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Closed-Form Solutions in Weber Electrodynamics

Derivation and survey of closed-form analytical solutions to the Weber electrodynamic equations.

Introduction

Weber electrodynamics features a velocity-dependent potential that couples position and velocity, making most solutions involve elliptic integrals. However, several special cases admit elementary closed-form solutions. This document catalogs these cases systematically.

We work in absolute (Gaussian) units unless otherwise specified.


Preliminaries

Reduced Mass Formulation

For a two-body system, we work in the center-of-mass frame with reduced mass:

μ=m1m2m1+m2\mu = \frac{m_1 m_2}{m_1 + m_2}

Weber Potential Energy

For attractive charges (q1q2=κq_1 q_2 = -\kappa where κ>0\kappa > 0):

U=κr(1r˙22c2)U = -\frac{\kappa}{r}\left(1 - \frac{\dot{r}^2}{2c^2}\right)

For repulsive charges (q1q2=+kq_1 q_2 = +k where k>0k > 0):

U=+kr(1r˙22c2)U = +\frac{k}{r}\left(1 - \frac{\dot{r}^2}{2c^2}\right)

Key Parameter

Throughout, we define the Weber length scale:

a=q1q2c2a = \frac{|q_1 q_2|}{c^2}

This has dimensions of (mass × length) and characterizes the relativistic correction strength.


Solution 1: Zero-Energy Radial Infall (Attractive)

Setup

  • Attractive charges: q1q2=κq_1 q_2 = -\kappa
  • Zero angular momentum: L=0L = 0
  • Zero total energy: E=0E = 0
  • Initial conditions: r(0)=r0r(0) = r_0, r˙(0)<0\dot{r}(0) < 0 (infalling)

Energy Conservation

E=12μr˙2κr+κr˙22c2r=0E = \frac{1}{2}\mu\dot{r}^2 - \frac{\kappa}{r} + \frac{\kappa\dot{r}^2}{2c^2 r} = 0

Solving for r˙2\dot{r}^2:

r˙2=2κμr+a\dot{r}^2 = \frac{2\kappa}{\mu r + a}

where a=κ/c2a = \kappa/c^2.

Closed-Form Solution

r(t)=1μ[((μr0+a)3/23μ2κ2t)2/3a]\boxed{r(t) = \frac{1}{\mu}\left[\left((\mu r_0 + a)^{3/2} - \frac{3\mu\sqrt{2\kappa}}{2}\,t\right)^{2/3} - a\right]}

Or equivalently:

r(t)=1μ[(ABt)2/3a]r(t) = \frac{1}{\mu}\left[(A - Bt)^{2/3} - a\right]

where:

  • A=(μr0+a)3/2A = (\mu r_0 + a)^{3/2}
  • B=3μ2κ2B = \frac{3\mu\sqrt{2\kappa}}{2}

Velocity

r˙(t)=2κμr(t)+a\dot{r}(t) = -\sqrt{\frac{2\kappa}{\mu r(t) + a}}

Collision Time

The particles collide (r=0r = 0) at:

tcoll=(μr0+a)3/2a3/23μκ/2t_{\text{coll}} = \frac{(\mu r_0 + a)^{3/2} - a^{3/2}}{3\mu\sqrt{\kappa/2}}

Coulomb Limit

As cc \to \infty (so a0a \to 0):

r(t)(r03/2322κμt)2/3r(t) \to \left(r_0^{3/2} - \frac{3}{2}\sqrt{\frac{2\kappa}{\mu}}\,t\right)^{2/3}

This is the standard Coulomb E=0E = 0 radial solution.


Solution 2: Radial Infall from Rest (Attractive)

Setup

  • Attractive charges: q1q2=κq_1 q_2 = -\kappa
  • Zero angular momentum: L=0L = 0
  • Particles released from rest at separation r0r_0
  • Initial conditions: r(0)=r0r(0) = r_0, r˙(0)=0\dot{r}(0) = 0

Energy

E=κr0E = -\frac{\kappa}{r_0}

Velocity Equation

r˙2=2κ(1r/r0)μr+a\dot{r}^2 = \frac{2\kappa(1 - r/r_0)}{\mu r + a}

Time as Function of Position

Define:

  • v=1r/r0v = 1 - r/r_0 (dimensionless progress variable, v[0,1]v \in [0, 1])
  • β=μr0μr0+a\beta = \frac{\mu r_0}{\mu r_0 + a} (dimensionless parameter, β(0,1)\beta \in (0, 1))

Then the time to fall from r0r_0 to rr is:

t(r)=μr0+a2κμr0[arcsin(βv)+βv(1βv)]\boxed{t(r) = \frac{\mu r_0 + a}{\sqrt{2\kappa\mu r_0}}\left[\arcsin(\sqrt{\beta v}) + \sqrt{\beta v(1 - \beta v)}\right]}

where v=1r/r0v = 1 - r/r_0.

Collision Time

At r=0r = 0 (so v=1v = 1):

tcoll=μr0+a2κμr0[arcsin(β)+β(1β)]t_{\text{coll}} = \frac{\mu r_0 + a}{\sqrt{2\kappa\mu r_0}}\left[\arcsin(\sqrt{\beta}) + \sqrt{\beta(1 - \beta)}\right]

Coulomb Limit

As cc \to \infty, a0a \to 0, β1\beta \to 1:

tcollr0μr02κπ2=π2μr032κt_{\text{coll}} \to r_0\sqrt{\frac{\mu r_0}{2\kappa}} \cdot \frac{\pi}{2} = \frac{\pi}{2}\sqrt{\frac{\mu r_0^3}{2\kappa}}

This matches the classical Coulomb result (quarter period of a degenerate ellipse).


Solution 3: Circular Orbits

Key Insight

For circular motion, r=constr = \text{const}, so r˙=0\dot{r} = 0 and r¨=0\ddot{r} = 0. The Weber force reduces exactly to the Coulomb force!

Force Balance

For attractive charges in circular orbit:

μrω2=κr2\mu r\omega^2 = \frac{\kappa}{r^2}

Angular Velocity (Kepler's Third Law)

ω2=κμr3\boxed{\omega^2 = \frac{\kappa}{\mu r^3}}

This is identical to the Coulomb/Kepler result!

Orbital Period

T=2πμr3κT = 2\pi\sqrt{\frac{\mu r^3}{\kappa}}

Physical Interpretation

Since the radial velocity vanishes for circular orbits, the velocity-dependent Weber correction disappears entirely. Circular orbits in Weber electrodynamics are exact copies of Keplerian circular orbits.


Solution 4: Repulsive Scattering from Rest

Setup

  • Repulsive charges: q1q2=+kq_1 q_2 = +k
  • Zero angular momentum: L=0L = 0
  • Particles released from rest at separation r0r_0
  • Initial conditions: r(0)=r0r(0) = r_0, r˙(0)=0\dot{r}(0) = 0

Energy

E=+kr0E = +\frac{k}{r_0}

Velocity Equation

r˙2=2k(r/r01)μra\dot{r}^2 = \frac{2k(r/r_0 - 1)}{\mu r - a}

where a=k/c2a = k/c^2.

Note: This requires r>a/μr > a/\mu for physical solutions. Typically aμr0a \ll \mu r_0, so this is satisfied.

Asymptotic Velocity

As rr \to \infty:

r˙=2kμr0\dot{r}_\infty = \sqrt{\frac{2k}{\mu r_0}}

This is the same as the Coulomb result—the Weber correction affects the trajectory but not the asymptotic speed (conservation of energy).

Time as Function of Position

Define u=r/r0u = r/r_0 (so u1u \geq 1), and γ=aμr0\gamma = \frac{a}{\mu r_0} (typically γ1\gamma \ll 1).

t(r)=r0μr02k1r/r0uγu1dut(r) = r_0\sqrt{\frac{\mu r_0}{2k}} \int_1^{r/r_0} \sqrt{\frac{u - \gamma}{u - 1}}\, du

For γ=0\gamma = 0 (Coulomb limit):

t=r0μr02k[u(u1)+arcosh(u)]1r/r0t = r_0\sqrt{\frac{\mu r_0}{2k}}\left[\sqrt{u(u-1)} + \text{arcosh}(\sqrt{u})\right]_1^{r/r_0}

For small γ\gamma, the Weber correction adds a perturbative term.


Solution 5: Equilibrium and Critical Points

Radial Equilibrium

For the effective radial potential with angular momentum LL:

Ueff(r,r˙)=L22μr2κr(1r˙22c2)U_{\text{eff}}(r, \dot{r}) = \frac{L^2}{2\mu r^2} - \frac{\kappa}{r}\left(1 - \frac{\dot{r}^2}{2c^2}\right)

At circular orbit equilibrium (r˙=0\dot{r} = 0):

dUeffdrr˙=0=L2μr3+κr2=0\frac{dU_{\text{eff}}}{dr}\bigg|_{\dot{r}=0} = -\frac{L^2}{\mu r^3} + \frac{\kappa}{r^2} = 0

rcirc=L2μκ\boxed{r_{\text{circ}} = \frac{L^2}{\mu\kappa}}

This is identical to the Coulomb result.

Orbital Energy at Circular Orbit

Ecirc=L22μrcirc2κrcirc=μκ22L2E_{\text{circ}} = \frac{L^2}{2\mu r_{\text{circ}}^2} - \frac{\kappa}{r_{\text{circ}}} = -\frac{\mu\kappa^2}{2L^2}

Again, identical to Coulomb.


Solution 6: Small Oscillations About Circular Orbit

Effective Spring Constant

For small radial perturbations ξ=rrcirc\xi = r - r_{\text{circ}} about a circular orbit:

ξ¨+ωr2ξ=0\ddot{\xi} + \omega_r^2 \xi = 0

The radial oscillation frequency is:

ωr=ωϕ=κμrcirc3\omega_r = \omega_\phi = \sqrt{\frac{\kappa}{\mu r_{\text{circ}}^3}}

Since ωr=ωϕ\omega_r = \omega_\phi, orbits close after one revolution—the ellipse does not precess (to first order).

Precession in Weber (Higher Order)

For general (non-circular) orbits, Weber electrodynamics does predict orbital precession due to the velocity-dependent terms. However, this requires solving the full equations numerically or via perturbation theory.


Solution 7: Head-On Collision Velocity

Maximum Approach Velocity (Attractive)

For particles falling from infinity with E=0E = 0:

r˙2=2κμr+a\dot{r}^2 = \frac{2\kappa}{\mu r + a}

As r0r \to 0:

r˙max=2κa=2κc2κ=c2\dot{r}_{\max} = \sqrt{\frac{2\kappa}{a}} = \sqrt{\frac{2\kappa c^2}{\kappa}} = c\sqrt{2}

This exceeds the speed of light! This indicates that Weber electrodynamics, as a non-relativistic theory, breaks down at small separations where velocities become relativistic.

Critical Separation

The velocity reaches cc at:

rc=κμc2=aμr_c = \frac{\kappa}{\mu c^2} = \frac{a}{\mu}

For r<rcr < r_c, the theory predicts superluminal velocities, signaling its breakdown.


Solution 8: Turning Points (Repulsive Scattering with Angular Momentum)

Setup

  • Repulsive charges: q1q2=+kq_1 q_2 = +k
  • Angular momentum: L0L \neq 0
  • Energy: E>0E > 0

Effective Potential

Ueff=L22μr2+kr(1r˙22c2)U_{\text{eff}} = \frac{L^2}{2\mu r^2} + \frac{k}{r}\left(1 - \frac{\dot{r}^2}{2c^2}\right)

Turning Point Condition

At the distance of closest approach rminr_{\min}, r˙=0\dot{r} = 0:

E=L22μrmin2+krminE = \frac{L^2}{2\mu r_{\min}^2} + \frac{k}{r_{\min}}

This is identical to the Coulomb turning point equation! Solving:

rmin=k+k2+2EL2/μ2E\boxed{r_{\min} = \frac{k + \sqrt{k^2 + 2EL^2/\mu}}{2E}}

The turning point in Weber electrodynamics (at r˙=0\dot{r} = 0) coincides exactly with the Coulomb prediction.


Summary Table

| Case | Conditions | Solution Type | |------|------------|---------------| | Zero-energy radial infall | E=0E=0, L=0L=0, attractive | r(t)=1μ[(ABt)2/3a]r(t) = \frac{1}{\mu}[(A-Bt)^{2/3} - a] | | Infall from rest | r˙0=0\dot{r}_0=0, L=0L=0, attractive | t(r)t(r) via arcsin (elementary) | | Circular orbits | r˙=0\dot{r}=0, attractive | Same as Kepler | | Repulsive scattering | r˙0=0\dot{r}_0=0, L=0L=0, repulsive | r˙=2k/(μr0)\dot{r}_\infty = \sqrt{2k/(\mu r_0)} | | Turning points | r˙=0\dot{r}=0, repulsive | Same as Coulomb |


Dimensionless Formulation

Characteristic Scales

For a system with κ=q1q2\kappa = |q_1 q_2|, we can define:

  • Length: r0r_0 (initial separation)
  • Time: τ0=μr03/κ\tau_0 = \sqrt{\mu r_0^3 / \kappa}
  • Velocity: v0=κ/(μr0)v_0 = \sqrt{\kappa / (\mu r_0)}

Dimensionless Variables

ρ=r/r0,τ=t/τ0,ϵ=v0/c=κμr0c2\rho = r/r_0, \quad \tau = t/\tau_0, \quad \epsilon = v_0/c = \sqrt{\frac{\kappa}{\mu r_0 c^2}}

Dimensionless Energy Equation (Radial)

E~=12ρ˙21ρ+ϵ2ρ˙22ρ\tilde{E} = \frac{1}{2}\dot{\rho}^2 - \frac{1}{\rho} + \frac{\epsilon^2 \dot{\rho}^2}{2\rho}

where E~=Eμr0/κ\tilde{E} = E\mu r_0 / \kappa and ρ˙=dρ/dτ\dot{\rho} = d\rho/d\tau.

The parameter ϵ\epsilon controls the strength of Weber corrections. For ϵ1\epsilon \ll 1, Coulomb behavior dominates.


Physical Validity Regime

Weber electrodynamics is valid when:

  1. vcv \ll c (non-relativistic velocities)
  2. ra/μ=q1q2/(μc2)r \gg a/\mu = |q_1 q_2|/(\mu c^2) (above the critical separation)
  3. Radiation effects are negligible

For electrons: a/μ2.8×1015a/\mu \approx 2.8 \times 10^{-15} m (classical electron radius).

For macroscopic charged objects, Weber corrections are typically negligible.


Appendix: Derivation of Arcsin Solution

Starting from:

r˙2=2κ(1r/r0)μr+a\dot{r}^2 = \frac{2\kappa(1 - r/r_0)}{\mu r + a}

For infall (r˙<0\dot{r} < 0):

dt=μr+a2κ(1r/r0)drdt = -\sqrt{\frac{\mu r + a}{2\kappa(1 - r/r_0)}}\,dr

Substituting v=1r/r0v = 1 - r/r_0, r=r0(1v)r = r_0(1-v), dr=r0dvdr = -r_0\,dv:

dt=r0μr0(1v)+a2κvdv=r0μr0+a2κ1βvvdvdt = r_0\sqrt{\frac{\mu r_0(1-v) + a}{2\kappa v}}\,dv = r_0\sqrt{\frac{\mu r_0 + a}{2\kappa}}\sqrt{\frac{1 - \beta v}{v}}\,dv

where β=μr0/(μr0+a)\beta = \mu r_0/(\mu r_0 + a).

Using the integral:

0v1βuudu=1β[arcsin(βv)+βv(1βv)]\int_0^v \sqrt{\frac{1 - \beta u}{u}}\,du = \frac{1}{\sqrt{\beta}}\left[\arcsin(\sqrt{\beta v}) + \sqrt{\beta v(1-\beta v)}\right]

We obtain the closed-form result.


References

  1. Weber, W. (1846). Elektrodynamische Maassbestimmungen
  2. Assis, A.K.T. (1994). Weber's Electrodynamics
  3. Wesley, J.P. (1990). "Weber electrodynamics"