Damped Oscillation Flashcards

Introduction to Damped Oscillation

  • Simple Harmonic Motion (SHM) is conventionally categorized as free oscillation.

  • In physical reality, free oscillations rarely sustain indefinitely; they decay over time due to various resistive or dissipative forces that steadily diminish the total energy of the mechanical system.

  • The inclusion of damping forces alters system dynamics in multiple ways, including the potential elimination of oscillatory behavior altogether, causing the system to return to equilibrium without oscillating.

  • Damped motion is categorized based on the mathematical relationship between the natural frequency of vibration ω0\omega_0 and the damping factor γ\gamma.

Simple Harmonic Motion Primer

  • Definition 1: A particle executes Simple Harmonic Motion (SHM) if the net force acting upon it is directly proportional to its displacement relative to a designated origin and acts in the direction opposite to that displacement.

  • The governing differential equation of motion for SHM is:

mx¨=−kxm\ddot{x} = -kx

  • In this formulation, mm represents the particle mass, x=x(t)x = x(t) denotes particle position as a function of time tt, x˙=dxdt\dot{x} = \frac{dx}{dt} represents instantaneous velocity, x¨=d2xdt2\ddot{x} = \frac{d^2x}{dt^2} represents instantaneous acceleration, and k>0k > 0 is a constant stiffness parameter.

  • The differential equation can be expressed in canonical form as:

x¨=−ω02x\ddot{x} = -\omega_0^2 x

  • Here, ω0>0\omega_0 > 0 is a constant parameter representing the natural frequency of the system, defined by ω0=km\omega_0 = \sqrt{\frac{k}{m}}.

  • Remark 1 (Linearity and Homogeneity):

    • Linearity: If x1(t)x_1(t) and x2(t)x_2(t) are two distinct solutions to x¨=−ω02x\ddot{x} = -\omega_0^2 x, their linear combination x(t)=c1x1(t)+c2x2(t)x(t) = c_1 x_1(t) + c_2 x_2(t) (where c1c_1 and c2c_2 are arbitrary constants) is also a valid solution.

    • Homogeneity: The equation contains no non-zero terms independent of xx or its time derivatives. Consequently, the zero solution x(t)=0x(t) = 0 represents a valid trivial solution.

  • Derivation of the General Solution:

    • Substituting a trial exponential solution x(t)=eλtx(t) = e^{\lambda t} yields x˙(t)=λeλt\dot{x}(t) = \lambda e^{\lambda t} and x¨(t)=λ2eλt\ddot{x}(t) = \lambda^2 e^{\lambda t}.

    • Substitution into the canonical equation yields:

(λ2+ω02)eλt=0(\lambda^2 + \omega_0^2)e^{\lambda t} = 0

  • Because eλt≠0e^{\lambda t} \neq 0 for all tt, the characteristic equation is (λ2+ω02)=0(\lambda^2 + \omega_0^2) = 0, yielding complex roots λ=±iω0\lambda = \pm i\omega_0

  • The general mathematical solution is:

x(t)=c1eiω0t+c2e−iω0tx(t) = c_1 e^{i\omega_0 t} + c_2 e^{-i\omega_0 t}

  • Remark 2 (Physical Reality Condition):

    • Since x(t)x(t) measures real physical displacement, x(t)x(t) must equal its complex conjugate x∗(t)x^*(t), yielding:

c1eiω0t+c2e−iω0t=c1∗e−iω0t+c2∗eiω0tc_1 e^{i\omega_0 t} + c_2 e^{-i\omega_0 t} = c_1^* e^{-i\omega_0 t} + c_2^* e^{i\omega_0 t}

(c1−c2∗)eiω0t+(c1∗−c2)e−iω0t=0(c_1 - c_2^*)e^{i\omega_0 t} + (c_1^* - c_2)e^{-i\omega_0 t} = 0

  • Differentiating with respect to time tt gives:

(c1−c2∗)eiω0t−(c1∗−c2)e−iω0t=0(c_1 - c_2^*)e^{i\omega_0 t} - (c_1^* - c_2)e^{-i\omega_0 t} = 0

  • Summing these two equations yields 2(c1−c2∗)eiω0t=02(c_1 - c_2^*)e^{i\omega_0 t} = 0. Because eiω0t≠0e^{i\omega_0 t} \neq 0 for all tt, c1=c2∗c_1 = c_2^*, confirming that c1c_1 and c2c_2 are complex conjugates.

  • Writing c1=Ae−iθc_1 = A e^{-i\theta} (where AA and θ\theta are real constants) yields the physical displacement form:

x(t)=Aei(ω0t−θ)+Ae−i(ω0t−θ)=2Acos⁡(ω0t−θ)x(t) = A e^{i(\omega_0 t - \theta)} + A e^{-i(\omega_0 t - \theta)} = 2A \cos(\omega_0 t - \theta)

  • Determination of Integration Constants via Initial Conditions:

    • Case I (x(0)=0x(0) = 0, v(0)=dxdt∣t=0=v0v(0) = \frac{dx}{dt}\Big|_{t=0} = v_0):

0=2Acos⁡(θ)0 = 2A \cos(\theta)

v0=−2Aω0sin⁡(−θ)v_0 = -2A\omega_0 \sin(-\theta)

  • The first condition implies cos⁡(θ)=0  ⟹  θ=π2\cos(\theta) = 0 \implies \theta = \frac{\pi}{2}, while the second gives A=v02ω0A = \frac{v_0}{2\omega_0}. The physical solution is:

x(t)=(v0ω0)sin⁡(ω0t)x(t) = \left(\frac{v_0}{\omega_0}\right) \sin(\omega_0 t)

  • Case II (x(0)=x0x(0) = x_0, v(0)=dxdt∣t=0=0v(0) = \frac{dx}{dt}\Big|_{t=0} = 0):

x0=2Acos⁡(θ)x_0 = 2A \cos(\theta)

0=−2Aω0sin⁡(−θ)0 = -2A\omega_0 \sin(-\theta)

  • The second condition implies sin⁡(θ)=0  ⟹  θ=0\sin(\theta) = 0 \implies \theta = 0, while the first gives A=x02A = \frac{x_0}{2}. The physical solution is:

x(t)=x0cos⁡(ω0t)x(t) = x_0 \cos(\omega_0 t)


x(t) vs t for two different initial conditions
  • Definition 2: A non-trivial solution x(t)x(t) is classified as oscillatory if it intersects the tt-axis more than once within a specified time interval, and non-oscillatory if it intersects the tt-axis at most once within that interval.

  • Definition 3: Because x(t+2πω0)=x(t)x\left(t + \frac{2\pi}{\omega_0}\right) = x(t), free SHM is periodic with time period T = \frac{2\text{\pi}}{\omega_0}, where ω0\omega_0 represents the natural frequency.

  • Theorem 1 (Energy Conservation in SHM): The differential equation x¨+ω02x=0\ddot{x} + \omega_0^2 x = 0 conserves the total mechanical energy E=12mx˙2+12mω02x2E = \frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2

    • Proof: Multiplying x¨+ω02x=0\ddot{x} + \omega_0^2 x = 0 by 2x˙2\dot{x} gives 2x˙x¨+2ω02xx˙=02\dot{x}\ddot{x} + 2\omega_0^2 x\dot{x} = 0. Multiplying by mass mm yields:

ddt(12mx˙2+12mω02x2)=0\frac{d}{dt}\left(\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2\right) = 0

12mx˙2+12mω02x2=constant\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2 = \text{constant}

  • For x(t)=x0cos⁡(ω0t)x(t) = x_0 \cos(\omega_0 t), the energy constant equals 12mω02x02\frac{1}{2}m\omega_0^2 x_0^2. Dividing energy by 12mω02x02\frac{1}{2}m\omega_0^2 x_0^2 yields the normalized trajectory:

(x˙ω0x0)2+(xx0)2=1\left(\frac{\dot{x}}{\omega_0 x_0}\right)^2 + \left(\frac{x}{x_0}\right)^2 = 1

  • Remark 3 (Phase Space Representation):

    • The coordinate system defined by plotting displacement x(t)x(t) against velocity x˙(t)\dot{x}(t) constitutes the Phase Space of the dynamical system.

    • The equation (x˙ω0x0)2+(xx0)2=1\left(\frac{\dot{x}}{\omega_0 x_0}\right)^2 + \left(\frac{x}{x_0}\right)^2 = 1 describes an ellipse in phase space. A closed trajectory in phase space signifies periodic motion.


Phase space diagram for Simple Harmonic Motion
  • Origin Dependency and Influence of Constant Forces:

    • SHM representation depends on the chosen origin. For example, x(t)=Asin⁡2(ω0t)x(t) = A \sin^2(\omega_0 t) describes simple harmonic oscillation centered at x=A2x = \frac{A}{2} with frequency 2ω02\omega_0.

    • Under an additional constant force f0f_0 (acceleration unit), the equation of motion becomes:

x¨+ω02x=f0\ddot{x} + \omega_0^2 x = f_0

  • Here, ω0\omega_0 remains unchanged, but the equilibrium position shifts from x=0x = 0 to x=f0ω02x = \frac{f_0}{\omega_0^2} (such as a hanging spring-mass system in gravity where f0=gf_0 = g).

    • Definition 4 (Time Average): The time average of a time-dependent physical quantity g(t)g(t) over period TT is defined as:

⟨g(t)⟩=1T∫0Tg(t) dt\langle g(t) \rangle = \frac{1}{T} \int_0^T g(t)\,dt

  • Remark 4 (Standard Harmonic Time Averages):

⟨cos⁡(ω0t±ϕ)⟩=⟨sin⁡(ω0t±ϕ)⟩=0\langle \cos(\omega_0 t \pm \phi) \rangle = \langle \sin(\omega_0 t \pm \phi) \rangle = 0

⟨cos⁡2(ω0t±ϕ)⟩=⟨sin⁡2(ω0t±ϕ)⟩=12\langle \cos^2(\omega_0 t \pm \phi) \rangle = \langle \sin^2(\omega_0 t \pm \phi) \rangle = \frac{1}{2}

Constitutive Differential Equation of Damped Motion

  • In the presence of damping forces, the total mechanical energy decreases over time:

ddt(12mx˙2+12mω02x2)<0\frac{d}{dt}\left(\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2\right) < 0

  • Assuming the resistive damping force is directly proportional to velocity, Fdamping=Γv=Γx˙F_{\text{damping}} = \Gamma v = \Gamma \dot{x} (where Γ>0\Gamma > 0 is a constant), the rate of energy loss equals dissipated power P=Fdampingv=Γx˙2P = F_{\text{damping}} v = \Gamma \dot{x}^2:

ddt(12mx˙2+12mω02x2)=−Γx˙2\frac{d}{dt}\left(\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2\right) = -\Gamma \dot{x}^2

mx˙x¨+mω02xx˙=−Γx˙2  ⟹  x¨+Γmx˙+ω02x=0m\dot{x}\ddot{x} + m\omega_0^2 x\dot{x} = -\Gamma \dot{x}^2 \implies \ddot{x} + \frac{\Gamma}{m}\dot{x} + \omega_0^2 x = 0

x¨+2γx˙+ω02x=0\ddot{x} + 2\gamma\dot{x} + \omega_0^2 x = 0

  • Remark 5 (Damping Factor):

    • The parameter γ=Γ2m\gamma = \frac{\Gamma}{2m} is defined as the damping factor.

    • Dimensional analysis: [γ][x˙]=[L][T−2]  ⟹  [γ]=[T−1][\gamma][\dot{x}] = [\text{L}][\text{T}^{-2}] \implies [\gamma] = [\text{T}^{-1}], matching the dimensions of frequency.

  • Theorem 2 (Classification of Damped Solutions): The solutions of x¨+2γx˙+ω02x=0\ddot{x} + 2\gamma\dot{x} + \omega_0^2 x = 0 under initial conditions x(0)=x0x(0) = x_0 and v(0)=v0v(0) = v_0 are classified as:

    • Non-oscillatory when γ≥ω0\gamma \ge \omega_0

    • Oscillatory when γ<ω0\gamma < \omega_0

  • Proof: Substituting the trial function x(t)=e−γtf(t)x(t) = e^{-\gamma t} f(t) into the differential equation:

x˙=e−γtdfdt−γe−γtf(t)\dot{x} = e^{-\gamma t}\frac{df}{dt} - \gamma e^{-\gamma t} f(t)

x¨=e−γt(d2fdt2−2γdfdt+γ2f)\ddot{x} = e^{-\gamma t}\left(\frac{d^2f}{dt^2} - 2\gamma \frac{df}{dt} + \gamma^2 f\right)

  • Substitution into x¨+2γx˙+ω02x=0\ddot{x} + 2\gamma\dot{x} + \omega_0^2 x = 0 yields:

e−γt[f¨+(ω02−γ2)f]=0e^{-\gamma t}\left[\ddot{f} + (\omega_0^2 - \gamma^2)f\right] = 0

  • Because e−γt≠0e^{-\gamma t} \neq 0 for all t∈[0,∞]t \in [0, \infty], the reduced equation for f(t)f(t) is:

f¨+(ω02−γ2)f=0\ddot{f} + (\omega_0^2 - \gamma^2)f = 0

Analysis of Overdamping (Large Damping: γ>ω0\gamma > \omega_0)

  • When γ>ω0\gamma > \omega_0, define α=γ2−ω02>0\alpha = \sqrt{\gamma^2 - \omega_0^2} > 0.

  • The auxiliary equation becomes f¨−α2f=0\ddot{f} - \alpha^2 f = 0, yielding f(t)=Aeαt+Be−αtf(t) = A e^{\alpha t} + B e^{-\alpha t}.

  • The general displacement function x(t)=e−γtf(t)x(t) = e^{-\gamma t} f(t) is:

x(t)=Ae(α−γ)t+Be−(α+γ)tx(t) = A e^{(\alpha - \gamma)t} + B e^{-(\alpha + \gamma)t}

  • Applying initial conditions x(0)=x0x(0) = x_0 and x˙(0)=v0\dot{x}(0) = v_0:

x(0)=A+B=x0x(0) = A + B = x_0

x˙(0)=A(α−γ)−B(α+γ)=v0\dot{x}(0) = A(\alpha - \gamma) - B(\alpha + \gamma) = v_0

  • Solving for integration constants AA and BB yields:

A=x0(α+γ)+v02αA = \frac{x_0(\alpha + \gamma) + v_0}{2\alpha}

B=x0(α−γ)−v02αB = \frac{x_0(\alpha - \gamma) - v_0}{2\alpha}

  • The complete displacement equation is:

x(t)=[x0(α+γ)+v02α]e(α−γ)t+[x0(α−γ)−v02α]e−(α+γ)tx(t) = \left[\frac{x_0(\alpha + \gamma) + v_0}{2\alpha}\right] e^{(\alpha - \gamma)t} + \left[\frac{x_0(\alpha - \gamma) - v_0}{2\alpha}\right] e^{-(\alpha + \gamma)t}

  • Time Axis Intersections: Setting x(t0)=0x(t_0) = 0 determines when the path crosses the equilibrium axis:

t0=12αln⁡(v0+x0(γ−α)v0+x0(γ+α))t_0 = \frac{1}{2\alpha} \ln\left(\frac{v_0 + x_0(\gamma - \alpha)}{v_0 + x_0(\gamma + \alpha)}\right)

  • Sub-case Analysis:

    • Case (a) (x0=0x_0 = 0, v0≠0v_0 \neq 0):

x(t)=(v0α)e−γtsinh⁡(αt)x(t) = \left(\frac{v_0}{\alpha}\right) e^{-\gamma t} \sinh(\alpha t)

- Solving t0t_0 gives t0=0t_0 = 0 as the sole axis crossing.
  • Case (b) (x0≠0x_0 \neq 0, v0=0v_0 = 0):

x(t)=x0e−γtcosh⁡(αt)+(x0γα)e−γtsinh⁡(αt)x(t) = x_0 e^{-\gamma t} \cosh(\alpha t) + \left(\frac{x_0 \gamma}{\alpha}\right) e^{-\gamma t} \sinh(\alpha t)

- Evaluating t0t_0 yields t0=12αln⁡(γ−αγ+α)<0t_0 = \frac{1}{2\alpha} \ln\left(\frac{\gamma - \alpha}{\gamma + \alpha}\right) < 0. Because t0t_0 is negative, the displacement curve never intersects the tt-axis for t>0t > 0


Overdamped displacement vs time for two different initial conditions


Phase space diagram for overdamped motion
  • Case (c) (Arbitrary Initial Conditions x(0)=x0≠0x(0) = x_0 \neq 0, v(0)=v0v(0) = v_0):

t0=12αln⁡[v0x0+(γ−α)v0x0+(γ+α)]t_0 = \frac{1}{2\alpha} \ln\left[\frac{\frac{v_0}{x_0} + (\gamma - \alpha)}{\frac{v_0}{x_0} + (\gamma + \alpha)}\right]

- If v0x0>0\frac{v_0}{x_0} > 0 (x0x_0 and v0v_0 share the same sign, meaning the particle is pushed away from origin), the logarithmic argument is strictly less than 11, yielding t0<0t_0 < 0 (no physical crossing for t>0t > 0).
- If v0x0<0\frac{v_0}{x_0} < 0 (particle is projected back toward origin):
  - If ∣v0x0∣>γ+α>γ−α\left|\frac{v_0}{x_0}\right| > \gamma + \alpha > \gamma - \alpha, t0>0t_0 > 0 exists. The particle crosses the origin once before asymptotic return as t→∞t \to \infty
  - If γ+α>∣v0x0∣>γ−α\gamma + \alpha > \left|\frac{v_0}{x_0}\right| > \gamma - \alpha or γ+α>γ−α>∣v0x0∣\gamma + \alpha > \gamma - \alpha > \left|\frac{v_0}{x_0}\right|, no positive real solution for t0t_0 exists.
- Expressed in terms of initial velocity v(0)=v0≠0v(0) = v_0 \neq 0:

t0=12αln⁡[1+x0v0(γ−α)1+x0v0(γ+α)]t_0 = \frac{1}{2\alpha} \ln\left[\frac{1 + \frac{x_0}{v_0}(\gamma - \alpha)}{1 + \frac{x_0}{v_0}(\gamma + \alpha)}\right]


Overdamped displacement and velocity vs time crossing origin


Overdamped displacement and velocity vs time kicked away from origin


Phase space trajectories for overdamped motion with arbitrary initial conditions
  • Turning Point Dynamics:

    • For Case (a), setting x˙(t0)=0\dot{x}(t_0) = 0 gives:

x˙(t)=(v0α)[αe−γtcosh⁡(αt)−γe−γtsinh⁡(αt)]=0\dot{x}(t) = \left(\frac{v_0}{\alpha}\right)\left[\alpha e^{-\gamma t} \cosh(\alpha t) - \gamma e^{-\gamma t} \sinh(\alpha t)\right] = 0

tanh⁡(αt0)=αγ  ⟹  t0=1αtanh⁡−1(αγ)\tanh(\alpha t_0) = \frac{\alpha}{\gamma} \implies t_0 = \frac{1}{\alpha} \tanh^{-1}\left(\frac{\alpha}{\gamma}\right)

  • Case (b) exhibits no turning point. Highly damped non-oscillatory behavior of this type is described as dead beat.

Analysis of Critical Damping (γ=ω0\gamma = \omega_0)

  • When γ=ω0\gamma = \omega_0, f¨=0  ⟹  f(t)=At+B\ddot{f} = 0 \implies f(t) = A t + B.

  • The general displacement function is:

x(t)=e−γt(At+B)x(t) = e^{-\gamma t}(A t + B)

  • Applying initial conditions x(0)=x0x(0) = x_0 and x˙(0)=v0\dot{x}(0) = v_0 gives B=x0B = x_0 and A=v0+γx0A = v_0 + \gamma x_0, yielding:

x(t)=e−γt[v0t+x0(1+γt)]x(t) = e^{-\gamma t}\left[v_0 t + x_0(1 + \gamma t)\right]

  • Time Axis Intersections: Setting x(t0)=0x(t_0) = 0 yields:

t0=−x0v0+γx0t_0 = -\frac{x_0}{v_0 + \gamma x_0}

  • Specific Cases:

    • For x0=0x_0 = 0, v0≠0v_0 \neq 0: x(t)=v0te−γtx(t) = v_0 t e^{-\gamma t}, crossing the time axis only at t=0t = 0

    • For x0≠0x_0 \neq 0, v0=0v_0 = 0: x(t)=x0(1+γt)e−γtx(t) = x_0(1 + \gamma t)e^{-\gamma t}, yielding t0=−1γ<0t_0 = -\frac{1}{\gamma} < 0 (no positive intersection).


Critically damped displacement vs time for two initial conditions


Phase space diagram for critically damped motion
  • Parametric Crossing Conditions:

    • For x0=−ζ0x_0 = -\zeta_0 (ζ0>0\zeta_0 > 0) and v0>0v_0 > 0:

t0=ζ0v0−γζ0t_0 = \frac{\zeta_0}{v_0 - \gamma \zeta_0}

- Positivity of t0t_0 requires γ<v0ζ0\gamma < \frac{v_0}{\zeta_0}.
  • For x0=ξ0>0x_0 = \xi_0 > 0 and v0=−η0<0v_0 = -\eta_0 < 0 (η0>0\eta_0 > 0):

t0=ξ0η0−γξ0t_0 = \frac{\xi_0}{\eta_0 - \gamma \xi_0}

- Positivity of t0t_0 requires γ<η0x0\gamma < \frac{\eta_0}{x_0}.


Critically damped displacement and velocity vs time with positive time-axis crossing


Critically damped displacement and velocity vs time with no positive axis crossing


Phase space diagram for critical damping with arbitrary initial conditions
  • Turning Point Analysis: For x0=0x_0 = 0 and v0≠0v_0 \neq 0:

x˙(t)=v0[e−γt−γte−γt]=0  ⟹  t0=1γ=1ω0\dot{x}(t) = v_0\left[e^{-\gamma t} - \gamma t e^{-\gamma t}\right] = 0 \implies t_0 = \frac{1}{\gamma} = \frac{1}{\omega_0}

  • Critical damping provides the fastest rate of decay to equilibrium without overshoot or oscillation.

Analysis of Weak Damping (γ<ω0\gamma < \omega_0)

  • When γ<ω0\gamma < \omega_0, define ω~=ω02−γ2>0\tilde{\omega} = \sqrt{\omega_0^2 - \gamma^2} > 0

  • The differential equation for f(t)f(t) becomes f¨=−ω~2f\ddot{f} = -\tilde{\omega}^2 f, with general solution f(t)=Aeiω~t+Be−iω~tf(t) = A e^{i\tilde{\omega}t} + B e^{-i\tilde{\omega}t}.

  • Applying initial conditions x(0)=x0x(0) = x_0 and x˙(0)=v0\dot{x}(0) = v_0:

x(0)=A+B=x0x(0) = A + B = x_0

x˙(0)=−A(γ−iω~)−B(γ+iω~)=v0\dot{x}(0) = -A(\gamma - i\tilde{\omega}) - B(\gamma + i\tilde{\omega}) = v_0

  • Solving for AA and BB yields:

A=x0(iω~+γ)+v02iω~A = \frac{x_0(i\tilde{\omega} + \gamma) + v_0}{2i\tilde{\omega}}

B=x0(iω~−γ)−v02iω~B = \frac{x_0(i\tilde{\omega} - \gamma) - v_0}{2i\tilde{\omega}}

  • Substituting AA and BB into x(t)=e−γt(Aeiω~t+Be−iω~t)x(t) = e^{-\gamma t}(A e^{i\tilde{\omega}t} + B e^{-i\tilde{\omega}t}) produces:

x(t)=e−γt[x0cos⁡(ω~t)+(x0γ+v0ω~)sin⁡(ω~t)]x(t) = e^{-\gamma t}\left[x_0 \cos(\tilde{\omega} t) + \left(\frac{x_0\gamma + v_0}{\tilde{\omega}}\right) \sin(\tilde{\omega} t)\right]

x(t)=Ce−γtcos⁡(ω~t−θ0)x(t) = C e^{-\gamma t} \cos(\tilde{\omega} t - \theta_0)

  • In this expression, amplitude envelope CC and phase angle θ0\theta_0 are defined by:

C=1ω~x02ω~2+(x0γ+v0)2C = \frac{1}{\tilde{\omega}}\sqrt{x_0^2 \tilde{\omega}^2 + (x_0\gamma + v_0)^2}

θ0=tan⁡−1(x0γ+v0x0ω~)\theta_0 = \tan^{-1}\left(\frac{x_0\gamma + v_0}{x_0\tilde{\omega}}\right)

  • Specific Initial Condition Examples:

    • Case 1 (x(0)=0x(0) = 0, v(0)=v0≠0v(0) = v_0 \neq 0):

x(t)=(v0ω~)e−γtsin⁡(ω~t)x(t) = \left(\frac{v_0}{\tilde{\omega}}\right) e^{-\gamma t} \sin(\tilde{\omega} t)

  • Case 2 (x(0)=x0≠0x(0) = x_0 \neq 0, v(0)=0v(0) = 0):

x(t)=(x0ω0ω~)e−γtcos⁡(ω~t−tan⁡−1(γω~))x(t) = \left(\frac{x_0 \omega_0}{\tilde{\omega}}\right) e^{-\gamma t} \cos\left(\tilde{\omega} t - \tan^{-1}\left(\frac{\gamma}{\tilde{\omega}}\right)\right)


Weakly damped displacement vs time for two initial conditions


Phase space diagram for weakly damped motion
  • Quasi-Periodicity and Extrema Characteristics:

    • Zero-crossings occur at time intervals separated by Δt=πω~\Delta t = \frac{\pi}{\tilde{\omega}}. The quasi-period is T~=2πω~\tilde{T} = \frac{2\pi}{\tilde{\omega}}.

    • The time interval between a maximum and the subsequent minimum is πω~\frac{\pi}{\tilde{\omega}}, though extrema do not fall precisely halfway between zero-crossings.

    • Extrema occur when x˙(t)=0\dot{x}(t) = 0:

cos⁡(ω~t)−(γω~)sin⁡(ω~t)=0  ⟹  tan⁡(ω~t)=ω~γ\cos(\tilde{\omega} t) - \left(\frac{\gamma}{\tilde{\omega}}\right) \sin(\tilde{\omega} t) = 0 \implies \tan(\tilde{\omega} t) = \frac{\tilde{\omega}}{\gamma}

  • In the limit as γω~→0\frac{\gamma}{\tilde{\omega}} \to 0, ω~t→π2  ⟹  t→π2ω~\tilde{\omega} t \to \frac{\pi}{2} \implies t \to \frac{\pi}{2\tilde{\omega}}.

Energy, Power Dissipation, and Characteristics of Weakly Damped Oscillations

  • Energy Derivation under Weak Damping (γ≪ω0\gamma \ll \omega_0):

    • Writing displacement as x(t)=A(t)sin⁡(ω~t)x(t) = A(t) \sin(\tilde{\omega} t), where A(t)=(v0ω~)e−γtA(t) = \left(\frac{v_0}{\tilde{\omega}}\right) e^{-\gamma t} is the time-decaying amplitude.

    • The total instantaneous energy E(t)=12mx˙2+12mω02x2E(t) = \frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2 expands to:

E(t)=12m(v02ω~2)e−2γt[ω~2cos⁡2(ω~t)+γ2sin⁡2(ω~t)−2ω~γcos⁡(ω~t)sin⁡(ω~t)]+12mω02(v02ω~2)e−2γtsin⁡2(ω~t)E(t) = \frac{1}{2}m\left(\frac{v_0^2}{\tilde{\omega}^2}\right) e^{-2\gamma t}\left[\tilde{\omega}^2 \cos^2(\tilde{\omega} t) + \gamma^2 \sin^2(\tilde{\omega} t) - 2\tilde{\omega}\gamma \cos(\tilde{\omega} t) \sin(\tilde{\omega} t)\right] + \frac{1}{2}m\omega_0^2\left(\frac{v_0^2}{\tilde{\omega}^2}\right) e^{-2\gamma t} \sin^2(\tilde{\omega} t)

  • Over one quasi-period T~\tilde{T}, assuming e−2γte^{-2\gamma t} changes negligibly over single cycles (γ≪ω0\gamma \ll \omega_0), time averaging yields:

⟨cos⁡2(ω~t)⟩≈12\langle \cos^2(\tilde{\omega} t) \rangle \approx \frac{1}{2}

⟨sin⁡2(ω~t)⟩≈12\langle \sin^2(\tilde{\omega} t) \rangle \approx \frac{1}{2}

⟨sin⁡(2ω~t)⟩≈0\langle \sin(2\tilde{\omega} t) \rangle \approx 0

  • The cycle-averaged total energy is:

⟨E(t)⟩=1T~∫0T~E(t) dt=mv024ω~2e−2γt[ω~2+ω02+γ2]=12mA02ω02e−2γt\langle E(t) \rangle = \frac{1}{\tilde{T}} \int_0^{\tilde{T}} E(t)\,dt = \frac{m v_0^2}{4\tilde{\omega}^2} e^{-2\gamma t}\left[\tilde{\omega}^2 + \omega_0^2 + \gamma^2\right] = \frac{1}{2}m A_0^2 \omega_0^2 e^{-2\gamma t}

  • In this expression, A02=v02ω~2A_0^2 = \frac{v_0^2}{\tilde{\omega}^2} and ω~2=ω02−γ2\tilde{\omega}^2 = \omega_0^2 - \gamma^2


Time-averaged total energy vs time for weakly damped oscillation
  • Power Dissipation:

    • Instantaneous power dissipated by resistive force: Pdamping=Fdamping⋅v=2mγx˙2P_{\text{damping}} = F_{\text{damping}} \cdot v = 2m\gamma \dot{x}^2

    • Cycle-averaged dissipated power over T~\tilde{T}:

⟨P(t)⟩=12mA02ω02(2γ)e−2γt=2γ⟨E(t)⟩\langle P(t) \rangle = \frac{1}{2}m A_0^2 \omega_0^2 (2\gamma) e^{-2\gamma t} = 2\gamma \langle E(t) \rangle

  • Logarithmic Decrement:

    • Consider displacement peaks at quarter-period offsets t=T~4,3T~4,5T~4,…t = \frac{\tilde{T}}{4}, \frac{3\tilde{T}}{4}, \frac{5\tilde{T}}{4}, \dots


Logarithmic decrement amplitude peaks for weakly damped oscillation
  • Absolute amplitude values at successive half-period intervals:

A1=∣A(t=T~4)∣=A0e−γT~4A_1 = \left| A\left(t = \frac{\tilde{T}}{4}\right) \right| = A_0 e^{-\frac{\gamma \tilde{T}}{4}}

A2=∣A(t=3T~4)∣=A0e−3γT~4A_2 = \left| A\left(t = \frac{3\tilde{T}}{4}\right) \right| = A_0 e^{-\frac{3\gamma \tilde{T}}{4}}

A3=∣A(t=5T~4)∣=A0e−5γT~4A_3 = \left| A\left(t = \frac{5\tilde{T}}{4}\right) \right| = A_0 e^{-\frac{5\gamma \tilde{T}}{4}}

  • Ratio of successive amplitudes:

A1A2=A2A3=A3A4=⋯=An−1An=eγT~2=Δ\frac{A_1}{A_2} = \frac{A_2}{A_3} = \frac{A_3}{A_4} = \dots = \frac{A_{n-1}}{A_n} = e^{\frac{\gamma \tilde{T}}{2}} = \Delta

ln⁡(Δ)=γT~2\ln(\Delta) = \frac{\gamma \tilde{T}}{2}

  • For nn consecutive peaks:

A1An=A1A2⋅A2A3…An−1An=Δn−1  ⟹  ln⁡(A1An)=(n−1)ln⁡(Δ)\frac{A_1}{A_n} = \frac{A_1}{A_2} \cdot \frac{A_2}{A_3} \dots \frac{A_{n-1}}{A_n} = \Delta^{n-1} \implies \ln\left(\frac{A_1}{A_n}\right) = (n-1)\ln(\Delta)

ln⁡(Δ)=1n−1ln⁡(A1An)\ln(\Delta) = \frac{1}{n-1}\ln\left(\frac{A_1}{A_n}\right)

  • Definition 5: Logarithmic decrement λ\lambda is the natural logarithm of the ratio of two successive amplitudes separated by a half period T~2\frac{\tilde{T}}{2}:

λ=ln⁡(Δ)=γT~2\lambda = \ln(\Delta) = \frac{\gamma \tilde{T}}{2}

  • Relaxation Time:

    • Definition 6: Relaxation time τ=1γ\tau = \frac{1}{\gamma} is the time required for the amplitude to decay to 1e\frac{1}{e} of its initial magnitude.

    • Remark 9: Relationship between logarithmic decrement λ\lambda and relaxation time τ\tau:

λτ=T~2\lambda \tau = \frac{\tilde{T}}{2}

  • Quality Factor (QQ-Value):

    • From ⟨E(t)⟩=(2γ)−1⟨P(t)⟩\langle E(t) \rangle = (2\gamma)^{-1} \langle P(t) \rangle, multiplying both sides by T~\tilde{T} yields:

T~⟨E(t)⟩=T~(2γ)−1⟨P(t)⟩\tilde{T} \langle E(t) \rangle = \tilde{T}(2\gamma)^{-1} \langle P(t) \rangle

(2πω~)⟨E(t)⟩=(2πω~)(2γ)−1⟨P(t)⟩  ⟹  ω~2γ=2π⟨E(t)⟩T~⟨P(t)⟩\left(\frac{2\pi}{\tilde{\omega}}\right) \langle E(t) \rangle = \left(\frac{2\pi}{\tilde{\omega}}\right) (2\gamma)^{-1} \langle P(t) \rangle \implies \frac{\tilde{\omega}}{2\gamma} = \frac{2\pi \langle E(t) \rangle}{\tilde{T} \langle P(t) \rangle}

  • Definition 7: Quality factor Q=ω~2γQ = \frac{\tilde{\omega}}{2\gamma} is defined physically as:

Q=2π(Average energy stored in one periodAverage energy lost in one period)Q = 2\pi \left(\frac{\text{Average energy stored in one period}}{\text{Average energy lost in one period}}\right)

Solved Worked Examples and Practice Problems

  • Problem 1: The governing differential equation of a damped system is given by 5x¨+0.01x˙+α2x=05\ddot{x} + 0.01\dot{x} + \alpha^2 x = 0

    • (i) Find damping factor γ\gamma and natural frequency ω0\omega_0 for α=55\alpha = 5\sqrt{5}:

    • Divide equation by 55:

x¨+0.002x˙+25x=0\ddot{x} + 0.002\dot{x} + 25 x = 0

- Comparing with x¨+2γx˙+ω02x=0\ddot{x} + 2\gamma\dot{x} + \omega_0^2 x = 0 gives 2γ=0.002  ⟹  γ=0.001 s−12\gamma = 0.002 \implies \gamma = 0.001\,\text{s}^{-1} and ω02=25  ⟹  ω0=5 s−1\omega_0^2 = 25 \implies \omega_0 = 5\,\text{s}^{-1}.
  • (ii) Find conditions on α\alpha for large, critical, and weak damping:

    • Large damping (γ>ω0\gamma > \omega_0): α>0.001\alpha > 0.001

    • Critical damping (γ=ω0\gamma = \omega_0): α=0.001\alpha = 0.001

    • Weak damping (γ<ω0\gamma < \omega_0): α<0.001\alpha < 0.001

  • (iii) Find x(t)x(t) for α=55\alpha = 5\sqrt{5} if x(0)=3x(0) = 3 and v(0)=0v(0) = 0:

    • Weakly damped general solution: x(t)=e−γt[Acos⁡(ω~t)+Bsin⁡(ω~t)]x(t) = e^{-\gamma t}\left[A \cos(\tilde{\omega} t) + B \sin(\tilde{\omega} t)\right]

    • Here ω~=ω02−γ2=25−(0.001)2≈5 s−1\tilde{\omega} = \sqrt{\omega_0^2 - \gamma^2} = \sqrt{25 - (0.001)^2} \approx 5\,\text{s}^{-1}.

    • Applying initial conditions: x(0)=3=Ax(0) = 3 = A, and v(0)=−γA+Bω~=0  ⟹  B=γAω~=0.001×35=6×10−4v(0) = -\gamma A + B\tilde{\omega} = 0 \implies B = \frac{\gamma A}{\tilde{\omega}} = \frac{0.001 \times 3}{5} = 6 \times 10^{-4}.

    • Displacement function:

x(t)≈e−0.001t[3cos⁡(5t)+6×10−4sin⁡(5t)]x(t) \approx e^{-0.001 t}\left[3 \cos(5t) + 6 \times 10^{-4} \sin(5t)\right]

  • (iv) Repeat (iii) for initial conditions x(0)=5x(0) = 5 and v(0)=3v(0) = 3:

    • A=5A = 5, and 3 = -\gamma A + \tilde{\omega} B \implies 3 = -(0.001)(5) + 5 B \implies B = \frac{3.005}{5} = 0.601$.\n - Solution: x(t) = e^{-0.001 t}\left[5 \cos(5t) + 0.601 \sin(5t)\right].\n\n- **Problem 2:** A massless string suspended from a rigid rod carries a mass of 200\,\text{g}atitslowerend.Thesystemoscillateswithaperiodofat its lower end. The system oscillates with a period of0.2\,\text{s},andamplitudereducestohalfitsinitialvaluein, and amplitude reduces to half its initial value in30\,\text{s}. Calculate (a) relaxation time, (b) quality factor, and (c) logarithmic decrement.\n - **Solution:**\n - **(a) Relaxation Time:** Using A(t) = A(0)e^{-\gamma t},,\gamma t = \ln\left(\frac{A(0)}{A(t)} ight).For. Fort = 30\,\text{s}andand\frac{A(0)}{A(30)} = 2:\n\n\gamma (30) = \ln(2) \implies \gamma = \frac{\ln(2)}{30} \approx 0.023\,\text{s}^{-1}\n\n\tau = \frac{1}{\gamma} = \frac{30}{\ln(2)} \approx 43.28\,\text{s}\n\n - **(b) Quality Factor:** Natural frequency \omega_0 = \frac{2\pi}{T} = \frac{2\pi}{0.2} = 31.4\,\text{s}^{-1}.\n\nQ = \frac{\tilde{\omega}}{2\gamma} = \frac{\sqrt{\omega_0^2 - \gamma^2}}{2\gamma} \approx \frac{31.4}{2 \times 0.023} \approx 683\n\n - **(c) Logarithmic Decrement:**\n\n\lambda = \frac{\gamma \tilde{T}}{2} = \frac{\gamma \pi}{\tilde{\omega}} \approx \frac{0.023 \times \pi}{31.4} \approx 0.0025\n\n- **Problem 3:** A critically damped mechanical system is displaced by distance x_0fromequilibriumandreleasedfromrest.Showthatfrom equilibrium and released from rest. Show thatx(t) = x_0(1 + \omega_0 t)e^{-\omega_0 t}.\n - **Solution:**\n - For critical damping (\gamma = \omega_0),),x(t) = e^{-\gamma t}(A t + B).\n - Applying x(0) = x_0 \implies B = x_0\n - Applying v(0) = 0 = \left[-\gamma e^{-\gamma t}(A t + B) + e^{-\gamma t} A\right]{t=0} = -\gamma B + A \implies A = \gamma B = \gamma x_0 = \omega_0 x_0\n - Substituting constants yields:\n\nx(t) = x_0(1 + \omega_0 t)e^{-\omega_0 t}\n\n- **Problem 4:** A weakly damped oscillator has mass m,oscillationfrequency, oscillation frequency\alpha,andlogarithmicdecrement, and logarithmic decrement\lambda. Calculate the stiffness force and resistive force.\n - **Solution:**\n - Given damped frequency \tilde{\omega} = \alphaandlogarithmicdecrementand logarithmic decrement\lambda = \frac{\gamma \pi}{\alpha} \implies \gamma = \frac{\lambda \alpha}{\pi}.\n - Natural frequency relation: \omega_0^2 = \tilde{\omega}^2 + \gamma^2 = \alpha^2 + \frac{\lambda^2 \alpha^2}{\pi^2} = \alpha^2\left(1 + \frac{\lambda^2}{\pi^2}\right).\n - Stiffness force parameter:\n\nk x = m \omega_0^2 x = m \alpha^2 \left(1 + \frac{\lambda^2}{\pi^2}\right) x\n\n - Resistive damping force parameter:\n\n2 m \gamma v = \frac{2 m \lambda \alpha v}{\pi}\n\n- **Problem 5:** The ratio between frequency \tilde{\omega}ofaweaklydampedoscillatorandnaturalfrequencyof a weakly damped oscillator and natural frequency\omega_0isisr : 1(i.e.(i.e.\frac{\tilde{\omega}}{\omega_0} = r).\n - **(i) Logarithmic decrement \lambdaandQualityfactorand Quality factorQ:**\n - Damping factor \gamma = \sqrt{\omega_0^2 - \tilde{\omega}^2} = \omega_0 \sqrt{1 - r}\n - Logarithmic decrement:\n\n\lambda = \frac{\gamma \pi}{\tilde{\omega}} = \frac{\pi \sqrt{1 - r}}{r}\n\n - Quality factor:\n\nQ = \frac{\tilde{\omega}}{2\gamma} = \frac{r}{2\sqrt{1 - r}}\n\n - **(ii) System energy and time taken to reduce to \frac{1}{e}ofinitialenergyformaximuminitialdisplacementof initial energy for maximum initial displacementx{\text{max}}:**\n - Energy expression:\n\nE(t) = \frac{1}{2} m \omega_0^2 x_{\text{max}}^2 e^{-2\gamma t} = \frac{1}{2} m \omega_0^2 x_{\text{max}}^2 e^{-2\omega_0 \sqrt{1 - r} t}\n\n - Time t_1toreachto reach\frac{1}{e} initial energy:\n\n\frac{E(t_1)}{E(0)} = \frac{1}{e} = e^{-2\gamma t_1} \implies t_1 = \frac{1}{2\gamma} = \frac{1}{2\omega_0 \sqrt{1 - r}}\n\n - **(iii) Energy loss during the first cycle:**\n - Time for one cycle t = \frac{2\pi}{\tilde{\omega}}. Energy remaining after first cycle:\n\nE\left(\frac{2\pi}{\tilde{\omega}}\right) = E(0) e^{-\frac{4\pi \gamma}{\tilde{\omega}}}\n\n - Energy lost during first cycle:\n\n\Delta E = E(0) - E\left(\frac{2\pi}{\tilde{\omega}}\right) = E(0)\left(1 - e^{-\frac{4\pi}{r}\sqrt{1-r}}\right)</p></li></ul></li></ul><h5>IntroductiontoDampedOscillation</h5><ul><li><p>SimpleHarmonicMotion(SHM)isalsoknownasfreeoscillation,whereasystemoscillatesbackandforthwithoutstopping.</p></li><li><p>Inreallife,freeoscillationsdonotlastforeverbecausefriction,airresistance,andotheropposingforcesslowthemdownandreducetheirtotalenergyovertime.</p></li><li><p>Theseopposingforcesarecalleddampingforces.Dampingcanslowdownthemotionorevenstopthesystemfromswingingaltogether,causingittoreturntoitsrestpositionsmoothly.</p></li><li><p>Dampedmotionisdividedintodifferenttypesbasedontherelationshipbetweenthenaturalfrequency</p></li></ul></li></ul><h5>Introduction to Damped Oscillation</h5><ul><li><p>Simple Harmonic Motion (SHM) is also known as free oscillation, where a system oscillates back and forth without stopping.</p></li><li><p>In real life, free oscillations do not last forever because friction, air resistance, and other opposing forces slow them down and reduce their total energy over time.</p></li><li><p>These opposing forces are called damping forces. Damping can slow down the motion or even stop the system from swinging altogether, causing it to return to its rest position smoothly.</p></li><li><p>Damped motion is divided into different types based on the relationship between the natural frequency\omega_0andthedampingfactorand the damping factor\gamma.</p></li></ul><h5>SimpleHarmonicMotionPrimer</h5><ul><li><p><strong>Definition1:</strong>AparticleundergoesSimpleHarmonicMotion(SHM)whenthetotalforcepullingitbacktoitsstartingpointisdirectlyproportionaltohowfarithasmoved,andactsintheoppositedirectionofthatmovement.</p></li><li><p>ThebasicequationofmotionforSHMis:<br>.</p></li></ul><h5>Simple Harmonic Motion Primer</h5><ul><li><p><strong>Definition 1:</strong> A particle undergoes Simple Harmonic Motion (SHM) when the total force pulling it back to its starting point is directly proportional to how far it has moved, and acts in the opposite direction of that movement.</p></li><li><p>The basic equation of motion for SHM is:<br>m\ddot{x} = -k x</p></li><li><p>Inthisequation,</p></li><li><p>In this equation,misthemassoftheparticle,is the mass of the particle,x(t)isitspositionattimeis its position at timet,,\dot{x} = \frac{dx}{dt}isitsvelocity,is its velocity,\ddot{x} = \frac{d^2 x}{dt^2}isitsacceleration,andis its acceleration, andk > 0isthestiffnessconstantofthespringorrestoringforce.</p></li><li><p>Wecanrewritethisequationinstandardcanonicalformas:<br>is the stiffness constant of the spring or restoring force.</p></li><li><p>We can rewrite this equation in standard canonical form as:<br>\ddot{x} = -\omega_0^2 x</p></li><li><p>Here,</p></li><li><p>Here,\omega0 > 0isthenaturalfrequencyofthesystem,definedasis the natural frequency of the system, defined as\omega0 = \sqrt{\frac{k}{m}}.</p></li><li><p><strong>Remark1(LinearityandHomogeneity):</strong></p><ul><li><p>Linearity:If.</p></li><li><p><strong>Remark 1 (Linearity and Homogeneity):</strong></p><ul><li><p>Linearity: Ifx1(t)andandx2(t)aretwodifferentvalidsolutionstotheequation,anylinearcombinationare two different valid solutions to the equation, any linear combinationx(t) = c1 x1(t) + c2 x2(t)(where(wherec1andandc2areconstants)isalsoavalidsolution.</p></li><li><p>Homogeneity:Alltermsdependonare constants) is also a valid solution.</p></li><li><p>Homogeneity: All terms depend onxoritstimederivatives,meaningor its time derivatives, meaningx(t) = 0(stayingcompletelystill)isalsoavalidsolution.</p></li></ul></li><li><p><strong>DerivationoftheGeneralSolution:</strong></p><ul><li><p>Wetryatrialsolutionoftheform(staying completely still) is also a valid solution.</p></li></ul></li><li><p><strong>Derivation of the General Solution:</strong></p><ul><li><p>We try a trial solution of the formx(t) = e^{\lambda t}.Thisgivesvelocity. This gives velocity\dot{x}(t) = \lambda e^{\lambda t}andaccelerationand acceleration\ddot{x}(t) = \lambda^2 e^{\lambda t}.</p></li><li><p>Substitutingtheseintothestandardequationgives:<br>.</p></li><li><p>Substituting these into the standard equation gives:<br>(\lambda^2 + \omega_0^2) e^{\lambda t} = 0</p></li><li><p>Since</p></li><li><p>Sincee^{\lambda t}isneverzero,wegetthecharacteristicequationis never zero, we get the characteristic equation\lambda^2 + \omega0^2 = 0,whichyieldscomplexroots, which yields complex roots\lambda = \pm i\omega0</p></li><li><p>Thegeneralsolutionis:<br></p></li><li><p>The general solution is:<br>x(t) = c1 e^{i\omega0 t} + c2 e^{-i\omega0 t}</p></li></ul></li><li><p><strong>Remark2(PhysicalRealityCondition):</strong></p><ul><li><p>Sincephysicaldisplacement</p></li></ul></li><li><p><strong>Remark 2 (Physical Reality Condition):</strong></p><ul><li><p>Since physical displacementx(t)mustbearealnumber,must be a real number,x(t)mustequalitscomplexconjugatemust equal its complex conjugatex^*(t).</p></li><li><p>Thisrequirementforces.</p></li><li><p>This requirement forcesc1andandc2tobecomplexconjugatesofeachother(to be complex conjugates of each other (c1 = c2^*).</p></li><li><p>Setting).</p></li><li><p>Settingc1 = A e^{-i\theta}(where(whereAandand\thetaarerealconstants)givesthephysicaldisplacementformula:are real constants) gives the physical displacement formula:x(t) = 2A \cos(\omega0 t - \theta)</p></li></ul></li><li><p><strong>FindingConstantsusingInitialConditions:</strong></p><ul><li><p><strong>CaseI(Startsatoriginwithinitialvelocity</p></li></ul></li><li><p><strong>Finding Constants using Initial Conditions:</strong></p><ul><li><p><strong>Case I (Starts at origin with initial velocityv(0) = v0andpositionand positionx(0) = 0):</em></strong><em><br>):</em></strong><em><br>x(t) = \left(\frac{v0}{\omega0}\right) \sin(\omega0 t)</p></li><li><p><strong>CaseII(Releasedfromrestatposition</p></li><li><p><strong>Case II (Released from rest at positionx(0) = x0withvelocitywith velocityv(0) = 0):</em></strong><em><br>):</em></strong><em><br>x(t) = x0 \cos(\omega_0 t)</p></li></ul></li><li><p><strong>EnergyConservationinSHM:</strong></p><ul><li><p>Thetotalenergy</p></li></ul></li><li><p><strong>Energy Conservation in SHM:</strong></p><ul><li><p>The total energyEofthesystemremainsconstantovertime:<br>of the system remains constant over time:<br>\frac{d}{dt}\left(\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega0^2 x^2\right) = 0\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega0^2 x^2 = \text{constant}</p></li><li><p>Dividingbytotalenergygivesthenormalizedpathequation:<br></p></li><li><p>Dividing by total energy gives the normalized path equation:<br>\left(\frac{\dot{x}}{\omega0 x0}\right)^2 + \left(\frac{x}{x_0}\right)^2 = 1</p></li></ul></li><li><p><strong>Remark3(PhaseSpaceRepresentation):</strong></p><ul><li><p>Agraphplottingposition</p></li></ul></li><li><p><strong>Remark 3 (Phase Space Representation):</strong></p><ul><li><p>A graph plotting positionx(t)againstvelocityagainst velocity\dot{x}(t)iscalledPhaseSpace.</p></li><li><p>ForSHM,thetrajectoryformsanellipseinphasespace.Aclosedloopinphasespacemeansthemotionrepeatsperiodically.</p></li></ul></li><li><p><strong>Definition4(TimeAverage):</strong></p><ul><li><p>Thetimeaverageofaquantityis called Phase Space.</p></li><li><p>For SHM, the trajectory forms an ellipse in phase space. A closed loop in phase space means the motion repeats periodically.</p></li></ul></li><li><p><strong>Definition 4 (Time Average):</strong></p><ul><li><p>The time average of a quantityg(t)overatimeperiodover a time periodTis:<br>is:<br>\langle g(t) \rangle = \frac{1}{T} \int_0^T g(t)\,dt</p></li><li><p>Usefulstandardaverages:<br></p></li><li><p>Useful standard averages:<br>\langle \cos(\omega0 t \pm \phi) \rangle = \langle \sin(\omega0 t \pm \phi) \rangle = 0<br><br>\langle \cos^2(\omega0 t \pm \phi) \rangle = \langle \sin^2(\omega0 t \pm \phi) \rangle = \frac{1}{2}</p></li></ul></li></ul><h5>ConstitutiveDifferentialEquationofDampedMotion</h5><ul><li><p>Whendampingispresent,totalmechanicalenergydecreasesovertimeduetodragforces,whichareproportionaltovelocity(</p></li></ul></li></ul><h5>Constitutive Differential Equation of Damped Motion</h5><ul><li><p>When damping is present, total mechanical energy decreases over time due to drag forces, which are proportional to velocity (F_{\text{damping}} = \Gamma \dot{x}).</p></li><li><p>Therateofenergylossequalsthedissipatedpower).</p></li><li><p>The rate of energy loss equals the dissipated powerP = \Gamma \dot{x}^2:<br>:<br>\frac{d}{dt}\left(\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2\right) = -\Gamma \dot{x}^2</p></li><li><p>Thissimplifiestothefundamentaldifferentialequationfordampedmotion:<br></p></li><li><p>This simplifies to the fundamental differential equation for damped motion:<br>\ddot{x} + 2\gamma \dot{x} + \omega_0^2 x = 0</p></li><li><p><strong>Remark5(DampingFactor):</strong></p><ul><li><p>Theparameter</p></li><li><p><strong>Remark 5 (Damping Factor):</strong></p><ul><li><p>The parameter\gamma = \frac{\Gamma}{2m}iscalledthedampingfactor,andithasunitsoffrequency(is called the damping factor, and it has units of frequency (\text{s}^{-1}).</p></li></ul></li><li><p><strong>Theorem2(ClassificationofDampedMotion):</strong></p><ul><li><p><strong>Overdamping().</p></li></ul></li><li><p><strong>Theorem 2 (Classification of Damped Motion):</strong></p><ul><li><p><strong>Overdamping (\gamma > \omega_0):</strong>Strongdampingcausesthesystemtoreturnslowlytorestwithoutoscillating.</p></li><li><p><strong>CriticalDamping():</strong> Strong damping causes the system to return slowly to rest without oscillating.</p></li><li><p><strong>Critical Damping (\gamma = \omega_0):</strong>Thesystemreturnstorestasfastaspossiblewithoutoscillating.</p></li><li><p><strong>WeakDamping/Underdamping():</strong> The system returns to rest as fast as possible without oscillating.</p></li><li><p><strong>Weak Damping / Underdamping (\gamma < \omega_0):</strong>Thesystemcontinuestooscillatebackandforth,butitsamplitudedecaysexponentiallyovertimeaccordingto):</strong> The system continues to oscillate back and forth, but its amplitude decays exponentially over time according toe^{-\gamma t}$$.