The static quadratic-chaos input and the two-tail obstruction
The time-zero version of two-color covariance control is already a strong statement. The intrinsic estimate used here is Theorem 25.1 , from Letwin’s July 2026 version-1 preprint Letwin, 2026 . Its application to a localized posterior separates intrinsic quadratic control from the covariance-alignment problem created by unwhitening. The quantified two-tail configuration at the end of the chapter is the static obstruction that both branches of the fixed-cut approach must respect: it fixes the covariance weight of the near-Cheeger variant and marks the boundary of what slice-wise verification can establish for the all-cut variant.
Let X ∼ ν X\sim\nu X ∼ ν be isotropic and log-concave, and put
Z = X X T − I . Z=XX^T-I. Z = X X T − I . For a color
g = 1 E − p p q , p = ν ( E ) , q = 1 − p , g=\frac{\one_E-p}{\sqrt{pq}},
\qquad p=\nu(E),\quad q=1-p, g = pq 1 E − p , p = ν ( E ) , q = 1 − p , one computes
E [ g Z ] = p q ( Σ E − Σ F + ( q − p ) δ δ T ) . \E[gZ]=\sqrt{pq}\left(\Sigma_E-\Sigma_F+(q-p)\delta\delta^T\right). E [ g Z ] = pq ( Σ E − Σ F + ( q − p ) δ δ T ) . At exact balance, p = q = 1 / 2 p=q=1/2 p = q = 1/2 , this is 1 2 ( Σ E − Σ F ) \frac12(\Sigma_E-\Sigma_F) 2 1 ( Σ E − Σ F ) .
For isotropic log-concave ν \nu ν , define
Q ( ν ) = sup ∥ M ∥ H S = 1 Var ν ( X T M X ) . \calQ(\nu)=\sup_{\norm M_{\HS}=1}\Var_\nu(X^TMX). Q ( ν ) = ∥ M ∥ HS = 1 sup Var ν ( X T MX ) . The quadratic-chaos thin-shell assertion is
Q ( ν ) ≤ C \calQ(\nu)\le C Q ( ν ) ≤ C with a universal constant C C C .
If X X X is isotropic and log-concave on R n \R^n R n , then for every symmetric matrix M M M ,
Var ( X T M X ) ≤ 2 E ∣ ∇ ( X T M X ) ∣ 2 = 8 ∥ M ∥ H S 2 . \Var(X^TMX)
\ \le\ 2\,\E\abs{\nabla(X^TMX)}^2
\ =\ 8\norm M_{\HS}^2. Var ( X T MX ) ≤ 2 E ∣ ∣ ∇ ( X T MX ) ∣ ∣ 2 = 8 ∥ M ∥ HS 2 . Consequently Q ( ν ) ≤ 8 \calQ(\nu)\le8 Q ( ν ) ≤ 8 in Definition 25.1 .
Theorem 25.1 is Theorem 1.2 of Letwin’s preprint Letwin, 2026 (arXiv:2607.24164v1); its status records the check made here. The proof uses the moment measure of ν \nu ν , its positive symmetric Stein kernel, congruence, and an H − 1 H^{-1} H − 1 inequality (Section The noncommutativity trick ). The deductions below use this quadratic statement, not Theorem 1.1 of the preprint on general KLS.
Let ν \nu ν be centered and log-concave with positive-definite covariance A A A , let E E E have mass p ∈ ( 0 , 1 ) p\in(0,1) p ∈ ( 0 , 1 ) , put s = p ( 1 − p ) s=p(1-p) s = p ( 1 − p ) , and let K K K be the translation-invariant two-color contrast from Proposition 32.1 . Then
s ∥ A − 1 / 2 K A − 1 / 2 ∥ H S 2 ≤ 8 , s ∥ K ∥ H S 2 ≤ 8 λ max ( A ) 2 . s\norm{A^{-1/2}KA^{-1/2}}_{\HS}^2\le8,
\qquad
s\norm K_{\HS}^2\le8\lmax(A)^2. s ∥ ∥ A − 1/2 K A − 1/2 ∥ ∥ HS 2 ≤ 8 , s ∥ K ∥ HS 2 ≤ 8 λ m a x ( A ) 2 . If in addition p ∈ [ 1 / 3 , 2 / 3 ] p\in[1/3,2/3] p ∈ [ 1/3 , 2/3 ] , then
s ∥ G ∥ H S 2 ≤ 17 λ max ( A ) 2 . s\norm G_{\HS}^2\le17\lmax(A)^2. s ∥ G ∥ HS 2 ≤ 17 λ m a x ( A ) 2 . At exact balance, where K = G K=G K = G , the constant in the last display is 8.
Whiten Y = A − 1 / 2 X Y=A^{-1/2}X Y = A − 1/2 X . For any symmetric N N N , Proposition 32.1 and Cauchy–Schwarz give
s ⟨ A − 1 / 2 K A − 1 / 2 , N ⟩ 2 ≤ Var ( Y T N Y ) ≤ 8 ∥ N ∥ H S 2 , s\inner{A^{-1/2}KA^{-1/2}}{N}^2
\le \Var\bigl(Y^TNY\bigr)
\le 8\norm N_{\HS}^2, s ⟨ A − 1/2 K A − 1/2 , N ⟩ 2 ≤ Var ( Y T N Y ) ≤ 8 ∥ N ∥ HS 2 , where the last step is Theorem 25.1 . Taking the supremum over ∥ N ∥ H S ≤ 1 \norm N_{\HS}\le1 ∥ N ∥ HS ≤ 1 proves the first estimate in (25.7) . Since K = A 1 / 2 ( A − 1 / 2 K A − 1 / 2 ) A 1 / 2 K=A^{1/2}(A^{-1/2}KA^{-1/2})A^{1/2} K = A 1/2 ( A − 1/2 K A − 1/2 ) A 1/2 , the ideal property of the Hilbert–Schmidt norm gives the second estimate. Finally G = K − ( q − p ) δ δ T G=K-(q-p)\delta\delta^T G = K − ( q − p ) δ δ T , so on the coarse balanced window, using s ≥ 2 / 9 s\ge2/9 s ≥ 2/9 , ∣ q − p ∣ ≤ 1 / 3 \abs{q-p}\le1/3 ∣ q − p ∣ ≤ 1/3 , and r = s ∣ δ ∣ 2 ≤ λ max ( A ) r=s\abs{\delta}^2\le\lmax(A) r = s ∣ δ ∣ 2 ≤ λ m a x ( A ) from B ⪯ A B\preceq A B ⪯ A ,
s ∥ G ∥ H S 2 ≤ 2 s ∥ K ∥ H S 2 + 2 s ( q − p ) 2 ∣ δ ∣ 4 ≤ 16 λ max ( A ) 2 + 2 ( q − p ) 2 s r 2 ≤ 17 λ max ( A ) 2 . s\norm G_{\HS}^2
\le2s\norm K_{\HS}^2+2s(q-p)^2\abs{\delta}^4
\le16\lmax(A)^2+\frac{2(q-p)^2}{s}r^2
\le17\lmax(A)^2. s ∥ G ∥ HS 2 ≤ 2 s ∥ K ∥ HS 2 + 2 s ( q − p ) 2 ∣ δ ∣ 4 ≤ 16 λ m a x ( A ) 2 + s 2 ( q − p ) 2 r 2 ≤ 17 λ m a x ( A ) 2 . At balance the correction term vanishes.
Up to universal constants, (25.5) is equivalent to the balanced two-color estimate
p q ∥ Σ E − Σ F ∥ H S 2 ≤ C pq\norm{\Sigma_E-\Sigma_F}_{\HS}^2\le C pq ∥ Σ E − Σ F ∥ HS 2 ≤ C for all balanced cuts E E E .
Assume (25.5) . For ∥ M ∥ H S = 1 \norm M_{\HS}=1 ∥ M ∥ HS = 1 ,
⟨ E [ g Z ] , M ⟩ = E [ g ( X T M X − Tr M ) ] ≤ Var ( X T M X ) ≤ C . \inner{\E[gZ]}{M}
=\E\left[g\left(X^TMX-\Tr M\right)\right]
\le \sqrt{\Var(X^TMX)}\le\sqrt C . ⟨ E [ g Z ] , M ⟩ = E [ g ( X T MX − Tr M ) ] ≤ Var ( X T MX ) ≤ C . Taking the supremum over M M M and using (25.3) gives the two-color bound at balance; the slightly unbalanced case is handled by the explicit ( q − p ) δ δ T (q-p)\delta\delta^T ( q − p ) δ δ T term and B ⪯ A B\preceq A B ⪯ A .
Conversely, fix M M M with ∥ M ∥ H S = 1 \norm M_{\HS}=1 ∥ M ∥ HS = 1 and set Y = X T M X − Tr M Y=X^TMX-\Tr M Y = X T MX − Tr M . Since ν \nu ν is isotropic, its convex support has nonempty interior and ν \nu ν is absolutely continuous there. The polynomial x ↦ x T M x x\mapsto x^TMx x ↦ x T M x is nonconstant, because M ≠ 0 M\ne0 M = 0 , and each of its level sets has Lebesgue measure zero. Thus the law of Y Y Y is atomless, and there is a median m m m for which the deterministic cut E = { Y ≥ m } E=\{Y\ge m\} E = { Y ≥ m } has mass exactly 1 / 2 1/2 1/2 .
For this cut, g = 2 1 E − 1 = sgn ( Y − m ) g=2\one_E-1=\operatorname{sgn}(Y-m) g = 2 1 E − 1 = sgn ( Y − m ) almost surely and E g = 0 \E g=0 E g = 0 , so
E [ g Y ] = E [ g ( Y − m ) ] = E ∣ Y − m ∣ . \E[gY]=\E[g(Y-m)]=\E\abs{Y-m}. E [ g Y ] = E [ g ( Y − m )] = E ∣ Y − m ∣ . The balanced two-color estimate and (25.3) give ∥ E [ g Z ] ∥ H S ≤ C \norm{\E[gZ]}_{\HS}\le\sqrt C ∥ E [ g Z ] ∥ HS ≤ C , hence E ∣ Y − m ∣ = ⟨ E [ g Z ] , M ⟩ ≤ C \E\abs{Y-m}=\inner{\E[gZ]}M\le\sqrt C E ∣ Y − m ∣ = ⟨ E [ g Z ] , M ⟩ ≤ C . The Carbery–Wright reverse moment inequality for polynomials of degree at most two Carbery & Wright, 2001 now gives
Var ( Y ) ≤ ∥ Y − m ∥ L 2 ≲ ∥ Y − m ∥ L 1 ≲ C . \sqrt{\Var(Y)}
\le\norm{Y-m}_{L^2}
\lesssim\norm{Y-m}_{L^1}
\lesssim\sqrt C. Var ( Y ) ≤ ∥ Y − m ∥ L 2 ≲ ∥ Y − m ∥ L 1 ≲ C . Taking the supremum over symmetric M M M with ∥ M ∥ H S = 1 \norm M_{\HS}=1 ∥ M ∥ HS = 1 proves Var ( X T M X ) ≲ C ∥ M ∥ H S 2 \Var(X^TMX)\lesssim C\norm M_{\HS}^2 Var ( X T MX ) ≲ C ∥ M ∥ HS 2 .
Why ordinary thin shell did not suffice ¶ The thin-shell theorem controls the radial quadratic form:
Var ( ∣ X ∣ 2 ) ≤ C n , \Var(\abs X^2)\le Cn, Var ( ∣ X ∣ 2 ) ≤ C n , which is (25.5) only for M = I / n M=I/\sqrt n M = I / n . Applying thin shell to every projection P P P gives
Var ( X T P X ) ≤ C rank ( P ) . \Var(X^TPX)\le C\operatorname{rank}(P). Var ( X T PX ) ≤ C rank ( P ) . For a positive semidefinite matrix M = ∫ 0 ∞ P s d s M=\int_0^\infty P_s\dd s M = ∫ 0 ∞ P s d s , where P s = 1 { M ≥ s } P_s=\one_{\{M\ge s\}} P s = 1 { M ≥ s } , Minkowski yields
∥ X T M X − Tr M ∥ L 2 ≤ C ∫ 0 ∞ rank ( P s ) d s . \norm{X^TMX-\Tr M}_{L^2}
\le C\int_0^\infty\sqrt{\operatorname{rank}(P_s)}\dd s. ∥ ∥ X T MX − Tr M ∥ ∥ L 2 ≤ C ∫ 0 ∞ rank ( P s ) d s . The right-hand side is the Lorentz ℓ 2 , 1 \ell_{2,1} ℓ 2 , 1 norm of the eigenvalue sequence of M M M , bounded by C log n ∥ M ∥ H S C\sqrt{\log n}\norm M_{\HS} C log n ∥ M ∥ HS . Thus projection thin-shell estimates by themselves give only
Var ( X T M X ) ≲ log n ∥ M ∥ H S 2 , \Var(X^TMX)\lesssim \log n\,\norm M_{\HS}^2, Var ( X T MX ) ≲ log n ∥ M ∥ HS 2 , a factor log n \log n log n away from the dimension-free conclusion of Theorem 25.1 .
Projection tests cannot remove the logarithm ¶ The logarithm is not merely an artifact of the integration. There is an abstract positive operator T T T on symmetric matrices such that
⟨ P , T P ⟩ ≤ C rank ( P ) \inner{P}{TP}\le C\operatorname{rank}(P) ⟨ P , TP ⟩ ≤ C rank ( P ) for every orthogonal projection P P P , while ∥ T ∥ o p ≃ log n \norm T_{\op}\simeq\log n ∥ T ∥ op ≃ log n .
Let
H n = ∑ i = 1 n 1 i , N = diag ( 1 H n , 1 2 H n , … , 1 n H n ) , H_n=\sum_{i=1}^n\frac1i,
\qquad
N=\diag\left(\frac1{\sqrt{H_n}},\frac1{\sqrt{2H_n}},\ldots,\frac1{\sqrt{nH_n}}\right), H n = i = 1 ∑ n i 1 , N = diag ( H n 1 , 2 H n 1 , … , n H n 1 ) , so that ∥ N ∥ H S = 1 \norm N_{\HS}=1 ∥ N ∥ HS = 1 , and define
T ( M ) = H n ⟨ M , N ⟩ N . T(M)=H_n\inner{M}{N}N. T ( M ) = H n ⟨ M , N ⟩ N . Ky Fan’s principle gives, for every rank-r r r projection P P P ,
⟨ P , N ⟩ ≤ ∑ i = 1 r 1 i H n ≤ 2 r H n . \inner{P}{N}\le\sum_{i=1}^r\frac1{\sqrt{iH_n}}\le2\sqrt{\frac r{H_n}}. ⟨ P , N ⟩ ≤ i = 1 ∑ r i H n 1 ≤ 2 H n r . Therefore ⟨ P , T P ⟩ ≤ 4 r \inner{P}{TP}\le4r ⟨ P , TP ⟩ ≤ 4 r , whereas ∥ T ∥ o p = H n ≃ log n \norm T_{\op}=H_n\simeq\log n ∥ T ∥ op = H n ≃ log n . This is not a log-concave counterexample. It shows that projection tests alone cannot imply quadratic-chaos thin shell; Letwin’s proof escapes the obstruction by using moment measures and a matrix Stein kernel rather than only projection data.
Static lesson ¶ A fixed-cut argument cannot rely only on radial information or on projection tests. Theorem 25.1 supplies the full intrinsic quadratic-chaos estimate, but Corollary 25.1 shows exactly what whitening loses: the Euclidean Riccati source may still be amplified by λ max ( A t ) 2 \lmax(A_t)^2 λ m a x ( A t ) 2 . The remaining task is therefore dynamic or geometric control of the alignment with A t A_t A t , attached to the fixed cut E E E .
The quantified two-tail obstruction and the weight calibration ¶ The following sharpens the qualitative two-tail warning above by tracking the excess of the configuration, not only its covariance contrast. It is the static obstruction used in covariance-weighted form by the near-Cheeger variant (Chapter The fixed cut: the near-Cheeger variant ) and the configuration whose dynamical occupation the all-cut variant must control (Chapter The fixed cut: the mass martingale and the Carleson estimate ).
Let Λ ≥ 1 \Lambda\ge1 Λ ≥ 1 , ν Λ = N ( 0 , diag ( Λ , 1 , … , 1 ) ) \nu_\Lambda=N(0,\diag(\Lambda,1,\dots,1)) ν Λ = N ( 0 , diag ( Λ , 1 , … , 1 )) on R n \R^n R n , and
E Λ = { x : ∣ x 1 ∣ ≥ a Λ } , a = Φ − 1 ( 3 / 4 ) ≈ 0.6745 , E_\Lambda=\bigl\{x:\abs{x_1}\ge a\sqrt\Lambda\bigr\},
\qquad a=\Phi^{-1}(3/4)\approx0.6745, E Λ = { x : ∣ x 1 ∣ ≥ a Λ } , a = Φ − 1 ( 3/4 ) ≈ 0.6745 , so that ν Λ ( E Λ ) = 1 2 \nu_\Lambda(E_\Lambda)=\tfrac12 ν Λ ( E Λ ) = 2 1 . Write φ \varphi φ for the standard Gaussian density. Then:
(i) δ = 0 \delta=0 δ = 0 , hence r = D = 0 r=D=0 r = D = 0 and K = G K=G K = G ;
(ii) G = 8 a φ ( a ) Λ e 1 e 1 T G=8a\varphi(a)\,\Lambda\,e_1e_1^T G = 8 a φ ( a ) Λ e 1 e 1 T , hence S ν Λ ( E Λ ) / s = 16 a 2 φ ( a ) 2 Λ 2 ≈ 0.735 Λ 2 \calS_{\nu_\Lambda}(E_\Lambda)/s=16a^2\varphi(a)^2\Lambda^2\approx0.735\,\Lambda^2 S ν Λ ( E Λ ) / s = 16 a 2 φ ( a ) 2 Λ 2 ≈ 0.735 Λ 2 ;
(iii) ν Λ + ( E Λ ) = 2 φ ( a ) Λ − 1 / 2 \nu_\Lambda^+(E_\Lambda)=2\varphi(a)\Lambda^{-1/2} ν Λ + ( E Λ ) = 2 φ ( a ) Λ − 1/2 and, exactly,
e 0 ( E Λ ) = ( 2 φ ( a ) − φ ( 0 ) ) Λ − 1 / 2 ≈ 0.237 Λ − 1 / 2 → 0 ; e_0(E_\Lambda)=\bigl(2\varphi(a)-\varphi(0)\bigr)\Lambda^{-1/2}
\approx0.237\,\Lambda^{-1/2}\to0; e 0 ( E Λ ) = ( 2 φ ( a ) − φ ( 0 ) ) Λ − 1/2 ≈ 0.237 Λ − 1/2 → 0 ; (iv) the relative excess is constant uniformly in Λ \Lambda Λ and n n n :
e 0 ( E Λ ) I ν Λ ( 1 / 2 ) = 2 φ ( a ) φ ( 0 ) − 1 ≈ 0.593. \frac{e_0(E_\Lambda)}{I_{\nu_\Lambda}(1/2)}\ =\ \frac{2\varphi(a)}{\varphi(0)}-1
\ \approx\ 0.593 . I ν Λ ( 1/2 ) e 0 ( E Λ ) = φ ( 0 ) 2 φ ( a ) − 1 ≈ 0.593. Consequently, no inequality of the slice-wise form S ν ( E ) / s ≤ C 0 + C 1 r + β D + C 2 e ( E ) \calS_\nu(E)/s\le C_0+C_1r+\beta D+C_2\,e(E) S ν ( E ) / s ≤ C 0 + C 1 r + β D + C 2 e ( E ) , with constants independent of the measure, can hold for all log-concave ν \nu ν and all sets of mass 1 2 \tfrac12 2 1 .
(i) is symmetry. (ii): conditioning on { ∣ Z ∣ ≥ a } \{\abs Z\ge a\} { ∣ Z ∣ ≥ a } for Z = X 1 / Λ ∼ N ( 0 , 1 ) Z=X_1/\sqrt\Lambda\sim N(0,1) Z = X 1 / Λ ∼ N ( 0 , 1 ) affects only the first coordinate, and the Gaussian integrations ∫ a ∞ z 2 φ = a φ ( a ) + 1 − Φ ( a ) \int_a^\infty z^2\varphi=a\varphi(a)+1-\Phi(a) ∫ a ∞ z 2 φ = a φ ( a ) + 1 − Φ ( a ) , 1 − Φ ( a ) = 1 4 1-\Phi(a)=\tfrac14 1 − Φ ( a ) = 4 1 , give E [ Z 2 ∣ ∣ Z ∣ ≥ a ] = 1 + 4 a φ ( a ) \E[Z^2\mid\abs Z\ge a]=1+4a\varphi(a) E [ Z 2 ∣ ∣ Z ∣ ≥ a ] = 1 + 4 a φ ( a ) and E [ Z 2 ∣ ∣ Z ∣ < a ] = 1 − 4 a φ ( a ) \E[Z^2\mid\abs Z<a]=1-4a\varphi(a) E [ Z 2 ∣ ∣ Z ∣ < a ] = 1 − 4 a φ ( a ) , hence G 11 = 8 a φ ( a ) Λ G_{11}=8a\varphi(a)\Lambda G 11 = 8 a φ ( a ) Λ with all other entries zero; then S / s = s ∥ G ∥ H S 2 = 1 4 ⋅ 64 a 2 φ ( a ) 2 Λ 2 \calS/s=s\norm G_\HS^2=\tfrac14\cdot64a^2\varphi(a)^2\Lambda^2 S / s = s ∥ G ∥ HS 2 = 4 1 ⋅ 64 a 2 φ ( a ) 2 Λ 2 . (iii): the boundary consists of the two hyperplanes { x 1 = ± a Λ } \{x_1=\pm a\sqrt\Lambda\} { x 1 = ± a Λ } , each of boundary density φ ( a ) Λ − 1 / 2 \varphi(a)\Lambda^{-1/2} φ ( a ) Λ − 1/2 . To compute the excess, write ν Λ = T # γ n \nu_\Lambda=T_\#\gamma_n ν Λ = T # γ n with ∥ T ∥ o p = Λ \norm T_\op=\sqrt\Lambda ∥ T ∥ op = Λ . Gaussian isoperimetry and whitening give I ν Λ ( 1 / 2 ) ≥ φ ( 0 ) Λ − 1 / 2 I_{\nu_\Lambda}(1/2)\ge\varphi(0)\Lambda^{-1/2} I ν Λ ( 1/2 ) ≥ φ ( 0 ) Λ − 1/2 , while the long-axis halfspace { x 1 ≤ 0 } \{x_1\le0\} { x 1 ≤ 0 } attains the reverse inequality. Thus I ν Λ ( 1 / 2 ) = φ ( 0 ) Λ − 1 / 2 I_{\nu_\Lambda}(1/2)=\varphi(0)\Lambda^{-1/2} I ν Λ ( 1/2 ) = φ ( 0 ) Λ − 1/2 , proving (iii) and (iv). The final claim follows by letting Λ → ∞ \Lambda\to\infty Λ → ∞ : the left side grows like Λ 2 \Lambda^2 Λ 2 , the right side is C 0 + C 2 O ( Λ − 1 / 2 ) C_0+C_2O(\Lambda^{-1/2}) C 0 + C 2 O ( Λ − 1/2 ) .
Three consequences.
(a) No slice-wise proof. At t = 0 t=0 t = 0 the initial measure is isotropic and the configuration of Proposition 25.2 cannot occur; but anisotropic posteriors μ t \mu_t μ t with λ max ( A t ) = Λ ≫ 1 \lmax(A_t)=\Lambda\gg1 λ m a x ( A t ) = Λ ≫ 1 are exactly the states the dynamics may visit, and there the slice-wise inequality fails. Any proof of the Stein-trace estimate must therefore show that such configurations carry negligible expected occupation — a covariance-occupation statement of the same nature as the Carleson problem itself. Thus the same stress configuration constrains both the excess-propagation and operator-to-trace proposals; no equivalence between them is asserted.
(b) The weight ( 1 + ∥ A ∥ o p ) 5 / 2 (1+\norm A_\op)^{5/2} ( 1 + ∥ A ∥ op ) 5/2 is calibrated, not chosen. Matching powers of Λ \Lambda Λ (S / s ≍ Λ 2 \calS/s\asymp\Lambda^2 S / s ≍ Λ 2 against e ≍ Λ − 1 / 2 e\asymp\Lambda^{-1/2} e ≍ Λ − 1/2 ) identifies ( 1 + ∥ A ∥ o p ) 5 / 2 (1+\norm{A}_\op)^{5/2} ( 1 + ∥ A ∥ op ) 5/2 as the minimal pure power of λ max ( A ) \lmax(A) λ m a x ( A ) multiplying absolute excess that is statically consistent with this slice inequality: indeed e 0 Λ 5 / 2 = ( 2 φ ( a ) − φ ( 0 ) ) Λ 2 e_0\Lambda^{5/2}=(2\varphi(a)-\varphi(0))\Lambda^2 e 0 Λ 5/2 = ( 2 φ ( a ) − φ ( 0 )) Λ 2 , and the ratio of the leading S / s \calS/s S / s coefficient to this coefficient is approximately 3.11. The uniform value in (iv) of the relative excess is consistent evidence: two-tail sets are never relatively near-minimal in the Gaussian model, so a stability theory normalized at the Cheeger scale of the posterior is not contradicted by the example.
(c) What a T 1 + γ T^{1+\gamma} T 1 + γ rate would require. By the Brascamp–Lieb cap (23.10) the weight is at most ( 1 + t − 1 ) 5 / 2 (1+t^{-1})^{5/2} ( 1 + t − 1 ) 5/2 pathwise. If that cap were saturated deterministically, the pointwise condition E e t ≲ t 5 / 2 + γ \E e_t\lesssim t^{5/2+\gamma} E e t ≲ t 5/2 + γ would be sufficient to produce a T 1 + γ T^{1+\gamma} T 1 + γ integral; the formerly suggested t 3 / 2 t^{3/2} t 3/2 rate would instead leave the nonintegrable factor t − 1 t^{-1} t − 1 . A realistic proof would more likely need a joint rare-event bound coupling excess to large ∥ A t ∥ o p \norm{A_t}_\op ∥ A t ∥ op , rather than separate pointwise estimates. Thus the T 1 + γ T^{1+\gamma} T 1 + γ term in (28.12) is a deliberately strong requirement, not a consequence of the static power matching in part (b).
What this chapter argues against ¶ The two remarks below name the proof shapes the computations of this chapter argue against. Each records what a proof should not try to do, not a theorem; later chapters cite them as heuristic barriers, never as a step in a proof.
The anisotropic Gaussian two-tail cut of Proposition 25.2 rules out a slice-wise stable Stein estimate carrying an absolute-scale excess term. On that cut r = D = 0 r=D=0 r = D = 0 while the Stein source is of order Λ 2 \Lambda^{2} Λ 2 and the excess of order Λ − 1 / 2 \Lambda^{-1/2} Λ − 1/2 , so a slice-wise excess estimate needs covariance weight at least ( 1 + ∥ A ∥ o p ) 5 / 2 (1+\norm{A}_{\op})^{5/2} ( 1 + ∥ A ∥ op ) 5/2 . An unweighted proof must instead control the expected occupation of inflated configurations.
Radial and projection-only information yields at best Var ( X T M X ) ≲ log n ∥ M ∥ H S 2 \Var(X^{T}MX)\lesssim\log n\,\norm{M}_{\HS}^{2} Var ( X T MX ) ≲ log n ∥ M ∥ HS 2 , by (25.18) and the adjacent operator construction. A proof requiring dimension-free quadratic-chaos control must therefore use tensor-aware information beyond projection tests.
Letwin, B. (2026). The KLS Constant is O(\log1/4 n) . Carbery, A., & Wright, J. (2001). Distributional and Lq Norm Inequalities for Polynomials over Convex Bodies in \mathbbRn. Mathematical Research Letters , 8 (3), 233–248. 10.4310/MRL.2001.v8.n3.a1