions relate voltage and current at the same terminals; transfer functions relate different terminals. For the running circuit \(\mathbf{Z}(s) = (s+2)(s+3)/s\) — its zeros are the natural frequencies. All network functions of one network share a denominator.
Problem 18ChallengePoles, Zeros and Topology

Show that the three outputs of a series \(RLC\) circuit have transfer functions summing to unity, and explain what this says about poles, zeros and filter type.

Solution

The three transfer functions, all with denominator \(D(s) = s^2+(R/L)s+1/LC\):

OutputNumeratorZerosType
Across \(C\)\(1/LC\)Two at \(\infty\)Low-pass
Across \(L\)\(s^2\)Double at originHigh-pass
Across \(R\)\((R/L)s\)One at origin, one at \(\infty\)Band-pass

Add them:

\[ H_C+H_L+H_R = \frac{\dfrac{1}{LC}+s^2+\dfrac{R}{L}s}{s^2+\dfrac{R}{L}s+\dfrac{1}{LC}} = 1 \]

Exactly unity, at every frequency. The reason is KVL: the three element voltages must sum to the source voltage at every instant, so their transfer functions must sum to 1. The numerators are forced to be the terms of the denominator.

Verify with the running values (\(R=5\), \(L=1\), \(C=\tfrac16\)):

\[ \frac{6}{s^2+5s+6}+\frac{s^2}{s^2+5s+6}+\frac{5s}{s^2+5s+6} = \frac{s^2+5s+6}{s^2+5s+6} = 1\;\checkmark \]
Output\(H(0)\)\(H(\infty)\)
Across \(C\)10
Across \(L\)01
Across \(R\)00
Sum11

At DC the capacitor takes the whole source; at high frequency the inductor does; and the resistor takes it only in between. The three filters partition the source voltage.

The structural lesson, which Set 30 relied on without stating:

Determined byFeature
The network (element values, topology)Poles — \(\omega_0\), \(Q\), damping, settling time
Where you measureZeros — filter type, DC and HF gain

This is why Set 30's low-pass-to-high-pass transformation left the order unchanged: it moved zeros, not poles. Choosing a filter family is choosing poles; choosing a filter type is choosing zeros.

What zeros do to the response. Poles alone give a sum of decaying exponentials; zeros determine how those exponentials are weighted:

Zero locationEffect
At the originBlocks DC — removes the steady-state term
At infinityRolls off — limits high-frequency response
On a poleCancels that mode — Problem 13
Near a poleReduces that mode's residue
In the RHPInitial undershoot; extra phase lag

The fourth row is the practical one: a zero near a pole makes that mode's contribution small without eliminating it, which is how a real compensator works when exact cancellation is unattainable.

Counting poles from the circuit. The number of poles equals the number of independent energy-storage elements:

CircuitPoles
Single \(RC\) or \(RL\)1
Series or parallel \(RLC\)2
Two capacitors in parallel1 — not independent
Capacitor loop with no resistanceReduced count

"Independent" matters. Two capacitors directly in parallel combine into one, so a circuit's order can be lower than its element count suggests — which is why the order is properly read from the denominator degree rather than counted on the diagram.

The poles are the circuit; the zeros are the question you ask of it. One \(RLC\) loop provides a low-pass, a high-pass and a band-pass simultaneously, with identical \(\omega_0\) and \(Q\) — and the three responses sum to the source, because KVL leaves them no choice.
Answer\(H_C+H_L+H_R = 1\) identically, forced by KVL. Poles are set by the network; zeros by the measurement point — which is why one circuit yields three filter types with the same \(\omega_0\) and \(Q\).
Problem 19ChallengeWhy Part 1 Survives

Audit the claim that every technique of Part 1 transfers to the \(s\)-domain, identifying any that need qualification.

Solution

What the techniques actually rest on. Every method in Sets 3 to 12 was built from exactly three ingredients:

\[ \text{KVL} + \text{KCL} + \left(V = \mathbf{Z}I \text{ for each element}\right) \]

KVL and KCL are statements about charge conservation and the single-valuedness of potential; they hold instant by instant, and the transform is linear, so they hold for transformed quantities too. Problem 1 supplied the third. Therefore the methods must transfer — the only question is whether any of them used something extra.

The audit:

TechniqueSetTransfers?Note
Series–parallel reduction3Same rules
Voltage and current dividers3Problem 8 used it
Mesh analysis4Problem 5
Nodal analysis5Problem 6
Supermesh and supernode6, 7Unchanged
Source transformation8Problem 2 relied on it
Thévenin and Norton9, 10Problem 8
Superposition11Problem 9 — extends to ICs
Dependent sources12Coefficients may be functions of \(s\)
ReciprocityBilateral networks only, as before
Maximum power transfer24QualifiedSee below
Star–delta3But the result may not be realisable

The genuine qualification: maximum power transfer. Set 24 established \(\mathbf{Z}_L = \mathbf{Z}_{Th}^*\), and the conjugate is the difficulty:

\[ \mathbf{Z}_{Th}^*(j\omega) \ \text{is defined; } \ \mathbf{Z}_{Th}^*(s) \ \text{is not} \]

Conjugation is an operation on the imaginary axis. Average power is inherently a steady-state, single-frequency concept — it requires a settled sinusoid, so it belongs to \(s = j\omega\) and does not generalise to arbitrary \(s\). For a transient, one computes energy by integrating \(vi\), and there is no simple matching condition.

The star–delta caveat is subtler and worth noting. The transformation is algebraically valid:

\[ \mathbf{Z}_a = \frac{\mathbf{Z}_1\mathbf{Z}_2}{\mathbf{Z}_1+\mathbf{Z}_2+\mathbf{Z}_3} \]

but the resulting \(\mathbf{Z}_a(s)\) may not correspond to any physical \(R\), \(L\) or \(C\) combination — it can require a negative element. As a computational device it is fine; as a physical equivalent it may not be buildable. The same reservation applied in Set 3 whenever a negative resistance appeared.

What is genuinely new, as against merely inherited:

New capabilitySource
Initial conditions handled as sourcesProblem 2
Arbitrary inputs, not just DC or sinusoidsProblem 12
Transient and steady state in one calculationProblem 4
Stability visible from the denominatorProblem 17
Filter type read from the zerosProblem 18

Every one of these is a consequence of the element models, not of a new circuit principle. The physics did not change; the algebra did.

The practical upshot. A student who can analyse a resistive network can analyse any linear circuit:

\[ \text{transform the elements} \to \text{solve as resistive} \to \text{invert} \]

with the difficulty concentrated in the last step — partial fractions — rather than in the circuit analysis. That is a considerable simplification over Sets 18 and 19, where each new topology required its own differential equation.

Part 1 was never about resistors; it was about KVL, KCL and Ohm's law. Those three survive any change of variable that preserves linearity, which is why sixteen sets of technique carry over to the \(s\)-domain with exactly one genuine exception — maximum power transfer, and only because average power is a steady-state idea.
AnswerAll of Part 1 transfers, since the methods used only KVL, KCL and \(V=\mathbf{Z}I\). The one real exception is maximum power transfer, whose conjugate condition is defined only on \(s=j\omega\). Star–delta transfers algebraically but may not yield realisable elements.
Problem 20ChallengeWhat Has Been Unified

Draw together what Sets 31 and 32 have achieved, and identify what the remaining sets must supply.

Solution

The method, complete:

StepActionProblem
1Replace each element by its impedance1
2Add a source for each initial condition2
3Solve by any Part 1 method5, 6, 8, 9
4Invert by partial fractionsSet 31
5Check the endpoints against the circuit14

Only step 4 involves anything the earlier sets did not already contain.

What the two sets together have replaced:

Earlier methodNow
Set 18: first-order transients by \(\tau\) and endpointsA single pole
Set 19: three damping cases, separately treatedThree ways a quadratic factors — Problem 7
Set 20: phasors for the steady state\(s = j\omega\), valid when stable
Sets 28–30: \(H(j\omega)\) and filter designPole and zero placement — Problem 18

Four separate bodies of technique, reduced to one. They were never different subjects — they were the same rational function examined on different parts of the \(s\)-plane.

The recurring structural facts, worth carrying forward:

FactWhere established
Poles belong to the network; zeros to the measurementProblem 18
Initial conditions place a zeroProblem 13
Final values are IC-independentProblem 14
All network functions share a denominatorProblem 17
Stored energy is indistinguishable from a sourceProblem 2

What remains unaddressed. Two gaps, both genuine:

GapWhy it matters
Periodic inputsSet 31, Problem 17 gave \(F_1/(1-e^{-sT_p})\) — a transcendental factor that resists inversion
Cascading with loadingSet 28, Problem 14 found a cascade is not the product of its parts — \(1+3sT+(sT)^2\), not \((1+sT)^2\)

The first is a computational obstacle: Laplace establishes that a square wave has poles at the odd harmonics but gives no practical route to the response. The second is worse — it means \(H(s)\) for a two-stage circuit cannot be found by multiplying the stages.

The remaining programme:

SetTopicSupplies
33Fourier seriesPeriodic inputs, one harmonic at a time
34Fourier transformWhy bandwidth and duration are reciprocal
35Two-port networksCascades handled exactly, loading included

Set 33 attacks the first gap by abandoning the closed form: a periodic input becomes a sum of sinusoids, each handled by the phasor method that Set 31, Problem 16 has now justified. Set 35 closes the second by characterising a network with four parameters instead of one, so that loading is accounted for rather than assumed away.

Transform the elements and the circuit becomes resistive. That single move absorbed transient analysis, steady-state analysis and filter theory into one procedure — and the price was only that impedances became polynomials and the last step became partial fractions.
AnswerFive steps, of which only partial fractions is new. Sets 18, 19, 20 and 28–30 all become one method. What remains is periodic inputs (Set 33) and cascades with loading (Set 35).
Practice

Practice Problems

Work each on paper before opening the answer. The answer is given so you can check yourself; the method is deliberately not.

  1. P1. Give the \(s\)-domain impedance of a 2 H inductor and a 5 µF capacitor.

    Show answer
    \(2s\) and \(1/(5\times10^{-6}s) = 2\times10^5/s\) — Problem 1.
  2. P2. A 0.5 H inductor carries 4 A at \(t=0^-\). Give both source models.

    Show answer
    Series voltage \(Li(0^-) = 2\) V, or parallel current \(4/s\) A — Problem 2.
  3. P3. A 10 µF capacitor is charged to 50 V. Give both source models.

    Show answer
    Series voltage \(50/s\), or parallel current \(Cv(0^-) = 5\times10^{-4}\) A — Problem 2.
  4. P4. Find \(\mathbf{Z}(s)\) for \(R = 3\ \Omega\), \(L = 1\) H and \(C = \tfrac12\) F in series.

    Show answer
    \(3+s+2/s = (s^2+3s+2)/s = (s+1)(s+2)/s\) — Problem 1.
  5. P5. What are the natural frequencies of that circuit?

    Show answer
    \(-1\) and \(-2\) — the zeros of \(\mathbf{Z}(s)\) — Problem 17.
  6. P6. At \(t=0^+\) what does an uncharged capacitor look like? And at \(t=\infty\)?

    Show answer
    Short circuit, then open circuit — Problem 14.
  7. P7. A parallel \(RL\) circuit is driven by a DC current source. What is the final voltage?

    Show answer
    Zero — the inductor is a short at DC and takes all the current — Problem 6.
  8. P8. Write \(H(s)\) for an \(RC\) low-pass with output across the capacitor.

    Show answer
    \((1/sC)/(R+1/sC) = 1/(1+sRC)\) — Problem 10.
  9. P9. Taking the output across \(L\) in a series \(RLC\), where are the zeros?

    Show answer
    A double zero at the origin, giving a high-pass — Problem 18.
  10. P10. If \(H(s) = 4/[(s+1)(s+4)]\), what is the impulse response?

    Show answer
    \(h(t) = \frac43(e^{-t}-e^{-4t})\), with area \(H(0) = 1\) — Problem 11.
  11. P11. Find \(\mathbf{Z}_{Th}(s)\) looking into a 2 Ω resistor in parallel with a 1 H inductor.

    Show answer
    \(2s/(2+s)\) — zero at DC (inductor shorts), tending to 2 Ω at high frequency — Problem 8.
  12. P12. Which Part 1 theorem does not generalise to arbitrary \(s\)?

    Show answer
    Maximum power transfer — the conjugate \(\mathbf{Z}_{Th}^*\) is defined only on \(s = j\omega\) — Problem 19.
Challenge

Challenge Problems

Each needs an idea rather than a formula. Decide what the governing principle is before opening the answer.

  1. C1. Two identical \(RC\) low-pass sections (\(R = 1\ \Omega\), \(C = 1\) F) are cascaded directly. Show that \(H(s) \ne 1/(1+s)^2\), find the true result, and quantify what the error costs.

    Show answer
    The naive answer assumes each section is unaffected by the next:
    \[ H_{\text{naive}} = \frac{1}{(1+s)^2} = \frac{1}{s^2+2s+1} \]
    a double pole at \(-1\). This is wrong, because the second section draws current through the first, so the first no longer sees an open circuit.

    Analyse the ladder properly. Working back from the output, the impedance loading the first resistor is \(C_1\) in parallel with the whole second section:
    \[ \mathbf{Z}_p = \frac{1}{s}\parallel\left(1+\frac{1}{s}\right) = \frac{(1/s)(1+1/s)}{1/s+1+1/s} = \frac{s+1}{s(s+2)} \]
    Then the overall transfer function is the product of two dividers:
    \[ H(s) = \frac{\mathbf{Z}_p}{1+\mathbf{Z}_p}\cdot\frac{1/s}{1+1/s} \]
    \[ \boxed{\;H(s) = \frac{1}{s^2+3s+1}\;} \]
    The middle coefficient is 3, not 2. That single difference changes everything:
    NaiveActual
    Denominator\(s^2+2s+1\)\(s^2+3s+1\)
    Poles\(-1, -1\) (repeated)\(-0.382, -2.618\)
    DampingCritically dampedOverdamped
    \(-3\) dB frequency0.644 rad/s0.374 rad/s
    The bandwidth is 42% lower than predicted — a substantial error, not a refinement.

    Where the poles went. The repeated pole has split into a slow one and a fast one, and their product is unchanged:
    \[ (-0.382)(-2.618) = 1 = \text{constant term}\;\checkmark \]
    The dominant pole moved from \(-1\) to \(-0.382\), which is what slows the circuit. (These are \((3\mp\sqrt5)/2\), the golden-ratio pair — a curiosity of equal sections.)

    Why the extra \(s\) appears. The loading current through \(R_1\) is proportional to \(sC_1V_1\), contributing an extra \(R_1C_1s\) term. In general, for sections with time constants \(T_1\) and \(T_2\):
    \[ D(s) = T_1T_2s^2+\left(T_1+T_2+R_1C_2\right)s+1 \]
    The cross-term \(R_1C_2\) is the loading. It vanishes only if \(R_1 \to 0\) or \(C_2 \to 0\) — that is, if the second stage draws no current.

    The two cures:
    CureHow
    BufferA unity-gain follower between stages makes the product exact
    Impedance scalingMake stage 2 much higher impedance, so \(R_1C_2 \ll T_1\)
    The second is why Set 30's Sallen–Key sections are cascaded through op-amp outputs, and why passive ladder filters must be designed as a whole rather than section by section (Set 30, Problem 16).

    The general lesson. Set 28, Problem 14 met this same penalty; here it is derived from the circuit. Transfer functions multiply only when the interface carries no power — and a direct connection between two passive sections always does.
  2. C2. A 1 F capacitor charged to 10 V is switched onto an uncharged 1 F capacitor through a resistance \(R\). Find the energy dissipated, and explain the result as \(R \to 0\).

    Show answer
    Solve in the \(s\)-domain. The charged capacitor contributes a source \(10/s\); both capacitors contribute \(1/s\) of impedance:
    \[ I(s) = \frac{10/s}{R+1/s+1/s} = \frac{10}{Rs+2} \]
    \[ i(t) = \frac{10}{R}e^{-2t/R} \]
    Energy dissipated in the resistor:
    \[ W_R = \int_0^{\infty}Ri^2dt = R\cdot\frac{100}{R^2}\int_0^{\infty}e^{-4t/R}dt = \frac{100}{R}\cdot\frac{R}{4} \]
    \[ \boxed{\;W_R = 25\ \text{J, independent of } R\;} \]
    Check by energy accounting. Charge is conserved, so the final common voltage is 5 V:
    StageEnergy
    Before\(\frac12(1)(10)^2 = 50\) J
    After\(2\times\frac12(1)(5)^2 = 25\) J
    Lost25 J — exactly half ✓
    Exactly half the stored energy is always lost, for equal capacitors, whatever \(R\) is.

    The paradox as \(R \to 0\). Watch what happens to the current:
    \(R\) (Ω)Peak currentTime constantEnergy lost
    101 A5 s25 J
    110 A0.5 s25 J
    0.011000 A5 ms25 J
    \(\to 0\)→ ∞→ 025 J
    The current becomes an impulse — infinite height, zero width, finite area of 5 C. The product \(Ri^2\) integrated over time stays at exactly 25 J because the shrinking \(R\) is precisely offset by the growing \(i^2\).

    Where does the energy go with no resistance at all? The idealisation breaks down, and the answer depends on what was neglected:
    Real effectFate of the 25 J
    Wiring resistanceHeat — the case computed above
    Wiring inductanceOscillation, then radiated or dissipated
    RadiationElectromagnetic emission
    Something always absorbs it. A truly lossless zero-inductance connection is not physically possible, which is the resolution: the 25 J is not lost by the mathematics but by the model's refusal to say where it went.

    Why this matters. Set 18's continuity rule — capacitor voltage cannot change instantaneously — is violated here in the limit, and the culprit is the impulsive current of Set 31, Problem 13. A loop of capacitors with no resistance is exactly the degenerate case flagged in Problem 18: the two capacitors are not independent, the circuit order drops from 2 to 1, and the missing state variable is what allows the discontinuity. Switched-capacitor converters live with this: charge-transfer efficiency is capped at 50% unless an inductor is added to make the transfer resonant.
  3. C3. A circuit has \(H(s) = (1-s)/[(s+1)(s+2)]\). Predict the step response before computing it, then verify.

    Show answer
    Read the pole–zero pattern first.
    FeatureLocationImplication
    Poles\(-1, -2\)Stable, overdamped
    Zero\(+1\)Right half-plane
    \(H(0)\)\(1/2\)Final value 0.5
    The RHP zero is the whole story. By Set 28, Challenge C3 this is a non-minimum-phase system, and the signature is an initial undershoot: the response first moves in the wrong direction.

    Predict the initial slope without inverting. The initial value theorem applied to the derivative:
    \[ \left.\frac{da}{dt}\right|_{0^+} = \lim_{s\to\infty}s\cdot s\cdot\frac{H(s)}{s} = \lim_{s\to\infty}\frac{s(1-s)}{(s+1)(s+2)} = -1 \]
    Negative — confirmed before any inversion. The response starts downward even though it must end at \(+0.5\).

    Now verify. Expanding \(H(s)/s\):
    \[ \frac{1-s}{s(s+1)(s+2)} = \frac{1/2}{s}-\frac{2}{s+1}+\frac{3/2}{s+2} \]
    \[ \boxed{\;a(t) = \frac12-2e^{-t}+\frac32e^{-2t}\;} \]
    \(t\)\(a(t)\)Comment
    0\(0.5-2+1.5 = 0\)Starts at zero ✓
    0.2−0.132Going the wrong way
    0.405−0.167Maximum undershoot
    1.0−0.033Recovering
    2.0+0.257Now positive
    +0.500Final value ✓
    The undershoot reaches \(-1/6\) — a third of the final value, in the wrong direction.

    Why the zero does this. The response is a sum of two decaying terms with opposite signs, and the RHP zero forces the faster term to dominate initially:
    \[ a(t) = \underbrace{\tfrac32e^{-2t}}_{\text{fast, positive}}\underbrace{-2e^{-t}}_{\text{slow, negative}}+\tfrac12 \]
    At \(t=0\) they cancel exactly. The fast term then dies first, exposing the negative one — which is why the output dips before the slow term itself decays and lets the constant through.

    What the RHP zero costs in feedback. Non-minimum-phase behaviour is a hard limitation, not a nuisance:
    ConsequenceReason
    Bandwidth is fundamentally cappedExtra phase lag with no magnitude benefit
    Cannot be cancelledA RHP pole in the compensator would be unstable
    Fast feedback makes it worseThe controller reacts to the wrong-way motion
    Real examples abound: a boost converter's output dips when the duty cycle increases; an aircraft's altitude drops briefly when the elevator commands a climb; a bicycle steers left before turning right. In each case the physical mechanism differs, but the transfer function has a zero at \(+a\) and the step response undershoots by the same mathematics.
MCQ

Multiple-Choice Questions

Twelve questions in GATE/ESE style. Commit to an answer before opening the explanation.

  1. Q1. The \(s\)-domain impedance of a capacitor is

    (a) \(sC\)   (b) \(1/sC\)   (c) \(C/s\)   (d) \(s/C\)

    Show answer
    (b) — and \(sC\) is its admittance — Problem 1.
  2. Q2. An inductor with initial current \(i_0\) is modelled as \(sL\) in series with

    (a) \(i_0/s\)   (b) \(Li_0\)   (c) \(Li_0/s\)   (d) \(i_0\)

    Show answer
    (b), a voltage source — an impulse in the time domain. The Norton form uses \(i_0/s\) in parallel — Problem 2.
  3. Q3. At \(t = 0^+\) an uncharged capacitor behaves as

    (a) an open circuit   (b) a short circuit   (c) a resistor   (d) a current source

    Show answer
    (b)\(1/sC \to 0\) as \(s\to\infty\) — Problem 14.
  4. Q4. A parallel \(RLC\) circuit driven by a DC current source settles to a voltage of

    (a) \(IR\)   (b) zero   (c) infinite   (d) \(I\sqrt{L/C}\)

    Show answer
    (b) — the inductor shorts the node at DC and takes all the current — Problem 6.
  5. Q5. In \(s\)-domain mesh analysis, the impedance matrix of a passive network is

    (a) diagonal   (b) symmetric   (c) antisymmetric   (d) singular

    Show answer
    (b), exactly as in Set 4 — and an asymmetric result signals an error — Problem 5.
  6. Q6. The natural frequencies of a series \(RLC\) circuit are the

    (a) poles of \(\mathbf{Z}(s)\)   (b) zeros of \(\mathbf{Z}(s)\)   (c) zeros of \(\mathbf{Y}(s)\)   (d) poles of the source

    Show answer
    (b) — current can flow with the terminals shorted — Problem 17.
  7. Q7. A transfer function is defined with

    (a) any initial conditions   (b) zero initial conditions   (c) a step input   (d) a sinusoidal input

    Show answer
    (b). Otherwise the output is not proportional to the input — Problem 10.
  8. Q8. Taking the output across \(R\) in a series \(RLC\) circuit gives a

    (a) low-pass   (b) high-pass   (c) band-pass   (d) band-stop

    Show answer
    (c) — one zero at the origin, one at infinity — Problem 18.
  9. Q9. Compared with the low-pass version, the high-pass output of the same \(RLC\) circuit has

    (a) different poles   (b) the same poles   (c) no poles   (d) more poles

    Show answer
    (b) — poles belong to the network, zeros to the measurement point — Problem 18.
  10. Q10. The area under a circuit's impulse response equals

    (a) 1   (b) \(H(0)\)   (c) \(H(\infty)\)   (d) the time constant

    Show answer
    (b), the DC gain — a quick and useful check — Problem 11.
  11. Q11. Two \(RC\) sections cascaded directly have a transfer function equal to

    (a) the product of the two   (b) less than the product   (c) the sum   (d) the product divided by 2

    Show answer
    (b) — loading adds a cross-term, giving \(s^2+3s+1\) rather than \(s^2+2s+1\) — Challenge C1.
  12. Q12. A right-half-plane zero in a stable system causes

    (a) instability   (b) initial undershoot   (c) infinite gain   (d) no observable effect

    Show answer
    (b) — the step response moves the wrong way first — Challenge C3.
Formulas

Key Formulas

QuantityRelationNotes
Element impedances\(R\), \(sL\), \(1/sC\)Set \(s = j\omega\) to recover phasors
Inductor with \(i(0^-)\)\(V = sLI-Li(0^-)\)Series source \(Li(0^-)\)
Inductor, Norton\(I = \dfrac{V}{sL}+\dfrac{i(0^-)}{s}\)Parallel source \(i(0^-)/s\)
Capacitor with \(v(0^-)\)\(V = \dfrac{I}{sC}+\dfrac{v(0^-)}{s}\)Series source \(v(0^-)/s\)
Capacitor, Norton\(I = sCV-Cv(0^-)\)Parallel source \(Cv(0^-)\)
Series \(RLC\)\(\mathbf{Z}(s) = \dfrac{s^2LC+sRC+1}{sC}\)Zeros are the natural frequencies
Parallel \(RLC\)\(\mathbf{Y}(s) = \dfrac{1}{R}+sC+\dfrac{1}{sL}\)Zeros of \(\mathbf{Y}\) are the natural frequencies
Second-order form\(D(s) = s^2+\dfrac{\omega_0}{Q}s+\omega_0^2\)Series: \(\omega_0 = 1/\sqrt{LC}\), \(Q = \frac1R\sqrt{L/C}\)
Low-pass (across \(C\))\(H = \dfrac{1/LC}{D(s)}\)Two zeros at infinity
High-pass (across \(L\))\(H = \dfrac{s^2}{D(s)}\)Double zero at the origin
Band-pass (across \(R\))\(H = \dfrac{(R/L)s}{D(s)}\)One zero at the origin
KVL identity\(H_C+H_L+H_R = 1\)At every frequency
Inverting op-amp\(H(s) = -\dfrac{\mathbf{Z}_f}{\mathbf{Z}_i}\)Covers every inverting topology
Practical integrator\(H = \dfrac{-R_f/R_i}{1+sR_fC_f}\)Pure integrator is marginally stable
Coupled inductors\(\begin{bmatrix}sL_1 & \pm sM\\ \pm sM & sL_2\end{bmatrix}\)Plus IC sources \(L_1i_1(0^-) \pm Mi_2(0^-)\)
Reflected impedance\(\mathbf{Z}_{\text{in}} = sL_1+\dfrac{(sM)^2}{sL_2+\mathbf{Z}_L}\)Dot convention irrelevant — \(M\) squared
Impulse and step\(h = \mathcal{L}^{-1}\{H\}\), \(a = \mathcal{L}^{-1}\{H/s\}\)\(\int_0^\infty h\,dt = H(0)\)
Endpoints\(s\to\infty\): \(L\) open, \(C\) short\(s\to0\): \(L\) short, \(C\) open
Cascade with loading\(D = T_1T_2s^2+(T_1+T_2+R_1C_2)s+1\)Cross-term \(R_1C_2\) is the loading
Pitfalls

Common Mistakes

  1. Reversing an initial-condition source. Fix the current direction first, write the transformed law, then draw the source to match — and check with the initial value theorem — Problems 2 and 4.

  2. Forgetting the initial-condition term when recovering an element voltage. \(V_C = I/sC\) gives only the change; the \(v(0^-)/s\) must be added back — Problem 4.

  3. Assuming a parallel \(RLC\) settles to \(IR\). The inductor shorts the node at DC, so the final voltage is zero — Problem 6.

  4. Using \(\mathbf{Z}\) for a parallel circuit. Work with \(\mathbf{Y}\) and nodal analysis; the natural frequencies then come from its numerator — Problem 6.

  5. Defining a transfer function with initial conditions present. \(H(s)\) requires zero stored energy, or the output is not proportional to the input — Problem 10.

  6. Multiplying transfer functions of directly cascaded passive stages. Loading adds a cross-term and can cost 42% of the bandwidth — Challenge C1.

  7. Believing a pole–zero cancellation removes a mode. It leaves it unexcited; the smallest mismatch brings it back — Problem 13.

  8. Applying maximum power transfer at general \(s\). The conjugate condition exists only on \(s = j\omega\) — Problem 19.

  9. Counting energy-storage elements to get the order. Only independent ones count; two parallel capacitors give one pole — Problem 18.

  10. Skipping the endpoint check. Two degenerate circuits drawn in seconds catch most sign errors — Problem 14.

Looking Ahead

Set 31 built the transform but always began from a differential equation someone else had written. This set removed that step: replace each element by \(R\), \(sL\) or \(1/sC\), draw a source for every initial condition, and what remains is a resistive network. Because Part 1's methods rested on nothing but KVL, KCL and \(V = \mathbf{Z}I\), all of them survive the change intact — mesh and nodal analysis, Thévenin and Norton, superposition and source transformation. Problem 19's audit found exactly one genuine casualty: maximum power transfer, whose conjugate condition lives only on the imaginary axis because average power is a steady-state idea.

Several structural facts emerged that are worth carrying forward. Poles belong to the network and zeros to the measurement point, which is why one \(RLC\) loop delivers a low-pass, a high-pass and a band-pass with identical \(\omega_0\) and \(Q\) — and why the three transfer functions sum to exactly 1, since KVL leaves them no alternative. Initial conditions do more than scale the answer: they place a zero. Problem 13 exploited this to make a second-order circuit respond as a first-order one, silencing the \(e^{-3t}\) mode entirely with \(i_0 = 2\) A and the \(e^{-2t}\) mode instead with \(i_0 = 3\) A. The mode is dormant, not absent, and any mismatch resurrects it.

The challenges pressed on the limits. Two \(RC\) sections cascaded directly do not give \((1+s)^{-2}\) but \(1/(s^2+3s+1)\) — a repeated pole split into \(-0.382\) and \(-2.618\), costing 42% of the bandwidth. Two capacitors sharing charge lose exactly half their energy whatever the resistance, and the loss survives even as \(R \to 0\), because the current becomes impulsive at precisely the rate needed to keep \(\int Ri^2dt\) at 25 J. And a right-half-plane zero makes a stable circuit's step response set off in the wrong direction — undershooting to \(-1/6\) before climbing to \(+0.5\).

Next: Set 33 — Fourier Series. Two gaps remain. Set 31, Problem 17 showed a periodic input transforms to \(F_1(s)/(1-e^{-sT_p})\), whose transcendental factor resists inversion entirely; and Challenge C1 has just shown that cascades cannot be handled by multiplication. Set 33 addresses the first by giving up on a closed form and decomposing the input into harmonics, each handled by the phasor method that Set 31 finally justified. Set 35 will close the second.