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Definition: a=ω2xa = -\omega^2 x

Restoring acceleration proportional to displacement.

a=ω2xa = -\omega^2 x

Differential Equation: d2x/dt2 = -ω2x:

d2xdt2=ω2x\frac{d^2x}{dt^2} = -\omega^2 x

Simple harmonic oscillator equation.

x(t)=Acos(ωt+ϕ)x(t) = A \cos(\omega t + \phi)

Position as function of time.

Where:

  • A = amplitude (maximum displacement)
  • ω\omega = angular frequency
  • ϕ\phi = phase constant

v(t)=ωAsin(ωt+ϕ)v(t) = -\omega A \sin(\omega t + \phi)

Velocity as function of time.

v(t)=dxdt=ωAsin(ωt+ϕ)v(t) = \frac{dx}{dt} = -\omega A\sin(\omega t + \phi)

a(t)=ω2Acos(ωt+ϕ)a(t) = -\omega^2 A \cos(\omega t + \phi)

Acceleration as function of time.

a(t)=dvdt=ω2Acos(ωt+ϕ)=ω2x(t)a(t) = \frac{dv}{dt} = -\omega^2 A\cos(\omega t + \phi) = -\omega^2 x(t)

Analyzing Mass-spring Systems

Spring provides restoring force: F=kxF = -kx (Hooke's Law)

Equation of motion: md2xdt2=kxm\frac{d^2x}{dt^2} = -kx

d2xdt2=kmx\frac{d^2x}{dt^2} = -\frac{k}{m}x

Compare to SHM equation: ω2=km\omega^2 = \frac{k}{m}

Spring Force (Hooke's Law): F=kxF = -kx

F=kxF = -kx

Where k = spring constant (N/m).

Period: T = 2π√(m/k):

T=2πmkT = 2\pi\sqrt{\frac{m}{k}}

Frequency: f=1T=12πkmf = \frac{1}{T} = \frac{1}{2\pi}\sqrt{\frac{k}{m}}

Angular frequency: ω=2πf=km\omega = 2\pi f = \sqrt{\frac{k}{m}}

Period: T=2πLgT = 2\pi\sqrt{\frac{L}{g}} (For Small Angles)

T=2πLgT = 2\pi\sqrt{\frac{L}{g}}

Valid for small angles (θ < 15 degrees ), where sinθθ\sin\theta \approx \theta.

Properties:

  • Independent of mass!
  • Independent of amplitude (small angles)
  • Period increases with length

Total Mechanical Energy E=12kA2E = \frac{1}{2}kA^2 (Constant)

Etotal=K+U=constant=12kA2E_{total} = K + U = \text{constant} = \frac{1}{2}kA^2

At any position: 12mv2+12kx2=12kA2\frac{1}{2}mv^2 + \frac{1}{2}kx^2 = \frac{1}{2}kA^2

Energy exchange:

  • x = 0: K maximum, U = 0
  • x = ±A: K = 0, U maximum
  • Continuous exchange between K and U

Restoring Torque

For small angles, gravity provides restoring torque.

τ=mgLsinθmgLθ\tau = -mgL\sin\theta \approx -mgL\theta

Equation of motion: mL2d2θdt2=mgLθmL^2\frac{d^2\theta}{dt^2} = -mgL\theta

d2θdt2=gLθ\frac{d^2\theta}{dt^2} = -\frac{g}{L}\theta

Compare to SHM: ω2=gL\omega^2 = \frac{g}{L}

Period: T=2πmkT = 2\pi\sqrt{\frac{m}{k}}

T=2πmkT = 2\pi\sqrt{\frac{m}{k}}

Frequency: f=1T=12πkmf = \frac{1}{T} = \frac{1}{2\pi}\sqrt{\frac{k}{m}}

Angular frequency: ω=2πf=km\omega = 2\pi f = \sqrt{\frac{k}{m}}

Underdamped System

Damping small enough for oscillations.

Differential equation: md2xdt2+bdxdt+kx=0m\frac{d^2x}{dt^2} + b\frac{dx}{dt} + kx = 0

Solution: Oscillation with exponentially decaying amplitude.

Critically Damped System

Minimum damping without oscillation.

Condition: b2=4mkb^2 = 4mk

Returns to equilibrium fastest without overshooting.

Overdamped System

Large damping, no oscillations.

Condition: b2>4mkb^2 > 4mk

Returns to equilibrium slowly, no overshoot.

F=Gm1m2r2F = G \frac{m_1 m_2}{r^2}

F = G m1 m2 / r2:

Newton's law of universal gravitation.

F=Gm1m2r2F = G\frac{m_1 m_2}{r^2}

Where:

  • G = 6.674 × 10-11 N - m2/kg2
  • r = separation distance

Gravitational Potential Energy

U=Gm1m2rU = -\frac{Gm_1 m_2}{r}

Reference: U = 0 at r -> ∞

Escape velocity: vesc=2GMRv_{esc} = \sqrt{\frac{2GM}{R}}

Kepler's Laws

First Law: Planetary (and satellite) orbits are ellips with central mass at one focus.

Second Law (Equal Area): Radius vector sweeps equal areas in equal times (consequence of angular momentum conservation).

Third Law: T2a3T^2 \propto a^3 (period squared ∝ semi-major axis cubed)

T2a3=4π2GM=constant\frac{T^2}{a^3} = \frac{4\pi^2}{GM} = \text{constant}

Circular Orbits

Special case of elliptical orbit with e = 0.

Circular orbit condition: Fg=FcF_g = F_c

GMmr2=mv2r\frac{GMm}{r^2} = \frac{mv^2}{r}

Orbital speed: v=GMrv = \sqrt{\frac{GM}{r}}

Orbital period: T=2πrv=2πr3GMT = \frac{2\pi r}{v} = 2\pi\sqrt{\frac{r^3}{GM}}

Total mechanical energy: E=K+U=GMm2rE = K + U = -\frac{GMm}{2r} (negative for bound orbits)