Introduction
Local maxima provide natural candidates for detecting signals in temporal and spatial data. Applications include neuroimaging, genomics, change point analysis, and environmental signal detection. Selecting a point because it is a local maximum changes its null height distribution: a marginally Gaussian process need not have Gaussian heights at its selected peaks. Conditional peak height distributions therefore provide a building block for inference at local maxima [5 , 6 , 9 , 18 ] .
For smooth Gaussian processes and fields, expected numbers and height distributions of local maxima are studied through Kac–Rice formulas [1 , 2 , 10 , 17 ] . Explicit peak height distributions and their dependence on covariance structure have been developed in [4 , 7 , 8 ] . There is an essential distinction between continuous and discrete parameter spaces. Under the usual nondegeneracy and smoothness conditions, a fixed deterministic point of a continuous process is a local maximum with probability zero. The height distribution of a continuous peak is then defined through local Palm sampling and calculated by Kac–Rice. On a discrete grid, the event that a specified site exceeds its two neighbors has positive probability under the finite-dimensional nondegeneracy conditions, so its height has an ordinary conditional law.
The discrete law is directly relevant when data are recorded at finitely many locations and peaks are identified by comparisons between neighboring observations. A continuous approximation may be accurate for a sufficiently fine grid and a sufficiently smooth process, but its accuracy depends on both the covariance and the mesh. Discrete local maximum methods for bounding excursion probabilities were developed by [20 , 21 ] . In particular, Taylor et al. [20 ] calculate the conditional probability that neighboring observations fall below a given central height and integrate this probability against the Gaussian density. In one dimension, that calculation is equivalent to the stationary joint height and peak probability used here. Lin et al. [13 ] explicitly normalize such probabilities to obtain finite-lattice peak height laws and develop a Monte Carlo method for general stationary neighborhood covariance matrices.
The present paper complements these finite-lattice calculations with nonstationary formulas and rigorous infill limits. We establish convergence to a curvature-weighted density under fourth-order covariance smoothness, give a necessary and sufficient nonstationary criterion for a Gaussian height limit, and classify stationary limits through the fourth spectral moment. Remark 4.2 organizes the resulting height laws in the continuous family { h η S M : 0 ≤ η ≤ 1 } \{h_{\eta}^{\mathrm{SM}}: 0 \le\eta\le1\} { h η SM : 0 ≤ η ≤ 1 } , whose endpoints are Gaussian and Rayleigh. The finite-dimensional Gaussian conditioning calculation is an established ingredient; our principal results concern how discrete peak selection and covariance regularity determine the limiting law and the accuracy of its finite-grid approximation.
Let X = { X ( t ) : t ∈ I } X = \{X(t): t \in I\} X = { X ( t ) : t ∈ I } be a centered, unit-variance, real-valued Gaussian process on an interval I ⊂ R I \subset\mathbb{R} I ⊂ R , with covariance
C ( s , t ) = Cov { X ( s ) , X ( t ) } . C(s,t) = \operatorname{Cov}\{X(s), X(t)\}. C ( s , t ) = Cov { X ( s ) , X ( t )} .
In the stationary case, we write C ( s , t ) = r ( s − t ) C(s,t) = r(s-t) C ( s , t ) = r ( s − t ) . Under stationarity, since the quantities below do not depend on location, we omit their subscript t t t ; for the spectral results, X X X is understood to be defined on R \mathbb{R} R and observed only on I I I .
For a mesh size d > 0 d > 0 d > 0 and a site whose two neighbors lie in I I I , write the event of observing a local maximum at t t t as
A t , d = { X ( t ) > X ( t − d ) , X ( t ) > X ( t + d ) } . \mathcal{A}_{t,d} = \{X(t) > X(t-d),\ X(t) > X(t+d)\}. A t , d = { X ( t ) > X ( t − d ) , X ( t ) > X ( t + d )} .
We study the sitewise peak probability p t , d = P ( A t , d ) p_{t,d} = \mathbb{P}(\mathcal{A}_{t,d}) p t , d = P ( A t , d ) and the conditional peak height density
h t , d ( x ) = d d x P { X ( t ) ≤ x ∣ A t , d } . h_{t,d}(x) = \frac{\mathrm{d}}{\mathrm{d}x}\mathbb{P}\{X(t) \le x \mid\mathcal{A}_{t,d}\}. h t , d ( x ) = d x d P { X ( t ) ≤ x ∣ A t , d } .
The main contributions are as follows.
We express p t , d p_{t,d} p t , d and h t , d h_{t,d} h t , d using a bivariate Gaussian orthant probability and a bivariate Gaussian distribution function. The formulas require only the covariance matrix of { X ( t − d ) , X ( t ) , X ( t + d ) } \{X(t-d), X(t), X(t+d)\} { X ( t − d ) , X ( t ) , X ( t + d )} and no sample path differentiability. Summing the sitewise peak probabilities and integrating the joint height densities gives exact expected counts of all grid peaks and of grid peaks above a threshold.
When C C C has four derivatives near the diagonal, we prove that p t , d / d p_{t,d}/d p t , d / d converges to a curvature-weighted intensity and h t , d h_{t,d} h t , d converges to h η t S M h^{\mathrm{SM}}_{\eta_t} h η t SM , with η t ∈ ( 0 , 1 ] \eta_t \in(0,1] η t ∈ ( 0 , 1 ] ; see Theorem 3.2 . The height law depends on the single parameter η t \eta_t η t , the magnitude of the conditional height-curvature correlation. The endpoint η t = 1 \eta_t = 1 η t = 1 has zero conditional curvature variance and a Rayleigh height law. Under additional sample path and Kac–Rice regularity assumptions, these limits describe the intensity and Palm height distribution of continuous local maxima.
For general nonstationary covariance, let v t , d ± = 1 − C ( t , t ± d ) v^{\pm}_{t,d} = 1 - C(t,t \pm d) v t , d ± = 1 − C ( t , t ± d ) and let q t , d q_{t,d} q t , d be the correlation between X ( t ) − X ( t − d ) X(t) - X(t-d) X ( t ) − X ( t − d ) and X ( t ) − X ( t + d ) X(t) - X(t+d) X ( t ) − X ( t + d ) . We prove that
R t , d = v t , d − + v t , d + 1 + q t , d → 0 R_{t,d} = \frac{v^-_{t,d} + v^+_{t,d}}{1 + q_{t,d}} \to0 R t , d = 1 + q t , d v t , d − + v t , d + → 0
is necessary and sufficient for weak convergence of peak heights to N ( 0 , 1 ) N(0,1) N ( 0 , 1 ) , and is equivalent to pointwise and L 1 L^1 L 1 convergence of their densities. The criterion allows the peak probability to vanish and does not require convergence of q t , d q_{t,d} q t , d . Explicit finite-grid bounds give uniform sitewise approximations and control relative tail errors over a specified threshold range. In the stationary case, R d = 4 { 1 − r ( d ) } 2 / [ 4 { 1 − r ( d ) } − { 1 − r ( 2 d ) } ] R_d = 4\{1-r(d)\}^2/[4\{1-r(d)\} - \{1-r(2d)\}] R d = 4 { 1 − r ( d ) } 2 / [ 4 { 1 − r ( d )} − { 1 − r ( 2 d )}] . The criterion includes nondifferentiable processes and processes with one, but not two, mean-square derivatives.
For each fixed nonconstant, mean-square continuous stationary process with spectral moments m j m_j m j , we give a complete classification. If m 4 < ∞ m_4 < \infty m 4 < ∞ , the limiting density is h η S M h^{\mathrm{SM}}_{\eta} h η SM with η = m 2 / m 4 ∈ ( 0 , 1 ] \eta= m_2/\sqrt{m_4} \in(0,1] η = m 2 / m 4 ∈ ( 0 , 1 ] . If m 4 = ∞ m_4 = \infty m 4 = ∞ , the limit is the Gaussian endpoint h 0 S M = ϕ h^{\mathrm{SM}}_0 = \phi h 0 SM = ϕ , and expected peak counts diverge on every interval of positive length. The Matérn family illustrates this boundary, including its logarithmic cases.
The unification in Remark 4.2 gives a common description of the limiting height laws established in this paper. The smooth density h η S M h^{\mathrm{SM}}_{\eta} h η SM extends continuously to the Gaussian law as η ↓ 0 \eta\downarrow0 η ↓ 0 and to the Rayleigh law as η ↑ 1 \eta\uparrow1 η ↑ 1 , with convergence in total variation at both endpoints. In the smooth regime, η \eta η measures the relation between height and curvature conditional on zero slope; the Gaussian endpoint describes asymptotically height-neutral peak selection. For a fixed stationary process, the spectral classification specifies the member that arises: η = 0 \eta= 0 η = 0 when m 4 = ∞ m_4 = \infty m 4 = ∞ , and η = m 2 / m 4 > 0 \eta= m_2/\sqrt{m_4} > 0 η = m 2 / m 4 > 0 when m 4 < ∞ m_4 < \infty m 4 < ∞ . The interpolation of the family therefore describes variation across covariance models, while the infill theorems identify the limits under their respective assumptions.
The difference between the smooth and rough regimes is fundamental. For a smooth process, the probability that a specified grid point is a local maximum is of order d d d ; summing over approximately d − 1 d^{-1} d − 1 sites produces a finite limiting number of continuous local maxima. The comparison event concentrates near zero slope, with a width proportional to negative curvature, and produces the curvature weighting in h η t S M h^{\mathrm{SM}}_{\eta t} h η t SM which is generally non-Gaussian. For a rough process, grid peaks become increasingly numerous as the grid is refined. Whether t t t is a discrete local maximum is determined by the increments from X ( t ) X(t) X ( t ) to its neighboring grid values. As the grid spacing tends to zero, these increments become asymptotically independent of X ( t ) X(t) X ( t ) , so the local maximum event carries essentially no information about the height at t t t . This explains why the marginal Gaussian density reappears after conditioning.
The rest of the paper is organized as follows. Section 2 derives the exact finite-mesh distributions and expected count formulas. Section 3 proves the smooth infill limit and its stationary specialization. Section 4 gives the nonstationary Gaussian-limit criterion, the unified family interpretation, and the stationary spectral classification. Section 5 treats common covariance models, with stationary and nonstationary examples and numerical comparisons. Section 6 discusses approximation choices and the scope of the inference implications.
Exact Discrete Distributions
Grid peaks and notation
Let I = [ a , b ] I = [a,b] I = [ a , b ] and, for d > 0 d > 0 d > 0 , define
G d = I ∩ ( a + d Z ) , G d ∘ = { t ∈ G d : t − d , t + d ∈ G d } . \mathcal{G}_d = I \cap(a + d\mathbb{Z}), \qquad\mathcal{G}^{\circ}_d = \{t \in\mathcal{G}_d : t-d, t+d \in\mathcal{G}_d\}. G d = I ∩ ( a + d Z ) , G d ∘ = { t ∈ G d : t − d , t + d ∈ G d } .
We restrict attention to grid points whose two neighboring grid points also lie in I I I . Boundary points, which require a separate one-sided definition of a local maximum, are not considered here. Throughout, X X X is centered and Var { X ( t ) } = 1 \operatorname{Var}\{X(t)\} = 1 Var { X ( t )} = 1 . Write ϕ \phi ϕ , Φ \Phi Φ , and Ψ = 1 − Φ \Psi= 1 - \Phi Ψ = 1 − Φ for the standard Gaussian density, distribution function, and survival function. For ρ ∈ [ − 1 , 1 ] \rho\in[-1,1] ρ ∈ [ − 1 , 1 ] , let Φ 2 ( x , y ; ρ ) \Phi_2(x,y;\rho) Φ 2 ( x , y ; ρ ) be the distribution function of a standard bivariate Gaussian vector with correlation ρ \rho ρ . This definition includes the singular cases:
Φ 2 ( x , y ; 1 ) = Φ ( min { x , y } ) , Φ 2 ( x , y ; − 1 ) = [ Φ ( x ) − Φ ( − y ) ] + . (1) \Phi_2(x,y;1) = \Phi(\min\{x,y\}), \qquad\Phi_2(x,y;-1) = [\Phi(x) - \Phi(-y)]_+. \tag*{(1)} Φ 2 ( x , y ; 1 ) = Φ ( min { x , y }) , Φ 2 ( x , y ; − 1 ) = [ Φ ( x ) − Φ ( − y ) ] + . (1)
where z + = max { z , 0 } z_+ = \max\{z,0\} z + = max { z , 0 } .
For t ∈ G d ∘ t \in\mathcal{G}^{\circ}_d t ∈ G d ∘ , define the event of local maximum at t t t and the corresponding probability as
A t , d = { X ( t ) > X ( t − d ) , X ( t ) > X ( t + d ) } , p t , d = P ( A t , d ) . (2) \mathcal{A}_{t,d} = \{X(t) > X(t-d), X(t) > X(t+d)\}, \qquad p_{t,d} = \mathbb{P}(\mathcal{A}_{t,d}). \tag*{(2)} A t , d = { X ( t ) > X ( t − d ) , X ( t ) > X ( t + d )} , p t , d = P ( A t , d ) . (2)
Whenever p t , d > 0 p_{t,d}>0 p t , d > 0 , define respectively the cumulative distribution function and the density function of the height of a local maximum at t t t as
H t , d ( u ) = P { X ( t ) ≤ u ∣ A t , d } , h t , d ( u ) = H t , d ′ ( u ) . H_{t,d}(u)=\mathbb{P}\{X(t)\leq u\mid A_{t,d}\},\qquad h_{t,d}(u)=H'_{t,d}(u). H t , d ( u ) = P { X ( t ) ≤ u ∣ A t , d } , h t , d ( u ) = H t , d ′ ( u ) .
Denote by H ‾ t , d ( u ) = 1 − H t , d ( u ) \overline{H}_{t,d}(u)=1-H_{t,d}(u) H t , d ( u ) = 1 − H t , d ( u ) the tail of peak height distribution.
The exact nonstationary formula
For compact notation, set
c − = C ( t , t − d ) , c + = C ( t , t + d ) , c 0 = C ( t − d , t + d ) . c_{-}=C(t,t-d),\qquad c_{+}=C(t,t+d),\qquad c_{0}=C(t-d,t+d). c − = C ( t , t − d ) , c + = C ( t , t + d ) , c 0 = C ( t − d , t + d ) .
When c ± < 1 c_{\pm}<1 c ± < 1 , the two comparison differences X ( t ) − X ( t − d ) X(t)-X(t-d) X ( t ) − X ( t − d ) and X ( t ) − X ( t + d ) X(t)-X(t+d) X ( t ) − X ( t + d ) have positive variances 2 ( 1 − c ± ) 2(1-c_{\pm}) 2 ( 1 − c ± ) , so ties between the center and either neighbor have probability zero. Their correlation is
q t , d = Corr { X ( t ) − X ( t − d ) , X ( t ) − X ( t + d ) } = 1 − c − − c + + c 0 2 ( 1 − c − ) ( 1 − c + ) . (3) q_{t,d}=\operatorname{Corr}\{X(t)-X(t-d),X(t)-X(t+d)\}=\frac{1-c_{-}-c_{+}+c_{0}}{2\sqrt{(1-c_{-})(1-c_{+})}}. \tag*{(3)} q t , d = Corr { X ( t ) − X ( t − d ) , X ( t ) − X ( t + d )} = 2 ( 1 − c − ) ( 1 − c + ) 1 − c − − c + + c 0 . (3)
For c ± ∈ ( − 1 , 1 ) c_{\pm}\in(-1,1) c ± ∈ ( − 1 , 1 ) , also let
ξ t , d = c 0 − c − c + ( 1 − c − 2 ) ( 1 − c + 2 ) , b t , d − = 1 − c − 1 + c − , b t , d + = 1 − c + 1 + c + . (4) \xi_{t,d}=\frac{c_{0}-c_{-}c_{+}}{\sqrt{(1-c_{-}^{2})(1-c_{+}^{2})}},\qquad b_{t,d}^{-}=\sqrt{\frac{1-c_{-}}{1+c_{-}}},\qquad b_{t,d}^{+}=\sqrt{\frac{1-c_{+}}{1+c_{+}}}. \tag*{(4)} ξ t , d = ( 1 − c − 2 ) ( 1 − c + 2 ) c 0 − c − c + , b t , d − = 1 + c − 1 − c − , b t , d + = 1 + c + 1 − c + . (4)
Theorem 2.1 (Exact sitewise peak law). Suppose c ± ∈ ( − 1 , 1 ) c_{\pm}\in(-1,1) c ± ∈ ( − 1 , 1 ) . Then q t , d ∈ ( − 1 , 1 ] q_{t,d}\in(-1,1] q t , d ∈ ( − 1 , 1 ] and the peak height density at t t t is given by
h t , d ( x ) = ϕ ( x ) Φ 2 ( b t , d − x , b t , d + x ; ξ t , d ) p t , d , p t , d = 1 4 + 1 2 π arcsin ( q t , d ) > 0 , x ∈ R . (5) h_{t,d}(x)=\frac{\phi(x)\Phi_{2}\left(b_{t,d}^{-}x,b_{t,d}^{+}x;\xi_{t,d}\right)}{p_{t,d}},\qquad p_{t,d}=\frac{1}{4}+\frac{1}{2\pi}\arcsin(q_{t,d})>0,\qquad x\in\mathbb{R}. \tag*{(5)} h t , d ( x ) = p t , d ϕ ( x ) Φ 2 ( b t , d − x , b t , d + x ; ξ t , d ) , p t , d = 4 1 + 2 π 1 arcsin ( q t , d ) > 0 , x ∈ R . (5)
Proof. Let Y − = X ( t ) − X ( t − d ) Y_{-}=X(t)-X(t-d) Y − = X ( t ) − X ( t − d ) and Y + = X ( t ) − X ( t + d ) Y_{+}=X(t)-X(t+d) Y + = X ( t ) − X ( t + d ) . Since X X X is centered and has unit variance,
Var ( Y ± ) = 2 ( 1 − c ± ) > 0 , Cov { X ( t ) , Y ± } = 1 − c ± > 0. \operatorname{Var}(Y_{\pm})=2(1-c_{\pm})>0,\qquad\operatorname{Cov}\{X(t),Y_{\pm}\}=1-c_{\pm}>0. Var ( Y ± ) = 2 ( 1 − c ± ) > 0 , Cov { X ( t ) , Y ± } = 1 − c ± > 0.
Define Z ± = Y ± / 2 ( 1 − c ± ) Z_{\pm}=Y_{\pm}/\sqrt{2(1-c_{\pm})} Z ± = Y ± / 2 ( 1 − c ± ) . These are standard Gaussian variables with correlation q t , d q_{t,d} q t , d , and
Cov { X ( t ) , Z ± } = 1 − c ± 2 > 0. \operatorname{Cov}\{X(t),Z_{\pm}\}=\sqrt{\frac{1-c_{\pm}}{2}}>0. Cov { X ( t ) , Z ± } = 2 1 − c ± > 0.
By Cauchy–Schwarz, together with Var { X ( t ) } = 1 \operatorname{Var}\{X(t)\}=1 Var { X ( t )} = 1 , we obtain
2 ( 1 + q t , d ) = Var ( Z − + Z + ) ≥ { 1 − c − 2 + 1 − c + 2 } 2 > 0. 2(1+q_{t,d})=\operatorname{Var}(Z_{-}+Z_{+})\geq\left\{\sqrt{\frac{1-c_{-}}{2}}+\sqrt{\frac{1-c_{+}}{2}}\right\}^{2}>0. 2 ( 1 + q t , d ) = Var ( Z − + Z + ) ≥ { 2 1 − c − + 2 1 − c + } 2 > 0.
Hence q t , d > − 1 q_{t,d}>-1 q t , d > − 1 . The bivariate Gaussian orthant identity [3 ] , including the singular case q t , d = 1 q_{t,d}=1 q t , d = 1 , gives
p t , d = P ( Y − > 0 , Y + > 0 ) = 1 4 + 1 2 π arcsin ( q t , d ) > 0. p_{t,d}=\mathbb{P}(Y_{-}>0,Y_{+}>0)=\frac{1}{4}+\frac{1}{2\pi}\arcsin(q_{t,d})>0. p t , d = P ( Y − > 0 , Y + > 0 ) = 4 1 + 2 π 1 arcsin ( q t , d ) > 0.
The conditional vector ( X ( t − d ) , X ( t + d ) ∣ X ( t ) = x ) (X(t-d),X(t+d)\mid X(t)=x) ( X ( t − d ) , X ( t + d ) ∣ X ( t ) = x ) has mean ( c − x , c + x ) (c_{-}x,c_{+}x) ( c − x , c + x ) and covariance
( 1 − c − 2 c 0 − c − c + c 0 − c − c + 1 − c + 2 ) . \begin{pmatrix}
1-c_{-}^{2} & c_{0}-c_{-}c_{+} \\
c_{0}-c_{-}c_{+} & 1-c_{+}^{2}
\end{pmatrix}. ( 1 − c − 2 c 0 − c − c + c 0 − c − c + 1 − c + 2 ) .
Both conditional marginal variances are positive, and their standardized correlation is ξ t , d ∈ [ − 1 , 1 ] \xi_{t,d}\in[-1,1] ξ t , d ∈ [ − 1 , 1 ] . On defining
Z 1 = X ( t − d ) − c − x 1 − c − 2 , Z 2 = X ( t + d ) − c + x 1 − c + 2 , Z_{1}=\frac{X(t-d)-c_{-}x}{\sqrt{1-c_{-}^{2}}},\qquad Z_{2}=\frac{X(t+d)-c_{+}x}{\sqrt{1-c_{+}^{2}}}, Z 1 = 1 − c − 2 X ( t − d ) − c − x , Z 2 = 1 − c + 2 X ( t + d ) − c + x ,
the conditional vector ( Z 1 , Z 2 ∣ X ( t ) = x ) (Z_{1},Z_{2}\mid X(t)=x) ( Z 1 , Z 2 ∣ X ( t ) = x ) is standard bivariate Gaussian with correlation ξ t , d \xi_{t,d} ξ t , d . Hence
P ( A t , d ∣ X ( t ) = x ) = P ( X ( t − d ) < x , X ( t + d ) < x ∣ X ( t ) = x ) = P ( Z 1 < b t , d − x , Z 2 < b t , d + x ∣ X ( t ) = x ) = Φ 2 ( b t , d − x , b t , d + x ; ξ t , d ) . (6) \begin{aligned}
\mathbb{P}(A_{t,d}\mid X(t)=x)
&=\mathbb{P}(X(t-d)<x,X(t+d)<x\mid X(t)=x)\\
&=\mathbb{P}(Z_{1}<b^{-}_{t,d}x,Z_{2}<b^{+}_{t,d}x\mid X(t)=x)\\
&=\Phi_{2}\left(b^{-}_{t,d}x,b^{+}_{t,d}x;\xi_{t,d}\right). \tag*{(6)}
\end{aligned} P ( A t , d ∣ X ( t ) = x ) = P ( X ( t − d ) < x , X ( t + d ) < x ∣ X ( t ) = x ) = P ( Z 1 < b t , d − x , Z 2 < b t , d + x ∣ X ( t ) = x ) = Φ 2 ( b t , d − x , b t , d + x ; ξ t , d ) . (6)
This argument remains valid when the conditional vector is singular. It follows that
H t , d ( u ) = 1 p t , d P { A t , d , X ( t ) ≤ u } = 1 p t , d ∫ − ∞ u P { A t , d ∣ X ( t ) = x } ϕ ( x ) d x . H_{t,d}(u)=\frac{1}{p_{t,d}}\mathbb{P}\{A_{t,d},X(t)\leq u\}=\frac{1}{p_{t,d}}\int_{-\infty}^{u}\mathbb{P}\{A_{t,d}\mid X(t)=x\}\phi(x)\,\mathrm{d}x. H t , d ( u ) = p t , d 1 P { A t , d , X ( t ) ≤ u } = p t , d 1 ∫ − ∞ u P { A t , d ∣ X ( t ) = x } ϕ ( x ) d x .
The integrand is continuous, including at ξ t , d = ± 1 \xi_{t,d}=\pm1 ξ t , d = ± 1 . Plugging (6) and taking differentiation proves (5) .
Define the joint height and peak-event density by
g t , d ( x ) = ϕ ( x ) Φ 2 ( b t , d − x , b t , d + x ; ξ t , d ) = ϕ ( x ) P ( A t , d ∣ X ( t ) = x ) . (7) g_{t,d}(x)=\phi(x)\Phi_{2}\left(b^{-}_{t,d}x,b^{+}_{t,d}x;\xi_{t,d}\right)=\phi(x)\mathbb{P}(A_{t,d}\mid X(t)=x). \tag*{(7)} g t , d ( x ) = ϕ ( x ) Φ 2 ( b t , d − x , b t , d + x ; ξ t , d ) = ϕ ( x ) P ( A t , d ∣ X ( t ) = x ) . (7)
Then
P { X ( t ) ∈ d x , A t , d } = g t , d ( x ) d x , ∫ R g t , d ( x ) d x = p t , d . (8) \mathbb{P}\{X(t)\in\mathrm{d}x,A_{t,d}\}=g_{t,d}(x)\,\mathrm{d}x,\qquad\int_{\mathbb{R}}g_{t,d}(x)\,\mathrm{d}x=p_{t,d}. \tag*{(8)} P { X ( t ) ∈ d x , A t , d } = g t , d ( x ) d x , ∫ R g t , d ( x ) d x = p t , d . (8)
Remark 2.2. The positive definiteness of the covariance matrix of ( X ( t − d ) , X ( t ) , X ( t + d ) ) (X(t-d),X(t),X(t+d)) ( X ( t − d ) , X ( t ) , X ( t + d )) is sufficient for the assumption in Theorem 2.1 , but is not necessary. Singular covariance matrices are permitted with the convention (1) .
Remark 2.3 (Equivalent sign convention). If one uses
γ t , d = Corr { X ( t ) − X ( t − d ) , X ( t + d ) − X ( t ) } = − q t , d , \gamma_{t,d}=\operatorname{Corr}\{X(t)-X(t-d),X(t+d)-X(t)\}=-q_{t,d}, γ t , d = Corr { X ( t ) − X ( t − d ) , X ( t + d ) − X ( t )} = − q t , d ,
then p t , d = arccos ( γ t , d ) / ( 2 π ) p_{t,d}=\arccos(\gamma_{t,d})/(2\pi) p t , d = arccos ( γ t , d ) / ( 2 π ) . The convention used in (2) keeps the local maximum event in the positive orthant.
Expected counts of peaks
Define the numbers of all interior grid peaks and of peaks above u u u by
M d ( I ) = ∑ t ∈ G d ∘ 1 A t , d , M u , d ( I ) = ∑ t ∈ G d ∘ 1 A t , d 1 { X ( t ) > u } . M_d(I) = \sum_{t \in\mathcal{G}_d^\circ} \mathbb{1}_{A_{t,d}}, \qquad M_{u,d}(I) = \sum_{t \in\mathcal{G}_d^\circ} \mathbb{1}_{A_{t,d}}\mathbb{1}\{X(t)>u\}. M d ( I ) = t ∈ G d ∘ ∑ 1 A t , d , M u , d ( I ) = t ∈ G d ∘ ∑ 1 A t , d 1 { X ( t ) > u } .
Linearity of expectation, together with (2.7) and (2.8), yields
E M d ( I ) = ∑ t ∈ G d ∘ p t , d , E M u , d ( I ) = ∑ t ∈ G d ∘ ∫ u ∞ g t , d ( x ) d x . (9) \mathbb{E}M_d(I) = \sum_{t \in\mathcal{G}_d^\circ} p_{t,d}, \qquad\mathbb{E}M_{u,d}(I) = \sum_{t \in\mathcal{G}_d^\circ} \int_u^\infty g_{t,d}(x)\,dx. \tag*{(9)} E M d ( I ) = t ∈ G d ∘ ∑ p t , d , E M u , d ( I ) = t ∈ G d ∘ ∑ ∫ u ∞ g t , d ( x ) d x . (9)
No independence between sites is required. The bivariate CDF expressions apply whenever − 1 < c ± < 1 -1<c_{\pm}<1 − 1 < c ± < 1 at every included site. The quantity p t , d p_{t,d} p t , d in (2.5) is a sitewise probability, rather than a count intensity per unit length; its length-normalized counterpart is p t , d / d p_{t,d}/d p t , d / d .
Stationary specialization
Suppose now that X X X is stationary with correlation r ( s ) = E { X ( t ) X ( t + s ) } r(s)=\mathbb{E}\{X(t)X(t+s)\} r ( s ) = E { X ( t ) X ( t + s )} . Let
q d = 1 − 2 r ( d ) + r ( 2 d ) 2 { 1 − r ( d ) } , ξ d = r ( 2 d ) − r ( d ) 2 1 − r ( d ) 2 , b d = 1 − r ( d ) 1 + r ( d ) . (10) q_d = \frac{1-2r(d)+r(2d)}{2\{1-r(d)\}}, \qquad\xi_d = \frac{r(2d)-r(d)^2}{1-r(d)^2}, \qquad b_d = \sqrt{\frac{1-r(d)}{1+r(d)}}. \tag*{(10)} q d = 2 { 1 − r ( d )} 1 − 2 r ( d ) + r ( 2 d ) , ξ d = 1 − r ( d ) 2 r ( 2 d ) − r ( d ) 2 , b d = 1 + r ( d ) 1 − r ( d ) . (10)
Corollary 2.4 (Exact stationary peak law). Suppose r ( d ) ∈ ( − 1 , 1 ) r(d)\in(-1,1) r ( d ) ∈ ( − 1 , 1 ) . At every interior site, the peak height density is given by
h d ( x ) = ϕ ( x ) Φ 2 ( b d x , b d x ; ξ d ) p d , p d = 1 4 + 1 2 π arcsin ( q d ) , x ∈ R . (11) h_d(x) = \frac{\phi(x)\Phi_2(b_dx,b_dx;\xi_d)}{p_d}, \qquad p_d = \frac{1}{4}+\frac{1}{2\pi}\arcsin(q_d), \qquad x\in\mathbb{R}. \tag*{(11)} h d ( x ) = p d ϕ ( x ) Φ 2 ( b d x , b d x ; ξ d ) , p d = 4 1 + 2 π 1 arcsin ( q d ) , x ∈ R . (11) If the grid has n d n_d n d interior sites, then
E M d = n d p d , E M u , d = n d ∫ u ∞ ϕ ( x ) Φ 2 ( b d x , b d x ; ξ d ) d x . (12) \mathbb{E}M_d=n_dp_d, \qquad\mathbb{E}M_{u,d}=n_d\int_u^\infty\phi(x)\Phi_2(b_dx,b_dx;\xi_d)\,dx. \tag*{(12)} E M d = n d p d , E M u , d = n d ∫ u ∞ ϕ ( x ) Φ 2 ( b d x , b d x ; ξ d ) d x . (12)
Proof. Stationarity gives c − = c + = r ( d ) c_-=c_+=r(d) c − = c + = r ( d ) and c 0 = r ( 2 d ) c_0=r(2d) c 0 = r ( 2 d ) . Substitution in (2.3) and (2.4) yields q t , d = q d q_{t,d}=q_d q t , d = q d , ξ t , d = ξ d \xi_{t,d}=\xi_d ξ t , d = ξ d and b t , d − = b t , d + = b d b^-_{t,d}=b^+_{t,d}=b_d b t , d − = b t , d + = b d . Theorem 2.1 therefore gives (2.11), independently of the interior site t t t . Finally, (2.12) follows from (2.9) with n d = ∣ G d ∘ ∣ n_d=|\mathcal{G}_d^\circ| n d = ∣ G d ∘ ∣ .
Example 2.5 (Independent Gaussian observations). For an i.i.d. standard Gaussian sequence, r ( d ) = r ( 2 d ) = 0 r(d)=r(2d)=0 r ( d ) = r ( 2 d ) = 0 at distinct grid sites. Hence p d = 1 / 3 p_d=1/3 p d = 1/3 and h d ( x ) = 3 ϕ ( x ) Φ ( x ) 2 h_d(x)=3\phi(x)\Phi(x)^2 h d ( x ) = 3 ϕ ( x ) Φ ( x ) 2 . This is the density of the maximum of three independent standard Gaussian variables. This model is not mean-square continuous and lies outside the infill classification below.
The Infill Limit for Smooth Covariance
The smooth covariance target and its Palm interpretation
Fix an interior point t t t . Assume that C C C has continuous partial derivatives through total order four in a neighborhood of ( t , t ) (t,t) ( t , t ) . Then X X X has the first and second mean-square derivatives there. Write
λ 1 ( t ) = Var { X ′ ( t ) } > 0 , λ 2 ( t ) = Var { X ′ ′ ( t ) } , \lambda_1(t)=\operatorname{Var}\{X'(t)\}>0,\qquad\lambda_2(t)=\operatorname{Var}\{X''(t)\}, λ 1 ( t ) = Var { X ′ ( t )} > 0 , λ 2 ( t ) = Var { X ′′ ( t )} ,
a ( t ) = Cov { X ′ ( t ) , X ′ ′ ( t ) } = λ 1 ′ ( t ) / 2 , (13) a(t)=\operatorname{Cov}\{X'(t),X''(t)\}=\lambda_1'(t)/2, \tag*{(13)} a ( t ) = Cov { X ′ ( t ) , X ′′ ( t )} = λ 1 ′ ( t ) /2 , (13)
δ t 2 = Var { X ′ ′ ( t ) ∣ X ′ ( t ) } = λ 2 ( t ) − a ( t ) 2 / λ 1 ( t ) . \delta_t^2=\operatorname{Var}\{X''(t)\mid X'(t)\}=\lambda_2(t)-a(t)^2/\lambda_1(t). δ t 2 = Var { X ′′ ( t ) ∣ X ′ ( t )} = λ 2 ( t ) − a ( t ) 2 / λ 1 ( t ) .
The unit-variance condition C ( t , t ) = 1 C(t,t)=1 C ( t , t ) = 1 implies Cov { X ( t ) , X ′ ( t ) } = 0 \operatorname{Cov}\{X(t),X'(t)\}=0 Cov { X ( t ) , X ′ ( t )} = 0 and Cov { X ( t ) , X ′ ′ ( t ) } = − λ 1 ( t ) \operatorname{Cov}\{X(t),X''(t)\}=-\lambda_1(t) Cov { X ( t ) , X ′′ ( t )} = − λ 1 ( t ) . Consequently,
τ t 2 = Var { X ′ ′ ( t ) ∣ X ( t ) , X ′ ( t ) } = δ t 2 − λ 1 ( t ) 2 ≥ 0 , (14) \tau_t^2=\operatorname{Var}\{X''(t)\mid X(t),X'(t)\}=\delta_t^2-\lambda_1(t)^2\ge0, \tag*{(14)} τ t 2 = Var { X ′′ ( t ) ∣ X ( t ) , X ′ ( t )} = δ t 2 − λ 1 ( t ) 2 ≥ 0 , (14)
η t = − Corr { X ( t ) , X ′ ′ ( t ) ∣ X ′ ( t ) } = λ 1 ( t ) / δ t ∈ ( 0 , 1 ] . (15) \eta_t=-\operatorname{Corr}\{X(t),X''(t)\mid X'(t)\}=\lambda_1(t)/\delta_t\in(0,1]. \tag*{(15)} η t = − Corr { X ( t ) , X ′′ ( t ) ∣ X ′ ( t )} = λ 1 ( t ) / δ t ∈ ( 0 , 1 ] . (15)
In particular, the degenerate case η t = 1 \eta_t=1 η t = 1 is equivalent to τ t = 0 \tau_t=0 τ t = 0 .
Recall ( y ) + = max { y , 0 } (y)_+=\max\{y,0\} ( y ) + = max { y , 0 } . By [4 ] , for a smooth process, its peak height density is the ratio of intensities J t ( x ) J_t(x) J t ( x ) and J t J_t J t :
h η t S M ( x ) = J t ( x ) / J t , (16) h_{\eta_t}^{\mathrm{SM}}(x)=J_t(x)/J_t, \tag*{(16)} h η t SM ( x ) = J t ( x ) / J t , (16)
where
J t ( x ) = f X ( t ) , X ′ ( t ) ( x , 0 ) E [ ( − X ′ ′ ( t ) ) + ∣ X ( t ) = x , X ′ ( t ) = 0 ] = { δ t ϕ ( x ) 2 π λ 1 ( t ) { 1 − η t 2 ϕ ( η t x 1 − η t 2 ) + η t x Φ ( η t x 1 − η t 2 ) } , 0 < η t < 1 , λ 1 ( t ) 2 π x e − x 2 / 2 1 { x > 0 } , η t = 1 , (17) \begin{aligned}
J_t(x)=f_{X(t),X'(t)}(x,0)\mathbb{E}\left[(-X''(t))_+\mid X(t)=x,X'(t)=0\right] \\
&=\begin{cases}
\dfrac{\delta_t\phi(x)}{\sqrt{2\pi\lambda_1(t)}}\left\{\sqrt{1-\eta_t^2}\,\phi\left(\dfrac{\eta_t x}{\sqrt{1-\eta_t^2}}\right)+\eta_t x\Phi\left(\dfrac{\eta_t x}{\sqrt{1-\eta_t^2}}\right)\right\}, & 0<\eta_t<1,\\[1.2em]
\dfrac{\sqrt{\lambda_1(t)}}{2\pi}xe^{-x^2/2}\mathbf{1}_{\{x>0\}}, & \eta_t=1,
\end{cases} \tag*{(17)}
\end{aligned} J t ( x ) = f X ( t ) , X ′ ( t ) ( x , 0 ) E [ ( − X ′′ ( t ) ) + ∣ X ( t ) = x , X ′ ( t ) = 0 ] = ⎩ ⎨ ⎧ 2 π λ 1 ( t ) δ t ϕ ( x ) { 1 − η t 2 ϕ ( 1 − η t 2 η t x ) + η t x Φ ( 1 − η t 2 η t x ) } , 2 π λ 1 ( t ) x e − x 2 /2 1 { x > 0 } , 0 < η t < 1 , η t = 1 , (17)
and
J t = f X ′ ( t ) ( 0 ) E [ ( − X ′ ′ ( t ) ) + ∣ X ′ ( t ) = 0 ] = δ t 2 π λ 1 ( t ) > 0. (18) J_t=f_{X'(t)}(0)\mathbb{E}\left[(-X''(t))_+\mid X'(t)=0\right]=\frac{\delta_t}{2\pi\sqrt{\lambda_1(t)}}>0. \tag*{(18)} J t = f X ′ ( t ) ( 0 ) E [ ( − X ′′ ( t ) ) + ∣ X ′ ( t ) = 0 ] = 2 π λ 1 ( t ) δ t > 0. (18)
Integrating J t ( x ) J_t(x) J t ( x ) over x x x gives J t J_t J t , thus the ratio in (16) is a probability density. When η t = 1 \eta_t=1 η t = 1 , δ t = λ 1 ( t ) \delta_t=\lambda_1(t) δ t = λ 1 ( t ) and hence J t = λ 1 ( t ) / ( 2 π ) J_t=\sqrt{\lambda_1(t)}/(2\pi) J t = λ 1 ( t ) / ( 2 π ) . If an a.s. C 2 C^2 C 2 version and the standard Kac–Rice regularity assumptions hold, then J t J_t J t is the local intensity of continuous local maxima and h η t S M h_{\eta_t}^{\mathrm{SM}} h η t SM is the local Palm height density [1 , 2 , 4 ] . The discrete infill limits below require only the stated covariance assumptions.
A uniform bivariate Gaussian scaling lemma
The following lemma makes the infill argument uniform even when the conditional variance τ t 2 = 0 \tau_t^2=0 τ t 2 = 0 . As in Section 2, Φ 2 \Phi_2 Φ 2 includes singular Gaussian laws at correlation ξ t , d = − 1 \xi_{t,d}=-1 ξ t , d = − 1 .
Lemma 3.1 (Uniform bivariate Gaussian scaling limit). Let Θ \Theta Θ be an index set. For θ ∈ Θ \theta\in\Theta θ ∈ Θ , suppose A θ , d , B θ , d ∈ R A_{\theta,d},B_{\theta,d}\in\mathbb{R} A θ , d , B θ , d ∈ R and ζ θ , d ∈ [ − 1 , 1 ] \zeta_{\theta,d}\in[-1,1] ζ θ , d ∈ [ − 1 , 1 ] satisfy, uniformly in θ \theta θ ,
A θ , d d → A θ , B θ , d d → B θ , 1 + ζ θ , d d 2 → β θ , \frac{A_{\theta,d}}{d}\to A_\theta,\qquad
\frac{B_{\theta,d}}{d}\to B_\theta,\qquad
\frac{1+\zeta_{\theta,d}}{d^2}\to\beta_\theta, d A θ , d → A θ , d B θ , d → B θ , d 2 1 + ζ θ , d → β θ ,
where A θ , B θ ∈ R A_\theta, B_\theta\in\mathbb{R} A θ , B θ ∈ R and β θ ≥ 0 \beta_\theta\ge0 β θ ≥ 0 are uniformly bounded. Then
sup θ ∈ Θ ∣ Φ 2 ( A θ , d , B θ , d ; ζ θ , d ) d − ϕ ( 0 ) E [ ( A θ + B θ − 2 β θ U ) + ] ∣ → 0 , (19) \sup_{\theta\in\Theta}\left|\frac{\Phi_2(A_{\theta,d},B_{\theta,d};\zeta_{\theta,d})}{d}-\phi(0)\mathbb{E}\left[(A_\theta+B_\theta-\sqrt{2\beta_\theta}U)_+\right]\right|\to0, \tag*{(19)} θ ∈ Θ sup d Φ 2 ( A θ , d , B θ , d ; ζ θ , d ) − ϕ ( 0 ) E [ ( A θ + B θ − 2 β θ U ) + ] → 0 , (19)
where U ∼ N ( 0 , 1 ) U\sim N(0,1) U ∼ N ( 0 , 1 ) . Moreover, if ∣ A θ , d ∣ / d + ∣ B θ , d ∣ / d ≤ L |A_{\theta,d}|/d+|B_{\theta,d}|/d\le L ∣ A θ , d ∣/ d + ∣ B θ , d ∣/ d ≤ L and ( 1 + ζ θ , d ) / d 2 ≤ K (1+\zeta_{\theta,d})/d^2\le K ( 1 + ζ θ , d ) / d 2 ≤ K for all sufficiently small d d d , then Φ 2 ( A θ , d , B θ , d ; ζ θ , d ) / d ≤ c ( L + K ) \Phi_2(A_{\theta,d},B_{\theta,d};\zeta_{\theta,d})/d\le c(L+\sqrt{K}) Φ 2 ( A θ , d , B θ , d ; ζ θ , d ) / d ≤ c ( L + K ) , where c > 0 c>0 c > 0 is a constant independent of θ \theta θ and d d d .
Proof. Suppress θ \theta θ temporarily and let ( Z 1 , Z 2 ) (Z_1,Z_2) ( Z 1 , Z 2 ) be standard bivariate Gaussian with correlation ζ d \zeta_d ζ d . The independent Gaussian coordinates
S = ( Z 1 + Z 2 ) / 2 = d κ U , T = ( Z 1 − Z 2 ) / 2 = ν V , S=(Z_1+Z_2)/2=d\kappa U,\qquad T=(Z_1-Z_2)/2=\nu V, S = ( Z 1 + Z 2 ) /2 = d κ U , T = ( Z 1 − Z 2 ) /2 = ν V ,
have κ = ( 1 + ζ d ) / ( 2 d 2 ) \kappa=\sqrt{(1+\zeta_d)/(2d^2)} κ = ( 1 + ζ d ) / ( 2 d 2 ) and ν = ( 1 − ζ d ) / 2 \nu=\sqrt{(1-\zeta_d)/2} ν = ( 1 − ζ d ) /2 , where U , V U,V U , V are independent standard Gaussian. The assumptions give ν → 1 \nu\to1 ν → 1 uniformly, so ν \nu ν is bounded away from zero for small d d d . This representation also holds when κ = 0 \kappa=0 κ = 0 . Let a = A d / d a=A_d/d a = A d / d , b = B d / d b=B_d/d b = B d / d and f ν ( y ) = ν − 1 ϕ ( y / ν ) f_\nu(y)=\nu^{-1}\phi(y/\nu) f ν ( y ) = ν − 1 ϕ ( y / ν ) . The two inequalities Z 1 ≤ A d Z_1\le A_d Z 1 ≤ A d and Z 2 ≤ B d Z_2\le B_d Z 2 ≤ B d defining Φ 2 \Phi_2 Φ 2 are equivalent to d ( κ U − b ) ≤ T ≤ d ( a − κ U ) d(\kappa U-b)\le T\le d(a-\kappa U) d ( κ U − b ) ≤ T ≤ d ( a − κ U ) . Using the restriction κ U − b < a − κ U \kappa U-b<a-\kappa U κ U − b < a − κ U and making the substitution y = d z y=dz y = d z , we obtain
Φ 2 ( A d , B d ; ζ d ) d = E [ 1 { 2 κ U < a + b } ∫ κ U − b a − κ U f ν ( d z ) d z ] . (20) \frac{\Phi_2(A_d,B_d;\zeta_d)}{d}=\mathbb{E}\left[\mathbf{1}_{\{2\kappa U<a+b\}}\int_{\kappa U-b}^{a-\kappa U}f_\nu(dz)\,\mathrm{d}z\right]. \tag*{(20)} d Φ 2 ( A d , B d ; ζ d ) = E [ 1 { 2 κ U < a + b } ∫ κ U − b a − κ U f ν ( d z ) d z ] . (20)
Endpoint equalities do not affect the integral. Its interval length is ℓ = ( a + b − 2 κ U ) + \ell=(a+b-2\kappa U)_+ ℓ = ( a + b − 2 κ U ) + , which is bounded by ∣ a ∣ + ∣ b ∣ + 2 κ ∣ U ∣ |a|+|b|+2\kappa|U| ∣ a ∣ + ∣ b ∣ + 2 κ ∣ U ∣ . This proves the asserted probability bound, since sup y f ν ( y ) = ϕ ( 0 ) / ν \sup_y f_\nu(y)=\phi(0)/\nu sup y f ν ( y ) = ϕ ( 0 ) / ν .
For the convergence, boundedness gives a constant M M M such that ∣ a ∣ , ∣ b ∣ , κ ≤ M |a|,|b|,\kappa\le M ∣ a ∣ , ∣ b ∣ , κ ≤ M uniformly. Every integration point in (3.8) has ∣ z ∣ ≤ M ( 1 + ∣ U ∣ ) |z|\le M(1+|U|) ∣ z ∣ ≤ M ( 1 + ∣ U ∣ ) . Thus the absolute difference between that expression and ϕ ( 0 ) E ℓ \phi(0)\mathbb{E}\ell ϕ ( 0 ) E ℓ is bounded by
E [ 2 M ( 1 + ∣ U ∣ ) sup ∣ z ∣ ≤ M ( 1 + ∣ U ∣ ) ∣ f ν ( d z ) − ϕ ( 0 ) ∣ ] . \mathbb{E}\left[2M(1+|U|)\sup_{|z|\le M(1+|U|)}|f_\nu(dz)-\phi(0)|\right]. E [ 2 M ( 1 + ∣ U ∣ ) ∣ z ∣ ≤ M ( 1 + ∣ U ∣ ) sup ∣ f ν ( d z ) − ϕ ( 0 ) ∣ ] .
The supremum tends to zero for each fixed U U U , uniformly in θ \theta θ , and is bounded by a constant. The integrable envelope M ′ ( 1 + ∣ U ∣ ) M'(1+|U|) M ′ ( 1 + ∣ U ∣ ) for some constant M ′ M' M ′ therefore proves convergence uniformly in θ \theta θ . Finally, y ↦ ( y ) + y\mapsto(y)_+ y ↦ ( y ) + is Lipschitz with constant one, and
∣ E ( a + b − 2 κ U ) + − E ( A θ + B θ − 2 β θ U ) + ∣ ≤ ∣ a − A θ ∣ + ∣ b − B θ ∣ + ∣ 2 κ − 2 β θ ∣ E ∣ U ∣ . \left|\mathbb{E}(a+b-2\kappa U)_+-\mathbb{E}(A_\theta+B_\theta-\sqrt{2\beta_\theta}U)_+\right|\le|a-A_\theta|+|b-B_\theta|+|2\kappa-\sqrt{2\beta_\theta}|\mathbb{E}|U|. E ( a + b − 2 κ U ) + − E ( A θ + B θ − 2 β θ U ) + ≤ ∣ a − A θ ∣ + ∣ b − B θ ∣ + ∣2 κ − 2 β θ ∣ E ∣ U ∣.
The right-hand side tends to zero uniformly; convergence of the square roots holds also at β θ = 0 \beta_\theta=0 β θ = 0 . This proves the lemma.
Convergence of probabilities, densities and counts
Theorem 3.2 (Smooth infill limit). Suppose C C C has continuous partial derivatives through total order four in a neighborhood of ( t , t ) (t,t) ( t , t ) , and λ 1 ( t ) > 0 \lambda_1(t)>0 λ 1 ( t ) > 0 . Then, for a fixed interior point t t t , as $d\downarrow 0,
p t , d / d → J t p_{t,d}/d \to J_t p t , d / d → J t and g t , d ( x ) / d → J t ( x ) g_{t,d}(x)/d \to J_t(x) g t , d ( x ) / d → J t ( x ) for every x ∈ R x \in\mathbb{R} x ∈ R . Consequently, h t , d ( x ) h_{t,d}(x) h t , d ( x ) converges pointwise and in L 1 ( R ) L^1(\mathbb{R}) L 1 ( R ) to the smooth peak height density
h η t S M ( x ) = { 1 − η t 2 ϕ ( x 1 − η t 2 ) + 2 π η t x ϕ ( x ) Φ ( η t x 1 − η t 2 ) , 0 < η t < 1 , x e − x 2 / 2 1 { x > 0 } , η t = 1 , (21) h_{\eta_t}^{\mathrm{SM}}(x)=
\begin{cases}
\sqrt{1-\eta_t^2}\,\phi\left(\dfrac{x}{\sqrt{1-\eta_t^2}}\right)+\sqrt{2\pi}\,\eta_t x\phi(x)\Phi\left(\dfrac{\eta_t x}{\sqrt{1-\eta_t^2}}\right), & 0<\eta_t<1,\\
xe^{-x^2/2}\mathbf{1}_{\{x>0\}}, & \eta_t=1,
\end{cases} \tag*{(21)} h η t SM ( x ) = ⎩ ⎨ ⎧ 1 − η t 2 ϕ ( 1 − η t 2 x ) + 2 π η t x ϕ ( x ) Φ ( 1 − η t 2 η t x ) , x e − x 2 /2 1 { x > 0 } , 0 < η t < 1 , η t = 1 , (21)
and thus the discrete peak height distributions converge in total variation.
Proof. (i) We first prove the nondegenerate case 0 < η t < 1 0<\eta_t<1 0 < η t < 1 (i.e., τ > 0 \tau>0 τ > 0 ). For brevity, suppress the argument t t t and write λ 1 = λ 1 ( t ) \lambda_1=\lambda_1(t) λ 1 = λ 1 ( t ) , λ 2 = λ 2 ( t ) \lambda_2=\lambda_2(t) λ 2 = λ 2 ( t ) , a = a ( t ) a=a(t) a = a ( t ) , δ = δ t \delta=\delta_t δ = δ t , and τ = τ t \tau=\tau_t τ = τ t . For i , j ≥ 0 i,j\geq0 i , j ≥ 0 , let
C i j = ∂ i + j ∂ s i ∂ v j C ( s , v ) ∣ s = v = t . C_{ij}=\left.\frac{\partial^{i+j}}{\partial s^i\partial v^j}C(s,v)\right|_{s=v=t}. C ij = ∂ s i ∂ v j ∂ i + j C ( s , v ) s = v = t .
Symmetry gives C i j = C j i C_{ij}=C_{ji} C ij = C j i . Differentiating C ( s , s ) = 1 C(s,s)=1 C ( s , s ) = 1 along the diagonal yields
C 01 = 0 , C 02 = − C 11 , C 03 = − 3 C 12 , C 04 = − 4 C 13 − 3 C 22 . (22) C_{01}=0,\qquad C_{02}=-C_{11},\qquad C_{03}=-3C_{12},\qquad C_{04}=-4C_{13}-3C_{22}. \tag*{(22)} C 01 = 0 , C 02 = − C 11 , C 03 = − 3 C 12 , C 04 = − 4 C 13 − 3 C 22 . (22)
By (13) and (14) , C 11 = λ 1 C_{11}=\lambda_1 C 11 = λ 1 , C 12 = a C_{12}=a C 12 = a , C 22 = λ 2 C_{22}=\lambda_2 C 22 = λ 2 , δ 2 = λ 2 − a 2 / λ 1 \delta^2=\lambda_2-a^2/\lambda_1 δ 2 = λ 2 − a 2 / λ 1 , and τ 2 = δ 2 − λ 1 2 \tau^2=\delta^2-\lambda_1^2 τ 2 = δ 2 − λ 1 2 . Fourth-order Taylor expansion of C C C at ( t , t ) (t,t) ( t , t ) gives
c − = 1 − λ 1 2 d 2 + a 2 d 3 + C 04 24 d 4 + o ( d 4 ) , c_-=1-\frac{\lambda_1}{2}d^2+\frac{a}{2}d^3+\frac{C_{04}}{24}d^4+o(d^4), c − = 1 − 2 λ 1 d 2 + 2 a d 3 + 24 C 04 d 4 + o ( d 4 ) ,
c + = 1 − λ 1 2 d 2 − a 2 d 3 + C 04 24 d 4 + o ( d 4 ) , c_+=1-\frac{\lambda_1}{2}d^2-\frac{a}{2}d^3+\frac{C_{04}}{24}d^4+o(d^4), c + = 1 − 2 λ 1 d 2 − 2 a d 3 + 24 C 04 d 4 + o ( d 4 ) ,
c 0 = 1 − 2 λ 1 d 2 + C 04 + 3 λ 2 − 4 C 13 12 d 4 + o ( d 4 ) . c_0=1-2\lambda_1d^2+\frac{C_{04}+3\lambda_2-4C_{13}}{12}d^4+o(d^4). c 0 = 1 − 2 λ 1 d 2 + 12 C 04 + 3 λ 2 − 4 C 13 d 4 + o ( d 4 ) .
For the peak probability, Remark 2.3 gives p t , d = ( 2 π ) − 1 arccos γ t , d p_{t,d}=(2\pi)^{-1}\arccos\gamma_{t,d} p t , d = ( 2 π ) − 1 arccos γ t , d , where γ t , d = − q t , d \gamma_{t,d}=-q_{t,d} γ t , d = − q t , d ,
c − + c + − 1 − c 0 = λ 1 d 2 + 4 C 13 − 3 λ 2 12 d 4 + o ( d 4 ) , c_-+c_+-1-c_0=\lambda_1d^2+\frac{4C_{13}-3\lambda_2}{12}d^4+o(d^4), c − + c + − 1 − c 0 = λ 1 d 2 + 12 4 C 13 − 3 λ 2 d 4 + o ( d 4 ) ,
2 ( 1 − c − ) ( 1 − c + ) = λ 1 d 2 { 1 − ( C 04 12 λ 1 + a 2 2 λ 1 2 ) d 2 + o ( d 2 ) } . 2\sqrt{(1-c_-)(1-c_+)}=\lambda_1d^2\left\{1-\left(\frac{C_{04}}{12\lambda_1}+\frac{a^2}{2\lambda_1^2}\right)d^2+o(d^2)\right\}. 2 ( 1 − c − ) ( 1 − c + ) = λ 1 d 2 { 1 − ( 12 λ 1 C 04 + 2 λ 1 2 a 2 ) d 2 + o ( d 2 ) } .
Substitution of (22) therefore yields
γ t , d = 1 − 1 2 λ 1 ( λ 2 − a 2 λ 1 ) d 2 + o ( d 2 ) = 1 − δ 2 2 λ 1 d 2 + o ( d 2 ) . (23) \gamma_{t,d}=1-\frac{1}{2\lambda_1}\left(\lambda_2-\frac{a^2}{\lambda_1}\right)d^2+o(d^2)=1-\frac{\delta^2}{2\lambda_1}d^2+o(d^2). \tag*{(23)} γ t , d = 1 − 2 λ 1 1 ( λ 2 − λ 1 a 2 ) d 2 + o ( d 2 ) = 1 − 2 λ 1 δ 2 d 2 + o ( d 2 ) . (23)
Since arccos ( 1 − y ) ∼ 2 y \arccos(1-y)\sim\sqrt{2y} arccos ( 1 − y ) ∼ 2 y , we obtain p t , d / d → δ / ( 2 π λ 1 ) = J t p_{t,d}/d\to\delta/(2\pi\sqrt{\lambda_1})=J_t p t , d / d → δ / ( 2 π λ 1 ) = J t .
For the conditional Gaussian law, the same expansions give
c 0 − c − c + = − λ 1 d 2 + ( λ 2 4 − C 13 3 − λ 1 2 4 ) d 4 + o ( d 4 ) , c_0-c_-c_+=-\lambda_1d^2+\left(\frac{\lambda_2}{4}-\frac{C_{13}}{3}-\frac{\lambda_1^2}{4}\right)d^4+o(d^4), c 0 − c − c + = − λ 1 d 2 + ( 4 λ 2 − 3 C 13 − 4 λ 1 2 ) d 4 + o ( d 4 ) ,
( 1 − c − 2 ) ( 1 − c + 2 ) = λ 1 d 2 { 1 − ( C 04 12 λ 1 + λ 1 4 + a 2 2 λ 1 2 ) d 2 + o ( d 2 ) } . \sqrt{(1-c_-^2)(1-c_+^2)}=\lambda_1d^2\left\{1-\left(\frac{C_{04}}{12\lambda_1}+\frac{\lambda_1}{4}+\frac{a^2}{2\lambda_1^2}\right)d^2+o(d^2)\right\}. ( 1 − c − 2 ) ( 1 − c + 2 ) = λ 1 d 2 { 1 − ( 12 λ 1 C 04 + 4 λ 1 + 2 λ 1 2 a 2 ) d 2 + o ( d 2 ) } .
After another use of (22) yields
ξ t , d = − 1 + τ 2 2 λ 1 d 2 + o ( d 2 ) , b t , d ± d ⟶ λ 1 2 . (24) \xi_{t,d}=-1+\frac{\tau^2}{2\lambda_1}d^2+o(d^2),\qquad\frac{b_{t,d}^{\pm}}{d}\longrightarrow\frac{\sqrt{\lambda_1}}{2}. \tag*{(24)} ξ t , d = − 1 + 2 λ 1 τ 2 d 2 + o ( d 2 ) , d b t , d ± ⟶ 2 λ 1 . (24)
Because 1 − c ± 2 = λ 1 d 2 + o ( d 2 ) 1-c_{\pm}^2=\lambda_1d^2+o(d^2) 1 − c ± 2 = λ 1 d 2 + o ( d 2 ) , the condition in Theorem 2.1 is satisfied. Apply Lemma 3.1 with A d = b t , d − x A_d=b_{t,d}^{-}x A d = b t , d − x , B d = b t , d + x B_d=b_{t,d}^{+}x B d = b t , d + x , and β = τ 2 / ( 2 λ 1 ) \beta=\tau^2/(2\lambda_1) β = τ 2 / ( 2 λ 1 ) . Multiplication by ϕ ( x ) \phi(x) ϕ ( x ) , together with τ = δ 1 − η t 2 \tau=\delta\sqrt{1-\eta_t^2} τ = δ 1 − η t 2 and λ 1 / τ = η t / 1 − η t 2 \lambda_1/\tau=\eta_t/\sqrt{1-\eta_t^2} λ 1 / τ = η t / 1 − η t 2 , gives
g t , d ( x ) d ⟶ ϕ ( x ) 2 π E [ ( λ 1 x − τ λ 1 U ) + ] = ϕ ( x ) 2 π λ 1 { τ ϕ ( λ 1 x τ ) + λ 1 x Φ ( λ 1 x τ ) } = J t ( x ) . \begin{aligned}
\frac{g_{t,d}(x)}{d}\longrightarrow\frac{\phi(x)}{\sqrt{2\pi}}\mathbb{E}\left[\left(\sqrt{\lambda_1}x-\frac{\tau}{\sqrt{\lambda_1}}U\right)_{+}\right] \\
&=\frac{\phi(x)}{\sqrt{2\pi\lambda_1}}\left\{\tau\phi\left(\frac{\lambda_1x}{\tau}\right)+\lambda_1x\Phi\left(\frac{\lambda_1x}{\tau}\right)\right\}=J_t(x).
\end{aligned} d g t , d ( x ) ⟶ 2 π ϕ ( x ) E [ ( λ 1 x − λ 1 τ U ) + ] = 2 π λ 1 ϕ ( x ) { τ ϕ ( τ λ 1 x ) + λ 1 x Φ ( τ λ 1 x ) } = J t ( x ) .
Combining the two limits yields the pointwise convergence to the first case of (21) ,
h t , d ( x ) = g t , d ( x ) / d p t , d / d ⟶ J t ( x ) J t = h η t S M ( x ) , x ∈ R . h_{t,d}(x)=\frac{g_{t,d}(x)/d}{p_{t,d}/d}\longrightarrow\frac{J_t(x)}{J_t}=h_{\eta_t}^{\mathrm{SM}}(x),\qquad x\in\mathbb{R}. h t , d ( x ) = p t , d / d g t , d ( x ) / d ⟶ J t J t ( x ) = h η t SM ( x ) , x ∈ R .
Since both h t , d h_{t,d} h t , d and h η t S M h_{\eta_t}^{\mathrm{SM}} h η t SM are probability densities, Scheffé’s theorem gives L 1 L^1 L 1 and total variation convergence ∫ R ∣ h t , d ( x ) − h η t S M ( x ) ∣ d x → 0 \int_{\mathbb{R}}\lvert h_{t,d}(x)-h_{\eta_t}^{\mathrm{SM}}(x)\rvert\,dx\to0 ∫ R ∣ h t , d ( x ) − h η t SM ( x )∣ d x → 0 .
(ii) We next prove the degenerate case η t = 1 \eta_t=1 η t = 1 (i.e., τ = 0 \tau=0 τ = 0 ). The Taylor calculations above do not use τ > 0 \tau>0 τ > 0 . Here δ = λ 1 \delta=\lambda_1 δ = λ 1 and τ = 0 \tau=0 τ = 0 , so (3.11) gives p t , d / d → λ 1 / ( 2 π ) p_{t,d}/d\to\sqrt{\lambda_1}/(2\pi) p t , d / d → λ 1 / ( 2 π ) . Apply Lemma 3.1 with A d = b t , d − x A_d=b_{t,d}^{-}x A d = b t , d − x , B d = b t , d + x B_d=b_{t,d}^{+}x B d = b t , d + x , and β = 0 \beta=0 β = 0 . We obtain
g t , d ( x ) d ⟶ ϕ ( x ) 2 π ( λ 1 x ) + = λ 1 2 π x e − x 2 / 2 1 { x > 0 } = J t ( x ) , x ∈ R . \frac{g_{t,d}(x)}{d}\longrightarrow\frac{\phi(x)}{\sqrt{2\pi}}(\sqrt{\lambda_1}x)_{+}=\frac{\sqrt{\lambda_1}}{2\pi}xe^{-x^2/2}\mathbf{1}_{\{x>0\}}=J_t(x),\qquad x\in\mathbb{R}. d g t , d ( x ) ⟶ 2 π ϕ ( x ) ( λ 1 x ) + = 2 π λ 1 x e − x 2 /2 1 { x > 0 } = J t ( x ) , x ∈ R .
Taking the ratio of two limits yields (21) . Scheffé’s theorem again proves L 1 L^1 L 1 convergence.
The endpoint includes the process X ( t ) = Z 1 cos ( ω t ) + Z 2 sin ( ω t ) X(t)=Z_1\cos(\omega t)+Z_2\sin(\omega t) X ( t ) = Z 1 cos ( ω t ) + Z 2 sin ( ω t ) , where Z 1 , Z 2 Z_1,Z_2 Z 1 , Z 2 are independent standard Gaussian variables and ω ≠ 0 \omega\ne0 ω = 0 . Its covariance is r ( s ) = cos ( ω s ) r(s)=\cos(\omega s) r ( s ) = cos ( ω s ) , η = 1 \eta=1 η = 1 and the covariance matrix of ( X ( t − d ) , X ( t ) , X ( t + d ) ) (X(t-d),X(t),X(t+d)) ( X ( t − d ) , X ( t ) , X ( t + d )) has rank two. For 0 < ∣ ω ∣ d < π 0<\lvert\omega\rvert d<\pi 0 < ∣ ω ∣ d < π , ξ d = − 1 \xi_d=-1 ξ d = − 1 exactly and p d = ∣ ω ∣ d / ( 2 π ) p_d=\lvert\omega\rvert d/(2\pi) p d = ∣ ω ∣ d / ( 2 π ) . The degenerate representation in Lemma 3.1 and Theorem 3.2 therefore covers an actual model, rather than only a limiting case of nonsingular matrices.
Corollary 3.3 (Limit of expected counts). Suppose that C C C has continuous partial derivatives through total order four on a neighborhood of the diagonal { ( t , t ) : t ∈ I } \{(t,t):t\in I\} {( t , t ) : t ∈ I } , where I = [ a , b ] I=[a,b] I = [ a , b ] , and that inf t ∈ I λ 1 ( t ) > 0 \inf_{t\in I}\lambda_1(t)>0 inf t ∈ I λ 1 ( t ) > 0 . Then, for every fixed u ∈ R u\in\mathbb{R} u ∈ R ,
E M d ( I ) ⟶ ∫ a b J t d t , E M u , d ( I ) ⟶ ∫ a b ∫ u ∞ J t ( x ) d x d t . (25) \mathbb{E}M_d(I)\longrightarrow\int_a^b J_t\,dt,\qquad\mathbb{E}M_{u,d}(I)\longrightarrow\int_a^b\int_u^\infty J_t(x)\,dx\,dt. \tag*{(25)} E M d ( I ) ⟶ ∫ a b J t d t , E M u , d ( I ) ⟶ ∫ a b ∫ u ∞ J t ( x ) d x d t . (25)
Proof. Continuity of the fourth derivatives and compactness make every Taylor remainder in the proof of Theorem 3.2 uniform over t ∈ G d ∘ t\in G_d^\circ t ∈ G d ∘ . All derivative variances are bounded there, and λ 1 ( t ) \lambda_1(t) λ 1 ( t ) is bounded away from zero. Moreover δ t 2 ≥ λ 1 ( t ) 2 \delta_t^2\ge\lambda_1(t)^2 δ t 2 ≥ λ 1 ( t ) 2 , so δ t 2 / ( 2 λ 1 ( t ) ) \delta_t^2/(2\lambda_1(t)) δ t 2 / ( 2 λ 1 ( t )) is bounded away from zero. The expansion (3.11) and the arccosine asymptotic give
sup t ∈ G d ∘ ∣ p t , d d − J t ∣ ⟶ 0. (26) \sup_{t\in G_d^\circ}\left\lvert\frac{p_{t,d}}{d}-J_t\right\rvert\longrightarrow0. \tag*{(26)} t ∈ G d ∘ sup d p t , d − J t ⟶ 0. (26)
For each fixed x x x , apply Lemma 3.1 with index θ = t \theta=t θ = t , A t , d = b t , d + x A_{t,d}=b_{t,d}^{+}x A t , d = b t , d + x , B t , d = b t , d + x B_{t,d}=b_{t,d}^{+}x B t , d = b t , d + x , and β t = τ t 2 / ( 2 λ 1 ( t ) ) \beta_t=\tau_t^2/(2\lambda_1(t)) β t = τ t 2 / ( 2 λ 1 ( t )) . Uniformity of (24) gives all the lemma’s hypotheses. Thus
sup t ∈ G d ∘ ∣ g t , d ( x ) d − J t ( x ) ∣ → 0. \sup_{t\in G_d^\circ}\left|\frac{g_{t,d}(x)}{d}-J_t(x)\right|\to0. t ∈ G d ∘ sup d g t , d ( x ) − J t ( x ) → 0.
The probability bound in Lemma 3.1 , together with uniformly bounded b t , d ± / d b_{t,d}^{\pm}/d b t , d ± / d and ( 1 + ξ t , d ) / d 2 (1+\xi_{t,d})/d^2 ( 1 + ξ t , d ) / d 2 , gives g t , d ( x ) / d ≤ K ( 1 + ∣ x ∣ ) ϕ ( x ) g_{t,d}(x)/d\le K(1+|x|)\phi(x) g t , d ( x ) / d ≤ K ( 1 + ∣ x ∣ ) ϕ ( x ) for some constant K > 0 K>0 K > 0 . The representation in the first line of (17) gives the same bound for J t ( x ) J_t(x) J t ( x ) . Hence
g t , d ( x ) d + J t ( x ) ≤ K ( 1 + ∣ x ∣ ) ϕ ( x ) \frac{g_{t,d}(x)}{d}+J_t(x)\le K(1+|x|)\phi(x) d g t , d ( x ) + J t ( x ) ≤ K ( 1 + ∣ x ∣ ) ϕ ( x )
uniformly in t , x t,x t , x and small d d d . Therefore, by the dominated convergence theorem,
sup t ∈ G d ∘ ∣ ∫ u ∞ g t , d ( x ) d d x − ∫ u ∞ J t ( x ) d x ∣ → 0. (27) \sup_{t\in G_d^\circ}\left|\int_u^\infty\frac{g_{t,d}(x)}{d}\,dx-\int_u^\infty J_t(x)\,dx\right|\to0. \tag*{(27)} t ∈ G d ∘ sup ∫ u ∞ d g t , d ( x ) d x − ∫ u ∞ J t ( x ) d x → 0. (27)
Finally,
E M d ( I ) = d ∑ t ∈ G d ∘ p t , d d , E M u , d ( I ) = d ∑ t ∈ G d ∘ ∫ u ∞ g t , d ( x ) d d x . EM_d(I)=d\sum_{t\in G_d^\circ}\frac{p_{t,d}}{d},\qquad EM_{u,d}(I)=d\sum_{t\in G_d^\circ}\int_u^\infty\frac{g_{t,d}(x)}{d}\,dx. E M d ( I ) = d t ∈ G d ∘ ∑ d p t , d , E M u , d ( I ) = d t ∈ G d ∘ ∑ ∫ u ∞ d g t , d ( x ) d x .
The functions J t J_t J t and J t ( x ) J_t(x) J t ( x ) are continuous in t t t , including where τ t = 0 \tau_t=0 τ t = 0 . The envelope also makes t ↦ ∫ u ∞ J t ( x ) d x t\mapsto\int_u^\infty J_t(x)\,dx t ↦ ∫ u ∞ J t ( x ) d x continuous. Since d ∣ G d ∘ ∣ d|G_d^\circ| d ∣ G d ∘ ∣ is bounded, the uniform limits (26) and (27) reduce both expressions to their corresponding Riemann sums. This proves the two asserted limits of expected counts in (25) .
The second limit in (25) can also be written as E M u , d ( I ) → ∫ a b H ‾ η t S M ( u ) d t EM_{u,d}(I)\to\int_a^b \overline{H}_{\eta_t}^{\mathrm{SM}}(u)\,dt E M u , d ( I ) → ∫ a b H η t SM ( u ) d t , where H ‾ η t S M \overline{H}_{\eta_t}^{\mathrm{SM}} H η t SM is the tail of the smooth peak height distribution. By [4 ] or direct integration of (21) ,
H ‾ η t S M ( u ) = { Ψ ( u 1 − η t 2 ) + 2 π η t ϕ ( u ) Φ ( η t u 1 − η t 2 ) , 0 < η t < 1 , e − ( u + ) 2 / 2 , η t = 1. \overline{H}_{\eta_t}^{\mathrm{SM}}(u)=
\begin{cases}
\Psi\left(\dfrac{u}{\sqrt{1-\eta_t^2}}\right)+\sqrt{2\pi}\eta_t\phi(u)\Phi\left(\dfrac{\eta_tu}{\sqrt{1-\eta_t^2}}\right), & 0<\eta_t<1,\\
e^{-(u_+)^2/2}, & \eta_t=1.
\end{cases} H η t SM ( u ) = ⎩ ⎨ ⎧ Ψ ( 1 − η t 2 u ) + 2 π η t ϕ ( u ) Φ ( 1 − η t 2 η t u ) , e − ( u + ) 2 /2 , 0 < η t < 1 , η t = 1.
Stationary specialization
Let X X X be stationary with covariance C ( s , t ) = r ( t − s ) C(s,t)=r(t-s) C ( s , t ) = r ( t − s ) . Omit the site subscript and write
λ 1 = − r ′ ′ ( 0 ) > 0 , λ 2 = r ( 4 ) ( 0 ) , η = λ 1 λ 2 ∈ ( 0 , 1 ] . \lambda_1=-r^{\prime\prime}(0)>0,\qquad\lambda_2=r^{(4)}(0),\qquad\eta=\frac{\lambda_1}{\sqrt{\lambda_2}}\in(0,1]. λ 1 = − r ′′ ( 0 ) > 0 , λ 2 = r ( 4 ) ( 0 ) , η = λ 2 λ 1 ∈ ( 0 , 1 ] .
Stationarity gives a = 0 a=0 a = 0 , δ 2 = λ 2 \delta^2=\lambda_2 δ 2 = λ 2 , and J = ( 2 π ) − 1 λ 2 / λ 1 J=(2\pi)^{-1}\sqrt{\lambda_2/\lambda_1} J = ( 2 π ) − 1 λ 2 / λ 1 . Consequently, Theorem 3.2 yields the following specialization.
Corollary 3.4 (Stationary smooth limit). Suppose that r r r is C 4 C^4 C 4 in a neighborhood of the origin and λ 1 > 0 \lambda_1>0 λ 1 > 0 . Then, p d / d → J p_d/d\to J p d / d → J and g d ( x ) / d → J ( x ) g_d(x)/d\to J(x) g d ( x ) / d → J ( x ) for every x ∈ R x\in\mathbb{R} x ∈ R . Consequently, h d ( x ) h_d(x) h d ( x ) converges pointwise and in L 1 ( R ) L^1(\mathbb{R}) L 1 ( R ) to the smooth peak height density
h η S M ( x ) = { 1 − η 2 ϕ ( x 1 − η 2 ) + 2 π η x ϕ ( x ) Φ ( η x 1 − η 2 ) , 0 < η < 1 , x e − x 2 / 2 1 { x > 0 } , η = 1 , (28) h_\eta^{\mathrm{SM}}(x)=
\begin{cases}
\sqrt{1-\eta^2}\,\phi\left(\dfrac{x}{\sqrt{1-\eta^2}}\right)+\sqrt{2\pi}\,\eta x\phi(x)\Phi\left(\dfrac{\eta x}{\sqrt{1-\eta^2}}\right), & 0<\eta<1,\\
xe^{-x^2/2}\mathbf{1}_{\{x>0\}}, & \eta=1,
\end{cases} \tag*{(28)} h η SM ( x ) = ⎩ ⎨ ⎧ 1 − η 2 ϕ ( 1 − η 2 x ) + 2 π η x ϕ ( x ) Φ ( 1 − η 2 η x ) , x e − x 2 /2 1 { x > 0 } , 0 < η < 1 , η = 1 , (28) and thus the discrete peak height distributions converge in total variation.
Rough Covariance and Gaussian Peak Heights
We characterize when discrete peak selection becomes asymptotically neutral with respect to height. We give a necessary and sufficient criterion for a standard Gaussian height limit. The criterion applies to general nonstationary covariance and allows the peak probability to vanish. An explicit finite-grid bound yields uniform approximations across sites. Under stationarity, the criterion reduces to a ratio of covariance increments.
We also give a complete spectral classification for a fixed stationary process. The process is assumed to be nonconstant and mean-square continuous. A finite fourth spectral moment yields the smooth height law of § 3 , whereas an infinite fourth moment yields the marginal Gaussian law.
A nonstationary criterion for Gaussian limit
At a fixed interior point t t t , let
ν t , d ± = 1 − c ± . \nu_{t,d}^{\pm}=1-c_{\pm}. ν t , d ± = 1 − c ± .
Assume − 1 < c ± < 1 -1<c_{\pm}<1 − 1 < c ± < 1 for all sufficiently small d d d , and define
Z − , d = X ( t ) − X ( t − d ) 2 ν t , d − , Z + , d = X ( t ) − X ( t + d ) 2 ν t , d + . Z_{-,d}=\frac{X(t)-X(t-d)}{\sqrt{2\nu_{t,d}^{-}}},\qquad Z_{+,d}=\frac{X(t)-X(t+d)}{\sqrt{2\nu_{t,d}^{+}}}. Z − , d = 2 ν t , d − X ( t ) − X ( t − d ) , Z + , d = 2 ν t , d + X ( t ) − X ( t + d ) .
These are standard normal with correlation q t , d q_{t,d} q t , d in (3) , and A t , d = { Z − , d > 0 , Z + , d > 0 } A_{t,d}=\{Z_{-,d}>0,Z_{+,d}>0\} A t , d = { Z − , d > 0 , Z + , d > 0 } . Moreover, q t , d > − 1 q_{t,d}>-1 q t , d > − 1 : equality would force Z − , d + Z + , d = 0 Z_{-,d}+Z_{+,d}=0 Z − , d + Z + , d = 0 almost surely, whereas its covariance with X ( t ) X(t) X ( t ) is ν t , d − / 2 + ν t , d + / 2 > 0 \sqrt{\nu_{t,d}^{-}/2}+\sqrt{\nu_{t,d}^{+}/2}>0 ν t , d − /2 + ν t , d + /2 > 0 . Thus p t , d > 0 p_{t,d}>0 p t , d > 0 by (5) .
The standardized comparison sum and its height correlation are
S t , d = Z − , d + Z + , d 2 ( 1 + q t , d ) , η t , d = Corr { X ( t ) , S t , d } = ν t , d − + ν t , d + 2 1 + q t , d . (29) S_{t,d}=\frac{Z_{-,d}+Z_{+,d}}{\sqrt{2(1+q_{t,d})}},\qquad\eta_{t,d}=\operatorname{Corr}\{X(t),S_{t,d}\}=\frac{\sqrt{\nu_{t,d}^{-}}+\sqrt{\nu_{t,d}^{+}}}{2\sqrt{1+q_{t,d}}}. \tag*{(29)} S t , d = 2 ( 1 + q t , d ) Z − , d + Z + , d , η t , d = Corr { X ( t ) , S t , d } = 2 1 + q t , d ν t , d − + ν t , d + . (29)
Under the smoothness assumptions in Theorem 3.2 ,
ν t , d ± = λ 1 ( t ) 2 d 2 + o ( d 2 ) , 1 + q t , d = δ t 2 2 λ 1 ( t ) d 2 + o ( d 2 ) , \nu_{t,d}^{\pm}=\frac{\lambda_1(t)}{2}d^2+o(d^2),\qquad1+q_{t,d}=\frac{\delta_t^2}{2\lambda_1(t)}d^2+o(d^2), ν t , d ± = 2 λ 1 ( t ) d 2 + o ( d 2 ) , 1 + q t , d = 2 λ 1 ( t ) δ t 2 d 2 + o ( d 2 ) ,
yielding that η t , d 2 → λ 1 ( t ) 2 / δ t 2 = η t 2 ∈ ( 0 , 1 ] \eta_{t,d}^2\to\lambda_1(t)^2/\delta_t^2=\eta_t^2\in(0,1] η t , d 2 → λ 1 ( t ) 2 / δ t 2 = η t 2 ∈ ( 0 , 1 ] . Thus the finite-grid parameter agrees asymptotically with the smooth parameter. Define
R t , d = ν t , d − + ν t , d + 1 + q t , d . (30) R_{t,d}=\frac{\nu_{t,d}^{-}+\nu_{t,d}^{+}}{1+q_{t,d}}. \tag*{(30)} R t , d = 1 + q t , d ν t , d − + ν t , d + . (30)
Then
R t , d 4 ≤ η t , d 2 ≤ R t , d 2 . (31) \frac{R_{t,d}}{4}\leq\eta_{t,d}^2\leq\frac{R_{t,d}}{2}. \tag*{(31)} 4 R t , d ≤ η t , d 2 ≤ 2 R t , d . (31)
Thus R t , d → 0 R_{t,d}\to0 R t , d → 0 is equivalent to loss of correlation between height and the standardized comparison sum. In the smooth regime, R t , d → 2 η t 2 > 0 R_{t,d}\to2\eta_t^2>0 R t , d → 2 η t 2 > 0 , so this dependence persists.
Theorem 4.1 (Nonstationary criterion for Gaussian limit). Fix an interior point t t t and assume − 1 < c ± < 1 -1<c_{\pm}<1 − 1 < c ± < 1 for all sufficiently small d d d . The following are equivalent as d → 0 d\to0 d → 0 :
(i) R t , d → 0 R_{t,d}\to0 R t , d → 0 ;
(ii) η t , d → 0 \eta_{t,d}\to0 η t , d → 0 ;
(iii) L { X ( t ) ∣ A t , d } ⇒ N ( 0 , 1 ) \mathcal{L}\{X(t)\mid\mathcal{A}_{t,d}\}\Rightarrow N(0,1) L { X ( t ) ∣ A t , d } ⇒ N ( 0 , 1 ) ;
(iv) h t , d ( x ) → ϕ ( x ) h_{t,d}(x)\to\phi(x) h t , d ( x ) → ϕ ( x ) for every x ∈ R x\in\mathbb{R} x ∈ R ;
(v) ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x → 0 \int_{\mathbb{R}}|h_{t,d}(x)-\phi(x)|\,\mathrm{d}x\to0 ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x → 0 .
Moreover, whenever R t , d ≤ 1 / 4 R_{t,d}\le1/4 R t , d ≤ 1/4 ,
∣ h t , d ( x ) ϕ ( x ) − 1 ∣ ≤ ( π 2 + 2 1 3 ∣ x ∣ ) R t , d , x ∈ R , (32) \left|\frac{h_{t,d}(x)}{\phi(x)}-1\right|\le\left(\frac{\pi}{2}+2\sqrt{\frac{1}{3}}|x|\right)\sqrt{R_{t,d}},\qquad x\in\mathbb{R}, \tag*{(32)} ϕ ( x ) h t , d ( x ) − 1 ≤ ( 2 π + 2 3 1 ∣ x ∣ ) R t , d , x ∈ R , (32) ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x ≤ C 0 R t , d , C 0 = π 2 + 2 2 3 < 4. (33) \int_{\mathbb{R}}|h_{t,d}(x)-\phi(x)|\,\mathrm{d}x\le C_0\sqrt{R_{t,d}},\qquad C_0=\frac{\pi}{2}+2\sqrt{\frac{2}{3}}<4. \tag*{(33)} ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x ≤ C 0 R t , d , C 0 = 2 π + 2 3 2 < 4. (33)
Proof. Conditions (i) and (ii) are equivalent by (31) . We prove the quantitative bounds first. Suppress t , d t,d t , d , let v = v − + v + v=v^{-}+v^{+} v = v − + v + , and write
ρ ± = v ± / 2 , D = ( 1 − ρ − 2 ) ( 1 − ρ + 2 ) , ε = 1 + q , e = 1 + ξ . \rho_{\pm}=\sqrt{v^{\pm}/2},\qquad D=\sqrt{(1-\rho_{-}^{2})(1-\rho_{+}^{2})},\qquad\varepsilon=1+q,\qquad e=1+\xi. ρ ± = v ± /2 , D = ( 1 − ρ − 2 ) ( 1 − ρ + 2 ) , ε = 1 + q , e = 1 + ξ .
The parameters in (4) satisfy
b ± = ρ ± 1 − ρ ± 2 , ξ = q − ρ − ρ + D , e = ε − ( 1 − D + ρ − ρ + ) D . b^{\pm}=\frac{\rho_{\pm}}{\sqrt{1-\rho_{\pm}^{2}}},\qquad\xi=\frac{q-\rho_{-}\rho_{+}}{D},\qquad e=\frac{\varepsilon-(1-D+\rho_{-}\rho_{+})}{D}. b ± = 1 − ρ ± 2 ρ ± , ξ = D q − ρ − ρ + , e = D ε − ( 1 − D + ρ − ρ + ) .
Since ε = 1 + q ≤ 2 \varepsilon=1+q\le2 ε = 1 + q ≤ 2 , the restriction R = v / ε ≤ 1 / 4 R=v/\varepsilon\le1/4 R = v / ε ≤ 1/4 gives v ≤ 1 / 2 v\le1/2 v ≤ 1/2 and D ≥ 3 / 4 D\ge3/4 D ≥ 3/4 . Also 1 − D ≤ ρ − 2 + ρ + 2 = v / 2 1-D\le\rho_{-}^{2}+\rho_{+}^{2}=v/2 1 − D ≤ ρ − 2 + ρ + 2 = v /2 , ρ − ρ + ≤ v / 4 \rho_{-}\rho_{+}\le v/4 ρ − ρ + ≤ v /4 and ρ ± 2 ≤ v / 2 ≤ 1 / 4 \rho_{\pm}^{2}\le v/2\le1/4 ρ ± 2 ≤ v /2 ≤ 1/4 . Therefore
∣ e − ε ∣ = ∣ q ( 1 − D ) − ρ − ρ + ∣ D ≤ v , ( b − + b + ) 2 ≤ 4 3 v . (34) |e-\varepsilon|=\frac{|q(1-D)-\rho_{-}\rho_{+}|}{D}\le v,\qquad(b^{-}+b^{+})^{2}\le\frac{4}{3}v. \tag*{(34)} ∣ e − ε ∣ = D ∣ q ( 1 − D ) − ρ − ρ + ∣ ≤ v , ( b − + b + ) 2 ≤ 3 4 v . (34)
Let F ( s ) = arccos ( 1 − s ) / ( 2 π ) F(s)=\arccos(1-s)/(2\pi) F ( s ) = arccos ( 1 − s ) / ( 2 π ) for 0 ≤ s ≤ 2 0\le s\le2 0 ≤ s ≤ 2 . The orthant identity gives p t , d = F ( ε ) p_{t,d}=F(\varepsilon) p t , d = F ( ε ) and Φ 2 ( 0 , 0 ; ξ ) = F ( e ) \Phi_{2}(0,0;\xi)=F(e) Φ 2 ( 0 , 0 ; ξ ) = F ( e ) . For s ∈ [ 0 , 2 ] s\in[0,2] s ∈ [ 0 , 2 ] ,
F ( s ) ≥ 2 s 2 π , ∣ arccos u − arccos w ∣ ≤ π 2 ∣ u − w ∣ , u , w ∈ [ − 1 , 1 ] . F(s)\ge\frac{\sqrt{2s}}{2\pi},\qquad|\arccos u-\arccos w|\le\frac{\pi}{\sqrt{2}}\sqrt{|u-w|},\qquad u,w\in[-1,1]. F ( s ) ≥ 2 π 2 s , ∣ arccos u − arccos w ∣ ≤ 2 π ∣ u − w ∣ , u , w ∈ [ − 1 , 1 ] .
The first bound follows from 1 − cos y ≤ y 2 / 2 1-\cos y\le y^{2}/2 1 − cos y ≤ y 2 /2 . For the second, write A = arccos u A=\arccos u A = arccos u , B = arccos w B=\arccos w B = arccos w , and δ = ∣ A − B ∣ \delta=|A-B| δ = ∣ A − B ∣ ; then ∣ u − w ∣ ≥ 2 sin 2 ( δ / 2 ) ≥ 2 δ 2 / π 2 |u-w|\ge2\sin^{2}(\delta/2)\ge2\delta^{2}/\pi^{2} ∣ u − w ∣ ≥ 2 sin 2 ( δ /2 ) ≥ 2 δ 2 / π 2 . Consequently,
∣ Φ 2 ( 0 , 0 ; ξ ) p t , d − 1 ∣ ≤ 1 p t , d 1 2 π π 2 ∣ e − ε ∣ ≤ π 2 R . (35) \left|\frac{\Phi_{2}(0,0;\xi)}{p_{t,d}}-1\right|\le\frac{1}{p_{t,d}}\frac{1}{2\pi}\frac{\pi}{\sqrt{2}}\sqrt{|e-\varepsilon|}\le\frac{\pi}{2}\sqrt{R}. \tag*{(35)} p t , d Φ 2 ( 0 , 0 ; ξ ) − 1 ≤ p t , d 1 2 π 1 2 π ∣ e − ε ∣ ≤ 2 π R . (35)
The change from zero thresholds to ( b − x , b + x ) (b^{-}x,b^{+}x) ( b − x , b + x ) is contained in the two marginal strips. Since standard normal marginal densities are bounded by ϕ ( 0 ) \phi(0) ϕ ( 0 ) ,
∣ Φ 2 ( b − x , b + x ; ξ ) − Φ 2 ( 0 , 0 ; ξ ) ∣ ≤ ϕ ( 0 ) ∣ x ∣ ( b − + b + ) . |\Phi_{2}(b^{-}x,b^{+}x;\xi)-\Phi_{2}(0,0;\xi)|\le\phi(0)|x|(b^{-}+b^{+}). ∣ Φ 2 ( b − x , b + x ; ξ ) − Φ 2 ( 0 , 0 ; ξ ) ∣ ≤ ϕ ( 0 ) ∣ x ∣ ( b − + b + ) .
Dividing by p t , d ≥ ε / ( π 2 ) p_{t,d} \ge\sqrt{\varepsilon/(\pi\sqrt{2})} p t , d ≥ ε / ( π 2 ) and using (4.6) bounds this relative error by 2 π / 3 ∣ x ∣ R 2\sqrt{\pi/3}|x|\sqrt{\mathcal{R}} 2 π /3 ∣ x ∣ R . Together with (4.7) and (2.5), this proves (4.4). Integration against ϕ \phi ϕ , using ∫ R ∣ x ∣ ϕ ( x ) d x = 2 / π \int_{\mathbb{R}} |x|\phi(x)\,\mathrm{d}x = \sqrt{2/\pi} ∫ R ∣ x ∣ ϕ ( x ) d x = 2/ π , proves (4.5).
Under (i), these bounds prove (iv) and (v). Also, (iv) implies (v) by Scheffé’s theorem, and (v) implies (iii), with
d T V ( L { X ( t ) ∣ A t , d } , N ( 0 , 1 ) ) = 1 2 ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x . (36) d_{\mathrm{TV}}\bigl(\mathcal{L}\{X(t)\mid A_{t,d}\},N(0,1)\bigr)=\frac{1}{2}\int_{\mathbb{R}}|h_{t,d}(x)-\phi(x)|\,\mathrm{d}x. \tag*{(36)} d TV ( L { X ( t ) ∣ A t , d } , N ( 0 , 1 ) ) = 2 1 ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x . (36)
Finally, suppose (iii) holds. Suppress t , d t,d t , d , write S = S t , d S=S_{t,d} S = S t , d and η = η t , d \eta=\eta_{t,d} η = η t , d , and first take q < 1 q<1 q < 1 . The variable T = ( Z − , d − Z + , d ) / 2 ( 1 − q ) T=(Z_{-,d}-Z_{+,d})/\sqrt{2(1-q)} T = ( Z − , d − Z + , d ) / 2 ( 1 − q ) is standard normal and independent of S S S . The Gaussian conditioning formula gives
X ( t ) = η S + κ T + σ G , κ = Corr { X ( t ) , T } = ρ − − ρ + 2 ( 1 − q ) , σ 2 = 1 − η 2 − κ 2 ≥ 0 , X(t)=\eta S+\kappa T+\sigma G,\qquad\kappa=\operatorname{Corr}\{X(t),T\}=\frac{\rho_{-}-\rho_{+}}{\sqrt{2(1-q)}},\qquad\sigma^2=1-\eta^2-\kappa^2\ge0, X ( t ) = η S + κ T + σ G , κ = Corr { X ( t ) , T } = 2 ( 1 − q ) ρ − − ρ + , σ 2 = 1 − η 2 − κ 2 ≥ 0 ,
with G G G independent standard normal; the formula allows σ = 0 \sigma=0 σ = 0 . The peak event can be written as A t , d = { S > 0 , ∣ T ∣ < ( tan ϑ ) S } A_{t,d}=\{S>0,\ |T|<(\tan\vartheta)S\} A t , d = { S > 0 , ∣ T ∣ < ( tan ϑ ) S } , where
ϑ = arctan 1 + q 1 − q ∈ ( 0 , π / 2 ) . \vartheta=\arctan\sqrt{\frac{1+q}{1-q}}\in(0,\pi/2). ϑ = arctan 1 − q 1 + q ∈ ( 0 , π /2 ) .
In polar coordinates S = R cos α S=\mathcal{R}\cos\alpha S = R cos α and T = R sin α T=\mathcal{R}\sin\alpha T = R sin α , the peak event conditioning restricts the angle α \alpha α uniform on ( − ϑ , ϑ ) (-\vartheta,\vartheta) ( − ϑ , ϑ ) and leaves the independent radius R \mathcal{R} R unchanged. Since R \mathcal{R} R has Rayleigh distribution with E R = π / 2 \mathbb{E}\mathcal{R}=\sqrt{\pi/2} E R = π /2 and E R 2 = 2 \mathbb{E}\mathcal{R}^2=2 E R 2 = 2 , symmetry and angular integration give
E { X ( t ) ∣ A t , d } = η E R E { cos α ∣ ∣ α ∣ < ϑ } = η π 2 sin ϑ ϑ ≥ 2 π η . (37) \mathbb{E}\{X(t)\mid A_{t,d}\}=\eta\,\mathbb{E}\mathcal{R}\,\mathbb{E}\{\cos\alpha\mid|\alpha|<\vartheta\}=\eta\sqrt{\frac{\pi}{2}}\frac{\sin\vartheta}{\vartheta}\ge\sqrt{\frac{2}{\pi}}\,\eta. \tag*{(37)} E { X ( t ) ∣ A t , d } = η E R E { cos α ∣ ∣ α ∣ < ϑ } = η 2 π ϑ sin ϑ ≥ π 2 η . (37)
Also, Cauchy–Schwarz yields
E { X ( t ) 2 ∣ A t , d } ≤ ( η 2 + κ 2 ) E ( S 2 + T 2 ∣ A t , d ) + σ 2 = 2 ( η 2 + κ 2 ) + σ 2 ≤ 2. \mathbb{E}\{X(t)^2\mid A_{t,d}\}\le(\eta^2+\kappa^2)\mathbb{E}(S^2+T^2\mid A_{t,d})+\sigma^2=2(\eta^2+\kappa^2)+\sigma^2\le2. E { X ( t ) 2 ∣ A t , d } ≤ ( η 2 + κ 2 ) E ( S 2 + T 2 ∣ A t , d ) + σ 2 = 2 ( η 2 + κ 2 ) + σ 2 ≤ 2.
If q = 1 q=1 q = 1 , then Z − , d = Z + , d Z_{-,d}=Z_{+,d} Z − , d = Z + , d almost surely and A t , d = { S > 0 } A_{t,d}=\{S>0\} A t , d = { S > 0 } with S = Z − , d = Z + , d S=Z_{-,d}=Z_{+,d} S = Z − , d = Z + , d . The formula of Gaussian conditional on S S S gives conditional mean 2 / π η \sqrt{2/\pi}\,\eta 2/ π η and second moment 1 1 1 . Thus the same bounds hold for all possible q q q . The second-moment bound ensures uniform integrability, so (iii) implies E { X ( t ) ∣ A t , d } → 0 \mathbb{E}\{X(t)\mid A_{t,d}\}\to0 E { X ( t ) ∣ A t , d } → 0 . The mean bound in (4.9) then gives η t , d → 0 \eta_{t,d}\to0 η t , d → 0 , proving (ii) and completing the equivalence.
Remark 4.2 (A unified family of limiting height densities). For fixed t t t , recall the smooth peak height density in (3.9)
h η t S M ( x ) = 1 − η t 2 ϕ ( x 1 − η t 2 ) + 2 π η t x ϕ ( x ) Φ ( η t x 1 − η t 2 ) , 0 < η t < 1. h_{\eta_t}^{\mathrm{SM}}(x)=\sqrt{1-\eta_t^2}\,\phi\left(\frac{x}{\sqrt{1-\eta_t^2}}\right)+\sqrt{2\pi}\,\eta_t x\phi(x)\Phi\left(\frac{\eta_t x}{\sqrt{1-\eta_t^2}}\right),\qquad0<\eta_t<1. h η t SM ( x ) = 1 − η t 2 ϕ ( 1 − η t 2 x ) + 2 π η t x ϕ ( x ) Φ ( 1 − η t 2 η t x ) , 0 < η t < 1.
Viewed as a family indexed by η t \eta_t η t , these densities have the pointwise endpoint limits
lim η t ↓ 0 h η t S M ( x ) = ϕ ( x ) , lim η t ↑ 1 h η t S M ( x ) = x e − x 2 / 2 1 { x > 0 } , x ∈ R . \lim_{\eta_t\downarrow0}h_{\eta_t}^{\mathrm{SM}}(x)=\phi(x),\qquad\lim_{\eta_t\uparrow1}h_{\eta_t}^{\mathrm{SM}}(x)=xe^{-x^2/2}\mathbf{1}_{\{x>0\}},\qquad x\in\mathbb{R}. η t ↓ 0 lim h η t SM ( x ) = ϕ ( x ) , η t ↑ 1 lim h η t SM ( x ) = x e − x 2 /2 1 { x > 0 } , x ∈ R .
Define h η t S M h_{\eta_t}^{\mathrm{SM}} h η t SM and h 1 S M h_1^{\mathrm{SM}} h 1 SM by these limits. Since the endpoint limits are probability densities, Scheffé’s theorem also gives convergence in L 1 ( R ) L^1(\mathbb{R}) L 1 ( R ) and hence in total variation.
The extended family { h η t S M : 0 ≤ η t ≤ 1 } \{h_{\eta_t}^{\mathrm{SM}}: 0 \le\eta_t \le1\} { h η t SM : 0 ≤ η t ≤ 1 } therefore unifies the Gaussian, smooth, and Rayleigh limiting height laws established in this paper. In the smooth nonstationary regime, the limiting density is h η t S M h_{\eta_t}^{\mathrm{SM}} h η t SM , where η t ∈ ( 0 , 1 ] \eta_t \in(0,1] η t ∈ ( 0 , 1 ] . The endpoint η t = 1 \eta_t=1 η t = 1 corresponds to the Rayleigh distribution. The Gaussian law is the endpoint extension at η t = 0 \eta_t=0 η t = 0 . The covariance assumptions in the corresponding infill theorems determine which member of the family arises.
Corollary 4.4 (Gaussian limit with positive peak probability). Suppose c ± → 1 c_{\pm}\to1 c ± → 1 , 1 − c ± > 0 1-c_{\pm}>0 1 − c ± > 0 for all sufficiently small d d d , and q t , d → q t ∈ ( − 1 , 1 ] q_{t,d}\to q_t\in(-1,1] q t , d → q t ∈ ( − 1 , 1 ] . Then
p t , d → 1 4 + arcsin q t 2 π > 0 , h t , d ( x ) → ϕ ( x ) , x ∈ R , p_{t,d}\to\frac{1}{4}+\frac{\arcsin q_t}{2\pi}>0,\qquad h_{t,d}(x)\to\phi(x),\quad x\in\mathbb{R}, p t , d → 4 1 + 2 π arcsin q t > 0 , h t , d ( x ) → ϕ ( x ) , x ∈ R , and the density convergence also holds in L 1 L^1 L 1 .
Proof. The assumptions imply − 1 < c ± < 1 -1<c_{\pm}<1 − 1 < c ± < 1 , while the numerator of R t , d R_{t,d} R t , d tends to zero and its denominator tends to 1 + q t > 0 1+q_t>0 1 + q t > 0 . The results follow directly from Theorem 4.1 and (5) . □
For example, if locally
c ± = 1 − a ± d α + o ( d α ) , c 0 = 1 − b d α + o ( d α ) , a ± > 0 , c_{\pm}=1-a_{\pm}d^{\alpha}+o(d^{\alpha}),\qquad c_0=1-bd^{\alpha}+o(d^{\alpha}),\qquad a_{\pm}>0, c ± = 1 − a ± d α + o ( d α ) , c 0 = 1 − b d α + o ( d α ) , a ± > 0 ,
then q t , d → ( a − + a + − b ) / ( 2 a − a + ) q_{t,d}\to(a_-+a_+-b)/(2\sqrt{a_-a_+}) q t , d → ( a − + a + − b ) / ( 2 a − a + ) . Corollary 4.4 applies when this limit exceeds − 1 -1 − 1 . If q t , d → − 1 q_{t,d}\to-1 q t , d → − 1 , Theorem 4.1 still applies provided v t , d − + v t , d + = o ( 1 + q t , d ) v_{t,d}^{-}+v_{t,d}^{+}=o(1+q_{t,d}) v t , d − + v t , d + = o ( 1 + q t , d ) .
Corollary 4.5 (Uniform sitewise Gaussian approximations). For each sufficiently small d d d , let T d \mathcal{T}_d T d be a nonempty set of sites with t , t ± d ∈ I t,t\pm d\in I t , t ± d ∈ I satisfying − 1 < c ± < 1 -1<c_{\pm}<1 − 1 < c ± < 1 , and suppose
R d ∗ : = sup t ∈ T d R t , d → 0. R_d^*:=\sup_{t\in\mathcal{T}_d}R_{t,d}\to0. R d ∗ := t ∈ T d sup R t , d → 0. Then the density convergence in Theorem 4.1 is uniform across t ∈ T d t\in\mathcal{T}_d t ∈ T d , both in L 1 L^1 L 1 and in absolute error on R \mathbb{R} R . For sufficiently small d d d ,
sup t ∈ T d ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x ≤ C 0 R d ∗ , \sup_{t\in\mathcal{T}_d}\int_{\mathbb{R}}|h_{t,d}(x)-\phi(x)|\,\mathrm{d}x\le C_0\sqrt{R_d^*}, t ∈ T d sup ∫ R ∣ h t , d ( x ) − ϕ ( x ) ∣ d x ≤ C 0 R d ∗ , sup t ∈ T d , u ∈ R ∣ H ‾ t , d ( u ) − Ψ ( u ) ∣ ≤ C 0 2 R d ∗ . \sup_{t\in\mathcal{T}_d,\,u\in\mathbb{R}}|\overline{H}_{t,d}(u)-\Psi(u)|\le\frac{C_0}{2}\sqrt{R_d^*}. t ∈ T d , u ∈ R sup ∣ H t , d ( u ) − Ψ ( u ) ∣ ≤ 2 C 0 R d ∗ . Proof. Eventually R d ∗ ≤ 1 / 4 R_d^*\le1/4 R d ∗ ≤ 1/4 , so apply (32) –(33) uniformly in t t t . The survival error is bounded by the total variation distance in (36) . □
The stationary criterion and height–curvature correlation
For a stationary, unit-variance process, let
V ( d ) = 1 − r ( d ) , Δ ( d ) = 4 V ( d ) − V ( 2 d ) . V(d)=1-r(d),\qquad\Delta(d)=4V(d)-V(2d). V ( d ) = 1 − r ( d ) , Δ ( d ) = 4 V ( d ) − V ( 2 d ) .
For the central second difference D d = X ( d ) − 2 X ( 0 ) + X ( − d ) D_d=X(d)-2X(0)+X(-d) D d = X ( d ) − 2 X ( 0 ) + X ( − d ) ,
Var ( D d ) = 2 Δ ( d ) , Cov { X ( 0 ) , D d } = − 2 V ( d ) . \operatorname{Var}(D_d)=2\Delta(d),\qquad\operatorname{Cov}\{X(0),D_d\}=-2V(d). Var ( D d ) = 2Δ ( d ) , Cov { X ( 0 ) , D d } = − 2 V ( d ) .
Thus Δ ( d ) \Delta(d) Δ ( d ) is one half of the second-difference variance, and Cauchy–Schwarz gives Δ ( d ) ≥ 2 V ( d ) 2 \Delta(d)\ge2V(d)^2 Δ ( d ) ≥ 2 V ( d ) 2 . When V ( d ) > 0 V(d)>0 V ( d ) > 0 , define
η d = − Corr { X ( 0 ) , D d } = 2 V ( d ) Δ ( d ) ∈ ( 0 , 1 ] . \eta_d=-\operatorname{Corr}\{X(0),D_d\}=\frac{\sqrt{2}V(d)}{\sqrt{\Delta(d)}}\in(0,1]. η d = − Corr { X ( 0 ) , D d } = Δ ( d ) 2 V ( d ) ∈ ( 0 , 1 ] .
This is the stationary specialization of (4.1) and (4.2):
η t , d = η d , R t , d = 4 V ( d ) 2 Δ ( d ) = 2 η d 2 . (39) \eta_{t,d}=\eta_d,\qquad R_{t,d}=\frac{4V(d)^2}{\Delta(d)}=2\eta_d^2. \tag*{(39)} η t , d = η d , R t , d = Δ ( d ) 4 V ( d ) 2 = 2 η d 2 . (39)
Corollary 4.7 (Stationary Gaussian-limit characterization). Suppose − 1 < r ( d ) < 1 -1<r(d)<1 − 1 < r ( d ) < 1 for all sufficiently small d d d . Then Δ ( d ) > 0 \Delta(d)>0 Δ ( d ) > 0 , and the condition
V ( d ) 2 Δ ( d ) → 0 (40) \frac{V(d)^2}{\Delta(d)}\to0 \tag*{(40)} Δ ( d ) V ( d ) 2 → 0 (40) is equivalent to weak convergence of the discrete peak height distributions to N ( 0 , 1 ) N(0,1) N ( 0 , 1 ) , to pointwise convergence h d ( x ) → ϕ ( x ) h_d(x)\to\phi(x) h d ( x ) → ϕ ( x ) , and to L 1 L^1 L 1 convergence of these densities. The quantitative bounds of Theorem 4.1 apply with R d = 4 V ( d ) 2 / Δ ( d ) R_d=4V(d)^2/\Delta(d) R d = 4 V ( d ) 2 /Δ ( d ) .
Proof. The results are direct consequences of Theorem 4.1 and (4.11).
The criterion in (4.12) is equivalent to η d → 0 \eta_d\to0 η d → 0 , showing that discrete curvature becomes asymptotically uncorrelated with the height.
The fourth spectral moment boundary
Assume that r r r is continuous at the origin, equivalently that X X X is mean-square continuous. By Bochner’s theorem, its symmetric spectral probability measure F F F satisfies
r ( s ) = ∫ R cos ( s λ ) F ( d λ ) . r(s)=\int_{\mathbb{R}}\cos(s\lambda)F(\mathrm{d}\lambda). r ( s ) = ∫ R cos ( s λ ) F ( d λ ) .
Letting Y d ( λ ) = 1 − cos ( d λ ) Y_d(\lambda)=1-\cos(d\lambda) Y d ( λ ) = 1 − cos ( d λ ) , we have
V ( d ) = ∫ R Y d d F , Δ ( d ) = 2 ∫ R Y d 2 d F , η d 2 = { ∫ R Y d d F } 2 ∫ R Y d 2 d F . (41) V(d)=\int_{\mathbb{R}}Y_d\,\mathrm{d}F,\qquad\Delta(d)=2\int_{\mathbb{R}}Y_d^2\,\mathrm{d}F,\qquad\eta_d^2=\frac{\left\{\int_{\mathbb{R}}Y_d\,\mathrm{d}F\right\}^2}{\int_{\mathbb{R}}Y_d^2\,\mathrm{d}F}. \tag*{(41)} V ( d ) = ∫ R Y d d F , Δ ( d ) = 2 ∫ R Y d 2 d F , η d 2 = ∫ R Y d 2 d F { ∫ R Y d d F } 2 . (41)
Denote by m j = ∫ R λ j F ( d λ ) m_j=\int_{\mathbb{R}}\lambda^jF(\mathrm{d}\lambda) m j = ∫ R λ j F ( d λ ) the j j j -th spectral moment.
Theorem 4.8 (Fourth spectral moment classification). Assume that X X X is mean-square continuous and stationary, and is nonconstant, equivalently F ≠ δ 0 F\ne\delta_0 F = δ 0 or r ≢ 1 r\not\equiv1 r ≡ 1 . Then V ( d ) V(d) V ( d ) and Δ ( d ) \Delta(d) Δ ( d ) are positive for all sufficiently small d d d , and exactly one of the following alternatives holds:
If m 4 < ∞ m_4<\infty m 4 < ∞ , then 0 < m 2 < ∞ 0<m_2<\infty 0 < m 2 < ∞ , r ∈ C 4 r\in C^4 r ∈ C 4 , and
η d → η = m 2 m 4 ∈ ( 0 , 1 ] , p d d → 1 2 π m 4 m 2 , h d ( x ) → h η S M ( x ) , x ∈ R . \eta_d\to\eta=\frac{m_2}{\sqrt{m_4}}\in(0,1],\qquad\frac{p_d}{d}\to\frac{1}{2\pi}\sqrt{\frac{m_4}{m_2}},\qquad h_d(x)\to h_\eta^{\mathrm{SM}}(x),\quad x\in\mathbb{R}. η d → η = m 4 m 2 ∈ ( 0 , 1 ] , d p d → 2 π 1 m 2 m 4 , h d ( x ) → h η SM ( x ) , x ∈ R . If m 4 = ∞ m_4=\infty m 4 = ∞ , then η d → 0 \eta_d\to0 η d → 0 and h d ( x ) → ϕ ( x ) h_d(x)\to\phi(x) h d ( x ) → ϕ ( x ) for every x ∈ R x\in\mathbb{R} x ∈ R .
In both cases the density convergence also holds in L 1 L^1 L 1 , and hence in total variation.
Proof. First, V ( d ) → 0 V(d)\to0 V ( d ) → 0 by dominated convergence. Nonconstancy implies that Δ ( d ) > 0 \Delta(d)>0 Δ ( d ) > 0 for all sufficiently small d d d . Otherwise, along a sequence d n ↓ 0 d_n\downarrow0 d n ↓ 0 , the nonnegative integrand in (41) would give d n λ ∈ 2 π Z d_n\lambda\in2\pi\mathbb{Z} d n λ ∈ 2 π Z for every n n n , for F F F -almost every λ \lambda λ . Since d n λ → 0 d_n\lambda\to0 d n λ → 0 , this forces λ = 0 \lambda=0 λ = 0 , contradicting nonconstancy. Moreover, Δ ( d ) > 0 \Delta(d)>0 Δ ( d ) > 0 implies V ( d ) > 0 V(d)>0 V ( d ) > 0 , for all sufficiently small d d d , through the same spectral identities.
Suppose first that m 4 < ∞ m_4<\infty m 4 < ∞ . Since
0 ≤ Y d ( λ ) d 2 ≤ λ 2 2 , 0 ≤ 2 Y d ( λ ) 2 d 4 ≤ λ 4 2 , 0\le\frac{Y_d(\lambda)}{d^2}\le\frac{\lambda^2}{2},\qquad0\le\frac{2Y_d(\lambda)^2}{d^4}\le\frac{\lambda^4}{2}, 0 ≤ d 2 Y d ( λ ) ≤ 2 λ 2 , 0 ≤ d 4 2 Y d ( λ ) 2 ≤ 2 λ 4 ,
dominated convergence gives
V ( d ) d 2 → m 2 2 , Δ ( d ) d 4 → m 4 2 , η d = 2 V ( d ) Δ ( d ) → m 2 m 4 = η . \frac{V(d)}{d^2}\to\frac{m_2}{2},\qquad\frac{\Delta(d)}{d^4}\to\frac{m_4}{2},\qquad\eta_d=\frac{\sqrt{2V(d)}}{\sqrt{\Delta(d)}}\to\frac{m_2}{\sqrt{m_4}}=\eta. d 2 V ( d ) → 2 m 2 , d 4 Δ ( d ) → 2 m 4 , η d = Δ ( d ) 2 V ( d ) → m 4 m 2 = η .
Nonconstancy gives m 2 > 0 m_2>0 m 2 > 0 , and m 2 2 ≤ m 4 m_2^2\le m_4 m 2 2 ≤ m 4 by Cauchy–Schwarz. Differentiation under the spectral integral gives r ∈ C 4 r\in C^4 r ∈ C 4 , with − r ′ ′ ( 0 ) = m 2 -r^{\prime\prime}(0)=m_2 − r ′′ ( 0 ) = m 2 and r ( 4 ) ( 0 ) = m 4 r^{(4)}(0)=m_4 r ( 4 ) ( 0 ) = m 4 . The asserted probability and density limits now follow from Corollary 3.4 , including the degenerate endpoint m 4 = m 2 2 m_4=m_2^2 m 4 = m 2 2 .
Now suppose that m 4 = ∞ m_4=\infty m 4 = ∞ . We first prove that η d → 0 \eta_d\to0 η d → 0 . Otherwise, there would exist ϵ > 0 \epsilon>0 ϵ > 0 and a sequence d n ↓ 0 d_n\downarrow0 d n ↓ 0 such that η d n ≥ ϵ \eta_{d_n}\ge\epsilon η d n ≥ ϵ . Define W n ( λ ) = Y d n ( λ ) / V ( d n ) W_n(\lambda)=Y_{d_n}(\lambda)/V(d_n) W n ( λ ) = Y d n ( λ ) / V ( d n ) . Then
∫ R W n d F = 1 , ∫ R W n 2 d F = η d n − 2 ≤ ϵ − 2 , (42) \int_{\mathbb{R}}W_n\,\mathrm{d}F=1,\qquad\int_{\mathbb{R}}W_n^2\,\mathrm{d}F=\eta_{d_n}^{-2}\le\epsilon^{-2}, \tag*{(42)} ∫ R W n d F = 1 , ∫ R W n 2 d F = η d n − 2 ≤ ϵ − 2 , (42)
so { W n } \{W_n\} { W n } is uniformly integrable. If m 2 = ∞ m_2=\infty m 2 = ∞ , Fatou’s lemma gives
lim inf n → ∞ V ( d n ) d n 2 ≥ 1 2 ∫ R λ 2 F ( d λ ) = ∞ . \liminf_{n\to\infty}\frac{V(d_n)}{d_n^2}\ge\frac{1}{2}\int_{\mathbb{R}}\lambda^2F(\mathrm{d}\lambda)=\infty. n → ∞ lim inf d n 2 V ( d n ) ≥ 2 1 ∫ R λ 2 F ( d λ ) = ∞.
Since Y d n ( λ ) / d n 2 → λ 2 / 2 Y_{d_n}(\lambda)/d_n^2\to\lambda^2/2 Y d n ( λ ) / d n 2 → λ 2 /2 for every fixed λ \lambda λ , it follows that W n ( λ ) → 0 W_n(\lambda)\to0 W n ( λ ) → 0 for almost every λ \lambda λ . Uniform integrability would then imply ∫ W n d F → 0 \int W_n\,\mathrm{d}F\to0 ∫ W n d F → 0 , contradicting ∫ W n d F = 1 \int W_n\,\mathrm{d}F=1 ∫ W n d F = 1 . Thus m 2 < ∞ m_2<\infty m 2 < ∞ , and dominated convergence gives V ( d n ) / d n 2 → m 2 / 2 V(d_n)/d_n^2\to m_2/2 V ( d n ) / d n 2 → m 2 /2 . But
∫ R { Y d n ( λ ) d n 2 } 2 F ( d λ ) = { V ( d n ) / d n 2 } 2 η d n 2 \int_{\mathbb{R}}\left\{\frac{Y_{d_n}(\lambda)}{d_n^2}\right\}^2F(\mathrm{d}\lambda)=\frac{\{V(d_n)/d_n^2\}^2}{\eta_{d_n}^2} ∫ R { d n 2 Y d n ( λ ) } 2 F ( d λ ) = η d n 2 { V ( d n ) / d n 2 } 2
is bounded. Fatou’s lemma would therefore give
m 4 4 ≤ lim inf n → ∞ ∫ R { Y d n ( λ ) d n 2 } 2 F ( d λ ) < ∞ , \frac{m_4}{4}\le\liminf_{n\to\infty}\int_{\mathbb{R}}\left\{\frac{Y_{d_n}(\lambda)}{d_n^2}\right\}^2F(\mathrm{d}\lambda)<\infty, 4 m 4 ≤ n → ∞ lim inf ∫ R { d n 2 Y d n ( λ ) } 2 F ( d λ ) < ∞ ,
contradicting m 4 = ∞ m_4=\infty m 4 = ∞ . Hence η d → 0 \eta_d\to0 η d → 0 , or equivalently V ( d ) 2 / Δ ( d ) → 0 V(d)^2/\Delta(d)\to0 V ( d ) 2 /Δ ( d ) → 0 . Corollary 4.7 now gives the Gaussian limit and its L 1 L^1 L 1 convergence.
Remark 4.9. Under the assumptions of Theorem 4.8 , a positive limiting value of η d \eta_d η d requires m 4 < ∞ m_4<\infty m 4 < ∞ . The covariance then belongs to C 4 C^4 C 4 , and the limiting parameter is η = m 2 / m 4 ∈ ( 0 , 1 ] \eta=m_2/\sqrt{m_4}\in(0,1] η = m 2 / m 4 ∈ ( 0 , 1 ] . If m 4 = ∞ m_4=\infty m 4 = ∞ , then η d → 0 \eta_d\to0 η d → 0 and the limiting height law is Gaussian. Finiteness of the fourth spectral moment therefore exactly separates the two regimes for each fixed nonconstant, mean-square continuous stationary process.
Remark 4.2 connects these limits within the same continuous family with the Gaussian density at η = 0 \eta=0 η = 0 . This interpolation describes variation across covariance models. At η = 1 \eta=1 η = 1 , equality m 4 = m 2 2 m_4=m_2^2 m 4 = m 2 2 forces spectral support on { ± m 2 } \{\pm\sqrt{m_2}\} { ± m 2 } , so r ( s ) = cos ( m 2 s ) r(s)=\cos(\sqrt{m_2}s) r ( s ) = cos ( m 2 s ) . The conditional curvature variance vanishes, while the limiting height law is the nondegenerate Rayleigh law.
Corollary 4.10 (Divergence of expected peak counts in the rough regime). Under the assumptions of Theorem 4.8, if m 4 = ∞ m_4=\infty m 4 = ∞ , then p d / d → ∞ p_d/d\to\infty p d / d → ∞ . On an interval I I I of length T > 0 T>0 T > 0 , for every fixed u ∈ R u\in\mathbb{R} u ∈ R ,
E M d ( I ) → ∞ , E M u , d ( I ) → ∞ , E M u , d ( I ) E M d ( I ) → Ψ ( u ) . \mathbb{E}M_d(I)\to\infty,\qquad\mathbb{E}M_{u,d}(I)\to\infty,\qquad\frac{\mathbb{E}M_{u,d}(I)}{\mathbb{E}M_d(I)}\to\Psi(u). E M d ( I ) → ∞ , E M u , d ( I ) → ∞ , E M d ( I ) E M u , d ( I ) → Ψ ( u ) .
Proof. Let ϵ d = Δ ( d ) / ( 2 V ( d ) ) ∈ ( 0 , 2 ] \epsilon_d=\Delta(d)/(2V(d))\in(0,2] ϵ d = Δ ( d ) / ( 2 V ( d )) ∈ ( 0 , 2 ] . The orthant formula and cos z ≥ 1 − z 2 / 2 \cos z\ge1-z^2/2 cos z ≥ 1 − z 2 /2 give
p d d = arccos ( 1 − ϵ d ) 2 π d ≥ 2 ϵ d 2 π d . \frac{p_d}{d}=\frac{\arccos(1-\epsilon_d)}{2\pi d}\ge\frac{\sqrt{2\epsilon_d}}{2\pi d}. d p d = 2 π d arccos ( 1 − ϵ d ) ≥ 2 π d 2 ϵ d .
If m 2 = ∞ m_2=\infty m 2 = ∞ , Fatou’s lemma gives V ( d ) / d 2 → ∞ V(d)/d^2\to\infty V ( d ) / d 2 → ∞ , and ϵ d ≥ V ( d ) \epsilon_d\ge V(d) ϵ d ≥ V ( d ) implies ϵ d / d 2 → ∞ \epsilon_d/d^2\to\infty ϵ d / d 2 → ∞ . If 0 < m 2 < ∞ 0<m_2<\infty 0 < m 2 < ∞ , then V ( d ) / d 2 → m 2 / 2 V(d)/d^2\to m_2/2 V ( d ) / d 2 → m 2 /2 , whereas Fatou’s lemma applied to the second identity in (41) gives Δ ( d ) / d 4 → ∞ \Delta(d)/d^4\to\infty Δ ( d ) / d 4 → ∞ . Again ϵ d / d 2 → ∞ \epsilon_d/d^2\to\infty ϵ d / d 2 → ∞ . Thus p d / d → ∞ p_d/d\to\infty p d / d → ∞ in either case. With N d = ∣ G d ∘ ∣ = T / d + O ( 1 ) N_d=|\mathcal{G}_d^\circ|=T/d+O(1) N d = ∣ G d ∘ ∣ = T / d + O ( 1 ) , stationarity yields E M d ( I ) = N d p d \mathbb{E}M_d(I)=N_dp_d E M d ( I ) = N d p d and
E M u , d ( I ) E M d ( I ) = ∫ u ∞ h d ( x ) d x → Ψ ( u ) \frac{\mathbb{E}M_{u,d}(I)}{\mathbb{E}M_d(I)}=\int_u^\infty h_d(x)\,\mathrm{d}x\to\Psi(u) E M d ( I ) E M u , d ( I ) = ∫ u ∞ h d ( x ) d x → Ψ ( u )
by total variation convergence. Since Ψ ( u ) > 0 \Psi(u)>0 Ψ ( u ) > 0 for finite u u u , both expected counts diverge.
Regular variation and subquartic covariance expansions
A positive measurable function L L L is slowly varying at zero if L ( s d ) / L ( d ) → 1 L(sd)/L(d) \to1 L ( s d ) / L ( d ) → 1 as d ↓ 0 d \downarrow0 d ↓ 0 for every s > 0 s > 0 s > 0 .
Corollary 4.11 (Nondifferentiable regular variation regime). Suppose
V ( d ) = 1 − r ( d ) ∼ c d α L ( d ) , c > 0 , 0 < α < 2 , (43) V(d) = 1-r(d) \sim cd^\alpha L(d), \qquad c>0,\quad0<\alpha<2, \tag*{(43)} V ( d ) = 1 − r ( d ) ∼ c d α L ( d ) , c > 0 , 0 < α < 2 , (43) where L L L is slowly varying at zero. Then (4.12) holds, h d ( x ) → ϕ ( x ) h_d(x) \to\phi(x) h d ( x ) → ϕ ( x ) for all x x x , and the density convergence is in L 1 L^1 L 1 . Moreover,
q d → q = 1 − 2 α − 1 , p d → p = 1 4 + 1 2 π arcsin ( q ) > 0. q_d \to q=1-2^{\alpha-1}, \qquad p_d \to p=\frac{1}{4}+\frac{1}{2\pi}\arcsin(q)>0. q d → q = 1 − 2 α − 1 , p d → p = 4 1 + 2 π 1 arcsin ( q ) > 0. On an interval of length T T T , for every fixed finite threshold u u u ,
E M d ∼ T d p , E M u , d ∼ T d p Ψ ( u ) . \mathbb{E}M_d \sim\frac{T}{d}p, \qquad\mathbb{E}M_{u,d} \sim\frac{T}{d}p\Psi(u). E M d ∼ d T p , E M u , d ∼ d T p Ψ ( u ) .
Proof. Regular variation gives V ( 2 d ) / V ( d ) → 2 α V(2d)/V(d) \to2^\alpha V ( 2 d ) / V ( d ) → 2 α and V ( d ) → 0 V(d) \to0 V ( d ) → 0 . Therefore
Δ ( d ) V ( d ) = 4 − V ( 2 d ) V ( d ) → 4 − 2 α > 0 , V ( d ) 2 Δ ( d ) = V ( d ) Δ ( d ) / V ( d ) → 0. \frac{\Delta(d)}{V(d)}=4-\frac{V(2d)}{V(d)}\to4-2^\alpha>0,\qquad
\frac{V(d)^2}{\Delta(d)}=\frac{V(d)}{\Delta(d)/V(d)}\to0. V ( d ) Δ ( d ) = 4 − V ( d ) V ( 2 d ) → 4 − 2 α > 0 , Δ ( d ) V ( d ) 2 = Δ ( d ) / V ( d ) V ( d ) → 0.
Corollary 4.7 yields the density assertions. Since q d = 1 − V ( 2 d ) / ( 2 V ( d ) ) q_d=1-V(2d)/(2V(d)) q d = 1 − V ( 2 d ) / ( 2 V ( d )) , we obtain q d → 1 − 2 α − 1 ∈ ( − 1 , 1 / 2 ) q_d \to1-2^{\alpha-1}\in(-1,1/2) q d → 1 − 2 α − 1 ∈ ( − 1 , 1/2 ) , and the orthant identity gives the limit of p d p_d p d . With N d = T / d + O ( 1 ) N_d=T/d+O(1) N d = T / d + O ( 1 ) , the exact count identities and total variation convergence give
E M d = N d p d ∼ T d p , H ‾ d ( u ) = ∫ u ∞ h d ( x ) d x → Ψ ( u ) , \mathbb{E}M_d=N_dp_d\sim\frac{T}{d}p,\qquad
\overline{H}_d(u)=\int_u^\infty h_d(x)\,dx\to\Psi(u), E M d = N d p d ∼ d T p , H d ( u ) = ∫ u ∞ h d ( x ) d x → Ψ ( u ) ,
which proves the assertion for E M u , d \mathbb{E}M_{u,d} E M u , d .
The local form (4.14) is standard in the extreme value theory of nonsmooth Gaussian processes [12 , 15 , 16 ] .
Corollary 4.12 (Once but not twice mean-square differentiable). Suppose, for some 2 < β < 4 2<\beta<4 2 < β < 4 ,
r ( d ) = 1 − λ 1 2 d 2 + c ∣ d ∣ β + o ( ∣ d ∣ β ) , λ 1 , c > 0. r(d)=1-\frac{\lambda_1}{2}d^2+c|d|^\beta+o(|d|^\beta),\qquad\lambda_1,c>0. r ( d ) = 1 − 2 λ 1 d 2 + c ∣ d ∣ β + o ( ∣ d ∣ β ) , λ 1 , c > 0. Then (4.12) holds and h d → ϕ h_d\to\phi h d → ϕ pointwise and in L 1 L^1 L 1 . With K β = c ( 2 β − 4 ) / λ 1 K_\beta=c(2^\beta-4)/\lambda_1 K β = c ( 2 β − 4 ) / λ 1 ,
p d ∼ 2 K β 2 π d ( β − 2 ) / 2 , E M d ∼ T 2 K β 2 π d ( β − 4 ) / 2 p_d\sim\frac{\sqrt{2K_\beta}}{2\pi}d^{(\beta-2)/2},\qquad
\mathbb{E}M_d\sim\frac{T\sqrt{2K_\beta}}{2\pi}d^{(\beta-4)/2} p d ∼ 2 π 2 K β d ( β − 2 ) /2 , E M d ∼ 2 π T 2 K β d ( β − 4 ) /2 on an interval of length T T T . For every fixed finite u u u , the latter expected count multiplied by Ψ ( u ) \Psi(u) Ψ ( u ) is asymptotic to E M u , d \mathbb{E}M_{u,d} E M u , d .
Proof. The covariance expansion gives
V ( d ) = λ 1 2 d 2 − c d β + o ( d β ) , Δ ( d ) = c ( 2 β − 4 ) d β + o ( d β ) . V(d) = \frac{\lambda_1}{2}d^2 - cd^\beta+ o(d^\beta), \qquad\Delta(d) = c(2^\beta- 4)d^\beta+ o(d^\beta). V ( d ) = 2 λ 1 d 2 − c d β + o ( d β ) , Δ ( d ) = c ( 2 β − 4 ) d β + o ( d β ) .
Thus
V ( d ) 2 Δ ( d ) ∼ λ 1 2 4 c ( 2 β − 4 ) d 4 − β → 0 , ϵ d = 1 + q d = Δ ( d ) 2 V ( d ) ∼ K β d β − 2 . \frac{V(d)^2}{\Delta(d)} \sim\frac{\lambda_1^2}{4c(2^\beta-4)}d^{4-\beta} \to0, \qquad\epsilon_d = 1 + q_d = \frac{\Delta(d)}{2V(d)} \sim K_\beta d^{\beta-2}. Δ ( d ) V ( d ) 2 ∼ 4 c ( 2 β − 4 ) λ 1 2 d 4 − β → 0 , ϵ d = 1 + q d = 2 V ( d ) Δ ( d ) ∼ K β d β − 2 .
Corollary 4.7 proves the Gaussian limit, while p d = arccos ( 1 − ϵ d ) / ( 2 π ) ∼ 2 ϵ d / ( 2 π ) p_d = \arccos(1-\epsilon_d)/(2\pi) \sim\sqrt{2\epsilon_d}/(2\pi) p d = arccos ( 1 − ϵ d ) / ( 2 π ) ∼ 2 ϵ d / ( 2 π ) proves the peak probability asymptotic. Multiplication by N d = T / d + O ( 1 ) N_d = T/d + O(1) N d = T / d + O ( 1 ) proves the count assertions. Finally, Fatou’s lemma and V ( d ) / d 2 → λ 1 / 2 V(d)/d^2 \to\lambda_1/2 V ( d ) / d 2 → λ 1 /2 imply m 2 < ∞ m_2 < \infty m 2 < ∞ ; dominated convergence then identifies m 2 = λ 1 m_2 = \lambda_1 m 2 = λ 1 . The relation Δ ( d ) / d 4 → ∞ \Delta(d)/d^4 \to\infty Δ ( d ) / d 4 → ∞ excludes m 4 < ∞ m_4 < \infty m 4 < ∞ . Hence the process has one, but not two, mean-square derivatives.
Examples and Numerical Comparisons
Ornstein–Uhlenbeck and powered-exponential correlations
For the Ornstein–Uhlenbeck correlation r ( s ) = e − λ ∣ s ∣ r(s) = e^{-\lambda|s|} r ( s ) = e − λ ∣ s ∣ , λ > 0 \lambda> 0 λ > 0 , the identity r ( 2 d ) = r ( d ) 2 r(2d) = r(d)^2 r ( 2 d ) = r ( d ) 2 gives ξ d = 0 \xi_d = 0 ξ d = 0 . Thus
h d ( x ) = ϕ ( x ) Φ ( b d x ) 2 p d , p d = 1 4 + 1 2 π arcsin ( 1 − r ( d ) 2 ) . (44) h_d(x) = \frac{\phi(x)\Phi(b_d x)^2}{p_d}, \qquad p_d = \frac{1}{4} + \frac{1}{2\pi}\arcsin\left(\frac{1-r(d)}{2}\right). \tag*{(44)} h d ( x ) = p d ϕ ( x ) Φ ( b d x ) 2 , p d = 4 1 + 2 π 1 arcsin ( 2 1 − r ( d ) ) . (44)
Since 1 − r ( d ) ∼ λ d 1-r(d) \sim\lambda d 1 − r ( d ) ∼ λ d , p d → 1 / 4 p_d \to1/4 p d → 1/4 and h d → ϕ h_d \to\phi h d → ϕ pointwise and in L 1 L^1 L 1 . The expected number of interior peaks on an interval of length T T T is asymptotic to T / ( 4 d ) T/(4d) T / ( 4 d ) .
More generally, the powered-exponential family r ( s ) = exp ( − c ∣ s ∣ α ) r(s) = \exp(-c|s|^\alpha) r ( s ) = exp ( − c ∣ s ∣ α ) , with c > 0 c > 0 c > 0 and 0 < α < 2 0 < \alpha< 2 0 < α < 2 , satisfies Corollary 4.11. Its limiting peak probability is ( 2 π ) − 1 arccos ( 2 α − 1 − 1 ) (2\pi)^{-1}\arccos(2^{\alpha-1}-1) ( 2 π ) − 1 arccos ( 2 α − 1 − 1 ) and its height limit is Gaussian. At α = 2 \alpha= 2 α = 2 the covariance is smooth and the next example applies.
Squared-exponential correlation
For r ( s ) = exp { − s 2 / ( 2 ℓ 2 ) } r(s) = \exp\{-s^2/(2\ell^2)\} r ( s ) = exp { − s 2 / ( 2 ℓ 2 )} , one has λ 1 = ℓ − 2 \lambda_1 = \ell^{-2} λ 1 = ℓ − 2 , λ 2 = 3 ℓ − 4 \lambda_2 = 3\ell^{-4} λ 2 = 3 ℓ − 4 , and η = 1 / 3 \eta= 1/\sqrt{3} η = 1/ 3 . The limit is
h η S M ( x ) = 2 3 ϕ ( 3 2 x ) + 2 π 3 x ϕ ( x ) Φ ( x 2 ) . h_\eta^{\mathrm{SM}}(x) = \sqrt{\frac{2}{3}}\,\phi\left(\sqrt{\frac{3}{2}}x\right) + \sqrt{\frac{2\pi}{3}}\,x\phi(x)\Phi\left(\frac{x}{\sqrt{2}}\right). h η SM ( x ) = 3 2 ϕ ( 2 3 x ) + 3 2 π x ϕ ( x ) Φ ( 2 x ) .
Here J = 3 / ( 2 π ℓ ) J = \sqrt{3}/(2\pi\ell) J = 3 / ( 2 π ℓ ) . The limiting height law does not depend on the correlation length ℓ \ell ℓ , whereas the peak intensity does.
The Matérn smoothness phase diagram
Consider the Matérn correlation function
r ν ( s ) = 2 1 − ν Γ ( ν ) ( θ ∣ s ∣ ) ν K ν ( θ ∣ s ∣ ) , ν , θ > 0. (45) r_\nu(s) = \frac{2^{1-\nu}}{\Gamma(\nu)}(\theta|s|)^\nu K_\nu(\theta|s|), \qquad\nu,\theta> 0. \tag*{(45)} r ν ( s ) = Γ ( ν ) 2 1 − ν ( θ ∣ s ∣ ) ν K ν ( θ ∣ s ∣ ) , ν , θ > 0. (45)
where K ν K_\nu K ν is the modified Bessel function. The parameter ν \nu ν controls mean-square differentiability [11 , 19 ] . Its one-dimensional spectral density is
f ν ( λ ) = Γ ( ν + 1 / 2 ) π Γ ( ν ) θ 2 ν ( θ 2 + λ 2 ) ν + 1 / 2 . (46) f_\nu(\lambda)=\frac{\Gamma(\nu+1/2)}{\sqrt{\pi}\Gamma(\nu)}\frac{\theta^{2\nu}}{(\theta^2+\lambda^2)^{\nu+1/2}}. \tag*{(46)} f ν ( λ ) = π Γ ( ν ) Γ ( ν + 1/2 ) ( θ 2 + λ 2 ) ν + 1/2 θ 2 ν . (46)
For j ≥ 0 j\ge0 j ≥ 0 , m j < ∞ m_j<\infty m j < ∞ precisely when j < 2 ν j<2\nu j < 2 ν . In particular, Theorem 4.8 gives a Gaussian peak height limit for ν ≤ 2 \nu\le2 ν ≤ 2 and a smooth limit for ν > 2 \nu>2 ν > 2 . Write L d = log { 1 / ( θ d ) } L_d=\log\{1/(\theta d)\} L d = log { 1/ ( θ d )} , which tends to infinity logarithmically as d ↓ 0 d\downarrow0 d ↓ 0 for fixed θ \theta θ . The covariance expansions follow from the small-argument series for K ν K_\nu K ν ; the logarithmic cases use [14 Section 10.31.1] .
For noninteger ν \nu ν , the two series branches have leading terms
r ν ( d ) = 1 + ( θ d ) 2 4 ( 1 − ν ) + ⋯ + Γ ( − ν ) 2 2 ν Γ ( ν ) ( θ d ) 2 ν { 1 + O ( d 2 ) } . r_\nu(d)=1+\frac{(\theta d)^2}{4(1-\nu)}+\cdots+\frac{\Gamma(-\nu)}{2^{2\nu}\Gamma(\nu)}(\theta d)^{2\nu}\{1+O(d^2)\}. r ν ( d ) = 1 + 4 ( 1 − ν ) ( θ d ) 2 + ⋯ + 2 2 ν Γ ( ν ) Γ ( − ν ) ( θ d ) 2 ν { 1 + O ( d 2 )} .
When 0 < ν < 1 0<\nu<1 0 < ν < 1 , this gives 1 − r ν ( d ) ∼ c ν d 2 ν 1-r_\nu(d)\sim c_\nu d^{2\nu} 1 − r ν ( d ) ∼ c ν d 2 ν , where c ν = − Γ ( − ν ) θ 2 ν / { 2 2 ν Γ ( ν ) } > 0 c_\nu=-\Gamma(-\nu)\theta^{2\nu}/\{2^{2\nu}\Gamma(\nu)\}>0 c ν = − Γ ( − ν ) θ 2 ν / { 2 2 ν Γ ( ν )} > 0 . When 1 < ν < 2 1<\nu<2 1 < ν < 2 , it gives
r ν ( d ) = 1 − θ 2 4 ( ν − 1 ) d 2 + c ν d 2 ν + o ( d 2 ν ) , c ν = Γ ( − ν ) θ 2 ν 2 2 ν Γ ( ν ) > 0. r_\nu(d)=1-\frac{\theta^2}{4(\nu-1)}d^2+c_\nu d^{2\nu}+o(d^{2\nu}),\qquad c_\nu=\frac{\Gamma(-\nu)\theta^{2\nu}}{2^{2\nu}\Gamma(\nu)}>0. r ν ( d ) = 1 − 4 ( ν − 1 ) θ 2 d 2 + c ν d 2 ν + o ( d 2 ν ) , c ν = 2 2 ν Γ ( ν ) Γ ( − ν ) θ 2 ν > 0.
Corollaries 4.11 and 4.12 then give the respective probabilities and count rates.
At ν = 1 \nu=1 ν = 1 , the integer-order expansion gives
V ( d ) = θ 2 2 d 2 L d + B θ d 2 + O ( d 4 L d ) , B θ = θ 2 2 ( log 2 − γ E + 1 2 ) . V(d)=\frac{\theta^2}{2}d^2L_d+B_\theta d^2+O(d^4L_d),\qquad B_\theta=\frac{\theta^2}{2}\left(\log2-\gamma_E+\frac{1}{2}\right). V ( d ) = 2 θ 2 d 2 L d + B θ d 2 + O ( d 4 L d ) , B θ = 2 θ 2 ( log 2 − γ E + 2 1 ) .
where γ E \gamma_E γ E is Euler’s constant. Since L 2 d = L d − log 2 L_{2d}=L_d-\log2 L 2 d = L d − log 2 , the quadratic constants cancel in 4 V ( d ) − V ( 2 d ) 4V(d)-V(2d) 4 V ( d ) − V ( 2 d ) , giving
Δ ( d ) ∼ 2 θ 2 ( log 2 ) d 2 , V ( d ) 2 Δ ( d ) ∼ θ 2 d 2 L d 2 8 log 2 → 0. \Delta(d)\sim2\theta^2(\log2)d^2,\qquad\frac{V(d)^2}{\Delta(d)}\sim\frac{\theta^2d^2L_d^2}{8\log2}\to0. Δ ( d ) ∼ 2 θ 2 ( log 2 ) d 2 , Δ ( d ) V ( d ) 2 ∼ 8 log 2 θ 2 d 2 L d 2 → 0.
Consequently,
p d ∼ log 2 π L d , E M d ∼ T log 2 π d L d . p_d\sim\frac{\sqrt{\log2}}{\pi\sqrt{L_d}},\qquad EM_d\sim\frac{T\sqrt{\log2}}{\pi d\sqrt{L_d}}. p d ∼ π L d log 2 , E M d ∼ π d L d T log 2 .
At ν = 2 \nu= 2 ν = 2 , the first nonsmooth term has quartic logarithmic order:
r 2 ( d ) = 1 − θ 2 4 d 2 + θ 4 16 d 4 L d + O ( d 4 ) . r_2(d) = 1 - \frac{\theta^2}{4}d^2 + \frac{\theta^4}{16}d^4L_d + O(d^4). r 2 ( d ) = 1 − 4 θ 2 d 2 + 16 θ 4 d 4 L d + O ( d 4 ) .
Therefore,
Δ ( d ) ∼ 3 θ 4 4 d 4 L d , V ( d ) 2 Δ ( d ) ∼ 1 12 L d , η d 2 ∼ 1 6 L d . \Delta(d) \sim\frac{3\theta^4}{4}d^4L_d,\qquad\frac{V(d)^2}{\Delta(d)} \sim\frac{1}{12L_d},\qquad\eta_d^2 \sim\frac{1}{6L_d}. Δ ( d ) ∼ 4 3 θ 4 d 4 L d , Δ ( d ) V ( d ) 2 ∼ 12 L d 1 , η d 2 ∼ 6 L d 1 .
The Gaussian limit persists at this boundary, but the height-curvature correlation decays only logarithmically. Moreover,
p d ∼ 3 θ 2 π d L d , E M d ∼ T 3 θ 2 π L d . p_d \sim\frac{\sqrt{3}\theta}{2\pi}d\sqrt{L_d},\qquad\mathbb{E}M_d \sim\frac{T\sqrt{3}\theta}{2\pi}\sqrt{L_d}. p d ∼ 2 π 3 θ d L d , E M d ∼ 2 π T 3 θ L d .
For both integer boundaries, the expected count above any fixed finite threshold is asymptotic to the displayed total count multiplied by Ψ ( u ) \Psi(u) Ψ ( u ) .
For ν > 2 \nu> 2 ν > 2 , integrating (46) gives
m 2 = θ 2 2 ( ν − 1 ) , m 4 = 3 θ 4 4 ( ν − 1 ) ( ν − 2 ) , η = ν − 2 3 ( ν − 1 ) , J = θ 2 π 3 2 ( ν − 2 ) . m_2 = \frac{\theta^2}{2(\nu- 1)},\qquad m_4 = \frac{3\theta^4}{4(\nu- 1)(\nu- 2)},\qquad\eta= \sqrt{\frac{\nu- 2}{3(\nu- 1)}},\qquad J = \frac{\theta}{2\pi}\sqrt{\frac{3}{2(\nu- 2)}}. m 2 = 2 ( ν − 1 ) θ 2 , m 4 = 4 ( ν − 1 ) ( ν − 2 ) 3 θ 4 , η = 3 ( ν − 1 ) ν − 2 , J = 2 π θ 2 ( ν − 2 ) 3 .
These moments also make explicit why the limiting height shape is independent of θ \theta θ , while the count intensity scales with θ \theta θ .
Table 1 summarizes the peak probability asymptotics, limiting height distributions, and expected peak count rates for the Matérn family over the full range ν > 0 \nu> 0 ν > 0 .
Table 1. One-dimensional Matérn infill limits on a fixed interval of positive length. Here L d = log { 1 / ( θ d ) } L_d=\log\{1/(\theta d)\} L d = log { 1/ ( θ d )} , and a , c a,c a , c denote positive constants that may differ between rows. The notation f ≍ g f\asymp g f ≍ g means that f / g f/g f / g is bounded above and below by positive constants for small d d d .
Nonstationary unit-variance examples
Let Y Y Y be a centered stationary unit-variance process with smooth covariance r r r and 0 < m 2 , m 4 < ∞ 0 < m_2,m_4 < \infty 0 < m 2 , m 4 < ∞ . For a C 4 C^4 C 4 function f f f with f ′ ( t ) > 0 f'(t) > 0 f ′ ( t ) > 0 , define X ( t ) = Y ( f ( t ) ) X(t) = Y(f(t)) X ( t ) = Y ( f ( t )) . Then
C ( s , t ) = r ( f ( t ) − f ( s ) ) , c ± = r ( f ( t ± d ) − f ( t ) ) , c 0 = r ( f ( t + d ) − f ( t − d ) ) . C(s,t) = r(f(t)-f(s)),\qquad c_{\pm} = r(f(t\pm d)-f(t)),\qquad c_0 = r(f(t+d)-f(t-d)). C ( s , t ) = r ( f ( t ) − f ( s )) , c ± = r ( f ( t ± d ) − f ( t )) , c 0 = r ( f ( t + d ) − f ( t − d )) .
These three correlations give the exact nonstationary law in Theorem 2.1 ; the two center-neighbor correlations generally differ even though the observation grid is uniform. The mean-square chain rule yields
λ 1 ( t ) = f ′ ( t ) 2 m 2 , a ( t ) = f ′ ( t ) f ′ ′ ( t ) m 2 , λ 2 ( t ) = f ′ ′ ( t ) 2 m 2 + f ′ ( t ) 4 m 4 . \lambda_1(t) = f'(t)^2m_2,\qquad a(t) = f'(t)f''(t)m_2,\qquad\lambda_2(t) = f''(t)^2m_2 + f'(t)^4m_4. λ 1 ( t ) = f ′ ( t ) 2 m 2 , a ( t ) = f ′ ( t ) f ′′ ( t ) m 2 , λ 2 ( t ) = f ′′ ( t ) 2 m 2 + f ′ ( t ) 4 m 4 .
Thus
δ t 2 = f ′ ( t ) 4 m 4 , η t = m 2 m 4 , J t = f ′ ( t ) 2 π m 4 m 2 . (47) \delta_t^2 = f'(t)^4m_4,\qquad\eta_t = \frac{m_2}{\sqrt{m_4}},\qquad J_t = \frac{f'(t)}{2\pi}\sqrt{\frac{m_4}{m_2}}. \tag*{(47)} δ t 2 = f ′ ( t ) 4 m 4 , η t = m 4 m 2 , J t = 2 π f ′ ( t ) m 2 m 4 . (47)
The conditional curvature correction removes the f ′ ′ ( t ) 2 m 2 f''(t)^2m_2 f ′′ ( t ) 2 m 2 term. On [ a , b ] [a,b] [ a , b ] , the limiting expected peak count is ( f ( b ) − f ( a ) ) m 4 / m 2 / ( 2 π ) (f(b)-f(a))\sqrt{m_4/m_2}/(2\pi) ( f ( b ) − f ( a )) m 4 / m 2 / ( 2 π ) , consistent with the transformed interval length.
A smooth mixture can also change the limiting height shape. Let Y 1 , Y 2 Y_1,Y_2 Y 1 , Y 2 be independent centered stationary unit-variance processes with smooth covariances r j r_j r j and moments m 2 , j , m 4 , j m_{2,j},m_{4,j} m 2 , j , m 4 , j . For C 4 C^4 C 4 weights w 1 ( t ) = cos θ ( t ) w_1(t) = \cos\theta(t) w 1 ( t ) = cos θ ( t ) and w 2 ( t ) = sin θ ( t ) w_2(t) = \sin\theta(t) w 2 ( t ) = sin θ ( t ) , set
X ( t ) = w 1 ( t ) Y 1 ( t ) + w 2 ( t ) Y 2 ( t ) , C ( s , t ) = ∑ j = 1 2 w j ( s ) w j ( t ) r j ( t − s ) . X(t) = w_1(t)Y_1(t) + w_2(t)Y_2(t),\qquad C(s,t) = \sum_{j=1}^{2} w_j(s)w_j(t)r_j(t-s). X ( t ) = w 1 ( t ) Y 1 ( t ) + w 2 ( t ) Y 2 ( t ) , C ( s , t ) = j = 1 ∑ 2 w j ( s ) w j ( t ) r j ( t − s ) .
The variance is one because w 1 2 + w 2 2 = 1 w_1^2+w_2^2=1 w 1 2 + w 2 2 = 1 , and direct differentiation gives
λ 1 ( t ) = ∑ j = 1 2 { w j ′ ( t ) 2 + m 2 , j w j ( t ) 2 } , (48) \lambda_1(t)=\sum_{j=1}^{2}\{w_j'(t)^2+m_{2,j}w_j(t)^2\}, \tag*{(48)} λ 1 ( t ) = j = 1 ∑ 2 { w j ′ ( t ) 2 + m 2 , j w j ( t ) 2 } , (48)
λ 2 ( t ) = ∑ j = 1 2 { w j ′ ′ ( t ) 2 + 4 m 2 , j w j ′ ( t ) 2 + m 4 , j w j ( t ) 2 − 2 m 2 , j w j ( t ) w j ′ ′ ( t ) } . (49) \lambda_2(t)=\sum_{j=1}^{2}\{w_j''(t)^2+4m_{2,j}w_j'(t)^2+m_{4,j}w_j(t)^2-2m_{2,j}w_j(t)w_j''(t)\}. \tag*{(49)} λ 2 ( t ) = j = 1 ∑ 2 { w j ′′ ( t ) 2 + 4 m 2 , j w j ′ ( t ) 2 + m 4 , j w j ( t ) 2 − 2 m 2 , j w j ( t ) w j ′′ ( t )} . (49)
Together with a ( t ) = λ 1 ′ ( t ) / 2 a(t)=\lambda_1'(t)/2 a ( t ) = λ 1 ′ ( t ) /2 , these expressions determine δ t \delta_t δ t , η t \eta_t η t , and J t J_t J t . For a concrete example, take squared-exponential r j r_j r j with length scales ℓ 1 = 1 \ell_1=1 ℓ 1 = 1 , ℓ 2 = 2 \ell_2=2 ℓ 2 = 2 , and θ ( t ) = t \theta(t)=t θ ( t ) = t . At t = 0 t=0 t = 0 the values are λ 1 = 2 \lambda_1=2 λ 1 = 2 , a = 0 a=0 a = 0 , and λ 2 = 7 \lambda_2=7 λ 2 = 7 , so η 0 = 2 / 7 \eta_0=2/\sqrt{7} η 0 = 2/ 7 . At t = π / 2 t=\pi/2 t = π /2 they are λ 1 = 5 / 4 \lambda_1=5/4 λ 1 = 5/4 , a = 0 a=0 a = 0 , and λ 2 = 91 / 16 \lambda_2=91/16 λ 2 = 91/16 , so η π / 2 = 5 / 91 \eta_{\pi/2}=5/\sqrt{91} η π /2 = 5/ 91 . Thus the limiting peak height densities differ at the two locations. Finite-grid probabilities and densities follow from the same exact formula.
Deterministic numerical comparisons
For all numerical comparisons we set λ = 1 \lambda=1 λ = 1 in the Ornstein–Uhlenbeck covariance, θ = 1 \theta=1 θ = 1 in the Matérn covariance, and ℓ = 1 \ell=1 ℓ = 1 in the squared-exponential covariance. Thus the mesh values in the density figure and the error table use the same model scales. The peak probability p d p_d p d and finite-mesh peak height density h d ( x ) h_d(x) h d ( x ) are computed from (11) .
Figure 1 compares finite-mesh densities with their limiting laws. Figure 2 shows the corresponding Matérn peak intensity per unit length. The distinction between convergence of the entire density and relative accuracy of a small tail probability is quantified by
Figure 1. Exact finite-grid peak height densities at mesh sizes d = 1 d=1 d = 1 , 0.5 0.5 0.5 , 0.1 0.1 0.1 , 0.01 0.01 0.01 , with their limiting densities. The Ornstein–Uhlenbeck and Matérn ν = 2 \nu=2 ν = 2 limits are ϕ \phi ϕ ; the Matérn ν = 5 / 2 \nu=5/2 ν = 5/2 and squared-exponential limits are the smooth densities with η = 1 / 3 \eta=1/3 η = 1/3 and η = 1 / 3 \eta=1/\sqrt{3} η = 1/ 3 , respectively. All curves are obtained by deterministic numerical evaluations.
Figure 2. Exact Matérn peak intensities per unit length, p d / d p_d/d p d / d , with θ = 1 \theta=1 θ = 1 . On an interval of length T T T , the expected number of interior grid peaks is T p d / d + O ( p d ) Tp_d/d+O(p_d) T p d / d + O ( p d ) . The dashed line is the finite limit 3 / ( 2 π ) \sqrt{3}/(2\pi) 3 / ( 2 π ) for ν = 5 / 2 \nu=5/2 ν = 5/2 ; the curves for ν ≤ 2 \nu\leq2 ν ≤ 2 diverge as d ↓ 0 d\downarrow0 d ↓ 0 .
E 1 ( d ) = ∫ R ∣ h d ( x ) − h ∞ ( x ) ∣ d x , R u ( d ) = H ‾ d ( u ) H ‾ ∞ ( u ) − 1. E_1(d)=\int_{\mathbb{R}}\lvert h_d(x)-h_\infty(x)\rvert\,\mathrm{d}x,\qquad R_u(d)=\frac{\overline{H}_d(u)}{\overline{H}_\infty(u)}-1. E 1 ( d ) = ∫ R ∣ h d ( x ) − h ∞ ( x )∣ d x , R u ( d ) = H ∞ ( u ) H d ( u ) − 1.
where h ∞ = ϕ h_\infty=\phi h ∞ = ϕ in the rough cases and h ∞ = h S M h_\infty=h^{\mathrm{SM}} h ∞ = h SM in the smooth cases. Positive R u R_u R u means that the limiting law underestimates the exact upper tail.
Table 2 illustrates the slow boundary behavior. At d = 0.01 d=0.01 d = 0.01 , the Matérn ν = 2 \nu=2 ν = 2 height-curvature correlation is about 0.191, but the Gaussian tail at u = 3 u=3 u = 3 is smaller than the exact tail by a factor of about 1.97. The squared-exponential smooth approximation at the same mesh is much more accurate. These comparisons show that the accuracy of a limiting approximation depends on the covariance model. When accurate tail probabilities are needed, the exact discrete distribution at the observed grid spacing is therefore preferable. The table reports errors and correlations to at most three significant digits.
Table 2. Errors of the limiting density and tails at the stated mesh. Here E 1 ( d ) = ∫ R ∣ h d ( x ) − h ∞ ( x ) ∣ d x E_1(d) = \int_{\mathbb{R}} \lvert h_d(x) - h_\infty(x)\rvert\,\mathrm{d}x E 1 ( d ) = ∫ R ∣ h d ( x ) − h ∞ ( x )∣ d x and R u ( d ) = H ‾ d ( u ) / H ‾ ∞ ( u ) − 1 R_u(d) = \overline{H}_d(u)/\overline{H}_\infty(u) - 1 R u ( d ) = H d ( u ) / H ∞ ( u ) − 1 .
Discussion
The exact discrete law and the continuous peak law describe related sampling rules. The discrete law is an ordinary conditional distribution determined by three Gaussian observations. Under the smooth covariance and nondegeneracy assumptions of § 3 , its infill limit is h η t S M h_{\eta_t}^{\mathrm{SM}} h η t SM with η t ∈ ( 0 , 1 ] \eta_t\in(0,1] η t ∈ ( 0 , 1 ] . An interpretation as the Palm law of continuous local maxima requires the additional sample path and Kac–Rice assumptions stated there. Theorem 4.1 characterizes convergence to the Gaussian law for general nonstationary covariance, including vanishing peak probabilities.
Remark 4.2 places these established limits in the same continuous family: h 0 S M = ϕ h_0^{\mathrm{SM}} = \phi h 0 SM = ϕ , the interior members are the smooth peak laws, and h 1 S M h_1^{\mathrm{SM}} h 1 SM is Rayleigh. For each fixed nonconstant, mean-square continuous stationary process, the fourth spectral moment identifies the parameter: η = 0 \eta= 0 η = 0 for m 4 = ∞ m_4 = \infty m 4 = ∞ and η = m 2 / m 4 ∈ ( 0 , 1 ] \eta= m_2/\sqrt{m_4} \in(0,1] η = m 2 / m 4 ∈ ( 0 , 1 ] for m 4 < ∞ m_4 < \infty m 4 < ∞ . This connects Gaussian height neutrality and smooth curvature weighting within a single family, while retaining the assumptions that determine which limit applies.
The height laws converge in total variation, which implies
sup u ∈ R ∣ H ‾ d ( u ) − H ‾ ∞ ( u ) ∣ ≤ 1 2 ∫ R ∣ h d ( x ) − h ∞ ( x ) ∣ d x → 0. \sup_{u\in\mathbb{R}} \lvert\overline{H}_d(u) - \overline{H}_\infty(u)\rvert\le\frac{1}{2}\int_{\mathbb{R}} \lvert h_d(x) - h_\infty(x)\rvert\,\mathrm{d}x \to0. u ∈ R sup ∣ H d ( u ) − H ∞ ( u )∣ ≤ 2 1 ∫ R ∣ h d ( x ) − h ∞ ( x )∣ d x → 0.
This is uniform absolute tail convergence. It does not alone imply that the ratio of the tails tends to one at thresholds u d → ∞ u_d \to\infty u d → ∞ . The stronger density bound in Remark 4.6 does give relative Gaussian tail convergence when u d R t , d → 0 u_d\sqrt{R_{t,d}} \to0 u d R t , d → 0 , with R t , d → 0 R_{t,d} \to0 R t , d → 0 . In the stationary case this sufficient condition is u d η d → 0 u_d\eta_d \to0 u d η d → 0 . Outside such controlled ranges, the distinction remains essential. The following consequence of the Ornstein–Uhlenbeck formula makes this distinction explicit. Fix c > 0 c > 0 c > 0 and let u d = c / b d u_d = c/b_d u d = c / b d . Since b d → 0 b_d \to0 b d → 0 , u d → ∞ u_d \to\infty u d → ∞ , and
H ‾ d ( u d ) Ψ ( u d ) = 1 p d E { Φ ( b d Z ) ∣ Z > u d } → 4 Φ ( c ) 2 . (50) \frac{\overline{H}_d(u_d)}{\Psi(u_d)} = \frac{1}{p_d}\mathbb{E}\{\Phi(b_dZ) \mid Z > u_d\} \to4\Phi(c)^2. \tag*{(50)} Ψ ( u d ) H d ( u d ) = p d 1 E { Φ ( b d Z ) ∣ Z > u d } → 4Φ ( c ) 2 . (50)
where Z Z Z is standard Gaussian. Indeed, for each $\varepsilon > 0,
P { b d Z > c + ε ∣ Z > c / b d } = Ψ ( ( c + ε ) / b d ) Ψ ( c / b d ) → 0 \mathbb{P}\{b_dZ > c + \varepsilon\mid Z > c/b_d\} = \frac{\Psi((c+\varepsilon)/b_d)}{\Psi(c/b_d)} \to0 P { b d Z > c + ε ∣ Z > c / b d } = Ψ ( c / b d ) Ψ (( c + ε ) / b d ) → 0
by the Gaussian tail asymptotic. Thus b d Z → c b_dZ \to c b d Z → c in conditional probability, and bounded continuity gives the expectation limit in (6.1); finally p d → 1 / 4 p_d \to1/4 p d → 1/4 . For this covariance,
u d η d = c 2 { 1 + r ( d ) } 3 − r ( d ) → 2 c > 0. u_d\eta_d = c\sqrt{\frac{2\{1+r(d)\}}{3-r(d)}} \to\sqrt{2}\,c > 0. u d η d = c 3 − r ( d ) 2 { 1 + r ( d )} → 2 c > 0.
These thresholds therefore lie outside the sufficient range u d η d → 0 u_d\eta_d \to0 u d η d → 0 for relative Gaussian tail convergence. Relative approximation outside that range requires further tail analysis or direct use of the exact finite-grid law.
Extensions to nonzero mean, varying variance, irregular observation grids, and Gaussian fields on N N N -dimensional lattices remain natural. Finite-dimensional Gaussian conditioning still yields exact comparison probabilities in these settings. The limiting peak height law may, however, change with the process model and the geometry of the comparisons.
Acknowledgments
The authors were supported by NSF Grant DMS-2220523 and Simons Foundation Collaboration Grant #854127.
Dan Cheng and John Ginos School of Mathematical and Statistical Sciences Arizona State University 900 S. Palm Walk Tempe, AZ 85281, U.S.A. E-mail: cheng.stats@gmail.com