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Hamilton-Jacobi Separation in Kerr

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Kerr geodesics are exceptional because their Hamilton–Jacobi equation separates into one radial and one polar ordinary differential equation. The separation is not a lucky algebraic trick: it reflects the metric’s principal hidden symmetry and supplies the fourth first integral needed for complete geodesic integrability. Here m=GMphysm=G M_{\mathrm{phys}} and a=Jphys/Mphysa=J_{\mathrm{phys}}/M_{\mathrm{phys}} (with c=1c=1) are length parameters, and the treatment concerns test-particle and null-ray kinematics, not self-force or orbital stability.

Required background. Killing Fields and Isometry Groups supplies the manifest energy and axial-angular-momentum integrals; Affine and Variational Geodesics supplies the Hamilton–Jacobi formulation of geodesic motion.

Helpful background. Einstein’s Equation fixes the background field equation; The Riemann Curvature Tensor supplies curvature conventions; Exact Solutions of Einstein’s Equations locates Kerr in the family atlas; Frames, Coframes, and Anholonomy prepares the principal-frame interpretation.

In Boyer–Lindquist coordinates define

Σ=r2+a2cos⁡2θ,Δ=r2−2mr+a2.\Sigma=r^2+a^2\cos^2\theta, \qquad \Delta=r^2-2mr+a^2.

The decisive property is that multiplying the inverse metric by Σ\Sigma makes its rr and θ\theta dependence additive. Equivalently, for any covector pap_a,

Σgabpapb=Δpr2+pθ2−[(r2+a2)pt+apϕ]2Δ+[pϕ+asin⁡2θ pt]2sin⁡2θ.\begin{aligned} \Sigma g^{ab}p_ap_b={}& \Delta p_r^2+p_\theta^2 -\frac{\big[(r^2+a^2)p_t+a p_\phi\big]^2}{\Delta}\\ &+\frac{\big[p_\phi+a\sin^2\theta\,p_t\big]^2}{\sin^2\theta}. \end{aligned}

This identity is the coordinate-level answer to why additive separation works. Stationarity and axisymmetry make pt=−Ep_t=-E and pϕ=Lzp_\phi=L_z constant, but those two Killing symmetries alone do not explain the split between rr and θ\theta.

For a particle of rest mass μ\mu, take

S=+12μ2λ−Et+Lzϕ+Sr(r)+Sθ(θ).S=+\frac12\mu^2\lambda-Et+L_z\phi+S_r(r)+S_\theta(\theta).

The plus sign is fixed by the parameter-dependent Hamilton–Jacobi equation ∂λS+H=0\partial_\lambda S+H=0: on the mass shell, H=12gabpapb=−μ2/2H=\tfrac12g^{ab}p_ap_b=-\mu^2/2, so ∂λS=+μ2/2\partial_\lambda S=+\mu^2/2. If one uses only the mass-shell equation below, the additive λ\lambda term drops out, but writing it with the wrong sign would make the two Hamilton–Jacobi formulations inconsistent.

Substitution into gab∂aS∂bS=−μ2g^{ab}\partial_aS\partial_bS=-\mu^2 leaves one function of rr equal to minus one function of θ\theta. Both must therefore equal a constant. This derivation and its geometric generalization are developed in Frolov, Krtouš, and Kubizňák 2017, §§6.1–6.2, printed pp. 117–125, Open PDF.

Choose the separated constant QQ so that the first-order equations read

Σ2(drdλ)2=R(r),Σ2(dθdλ)2=Θ(θ),\Sigma^2\left(\frac{dr}{d\lambda}\right)^2=R(r), \qquad \Sigma^2\left(\frac{d\theta}{d\lambda}\right)^2=\Theta(\theta),

with

R=[E(r2+a2)−aLz]2−Δ[μ2r2+(Lz−aE)2+Q],R=\big[E(r^2+a^2)-aL_z\big]^2 -\Delta\big[\mu^2r^2+(L_z-aE)^2+Q\big], Θ=Q−cos⁡2θ[a2(μ2−E2)+Lz2sin⁡2θ].\Theta=Q-\cos^2\theta \left[a^2(\mu^2-E^2)+\frac{L_z^2}{\sin^2\theta}\right].

Only regions with R≥0R\geq0 and Θ≥0\Theta\geq0 are accessible. Zeros of either potential are turning points unless the zero is multiple; a double radial root instead identifies a constant-radius orbit. For null rays set μ=0\mu=0. The affine parameter λ\lambda above is the physical affine parameter; introducing Mino time by dλM=dλ/Σd\lambda_{\rm M}=d\lambda/\Sigma removes the common Σ\Sigma and decouples the radial and polar motions.

The cyclic coordinates follow from the same separated action. With P(r)=E(r2+a2)−aLzP(r)=E(r^2+a^2)-aL_z,

Σdtdλ=a(Lz−aEsin⁡2θ)+(r2+a2)PΔ,\Sigma\frac{dt}{d\lambda} =a(L_z-aE\sin^2\theta) +\frac{(r^2+a^2)P}{\Delta}, Σdϕdλ=(Lzsin⁡2θ−aE)+aPΔ.\Sigma\frac{d\phi}{d\lambda} =\left(\frac{L_z}{\sin^2\theta}-aE\right) +\frac{aP}{\Delta}.

Their 1/Δ1/\Delta behavior at a horizon is a Boyer–Lindquist coordinate effect; a horizon-penetrating chart combines the divergent pieces into regular ingoing quantities.

There are two widespread constant conventions. On this page QQ is the quantity displayed in Θ\Theta, while

K=Q+(Lz−aE)2K=Q+(L_z-aE)^2

is the direct quadratic contraction with a suitably normalized rank-two Killing tensor. Papers may call either QQ or KK “the Carter constant.” Stating the radial potential removes the ambiguity. Carter’s original separation result is Carter 1968, pp. 1559–1571.

In the Schwarzschild limit a→0a\to0,

Θ=Q−Lz2cot⁡2θ,L2=Q+Lz2.\Theta=Q-L_z^2\cot^2\theta, \qquad L^2=Q+L_z^2.

Thus the hidden constant becomes the familiar total angular momentum squared after spherical symmetry is restored. For an equatorial orbit, θ=π/2\theta=\pi/2 and dθ/dλ=0d\theta/d\lambda=0 require Q=0Q=0; reflection symmetry then keeps the orbit in the plane. These two limits independently check the signs in Θ\Theta.

The potentials also expose parameter redundancies and dimensions. For null geodesics with E≠0E\neq0, rescaling the affine parameter rescales (E,Lz,Q)(E,L_z,\sqrt Q) together, so the unparametrized trajectory depends on the impact parameters ξ=Lz/E\xi=L_z/E and η=Q/E2\eta=Q/E^2. A radial spherical photon orbit at r=r0r=r_0 must satisfy both R(r0)=0R(r_0)=0 and R′(r0)=0R'(r_0)=0; the first condition alone identifies a turning point, not a constant-radius ray. For massive geodesics, EE is specific energy when the momentum is divided by μ\mu, and that normalization should not be mixed with the null impact-parameter convention.

Boyer–Lindquist separation is valid on any coordinate patch where the displayed inverse metric applies, including regions where Δ\Delta changes sign, but the interpretation of rr as a spatial variable and tt as a time coordinate then changes. The separated first integrals remain tensorial statements; the chart-based signs of individual coordinate velocities do not.

Separation gives quadratures, not automatically elementary closed-form trajectories. It also does not decide whether a permitted orbit is stable, bound, future-complete, or physically realizable under radiation reaction. Those questions require analysis of the potentials or dynamical methods beyond the exact background geometry.

Show that a null geodesic with constant latitude away from the axis must obey both Θ(θ0)=0\Theta(\theta_0)=0 and Θ′(θ0)=0\Theta'(\theta_0)=0.

Solution

In Mino time, (dθ/dλM)2=Θ(θ)(d\theta/d\lambda_{\rm M})^2=\Theta(\theta). A constant solution has zero polar velocity, so Θ(θ0)=0\Theta(\theta_0)=0. Its differentiated equation is 2θ′θ′′=Θ′θ′2\theta'\theta''=\Theta'\theta', which loses information at θ′=0\theta'=0; using the second-order geodesic equation, or taking the continuous limit from nearby trajectories, additionally gives θ′′=Θ′(θ0)/2=0\theta''=\Theta'(\theta_0)/2=0. Hence the root must be stationary. The equatorial case satisfies this automatically by reflection symmetry when Q=0Q=0.

  • Carter, Brandon. “Global Structure of the Kerr Family of Gravitational Fields.” Physical Review 174 (1968): 1559–1571. DOI.
  • Frolov, Valeri P., Pavel Krtouš, and David Kubizňák. “Black Holes, Hidden Symmetries, and Complete Integrability.” Living Reviews in Relativity 20 (2017): 6. DOI; Open PDF.