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The is a powerful tool for analyzing continuous-time signals and systems. It converts complex time-domain problems into simpler algebraic equations in the frequency domain, making it easier to solve differential equations and study system behavior.

This section covers the fundamentals of Laplace transforms, including their definition, properties, and applications. We'll explore how to use Laplace transforms to characterize systems, solve differential equations, and analyze system stability and performance in the frequency domain.

Laplace Transform Fundamentals

Definition and Properties

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  • Laplace transform converts a time-domain signal f(t)f(t) into a complex frequency-domain representation F(s)F(s)
    • Defined as F(s)=0f(t)estdtF(s) = \int_{0}^{\infty} f(t) e^{-st} dt, where ss is a complex variable
    • Useful for analyzing linear time-invariant (LTI) systems and
  • recovers the time-domain signal f(t)f(t) from its Laplace transform F(s)F(s)
    • Denoted as f(t)=L1{F(s)}f(t) = \mathcal{L}^{-1}\{F(s)\}
    • Can be computed using partial fraction expansion, tables of common transforms, or complex integration (residue theorem)
  • (ROC) specifies the values of ss for which the Laplace transform integral converges
    • Determines the uniqueness and stability of the system
    • ROC must include the of F(s)F(s) for a stable, causal system (right-sided ROC)
    • Example: For a causal system with poles at s=1s=-1 and s=2s=-2, the ROC is Re(s)>1\text{Re}(s) > -1

S-Plane Representation

  • is a complex plane where the Laplace transform is defined
    • Real part of ss represents the damping or decay of the signal
    • Imaginary part of ss represents the oscillation or frequency of the signal
  • Poles and of F(s)F(s) in the s-plane provide insights into the system's behavior
    • Poles are values of ss where F(s)F(s) becomes infinite, indicating resonances or instabilities
    • Zeros are values of ss where F(s)F(s) becomes zero, indicating signal cancellations or notches
  • Example: A system with a pole at s=3+j4s=-3+j4 and a zero at s=2s=-2 will have a resonance at ω=4\omega=4 rad/s and a notch at ω=2\omega=2 rad/s

System Characterization

Transfer Function

  • H(s)H(s) describes the input-output relationship of an LTI system in the Laplace domain
    • Defined as the ratio of the output Laplace transform Y(s)Y(s) to the input Laplace transform X(s)X(s): H(s)=Y(s)X(s)H(s) = \frac{Y(s)}{X(s)}
    • Represents the system's and stability properties
  • Poles and zeros of the transfer function determine the system's dynamics and stability
    • Poles in the left half-plane (LHP) indicate stable modes, while poles in the right half-plane (RHP) indicate unstable modes
    • Zeros in the LHP or RHP affect the system's and steady-state behavior
  • Example: A low-pass filter with transfer function H(s)=1s+1H(s) = \frac{1}{s+1} has a pole at s=1s=-1, resulting in a stable system with a cutoff frequency of 1 rad/s

Initial and Final Value Theorems

  • determines the initial value of a time-domain signal from its Laplace transform
    • Stated as limt0+f(t)=limssF(s)\lim_{t \to 0^+} f(t) = \lim_{s \to \infty} sF(s)
    • Useful for analyzing the system's response at the start of an input signal
  • determines the steady-state value of a time-domain signal from its Laplace transform
    • Stated as limtf(t)=lims0sF(s)\lim_{t \to \infty} f(t) = \lim_{s \to 0} sF(s), provided the limits exist and all poles of sF(s)sF(s) are in the LHP
    • Useful for analyzing the system's long-term behavior or steady-state error
  • Example: For a step input u(t)u(t) with Laplace transform U(s)=1sU(s)=\frac{1}{s}, the final value of the output signal y(t)=L1{H(s)U(s)}y(t)=\mathcal{L}^{-1}\{H(s)U(s)\} is given by limty(t)=lims0sH(s)U(s)=lims0H(s)\lim_{t \to \infty} y(t) = \lim_{s \to 0} sH(s)U(s) = \lim_{s \to 0} H(s)

Applications of Laplace Transform

Solving Differential Equations

  • Laplace transform simplifies the process of solving linear differential equations by converting them into algebraic equations
    • Take the Laplace transform of both sides of the differential equation, considering initial conditions
    • Solve the resulting algebraic equation for the output Laplace transform Y(s)Y(s)
    • Apply the inverse Laplace transform to obtain the time-domain solution y(t)y(t)
  • Example: Solve the differential equation d2y(t)dt2+3dy(t)dt+2y(t)=u(t)\frac{d^2y(t)}{dt^2}+3\frac{dy(t)}{dt}+2y(t)=u(t) with initial conditions y(0)=0y(0)=0 and dy(0)dt=0\frac{dy(0)}{dt}=0
    • Taking the Laplace transform yields: s2Y(s)+3sY(s)+2Y(s)=1ss^2Y(s)+3sY(s)+2Y(s)=\frac{1}{s}
    • Solving for Y(s)Y(s): Y(s)=1s(s2+3s+2)Y(s)=\frac{1}{s(s^2+3s+2)}
    • Applying the inverse Laplace transform gives the time-domain solution: y(t)=12(1etcos(t)etsin(t))y(t)=\frac{1}{2}(1-e^{-t}\cos(t)-e^{-t}\sin(t))

System Analysis using Laplace Transform

  • Laplace transform enables the analysis of LTI systems in the frequency domain
    • : Determine the stability of the system based on the pole locations in the s-plane
    • Frequency response: Evaluate the system's gain and phase response by setting s=jωs=j\omega in the transfer function H(s)H(s)
    • Transient response: Analyze the system's time-domain behavior for different inputs using the inverse Laplace transform
  • Laplace transform also facilitates the design of and filters
    • Design feedback controllers by manipulating the pole and zero locations of the closed-loop transfer function
    • Implement filters with desired frequency responses by selecting appropriate pole and zero locations in the s-plane
  • Example: Analyze the stability and steady-state error of a unity feedback system with open-loop transfer function G(s)=Ks(s+2)G(s)=\frac{K}{s(s+2)}
    • The closed-loop transfer function is H(s)=G(s)1+G(s)=Ks2+2s+KH(s)=\frac{G(s)}{1+G(s)}=\frac{K}{s^2+2s+K}
    • For stability, the poles of H(s)H(s) must be in the LHP, requiring K>0K>0
    • The steady-state error for a step input is ess=lims011+G(s)=11+lims0Ks(s+2)=2Ke_{ss}=\lim_{s \to 0} \frac{1}{1+G(s)}=\frac{1}{1+\lim_{s \to 0} \frac{K}{s(s+2)}}=\frac{2}{K}, which can be reduced by increasing the gain KK
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© 2024 Fiveable Inc. All rights reserved.
AP® and SAT® are trademarks registered by the College Board, which is not affiliated with, and does not endorse this website.

© 2024 Fiveable Inc. All rights reserved.
AP® and SAT® are trademarks registered by the College Board, which is not affiliated with, and does not endorse this website.
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