13.3 First-Order & Second-Order Circuit Transients

Key Takeaways

  • First-order RC and RL transient responses follow exponential curves defined by time constants \tau = RC and \tau = \frac{L}{R}, reaching 63.2\% of final value at 1\tau and over 99.3\% at 5\tau.
  • Step response for first-order systems follows the general formula x(t) = x(\infty) + [x(0^+) - x(\infty)]e^{-t/\tau}, where initial state x(0^+) respects energy continuity: v_C(0^+) = v_C(0^-) and i_L(0^+) = i_L(0^-).
  • Second-order RLC transient behavior is dictated by the characteristic equation s^2 + 2\alpha s + \omega_0^2 = 0, with undamped natural frequency \omega_0 = \frac{1}{\sqrt{LC}} and attenuation factor \alpha = \frac{R}{2L} (series) or \alpha = \frac{1}{2RC} (parallel).
  • RLC systems exhibit three distinct damping regimes based on root locations: Overdamped (\alpha > \omega_0, real distinct roots), Critically Damped (\alpha = \omega_0, real double root), and Underdamped (\alpha < \omega_0, complex conjugate roots with damped frequency \omega_d = \sqrt{\omega_0^2 - \alpha^2}).
  • Power system switching transients generate high Transient Recovery Voltages (TRV), capacitive charging inrushes, and inductive voltage spikes (v = L \frac{di}{dt}), requiring protective snubber circuits and surge arresters.
Last updated: August 2026

13.3 First-Order & Second-Order Circuit Transients

Circuit transients represent the temporary transition state when an electrical network shifts from one steady-state condition to another due to switching operations, short-circuit faults, or sudden load changes. For the PRC Registered Electrical Engineer (REE) Licensure Examination, mastering time constants, step response formulas, second-order $RLC$ damping classifications, and Laplace transform $s$-domain methods is vital.


1. Fundamentals of Transients & Initial Energy Continuity

Transients arise because energy stored in reactive elements cannot change instantaneously:

  • Inductor Magnetic Energy: $W_L = \frac{1}{2} L i_L^2 \implies$ Inductor current cannot change instantaneously: iL(0+)=iL(0)i_L(0^+) = i_L(0^-)
  • Capacitor Electric Energy: $W_C = \frac{1}{2} C v_C^2 \implies$ Capacitor voltage cannot change instantaneously: vC(0+)=vC(0)v_C(0^+) = v_C(0^-)

where $t = 0^-$ represents the instant immediately prior to switching, and $t = 0^+$ represents the instant immediately after switching.


2. First-Order $RC$ and $RL$ Transients

First-order circuits contain a single energy storage element (or equivalent $L$ or $C$) alongside resistive networks.

Time Constant (\tau) Equations

  • $RC$ Circuit Time Constant: τ=ReqC(seconds)\tau = R_{\text{eq}} C \quad (\text{seconds})
  • $RL$ Circuit Time Constant: τ=LReq(seconds)\tau = \frac{L}{R_{\text{eq}}} \quad (\text{seconds})

where $R_{\text{eq}}$ is the Thevenin equivalent resistance seen from the terminals of the storage element.

General First-Order Step Response Formula

For any first-order variable $x(t)$ (representing capacitor voltage $v_C(t)$ or inductor current $i_L(t)$):

x(t)=x()+[x(0+)x()]et/τfor t0x(t) = x(\infty) + \left[ x(0^+) - x(\infty) \right] e^{-t/\tau} \quad \text{for } t \ge 0

where:

  • $x(0^+)$ is the initial value immediately after switching;
  • $x(\infty)$ is the final steady-state value as $t \to \infty$;
  • $\tau$ is the circuit time constant.

Time Constant Progression & Response Characteristics

Elapsed Time ($t$)Remaining Transient Amplitude ($e^{-t/\tau}$)Percentage of Total Change Completed
$1\tau$$e^{-1} \approx 0.3679$$63.2%$
$2\tau$$e^{-2} \approx 0.1353$$86.5%$
$3\tau$$e^{-3} \approx 0.0498$$95.0%$
$4\tau$$e^{-4} \approx 0.0183$$98.2%$
$5\tau$$e^{-5} \approx 0.0067$$99.3%$ (Considered Steady State)

3. Second-Order $RLC$ Transients & Damping Regimes

Second-order circuits contain two uncoupled energy storage elements ($L$ and $C$), yielding a second-order linear differential equation.

Governing Differential Equations

  • Series $RLC$ Circuit: Ld2i(t)dt2+Rdi(t)dt+1Ci(t)=0    d2idt2+2αdidt+ω02i=0L \frac{d^2 i(t)}{dt^2} + R \frac{di(t)}{dt} + \frac{1}{C} i(t) = 0 \implies \frac{d^2 i}{dt^2} + 2\alpha \frac{di}{dt} + \omega_0^2 i = 0
  • Parallel $RLC$ Circuit: Cd2v(t)dt2+1Rdv(t)dt+1Lv(t)=0    d2vdt2+2αdvdt+ω02v=0C \frac{d^2 v(t)}{dt^2} + \frac{1}{R} \frac{dv(t)}{dt} + \frac{1}{L} v(t) = 0 \implies \frac{d^2 v}{dt^2} + 2\alpha \frac{dv}{dt} + \omega_0^2 v = 0

Key Parameters

  1. Undamped Natural Frequency (\omega_0): ω0=1LC(rad/s)\omega_0 = \frac{1}{\sqrt{LC}} \quad (\text{rad/s})
  2. Damping Attenuation Factor (\alpha): Series RLC:α=R2L,Parallel RLC:α=12RC\text{Series } RLC: \alpha = \frac{R}{2L}, \qquad \text{Parallel } RLC: \alpha = \frac{1}{2RC}
  3. Damping Ratio (\zeta): ζ=αω0\zeta = \frac{\alpha}{\omega_0}

Characteristic Equation & Roots

Substituting $x(t) = A e^{st}$ yields the characteristic equation:

s2+2αs+ω02=0s^2 + 2\alpha s + \omega_0^2 = 0

Roots are given by the quadratic formula:

s1,2=α±α2ω02s_{1,2} = -\alpha \pm \sqrt{\alpha^2 - \omega_0^2}

Classification of Damping Regimes

Damping StateMathematical ConditionCharacteristic Roots ($s_{1,2}$)Time-Domain Response Expression $x(t)$Physical System Trajectory
Overdamped$\alpha > \omega_0$ ($\zeta > 1$)Two real, distinct negative roots$x(t) = A_1 e^{s_1 t} + A_2 e^{s_2 t}$Slow, non-oscillatory exponential return to steady state.
Critically Damped$\alpha = \omega_0$ ($\zeta = 1$)Two real, equal roots ($s_1 = s_2 = -\alpha$)$x(t) = (A_1 + A_2 t) e^{-\alpha t}$Fastest non-oscillatory return to equilibrium without overshoot.
Underdamped$\alpha < \omega_0$ ($\zeta < 1$)Complex conjugate roots ($-\alpha \pm j\omega_d$)$x(t) = e^{-\alpha t} \left[ A_1 \cos(\omega_d t) + A_2 \sin(\omega_d t) \right]$Damped oscillatory response with frequency $\omega_d = \sqrt{\omega_0^2 - \alpha^2}$.

Damped Natural Frequency: ωd=ω02α2(rad/s),fd=ωd2π(Hz)\text{Damped Natural Frequency: } \omega_d = \sqrt{\omega_0^2 - \alpha^2} \quad (\text{rad/s}), \qquad f_d = \frac{\omega_d}{2\pi} \quad (\text{Hz})


4. Laplace Transform ($s$-Domain) Methods for Transients

Laplace transform converts differential equations into algebraic equations in the complex frequency domain ($s = \sigma + j\omega$).

Key Laplace Transform Pairs

  • $\mathcal{L}{ 1 } = \frac{1}{s}$
  • $\mathcal{L}{ e^{-at} } = \frac{1}{s + a}$
  • $\mathcal{L}{ \sin(\omega t) } = \frac{\omega}{s^2 + \omega^2}$
  • $\mathcal{L}{ \cos(\omega t) } = \frac{s}{s^2 + \omega^2}$
  • $\mathcal{L}\left{ \frac{df(t)}{dt} \right} = s F(s) - f(0^+)$
  • $\mathcal{L}\left{ \frac{d^2f(t)}{dt^2} \right} = s^2 F(s) - s f(0^+) - f'(0^+)$

Circuit Element Equivalent $s$-Domain Models

  • Resistor ($R$): $Z(s) = R$
  • Inductor ($L$): Series combination of impedance $sL$ and voltage source $L i_L(0^+)$ (or parallel current source $\frac{i_L(0^+)}{s}$)
  • Capacitor ($C$): Series combination of impedance $\frac{1}{sC}$ and voltage source $\frac{v_C(0^+)}{s}$

5. Power System Switching Transients & Protective Measures

In high-voltage power networks, transient phenomena can trigger destructive voltage spikes and insulation breakdown:

  1. Transient Recovery Voltage (TRV): When a circuit breaker interrupts an inductive fault current, high frequency oscillations occur across the opening contacts as energy transfers between grid inductance and stray capacitance.
  2. Inductive Kickback ($v_L = L \frac{di}{dt}$): Opening an inductive circuit (such as a motor field winding or transformer) abruptly produces severe overvoltage surges. Protection requires RC snubber circuits, flyback diodes, or metal-oxide varistors (MOVs).
  3. Capacitor Bank Inrush Current: Energizing distribution capacitor banks creates high-magnitude, high-frequency current transients. Damping reactors or pre-insertion resistors are installed to limit inrush currents.

Solved Board Exam Numerical Problems

Problem 1: First-Order $RL$ Transient Step Response

Question: A series $RL$ circuit containing a resistor $R = 10\ \Omega$ and an inductor $L = 2.0\ \text{H}$ is connected to a constant $100\ \text{V}$ DC source at $t = 0$. Assuming zero initial current ($i_L(0^-) = 0$), determine: (a) the circuit time constant $\tau$, (b) the current at $t = 0.10\ \text{s}$, (c) the steady-state current as $t \to \infty$, and (d) the time required for current to reach $90%$ of its final value.

Solution:

  1. Calculate time constant $\tau$: τ=LR=2.0 H10 Ω=0.20 seconds\tau = \frac{L}{R} = \frac{2.0\ \text{H}}{10\ \Omega} = 0.20\ \text{seconds}

  2. Determine steady-state current $i(\infty)$: i()=VR=100 V10 Ω=10 Amperesi(\infty) = \frac{V}{R} = \frac{100\ \text{V}}{10\ \Omega} = 10\ \text{Amperes}

  3. Apply first-order step response equation: i(t)=i()+[i(0+)i()]et/τ=10+[010]et/0.20=10(1e5t) Ai(t) = i(\infty) + [i(0^+) - i(\infty)] e^{-t/\tau} = 10 + [0 - 10] e^{-t/0.20} = 10 \left( 1 - e^{-5t} \right)\ \text{A}

  4. Compute current at $t = 0.10\ \text{s}$: i(0.10)=10(1e5(0.10))=10(1e0.5)=10(10.6065)=3.935 Amperesi(0.10) = 10 \left( 1 - e^{-5(0.10)} \right) = 10 \left( 1 - e^{-0.5} \right) = 10 (1 - 0.6065) = 3.935\ \text{Amperes}

  5. Calculate time $t$ to reach $90%$ ($9.0\ \text{A}$): 9.0=10(1et/0.20)    0.90=1et/0.20    et/0.20=0.109.0 = 10 \left( 1 - e^{-t/0.20} \right) \implies 0.90 = 1 - e^{-t/0.20} \implies e^{-t/0.20} = 0.10 t0.20=ln(0.10)=2.3026    t=0.20×2.3026=0.4605 seconds-\frac{t}{0.20} = \ln(0.10) = -2.3026 \implies t = 0.20 \times 2.3026 = 0.4605\ \text{seconds}


Problem 2: Series $RLC$ Transient Response Classification & Frequency

Question: A series $RLC$ circuit has parameters $R = 40\ \Omega$, $L = 100\ \text{mH}$ ($0.10\ \text{H}$), and $C = 25\ \mu\text{F}$ ($25 \times 10^{-6}\ \text{F}$). Determine: (a) the attenuation factor $\alpha$, (b) the undamped natural frequency $\omega_0$, (c) the damping regime classification, and (d) the damped natural frequency $\omega_d$ and cyclic frequency $f_d$.

Solution:

  1. Calculate attenuation factor $\alpha$ for series $RLC$: α=R2L=402×0.10=400.20=200 rad/s\alpha = \frac{R}{2L} = \frac{40}{2 \times 0.10} = \frac{40}{0.20} = 200\ \text{rad/s}

  2. Calculate undamped natural frequency $\omega_0$: ω0=1LC=10.10×25×106=12.5×106=10.0015811=632.46 rad/s\omega_0 = \frac{1}{\sqrt{LC}} = \frac{1}{\sqrt{0.10 \times 25 \times 10^{-6}}} = \frac{1}{\sqrt{2.5 \times 10^{-6}}} = \frac{1}{0.0015811} = 632.46\ \text{rad/s}

  3. Classify damping regime by comparing $\alpha$ and $\omega_0$: Since α=200 rad/s<ω0=632.46 rad/s, the system is UNDERDAMPED (oscillatory).\text{Since } \alpha = 200\ \text{rad/s} < \omega_0 = 632.46\ \text{rad/s}, \text{ the system is } \mathbf{UNDERDAMPED} \text{ (oscillatory).}

  4. Calculate damped natural frequency $\omega_d$ and cyclic frequency $f_d$: ωd=ω02α2=(632.46)2(200)2=400,00040,000=360,000=600 rad/s\omega_d = \sqrt{\omega_0^2 - \alpha^2} = \sqrt{(632.46)^2 - (200)^2} = \sqrt{400,000 - 40,000} = \sqrt{360,000} = 600\ \text{rad/s} fd=ωd2π=6002π=95.49 Hzf_d = \frac{\omega_d}{2\pi} = \frac{600}{2\pi} = 95.49\ \text{Hz}

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Classification of Second-Order RLC Damping Regimes
First-Order Step Response Percentage Completion vs Time Constants
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What is the time constant of a series circuit consisting of a 50 mH inductor and a 25 Ω resistor?

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A series RLC circuit has R = 20 Ω, L = 0.1 H, and C = 100 μF. Which damping state characterizes the transient response of this circuit?

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How many time constants must elapse for a first-order RC or RL step response to reach at least 99% of its final steady-state value?

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