A Worked Example of the Proof of KLS Conjecture

This worked example accompanies “A Dimension-Free Bound on the Poincaré Constant of Isotropic Log-Concave Measures”, by Krishnakumar Balasubramanian and Shiva Kasiviswanathan.

Here, we consider a two-dimensional example that makes the ingredients of the paper’s argument concrete. We work through its calculations below and identify the general results we use from the paper by name and number. This companion illustrates the proposed argument; it does not independently verify the paper’s general theorems.

The Poincaré inequality compares the variance of a function with the average squared size of its gradient:

Var⁡μf≤KP Eμ∣∇f∣2.\Var_\mu f\le K_{\mathrm{P}}\,\E_\mu|\nabla f|^2.

The left side measures how much a function fluctuates. The right side measures how much it changes locally. Recovering a centered function from its gradient is therefore exactly the operation we need to control. The gradient determines the function up to an additive constant, which the mean-zero condition fixes. For a centered function, variance is the average of its square, so the Poincaré inequality asks us to bound that average by a constant times the average squared gradient. The challenge is to control this recovery for every admissible gradient, starting from estimates for polynomials.

00 / The Distribution

The Radial Exponential Family

Let (X,Y)(X,Y) have a radial exponential law, whose density depends only on distance from the origin. Keep the scale parameter visible for now:

dμλ(x,y)=λ22πe−λr dx dy,r=x2+y2,λ>0.d\mu_\lambda(x,y)=\frac{\lambda^2}{2\pi}e^{-\lambda r}\,dx\,dy, \qquad r=\sqrt{x^2+y^2},\quad\lambda>0.

In polar coordinates, the angle is uniform and independent of the radius R=X2+Y2R=\sqrt{X^2+Y^2}. The radius has density λ2re−λr\lambda^2r e^{-\lambda r}. Integration by parts, starting with ∫0∞e−λrdr=1/λ\int_0^\infty e^{-\lambda r}dr=1/\lambda, gives, for integers j≥1j\ge1 and k≥0k\ge0,

∫0∞rje−λrdr=jλ∫0∞rj−1e−λrdr=j!λj+1,ERk=(k+1)!λk.\int_0^\infty r^j e^{-\lambda r}dr =\frac j\lambda\int_0^\infty r^{j-1}e^{-\lambda r}dr =\frac{j!}{\lambda^{j+1}},\qquad \E R^k=\frac{(k+1)!}{\lambda^k}.

The case k=0k=0 verifies normalization. Symmetry gives zero mean and zero cross-covariance. The angular average of cos⁡2θ\cos^2\theta is 1/21/2, so, writing Id\Id for the identity operator (here a two-by-two matrix),

Cov⁡(μλ)=ER22Id=3λ2Id.\Cov(\mu_\lambda)=\frac{\E R^2}{2}\Id=\frac3{\lambda^2}\Id.

Thus λ=3\lambda=\sqrt3 puts the law in isotropic position. We use that value from now on unless a scale is displayed explicitly.

Radial Scaling

Radial Density and Covariance

The plotted curve is the density of the radius, including the polar-coordinate Jacobian. Moving the scale parameter changes both the peak and the covariance.

The radius has density λ²r exp(−λr), and each coordinate has variance 3/λ².
Variance of each coordinate1.000
Most likely radius0.577

Analytic formulas: radial density λ2re−λr\lambda^2r e^{-\lambda r}, covariance (3/λ2)Id(3/\lambda^2)\Id. The article uses λ=3\lambda=\sqrt3, which makes the covariance Id\Id.

Isotropy does not mean independence. Here the angular averages of cos⁡4θ\cos^4\theta and cos⁡2θsin⁡2θ\cos^2\theta\sin^2\theta are 3/83/8 and 1/81/8, respectively. Hence

EX4=385!9=5,EX2Y2=185!9=53≠1=EX2 EY2.\E X^4=\frac38\frac{5!}{9}=5,\qquad \E X^2Y^2=\frac18\frac{5!}{9}=\frac53\ne1=\E X^2\,\E Y^2.

The common radius couples the coordinates. There is also a geometric obstruction: with er=(x,y)/re_r=(x,y)/r, the potential satisfies, away from the origin,

D2(3r)=3r(Id−erer⊤).D^2(\sqrt3r)=\frac{\sqrt3}{r}(\Id-e_re_r^\top).

Its radial eigenvalue is zero. A curvature bound of the form D2V⪰aIdD^2V\succeq a\Id, with a>0a>0, is therefore unavailable for the original law. This is why the later localization step has a job to do.

01 / Paper §3 · Lemma 3.1

Compatibility Projection and Its Energy Cost

A vector field v=(v1,v2)v=(v_1,v_2) can be a gradient only if ∂yv1=∂xv2\partial_yv_1=\partial_xv_2. On the plane this is the familiar compatibility condition. For a symmetric matrix field FF, the corresponding Hessian conditions are

∂yF11=∂xF12,∂yF12=∂xF22.\partial_yF_{11}=\partial_xF_{12},\qquad \partial_yF_{12}=\partial_xF_{22}.

At higher ranks, compatibility again says that exchanging the new derivative index with any tensor index changes nothing. These are the fields on which repeated integration makes sense.

To calculate with a smooth potential, temporarily replace 3r\sqrt3r by

Vε(x,y)=3ε2+r2+ε2r2,ε>0.V_\varepsilon(x,y)=\sqrt3\sqrt{\varepsilon^2+r^2}+\frac\varepsilon2r^2, \qquad\varepsilon>0.

Writing s=ε2+r2s=\sqrt{\varepsilon^2+r^2}, differentiation gives

Kε=D2Vε=εId+3(Ids−(x,y)(x,y)⊤s3).K_\varepsilon=D^2V_\varepsilon =\varepsilon \Id+\sqrt3\left(\frac{\Id}{s}-\frac{(x,y)(x,y)^\top}{s^3}\right).

Its radial and tangential eigenvalues are ε+3ε2/s3\varepsilon+\sqrt3\varepsilon^2/s^3 and ε+3/s\varepsilon+\sqrt3/s. Thus

εId⪯Kε⪯(ε+3ε)Id.\varepsilon \Id\preceq K_\varepsilon\preceq \left(\varepsilon+\frac{\sqrt3}{\varepsilon}\right)\Id.

All norms in the next calculation use the smooth density proportional to e−Vεe^{-V_\varepsilon}. In a weighted space, the adjoint of differentiation is ∂i∗=−∂i+Vi\partial_i^*=-\partial_i+V_i. Even a constant Hessian can lose compatibility under this adjoint:

F=D2(xy)=(0110),U=div⁡VF=(Vy,Vx).F=D^2(xy)=\begin{pmatrix}0&1\\1&0\end{pmatrix}, \qquad U=\operatorname{div}_V F=(V_y,V_x). CU:=∂xU2−∂yU1=Vxx−Vyy=3(y2−x2)(ε2+x2+y2)3/2.CU:=\partial_xU_2-\partial_yU_1 =V_{xx}-V_{yy} =\frac{\sqrt3(y^2-x^2)}{(\varepsilon^2+x^2+y^2)^{3/2}}.
Compatibility Defect

Curl of Weighted Divergence

For the mixed Hessian input, the weighted divergence is U=(Vy,Vx)U=(V_y,V_x). Its curl is positive near the vertical axis and negative near the horizontal axis.

Curl equals √3(y²−x²)/(ε²+x²+y²)^(3/2). It vanishes on y = ±x.
Negative curl Positive curl

The color range is symmetric, from −1.667 to the corresponding positive value, and rescales with ε. This picture illustrates the analytic curl identity; it does not compute the Hodge projection.

The correction is an orthogonal projection in L2(μ)L^2(\mu), rather than a pointwise alteration of the arrows. If PP projects onto compatible vector fields, weighted Hodge theory represents the discarded part as

(Id−P)U=C∗(CC∗)−1CU,∥(Id−P)U∥22=⟨CU,(CC∗)−1CU⟩.(\Id-P)U=C^*(CC^*)^{-1}CU,\qquad \|(\Id-P)U\|_2^2=\langle CU,(CC^*)^{-1}CU\rangle.
The Weighted Hodge Laplacian and Compatibility Projection

For a test function ϕ\phi, integration by parts in the two terms defining CC yields

C∗ϕ=(∂yϕ−Vyϕ,−∂xϕ+Vxϕ).C^*\phi=(\partial_y\phi-V_y\phi,-\partial_x\phi+V_x\phi).

Taking its curl and collecting the terms gives

CC∗ϕ=∂x(−∂xϕ+Vxϕ)−∂y(∂yϕ−Vyϕ)=−Δϕ+Vx∂xϕ+Vy∂yϕ+(Vxx+Vyy)ϕ=Hϕ+(ΔV)ϕ,H=−Δ+∇V⋅∇.\begin{aligned} CC^*\phi &=\partial_x(-\partial_x\phi+V_x\phi)-\partial_y(\partial_y\phi-V_y\phi)\\ &=-\Delta\phi+V_x\partial_x\phi+V_y\partial_y\phi+(V_{xx}+V_{yy})\phi\\ &=H\phi+(\Delta V)\phi,\qquad H=-\Delta+\nabla V\cdot\nabla. \end{aligned}

For the regularized law, ΔV≥2ε\Delta V\ge2\varepsilon, so the closed quadratic form gives an invertible positive operator. Put ω=(CC∗)−1CU\omega=(CC^*)^{-1}CU. Then C(U−C∗ω)=0C(U-C^*\omega)=0, while ⟨C∗ω,v⟩=⟨ω,Cv⟩=0\langle C^*\omega,v\rangle=\langle\omega,Cv\rangle=0 for every compatible vv in the form domain. Closing these identities gives the displayed orthogonal projection. Finally,

∥C∗ω∥22=⟨ω,CC∗ω⟩=⟨(CC∗)−1CU,CU⟩.\|C^*\omega\|_2^2=\langle\omega,CC^*\omega\rangle =\langle (CC^*)^{-1}CU,CU\rangle.

This calculation is on vector fields and two-forms. The manuscript's higher-rank comparison requires its additional constrained tensor argument.

The point of the comparison is to show that the projection leaves enough energy. In the manuscript's rank-two calculation, choose at each point an orthonormal basis in which K=D2VK=D^2V has eigenvalues κ1,κ2>0\kappa_1,\kappa_2>0. The curl term is (κ1−κ2)F12(\kappa_1-\kappa_2)F_{12}. The inverse-Hodge estimate bounds the energy lost by

∥(Id−P)U∥22≤E(κ1−κ2)2κ1+κ2F122.\|(\Id-P)U\|_2^2\le \E\frac{(\kappa_1-\kappa_2)^2}{\kappa_1+\kappa_2}F_{12}^2.

The unprojected mixed-component energy has weight κ1+κ2\kappa_1+\kappa_2. Subtracting the possible loss gives exactly

(κ1+κ2−(κ1−κ2)2κ1+κ2)F122=2κ1κ2κ1+κ2 (2F122).\left(\kappa_1+\kappa_2- \frac{(\kappa_1-\kappa_2)^2}{\kappa_1+\kappa_2}\right)F_{12}^2 =\frac{2\kappa_1\kappa_2}{\kappa_1+\kappa_2}\,(2F_{12}^2).

The factor 2F1222F_{12}^2 is the squared norm of the mixed symmetric component: both ordered entries are counted. The surviving curvature is its harmonic mean. Unequal curvatures create curl, but the correction does not erase the lower curvature bound.

From the Paper · Compatible-Tensor Hodge Estimate

Lemma 3.1 extends the curvature bound to every tensor rank. It applies to regular laws: centered laws with a smooth potential whose Hessian is bounded above and below by positive multiples of the identity. If D2V⪰aIdD^2V\succeq a\Id, write Dm\mathscr D_m for differentiation on centered compatible rank-mm fields. For every FF in the domain of its adjoint, the lemma gives

∥Dm∗F∥22≥∥∇F∥22+a∥F∥22.\|\mathscr D_m^*F\|_2^2\ge\|\nabla F\|_2^2+a\|F\|_2^2.

The lower curvature bound aa survives unchanged as the number of tensor indices grows. This uniformity is what lets the next step control arbitrarily long integration chains.

02 / Paper §4

Centered Integration and Appell Polynomials

For a compatible field F=∇uF=\nabla u, its centered primitive is u−Euu-\E u. The manuscript separates two kinds of inputs. The operator LrL_r integrates a constant tensor of rank r+1r+1; JrJ_r integrates a compatible field of that rank whose mean is already zero. Both return centered fields of rank rr. For a centered law, their defining identities are

LrT=T⌟x,∇JrF=F,EJrF=0.L_rT=T\mathbin{\lrcorner}x,\qquad \nabla J_rF=F,\qquad\E J_rF=0.

The constant-input chain along the first coordinate is completely explicit. Successive integrations and centering give

1 →L x →J x2−12 →J x3−3x6 →J x4−6x2+124.1\ \xrightarrow{L}\ x\ \xrightarrow{J}\ \frac{x^2-1}{2} \ \xrightarrow{J}\ \frac{x^3-3x}{6} \ \xrightarrow{J}\ \frac{x^4-6x^2+1}{24}.

For example, an antiderivative of (x3−3x)/6(x^3-3x)/6 is x4/24−x2/4x^4/24-x^2/4. Its mean is 5/24−1/4=−1/245/24-1/4=-1/24, so centering adds 1/241/24. This is why the final constant differs from the Gaussian one.

These are normalized Appell polynomials. We use the paper’s Appell tensors and scalar contractions, with the normalized shorthand

ez⋅xEez⋅X=∑d=0∞⟨Adμ(x),z⊗d⟩d!,pd[T]=Pdμ[T]d!=⟨T,Adμ⟩d!.\frac{e^{z\cdot x}}{\E e^{z\cdot X}} =\sum_{d=0}^\infty\frac{\langle \mathcal A_d^\mu(x),z^{\otimes d}\rangle}{d!}, \qquad p_d[T]=\frac{P_d^\mu[T]}{d!}=\frac{\langle T,\mathcal A_d^\mu\rangle}{d!}.

Coefficient comparison after differentiation and expectation gives Ddpd[T]=TD^dp_d[T]=T and EDjpd[T]=0\E D^jp_d[T]=0 for 0≤j<d0\le j<d. Thus

pd[T]=J0J1⋯Jd−2Ld−1T.p_d[T]=J_0J_1\cdots J_{d-2}L_{d-1}T.

The rightmost operator acts first. The distinct LL matters: a nonzero constant tensor is not a centered input for JJ.

The Radial Appell Generating Function

Rotational invariance implies that z⋅Xz\cdot X has the same law as ∣z∣X1|z|X_1 for real zz. The polar moments give

EX12k=(2k+1)!!(2k−1)!!3k,EX12k(2k)!=(3/2)k3kk!.\E X_1^{2k}=\frac{(2k+1)!!(2k-1)!!}{3^k},\qquad \frac{\E X_1^{2k}}{(2k)!}=\frac{(3/2)_k}{3^k k!}.

Here (3/2)k=(3/2)(5/2)⋯(3/2+k−1)(3/2)_k=(3/2)(5/2)\cdots(3/2+k-1), with value one at k=0k=0. Odd moments vanish. The binomial series therefore gives

M(z)=Eez⋅X=(1−z12+z223)−3/2,∣z∣<3.M(z)=\E e^{z\cdot X}=\left(1-\frac{z_1^2+z_2^2}{3}\right)^{-3/2},\qquad |z|<\sqrt3.

The Appell generating function is ez⋅x(1−(z12+z22)/3)3/2e^{z\cdot x}(1-(z_1^2+z_2^2)/3)^{3/2}. Only finitely many moments are needed at any fixed degree; the manuscript also uses this identity formally, without needing analytic convergence.

The Mixed Quartic Integration Chain

Use both coordinates by taking

q(x,y)=x2y2−x2−y2+13.q(x,y)=x^2y^2-x^2-y^2+\frac13.

Its mean is 5/3−1−1+1/3=05/3-1-1+1/3=0. Its first two derivatives are

∇q=(2x(y2−1)2y(x2−1)),D2q=(2(y2−1)4xy4xy2(x2−1)).\nabla q=\begin{pmatrix}2x(y^2-1)\\2y(x^2-1)\end{pmatrix},\qquad D^2q=\begin{pmatrix}2(y^2-1)&4xy\\4xy&2(x^2-1)\end{pmatrix}.

The cross derivatives of ∇q\nabla q both equal 4xy4xy; the matrix identities are ∂y[2(y2−1)]=∂x(4xy)=4y\partial_y[2(y^2-1)]=\partial_x(4xy)=4y and ∂y(4xy)=∂x[2(x2−1)]=4x\partial_y(4xy)=\partial_x[2(x^2-1)]=4x. Compatibility is visible entry by entry.

Constant-Tensor Integration

Successive Integration of a Constant Tensor

Start with the unit symmetric rank-four tensor whose six (1,1,2,2)(1,1,2,2) permutations each have entry 1/61/\sqrt6.

T1122=16,∥T∥HS2=6⋅16=1.T_{1122}=\frac1{\sqrt6},\qquad\|T\|_{\HS}^2=6\cdot\frac16=1.

A constant input: the first operation must be L3L_3.

The means vanish at every nonconstant stage. No coordinatewise choice of unrelated primitives is made.

Derivative Norms and Poincaré Test Quotients

The additional moments needed are EX4Y2=35/3\E X^4Y^2=35/3 and EX4Y4=105\E X^4Y^4=105. They follow from the same polar moment formula. Expanding gives

Eq2=105+10+19−1403+103+109−43=6449,E∣∇q∣2=8(353−103+1)=2243,E∥D2q∥HS2=8(5−2+1)+32⋅53=2563,E∥D3q∥HS2=3⋅16EX2+3⋅16EY2=96.\begin{aligned} \E q^2&=105+10+\tfrac19-\tfrac{140}3+\tfrac{10}3+\tfrac{10}9-\tfrac43=\tfrac{644}9,\\ \E|\nabla q|^2&=8(\tfrac{35}3-\tfrac{10}3+1)=\tfrac{224}3,\\ \E\|D^2q\|_{\HS}^2&=8(5-2+1)+32\cdot\tfrac53=\tfrac{256}3,\\ \E\|D^3q\|_{\HS}^2&=3\cdot16\E X^2+3\cdot16\E Y^2=96. \end{aligned}

Division by (46)2=96(4\sqrt6)^2=96 gives the displayed norms. A single test function yields a lower bound on the best Poincaré constant; these checks do not yet give an upper bound for all functions.

The draft's coefficient is the supremum over unit leading tensors:

cd(μ)=sup⁡∥T∥HS=1∥pd[T]∥2.c_d(\mu)=\sup_{\|T\|_{\HS}=1}\|p_d[T]\|_2.

Even at degree two, one direction does not attain this supremum. For a symmetric matrix TT, p2[T]=(x⊤Tx−Tr⁡T)/2p_2[T]=(x^\top Tx-\Tr T)/2. The fourth moments yield

∥p2[T]∥22=56∥T∥HS2+16(Tr⁡T)2.\|p_2[T]\|_2^2=\frac56\|T\|_{\HS}^2+\frac16(\Tr T)^2.

Since (Tr⁡T)2≤2∥T∥HS2(\Tr T)^2\le2\|T\|_{\HS}^2, equality at T=Id/2T=\Id/\sqrt2 gives c2(μ)2=7/6c_2(\mu)^2=7/6. In contrast, the directional polynomial (x2−1)/2(x^2-1)/2 has squared norm one.

The Degree-Two Appell Coefficient Norm

Write T=(abbc)T=\begin{pmatrix}a&b\\b&c\end{pmatrix}. Odd-coordinate moments vanish, so

E(X⊤TX)2=5a2+5c2+53(4b2+2ac),EX⊤TX=a+c.\E(X^\top TX)^2=5a^2+5c^2+\frac53(4b^2+2ac),\qquad \E X^\top TX=a+c.

Subtract the squared mean and divide by four:

∥p2[T]∥22=a2+c2+53b2+13ac=56(a2+2b2+c2)+16(a+c)2.\|p_2[T]\|_2^2=a^2+c^2+\frac53b^2+\frac13ac =\frac56(a^2+2b^2+c^2)+\frac16(a+c)^2.

This is the claimed tensor-norm formula.

03 / Paper §5 · Lemma 5.1 & Corollary 5.2

Uniform Bounds for Integration Powers

Appell norms observe integration chains that start at constant tensors. A general compatible input can depend on position in any square-integrable way. Curvature connects these special observations to the full integration operator.

The paper bundles all tensor ranks into one Hilbert space, so that a single operator J\mathsf J lowers rank and L\mathsf L supplies the constant-input primitives. The inverse comparison in §4.2, based on Lemma 3.1, gives the following inequality. Appendix B supplies the operator-domain details.

J∗J⪯g(JJ∗+LL∗),g(u)=u1+au,∥Jj−1L∥≤cj(ν).\mathsf J^*\mathsf J\preceq g(\mathsf J\mathsf J^*+\mathsf L\mathsf L^*),\qquad g(u)=\frac{u}{1+au}, \qquad \|\mathsf J^{j-1}\mathsf L\|\le c_j(\nu).

The function gg acts on the operator’s spectral values, just as a function of a symmetric matrix acts on its eigenvalues. Its denominator records the contribution of curvature. The uniform power lemma, Lemma 5.1, uses this comparison and finitely many constant-input bounds to control every power of J\mathsf J.

From the Paper · Uniform Integration Powers

For a regular centered law ν\nu with covariance at most Id\Id, curvature at least aIda\Id, and

cj(ν)≤ρj(j+1)4(2≤j≤D),ρ≥1, D≥2,c_j(\nu)\le\frac{\rho^j}{(j+1)^4}\quad(2\le j\le D),\qquad \rho\ge1,\ D\ge2,

Corollary 5.2 states, simultaneously for every q≥1q\ge1,

 ∥Jq∥2≤2Bq,B=ρ2max⁡{1,a−1/(D+1)}. \boxed{\ \|\mathsf J^q\|^2\le2B^q,\qquad B=\rho^2\max\{1,a^{-1/(D+1)}\}.\ }

The factor two is paid once for the whole chain. Applying a one-integration bound repeatedly would instead introduce 2q2^q, which is not the estimate used in the induction.

The Curvature Penalty

Degree Dependence of the Curvature Penalty

Hold a=10−6a=10^{-6} fixed and change the known polynomial cutoff.

Factor in B/ρ2B/\rho^22.8943

This is a−1/(D+1)a^{-1/(D+1)}, a direct evaluation of the bound. The dimension stays two; DD counts polynomial degrees.

There is still a circular-looking issue: the polynomial estimates needed by this result are themselves unknown at high degree. Localization and reverse transfer turn that circle into an induction, using only smaller degrees to establish the next one.

04 / Paper §6.1

Covariance-Normalized Stochastic Localization

Localization reweights a law by a linear tilt and a Gaussian factor. For our radial example, the tilted density is proportional to

exp⁡ ⁣(−3r+θt⋅x−12x⊤Λtx).\exp\!\left(-\sqrt3r+\theta_t\cdot x-\tfrac12x^\top\Lambda_t x\right).

The linear term moves the region carrying most of the mass; the quadratic term adds curvature. The paper proves its stochastic estimates first for bounded-support isotropic laws. For this example, it conditions on a large disk, rescales to restore isotropy, and then passes to the limit. The expandable calculation below describes that approximation.

For the bounded-support process, Et\E_t denotes expectation under the current random law, or posterior. Let mt=EtXm_t=\E_tX, At=Cov⁡t(X)A_t=\Cov_t(X), and let BtB_t be planar Brownian motion. The parameters obey

dθt=At−1/2dBt+At−1mt dt,dΛt=At−1dt,θ0=Λ0=0.d\theta_t=A_t^{-1/2}dB_t+A_t^{-1}m_t\,dt,\qquad d\Lambda_t=A_t^{-1}dt,\qquad\theta_0=\Lambda_0=0.

Consequently Λt=∫0tAs−1ds\Lambda_t=\int_0^tA_s^{-1}ds, and the posterior has curvature at least Λt\Lambda_t for t>0t>0. For a nonsmooth potential, this means that subtracting the corresponding quadratic leaves a convex function; it does not require a pointwise Hessian at the origin. The original radial symmetry generally disappears along a path, so neither AtA_t nor Λt\Lambda_t can be replaced by a scalar multiple of the identity.

Posterior Appell Coefficients

Gaussian Tilting and Appell Recentering

Explore the posterior density proportional to exp⁡(−3r+θx−(q1x2+q2y2)/2)\exp(-\sqrt3r+\theta x-(q_1x^2+q_2y^2)/2), with q1=τq_1=\tau and q2=ταq_2=\tau\alpha. It remains symmetric under y↦−yy\mapsto-y.

The tilted density is computed from the exact radial model. The gold point is the mean and the gold ellipse represents one covariance unit.

Gold: mean and covariance ellipse. The ellipse is not a probability contour. Density brightness uses a nonlinear scale for legibility.

q₁, q₂0.400, 0.700
Mean in x—
A₁₁—
A₂₂—
κ₁₂₂—
κ₁₁₂₂—

With z1=x−EXz_1=x-\E X and z2=yz_2=y, the centered mixed Appell polynomial is

P=z12z22−A11z22−A22z12−2κ122z1+A11A22−κ1122.P=z_1^2z_2^2-A_{11}z_2^2-A_{22}z_1^2-2\kappa_{122}z_1+A_{11}A_{22}-\kappa_{1122}.
Coefficient of z₂²—
Coefficient of z₁²—
Coefficient of z₁—
Constant term—

Numerical illustration: moments use Simpson quadrature of the one-dimensional Gaussian scale-mixture formula (800 intervals in log scale). These controls select deterministic posterior parameters; they do not simulate an adapted stochastic localization path or verify a theorem.

Gaussian Scale Mixtures and Posterior Moments

The radial law is a Gaussian scale mixture: take SS with Gamma shape 3/23/2 and rate 3/23/2, then X∣S=s∼N(0,sId)X\mid S=s\sim N(0,s\Id). Multiplying the two densities leaves a constant times

∫0∞s−1/2e−3s/2−r2/(2s)ds=2π3 e−3r.\int_0^\infty s^{-1/2}e^{-3s/2-r^2/(2s)}ds =\sqrt{\frac{2\pi}3}\,e^{-\sqrt3r}.

To check the integral identity, put I(a,b)=∫0∞s−1/2e−as−b/sdsI(a,b)=\int_0^\infty s^{-1/2}e^{-as-b/s}ds. For b>0b>0, substitute s=b/(at)s=b/(at) into −∂bI-\partial_b I; this gives ∂bI=−a/b I\partial_b I=-\sqrt{a/b}\,I. Integrating in bb, with I(a,0)=π/aI(a,0)=\sqrt{\pi/a}, gives I(a,b)=π/ae−2abI(a,b)=\sqrt{\pi/a}e^{-2\sqrt{ab}}. The normalized mixture therefore has exactly our radial density.

A deterministic tilt by eθ⋅x−x⊤Qx/2e^{\theta\cdot x-x^\top Qx/2} changes the conditional Gaussian to

Cs=(s−1Id+Q)−1,ms=Csθ,X∣S=s∼N(ms,Cs).C_s=(s^{-1}\Id+Q)^{-1},\qquad m_s=C_s\theta,\qquad X\mid S=s\sim N(m_s,C_s).

Completing its quadratic exponent shows that the updated scale density is proportional to

s1/2e−3s/2det⁡(Id+sQ)−1/2exp⁡ ⁣(12θ⊤Csθ).s^{1/2}e^{-3s/2}\det(\Id+sQ)^{-1/2} \exp\!\left(\tfrac12\theta^\top C_s\theta\right).

Normalize this density to π(ds)\pi(ds). Then m=∫msπ(ds)m=\int m_s\pi(ds) and A=∫(Cs+msms⊤)π(ds)−mm⊤A=\int(C_s+m_sm_s^\top)\pi(ds)-mm^\top. In the explorer Q=diag⁡(q1,q2)Q=\operatorname{diag}(q_1,q_2) and θ=(θ1,0)\theta=(\theta_1,0), so, writing ci=(Cs)iic_i=(C_s)_{ii} and m1=(ms)1m_1=(m_s)_1, the needed conditional moments are

E[X12∣s]=c1+m12,E[X22∣s]=c2,E[X1X22∣s]=m1c2,E[X12X22∣s]=(c1+m12)c2.\E[X_1^2\mid s]=c_1+m_1^2,\quad \E[X_2^2\mid s]=c_2,\quad \E[X_1X_2^2\mid s]=m_1c_2,\quad \E[X_1^2X_2^2\mid s]=(c_1+m_1^2)c_2.

Integrating these scalar expressions gives the displayed covariance and cumulants. The browser evaluates the integrals numerically; the identities above specify the exact quantities being approximated.

Compact-Support Approximation and Isotropic Normalization

The manuscript first proves its stochastic estimates for compactly supported isotropic laws. For this example, condition XX on ∣X∣≤R|X|\le R and divide by vR\sqrt{v_R}, where

vR=∫0Rr3e−3rdr2∫0Rre−3rdr.v_R=\frac{\int_0^R r^3e^{-\sqrt3r}dr}{2\int_0^R re^{-\sqrt3r}dr}.

The resulting law is isotropic and has density proportional to e−3vR∣y∣e^{-\sqrt3\sqrt{v_R}|y|} on the disk of radius R/vRR/\sqrt{v_R}. It is log-concave because the potential and support are convex. As R→∞R\to\infty, vR→1v_R\to1; dominated convergence gives every fixed moment of the original radial law. Appell coefficients at degree dd use only moments through 2d2d, so the coefficient inequalities pass to this limit. The untruncated family shown in the explorer makes the same tilt geometry visible.

For the bounded-support process, the special drift in θt\theta_t makes the normalized density a martingale:

dρt(x)=ρt(x)ξt(x)⋅dBt,ξt(x)=At−1/2(x−mt),ρt=dμtdμ0.d\rho_t(x)=\rho_t(x)\xi_t(x)\cdot dB_t, \qquad \xi_t(x)=A_t^{-1/2}(x-m_t),\quad \rho_t=\frac{d\mu_t}{d\mu_0}.

For a fixed test function, this gives dEtf=Et[(f−Etf)ξt]⋅dBtd\E_tf=\E_t[(f-\E_tf)\xi_t]\cdot dB_t. In particular, the mean moves and the covariance fluctuates according to

dmt=At1/2dBt,dAt=∑iUi,t dBi,t−Atdt,Ui,t=Et[(X−mt)(X−mt)⊤ξi,t].dm_t=A_t^{1/2}dB_t,\qquad dA_t=\sum_iU_{i,t}\,dB_{i,t}-A_tdt,\quad U_{i,t}=\E_t[(X-m_t)(X-m_t)^\top\xi_{i,t}].

The third moments vanish initially by symmetry, but generally become nonzero after tilting. The paper uses Letwin's quadratic variance inequality, stated in §2.3, to control them. That input leads to the mixed covariance bound needed later:

Epath ⁣[(At+δΛt−1)⊗q⊗At⊗(d−q)]⪯(1+δ/t)qe4d2tId.\E_{\rm path}\!\left[(A_t+\delta\Lambda_t^{-1})^{\otimes q} \otimes A_t^{\otimes(d-q)}\right] \preceq(1+\delta/t)^qe^{4d^2t}\Id.

This is the mixed covariance estimate from §6.1. The expectation here is over the localization path; Et\E_t instead means integration under its current random law. The ordered tensor slots keep the matrix factors in their proper places without requiring them to commute.

05 / Paper §6.2 · Lemma 6.2

Appell Polynomials Under Localization

Our original mixed quartic used EXi2=1\E X_i^2=1 and EX12X22=5/3\E X_1^2X_2^2=5/3. After localization, those moments change. Keeping the same polynomial would break the mean-zero constraints required by the integration chain.

Keep the leading tensor fixed, but replace all lower coefficients with the Appell coefficients of the current law. Write z=x−mtz=x-m_t. With covariance entries AijA_{ij}, third central moments κijk\kappa_{ijk}, and

κ1122=Etz12z22−A11A22−2A122,\kappa_{1122}=\E_tz_1^2z_2^2-A_{11}A_{22}-2A_{12}^2,

the moving mixed quartic is

P1122,t(x)=z12z22−A11z22−A22z12−4A12z1z2−2κ112z2−2κ122z1+A11A22+2A122−κ1122.\begin{aligned} P_{1122,t}(x)={}&z_1^2z_2^2-A_{11}z_2^2-A_{22}z_1^2-4A_{12}z_1z_2\\ &-2\kappa_{112}z_2-2\kappa_{122}z_1 +A_{11}A_{22}+2A_{12}^2-\kappa_{1122}. \end{aligned}

At time zero, A=IdA=\Id, the third moments are zero, and κ1122=2/3\kappa_{1122}=2/3. This recovers x2y2−x2−y2+1/3x^2y^2-x^2-y^2+1/3.

Centering Constraints for the Moving Quartic

Taking the expectation of the displayed quartic gives

EtP1122,t=(κ1122+A11A22+2A122)−2A11A22−4A122+A11A22+2A122−κ1122=0.\begin{aligned} \E_tP_{1122,t} ={}&(\kappa_{1122}+A_{11}A_{22}+2A_{12}^2) -2A_{11}A_{22}-4A_{12}^2\\ &+A_{11}A_{22}+2A_{12}^2-\kappa_{1122}=0. \end{aligned}

Its first derivatives are

∂1P1122,t=2(z1z22−A22z1−2A12z2−κ122),\partial_1P_{1122,t}=2(z_1z_2^2-A_{22}z_1-2A_{12}z_2-\kappa_{122}), ∂2P1122,t=2(z12z2−A11z2−2A12z1−κ112).\partial_2P_{1122,t}=2(z_1^2z_2-A_{11}z_2-2A_{12}z_1-\kappa_{112}).

They have zero mean because Etzi=0\E_tz_i=0, Etz1z22=κ122\E_tz_1z_2^2=\kappa_{122} and Etz12z2=κ112\E_tz_1^2z_2=\kappa_{112}. Its Hessian is

D2P1122,t=(2(z22−A22)4(z1z2−A12)4(z1z2−A12)2(z12−A11)),D^2P_{1122,t}=\begin{pmatrix} 2(z_2^2-A_{22})&4(z_1z_2-A_{12})\\ 4(z_1z_2-A_{12})&2(z_1^2-A_{11}) \end{pmatrix},

whose mean is zero entry by entry. The nonzero third derivatives are 4z24z_2 and 4z14z_1, with their permutations, so their means also vanish. The fourth derivative is the same constant tensor at all times. Commuting spatial derivatives retains compatibility throughout.

These identities preserve the integration constraints, but they do not say that the polynomial's variance is a martingale. Its coefficients are changing too. Lemma 6.2 estimates that additional effect.

From the Paper · Moving Appell Variance

Put pt=Pdμt[T]p_t=P_d^{\mu_t}[T] and V(t)=EpathEtpt2\mathcal V(t)=\E_{\rm path}\E_tp_t^2. If CkC_k bounds degree kk coefficients of every isotropic log-concave law for k<dk<d, set

Σd=∑k=2d−1(d−k+1)CkCd−k+1,Σ2=0.\Sigma_d=\sum_{k=2}^{d-1}(d-k+1)C_kC_{d-k+1},\qquad\Sigma_2=0.

The moving variance estimate in Lemma 6.2 gives

V(0)≤e(d+1)tV(t)+d!Σdt e(2d2+d+1)t∥T∥HS.\sqrt{\mathcal V(0)}\le e^{(d+1)t}\sqrt{\mathcal V(t)} +d!\Sigma_dt\,e^{(2d^2+d+1)t}\|T\|_{\HS}.

The error uses only smaller degrees. For the quartic, Σ4=3C2C3+2C3C2=5C2C3\Sigma_4=3C_2C_3+2C_3C_2=5C_2C_3. For degree two it is zero.

06 / Paper §7 · Proposition 7.1

Reverse Coefficient Transfer

The integration bound requires covariance at most Id\Id and curvature at least δId\delta \Id, where 0<δ≤10<\delta\le1. First consider a smooth posterior whose Hessian also has a finite upper bound. Write AA for its covariance and BB for a positive curvature lower bound. One change of coordinates arranges both conditions:

M=A+δB−1,Y=M−1/2(X−m),\mathsf M=A+\delta B^{-1},\qquad Y=\mathsf M^{-1/2}(X-m),

Here mm is the posterior mean. Since M⪰A\mathsf M\succeq A, Cov⁡(Y)=M−1/2AM−1/2⪯Id\Cov(Y)=\mathsf M^{-1/2}A\mathsf M^{-1/2}\preceq \Id. Also M⪰δB−1\mathsf M\succeq\delta B^{-1} implies B⪰δM−1B\succeq\delta \mathsf M^{-1}, so the potential in the new coordinates has Hessian at least M1/2BM1/2⪰δId\mathsf M^{1/2}B\mathsf M^{1/2}\succeq\delta \Id.

Let MqM_q bound the norm of qq centered integrations uniformly over regular laws with these two properties. Set ν=L(Y)\nu=\mathcal L(Y) and pˉ(y)=p(m+M1/2y)\bar p(y)=p(m+\mathsf M^{1/2}y). A degree-dd Appell polynomial can be recovered in these coordinates whenever 1≤q≤d−11\le q\le d-1:

pˉ=J0νJ1ν⋯Jq−1νDyqpˉ.\bar p=J_0^\nu J_1^\nu\cdots J_{q-1}^\nu D_y^q\bar p.

The endpoint q=dq=d is excluded because DdpD^dp is a nonzero constant, whereas JJ requires a centered input. Returning to the original coordinates by the chain rule gives

Eμp2≤Mq2Eμ⟨Dqp,M⊗qDqp⟩.\E_\mu p^2\le M_q^2\E_\mu\langle D^qp,\mathsf M^{\otimes q}D^qp\rangle.

The paper extends this polynomial inequality to nonsmooth posteriors by regular approximation, preserving the covariance and curvature bounds while the required moments converge. This is the step that permits its use for the tilted radial example.

For the moving quartic, two integrations recover it from the centered Hessian displayed above. This illustrates a permitted terminal estimate; the draft's actual induction chooses one derivative at small degrees, including degree four.

Differentiation lowers the polynomial degree. For pt=Pdμt[T]p_t=P_d^{\mu_t}[T], the degree-(d−q)(d-q) coefficient bound gives

Et⟨Dqpt,M⊗qDqpt⟩≤(d!)2Cd−q2⟨T,(M⊗q⊗At⊗(d−q))T⟩.\E_t\langle D^qp_t,\mathsf M^{\otimes q}D^qp_t\rangle \le(d!)^2C_{d-q}^2 \langle T,(\mathsf M^{\otimes q}\otimes A_t^{\otimes(d-q)})T\rangle.

There is no extra factorial cost: differentiation contributes d!/(d−q)!d!/(d-q)!, and the lower-degree norm contributes (d−q)!Cd−q(d-q)!C_{d-q}. Multiplication leaves d!Cd−qd!C_{d-q}. Apply this componentwise to the remaining symmetric polynomial slots and sum the squared component bounds.

At time tt, take B=ΛtB=\Lambda_t, so M=At+δΛt−1\mathsf M=A_t+\delta\Lambda_t^{-1}. The mixed covariance estimate from §6.1 then bounds the path average:

V(t)≤(d!)2Cd−q2Mq2(1+δ/t)qe4d2t∥T∥2.\mathcal V(t)\le(d!)^2C_{d-q}^2M_q^2(1+\delta/t)^q e^{4d^2t}\|T\|^2.

Choose t=η/d2t=\eta/d^2, δ=η2/d2\delta=\eta^2/d^2, with 0<η≤10<\eta\le1. Insert this estimate into Lemma 6.2 and divide by d!∥T∥d!\|T\|. Since δ/t=η\delta/t=\eta and (2d2+d+1)t≤3η(2d^2+d+1)t\le3\eta for d≥2d\ge2, the result is

 cd⋆≤e3η[(1+η)q/2MqCd−q+ηd2Σd]. \boxed{\ c_d^\star\le e^{3\eta}\left[(1+\eta)^{q/2}M_qC_{d-q} +\frac\eta{d^2}\Sigma_d\right].\ }

This is Proposition 7.1. The star means a supremum over all dimensions and all centered log-concave laws with covariance at most Id\Id. The supremum over laws is essential: the posteriors generated by our initially radial law need not be radial. Estimates for the initial radial density alone cannot supply the induction hypotheses.

07 / Paper §8 · Theorem 8.1 · Appendix E

Uniform Coefficient Induction

We now use bounds at smaller degrees to establish the same kind of bound at the next degree. The induction target has a fixed exponential growth rate:

w(d)=(d+1)−4,βd=R∗dw(d)=R∗d(d+1)4.w(d)=(d+1)^{-4},\qquad \beta_d=R_*^d w(d)=\frac{R_*^d}{(d+1)^4}.

The paper takes R∗=108R_*=10^8 and proves cd⋆≤βdc_d^\star\le\beta_d in every degree. Here R∗R_* controls coefficient growth; it is unrelated to the support radius used in approximation. Covariance supplies the base case, c1⋆≤1<R∗/16=β1c_1^\star\le1<R_*/16=\beta_1. The polynomial factor (d+1)−4(d+1)^{-4} supplies the slack that will close the induction.

Up to degree 10710^7, one integration suffices, using the quadratic seed in Corollary 5.3. For larger degrees, use about half the derivatives, q=⌊d/2⌋q=\lfloor d/2\rfloor, and coefficient bounds only through D=⌊d⌋D=\lfloor\sqrt d\rfloor. Lemma 5.1 then allows a scalar integration rate BB slightly below R∗2R_*^2:

B=R∗2e−1/(D+1)<R∗2,Mq=2 R∗qexp⁡ ⁣[−q2(D+1)].\begin{aligned}B&=R_*^2e^{-1/(D+1)}<R_*^2,\\M_q&=\sqrt2\,R_*^q\exp\!\left[-\frac{q}{2(D+1)}\right].\end{aligned}

The smaller rate is possible because squaring the degree-DD coefficient bound produces the factor (D+1)−8(D+1)^{-8}, of order d−4d^{-4}. The curvature threshold costs only a factor of order d−3d^{-3}. This leaves room in the power lemma’s strict hypothesis to choose B<R∗2B<R_*^2. Its prefactor is paid once for the whole chain, so the small gain at each integration accumulates:

exp⁡ ⁣[−q2(D+1)]=exp⁡ ⁣[−(14+o(1))d].\exp\!\left[-\frac{q}{2(D+1)}\right]=\exp\!\left[-\left(\frac14+o(1)\right)\sqrt d\right].

When this bound is inserted into reverse transfer, the powers of R∗R_* cancel. The remaining decay outweighs the localization cost and the bounded ratio of polynomial weights. A convolution estimate for those weights also controls the drift term, which involves only smaller degrees.

Parameter Choices and Induction Estimates

These are the choices in Appendix E; in both rows δ=η2/d2\delta=\eta^2/d^2.

Degree RangeIntegrations and InputsLocalization Parameter
2≤d≤1072\le d\le10^7q=1q=1; quadratic seed (Corollary 5.3)η=d/(100R∗)\eta=d/(100R_*)
d>107d>10^7q=⌊d/2⌋q=\lfloor d/2\rfloor, D=⌊d⌋D=\lfloor\sqrt d\rfloorη=d−1/2/(400R∗)\eta=d^{-1/2}/(400R_*)

The weight convolution has constant Cw=4C_w=4:

∑k=1sw(k)w(s−k)≤4w(s)(s≥1).\sum_{k=1}^s w(k)w(s-k)\le4w(s)\qquad(s\ge1).

Taking the smaller-degree bounds to be Ck=βkC_k=\beta_k gives

Σd≤dR∗d+1∑k=2d−1w(k)w(d−k+1)≤4dR∗d+1w(d+1).\Sigma_d\le dR_*^{d+1}\sum_{k=2}^{d-1}w(k)w(d-k+1)\le4dR_*^{d+1}w(d+1).

Degrees up to the cutoff. Here δ=(100R∗)−2\delta=(100R_*)^{-2}. Corollary 5.3 supplies

M1=(2/δ)1/6=[2(100R∗)2]1/6≤10R∗.M_1=(2/\delta)^{1/6}=\bigl[2(100R_*)^2\bigr]^{1/6}\le10\sqrt{R_*}.

Also βd−1/βd<16/R∗\beta_{d-1}/\beta_d<16/R_* and ηΣd/(d2βd)≤1/25\eta\Sigma_d/(d^2\beta_d)\le1/25. Substituting into reverse transfer gives

cd⋆βd≤e3η[1+η160R∗+125]<149125000<1.\frac{c_d^\star}{\beta_d}\le e^{3\eta}\left[\sqrt{1+\eta}\frac{160}{\sqrt{R_*}}+\frac1{25}\right]<\frac{1491}{25000}<1.

Degrees above the cutoff. Here δ=d−3/(400R∗)2\delta=d^{-3}/(400R_*)^2. Put γj=R∗j/(j+1)4\gamma_j=R_*^j/(j+1)^4 and apply Lemma 5.1 directly with B=R∗2e−1/(D+1)B=R_*^2e^{-1/(D+1)}. Its strict condition is

δBD+1=R∗2De 4002d3>R∗2D(D+1)8=γD2.\delta B^{D+1}=\frac{R_*^{2D}}{e\,400^2d^3}>\frac{R_*^{2D}}{(D+1)^8}=\gamma_D^2.

Indeed, D+1>dD+1>\sqrt d and d>107>e 4002d>10^7>e\,400^2. The common prefactor satisfies

QD(B)=1+∑j=1D−2j e(j+1)/(D+1)(j+2)8≤1+e384<2.\begin{aligned}Q_D(B)&=1+\sum_{j=1}^{D-2}\frac{j\,e^{(j+1)/(D+1)}}{(j+2)^8}\\&\le1+\frac{e}{384}<2.\end{aligned}

With the resulting MqM_q, the principal term in reverse transfer, divided by βd\beta_d, is at most

32exp⁡ ⁣{3η+q[η2−12(D+1)]}≤32exp⁡ ⁣(3100−d24)<14.\begin{aligned}32\exp\!\left\{3\eta+q\left[\frac\eta2-\frac1{2(D+1)}\right]\right\}&\le32\exp\!\left(\frac3{100}-\frac{\sqrt d}{24}\right)\\&<\frac14.\end{aligned}

The normalized drift term is at most e3η/(100d3/2)<1/50e^{3\eta}/(100d^{3/2})<1/50. The two terms sum to less than one, giving the induction step.

Theorem 8.1 is the result of this induction: coefficients at every degree share one fixed exponential growth bound. Localization has supplied curvature temporarily, while keeping the transfer error in degrees already controlled. The final step uses the availability of all degrees to remove the curvature dependence.

08 / Paper §8.2–9 · Appendix G

Curvature Removal and the Poincaré Bound

Fix a regular centered law with covariance at most Id\Id and lower curvature a>0a>0. Theorem 8.1 gives the hypotheses of Corollary 5.2 at every cutoff DD, with ρ=R∗\rho=R_*. For one integration,

Ccen(ν)=∥J∥2≤2R∗2max⁡{1,a−1/(D+1)}.C_{\mathrm{cen}}(\nu)=\|\mathsf J\|^2 \le2R_*^2\max\{1,a^{-1/(D+1)}\}.

Here we write Ccen(ν)=∥J∥2C_{\mathrm{cen}}(\nu)=\|\mathsf J\|^2 as shorthand for the squared norm of centered integration across all tensor ranks. In particular, it controls the recovery of a scalar function whose gradient has mean zero. Let D→∞D\to\infty while holding the law fixed. The curvature factor tends to one, giving Ccen(ν)≤2R∗2C_{\mathrm{cen}}(\nu)\le2R_*^2. This is a limit in polynomial degree.

It remains to restore the linear part of a function. For centered hh, set b=E∇hb=\E\nabla h, f=h−b⋅xf=h-b\cdot x. Then Ef=0\E f=0, E∇f=0\E\nabla f=0, and

E∣∇h∣2=E∣∇f∣2+∣b∣2,∥b⋅x∥2≤∣b∣.\E|\nabla h|^2=\E|\nabla f|^2+|b|^2,\qquad \|b\cdot x\|_2\le|b|.

Apply the triangle inequality, then Cauchy–Schwarz to the two terms:

∥h∥2≤Ccen ∥∇f∥2+∣b∣≤Ccen+1 ∥∇f∥22+∣b∣2=Ccen+1 ∥∇h∥2.\begin{aligned} \|h\|_2 &\le\sqrt{C_{\mathrm{cen}}}\,\|\nabla f\|_2+|b|\\ &\le\sqrt{C_{\mathrm{cen}}+1}\, \sqrt{\|\nabla f\|_2^2+|b|^2} =\sqrt{C_{\mathrm{cen}}+1}\,\|\nabla h\|_2. \end{aligned}

For our radial example, the smooth law with potential VεV_\varepsilon has covariance σε2Id\sigma_\varepsilon^2\Id, where σε2→1\sigma_\varepsilon^2\to1. Divide its random vector by σε\sigma_\varepsilon to make it isotropic. Its lower curvature becomes aε=εσε2>0a_\varepsilon=\varepsilon\sigma_\varepsilon^2>0. Apply the preceding bound, first let D→∞D\to\infty, and only then let ε↓0\varepsilon\downarrow0.

Stability Under Regular Approximation

The unnormalized densities satisfy e−Vε(x)≤e−3∣x∣e^{-V_\varepsilon(x)}\le e^{-\sqrt3|x|} and converge pointwise to it. The majorant and all of its polynomial multiples are integrable. Dominated convergence therefore gives convergence of normalization, covariance and every fixed moment. For smooth compactly supported ff, the variance and gradient integral under the covariance-normalized laws converge to their counterparts under μ\mu. Passing to the limit preserves the same constant. The approximation argument of §9 and Appendix F then extends the inequality to locally Lipschitz functions with finite gradient energy, as in Theorem 1.1.

Resulting Poincaré Bound

Explicit Poincaré Bound for the Radial Family

 Var⁡μf≤(1+2⋅1016) ∫R2∣∇f∣2 dμ. \boxed{\ \Var_\mu f\le (1+2\cdot10^{16})\, \int_{\mathbb R^2}|\nabla f|^2\,d\mu.\ }

This is the paper’s Appendix G value, KP=1+2R∗2K_{\mathrm{P}}=1+2R_*^2, applied to our example. The paper seeks a bound uniform across laws and dimensions; it does not optimize this constant.

For the full radial family, scaling Xλ=(3/λ)XX_\lambda=(\sqrt3/\lambda)X gives

Var⁡μλf≤3λ2(1+2⋅1016)∫∣∇f∣2 dμλ.\Var_{\mu_\lambda}f\le \frac3{\lambda^2}(1+2\cdot10^{16})\int|\nabla f|^2\,d\mu_\lambda.

The worked example exposes each role: compatibility allows integration; the Hodge estimate controls the cost of enforcing it; Appell polynomials record constant-input chains; the power lemma controls arbitrary chains; localization adds curvature; the moving coefficients preserve centering; reverse transfer closes the degree induction. Only after all degrees are available can the curvature dependence disappear.

Sharp Constant and Purpose of the Example

For this particular isotropic radial law, the optimal Poincaré constant is exactly

 CP(μ)=32,Var⁡μf≤32∫R2∣∇f∣2 dμ. \boxed{\ C_P(\mu)=\frac32,\qquad \Var_\mu f\le\frac32\int_{\mathbb R^2}|\nabla f|^2\,d\mu.\ }

More generally, CP(μλ)=9/(2λ2)C_P(\mu_\lambda)=9/(2\lambda^2). This exact value comes from separating radial and angular modes, as detailed below. In the isotropic case, equality is attained by f(x,y)=xexp⁡(x2+y2/3)f(x,y)=x\exp(\sqrt{x^2+y^2}/\sqrt3).

Why the Sharp Constant Is 3/2

The reciprocal of the Poincaré constant is the smallest nonzero spectral value of the weighted Laplacian. For an angular Fourier mode m∈Zm\in\mathbb Z, its radial part acts in the space with weight wλ(r)=re−λrw_\lambda(r)=r e^{-\lambda r} as

Hmh=−h′′−(1r−λ)h′+m2r2h.H_m h=-h''-\left(\frac1r-\lambda\right)h'+\frac{m^2}{r^2}h.

The positive radial function h1(r)=reλr/3h_1(r)=r e^{\lambda r/3} satisfies H1h1=(2λ2/9)h1H_1h_1=(2\lambda^2/9)h_1. Integration by parts gives the ground-state identity

∫0∞ ⁣(∣h′∣2+∣h∣2r2−2λ29∣h∣2)wλ dr=∫0∞h12∣(hh1)′∣2wλ dr≥0.\int_0^\infty\!\left(|h'|^2+\frac{|h|^2}{r^2}-\frac{2\lambda^2}{9}|h|^2\right)w_\lambda\,dr=\int_0^\infty h_1^2\left|\left(\frac h{h_1}\right)'\right|^2w_\lambda\,dr\ge0.

This proves the same lower bound for every mode with ∣m∣≥1|m|\ge1, since their angular term is larger. For the radial mode, let A=d/drA=d/dr with weighted adjoint A∗=−d/dr−1/r+λA^*=-d/dr-1/r+\lambda. Then H0=A∗AH_0=A^*A and H1=AA∗H_1=AA^* have the same nonzero spectrum. These identities use the closed energy operators; the integration-by-parts identity first holds away from the origin and extends by approximation. Thus every nonconstant mode has spectral value at least 2λ2/92\lambda^2/9.

The function h1(r)cos⁡θ=xeλr/3h_1(r)\cos\theta=x e^{\lambda r/3} is centered, has finite variance and gradient energy, and attains this value. Consequently CP(μλ)=9/(2λ2)C_P(\mu_\lambda)=9/(2\lambda^2), which becomes 3/23/2 when λ=3\lambda=\sqrt3.

The purpose of this worked example is to illustrate the proof ideas and how the steps of the paper fit together. The general argument above provides a universal bound; the sharp constant 3/23/2 uses additional structure specific to this radial family.