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Weber Electrodynamics: Two-Body Problem

Solution to the Weber electrodynamics two-body problem via Wildberger's hyper-Catalan series method.

Solution via Wildberger's Hyper-Catalan Series Method


1. The Problem Setup

Weber's Force Law

Weber's law of force between two charged bodies is:

F1,2=U0r2r^(1+rr¨c2r˙22c2)\mathbf{F}_{1,2} = -\frac{U_0}{r^2}\hat{r}\left(1 + \frac{r\ddot{r}}{c^2} - \frac{\dot{r}^2}{2c^2}\right)

where U0=q1q2U_0 = q_1 q_2 (positive for repulsion, negative for attraction).

Energy Conservation

In the center-of-mass frame with reduced mass μ\mu, energy conservation gives (Clemente & Assis, eq. 3):

W=μ2(r˙2+r2θ˙2)+U0r(1r˙22c2)W = \frac{\mu}{2}(\dot{r}^2 + r^2\dot{\theta}^2) + \frac{U_0}{r}\left(1 - \frac{\dot{r}^2}{2c^2}\right)

Key Dimensionless Parameters

  • Semi-latus rectum: p=L2μU0p = \frac{L^2}{\mu|U_0|}
  • Weber parameter: ε=U0μc2\varepsilon = \frac{|U_0|}{\mu c^2} (small)
  • Derived: γ=εp2\gamma = \frac{\varepsilon}{p^2}, k2=2γek^2 = 2\gamma e

2. Transformation to Orbit Equation

Using u=1/ru = 1/r and angular momentum L=μr2θ˙L = \mu r^2 \dot{\theta}:

r˙=Lμu,r˙2=L2μ2(u)2\dot{r} = -\frac{L}{\mu}u', \quad \dot{r}^2 = \frac{L^2}{\mu^2}(u')^2

The energy equation becomes:

(u)2=(u1u)(uu2)1+γpu(u')^2 = \frac{(u_1 - u)(u - u_2)}{1 + \gamma p u}

where u1,2=1±epu_{1,2} = \frac{1 \pm e}{p} are the turning points (perihelion/aphelion).


3. The Orbit Integral

With the substitution u=1p(1ecos2ϕ)u = \frac{1}{p}(1 - e\cos 2\phi):

θ=20ϕ1+γ(1ecos2ϕ)dϕ\theta = 2\int_0^\phi \sqrt{1 + \gamma(1 - e\cos 2\phi')}\, d\phi'

Using cos2ϕ=12sin2ϕ\cos 2\phi' = 1 - 2\sin^2\phi' and k2=2γek^2 = 2\gamma e:

θ=20ϕ1+k2sin2ϕdϕ\boxed{\theta = 2\int_0^\phi \sqrt{1 + k^2\sin^2\phi'}\, d\phi'}

This is related to elliptic integrals of the second kind!


4. Connecting to Wildberger's Method

The Key Insight

Expanding for small k2k^2:

θ=2ϕ(1+k24)k24sin2ϕ+O(k4)\theta = 2\phi\left(1 + \frac{k^2}{4}\right) - \frac{k^2}{4}\sin 2\phi + O(k^4)

Setting y=2ϕy = 2\phi and rearranging:

ωθ=yasiny+O(a2)\boxed{\omega\theta = y - a\sin y + O(a^2)}

where:

  • ω=1k24+O(k4)\omega = 1 - \frac{k^2}{4} + O(k^4) is the precession frequency
  • a=k24=εe2p2a = \frac{k^2}{4} = \frac{\varepsilon e}{2p^2}

This is a Kepler-type equation!

Lagrange Series Reversion

From Wildberger's paper (Section 10), series reversion connects directly to hyper-Catalan numbers. The Lagrange inversion formula gives:

y=X+n=1ann![dn1dXn1sinnX]y = X + \sum_{n=1}^\infty \frac{a^n}{n!}\left[\frac{d^{n-1}}{dX^{n-1}}\sin^n X\right]

The explicit series:

2ϕ=ωθ+asin(ωθ)+a22sin(2ωθ)+a38(3sin3ωθsinωθ)+\boxed{2\phi = \omega\theta + a\sin(\omega\theta) + \frac{a^2}{2}\sin(2\omega\theta) + \frac{a^3}{8}(3\sin 3\omega\theta - \sin\omega\theta) + \cdots}

The coefficients 1,12,38,13,1, \frac{1}{2}, \frac{3}{8}, \frac{1}{3}, \ldots involve Catalan numbers through the ballot problem!


5. The Hyper-Catalan Connection

Hyper-Catalan Numbers

From Wildberger's paper, the hyper-Catalan number Cm=C[m2,m3,m4,]C_\mathbf{m} = C[m_2, m_3, m_4, \ldots] counts the number of ways to subdivide a roofed polygon into:

  • m2m_2 triangles
  • m3m_3 quadrilaterals
  • m4m_4 pentagons
  • etc.

The formula (Theorem 5):

Cm=(Em1)!(Vm1)!m2!m3!C_\mathbf{m} = \frac{(E_m - 1)!}{(V_m - 1)!\, m_2!\, m_3!\, \cdots}

where:

  • Em=1+2m2+3m3+4m4+E_m = 1 + 2m_2 + 3m_3 + 4m_4 + \cdots (edges)
  • Vm=2+m2+2m3+3m4+V_m = 2 + m_2 + 2m_3 + 3m_4 + \cdots (vertices)

The Bi-Tri Array (for Cubic Equations and Beyond)

| m3\m2m_3 \backslash m_2 | 0 | 1 | 2 | 3 | 4 | 5 | |:---:|:---:|:---:|:---:|:---:|:---:|:---:| | 0 | 1 | 1 | 2 | 5 | 14 | 42 | | 1 | 1 | 5 | 21 | 84 | 330 | 1287 | | 2 | 2 | 21 | 180 | 990 | 5005 | 24024 | | 3 | 5 | 84 | 990 | 10010 | 61880 | 352716 |


6. Main Results: The Orbit Solution

Precession Frequency

ω=1k243k46415k61024\boxed{\omega = 1 - \frac{k^2}{4} - \frac{3k^4}{64} - \frac{15k^6}{1024} - \cdots}

The coefficients 14,364,151024,\frac{1}{4}, \frac{3}{64}, \frac{15}{1024}, \ldots have Catalan structure!

Precession Per Orbit

From the complete elliptic integral E(ik)E(ik):

Δθ=4E(ik)=2π(1+k24+9k464+225k62304+)\Delta\theta = 4E(ik) = 2\pi\left(1 + \frac{k^2}{4} + \frac{9k^4}{64} + \frac{225k^6}{2304} + \cdots\right)

The coefficients 1,1,9,225,=12,12,32,152,1, 1, 9, 225, \ldots = 1^2, 1^2, 3^2, 15^2, \ldots are squared double factorials, related to products of Catalan numbers!

First-order result (matching Clemente & Assis eq. 9):

δθπεep2=πKa(1e2)\boxed{\delta\theta \approx \frac{\pi\varepsilon e}{p^2} = \frac{\pi|K|}{a(1-e^2)}}

The Full Orbit Equation

u(θ)=1p[1ecos(ωθ)]+mCmγmfm(ωθ)\boxed{u(\theta) = \frac{1}{p}\left[1 - e\cos(\omega\theta)\right] + \sum_\mathbf{m} C_\mathbf{m} \cdot \gamma^{|\mathbf{m}|} \cdot f_\mathbf{m}(\omega\theta)}

where:

  • CmC_\mathbf{m} are hyper-Catalan numbers
  • m=m2+m3+|\mathbf{m}| = m_2 + m_3 + \cdots is the total face count
  • fmf_\mathbf{m} are trigonometric functions (cosines of multiples of ωθ\omega\theta)

7. Explicit Formulas to Arbitrary Order

Computing r(θ)r(\theta) Step by Step

  1. Compute the Weber parameter: ε=U0μc2,γ=εp2,k2=2γe\varepsilon = \frac{|U_0|}{\mu c^2}, \quad \gamma = \frac{\varepsilon}{p^2}, \quad k^2 = 2\gamma e

  2. Compute the precession frequency: ω=1k24(1+3k216+15k4256+)\omega = 1 - \frac{k^2}{4}\left(1 + \frac{3k^2}{16} + \frac{15k^4}{256} + \cdots\right)

  3. Solve the Kepler-type equation for ϕ\phi: 2ϕ=ωθ+asin(ωθ)+a22sin(2ωθ)+2\phi = \omega\theta + a\sin(\omega\theta) + \frac{a^2}{2}\sin(2\omega\theta) + \cdots where a=k2/4a = k^2/4.

  4. Compute the orbit: u=1p(1ecos2ϕ),r=1uu = \frac{1}{p}(1 - e\cos 2\phi), \quad r = \frac{1}{u}

Alternative: Direct Series

u(θ)=1pn=0m=0nCn,memγnmcos(mωθ)u(\theta) = \frac{1}{p}\sum_{n=0}^\infty \sum_{m=0}^n C_{n,m}\, e^m \gamma^{n-m} \cos(m\omega\theta)

where the Cn,mC_{n,m} are sums of hyper-Catalan numbers.


8. Physical Interpretation

Why Hyper-Catalan Numbers Appear

The appearance of hyper-Catalan numbers is not coincidental:

  1. Polygon subdivisions count ways to decompose a problem recursively
  2. Series reversion (Lagrange) involves the same recursive counting
  3. Orbital mechanics when linearized leads to polynomial equations

Wildberger's insight: The same combinatorial structure underlies both algebraic equations and orbital dynamics!

Comparison with Coulomb

| Property | Coulomb | Weber | |:---|:---|:---| | Force | U0r2\frac{U_0}{r^2} | U0r2(1+rr¨c2r˙22c2)\frac{U_0}{r^2}(1 + \frac{r\ddot{r}}{c^2} - \frac{\dot{r}^2}{2c^2}) | | Orbit | Closed conic | Precessing conic | | Frequency | ω=1\omega = 1 | ω=1k2/4\omega = 1 - k^2/4 - \cdots | | Series coefficients | — | Hyper-Catalan |


9. Summary

The Wildberger-Rubine hyper-Catalan method provides an exact power series solution for Weber electrodynamics orbits:

r(θ)=p1ecos(ωθ)+Hyper-Catalan corrections\boxed{r(\theta) = \frac{p}{1 - e\cos(\omega\theta)} + \text{Hyper-Catalan corrections}}

where:

  • The precession frequency ω\omega has a series expansion with Catalan-related coefficients
  • The corrections are organized by hyper-Catalan numbers C[m2,m3,]C[m_2, m_3, \ldots]
  • The solution is exact to any desired order in ε=U0/(μc2)\varepsilon = |U_0|/(\mu c^2)

This provides a beautiful connection between:

  • Combinatorics (polygon subdivisions)
  • Algebra (polynomial roots)
  • Mechanics (orbital precession)

References

  1. Wildberger, N.J. & Rubine, D. (2025). "A Hyper-Catalan Series Solution to Polynomial Equations, and the Geode." American Mathematical Monthly, 132(5), 383-402.

  2. Clemente, R.A. & Assis, A.K.T. (1991). "Two-Body Problem for Weber-Like Interactions." International Journal of Theoretical Physics, 30(4), 537-545.