Introduction
Stochastic differential equations (SDEs) model systems subject to random perturbations. They are widely used in biology, chemistry, mechanics, and finance [9 ] . Many applications require computing expectations of functions of SDE solutions. For example, such expectations are used to price financial derivatives [6 ] and to solve parabolic partial differential equations [19 ] .
In this paper, we study the numerical approximation of such expectations, focusing on SDEs with constant diffusion. Specifically, let I = E [ g ( X T ) ] I = \mathbb{E}[g(X_T)] I = E [ g ( X T )] , where X X X solves
d X t = b ( t , X t ) d t + Σ d W t , X 0 = x 0 , t ∈ [ 0 , T ] . (1) \mathrm{d}X_t = b(t, X_t)\,\mathrm{d}t + \Sigma\,\mathrm{d}W_t,\qquad X_0 = x_0,\qquad t \in[0,T]. \tag*{(1)} d X t = b ( t , X t ) d t + Σ d W t , X 0 = x 0 , t ∈ [ 0 , T ] . (1)
Here T > 0 T > 0 T > 0 is fixed, X t ∈ R d x \boldsymbol{X}_t \in\mathbb{R}^{d_x} X t ∈ R d x , and W \boldsymbol{W} W is a standard d w d_w d w -dimensional Brownian motion. The drift is b : [ 0 , T ] × R d x → R d x b : [0,T] \times\mathbb{R}^{d_x} \to\mathbb{R}^{d_x} b : [ 0 , T ] × R d x → R d x , the diffusion matrix Σ ∈ R d x × d w \Sigma\in\mathbb{R}^{d_x \times d_w} Σ ∈ R d x × d w is constant, and g : R d x → R g : \mathbb{R}^{d_x} \to\mathbb{R} g : R d x → R is the payoff function. The initial state x 0 ∈ R d x x_0 \in\mathbb{R}^{d_x} x 0 ∈ R d x is deterministic. SDEs of this form arise in various applications, including overdamped Langevin dynamics [26 ] .
Explicit solutions of SDEs are generally unavailable, so numerical schemes are used to approximate their sample paths. We use the Euler–Maruyama (EM) scheme [10 ] on the uniform grid { t i = i h : i = 0 , … , m } \{t_i = ih : i = 0, \ldots, m\} { t i = ih : i = 0 , … , m } , with h = T / m h = T/m h = T / m , and set s = d w m s = d_wm s = d w m . For z = ( z 1 , … , z m ) ∈ ( R d w ) m ≅ R s z = (z_1, \ldots, z_m) \in(\mathbb{R}^{d_w})^m \cong\mathbb{R}^s z = ( z 1 , … , z m ) ∈ ( R d w ) m ≅ R s , set X ~ t 0 ( z ) = x 0 \widetilde{X}_{t_0}(z) = x_0 X t 0 ( z ) = x 0 and define
X ~ t i + 1 ( z ) = X ~ t i ( z ) + h b ( t i , X ~ t i ( z ) ) + h Σ z i + 1 , i = 0 , … , m − 1. (2) \widetilde{X}_{t_{i+1}}(z) = \widetilde{X}_{t_i}(z) + hb(t_i,\widetilde{X}_{t_i}(z)) + \sqrt{h}\,\Sigma z_{i+1}, \qquad i = 0,\ldots,m-1. \tag*{(2)} X t i + 1 ( z ) = X t i ( z ) + hb ( t i , X t i ( z )) + h Σ z i + 1 , i = 0 , … , m − 1. (2)
Let Z ∼ N ( 0 , I d s ) Z \sim N(0,I_{d_s}) Z ∼ N ( 0 , I d s ) be an s s s -dimensional standard Gaussian vector. Then X ~ t m ( Z ) \widetilde{X}_{t_m}(Z) X t m ( Z ) is the EM approximation at time T T T . The corresponding approximation to I \mathcal{I} I can be written as
I m : = E [ g ( X ~ t m ( Z ) ) ] = ∫ ( 0 , 1 ) s g ( X ~ t m ( Φ − 1 ( u ) ) ) d u , (3) \mathcal{I}_m := \mathbb{E}[g(\widetilde{X}_{t_m}(Z))] = \int_{(0,1)^s} g(\widetilde{X}_{t_m}(\Phi^{-1}(u)))\,du, \tag*{(3)} I m := E [ g ( X t m ( Z ))] = ∫ ( 0 , 1 ) s g ( X t m ( Φ − 1 ( u ))) d u , (3)
where Φ \Phi Φ is the standard Gaussian distribution function and Φ − 1 \Phi^{-1} Φ − 1 acts componentwise. Under suitable regularity and growth conditions, I m \mathcal{I}_m I m approximates I \mathcal{I} I with the classical weak error bound ∣ I m − I ∣ ≤ C m − 1 |\mathcal{I}_m-\mathcal{I}| \leq Cm^{-1} ∣ I m − I ∣ ≤ C m − 1 , where C C C is independent of m m m ; see [10 Theorem 14.5.1] . Thus, increasing the number of time steps m m m reduces the discretization error.
To compute I m \mathcal{I}_m I m , however, we typically approximate the integral in (3) numerically, since it generally has no closed-form expression. In this paper, we focus on the error introduced by numerical integration, referred to as the sampling error , as distinct from the time discretization error ∣ I m − I ∣ |\mathcal{I}_m-\mathcal{I}| ∣ I m − I ∣ . The integration dimension s = d w m s=d_wm s = d w m grows as the time grid is refined and becomes arbitrarily large as m → ∞ m \to\infty m → ∞ . This growth poses a central challenge in obtaining sampling error bounds that remain uniform in m m m . Monte Carlo (MC) provides a straightforward approach. For independent uniform points u 0 , … , u N − 1 ∈ ( 0 , 1 ) s u_0,\ldots,u_{N-1} \in(0,1)^s u 0 , … , u N − 1 ∈ ( 0 , 1 ) s , the MC estimator is
1 N ∑ n = 0 N − 1 g ( X ~ t m ( Φ − 1 ( u n ) ) ) . (4) \frac{1}{N}\sum_{n=0}^{N-1} g(\widetilde{X}_{t_m}(\Phi^{-1}(u_n))). \tag*{(4)} N 1 n = 0 ∑ N − 1 g ( X t m ( Φ − 1 ( u n ))) . (4)
The estimator achieves a root mean square error of O ( N − 1 / 2 ) O(N^{-1/2}) O ( N − 1/2 ) , with an implied constant independent of m m m provided that the variance of the integrand is uniformly bounded. This convergence rate is nevertheless slow. Quasi-Monte Carlo (QMC) replaces independent random points with low-discrepancy point sets and achieves nearly first-order convergence under bounded-variation assumptions [2 , 17 , 4 ] . However, Φ − 1 \Phi^{-1} Φ − 1 in (3) can make the integrand unbounded near the cube boundary, placing it outside the scope of the classical theory. To address this limitation, approaches based on boundary growth conditions [23 ] , projection [22 ] , and weighted function spaces [16 ] have been developed. Nevertheless, the boundary-growth and projection-based approaches do not directly resolve the dimension dependence.
The weighted-space framework of Nichols and Kuo [16 ] allows dimension-independent bounds, but applying it here requires mixed derivative estimates and summability conditions on the function-space weights. The nested composition structure of the EM integrand makes such estimates difficult to obtain. It remains unclear whether the dependence of this integrand on the Gaussian inputs permits weights satisfying these conditions uniformly in m m m . Recent studies offer insights into possible low-dimensional structure that may help address this question. For EM approximations, Ouyang, Pan, and He [20 ] derive randomized QMC (RQMC) error bounds of the form C ε , s N − 1 + ε C_{\varepsilon,s}N^{-1+\varepsilon} C ε , s N − 1 + ε , but the constants grow with s s s . Ouyang and Wang [21 ] later establish effective-dimension bounds uniform in m m m . Numerical experiments in both studies show advantages of RQMC over MC. These findings suggest that EM integrands may possess low-dimensional structure favorable to QMC, raising the possibility that suitable weights satisfy the required summability conditions.
It is also worth noting that QMC performance depends on how Brownian paths are constructed from Gaussian inputs. Different constructions can be represented by replacing Φ − 1 ( u ) \Phi^{-1}(u) Φ − 1 ( u ) in (1.3) with U Φ − 1 ( u ) U\Phi^{-1}(u) U Φ − 1 ( u ) , where U ∈ R s × s U \in\mathbb{R}^{s \times s} U ∈ R s × s is orthogonal. Such transformations leave the standard MC error unchanged but alter the structure of the integrand, and hence can affect the QMC error [12 , 27 ] . In particular, we focus on the Brownian bridge (BB) construction, which first generates W T W_T W T and then samples conditional midpoint values on successively finer intervals [15 Section 1.1.2] . Such a construction assigns the largest-scale variation of the Brownian path to the Gaussian inputs generating W T W_T W T , while each subsequent refinement introduces Gaussian inputs that affect smaller-scale fluctuations with decreasing amplitude. This hierarchical structure may lead to low-dimensional structure in the integrand that is favorable to QMC.
In this paper, we use randomly shifted rank-1 lattice rules, an RQMC method whose points are generated by an integer generating vector and a uniform random shift. Combined with the Brownian bridge construction, these rules are used to approximate I m I_m I m for SDEs with constant diffusion. Within the weighted function-space framework of Nichols and Kuo [16 ] , we establish mixed derivative estimates and verify the required summability conditions on the weights. To handle the nested composition structure of the EM integrand, we use the multivariate Faà di Bruno formula [14 Theorem 1] (see also [3 , 8 ] ) to expand its mixed derivatives. We organize the resulting terms and their propagation through the EM recursion using a rooted-tree representation, following the standard terminology in [13 Section 4.2] . The decay and localized supports of the BB basis functions then allow us to obtain summability estimates uniform in m m m .
Since the resulting weights are not available in an explicitly computable form, a component-by-component (CBC) construction [18 , 16 ] is impractical for these weights. To avoid this difficulty, we choose generating vectors at random and use the median of independent lattice estimates [7 , 28 ] . Specifically, we independently generate R = 2 k − 1 R = 2k - 1 R = 2 k − 1 lattice estimates, each using a uniformly random generating vector and an independent uniform shift, and take their median. This approach requires no explicit knowledge of the weights. Taking the median also improves stability by reducing the influence of unusually large errors and increasing the probability of obtaining an accurate estimate.
Our analysis of the randomly shifted lattice rule and its median estimator yields the following main results on sampling error.
For an N N N -point randomly shifted lattice rule with a uniformly random generating vector, we prove a mean absolute sampling error bound of O ( N − 1 + ε ) O(N^{-1+\varepsilon}) O ( N − 1 + ε ) for every ε ∈ ( 0 , 1 / 2 ) \varepsilon\in(0,1/2) ε ∈ ( 0 , 1/2 ) and every prime N N N . The implied constant is independent of the number of time steps m m m . See Theorem 3.1 .
The median of R = 2 k − 1 R = 2k - 1 R = 2 k − 1 independent lattice estimates achieves an L q L^q L q sampling error of O ( N − 1 + ε ) O(N^{-1+\varepsilon}) O ( N − 1 + ε ) for every 1 ≤ q < k / ( 1 − ε ) 1 \le q < k/(1-\varepsilon) 1 ≤ q < k / ( 1 − ε ) , with an implied constant independent of m m m . In particular, the median of three estimates achieves the same rate in root mean square error. See Theorem 3.1 .
The remaining time discretization error is covered by the classical strong and weak convergence theory for Euler–Maruyama approximations; see, for example, [10 Chapters 10 and 14] and [9 Section 5] . We retain a general assumption on the Euler–Maruyama time discretization error and verify it under two sets of time regularity conditions. Theorems 3.6 and 3.7 establish bias rates of order m − 1 / 2 m^{-1/2} m − 1/2 and m − 1 m^{-1} m − 1 , respectively. The sampling error estimates and the Euler–Maruyama time discretization error bound together give the total error bounds for both estimators in Corollary 3.8.
The remainder of the paper is organized as follows. § 2 states the assumptions on the SDE (1.1) and payoff g g g and describes the Brownian bridge construction. § 3 states the sampling and total error results. § 4 establishes the mixed derivative summability result, and § 5 derives the lattice sampling error bounds. § 6 presents the numerical experiments. § 7 concludes the paper. Technical proofs are deferred to the appendices.
Notation and preliminaries
This section states the assumptions used in our analysis and reviews the Brownian bridge construction, the Euler–Maruyama scheme, the weighted function spaces of Nichols and Kuo [16 ] , and randomly shifted lattice rules. We also introduce the median lattice estimator following [7 , 28 ] . Before proceeding, we fix some notation.
We write Z \mathbb{Z} Z for the integers, N = { 1 , 2 , … } \mathbb{N} = \{1,2,\ldots\} N = { 1 , 2 , … } for the positive integers, and [ s ] = { 1 , … , s } [s] = \{1,\ldots,s\} [ s ] = { 1 , … , s } for s ∈ N s \in\mathbb{N} s ∈ N . For a finite set u u u , we denote its cardinality by ∣ u ∣ |u| ∣ u ∣ and the set of its partitions into nonempty blocks by P ( u ) \mathcal{P}(u) P ( u ) , with P ( ∅ ) = { ∅ } \mathcal{P}(\emptyset) = \{\emptyset\} P ( ∅ ) = { ∅ } . For π ∈ P ( u ) \pi\in\mathcal{P}(u) π ∈ P ( u ) , define the set of labels occurring as singleton blocks of π \pi π by
sing ( π ) : = { j ∈ u : { j } ∈ π } . (5) \operatorname{sing}(\pi) := \{j \in u : \{j\} \in\pi\}. \tag*{(5)} sing ( π ) := { j ∈ u : { j } ∈ π } . (5)
For an interval I ⊆ R I \subseteq\mathbb{R} I ⊆ R , ∣ I ∣ |I| ∣ I ∣ denotes its length. Throughout the paper, d x d_x d x and d w d_w d w denote the state and Brownian path dimensions, respectively. An unnamed C C C denotes a positive constant that may change from line to line. Named constants retain the definitions and parameter dependence specified when they are introduced. We write ϕ ( z ) = ( 2 π ) − 1 / 2 e − z 2 / 2 \phi(z) = (2\pi)^{-1/2}e^{-z^2/2} ϕ ( z ) = ( 2 π ) − 1/2 e − z 2 /2 and Φ \Phi Φ for the standard Gaussian density and distribution function, respectively, and ϕ s ( z ) = ∏ j = 1 s ϕ ( z j ) \phi_s(\boldsymbol{z}) = \prod_{j=1}^{s}\phi(z_j) ϕ s ( z ) = ∏ j = 1 s ϕ ( z j ) for the standard Gaussian density on R s \mathbb{R}^s R s . The inverse Φ − 1 \Phi^{-1} Φ − 1 is applied componentwise to vector arguments.
Vectors are denoted by bold symbols and their scalar components by unbolded symbols. The r r r th standard basis vector is denoted by e r \boldsymbol{e}_r e r , with its dimension determined by the context. For d ∈ N d \in\mathbb{N} d ∈ N , I d d \mathrm{Id}_d Id d denotes the d × d d \times d d × d identity matrix. For z = ( z 1 , … , z s ) \boldsymbol{z} = (z_1,\ldots,z_s) z = ( z 1 , … , z s ) and u ⊆ [ s ] u \subseteq[s] u ⊆ [ s ] , we write z u = ( z j ) j ∈ u \boldsymbol{z}_u = (z_j)_{j\in u} z u = ( z j ) j ∈ u and z − u = ( z j ) j ∉ u \boldsymbol{z}_{-u} = (z_j)_{j\notin u} z − u = ( z j ) j ∈ / u . For a sufficiently smooth scalar-valued function f : R s → R f : \mathbb{R}^s \to\mathbb{R} f : R s → R , we define
∂ u f ( z ) : = ( ∏ j ∈ u ∂ ∂ z j ) f ( z ) , ∂ ∅ f = f . \partial_u f(\boldsymbol{z}) := \left(\prod_{j\in u}\frac{\partial}{\partial z_j}\right)f(\boldsymbol{z}), \qquad\partial_{\emptyset}f = f. ∂ u f ( z ) := ( j ∈ u ∏ ∂ z j ∂ ) f ( z ) , ∂ ∅ f = f .
Thus ∂ u \partial_u ∂ u differentiates once with respect to each coordinate indexed by u u u .
For z ∈ R s \boldsymbol{z} \in\mathbb{R}^s z ∈ R s and a matrix A = ( A i j ) ∈ R r × w A = (A_{ij}) \in\mathbb{R}^{r\times w} A = ( A ij ) ∈ R r × w , we use the Euclidean vector norm, the induced matrix 2-norm, and the Hilbert–Schmidt matrix norm:
∣ z ∣ 2 = ( ∑ j = 1 s ∣ z j ∣ 2 ) 1 / 2 , ∥ A ∥ 2 = sup v ∈ R w , ∣ v ∣ 2 ≤ 1 ∣ A v ∣ 2 , ∥ A ∥ H S = ( ∑ i = 1 r ∑ j = 1 w ∣ A i j ∣ 2 ) 1 / 2 . |\boldsymbol{z}|_2 = \left(\sum_{j=1}^{s}|z_j|^2\right)^{1/2}, \qquad\|A\|_2 = \sup_{\boldsymbol{v}\in\mathbb{R}^w,\ |\boldsymbol{v}|_2\leq1}|A\boldsymbol{v}|_2, \qquad\|A\|_{\mathrm{HS}} = \left(\sum_{i=1}^{r}\sum_{j=1}^{w}|A_{ij}|^2\right)^{1/2}. ∣ z ∣ 2 = ( j = 1 ∑ s ∣ z j ∣ 2 ) 1/2 , ∥ A ∥ 2 = v ∈ R w , ∣ v ∣ 2 ≤ 1 sup ∣ A v ∣ 2 , ∥ A ∥ HS = ( i = 1 ∑ r j = 1 ∑ w ∣ A ij ∣ 2 ) 1/2 .
For 1 ≤ q < ∞ 1 \leq q < \infty 1 ≤ q < ∞ , we define the L q L^q L q norms of a scalar-valued random variable V V V and a vector-valued random variable V \boldsymbol{V} V by
∥ V ∥ L q = ( E [ ∣ V ∣ q ] ) 1 / q , ∥ V ∥ L q = ( E [ ∣ V ∣ 2 q ] ) 1 / q , \|V\|_{L^q} = \left(\mathbb{E}[|V|^q]\right)^{1/q}, \qquad\|\boldsymbol{V}\|_{L^q} = \left(\mathbb{E}[|\boldsymbol{V}|_2^q]\right)^{1/q}, ∥ V ∥ L q = ( E [ ∣ V ∣ q ] ) 1/ q , ∥ V ∥ L q = ( E [ ∣ V ∣ 2 q ] ) 1/ q ,
respectively.
We also fix notation for Fréchet derivatives and their norms. For a smooth function f : R d x → R d f f : \mathbb{R}^{d_x} \to\mathbb{R}^{d_f} f : R d x → R d f , the n n n th Fréchet derivative at x ∈ R d x \boldsymbol{x} \in\mathbb{R}^{d_x} x ∈ R d x ,
D x n f ( x ) : ( R d x ) n → R d f , n ≥ 1 , D_{\boldsymbol{x}}^n f(\boldsymbol{x}) : (\mathbb{R}^{d_x})^n \to\mathbb{R}^{d_f}, \qquad n \geq1, D x n f ( x ) : ( R d x ) n → R d f , n ≥ 1 ,
is a symmetric n n n -linear map. For spatial direction vectors v 1 , … , v n ∈ R d x v_1,\ldots,v_n \in\mathbb{R}^{d_x} v 1 , … , v n ∈ R d x , it is given by
D x n f ( x ) [ v 1 , … , v n ] = ∑ i 1 , … , i n = 1 d x ∂ x i 1 ⋯ ∂ x i n f ( x ) ( v 1 ) i 1 ⋯ ( v n ) i n . (6) D_x^n f(x)[v_1,\ldots,v_n] = \sum_{i_1,\ldots,i_n=1}^{d_x} \partial_{x_{i_1}}\cdots\partial_{x_{i_n}}f(x)(v_1)_{i_1}\cdots(v_n)_{i_n}. \tag*{(6)} D x n f ( x ) [ v 1 , … , v n ] = i 1 , … , i n = 1 ∑ d x ∂ x i 1 ⋯ ∂ x i n f ( x ) ( v 1 ) i 1 ⋯ ( v n ) i n . (6)
We define the operator norm and its supremum over x x x by
∥ D x n f ( x ) ∥ o p = sup ∣ v 1 ∣ 2 , … , ∣ v n ∣ 2 ≤ 1 ∣ D x n f ( x ) [ v 1 , … , v n ] ∣ 2 , ∥ D x n f ∥ ∞ = sup x ∈ R d x ∥ D x n f ( x ) ∥ o p . \lVert D_x^n f(x)\rVert_{\mathrm{op}} = \sup_{\lvert v_1\rvert_2,\ldots,\lvert v_n\rvert_2\le1}\lvert D_x^n f(x)[v_1,\ldots,v_n]\rvert_2,\qquad\lVert D_x^n f\rVert_\infty= \sup_{x\in\mathbb{R}^{d_x}}\lVert D_x^n f(x)\rVert_{\mathrm{op}}. ∥ D x n f ( x ) ∥ op = ∣ v 1 ∣ 2 , … , ∣ v n ∣ 2 ≤ 1 sup ∣ D x n f ( x ) [ v 1 , … , v n ] ∣ 2 , ∥ D x n f ∥ ∞ = x ∈ R d x sup ∥ D x n f ( x ) ∥ op .
Assumptions
In this subsection, we state the assumptions used in our analysis. Smoothness and derivative growth conditions on the drift and payoff allow us to estimate mixed derivatives of the integrand defining I m \mathcal{I}_m I m (3) . Additional uniform bounds on the model data and a summability condition on the diffusion columns yield error bounds independent of the state and Brownian path dimensions.
Assumption 2.1. The drift b : [ 0 , T ] × R d x → R d x b : [0,T] \times\mathbb{R}^{d_x} \to\mathbb{R}^{d_x} b : [ 0 , T ] × R d x → R d x is Borel measurable, b ( t , ⋅ ) ∈ C ∞ b(t,\cdot) \in C^\infty b ( t , ⋅ ) ∈ C ∞ for every t t t , and all its spatial derivatives are jointly Borel measurable. There are constants K 0 , B 0 , B 1 > 0 K_0,B_0,B_1>0 K 0 , B 0 , B 1 > 0 and a fixed τ ∈ [ 1 , 3 / 2 ) \tau\in[1,3/2) τ ∈ [ 1 , 3/2 ) such that
sup t ∈ [ 0 , T ] ∣ b ( t , 0 ) ∣ 2 ≤ K 0 , (7) \sup_{t\in[0,T]} \lvert b(t,0)\rvert_2 \le K_0, \tag*{(7)} t ∈ [ 0 , T ] sup ∣ b ( t , 0 ) ∣ 2 ≤ K 0 , (7)
sup t ∈ [ 0 , T ] , x ∈ R d x ∥ D x n b ( t , x ) ∥ o p ≤ B n : = B 0 B 1 n ( n ! ) τ , n ≥ 1. (8) \sup_{t\in[0,T],\,x\in\mathbb{R}^{d_x}} \lVert D_x^n b(t,x)\rVert_{\mathrm{op}} \le B_n := B_0 B_1^n(n!)^\tau,\qquad n\ge1. \tag*{(8)} t ∈ [ 0 , T ] , x ∈ R d x sup ∥ D x n b ( t , x ) ∥ op ≤ B n := B 0 B 1 n ( n ! ) τ , n ≥ 1. (8)
The payoff g : R d x → R g : \mathbb{R}^{d_x} \to\mathbb{R} g : R d x → R is C ∞ C^\infty C ∞ and satisfies, for some constants G 0 , G 1 , β g > 0 G_0,G_1,\beta_g>0 G 0 , G 1 , β g > 0 ,
∥ D x n g ( x ) ∥ o p ≤ G n e β g ∣ x ∣ 2 , G n : = G 0 G 1 n ( n ! ) τ , n ≥ 1. (9) \lVert D_x^n g(x)\rVert_{\mathrm{op}} \le G_n e^{\beta_g\lvert x\rvert_2},\qquad G_n := G_0 G_1^n(n!)^\tau,\qquad n\ge1. \tag*{(9)} ∥ D x n g ( x ) ∥ op ≤ G n e β g ∣ x ∣ 2 , G n := G 0 G 1 n ( n ! ) τ , n ≥ 1. (9)
In particular, the drift b b b is globally Lipschitz in the spatial variable, uniformly in time. The payoff g g g has at most exponential growth, as follows by integrating its first derivative along the segment from 0 0 0 to x x x . Specifically,
∣ b ( t , x ) − b ( t , y ) ∣ 2 ≤ B 1 ∣ x − y ∣ 2 , \lvert b(t,x)-b(t,y)\rvert_2 \le B_1\lvert x-y\rvert_2, ∣ b ( t , x ) − b ( t , y ) ∣ 2 ≤ B 1 ∣ x − y ∣ 2 ,
∣ b ( t , x ) ∣ 2 ≤ K 0 + B 1 ∣ x ∣ 2 , \lvert b(t,x)\rvert_2 \le K_0+B_1\lvert x\rvert_2, ∣ b ( t , x ) ∣ 2 ≤ K 0 + B 1 ∣ x ∣ 2 ,
∣ g ( x ) ∣ ≤ ∣ g ( 0 ) ∣ + G 0 G 1 β g ( e β g ∣ x ∣ 2 − 1 ) ≤ C g e β g ∣ x ∣ 2 , (10) \lvert g(x)\rvert\le\lvert g(0)\rvert+\frac{G_0G_1}{\beta_g}\left(e^{\beta_g\lvert x\rvert_2}-1\right)\le C_g e^{\beta_g\lvert x\rvert_2}, \tag*{(10)} ∣ g ( x )∣ ≤ ∣ g ( 0 )∣ + β g G 0 G 1 ( e β g ∣ x ∣ 2 − 1 ) ≤ C g e β g ∣ x ∣ 2 , (10)
where C g : = ∣ g ( 0 ) ∣ + G 0 G 1 / β g C_g := \lvert g(0)\rvert+G_0G_1/\beta_g C g := ∣ g ( 0 )∣ + G 0 G 1 / β g .
Assumption 2.1 will be used to establish RQMC sampling error bounds uniform in the number of time steps, with constants that may depend on the Brownian path dimension d w d_w d w . For bounds independent of d w d_w d w , we require an additional summability condition on the column norms of the diffusion matrix. To state this condition, define
σ r : = ∣ Σ e r ∣ 2 , Θ v : = ∑ r = 1 d w σ r v , v > 0. (11) \sigma_r := \lvert\Sigma e_r\rvert_2,\qquad\Theta_v := \sum_{r=1}^{d_w}\sigma_r^v,\qquad v>0. \tag*{(11)} σ r := ∣ Σ e r ∣ 2 , Θ v := r = 1 ∑ d w σ r v , v > 0. (11)
Assumption 2.2. Assumption 2.1 holds with constants K 0 , B 0 , B 1 , G 0 , G 1 , β g K_0,B_0,B_1,G_0,G_1,\beta_g K 0 , B 0 , B 1 , G 0 , G 1 , β g and τ \tau τ independent of d x , d w d_x,d_w d x , d w . Moreover, ∣ x 0 ∣ 2 ≤ R 0 \lvert x_0\rvert_2\le R_0 ∣ x 0 ∣ 2 ≤ R 0 for a constant R 0 < ∞ R_0<\infty R 0 < ∞ independent of d x , d w d_x,d_w d x , d w .
Assumption 2.3. For some constant M 2 / 3 < ∞ M_{2/3}<\infty M 2/3 < ∞ independent of d x , d w d_x,d_w d x , d w ,
Θ 2 / 3 = ∑ r = 1 d w ∣ Σ e r ∣ 2 2 / 3 ≤ M 2 / 3 . (12) \Theta_{2/3}=\sum_{r=1}^{d_w}\lvert\Sigma e_r\rvert_2^{2/3}\le M_{2/3}. \tag*{(12)} Θ 2/3 = r = 1 ∑ d w ∣ Σ e r ∣ 2 2/3 ≤ M 2/3 . (12)
For every v ≥ 2 / 3 v \ge2/3 v ≥ 2/3 , the map v ↦ Θ v 1 / v v \mapsto\Theta_v^{1/v} v ↦ Θ v 1/ v is nonincreasing, which gives Θ v ≤ Θ 2 / 3 3 v / 2 \Theta_v \le\Theta_{2/3}^{3v/2} Θ v ≤ Θ 2/3 3 v /2 without any further assumption. Under Assumption 2.3, we therefore obtain
Θ v ≤ Θ 2 / 3 3 v / 2 ≤ M 2 / 3 3 v / 2 , ∥ Σ ∥ H S 2 = Θ 2 ≤ M 2 / 3 3 . (13) \Theta_v \le\Theta_{2/3}^{3v/2} \le M_{2/3}^{3v/2}, \qquad\lVert\Sigma\rVert_{\mathrm{HS}}^2 = \Theta_2 \le M_{2/3}^3. \tag*{(13)} Θ v ≤ Θ 2/3 3 v /2 ≤ M 2/3 3 v /2 , ∥ Σ ∥ HS 2 = Θ 2 ≤ M 2/3 3 . (13)
Brownian bridge construction
In this subsection, we review the Brownian bridge construction and the properties used in our analysis. Throughout the remainder of the paper, m m m denotes the number of time steps and belongs to M : = { 2 J : J = 0 , 1 , … } \mathcal{M} := \{2^J : J = 0,1,\ldots\} M := { 2 J : J = 0 , 1 , … } . For each m ∈ M m \in\mathcal{M} m ∈ M , we use the uniform time grid G : = { t i = i h : i = 0 , … , m } \mathcal{G} := \{t_i = ih : i = 0,\ldots,m\} G := { t i = ih : i = 0 , … , m } with step size h = T / m h = T/m h = T / m . All bounds and suprema over m m m refer to this family of grids.
Construction. We use the dyadic Brownian bridge construction, corresponding to Lévy’s construction of Brownian motion [15 Section 1.1.2] . Let W = ( W ( 1 ) , … , W ( d w ) ) ⊤ \mathbf{W} = (W^{(1)}, \ldots, W^{(d_w)})^\top W = ( W ( 1 ) , … , W ( d w ) ) ⊤ . For each Brownian component r = 1 , … , d w r = 1,\ldots,d_w r = 1 , … , d w , first set
W 0 ( r ) = 0 , W T ( r ) = T z r , W_0^{(r)} = 0, \qquad W_T^{(r)} = \sqrt{T}z_r, W 0 ( r ) = 0 , W T ( r ) = T z r ,
where z 1 , … , z d w z_1,\ldots,z_{d_w} z 1 , … , z d w are independent standard Gaussian inputs. At each refinement level ℓ = 0 , … , J − 1 \ell= 0,\ldots,J-1 ℓ = 0 , … , J − 1 , define
u ℓ , μ = μ T 2 − ℓ , v ℓ , μ = ( μ + 1 ) T 2 − ℓ , c ℓ , μ = u ℓ , μ + v ℓ , μ 2 , μ = 0 , … , 2 ℓ − 1. u_{\ell,\mu} = \mu T2^{-\ell}, \qquad v_{\ell,\mu} = (\mu+1)T2^{-\ell}, \qquad c_{\ell,\mu} = \frac{u_{\ell,\mu}+v_{\ell,\mu}}{2}, \qquad\mu= 0,\ldots,2^\ell-1. u ℓ , μ = μ T 2 − ℓ , v ℓ , μ = ( μ + 1 ) T 2 − ℓ , c ℓ , μ = 2 u ℓ , μ + v ℓ , μ , μ = 0 , … , 2 ℓ − 1.
Generate the midpoint values recursively by
W c ℓ , μ ( r ) = W u ℓ , μ ( r ) + W v ℓ , μ ( r ) 2 + v ℓ , μ − u ℓ , μ 2 z ℓ , μ , r , (14) W_{c_{\ell,\mu}}^{(r)} = \frac{W_{u_{\ell,\mu}}^{(r)} + W_{v_{\ell,\mu}}^{(r)}}{2} + \frac{\sqrt{v_{\ell,\mu}-u_{\ell,\mu}}}{2}z_{\ell,\mu,r}, \tag*{(14)} W c ℓ , μ ( r ) = 2 W u ℓ , μ ( r ) + W v ℓ , μ ( r ) + 2 v ℓ , μ − u ℓ , μ z ℓ , μ , r , (14)
proceeding from level 0 0 0 to level J − 1 J-1 J − 1 for every component. The input z ℓ , μ , r z_{\ell,\mu,r} z ℓ , μ , r corresponds to interval μ \mu μ at level ℓ \ell ℓ in Brownian component r r r . These detail inputs are independent standard Gaussian inputs, also independent of the endpoint inputs.
We order the inputs with the d w d_w d w endpoint inputs first, followed by the detail inputs in lexicographic order of ( ℓ , μ , r ) (\ell,\mu,r) ( ℓ , μ , r ) . Let j j j denote the position of an input in this ordering. For detail inputs,
z ℓ , μ , r = z j , j = d w ( 2 ℓ + μ ) + r , 0 ≤ ℓ < J , 0 ≤ μ < 2 ℓ , 1 ≤ r ≤ d w . (15) z_{\ell,\mu,r} = z_j, \qquad j = d_w(2^\ell+\mu)+r, \qquad0 \le\ell< J,\quad0 \le\mu< 2^\ell,\quad1 \le r \le d_w. \tag*{(15)} z ℓ , μ , r = z j , j = d w ( 2 ℓ + μ ) + r , 0 ≤ ℓ < J , 0 ≤ μ < 2 ℓ , 1 ≤ r ≤ d w . (15)
Collecting the ordered inputs gives z = ( z 1 , … , z s ) ∈ R s z = (z_1,\ldots,z_s) \in\mathbb{R}^s z = ( z 1 , … , z s ) ∈ R s , where s = d w m s = d_wm s = d w m . The endpoint and detail index sets are
E w = { 1 , … , d w } , J m = { d w + 1 , … , s } . (16) \mathcal{E}_w = \{1,\ldots,d_w\}, \qquad\mathcal{J}_m = \{d_w+1,\ldots,s\}. \tag*{(16)} E w = { 1 , … , d w } , J m = { d w + 1 , … , s } . (16)
For j ∈ J m j \in\mathcal{J}_m j ∈ J m , let ( ℓ ( j ) , μ ( j ) , r ( j ) ) (\ell(j),\mu(j),r(j)) ( ℓ ( j ) , μ ( j ) , r ( j )) denote the unique triple determined by (15) , so r ( j ) r(j) r ( j ) identifies the Brownian component constructed using input z j z_j z j . For j ∈ E w j \in\mathcal{E}_w j ∈ E w , set r ( j ) = j r(j) = j r ( j ) = j . When J = 0 J = 0 J = 0 , there are no detail inputs.
Writing the resulting grid values as W t i ( z ) = ( W t i ( r ) ( z ) ) r = 1 d w \mathbf{W}_{t_i}(z) = (W_{t_i}^{(r)}(z))_{r=1}^{d_w} W t i ( z ) = ( W t i ( r ) ( z ) ) r = 1 d w , define B m ∈ R s × s \mathcal{B}_m \in\mathbb{R}^{s \times s} B m ∈ R s × s by the standardized increments in time order:
B m z : = ( W t i ( z ) − W t i − 1 ( z ) h ) i = 1 m . (17) \mathcal{B}_m z := \left(\frac{\mathbf{W}_{t_i}(z)-\mathbf{W}_{t_{i-1}}(z)}{\sqrt{h}}\right)_{i=1}^{m}. \tag*{(17)} B m z := ( h W t i ( z ) − W t i − 1 ( z ) ) i = 1 m . (17)
Since the standardized increments are independent standard Gaussian variables under standard Gaussian input, B m \mathcal{B}_m B m is orthogonal.
Coefficient functions and their properties. The BB grid values admit a finite Lévy–Ciesielski representation in Faber–Schauder hat functions [15 Proposition 1.44 and Remark 1.45] . To describe its coefficients, define the unit-height hat function
Λ ( x ) = { 2 x , 0 ≤ x ≤ 1 2 , 2 ( 1 − x ) , 1 2 < x ≤ 1 , 0 , otherwise , \Lambda(x)=
\begin{cases}
2x, & 0\le x\le\frac{1}{2},\\
2(1-x), & \frac{1}{2}<x\le1,\\
0, & \text{otherwise},
\end{cases} Λ ( x ) = ⎩ ⎨ ⎧ 2 x , 2 ( 1 − x ) , 0 , 0 ≤ x ≤ 2 1 , 2 1 < x ≤ 1 , otherwise ,
and the scalar coefficient functions, for t ∈ [ 0 , T ] t\in[0,T] t ∈ [ 0 , T ] , by
ϑ j ( t ) = { t T , j ∈ E w , T 2 2 − ℓ ( j ) / 2 Λ ( 2 ℓ ( j ) t T − μ ( j ) ) , j ∈ J m . (18) \vartheta_j(t)=
\begin{cases}
\frac{t}{\sqrt{T}}, & j\in\mathcal{E}_w,\\
\frac{\sqrt{T}}{2}2^{-\ell(j)/2}\Lambda\left(\frac{2^{\ell(j)}t}{T}-\mu(j)\right), & j\in\mathcal{J}_m.
\end{cases} \tag*{(18)} ϑ j ( t ) = ⎩ ⎨ ⎧ T t , 2 T 2 − ℓ ( j ) /2 Λ ( T 2 ℓ ( j ) t − μ ( j ) ) , j ∈ E w , j ∈ J m . (18)
Here ϑ j \vartheta_j ϑ j is the coefficient of input z j z_j z j in Brownian component r ( j ) r(j) r ( j ) . For j ∈ J m j\in\mathcal{J}_m j ∈ J m , its supporting interval is
I j = [ μ ( j ) T 2 − ℓ ( j ) , ( μ ( j ) + 1 ) T 2 − ℓ ( j ) ] . (19) I_j=[\mu(j)T2^{-\ell(j)},(\mu(j)+1)T2^{-\ell(j)}]. \tag*{(19)} I j = [ μ ( j ) T 2 − ℓ ( j ) , ( μ ( j ) + 1 ) T 2 − ℓ ( j ) ] . (19)
Define the corresponding coefficients in the diffusion term by
ξ j ( t ) : = Σ e r ( j ) ϑ j ( t ) , ∥ ξ j ∥ ∞ : = sup 0 ≤ t ≤ T ∣ ξ j ( t ) ∣ 2 . (20) \xi_j(t):=\Sigma e_{r(j)}\vartheta_j(t),\qquad\|\xi_j\|_\infty:=\sup_{0\le t\le T}|\xi_j(t)|_2. \tag*{(20)} ξ j ( t ) := Σ e r ( j ) ϑ j ( t ) , ∥ ξ j ∥ ∞ := 0 ≤ t ≤ T sup ∣ ξ j ( t ) ∣ 2 . (20)
For z ∈ R s z\in\mathbb{R}^s z ∈ R s and i = 0 , … , m i=0,\ldots,m i = 0 , … , m , the resulting linear representations are [15 Proposition 1.44 and Remark 1.45]
W t i ( z ) = ∑ j = 1 s e r ( j ) ϑ j ( t i ) z j , Σ W t i ( z ) = ∑ j = 1 s ξ j ( t i ) z j . (21) W_{t_i}(z)=\sum_{j=1}^{s}e_{r(j)}\vartheta_j(t_i)z_j,\qquad\Sigma W_{t_i}(z)=\sum_{j=1}^{s}\xi_j(t_i)z_j. \tag*{(21)} W t i ( z ) = j = 1 ∑ s e r ( j ) ϑ j ( t i ) z j , Σ W t i ( z ) = j = 1 ∑ s ξ j ( t i ) z j . (21)
Lemma 2.4. For j ∈ J m j\in\mathcal{J}_m j ∈ J m with ℓ ( j ) = ℓ \ell(j)=\ell ℓ ( j ) = ℓ , we have
∣ I j ∣ = T 2 − ℓ , ∥ ϑ j ∥ ∞ = T 2 2 − ℓ / 2 , |I_j|=T2^{-\ell},\qquad\|\vartheta_j\|_\infty=\frac{\sqrt{T}}{2}2^{-\ell/2}, ∣ I j ∣ = T 2 − ℓ , ∥ ϑ j ∥ ∞ = 2 T 2 − ℓ /2 , ∥ ξ j ∥ ∞ = 1 2 σ r ( j ) ∣ I j ∣ , ξ j ( T ) = 0. (22) \|\xi_j\|_\infty=\frac{1}{2}\sigma_{r(j)}\sqrt{|I_j|},\qquad\xi_j(T)=0. \tag*{(22)} ∥ ξ j ∥ ∞ = 2 1 σ r ( j ) ∣ I j ∣ , ξ j ( T ) = 0. (22) For j ∈ E w j\in\mathcal{E}_w j ∈ E w ,
ϑ j ( T ) = ∥ ϑ j ∥ ∞ = T , ∣ ξ j ( T ) ∣ 2 = ∥ ξ j ∥ ∞ = T σ j . \vartheta_j(T)=\|\vartheta_j\|_\infty=\sqrt{T},\qquad|\xi_j(T)|_2=\|\xi_j\|_\infty=\sqrt{T}\sigma_j. ϑ j ( T ) = ∥ ϑ j ∥ ∞ = T , ∣ ξ j ( T ) ∣ 2 = ∥ ξ j ∥ ∞ = T σ j .
Proof. The assertions follow directly from (2.14), (2.15), and the definition of ξ j \xi_j ξ j .
Euler–Maruyama integrand
Recall the EM recursion (2) . Under the BB construction, its standardized increments are given by B m z B_mz B m z . Define
X t i h ( z ) : = X ~ t i ( B m z ) , i = 0 , … , m . (23) X^h_{t_i}(z):=\widetilde{X}_{t_i}(B_mz),\qquad i=0,\ldots,m. \tag*{(23)} X t i h ( z ) := X t i ( B m z ) , i = 0 , … , m . (23)
All input derivatives below are taken with respect to the BB coordinates z z z . By (2) and (17) , we have X t 0 h ( z ) = x 0 X^h_{t_0}(z)=x_0 X t 0 h ( z ) = x 0 and
X t i + 1 h ( z ) = X t i h ( z ) + h b ( t i , X t i h ( z ) ) + Σ ( W t i + 1 ( z ) − W t i ( z ) ) , 0 ≤ i < m . (24) X^h_{t_{i+1}}(z)=X^h_{t_i}(z)+h\,b(t_i,X^h_{t_i}(z))+\Sigma\left(W_{t_{i+1}}(z)-W_{t_i}(z)\right),\qquad0\le i<m. \tag*{(24)} X t i + 1 h ( z ) = X t i h ( z ) + h b ( t i , X t i h ( z )) + Σ ( W t i + 1 ( z ) − W t i ( z ) ) , 0 ≤ i < m . (24)
We define the corresponding integrand by
F m ( z ) : = g ( X t m h ( z ) ) , z ∈ R s . (25) F_m(z):=g\left(X^h_{t_m}(z)\right),\qquad z\in\mathbb{R}^s. \tag*{(25)} F m ( z ) := g ( X t m h ( z ) ) , z ∈ R s . (25)
Since B m B_m B m is orthogonal, the BB transformation leaves the Gaussian integral unchanged. Thus,
I m = E [ F m ( Z ) ] = ∫ R s F m ( z ) φ s ( z ) d z , Z ∼ N ( 0 , I d s ) . (26) I_m=\mathbb{E}[F_m(Z)]=\int_{\mathbb{R}^s}F_m(z)\varphi_s(z)\,\mathrm{d}z,\qquad Z\sim N(0,I_d{}_s). \tag*{(26)} I m = E [ F m ( Z )] = ∫ R s F m ( z ) φ s ( z ) d z , Z ∼ N ( 0 , I d s ) . (26)
We will analyze F m F_m F m in the weighted function space introduced in § 2.5 .
Randomly shifted lattice rules and median estimators
In this subsection, we review randomly shifted rank-1 lattice rules and median estimators following [7 , 28 ] .
For a prime N ≥ 2 N \ge2 N ≥ 2 , let a ∈ { 1 , … , N − 1 } s \boldsymbol{a} \in\{1,\ldots,N-1\}^{s} a ∈ { 1 , … , N − 1 } s be a generating vector and let Δ \boldsymbol{\Delta} Δ be uniformly distributed on [ 0 , 1 ] s [0,1]^{s} [ 0 , 1 ] s . The lattice points are
u n = { n a / N + Δ } , n = 0 , … , N − 1 , (27) \boldsymbol{u}_{n} = \{n\boldsymbol{a}/N+\boldsymbol{\Delta}\}, \qquad n=0,\ldots,N-1, \tag*{(27)} u n = { n a / N + Δ } , n = 0 , … , N − 1 , (27)
where braces denote componentwise fractional parts. For the Gaussian integral I ( F ) : = ∫ R s F ( z ) ϕ s ( z ) d z \mathcal{I}(F) := \int_{\mathbb{R}^{s}} F(\boldsymbol{z})\phi_{s}(\boldsymbol{z})\,\mathrm{d}\boldsymbol{z} I ( F ) := ∫ R s F ( z ) ϕ s ( z ) d z , the randomly shifted lattice estimator is
Q a , Δ ( F ) : = 1 N ∑ n = 0 N − 1 F ( Φ − 1 ( u n ) ) . Q_{\boldsymbol{a},\boldsymbol{\Delta}}(F) := \frac{1}{N}\sum_{n=0}^{N-1} F\left(\Phi^{-1}(\boldsymbol{u}_{n})\right). Q a , Δ ( F ) := N 1 n = 0 ∑ N − 1 F ( Φ − 1 ( u n ) ) .
The uniform shift makes each lattice point uniformly distributed, so E Δ [ Q a , Δ ( F ) ] = I ( F ) \mathbb{E}_{\boldsymbol{\Delta}}[Q_{\boldsymbol{a},\boldsymbol{\Delta}}(F)] = \mathcal{I}(F) E Δ [ Q a , Δ ( F )] = I ( F ) for integrable F F F . In particular, our estimate of I m \mathcal{I}_{m} I m is
Q a , Δ N , m : = Q a , Δ ( F m ) = 1 N ∑ n = 0 N − 1 F m ( Φ − 1 ( { n a / N + Δ } ) ) . (28) Q_{\boldsymbol{a},\boldsymbol{\Delta}}^{N,m} := Q_{\boldsymbol{a},\boldsymbol{\Delta}}(F_{m}) = \frac{1}{N}\sum_{n=0}^{N-1} F_{m}\left(\Phi^{-1}(\{n\boldsymbol{a}/N+\boldsymbol{\Delta}\})\right). \tag*{(28)} Q a , Δ N , m := Q a , Δ ( F m ) = N 1 n = 0 ∑ N − 1 F m ( Φ − 1 ({ n a / N + Δ }) ) . (28)
We now follow the median approach in [7 , 28 ] to combine independent randomly shifted lattice estimates. For an odd integer R = 2 k − 1 R=2k-1 R = 2 k − 1 , k ≥ 1 k\ge1 k ≥ 1 , draw R R R independent pairs ( A 1 , Δ 1 ) , … , ( A R , Δ R ) (\boldsymbol{A}_{1},\boldsymbol{\Delta}_{1}),\ldots,(\boldsymbol{A}_{R},\boldsymbol{\Delta}_{R}) ( A 1 , Δ 1 ) , … , ( A R , Δ R ) , where each A ν \boldsymbol{A}_{\nu} A ν is uniform on { 1 , … , N − 1 } s \{1,\ldots,N-1\}^{s} { 1 , … , N − 1 } s and each Δ ν \boldsymbol{\Delta}_{\nu} Δ ν is uniform on [ 0 , 1 ] s [0,1]^{s} [ 0 , 1 ] s , independently of A ν \boldsymbol{A}_{\nu} A ν . The median estimator is
M R , N , m : = median ( Q A 1 , Δ 1 N , m , … , Q A R , Δ R N , m ) . (29) M_{R,N,m} := \operatorname{median}\left(Q_{\boldsymbol{A}_{1},\boldsymbol{\Delta}_{1}}^{N,m},\ldots,Q_{\boldsymbol{A}_{R},\boldsymbol{\Delta}_{R}}^{N,m}\right). \tag*{(29)} M R , N , m := median ( Q A 1 , Δ 1 N , m , … , Q A R , Δ R N , m ) . (29)
This estimator requires no dedicated construction of generating vectors. Taking the median can reduce the probability of a large integration error; see, for example, [25 , 7 , 28 ] .
Weighted Gaussian function space
In this subsection, we consider a Gaussian specialization of the weighted function space framework of Nichols and Kuo [16 ] .
Fix α > 0 \alpha>0 α > 0 and define the auxiliary weight function ψ ( t ) : = e − α ∣ t ∣ \psi(t):=e^{-\alpha|t|} ψ ( t ) := e − α ∣ t ∣ , t ∈ R t\in\mathbb{R} t ∈ R . Write ϕ − u ( z − u ) : = ∏ j ∉ u ϕ ( z j ) \phi_{-u}(\boldsymbol{z}_{-u}):=\prod_{j\notin u}\phi(z_{j}) ϕ − u ( z − u ) := ∏ j ∈ / u ϕ ( z j ) . For nonnegative subset weights γ : = ( γ u ) u ⊆ [ s ] \boldsymbol{\gamma}:=(\gamma_{u})_{u\subseteq[s]} γ := ( γ u ) u ⊆ [ s ] with γ ∅ = 1 \gamma_{\varnothing}=1 γ ∅ = 1 , the weighted unanchored Sobolev space H s , γ \mathcal{H}_{s,\boldsymbol{\gamma}} H s , γ consists of locally integrable functions F : R s → R F:\mathbb{R}^{s}\to\mathbb{R} F : R s → R with the required weak mixed derivatives for which the following norm is finite.
∥ F ∥ H s , γ 2 : = ∑ u ⊆ [ s ] 1 γ u ∫ R ∣ u ∣ ∣ ∫ R s − ∣ u ∣ ∂ u F ( z ) ϕ − u ( z − u ) d z − u ∣ 2 ∏ j ∈ u ψ ( z j ) 2 d z u . (30) \lVert F\rVert_{\mathcal{H}_{s,\boldsymbol{\gamma}}}^{2}:=\sum_{u\subseteq[s]}\frac{1}{\gamma_{u}}\int_{\mathbb{R}^{|u|}}\left|\int_{\mathbb{R}^{s-|u|}}\partial_{u}F(\boldsymbol{z})\phi_{-u}(\boldsymbol{z}_{-u})\,\mathrm{d}\boldsymbol{z}_{-u}\right|^{2}\prod_{j\in u}\psi(z_{j})^{2}\,\mathrm{d}\boldsymbol{z}_{u}. \tag*{(30)} ∥ F ∥ H s , γ 2 := u ⊆ [ s ] ∑ γ u 1 ∫ R ∣ u ∣ ∫ R s − ∣ u ∣ ∂ u F ( z ) ϕ − u ( z − u ) d z − u 2 j ∈ u ∏ ψ ( z j ) 2 d z u . (30)
If γ u = 0 \gamma_{u}=0 γ u = 0 , we require the corresponding numerator in (2.26) to vanish for every function in H s , γ \mathcal{H}_{s,\boldsymbol{\gamma}} H s , γ , and we use the convention 0 / 0 : = 0 0/0:=0 0/0 := 0 . The subset weights γ u \gamma_{u} γ u describe the relative importance of coordinate subsets u u u by scaling their contributions to the norm.
Following Nichols and Kuo [16 ] , we define the shift-averaged worst-case error of the rules in § 2.4 by
[ e s , N s h ( a ; γ ) ] 2 : = E Δ sup ∥ G ∥ H s , γ ≤ 1 ∣ Q a , Δ ( G ) − I ( G ) ∣ 2 . (31) [e_{s,N}^{\mathrm{sh}}(\boldsymbol{a};\boldsymbol{\gamma})]^{2}:=\mathbb{E}_{\boldsymbol{\Delta}}\sup_{\lVert G\rVert_{\mathcal{H}_{s,\boldsymbol{\gamma}}\leq1}}\left|Q_{\boldsymbol{a},\boldsymbol{\Delta}}(G)-\mathcal{I}(G)\right|^{2}. \tag*{(31)} [ e s , N sh ( a ; γ ) ] 2 := E Δ ∥ G ∥ H s , γ ≤ 1 sup ∣ Q a , Δ ( G ) − I ( G ) ∣ 2 . (31)
The following lemma is a Gaussian specialization of [28 Theorem 1, Eq. (13)] .
Lemma 2.5. Fix λ ∈ ( 1 / 2 , 1 ) \lambda\in(1/2,1) λ ∈ ( 1/2 , 1 ) and choose δ ∗ ∈ ( 1 / ( 2 λ ) , 1 ) \delta_* \in(1/(2\lambda),1) δ ∗ ∈ ( 1/ ( 2 λ ) , 1 ) . Set
C α , δ ∗ : = 2 π e α 2 / ( 1 − δ ∗ ) π 2 δ ∗ δ ∗ ( 1 − δ ∗ ) , ρ λ : = 2 C α , δ ∗ λ ζ ( 2 δ ∗ λ ) . (32) C_{\alpha,\delta_*} := \frac{\sqrt{2\pi}\,e^{\alpha^2/(1-\delta_*)}}{\pi^{2\delta_*}\delta_*(1-\delta_*)}, \qquad\rho_\lambda:= 2C_{\alpha,\delta_*}^{\lambda}\zeta(2\delta_*\lambda). \tag*{(32)} C α , δ ∗ := π 2 δ ∗ δ ∗ ( 1 − δ ∗ ) 2 π e α 2 / ( 1 − δ ∗ ) , ρ λ := 2 C α , δ ∗ λ ζ ( 2 δ ∗ λ ) . (32) Here ζ \zeta ζ is the Riemann zeta function. For prime N N N and nonnegative weights γ u \gamma_u γ u , let A A A be uniform on { 1 , … , N − 1 } s \{1,\ldots,N-1\}^s { 1 , … , N − 1 } s . Then
E A [ e s , N s h ( A ; γ ) 2 ] ≤ 1 N − 1 ∑ ∅ ≠ u ⊆ [ s ] γ u λ ∣ u ∣ . (33) \mathbb{E}_A\left[e_{s,N}^{\mathrm{sh}}(A;\gamma)^2\right] \le\frac{1}{N-1}\sum_{\emptyset\ne u\subseteq[s]}\gamma_u\lambda^{|u|}. \tag*{(33)} E A [ e s , N sh ( A ; γ ) 2 ] ≤ N − 1 1 ∅ = u ⊆ [ s ] ∑ γ u λ ∣ u ∣ . (33) Proof. The constant C α , δ ∗ C_{\alpha,\delta_*} C α , δ ∗ in (32) is given by [11 Example 5] for the Gaussian density and auxiliary weight used here. Since N N N is prime, exactly N − 1 N-1 N − 1 integers in { 1 , … , N − 1 } \{1,\ldots,N-1\} { 1 , … , N − 1 } are coprime to N N N ; [28 Theorem 1, Eq. (13)] , with C j = C α , δ ∗ C_j=C_{\alpha,\delta_*} C j = C α , δ ∗ and r j = δ ∗ r_j=\delta_* r j = δ ∗ for every coordinate (in the notation of [28 ] ), then gives (33) .
Main results
This section presents the sampling error bounds for the random lattice (28) and median estimators (29) , with constants independent of the number of time steps m m m . We then state an assumption on the Euler–Maruyama time discretization error and combine the two error bounds to obtain estimates for the total error.
Sampling error
Theorem 3.1. Suppose Assumption 2.1 holds. For every ε ∈ ( 0 , 1 / 2 ) \varepsilon\in(0,1/2) ε ∈ ( 0 , 1/2 ) , there exists a constant C ε > 0 C_\varepsilon>0 C ε > 0 , depending only on ε \varepsilon ε , τ \tau τ , T T T , K 0 K_0 K 0 , B 0 B_0 B 0 , B 1 B_1 B 1 , G 0 G_0 G 0 , G 1 G_1 G 1 , β g \beta_g β g , ∣ x 0 ∣ 2 |x_0|_2 ∣ x 0 ∣ 2 , Θ 1 \Theta_1 Θ 1 , Θ 2 / 3 \Theta_{2/3} Θ 2/3 , such that for every m ∈ M m\in\mathcal{M} m ∈ M and every prime N ≥ 2 N\ge2 N ≥ 2 , the single random lattice rule satisfies
∥ Q A , Δ N , m − I m ∥ L 1 ≤ C ε N − 1 + ε . (34) \left\|Q_{\boldsymbol{A},\Delta}^{N,m}-\mathcal{I}_m\right\|_{L_1}\le C_\varepsilon N^{-1+\varepsilon}. \tag*{(34)} Q A , Δ N , m − I m L 1 ≤ C ε N − 1 + ε . (34) Let R = 2 k − 1 R=2k-1 R = 2 k − 1 for a fixed integer k ≥ 1 k\ge1 k ≥ 1 . For every q q q satisfying 1 ≤ q < k / ( 1 − ε ) 1\le q<k/(1-\varepsilon) 1 ≤ q < k / ( 1 − ε ) , there exists a constant C ε , q , R > 0 C_{\varepsilon,q,R}>0 C ε , q , R > 0 , depending only on the same parameters as C ε C_\varepsilon C ε and on q q q , R R R , such that the median estimator in (29) satisfies
∥ M R , N , m − I m ∥ L q ≤ C ε , q , R N − 1 + ε . (35) \left\|M_{R,N,m}-\mathcal{I}_m\right\|_{L_q}\le C_{\varepsilon,q,R}N^{-1+\varepsilon}. \tag*{(35)} ∥ M R , N , m − I m ∥ L q ≤ C ε , q , R N − 1 + ε . (35) The expectations are over the generating vectors and random shifts.
With the other parameters fixed, the constants in Theorem 3.1 may still depend on d x , d w d_x,d_w d x , d w through Θ 1 \Theta_1 Θ 1 and Θ 2 / 3 \Theta_{2/3} Θ 2/3 . The following corollary gives the same convergence rates with constants independent of d x d_x d x and d w d_w d w under uniform bounds on the model parameters and a summability condition on the columns of Σ \Sigma Σ .
Corollary 3.3. Suppose the assumptions of Theorem 3.1 hold, together with Assumptions 2.2 and 2.3. Then the bounds (34) and (35) hold with constants C ε C_\varepsilon C ε and C ε , q , R C_{\varepsilon,q,R} C ε , q , R independent of m m m , N N N , d x d_x d x , d w d_w d w . These constants may depend on T T T , the uniform model bounds, and the parameters indicated by their subscripts.
Theorem 3.1 and Corollary 3.3 are proved in § 5.3 .
Remark 3.4. For any orthogonal matrix U U U , replacing Σ \Sigma Σ by Σ U \Sigma U Σ U preserves the law of the SDE and its Euler–Maruyama approximation. Let ς j \varsigma_j ς j denote the nonzero singular values of Σ \Sigma Σ . Then
min U T U = I d w ∑ r = 1 d w ∣ Σ U e r ∣ 2 2 / 3 = ∑ j = 1 rank ( Σ ) ς j 2 / 3 . \min_{U^{\mathsf{T}}U=I_{d_w}} \sum_{r=1}^{d_w} \lvert\Sigma U e_r\rvert_2^{2/3} = \sum_{j=1}^{\operatorname{rank}(\Sigma)} \varsigma_j^{2/3}. U T U = I d w min r = 1 ∑ d w ∣ Σ U e r ∣ 2 2/3 = j = 1 ∑ rank ( Σ ) ς j 2/3 .
Indeed, pad the singular values with zeros to obtain d w d_w d w values and write
Σ T Σ = V diag ( ς 1 2 , … , ς d w 2 ) V T . \Sigma^{\mathsf{T}}\Sigma= V \operatorname{diag}(\varsigma_1^2,\ldots,\varsigma_{d_w}^2)V^{\mathsf{T}}. Σ T Σ = V diag ( ς 1 2 , … , ς d w 2 ) V T .
Here V ∈ R d w × d w V \in\mathbb{R}^{d_w \times d_w} V ∈ R d w × d w is orthogonal. Set U ~ = V T U = ( u ~ j r ) 1 ≤ j , r ≤ d w \widetilde{U}=V^{\mathsf{T}}U=(\widetilde{u}_{jr})_{1\leq j,r\leq d_w} U = V T U = ( u j r ) 1 ≤ j , r ≤ d w . By concavity of x 1 / 3 x^{1/3} x 1/3 and orthogonality of U ~ \widetilde{U} U ,
∑ r = 1 d w ∣ Σ U e r ∣ 2 2 / 3 = ∑ r = 1 d w ( ∑ j = 1 d w u ~ j r 2 ς j 2 ) 1 / 3 ≥ ∑ r , j = 1 d w u ~ j r 2 ς j 2 / 3 = ∑ j = 1 d w ς j 2 / 3 . \sum_{r=1}^{d_w}\lvert\Sigma Ue_r\rvert_2^{2/3}
=\sum_{r=1}^{d_w}\left(\sum_{j=1}^{d_w}\widetilde{u}_{jr}^{\,2}\varsigma_j^2\right)^{1/3}
\geq\sum_{r,j=1}^{d_w}\widetilde{u}_{jr}^{\,2}\varsigma_j^{2/3}
=\sum_{j=1}^{d_w}\varsigma_j^{2/3}. r = 1 ∑ d w ∣ Σ U e r ∣ 2 2/3 = r = 1 ∑ d w ( j = 1 ∑ d w u j r 2 ς j 2 ) 1/3 ≥ r , j = 1 ∑ d w u j r 2 ς j 2/3 = j = 1 ∑ d w ς j 2/3 .
Equality holds for U = V U=V U = V , the matrix of right singular vectors. Thus there exists a choice of orthogonal matrices across dimensions for which the transformed diffusion matrices satisfy Assumption 2.3 if and only if the singular-value sums are uniformly bounded.
Euler–Maruyama time discretization error
Our main focus is on the sampling error relative to I m \mathcal{I}_m I m . To obtain total error bounds relative to I \mathcal{I} I , we additionally assume the following rate for the Euler–Maruyama time discretization error.
Assumption 3.5. For some θ > 0 \theta>0 θ > 0 and C b i a s < ∞ C_{\mathrm{bias}}<\infty C bias < ∞ , independent of m ∈ M m\in\mathcal{M} m ∈ M ,
∣ I m − I ∣ ≤ C b i a s m − θ . (36) \lvert\mathcal{I}_m-\mathcal{I}\rvert\leq C_{\mathrm{bias}}m^{-\theta}. \tag*{(36)} ∣ I m − I ∣ ≤ C bias m − θ . (36)
The following two theorems verify Assumption 3.5 with θ = 1 / 2 \theta=1/2 θ = 1/2 and θ = 1 \theta=1 θ = 1 , respectively, under different time regularity conditions on b b b .
Theorem 3.6. Suppose Assumption 2.1 holds and, for some L ~ t < ∞ \widetilde{L}_t<\infty L t < ∞ ,
∣ b ( t , x ) − b ( s , x ) ∣ 2 ≤ L ~ t ( 1 + ∣ x ∣ 2 ) ∣ t − s ∣ 1 / 2 , s , t ∈ [ 0 , T ] , x ∈ R d x . (37) \lvert b(t,x)-b(s,x)\rvert_2\leq\widetilde{L}_t(1+\lvert x\rvert_2)\lvert t-s\rvert^{1/2},\qquad s,t\in[0,T],\quad x\in\mathbb{R}^{d_x}. \tag*{(37)} ∣ b ( t , x ) − b ( s , x ) ∣ 2 ≤ L t ( 1 + ∣ x ∣ 2 ) ∣ t − s ∣ 1/2 , s , t ∈ [ 0 , T ] , x ∈ R d x . (37) Let X X X solve the SDE (1.1), and let X h X^h X h be the Euler–Maruyama approximation defined by (2.20), driven by the same Brownian motion W W W . Then the following conclusions hold.
(i) For fixed d x , d w d_x,d_w d x , d w , there are constants C s t r , 1 / 2 C_{\mathrm{str},1/2} C str , 1/2 and C b i a s , 1 / 2 C_{\mathrm{bias},1/2} C bias , 1/2 , independent of m ∈ M m\in\mathcal{M} m ∈ M , such that
∥ max 0 ≤ i ≤ m ∣ X t i h − X t i ∣ 2 ∥ L 2 ≤ C s t r , 1 / 2 m − 1 / 2 , (38) \left\|\max_{0\leq i\leq m}\lvert X^h_{t_i}-X_{t_i}\rvert_2\right\|_{L^2}\leq C_{\mathrm{str},1/2}m^{-1/2}, \tag*{(38)} 0 ≤ i ≤ m max ∣ X t i h − X t i ∣ 2 L 2 ≤ C str , 1/2 m − 1/2 , (38) ∣ I m − I ∣ ≤ C b i a s , 1 / 2 m − 1 / 2 . (39) \lvert\mathcal{I}_m-\mathcal{I}\rvert\leq C_{\mathrm{bias},1/2}m^{-1/2}. \tag*{(39)} ∣ I m − I ∣ ≤ C bias , 1/2 m − 1/2 . (39) The constant C s t r , 1 / 2 C_{\mathrm{str},1/2} C str , 1/2 depends only on T T T , K 0 K_0 K 0 , B 1 B_1 B 1 , L ~ t \widetilde{L}_t L t , ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 and ∥ Σ ∥ H S \lVert\Sigma\rVert_{\mathrm{HS}} ∥ Σ ∥ HS ; C b i a s , 1 / 2 C_{\mathrm{bias},1/2} C bias , 1/2 may also depend on G 0 G_0 G 0 , G 1 G_1 G 1 and β g \beta_g β g .
(ii) If Assumptions 2.2 and 2.3 also hold, and L ~ t \widetilde{L}_t L t in (3.4) is independent of d x , d w d_x,d_w d x , d w , then both constants can be chosen independent of m , d x , d w m,d_x,d_w m , d x , d w . They depend only on T , L ~ t , K 0 , B 0 , B 1 , G 0 , G 1 , β g , τ , R 0 T,\widetilde{L}_t,K_0,B_0,B_1,G_0,G_1,\beta_g,\tau,R_0 T , L t , K 0 , B 0 , B 1 , G 0 , G 1 , β g , τ , R 0 and M 2 / 3 M_{2/3} M 2/3 .
Theorem 3.7. Suppose Assumption 2.1 holds and, for some L t < ∞ L_t < \infty L t < ∞ ,
∣ b ( t , x ) − b ( s , x ) ∣ 2 ≤ L t ( 1 + ∣ x ∣ 2 ) ∣ t − s ∣ , s , t ∈ [ 0 , T ] , x ∈ R d x . (40) |b(t,x)-b(s,x)|_2 \le L_t(1+|x|_2)|t-s|,\qquad s,t\in[0,T],\quad x\in\mathbb{R}^{d_x}. \tag*{(40)} ∣ b ( t , x ) − b ( s , x ) ∣ 2 ≤ L t ( 1 + ∣ x ∣ 2 ) ∣ t − s ∣ , s , t ∈ [ 0 , T ] , x ∈ R d x . (40) Then the following conclusions hold.
(i) For fixed d x , d w d_x,d_w d x , d w , there is a constant C b i a s C_{\mathrm{bias}} C bias , independent of m ∈ M m\in\mathcal{M} m ∈ M , such that
∣ I m − I ∣ ≤ C b i a s m − 1 . (41) |I_m-I|\le C_{\mathrm{bias}}m^{-1}. \tag*{(41)} ∣ I m − I ∣ ≤ C bias m − 1 . (41) The constant depends only on T , K 0 , B 1 , B 2 , L t , G 0 , G 1 , β g , ∣ x 0 ∣ 2 T,K_0,B_1,B_2,L_t,G_0,G_1,\beta_g,|x_0|_2 T , K 0 , B 1 , B 2 , L t , G 0 , G 1 , β g , ∣ x 0 ∣ 2 and ∥ Σ ∥ H S \|\Sigma\|_{\mathrm{HS}} ∥Σ ∥ HS .
(ii) If Assumptions 2.2 and 2.3 also hold, and L t L_t L t in (3.7) is independent of d x , d w d_x,d_w d x , d w , then C b i a s C_{\mathrm{bias}} C bias in (3.8) can be chosen independent of m , d x , d w m,d_x,d_w m , d x , d w . It depends only on T , L t , K 0 , B 0 , B 1 , G 0 , G 1 , β g , τ , R 0 T,L_t,K_0,B_0,B_1,G_0,G_1,\beta_g,\tau,R_0 T , L t , K 0 , B 0 , B 1 , G 0 , G 1 , β g , τ , R 0 and M 2 / 3 M_{2/3} M 2/3 .
The proofs are given in Appendix E.
Total error
Combining the sampling estimates with Assumption 3.5 gives the following total error bounds.
Corollary 3.8. Under Assumptions 2.1 and 3.5, the rules in Theorem 3.1 satisfy
∥ Q A , Δ N , m − I ∥ L 1 ≤ C ε N − 1 + ε + C b i a s m − θ , (42) \left\|Q_{A,\Delta}^{N,m}-I\right\|_{L^1}\le C_{\varepsilon}N^{-1+\varepsilon}+C_{\mathrm{bias}}m^{-\theta}, \tag*{(42)} Q A , Δ N , m − I L 1 ≤ C ε N − 1 + ε + C bias m − θ , (42) ∥ M R , N , m − I ∥ L q ≤ C ε , q , R N − 1 + ε + C b i a s m − θ , (43) \left\|M_{R,N,m}-I\right\|_{L^q}\le C_{\varepsilon,q,R}N^{-1+\varepsilon}+C_{\mathrm{bias}}m^{-\theta}, \tag*{(43)} ∥ M R , N , m − I ∥ L q ≤ C ε , q , R N − 1 + ε + C bias m − θ , (43) with the same ranges of m , N , ε , q , R m,N,\varepsilon,q,R m , N , ε , q , R as in the sampling results. Under the assumptions of Corollary 3.3, the sampling constants C ε C_{\varepsilon} C ε and C ε , q , R C_{\varepsilon,q,R} C ε , q , R can be chosen independent of d x , d w d_x,d_w d x , d w . All constants are then independent of d x , d w d_x,d_w d x , d w if θ \theta θ and C b i a s C_{\mathrm{bias}} C bias in Assumption 3.5 are common to all dimensions.
Proof. Apply the triangle inequality to each sampling estimate and (3.3).
Regularity of the Euler–Maruyama integrand
In this section, we establish mixed derivative bounds for the Euler–Maruyama integrand F m F_m F m and prove their summability uniformly in m m m . These estimates will be used in Section 5.3 to derive the sampling error bounds.
Unless otherwise stated, constants in the estimates below are independent of m m m . Their dependence on other parameters is specified when relevant.
For ∅ ≠ u ⊆ [ s ] \emptyset\ne u\subseteq[s] ∅ = u ⊆ [ s ] , define the normalized derivative envelope by
D m , u : = sup z ∈ R s ∣ ∂ u F m ( z ) ∣ e β g ∣ X t m h ( z ) ∣ 2 . (44) D_{m,u}:=\sup_{z\in\mathbb{R}^s}\frac{|\partial_uF_m(z)|}{e^{\beta_g|X_{t_m}^h(z)|_2}}. \tag*{(44)} D m , u := z ∈ R s sup e β g ∣ X t m h ( z ) ∣ 2 ∣ ∂ u F m ( z ) ∣ . (44)
Theorem 4.1. Suppose Assumption 2.1 holds. For every κ > 0 \kappa>0 κ > 0 and p > 2 / 3 p>2/3 p > 2/3 , there exists a constant C D ( κ , p ; Θ 2 / 3 ) > 0 C_D(\kappa,p;\Theta_{2/3})>0 C D ( κ , p ; Θ 2/3 ) > 0 , depending only on κ , p , τ , T , B 0 , B 1 , G 0 , G 1 , Θ 2 / 3 \kappa,p,\tau,T,B_0,B_1,G_0,G_1,\Theta_{2/3} κ , p , τ , T , B 0 , B 1 , G 0 , G 1 , Θ 2/3 and nondecreasing in κ \kappa κ and Θ 2 / 3 \Theta_{2/3} Θ 2/3 , such that
sup m ∈ M ∑ ∅ ≠ u ⊆ [ s ] κ ∣ u ∣ D m , u p ≤ C D ( κ , p ; Θ 2 / 3 ) . (45) \sup_{m\in\mathcal{M}}\sum_{\emptyset\ne u\subseteq[s]}\kappa^{|u|}D_{m,u}^{p}\le C_D(\kappa,p;\Theta_{2/3}). \tag*{(45)} m ∈ M sup ∅ = u ⊆ [ s ] ∑ κ ∣ u ∣ D m , u p ≤ C D ( κ , p ; Θ 2/3 ) . (45)
The proof is completed in Section 4.3. The auxiliary results are proved in Appendices A–C.
Recursive expansions of state derivatives
We first derive recursive expansions for the mixed derivatives of the Euler–Maruyama state X t h X^h_t X t h with respect to the Brownian bridge input coordinates. Fix z z z and suppress the argument of X t i h ( z ) X^h_{t_i}(z) X t i h ( z ) and W t i ( z ) W_{t_i}(z) W t i ( z ) when convenient. The set-partition Faà di Bruno formula [14 Theorem 1] (see also [8 ] ) gives
∂ u ( f ∘ Ψ ) = ∑ π ∈ P ( u ) D x ∣ π ∣ f ( Ψ ) [ ∂ v Ψ : v ∈ π ] , u ≠ ∅ . (46) \partial_u(f \circ\Psi) = \sum_{\pi\in\mathcal{P}(u)} D_x^{|\pi|}f(\Psi)[\partial_v\Psi: v \in\pi], \qquad u \ne\varnothing. \tag*{(46)} ∂ u ( f ∘ Ψ ) = π ∈ P ( u ) ∑ D x ∣ π ∣ f ( Ψ ) [ ∂ v Ψ : v ∈ π ] , u = ∅ . (46)
For a fixed grid with h = T / m h = T/m h = T / m , set Y i ( z ) = X t i h ( z ) − ∑ W t i ( z ) Y_i(z) = X^h_{t_i}(z) - \sum W_{t_i}(z) Y i ( z ) = X t i h ( z ) − ∑ W t i ( z ) . It follows from (24) that, after suppressing z z z ,
Y i + 1 = Y i + h b ( t i , Y i + ∑ W t i ) , Y 0 = x 0 . (47) Y_{i+1} = Y_i + hb(t_i,Y_i + \sum W_{t_i}), \qquad Y_0 = x_0. \tag*{(47)} Y i + 1 = Y i + hb ( t i , Y i + ∑ W t i ) , Y 0 = x 0 . (47)
For every nonempty v ⊆ [ s ] v \subseteq[s] v ⊆ [ s ] , define
Y i , v = ∂ v Y i , X i , v h = ∂ v X t i h . Y_{i,v} = \partial_vY_i,\qquad X^h_{i,v} = \partial_vX^h_{t_i}. Y i , v = ∂ v Y i , X i , v h = ∂ v X t i h .
By (21) , these derivatives satisfy
X i , v h = Y i , v + { ξ j ( t i ) , v = { j } , 0 , ∣ v ∣ ≥ 2. X^h_{i,v} = Y_{i,v} + \begin{cases} \xi_j(t_i), & v = \{j\}, \\ 0, & |v| \ge2. \end{cases} X i , v h = Y i , v + { ξ j ( t i ) , 0 , v = { j } , ∣ v ∣ ≥ 2.
Lemma 4.2. Set
Ω i : = Id d x + h D x b ( t i , X t i h ) , 0 ≤ i < m . (48) \Omega_i := \operatorname{Id}_{d_x} + hD_xb(t_i,X^h_{t_i}), \qquad0 \le i < m. \tag*{(48)} Ω i := Id d x + h D x b ( t i , X t i h ) , 0 ≤ i < m . (48) For 0 ≤ i ′ < i 0 \le i' < i 0 ≤ i ′ < i , define P i , i ′ = Ω i − 1 ⋯ Ω i ′ + 1 P_{i,i'} = \Omega_{i-1}\cdots\Omega_{i'+1} P i , i ′ = Ω i − 1 ⋯ Ω i ′ + 1 , an empty product being Id d x \operatorname{Id}_{d_x} Id d x . For i ∈ { 0 , … , m } i \in\{0,\ldots,m\} i ∈ { 0 , … , m } and j ∈ [ s ] j \in[s] j ∈ [ s ] , we have
Y i , { j } = ∑ i ′ = 0 i − 1 P i , i ′ h D x b ( t i ′ , X t i ′ h ) [ ξ j ( t i ′ ) ] . (49) Y_{i,\{j\}} = \sum_{i'=0}^{i-1} P_{i,i'}hD_xb(t_{i'},X^h_{t_{i'}})[\xi_j(t_{i'})]. \tag*{(49)} Y i , { j } = i ′ = 0 ∑ i − 1 P i , i ′ h D x b ( t i ′ , X t i ′ h ) [ ξ j ( t i ′ )] . (49) For u ⊆ [ s ] u \subseteq[s] u ⊆ [ s ] with ∣ u ∣ ≥ 2 |u| \ge2 ∣ u ∣ ≥ 2 , we have
Y i , u = ∑ i ′ = 0 i − 1 ∑ S ⊆ u ∣ S ∣ + ∣ π ∣ ≥ 2 ∑ π ∈ P ( u ∖ S ) P i , i ′ h D x ∣ S ∣ + ∣ π ∣ b ( t i ′ , X t i ′ h ) [ ( ξ j ( t i ′ ) ) j ∈ S , ( Y i ′ , v ) v ∈ π ] . (50) Y_{i,u} = \sum_{i'=0}^{i-1}\sum_{\substack{S\subseteq u\\ |S|+|\pi|\ge2}}\sum_{\pi\in\mathcal{P}(u\setminus S)} P_{i,i'}hD_x^{|S|+|\pi|}b(t_{i'},X^h_{t_{i'}})\left[(\xi_j(t_{i'}))_{j\in S},(Y_{i',v})_{v\in\pi}\right]. \tag*{(50)} Y i , u = i ′ = 0 ∑ i − 1 S ⊆ u ∣ S ∣ + ∣ π ∣ ≥ 2 ∑ π ∈ P ( u ∖ S ) ∑ P i , i ′ h D x ∣ S ∣ + ∣ π ∣ b ( t i ′ , X t i ′ h ) [ ( ξ j ( t i ′ ) ) j ∈ S , ( Y i ′ , v ) v ∈ π ] . (50) Moreover,
∥ P i , i ′ ∥ 2 ≤ e B 1 T , (51) \lVert P_{i,i'}\rVert_2 \le e^{B_1T}, \tag*{(51)} ∥ P i , i ′ ∥ 2 ≤ e B 1 T , (51) where B 1 B_1 B 1 is defined in (8) .
The proof is given in Appendix § 8 .
Derivative majorant and summability estimates
To control each D m , u \mathcal{D}_{m,u} D m , u , we define the auxiliary quantity
η m ( S ) = h ∑ i = 0 m − 1 ∏ j ∈ S ∣ ξ j ( t i ) ∣ 2 , ∅ ≠ S ⊆ [ s ] . (52) \eta_m(S) = h\sum_{i=0}^{m-1}\prod_{j\in S}|\xi_j(t_i)|_2,\qquad\varnothing\ne S\subseteq[s]. \tag*{(52)} η m ( S ) = h i = 0 ∑ m − 1 j ∈ S ∏ ∣ ξ j ( t i ) ∣ 2 , ∅ = S ⊆ [ s ] . (52)
Repeatedly substituting the recursive expansions in Lemma 4.2 into the expression for ∂ u F m \partial_uF_m ∂ u F m , and using rooted trees to keep track of the resulting terms, yields the following estimate for D m , u \mathcal{D}_{m,u} D m , u . The proof is given in Appendix § 9 .
Proposition 4.3. For u ≠ ∅ u \ne\varnothing u = ∅ let D m , u D_{m,u} D m , u be the normalized derivative envelope defined in (44) . Under Assumption 2.1 there is C m a j ≥ 1 C_{\mathrm{maj}} \ge1 C maj ≥ 1 , depending only on T T T , B 0 B_0 B 0 , B 1 B_1 B 1 , G 0 G_0 G 0 , G 1 G_1 G 1 , τ \tau τ , such that
D m , u ≤ C m a j ∣ u ∣ ∑ E ⊆ u ∩ E w ( ∣ E ∣ ! ) τ ∏ j ∈ E ( T σ j ) τ ∑ π ∈ P ( u ∖ E ) C m a j ∣ π ∣ ( ∣ π ∣ ! ) τ ∏ S ∈ π ( ∣ S ∣ ! ) τ η m ( S ) . (53) D_{m,u} \le C_{\mathrm{maj}}^{|u|} \sum_{E\subseteq u\cap\mathcal{E}_w} (|E|!)^\tau\prod_{j\in E}(\sqrt{T}\,\sigma_j)^\tau\sum_{\pi\in\mathcal{P}(u\setminus E)} C_{\mathrm{maj}}^{|\pi|}(|\pi|!)^\tau\prod_{S\in\pi}(|S|!)^\tau\eta_m(S). \tag*{(53)} D m , u ≤ C maj ∣ u ∣ E ⊆ u ∩ E w ∑ ( ∣ E ∣ ! ) τ j ∈ E ∏ ( T σ j ) τ π ∈ P ( u ∖ E ) ∑ C maj ∣ π ∣ ( ∣ π ∣ ! ) τ S ∈ π ∏ ( ∣ S ∣ ! ) τ η m ( S ) . (53)
The following two technical lemmas control the summability of η m ( S ) \eta_m(S) η m ( S ) over ∅ ≠ S ⊆ J m \varnothing\ne S\subseteq\mathcal{J}_m ∅ = S ⊆ J m and over all nonempty input subsets. Their proofs are given in Appendix C.
Lemma 4.4. Let ∅ ≠ S ⊆ J m \varnothing\ne S\subseteq\mathcal{J}_m ∅ = S ⊆ J m , and recall the supporting intervals I j I_j I j from (19) . If ⋂ j ∈ S int ( I j ) = ∅ \bigcap_{j\in S}\operatorname{int}(I_j)=\varnothing ⋂ j ∈ S int ( I j ) = ∅ , then η m ( S ) = 0 \eta_m(S)=0 η m ( S ) = 0 . Otherwise choose j ∗ ∈ S j^*\in S j ∗ ∈ S such that ∣ I j ∗ ∣ = min j ∈ S ∣ I j ∣ |I_{j^*}|=\min_{j\in S}|I_j| ∣ I j ∗ ∣ = min j ∈ S ∣ I j ∣ . Then
η m ( S ) ≤ 3 2 ∣ I j ∗ ∣ ∏ j ∈ S ( σ r ( j ) 2 ∣ I j ∣ 1 / 2 ) . (54) \eta_m(S)\le\frac{3}{2}|I_{j^*}|\prod_{j\in S}\left(\frac{\sigma_{r(j)}}{2}|I_j|^{1/2}\right). \tag*{(54)} η m ( S ) ≤ 2 3 ∣ I j ∗ ∣ j ∈ S ∏ ( 2 σ r ( j ) ∣ I j ∣ 1/2 ) . (54) For every ρ > 2 / 3 \rho>2/3 ρ > 2/3 there exists C ρ , T > 0 C_{\rho,T}>0 C ρ , T > 0 , depending only on ρ , T \rho,T ρ , T , such that, for every integer n ≥ 1 n\ge1 n ≥ 1 ,
sup m ∈ M ∑ S ⊆ J m ∣ S ∣ = n η m ( S ) ρ ≤ C ρ , T n Θ ρ n ( n − 1 ) ! . (55) \sup_{m\in\mathcal{M}}\sum_{\substack{S\subseteq\mathcal{J}_m\\ |S|=n}}\eta_m(S)^\rho\le\frac{C_{\rho,T}^{n}\Theta_\rho^{n}}{(n-1)!}. \tag*{(55)} m ∈ M sup S ⊆ J m ∣ S ∣ = n ∑ η m ( S ) ρ ≤ ( n − 1 )! C ρ , T n Θ ρ n . (55)
Lemma 4.5. For every 2 / 3 < ρ < 1 / τ 2/3<\rho<1/\tau 2/3 < ρ < 1/ τ and κ > 0 \kappa>0 κ > 0 , define
Υ E ( κ ) : = ∑ E ⊆ E w κ ∣ E ∣ ( ∣ E ∣ ! ) τ ρ ∏ j ∈ E ( T σ j ) ρ . (56) \Upsilon^{\mathcal{E}}(\kappa):=\sum_{E\subseteq\mathcal{E}_w}\kappa^{|E|}(|E|!)^{\tau\rho}\prod_{j\in E}(\sqrt{T}\,\sigma_j)^\rho. \tag*{(56)} Υ E ( κ ) := E ⊆ E w ∑ κ ∣ E ∣ ( ∣ E ∣ ! ) τ ρ j ∈ E ∏ ( T σ j ) ρ . (56) and
Υ m ( κ ) : = ∑ ∅ ≠ S ⊆ [ s ] κ ∣ S ∣ ( ∣ S ∣ ! ) τ ρ η m ( S ) ρ . (57) \Upsilon_m(\kappa):=\sum_{\varnothing\ne S\subseteq[s]}\kappa^{|S|}(|S|!)^{\tau\rho}\eta_m(S)^\rho. \tag*{(57)} Υ m ( κ ) := ∅ = S ⊆ [ s ] ∑ κ ∣ S ∣ ( ∣ S ∣ ! ) τ ρ η m ( S ) ρ . (57) Then
max { Υ E ( κ ) , sup m ∈ M Υ m ( κ ) } ≤ C Υ ( κ , ρ , τ , T ; Θ ρ ) < ∞ , \max\left\{\Upsilon^{\mathcal{E}}(\kappa),\sup_{m\in\mathcal{M}}\Upsilon_m(\kappa)\right\}\le C_{\Upsilon}(\kappa,\rho,\tau,T;\Theta_\rho)<\infty, max { Υ E ( κ ) , m ∈ M sup Υ m ( κ ) } ≤ C Υ ( κ , ρ , τ , T ; Θ ρ ) < ∞ , where the finite constant C Υ ( κ , ρ , τ , T ; Θ ρ ) C_{\Upsilon}(\kappa,\rho,\tau,T;\Theta_\rho) C Υ ( κ , ρ , τ , T ; Θ ρ ) depends only on κ , ρ , τ , T , Θ ρ \kappa,\rho,\tau,T,\Theta_\rho κ , ρ , τ , T , Θ ρ and can be chosen nondecreasing in κ \kappa κ and Θ ρ \Theta_\rho Θ ρ .
Proof of the summability theorem
Proof of Theorem 4.1. Fix κ > 0 \kappa>0 κ > 0 and first take 2 / 3 < ρ < 1 / τ 2/3<\rho<1/\tau 2/3 < ρ < 1/ τ . Then 0 < ρ < 1 0<\rho<1 0 < ρ < 1 . Let C m a j C_{\mathrm{maj}} C maj be the constant in Proposition 4.3. Set
A 0 = κ C m a j ρ , w E ( E ) = A 0 ∣ E ∣ ( ∣ E ∣ ! ) τ ρ ∏ j ∈ E ( T σ j ) ρ , w ( S ) = A 0 ∣ S ∣ ( ∣ S ∣ ! ) τ ρ η m ( S ) ρ A_0=\kappa C_{\mathrm{maj}}^\rho,\qquad w_{\mathcal{E}}(E)=A_0^{|E|}(|E|!)^{\tau\rho}\prod_{j\in E}(\sqrt{T}\,\sigma_j)^\rho,\qquad w(S)=A_0^{|S|}(|S|!)^{\tau\rho}\eta_m(S)^\rho A 0 = κ C maj ρ , w E ( E ) = A 0 ∣ E ∣ ( ∣ E ∣ ! ) τ ρ j ∈ E ∏ ( T σ j ) ρ , w ( S ) = A 0 ∣ S ∣ ( ∣ S ∣ ! ) τ ρ η m ( S ) ρ
for E ⊆ E w E\subseteq\mathcal{E}_w E ⊆ E w and nonempty S ⊆ [ s ] S\subseteq[s] S ⊆ [ s ] . By (13) , Θ ρ ≤ Θ 2 / 3 3 ρ / 2 \Theta_\rho\le\Theta_{2/3}^{3\rho/2} Θ ρ ≤ Θ 2/3 3 ρ /2 . Using (56) , (57) , and the monotonicity of the constant in Lemma 4.5, we have
∑ E ⊆ E w w E ( E ) = Υ E ( A 0 ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ ρ ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ 2 / 3 3 ρ / 2 ) , (58) \sum_{E\subseteq\mathcal{E}_w}w_{\mathcal{E}}(E)=\Upsilon^{\mathcal{E}}(A_0)\le C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_\rho)\le C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_{2/3}^{3\rho/2}), \tag*{(58)} E ⊆ E w ∑ w E ( E ) = Υ E ( A 0 ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ ρ ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ 2/3 3 ρ /2 ) , (58)
∑ ∅ ≠ S ⊆ [ s ] w ( S ) = Υ m ( A 0 ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ ρ ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ 2 / 3 3 ρ / 2 ) . (59) \sum_{\varnothing\ne S\subseteq[s]}w(S)=\Upsilon_m(A_0)\le C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_\rho)\le C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_{2/3}^{3\rho/2}). \tag*{(59)} ∅ = S ⊆ [ s ] ∑ w ( S ) = Υ m ( A 0 ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ ρ ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ 2/3 3 ρ /2 ) . (59)
Using ( ∑ i a i ) ρ ≤ ∑ i a i ρ \left(\sum_i a_i\right)^\rho\le\sum_i a_i^\rho ( ∑ i a i ) ρ ≤ ∑ i a i ρ for a i ≥ 0 a_i\ge0 a i ≥ 0 and 0 < ρ < 1 0<\rho<1 0 < ρ < 1 in (53) , together with ∣ u ∣ = ∣ E ∣ + ∑ S ∈ π ∣ S ∣ |u|=|E|+\sum_{S\in\pi}|S| ∣ u ∣ = ∣ E ∣ + ∑ S ∈ π ∣ S ∣ , gives
κ ∣ u ∣ D m , u ρ ≤ ∑ E ⊆ u ∩ E w w E ( E ) ∑ π ∈ P ( u ∖ E ) C m a j ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ ∏ S ∈ π w ( S ) . \kappa^{|u|}D_{m,u}^\rho\le\sum_{E\subseteq u\cap\mathcal{E}_w}w_{\mathcal{E}}(E)\sum_{\pi\in\mathcal{P}(u\setminus E)}C_{\mathrm{maj}}^{\rho|\pi|}(|\pi|!)^{\tau\rho}\prod_{S\in\pi}w(S). κ ∣ u ∣ D m , u ρ ≤ E ⊆ u ∩ E w ∑ w E ( E ) π ∈ P ( u ∖ E ) ∑ C maj ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ S ∈ π ∏ w ( S ) .
Summing over u u u and setting v = u ∖ E v=u\setminus E v = u ∖ E yields
∑ ∅ ≠ u ⊆ [ s ] κ ∣ u ∣ D m , u ρ ≤ ∑ ∅ ≠ u ⊆ [ s ] ∑ E ⊆ u ∩ E w w E ( E ) ∑ π ∈ P ( u ∖ E ) C m a j ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ ∏ S ∈ π w ( S ) = ∑ E ⊆ E w w E ( E ) ∑ v ⊆ [ s ] ∖ E E ∪ v ≠ ∅ ∑ π ∈ P ( v ) C m a j ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ ∏ S ∈ π w ( S ) ≤ ∑ E ⊆ E w w E ( E ) ∑ v ⊆ [ s ] ∑ π ∈ P ( v ) C m a j ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ ∏ S ∈ π w ( S ) . \begin{aligned}
\sum_{\varnothing\ne u\subseteq[s]}\kappa^{|u|}\mathcal{D}_{m,u}^{\rho}
\le
\sum_{\varnothing\ne u\subseteq[s]}\sum_{E\subseteq u\cap E_w}w_E(E)
\sum_{\pi\in\mathcal{P}(u\setminus E)}C_{\mathrm{maj}}^{\rho|\pi|}(|\pi|!)^{\tau\rho}\prod_{S\in\pi}w(S) \\
&=
\sum_{E\subseteq E_w}w_E(E)
\sum_{\substack{v\subseteq[s]\setminus E\\E\cup v\ne\varnothing}}
\sum_{\pi\in\mathcal{P}(v)}C_{\mathrm{maj}}^{\rho|\pi|}(|\pi|!)^{\tau\rho}\prod_{S\in\pi}w(S) \\
&\le
\sum_{E\subseteq E_w}w_E(E)
\sum_{v\subseteq[s]}
\sum_{\pi\in\mathcal{P}(v)}C_{\mathrm{maj}}^{\rho|\pi|}(|\pi|!)^{\tau\rho}\prod_{S\in\pi}w(S).
\end{aligned} ∅ = u ⊆ [ s ] ∑ κ ∣ u ∣ D m , u ρ ≤ ∅ = u ⊆ [ s ] ∑ E ⊆ u ∩ E w ∑ w E ( E ) π ∈ P ( u ∖ E ) ∑ C maj ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ S ∈ π ∏ w ( S ) = E ⊆ E w ∑ w E ( E ) v ⊆ [ s ] ∖ E E ∪ v = ∅ ∑ π ∈ P ( v ) ∑ C maj ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ S ∈ π ∏ w ( S ) ≤ E ⊆ E w ∑ w E ( E ) v ⊆ [ s ] ∑ π ∈ P ( v ) ∑ C maj ρ ∣ π ∣ ( ∣ π ∣ ! ) τ ρ S ∈ π ∏ w ( S ) .
The equality reindexes the finite sum using the bijection ( u , E ) ↔ ( E , v ) (u,E)\leftrightarrow(E,v) ( u , E ) ↔ ( E , v ) , with v = u ∖ E v=u\setminus E v = u ∖ E and u = E ∪ ˙ v u=E\mathbin{\dot\cup}v u = E ∪ ˙ v . The last inequality drops the restriction v ∩ E = ∅ v\cap E=\varnothing v ∩ E = ∅ and E ∪ v ≠ ∅ E\cup v\ne\varnothing E ∪ v = ∅ . For n ≥ 0 n\ge0 n ≥ 0 , ordering the n n n distinct blocks of a partition and using (4.16) gives
∑ v ⊆ [ s ] π ∈ P ( v ) ∣ π ∣ = n ∏ S ∈ π w ( S ) = 1 n ! ∑ S 1 , … , S n ⊆ [ s ] , S i ≠ ∅ S i ∩ S j = ∅ ( i ≠ j ) ∏ j = 1 n w ( S j ) ≤ 1 n ! ( ∑ ∅ ≠ S ⊆ [ s ] w ( S ) ) n = Υ m ( A 0 ) n n ! ≤ C Υ ( A 0 , ρ , τ , T ; Θ 2 / 3 3 ρ / 2 ) n n ! . \begin{aligned}
\sum_{\substack{v\subseteq[s]\\\pi\in\mathcal{P}(v)\\|\pi|=n}}\prod_{S\in\pi}w(S)
=
\frac{1}{n!}
\sum_{\substack{S_1,\ldots,S_n\subseteq[s],\ S_i\ne\varnothing\\S_i\cap S_j=\varnothing\ (i\ne j)}}
\prod_{j=1}^{n}w(S_j)
\le
\frac{1}{n!}\left(\sum_{\varnothing\ne S\subseteq[s]}w(S)\right)^n \\
&=
\frac{\Upsilon_m(A_0)^n}{n!}
\le
\frac{C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_{2/3}^{3\rho/2})^n}{n!}.
\end{aligned} v ⊆ [ s ] π ∈ P ( v ) ∣ π ∣ = n ∑ S ∈ π ∏ w ( S ) = n ! 1 S 1 , … , S n ⊆ [ s ] , S i = ∅ S i ∩ S j = ∅ ( i = j ) ∑ j = 1 ∏ n w ( S j ) ≤ n ! 1 ∅ = S ⊆ [ s ] ∑ w ( S ) n = n ! Υ m ( A 0 ) n ≤ n ! C Υ ( A 0 , ρ , τ , T ; Θ 2/3 3 ρ /2 ) n .
Using the preceding inequality and (4.15), we obtain
∑ ∅ ≠ u ⊆ [ s ] κ ∣ u ∣ D m , u ρ ≤ ( ∑ E ⊆ E w w E ( E ) ) ∑ n = 0 ∞ C m a j ρ n ( n ! ) τ ρ ∑ v ⊆ [ s ] π ∈ P ( v ) ∣ π ∣ = n ∏ S ∈ π w ( S ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ 2 / 3 3 ρ / 2 ) ∑ n = 0 ∞ ( C m a j ρ C Υ ( A 0 , ρ , τ , T ; Θ 2 / 3 3 ρ / 2 ) ) n ( n ! ) τ ρ − 1 = : C s u m ( κ , ρ ; Θ 2 / 3 ) < ∞ . (60) \begin{aligned}
\sum_{\varnothing\ne u\subseteq[s]}\kappa^{|u|}\mathcal{D}_{m,u}^{\rho}
\le
\left(\sum_{E\subseteq E_w}w_E(E)\right)
\sum_{n=0}^{\infty}C_{\mathrm{maj}}^{\rho n}(n!)^{\tau\rho}
\sum_{\substack{v\subseteq[s]\\\pi\in\mathcal{P}(v)\\|\pi|=n}}
\prod_{S\in\pi}w(S) \\
&\le
C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_{2/3}^{3\rho/2})
\sum_{n=0}^{\infty}
\left(C_{\mathrm{maj}}^{\rho}C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_{2/3}^{3\rho/2})\right)^n
(n!)^{\tau\rho-1} \\
&=:C_{\mathrm{sum}}(\kappa,\rho;\Theta_{2/3})<\infty. \tag*{(60)}
\end{aligned} ∅ = u ⊆ [ s ] ∑ κ ∣ u ∣ D m , u ρ ≤ ( E ⊆ E w ∑ w E ( E ) ) n = 0 ∑ ∞ C maj ρ n ( n ! ) τ ρ v ⊆ [ s ] π ∈ P ( v ) ∣ π ∣ = n ∑ S ∈ π ∏ w ( S ) ≤ C Υ ( A 0 , ρ , τ , T ; Θ 2/3 3 ρ /2 ) n = 0 ∑ ∞ ( C maj ρ C Υ ( A 0 , ρ , τ , T ; Θ 2/3 3 ρ /2 ) ) n ( n ! ) τ ρ − 1 =: C sum ( κ , ρ ; Θ 2/3 ) < ∞. (60)
The ratio of consecutive terms in C s u m ( κ , ρ ; Θ 2 / 3 ) C_{\mathrm{sum}}(\kappa,\rho;\Theta_{2/3}) C sum ( κ , ρ ; Θ 2/3 ) is
C m a j ρ C Υ ( A 0 , ρ , τ , T ; Θ 2 / 3 3 ρ / 2 ) ( n + 1 ) τ ρ − 1 ⟶ 0 , C_{\mathrm{maj}}^{\rho}C_{\Upsilon}(A_0,\rho,\tau,T;\Theta_{2/3}^{3\rho/2})(n+1)^{\tau\rho-1}\longrightarrow0, C maj ρ C Υ ( A 0 , ρ , τ , T ; Θ 2/3 3 ρ /2 ) ( n + 1 ) τ ρ − 1 ⟶ 0 ,
so C s u m ( κ , ρ ; Θ 2 / 3 ) C_{\mathrm{sum}}(\kappa,\rho;\Theta_{2/3}) C sum ( κ , ρ ; Θ 2/3 ) is finite. Since A 0 = κ C m a j ρ A_0=\kappa C_{\mathrm{maj}}^{\rho} A 0 = κ C maj ρ and C m a j C_{\mathrm{maj}} C maj depends only on T , B 0 , B 1 , G 0 , G 1 , τ T,B_0,B_1,G_0,G_1,\tau T , B 0 , B 1 , G 0 , G 1 , τ , the constant C s u m ( κ , ρ ; Θ 2 / 3 ) C_{\mathrm{sum}}(\kappa,\rho;\Theta_{2/3}) C sum ( κ , ρ ; Θ 2/3 ) depends only on κ , ρ , τ , T , B 0 , B 1 , G 0 , G 1 , Θ 2 / 3 \kappa,\rho,\tau,T,B_0,B_1,G_0,G_1,\Theta_{2/3} κ , ρ , τ , T , B 0 , B 1 , G 0 , G 1 , Θ 2/3 and is nondecreasing in both κ \kappa κ and Θ 2 / 3 \Theta_{2/3} Θ 2/3 .
For general p > 2 / 3 p>2/3 p > 2/3 , take
ρ = 2 / 3 + min { p , 1 / τ } 2 . \rho=\frac{2/3+\min\{p,1/\tau\}}{2}. ρ = 2 2/3 + min { p , 1/ τ } .
Since τ < 3 / 2 \tau<3/2 τ < 3/2 , this gives 2 / 3 < ρ < min { p , 1 / τ } 2/3<\rho<\min\{p,1/\tau\} 2/3 < ρ < min { p , 1/ τ } . Put x u = κ ∣ u ∣ / p D m , u x_u=\kappa^{|u|/p}\mathcal{D}_{m,u} x u = κ ∣ u ∣/ p D m , u . Since p > ρ p>\rho p > ρ , we have
∑ u ≠ ∅ κ ∣ u ∣ D m , u p = ∑ u ≠ ∅ x u p ≤ ( ∑ u ≠ ∅ x u ρ ) p / ρ = ( ∑ u ≠ ∅ ( κ ρ / p ) ∣ u ∣ D m , u ρ ) p / ρ . \sum_{u\ne\varnothing}\kappa^{|u|}\mathcal{D}_{m,u}^{p}
=
\sum_{u\ne\varnothing}x_u^p
\le
\left(\sum_{u\ne\varnothing}x_u^\rho\right)^{p/\rho}
=
\left(\sum_{u\ne\varnothing}\left(\kappa^{\rho/p}\right)^{|u|}\mathcal{D}_{m,u}^{\rho}\right)^{p/\rho}. u = ∅ ∑ κ ∣ u ∣ D m , u p = u = ∅ ∑ x u p ≤ u = ∅ ∑ x u ρ p / ρ = u = ∅ ∑ ( κ ρ / p ) ∣ u ∣ D m , u ρ p / ρ .
Applying (4.17) with geometric factor κ ρ / p \kappa^{\rho/p} κ ρ / p and taking the supremum over m m m gives
sup m ∈ M ∑ u ≠ ∅ κ ∣ u ∣ D m , u p ≤ [ C s u m ( κ ρ / p , ρ ; Θ 2 / 3 ) ] p / ρ = : C D ( κ , p ; Θ 2 / 3 ) . \sup_{m\in\mathcal{M}}\sum_{u\ne\varnothing}\kappa^{|u|}\mathcal{D}_{m,u}^{p}
\le
\left[C_{\mathrm{sum}}\left(\kappa^{\rho/p},\rho;\Theta_{2/3}\right)\right]^{p/\rho}
=:C_D(\kappa,p;\Theta_{2/3}). m ∈ M sup u = ∅ ∑ κ ∣ u ∣ D m , u p ≤ [ C sum ( κ ρ / p , ρ ; Θ 2/3 ) ] p / ρ =: C D ( κ , p ; Θ 2/3 ) .
For later use, we denote this bound by C D ( κ , p ; Θ 2 / 3 ) C_D(\kappa,p;\Theta_{2/3}) C D ( κ , p ; Θ 2/3 ) , suppressing the other fixed parameters. This proves (4.2). The constant depends only on κ , p , τ , T , B 0 , B 1 , G 0 , G 1 , Θ 2 / 3 \kappa,p,\tau,T,B_0,B_1,G_0,G_1,\Theta_{2/3} κ , p , τ , T , B 0 , B 1 , G 0 , G 1 , Θ 2/3 and is nondecreasing in both κ \kappa κ and Θ 2 / 3 \Theta_{2/3} Θ 2/3 .
Lattice integration error
In this section, we use Theorem 4.1 to bound the weighted Gaussian-space norm introduced in § 2.5 . We then prove the lattice integration error bounds in Theorem 3.1 and Corollary 3.3 .
Bounds on the weighted Gaussian-space norm
Recall the space H s , γ \mathcal{H}_{s,\gamma} H s , γ from § 2.5 , with ψ ( t ) = e − α ∣ t ∣ \psi(t)=e^{-\alpha\lvert t\rvert} ψ ( t ) = e − α ∣ t ∣ . For u ⊆ [ s ] u\subseteq[s] u ⊆ [ s ] , define
S u ( F ) 2 : = ∫ R ∣ u ∣ ∣ ∫ R s − ∣ u ∣ ∂ u F ( z ) φ − u ( z − u ) d z − u ∣ 2 ∏ j ∈ u e − 2 α ∣ z j ∣ d z u . (61) S_u(F)^2:=\int_{\mathbb{R}^{\lvert u\rvert}}\left|\int_{\mathbb{R}^{s-\lvert u\rvert}}\partial_uF(z)\varphi_{-u}(z_{-u})\,\mathrm{d}z_{-u}\right|^2\prod_{j\in u}e^{-2\alpha\lvert z_j\rvert}\,\mathrm{d}z_u. \tag*{(61)} S u ( F ) 2 := ∫ R ∣ u ∣ ∫ R s − ∣ u ∣ ∂ u F ( z ) φ − u ( z − u ) d z − u 2 j ∈ u ∏ e − 2 α ∣ z j ∣ d z u . (61)
Then
∥ F ∥ H s , γ 2 = ∑ u ⊆ [ s ] S u ( F ) 2 γ u . \lVert F\rVert_{\mathcal{H}_{s,\gamma}}^2=\sum_{u\subseteq[s]}\frac{S_u(F)^2}{\gamma_u}. ∥ F ∥ H s , γ 2 = u ⊆ [ s ] ∑ γ u S u ( F ) 2 .
In view of the exponential growth of g g g in (2.5), we set the parameter α \alpha α in the weight function ψ \psi ψ to be
α = α 0 : = 1 + β g e B 1 T T Θ 1 ( 2 + 1 2 ) . (62) \alpha=\alpha_0:=1+\beta_g e^{B_1T}\sqrt{T}\,\Theta_1\left(2+\frac{1}{\sqrt{2}}\right). \tag*{(62)} α = α 0 := 1 + β g e B 1 T T Θ 1 ( 2 + 2 1 ) . (62)
With this choice, we first prove the following technical lemma.
Lemma 5.1. Suppose Assumption 2.1 holds. For each u ⊆ [ s ] u\subseteq[s] u ⊆ [ s ] , let Z ( u ) = ( Z 1 ( u ) , … , Z s ( u ) ) Z^{(u)}=(Z_1^{(u)},\ldots,Z_s^{(u)}) Z ( u ) = ( Z 1 ( u ) , … , Z s ( u ) ) have independent coordinates, standard Gaussian for j ∉ u j\notin u j ∈ / u and with density α 0 e − 2 α 0 ∣ z ∣ \alpha_0e^{-2\alpha_0\lvert z\rvert} α 0 e − 2 α 0 ∣ z ∣ for j ∈ u j\in u j ∈ u . Then
sup m ∈ M sup u ⊆ [ s ] E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) < ∞ . \sup_{m\in\mathcal{M}}\sup_{u\subseteq[s]}\mathbb{E}e^{2\beta_g\lvert X^h_{t_m}(Z^{(u)})\rvert_2}\leq C_{\mathrm{aux}}(\lvert x_0\rvert_2,\Theta_1)<\infty. m ∈ M sup u ⊆ [ s ] sup E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ C aux (∣ x 0 ∣ 2 , Θ 1 ) < ∞. Here C a u x C_{\mathrm{aux}} C aux depends only on β g \beta_g β g , T T T , K 0 K_0 K 0 , B 1 B_1 B 1 , ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 , Θ 1 \Theta_1 Θ 1 and is nondecreasing in ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 and Θ 1 \Theta_1 Θ 1 .
The proof is given in Appendix § 11 .
Using Lemma 5.1, we obtain the following estimate for S u ( F m ) S_u(F_m) S u ( F m ) .
Lemma 5.2. Under Assumption 2.1, we have
S u ( F m ) ≤ C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) 1 / 2 D m , u , u ≠ ∅ , (63) S_u(F_m)\leq C_{\mathrm{aux}}(\lvert x_0\rvert_2,\Theta_1)^{1/2}D_{m,u},\qquad u\neq\varnothing, \tag*{(63)} S u ( F m ) ≤ C aux (∣ x 0 ∣ 2 , Θ 1 ) 1/2 D m , u , u = ∅ , (63) where C a u x C_{\mathrm{aux}} C aux is the constant in Lemma 5.1.
The proof is given in Appendix § 11 .
A fractional-moment bound for the lattice estimator
The following proposition gives a fractional-moment bound for the error of the random lattice estimator.
Proposition 5.3. Fix 1 / 2 < λ < 1 1/2<\lambda<1 1/2 < λ < 1 , 1 / ( 2 λ ) < δ ∗ < 1 1/(2\lambda)<\delta_*<1 1/ ( 2 λ ) < δ ∗ < 1 , and use ρ λ \rho_\lambda ρ λ from (2.28). Let F : R s → R F:\mathbb{R}^s\to\mathbb{R} F : R s → R have the weak mixed derivatives appearing in (61) , with S u ( F ) < ∞ S_u(F)<\infty S u ( F ) < ∞ for every u ⊆ [ s ] u\subseteq[s] u ⊆ [ s ] , and let N N N be prime. Define
C λ ( F ) : = ( ∑ ∅ ≠ u ⊆ [ s ] ρ λ ∣ u ∣ / ( 1 + λ ) S u ( F ) 2 λ / ( 1 + λ ) ) 1 + λ . (64) C_\lambda(F):=\left(\sum_{\varnothing\neq u\subseteq[s]}\rho_\lambda^{\lvert u\rvert/(1+\lambda)}S_u(F)^{2\lambda/(1+\lambda)}\right)^{1+\lambda}. \tag*{(64)} C λ ( F ) := ∅ = u ⊆ [ s ] ∑ ρ λ ∣ u ∣ / ( 1 + λ ) S u ( F ) 2 λ / ( 1 + λ ) 1 + λ . (64) Let A A A be uniform on { 1 , … , N − 1 } s \{1,\ldots,N-1\}^s { 1 , … , N − 1 } s and Δ \Delta Δ uniform on [ 0 , 1 ] s [0,1]^s [ 0 , 1 ] s , independently of each other. Then
E A , Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 λ ≤ C λ ( F ) N − 1 . (65) \mathbb{E}_{A,\Delta}\lvert Q_{A,\Delta}(F)-I(F)\rvert^{2\lambda}\leq\frac{C_\lambda(F)}{N-1}. \tag*{(65)} E A , Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 λ ≤ N − 1 C λ ( F ) . (65)
Proof. Let F ∘ : = F − I ( F ) F^\circ:= F-\mathcal{I}(F) F ∘ := F − I ( F ) and choose
γ u = ( S u ( F ) 2 ρ λ ∣ u ∣ ) 1 / ( 1 + λ ) , ∅ ≠ u ⊆ [ s ] . (66) \gamma_u=\left(\frac{S_u(F)^2}{\rho_\lambda^{|u|}}\right)^{1/(1+\lambda)},\qquad\varnothing\ne u\subseteq[s]. \tag*{(66)} γ u = ( ρ λ ∣ u ∣ S u ( F ) 2 ) 1/ ( 1 + λ ) , ∅ = u ⊆ [ s ] . (66)
With the convention 0 / 0 = 0 0/0=0 0/0 = 0 from Section 2.5,
S u ( F ) 2 γ u = γ u λ ρ λ ∣ u ∣ = ρ λ ∣ u ∣ / ( 1 + λ ) S u ( F ) 2 λ / ( 1 + λ ) . \frac{S_u(F)^2}{\gamma_u}=\gamma_u^\lambda\rho_\lambda^{|u|}=\rho_\lambda^{|u|/(1+\lambda)}S_u(F)^{2\lambda/(1+\lambda)}. γ u S u ( F ) 2 = γ u λ ρ λ ∣ u ∣ = ρ λ ∣ u ∣/ ( 1 + λ ) S u ( F ) 2 λ / ( 1 + λ ) .
Since S ∅ ( F ∘ ) = 0 S_\varnothing(F^\circ)=0 S ∅ ( F ∘ ) = 0 and S u ( F ∘ ) = S u ( F ) S_u(F^\circ)=S_u(F) S u ( F ∘ ) = S u ( F ) for u ≠ ∅ u\ne\varnothing u = ∅ , we have ∥ F ∘ ∥ H s , γ 2 = ∑ u ≠ ∅ S u ( F ) 2 / γ u \|F^\circ\|_{\mathcal{H}_{s,\gamma}}^2=\sum_{u\ne\varnothing}S_u(F)^2/\gamma_u ∥ F ∘ ∥ H s , γ 2 = ∑ u = ∅ S u ( F ) 2 / γ u . Then (2.27) gives
E Δ ∣ Q a , Δ ( F ) − I ( F ) ∣ 2 = E Δ ∣ Q a , Δ ( F ∘ ) − I ( F ∘ ) ∣ 2 ≤ ( ∑ u ≠ ∅ S u ( F ) 2 γ u ) [ e s , N s h ( a ; γ ) ] 2 . \mathbb{E}_{\Delta}|Q_{a,\Delta}(F)-\mathcal{I}(F)|^2=\mathbb{E}_{\Delta}|Q_{a,\Delta}(F^\circ)-\mathcal{I}(F^\circ)|^2\le\left(\sum_{u\ne\varnothing}\frac{S_u(F)^2}{\gamma_u}\right)[e^{\mathrm{sh}}_{s,N}(a;\gamma)]^2. E Δ ∣ Q a , Δ ( F ) − I ( F ) ∣ 2 = E Δ ∣ Q a , Δ ( F ∘ ) − I ( F ∘ ) ∣ 2 ≤ u = ∅ ∑ γ u S u ( F ) 2 [ e s , N sh ( a ; γ ) ] 2 .
Raising this bound to the power λ \lambda λ , averaging over A A A , and applying (2.29) yields
E A [ E Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 ] λ ≤ ( ∑ u ≠ ∅ S u ( F ) 2 γ u ) λ E A [ e s , N s h ( A ; γ ) 2 λ ] ≤ 1 N − 1 ( ∑ u ≠ ∅ S u ( F ) 2 γ u ) λ ∑ u ≠ ∅ γ u λ ρ λ ∣ u ∣ = 1 N − 1 ( ∑ u ≠ ∅ ρ λ ∣ u ∣ / ( 1 + λ ) S u ( F ) 2 λ / ( 1 + λ ) ) 1 + λ = C λ ( F ) N − 1 . \begin{aligned}
\mathbb{E}_{A}\left[\mathbb{E}_{\Delta}|Q_{A,\Delta}(F)-\mathcal{I}(F)|^2\right]^\lambda
\le\left(\sum_{u\ne\varnothing}\frac{S_u(F)^2}{\gamma_u}\right)^\lambda\mathbb{E}_{A}\left[e^{\mathrm{sh}}_{s,N}(A;\gamma)^{2\lambda}\right] \\
&\le\frac{1}{N-1}\left(\sum_{u\ne\varnothing}\frac{S_u(F)^2}{\gamma_u}\right)^\lambda\sum_{u\ne\varnothing}\gamma_u^\lambda\rho_\lambda^{|u|} \\
&=\frac{1}{N-1}\left(\sum_{u\ne\varnothing}\rho_\lambda^{|u|/(1+\lambda)}S_u(F)^{2\lambda/(1+\lambda)}\right)^{1+\lambda}
=\frac{C_\lambda(F)}{N-1}.
\end{aligned} E A [ E Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 ] λ ≤ u = ∅ ∑ γ u S u ( F ) 2 λ E A [ e s , N sh ( A ; γ ) 2 λ ] ≤ N − 1 1 u = ∅ ∑ γ u S u ( F ) 2 λ u = ∅ ∑ γ u λ ρ λ ∣ u ∣ = N − 1 1 u = ∅ ∑ ρ λ ∣ u ∣/ ( 1 + λ ) S u ( F ) 2 λ / ( 1 + λ ) 1 + λ = N − 1 C λ ( F ) .
Finally, since 0 < λ < 1 0<\lambda<1 0 < λ < 1 , conditional Jensen’s inequality gives
E A , Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 λ ≤ E A ( E Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 ) λ , \mathbb{E}_{A,\Delta}|Q_{A,\Delta}(F)-\mathcal{I}(F)|^{2\lambda}\le\mathbb{E}_{A}\left(\mathbb{E}_{\Delta}|Q_{A,\Delta}(F)-\mathcal{I}(F)|^2\right)^\lambda, E A , Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 λ ≤ E A ( E Δ ∣ Q A , Δ ( F ) − I ( F ) ∣ 2 ) λ ,
which proves (5.5).
Proof of the sampling error bound
To prove Theorem 3.1, we first establish a moment bound for the median of independent copies of an error variable.
Lemma 5.4. Let E 1 , … , E R E_1,\ldots,E_R E 1 , … , E R be independent identically distributed real random variables, R = 2 k − 1 R=2k-1 R = 2 k − 1 , and suppose E ∣ E 1 ∣ q 0 ≤ K q 0 \mathbb{E}|E_1|^{q_0}\le K^{q_0} E ∣ E 1 ∣ q 0 ≤ K q 0 for q 0 > 0 q_0>0 q 0 > 0 and K ≥ 0 K\ge0 K ≥ 0 . For every 0 < q < q 0 k 0<q<q_0k 0 < q < q 0 k ,
E ∣ median ( E 1 , … , E R ) ∣ q ≤ q 0 k q 0 k − q ( R k ) q / ( q 0 k ) K q . (67) \mathbb{E}|\operatorname{median}(E_1,\ldots,E_R)|^q\le\frac{q_0k}{q_0k-q}\binom{R}{k}^{q/(q_0k)}K^q. \tag*{(67)} E ∣ median ( E 1 , … , E R ) ∣ q ≤ q 0 k − q q 0 k ( k R ) q / ( q 0 k ) K q . (67)
Proof. Write M R : = median ( E 1 , … , E R ) M_R:=\operatorname{median}(E_1,\ldots,E_R) M R := median ( E 1 , … , E R ) . If K = 0 K=0 K = 0 , then E ν = 0 E_\nu=0 E ν = 0 almost surely for every ν \nu ν . Suppose K > 0 K>0 K > 0 . If ∣ M R ∣ > t |M_R|>t ∣ M R ∣ > t , then ∣ E ν ∣ > t |E_\nu|>t ∣ E ν ∣ > t for at least k k k indices. Therefore, by a union bound over the k k k -element subsets A ⊆ { 1 , … , R } A\subseteq\{1,\ldots,R\} A ⊆ { 1 , … , R } and independence,
P ( ∣ M R ∣ > t ) ≤ ∑ ∣ A ∣ = k P ( ⋂ ν ∈ A { ∣ E ν ∣ > t } ) = ( R k ) P ( ∣ E 1 ∣ > t ) k ≤ ( R k ) ( K t ) q 0 k , \mathbb{P}(|M_R|>t)\le\sum_{|A|=k}\mathbb{P}\left(\bigcap_{\nu\in A}\{|E_\nu|>t\}\right)=\binom{R}{k}\mathbb{P}(|E_1|>t)^k\le\binom{R}{k}\left(\frac{K}{t}\right)^{q_0k}, P ( ∣ M R ∣ > t ) ≤ ∣ A ∣ = k ∑ P ( ν ∈ A ⋂ { ∣ E ν ∣ > t } ) = ( k R ) P ( ∣ E 1 ∣ > t ) k ≤ ( k R ) ( t K ) q 0 k ,
where the last inequality is Markov’s inequality. Hence
P ( ∣ M R ∣ > t ) ≤ min { 1 , ( R k ) ( K / t ) q 0 k } . \mathbb{P}(|M_R|>t)\le\min\left\{1,\binom{R}{k}(K/t)^{q_0k}\right\}. P ( ∣ M R ∣ > t ) ≤ min { 1 , ( k R ) ( K / t ) q 0 k } .
Set t ∗ = ( R k ) 1 / ( q 0 k ) K t_*=\binom{R}{k}^{1/(q_0k)}K t ∗ = ( k R ) 1/ ( q 0 k ) K . Since q < q 0 k q<q_0k q < q 0 k , the tail integral formula and the preceding bound give
E ∣ M R ∣ q = q ∫ 0 ∞ t q − 1 P ( ∣ M R ∣ > t ) d t ≤ q ∫ 0 t ∗ t q − 1 d t + q ( R k ) K q 0 k ∫ t ∗ ∞ t q − 1 − q 0 k d t = t ∗ q + q q 0 k − q ( R k ) K q 0 k t ∗ q − q 0 k = q 0 k q 0 k − q t ∗ q . \begin{aligned}
\mathbb{E}|M_R|^q=q\int_0^\infty t^{q-1}\mathbb{P}(|M_R|>t)\,\mathrm{d}t\le q\int_0^{t_*}t^{q-1}\,\mathrm{d}t+q\binom{R}{k}K^{q_0k}\int_{t_*}^\infty t^{q-1-q_0k}\,\mathrm{d}t \\
&=t_*^q+\frac{q}{q_0k-q}\binom{R}{k}K^{q_0k}t_*^{q-q_0k}=\frac{q_0k}{q_0k-q}t_*^q.
\end{aligned} E ∣ M R ∣ q = q ∫ 0 ∞ t q − 1 P ( ∣ M R ∣ > t ) d t ≤ q ∫ 0 t ∗ t q − 1 d t + q ( k R ) K q 0 k ∫ t ∗ ∞ t q − 1 − q 0 k d t = t ∗ q + q 0 k − q q ( k R ) K q 0 k t ∗ q − q 0 k = q 0 k − q q 0 k t ∗ q .
Inserting the value of t ∗ t_* t ∗ proves (67) .
Proof of Theorem 3.1 . Fix 0 < ε < 1 / 2 0<\varepsilon<1/2 0 < ε < 1/2 . Set α = α 0 \alpha=\alpha_0 α = α 0 as in (62) . In Proposition 5.3 , take λ = 1 / [ 2 ( 1 − ε ) ] \lambda=1/[2(1-\varepsilon)] λ = 1/ [ 2 ( 1 − ε )] and δ ∗ = 1 − ε / 2 \delta_* =1-\varepsilon/2 δ ∗ = 1 − ε /2 ; then 2 δ ∗ λ > 1 2\delta_*\lambda>1 2 δ ∗ λ > 1 . For this value of λ \lambda λ , we have 2 λ / ( 1 + λ ) = 2 / ( 3 − 2 ε ) > 2 / 3 2\lambda/(1+\lambda)=2/(3-2\varepsilon)>2/3 2 λ / ( 1 + λ ) = 2/ ( 3 − 2 ε ) > 2/3 . By (63) and (45) ,
sup m ∈ M ∑ u ≠ ∅ ρ λ ∣ u ∣ / ( 1 + λ ) S u ( F m ) 2 λ / ( 1 + λ ) ≤ C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) λ / ( 1 + λ ) sup m ∈ M ∑ u ≠ ∅ ( ρ λ 1 / ( 1 + λ ) ) ∣ u ∣ D m , u 2 λ / ( 1 + λ ) ≤ C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) λ / ( 1 + λ ) C D ( ρ λ 1 / ( 1 + λ ) , 2 λ 1 + λ ; Θ 2 / 3 ) . \begin{aligned}
\sup_{m\in\mathcal{M}}\sum_{u\ne\varnothing}\rho_\lambda^{|u|/(1+\lambda)}S_u(F_m)^{2\lambda/(1+\lambda)} \\
&\le C_{\mathrm{aux}}(|x_0|_2,\Theta_1)^{\lambda/(1+\lambda)}
\sup_{m\in\mathcal{M}}\sum_{u\ne\varnothing}\left(\rho_\lambda^{1/(1+\lambda)}\right)^{|u|}D_{m,u}^{2\lambda/(1+\lambda)} \\
&\le C_{\mathrm{aux}}(|x_0|_2,\Theta_1)^{\lambda/(1+\lambda)}
C_D\left(\rho_\lambda^{1/(1+\lambda)},\frac{2\lambda}{1+\lambda};\Theta_{2/3}\right).
\end{aligned} m ∈ M sup u = ∅ ∑ ρ λ ∣ u ∣/ ( 1 + λ ) S u ( F m ) 2 λ / ( 1 + λ ) ≤ C aux ( ∣ x 0 ∣ 2 , Θ 1 ) λ / ( 1 + λ ) m ∈ M sup u = ∅ ∑ ( ρ λ 1/ ( 1 + λ ) ) ∣ u ∣ D m , u 2 λ / ( 1 + λ ) ≤ C aux ( ∣ x 0 ∣ 2 , Θ 1 ) λ / ( 1 + λ ) C D ( ρ λ 1/ ( 1 + λ ) , 1 + λ 2 λ ; Θ 2/3 ) .
Here C a u x C_{\mathrm{aux}} C aux and C D C_D C D are the constants in Lemma 5.1 and Theorem 4.1 , respectively. By the definition of C λ C_\lambda C λ in (64) , we obtain
sup m ∈ M C λ ( F m ) ≤ C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) λ [ C D ( ρ λ 1 / ( 1 + λ ) , 2 λ 1 + λ ; Θ 2 / 3 ) ] 1 + λ = : C l a t ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2 / 3 ) < ∞ . (68) \begin{aligned}
\sup_{m\in\mathcal{M}}C_\lambda(F_m)\le C_{\mathrm{aux}}(|x_0|_2,\Theta_1)^\lambda\left[C_D\left(\rho_\lambda^{1/(1+\lambda)},\frac{2\lambda}{1+\lambda};\Theta_{2/3}\right)\right]^{1+\lambda} \\
&=:C_{\mathrm{lat}}(|x_0|_2,\Theta_1,\Theta_{2/3})<\infty. \tag*{(68)}
\end{aligned} m ∈ M sup C λ ( F m ) ≤ C aux ( ∣ x 0 ∣ 2 , Θ 1 ) λ [ C D ( ρ λ 1/ ( 1 + λ ) , 1 + λ 2 λ ; Θ 2/3 ) ] 1 + λ =: C lat ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2/3 ) < ∞. (68)
Since α 0 \alpha_0 α 0 is defined by (62) and ρ λ \rho_\lambda ρ λ by (32) , this bound depends only on ε \varepsilon ε , τ \tau τ , T T T , K 0 K_0 K 0 , B 0 B_0 B 0 , B 1 B_1 B 1 , G 0 G_0 G 0 , G 1 G_1 G 1 , β g \beta_g β g , ∣ x 0 ∣ 2 |x_0|_2 ∣ x 0 ∣ 2 , Θ 1 \Theta_1 Θ 1 , and Θ 2 / 3 \Theta_{2/3} Θ 2/3 . For fixed ε \varepsilon ε and fixed model parameters, it is nondecreasing in ∣ x 0 ∣ 2 |x_0|_2 ∣ x 0 ∣ 2 , Θ 1 \Theta_1 Θ 1 , and Θ 2 / 3 \Theta_{2/3} Θ 2/3 . Indeed, α 0 \alpha_0 α 0 and ρ λ \rho_\lambda ρ λ are nondecreasing in Θ 1 \Theta_1 Θ 1 , while C a u x C_{\mathrm{aux}} C aux and C D C_D C D have the monotonicities stated above.
Substituting F = F m F=F_m F = F m in (65) and using (68) yields
sup m ∈ M E A , Δ ∣ Q A , Δ N , m − I m ∣ 2 λ ≤ C l a t ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2 / 3 ) N − 1 . (69) \sup_{m\in\mathcal{M}}\mathbb{E}_{A,\Delta}|Q_{A,\Delta}^{N,m}-\mathcal{I}_m|^{2\lambda}\le\frac{C_{\mathrm{lat}}(|x_0|_2,\Theta_1,\Theta_{2/3})}{N-1}. \tag*{(69)} m ∈ M sup E A , Δ ∣ Q A , Δ N , m − I m ∣ 2 λ ≤ N − 1 C lat ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2/3 ) . (69)
Since 2 λ > 1 2\lambda>1 2 λ > 1 , Jensen’s inequality first gives
∥ Q A , Δ N , m − I m ∥ L 1 ≤ ( E ∣ Q A , Δ N , m − I m ∣ 2 λ ) 1 / ( 2 λ ) ≤ ( C l a t ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2 / 3 ) N − 1 ) 1 / ( 2 λ ) . \|Q_{A,\Delta}^{N,m}-\mathcal{I}_m\|_{L^1}\le\left(\mathbb{E}|Q_{A,\Delta}^{N,m}-\mathcal{I}_m|^{2\lambda}\right)^{1/(2\lambda)}
\le\left(\frac{C_{\mathrm{lat}}(|x_0|_2,\Theta_1,\Theta_{2/3})}{N-1}\right)^{1/(2\lambda)}. ∥ Q A , Δ N , m − I m ∥ L 1 ≤ ( E ∣ Q A , Δ N , m − I m ∣ 2 λ ) 1/ ( 2 λ ) ≤ ( N − 1 C lat ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2/3 ) ) 1/ ( 2 λ ) .
Since N − 1 ≥ N / 2 N-1\ge N/2 N − 1 ≥ N /2 and 1 / ( 2 λ ) = 1 − ε 1/(2\lambda)=1-\varepsilon 1/ ( 2 λ ) = 1 − ε , this proves (34) with
C ε : = 2 1 / ( 2 λ ) C l a t ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2 / 3 ) 1 / ( 2 λ ) . (70) C_\varepsilon:=2^{1/(2\lambda)}C_{\mathrm{lat}}(|x_0|_2,\Theta_1,\Theta_{2/3})^{1/(2\lambda)}. \tag*{(70)} C ε := 2 1/ ( 2 λ ) C lat ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2/3 ) 1/ ( 2 λ ) . (70)
For R = 2 k − 1 R=2k-1 R = 2 k − 1 and 1 ≤ q < 2 λ k = k / ( 1 − ε ) 1\le q<2\lambda k=k/(1-\varepsilon) 1 ≤ q < 2 λk = k / ( 1 − ε ) , apply Lemma 5.4 to the independent errors Q A ν , Δ ν N , m − I m Q_{A_\nu,\Delta_\nu}^{N,m}-\mathcal{I}_m Q A ν , Δ ν N , m − I m , with q 0 = 2 λ q_0=2\lambda q 0 = 2 λ and K = ( C l a t ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2 / 3 ) / ( N − 1 ) ) 1 / ( 2 λ ) K=(C_{\mathrm{lat}}(|x_0|_2,\Theta_1,\Theta_{2/3})/(N-1))^{1/(2\lambda)} K = ( C lat ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2/3 ) / ( N − 1 ) ) 1/ ( 2 λ ) . Then we have
∥ M R , N , m − I m ∥ L q ≤ ( 2 λ k 2 λ k − q ) 1 / q ( R k ) 1 / ( 2 λ k ) ( C l a t ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2 / 3 ) N − 1 ) 1 / ( 2 λ ) . \|M_{R,N,m}-\mathcal{I}_m\|_{L^q}\le\left(\frac{2\lambda k}{2\lambda k-q}\right)^{1/q}\binom{R}{k}^{1/(2\lambda k)}\left(\frac{C_{\mathrm{lat}}(|x_0|_2,\Theta_1,\Theta_{2/3})}{N-1}\right)^{1/(2\lambda)}. ∥ M R , N , m − I m ∥ L q ≤ ( 2 λk − q 2 λk ) 1/ q ( k R ) 1/ ( 2 λk ) ( N − 1 C lat ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2/3 ) ) 1/ ( 2 λ ) .
Using N − 1 ≥ N / 2 N-1 \ge N/2 N − 1 ≥ N /2 proves (35) with
C ε , q , R : = ( 2 λ k 2 λ k − q ) 1 / q ( R k ) 1 / ( 2 λ k ) C ε . (71) C_{\varepsilon,q,R}:=\left(\frac{2\lambda_k}{2\lambda_k-q}\right)^{1/q}\binom{R}{k}^{1/(2\lambda_k)}C_\varepsilon. \tag*{(71)} C ε , q , R := ( 2 λ k − q 2 λ k ) 1/ q ( k R ) 1/ ( 2 λ k ) C ε . (71)
By (68) and (70) , C ε C_\varepsilon C ε depends only on ε \varepsilon ε , τ \tau τ , T T T , K 0 K_0 K 0 , B 0 B_0 B 0 , B 1 B_1 B 1 , G 0 G_0 G 0 , G 1 G_1 G 1 , β g \beta_g β g , ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 , Θ 1 \Theta_1 Θ 1 , and Θ 2 / 3 \Theta_{2/3} Θ 2/3 . By (71) , C ε , q , R C_{\varepsilon,q,R} C ε , q , R additionally depends on q q q , R R R .
Proof of Corollary 3.3. Under Assumption 2.2, the model parameters have common bounds across dimensions. Under Assumption 2.3, (13) gives
0 ≤ Θ 1 ≤ M 2 / 3 3 / 2 , 0 ≤ Θ 2 / 3 ≤ M 2 / 3 . 0 \le\Theta_1 \le M_{2/3}^{3/2}, \qquad0 \le\Theta_{2/3} \le M_{2/3}. 0 ≤ Θ 1 ≤ M 2/3 3/2 , 0 ≤ Θ 2/3 ≤ M 2/3 .
By the monotonicity of C l a t C_{\mathrm{lat}} C lat established immediately after (68) , ∣ x 0 ∣ 2 ≤ R 0 \lvert x_0\rvert_2 \le R_0 ∣ x 0 ∣ 2 ≤ R 0 and (13) give
C l a t ( ∣ x 0 ∣ 2 , Θ 1 , Θ 2 / 3 ) ≤ C l a t ( R 0 , M 2 / 3 3 / 2 , M 2 / 3 ) . C_{\mathrm{lat}}(\lvert x_0\rvert_2,\Theta_1,\Theta_{2/3}) \le C_{\mathrm{lat}}(R_0,M_{2/3}^{3/2},M_{2/3}). C lat (∣ x 0 ∣ 2 , Θ 1 , Θ 2/3 ) ≤ C lat ( R 0 , M 2/3 3/2 , M 2/3 ) .
The right-hand side is independent of d x d_x d x , d w d_w d w . Therefore, (70) and (71) give dimension-independent bounds for C ε C_\varepsilon C ε and C ε , q , R C_{\varepsilon,q,R} C ε , q , R .
Numerical experiments
In this section, we use numerical examples to examine the sampling error of randomly shifted rank-1 lattice rules and of their median versions applied to the Euler–Maruyama scheme and to test the conclusions of Theorem 3.1 and Corollary 3.3 . We focus on their advantage over standard Monte Carlo (MC), the stability of the QMC error as the number of time steps m m m increases, and, under the stated summability condition on the columns of Σ \Sigma Σ , its stability as the Brownian path dimension d w d_w d w increases. All models use T = 1 T=1 T = 1 , and the target is the Euler–Maruyama expectation I m I_m I m . The code and data used for these numerical experiments are available at https://github.com/ZiyangYe2000/lattice4SDE.
We consider four estimators: MC, single QMC, median-of-three QMC, and median-of-thirteen QMC. In all experiments, d x = d w = d d_x=d_w=d d x = d w = d . For a fixed pair ( d , m ) (d,m) ( d , m ) , let s = d m s=dm s = d m and write F d , m ( z ) = g ( X m h ( z ) ) F_{d,m}(z)=g(X_m^h(z)) F d , m ( z ) = g ( X m h ( z )) for the integrand F m F_m F m in (25) , displaying its dependence on d d d . For a prescribed budget of n n n simulated Euler–Maruyama paths, the MC estimator is
I ^ m , n M C = 1 n ∑ ℓ = 1 n F d , m ( Z ℓ ) . \widehat{I}_{m,n}^{\mathrm{MC}}=\frac{1}{n}\sum_{\ell=1}^{n}F_{d,m}(Z_\ell). I m , n MC = n 1 ℓ = 1 ∑ n F d , m ( Z ℓ ) .
Here Z 1 , … , Z n ∼ i . i . d . N ( 0 , I d s ) Z_1,\ldots,Z_n \mathrel{\mathop{\sim}^{\mathrm{i.i.d.}}} N(0,I_{d_s}) Z 1 , … , Z n ∼ i.i.d. N ( 0 , I d s ) . For the lattice-rule estimators, each constituent rule independently randomizes both the generating vector and the shift: A ν A_\nu A ν is sampled uniformly from { 1 , … , N − 1 } \{1,\ldots,N-1\} { 1 , … , N − 1 } , while Δ ν \Delta_\nu Δ ν is uniform on [ 0 , 1 ] s [0,1]^s [ 0 , 1 ] s . The ν \nu ν -th randomized rank-1 lattice estimate, Q m , N ( ν ) = Q A ν , Δ ν N , m Q_{m,N}^{(\nu)}=Q_{A_\nu,\Delta_\nu}^{N,m} Q m , N ( ν ) = Q A ν , Δ ν N , m in (28) , is
Q m , N ( ν ) = 1 N ∑ ℓ = 0 N − 1 F d , m ( Φ − 1 ( { ℓ A ν N + Δ ν } ) ) . Q_{m,N}^{(\nu)}=\frac{1}{N}\sum_{\ell=0}^{N-1}F_{d,m}\left(\Phi^{-1}\left(\left\{\frac{\ell A_\nu}{N}+\Delta_\nu\right\}\right)\right). Q m , N ( ν ) = N 1 ℓ = 0 ∑ N − 1 F d , m ( Φ − 1 ( { N ℓ A ν + Δ ν } ) ) .
Single QMC uses one such rule,
I ^ m , n S Q M C = Q m , N 1 ( 1 ) , N 1 = the nearest prime to n . \widehat{I}_{m,n}^{\mathrm{SQMC}}=Q_{m,N_1}^{(1)}, \qquad N_1=\text{the nearest prime to }n. I m , n SQMC = Q m , N 1 ( 1 ) , N 1 = the nearest prime to n .
The other two estimators are
I ^ m , n m e d ( R ) = median { Q m , N R ( 1 ) , … , Q m , N R ( R ) } , R ∈ { 3 , 13 } , \widehat{I}_{m,n}^{\mathrm{med}(R)}=\operatorname{median}\left\{Q_{m,N_R}^{(1)},\ldots,Q_{m,N_R}^{(R)}\right\}, \qquad R\in\{3,13\}, I m , n med ( R ) = median { Q m , N R ( 1 ) , … , Q m , N R ( R ) } , R ∈ { 3 , 13 } ,
where N R N_R N R is the nearest prime to n / R n/R n / R . Hence, every estimator uses approximately n n n Euler–Maruyama paths in total. The figures use the actual number of path evaluations on the horizontal axis: n n n for MC, N 1 N_1 N 1 for single QMC, and R N R RN_R R N R for the median rules.
For each ( d , m ) (d,m) ( d , m ) , I m r e f \mathcal{I}^{\mathrm{ref}}_m I m ref is a high-accuracy estimate of the Euler–Maruyama expectation I m \mathcal{I}_m I m . Using n r e p = 32 n_{\mathrm{rep}}=32 n rep = 32 independent replications, we compute
RMSE ( n ) = { 1 n r e p ∑ ℓ = 1 n r e p ( I ^ m , n ( ℓ ) − I m r e f ) 2 } 1 / 2 . \operatorname{RMSE}(n)=\left\{\frac{1}{n_{\mathrm{rep}}}\sum_{\ell=1}^{n_{\mathrm{rep}}}\left(\widehat{\mathcal{I}}_{m,n}^{(\ell)}-\mathcal{I}^{\mathrm{ref}}_m\right)^2\right\}^{1/2}. RMSE ( n ) = { n rep 1 ℓ = 1 ∑ n rep ( I m , n ( ℓ ) − I m ref ) 2 } 1/2 .
Time-modulated asymmetric Kuramoto system
The first model is a noisy population of coupled phase oscillators,
d X j ( t ) = [ ω j + ( 1 + 1 2 sin ( 2 π t ) ) ∑ j ′ = 1 j ′ ≠ j d K j j ′ sin ( X j ′ ( t ) − X j ( t ) ) ] d t + 0.4 d W j ( t ) , j = 1 , … , d , (72) \mathrm{d}X_j(t)=\left[\omega_j+\left(1+\frac{1}{2}\sin(2\pi t)\right)\sum_{\substack{j'=1\\j'\ne j}}^d K_{jj'}\sin\left(X_{j'}(t)-X_j(t)\right)\right]\mathrm{d}t+0.4\,\mathrm{d}W_j(t),\qquad j=1,\ldots,d, \tag*{(72)} d X j ( t ) = ω j + ( 1 + 2 1 sin ( 2 π t ) ) j ′ = 1 j ′ = j ∑ d K j j ′ sin ( X j ′ ( t ) − X j ( t ) ) d t + 0.4 d W j ( t ) , j = 1 , … , d , (72)
where
ω j = − 0.5 + j − 1 d − 1 , K j j ′ = 1 + 0.15 sin ( j ( j ′ + 1 ) ) d ( j ≠ j ′ ) , \omega_j=-0.5+\frac{j-1}{d-1},\qquad K_{jj'}=\frac{1+0.15\sin\left(j(j'+1)\right)}{d}\quad(j\ne j'), ω j = − 0.5 + d − 1 j − 1 , K j j ′ = d 1 + 0.15 sin ( j ( j ′ + 1 ) ) ( j = j ′ ) ,
K j j = 0 , X j ( 0 ) = 2 π ( j − 1 ) d . K_{jj}=0,\qquad X_j(0)=\frac{2\pi(j-1)}{d}. K j j = 0 , X j ( 0 ) = d 2 π ( j − 1 ) .
This is a stochastic Kuramoto-type system with heterogeneous frequencies and asymmetric coupling [1 ] . The factor 1 + 1 2 sin ( 2 π t ) 1+\frac{1}{2}\sin(2\pi t) 1 + 2 1 sin ( 2 π t ) periodically modulates the common interaction strength and tests the time-dependent setting of Theorem 3.1 . We take the payoff function
g ( x ) = ∣ 1 d ∑ j = 1 d e i x j ∣ 2 , i 2 = − 1 , g(x)=\left|\frac{1}{d}\sum_{j=1}^d e^{\mathrm{i}x_j}\right|^2,\qquad\mathrm{i}^2=-1, g ( x ) = d 1 j = 1 ∑ d e i x j 2 , i 2 = − 1 ,
which is the squared Kuramoto order parameter. It is close to one for coherent phases and close to zero for a dispersed population. It is straightforward to verify Assumption 2.1 with τ = 1 \tau=1 τ = 1 for each fixed d d d . Here Σ = 0.4 I d \Sigma=0.4I_d Σ = 0.4 I d , so Θ 2 / 3 = 0.4 2 / 3 d \Theta^{2/3}=0.4^{2/3}d Θ 2/3 = 0. 4 2/3 d . Hence Θ 2 / 3 \Theta^{2/3} Θ 2/3 grows linearly in d d d , so Assumption 2.3 does not hold uniformly in d d d , and any stability in d d d observed for this model is not covered by Corollary 3.3 . Since the factor 1 + 1 2 sin ( 2 π t ) 1+\frac{1}{2}\sin(2\pi t) 1 + 2 1 sin ( 2 π t ) is Lipschitz continuous in t t t , Theorem 3.7 gives a time discretization error of order m − 1 m^{-1} m − 1 .
Figure 1 compares all four estimators at ( d , m ) = ( 8 , 256 ) (d,m)=(8,256) ( d , m ) = ( 8 , 256 ) . At comparable values of n n n , QMC generally improves upon MC. Although single QMC sometimes attains the smallest empirical RMSE, its curve contains pronounced upward fluctuations, reflecting occasional poor estimates from an individual randomized rule. Median-of-three and median-of-thirteen suppress this instability and have a smoother error decay. At the largest budgets, the median-QMC errors exhibit an empirical rate close to n − 0.9 n^{-0.9} n − 0.9 , substantially steeper than the MC reference rate n − 0.5 n^{-0.5} n − 0.5 .
Figure 1. Method comparison for the time-modulated asymmetric Kuramoto system (6.1) with d = 8 d = 8 d = 8 and m = 256 m = 256 m = 256 .
Figure 2 examines the effects of time refinement and state dimension. In both panels, median-of-thirteen has smaller RMSE than MC at comparable values of n n n , and its large-budget decay is close to the n − 0.8 n^{-0.8} n − 0.8 reference rate. In panel (a), we fix d = 8 d = 8 d = 8 and vary m ∈ { 64 , 256 , 1024 } m \in\{64, 256, 1024\} m ∈ { 64 , 256 , 1024 } . For both MC and median-of-thirteen, the three RMSE curves remain close as m m m increases, with no visible loss of accuracy under time refinement. In panel (b), we fix m = 256 m = 256 m = 256 and compare d = 4 d = 4 d = 4 with d = 16 d = 16 d = 16 . The RMSE is smaller at d = 16 d = 16 d = 16 for both methods. The decrease may be related to the 1 / d 1/d 1/ d normalization in the payoff.
(a) Fixed d = 8 d = 8 d = 8 ; varying m m m .
(b) Fixed m = 256 m = 256 m = 256 ; varying d d d .
Figure 2. Dependence on the number of time steps and the state dimension for the time-modulated asymmetric Kuramoto system (6.1).
Time-dependent overdamped Langevin system
The second model is a system of interacting particles governed by time-dependent overdamped Langevin dynamics [26 ] ,
d X j ( t ) = [ − X j ( t ) − a ( t ) { sin X j ( t ) + 0.5 d ∑ j ′ ≠ j sin ( X j ( t ) − X j ′ ( t ) ) } ] d t + 0.4 d W j ( t ) , j = 1 , … , d , (73) \begin{aligned}
\mathrm{d}X_j(t)={}&\left[-X_j(t)-a(t)\left\{\sin X_j(t)+\frac{0.5}{d}\sum_{j'\ne j}\sin\left(X_j(t)-X_{j'}(t)\right)\right\}\right]\mathrm{d}t\\
&+0.4\,\mathrm{d}W_j(t),\qquad j=1,\ldots,d, \tag*{(73)}
\end{aligned} d X j ( t ) = − X j ( t ) − a ( t ) ⎩ ⎨ ⎧ sin X j ( t ) + d 0.5 j ′ = j ∑ sin ( X j ( t ) − X j ′ ( t ) ) ⎭ ⎬ ⎫ d t + 0.4 d W j ( t ) , j = 1 , … , d , (73)
with
a ( t ) = 1 + 1 2 ∣ 2 t − 1 ∣ 1 / 2 , X j ( 0 ) = 0.2 cos ( 2 π ( j − 1 ) d ) . a(t)=1+\frac{1}{2}|2t-1|^{1/2},\qquad X_j(0)=0.2\cos\left(\frac{2\pi(j-1)}{d}\right). a ( t ) = 1 + 2 1 ∣2 t − 1 ∣ 1/2 , X j ( 0 ) = 0.2 cos ( d 2 π ( j − 1 ) ) .
Its drift is − ∇ x V ( t , x ) -\nabla_xV(t,x) − ∇ x V ( t , x ) for the time-dependent potential
V ( t , x ) = 1 2 ∣ x ∣ 2 + a ( t ) { ∑ j = 1 d ( 1 − cos x j ) + 0.5 d ∑ j < j ′ ( 1 − cos ( x j − x j ′ ) ) } . V(t,x)=\frac{1}{2}|x|^2+a(t)\left\{\sum_{j=1}^{d}(1-\cos x_j)+\frac{0.5}{d}\sum_{j<j'}(1-\cos(x_j-x_{j'}))\right\}. V ( t , x ) = 2 1 ∣ x ∣ 2 + a ( t ) ⎩ ⎨ ⎧ j = 1 ∑ d ( 1 − cos x j ) + d 0.5 j < j ′ ∑ ( 1 − cos ( x j − x j ′ )) ⎭ ⎬ ⎫ .
We take the payoff function
g ( x ) = exp ( 0.2 d ∑ j = 1 d x j ) . g(x)=\exp\left(\frac{0.2}{\sqrt{d}}\sum_{j=1}^{d}x_j\right). g ( x ) = exp ( d 0.2 j = 1 ∑ d x j ) .
This is the exponential of a normalized collective coordinate; the factor d − 1 / 2 d^{-1/2} d − 1/2 keeps its scale comparable as d d d varies. Assumption 2.1 is easily verified with τ = 1 \tau=1 τ = 1 for each fixed d d d . As in the first model, Θ 2 / 3 = 0.4 2 / 3 d \Theta_{2/3}=0.4^{2/3}d Θ 2/3 = 0. 4 2/3 d . Hence Assumption 2.3 again does not hold uniformly in d d d . The modulation a a a is 1/2-Hölder continuous but not Lipschitz continuous at t = 1 / 2 t=1/2 t = 1/2 , so Theorem 3.6 applies and gives a time discretization error of order m − 1 / 2 m^{-1/2} m − 1/2 , whereas Theorem 3.7 does not apply.
Figure 3 compares the four estimators at ( d , m ) = ( 8 , 256 ) (d,m)=(8,256) ( d , m ) = ( 8 , 256 ) . As in the previous example, all three QMC estimators have substantially smaller RMSE than MC. Single QMC has occasional upward jumps, whereas the two median estimators decay more steadily. At large budgets, median-of-thirteen has an empirical rate close to n − 0.7 n^{-0.7} n − 0.7 .
Figure 3. Method comparison for the time-dependent overdamped Langevin system (73) with d = 8 d=8 d = 8 and m = 256 m=256 m = 256 .
Figure 4 shows the dependence on m m m and d d d . In both panels, median-of-thirteen remains below MC and its decay is close to the n − 0.8 n^{-0.8} n − 0.8 reference rate. For fixed d = 8 d = 8 d = 8 , the RMSE curves change little as m m m increases from 64 to 1024. For fixed m = 256 m = 256 m = 256 , the curves for d = 4 d = 4 d = 4 and d = 64 d = 64 d = 64 are also close, with no visible deterioration at the larger dimension. This robustness in d d d is not covered by Corollary 3.3 , since Θ 2 / 3 \Theta_{2/3} Θ 2/3 grows linearly in d d d for this model; it suggests that Assumption 2.3 is sufficient but not necessary for dimension-stable behavior.
Figure 4. Dependence on the number of time steps and the state dimension for the time-dependent overdamped Langevin system (6.2).
Dimension-uniform design and coordinate rotation
The final experiment is designed around the dimension-independent conclusion of Corollary 3.3 . The aligned model is
d X t = [ − ( I d + 0.25 L d ) X t + 0.5 sin ( X t ) ] d t + Σ d a l d W t , g ( x ) = ∣ x ∣ 2 2 , \mathrm{d}X_t = \left[-(\mathrm{I}_d + 0.25L_d)X_t + 0.5\sin(X_t)\right]\mathrm{d}t + \Sigma_d^{\mathrm{al}}\mathrm{d}W_t,\qquad g(x) = |x|_2^2, d X t = [ − ( I d + 0.25 L d ) X t + 0.5 sin ( X t ) ] d t + Σ d al d W t , g ( x ) = ∣ x ∣ 2 2 ,
where X 0 = 0 X_0 = 0 X 0 = 0 and
L d = ( 2 − 1 − 1 2 − 1 ⋱ ⋱ ⋱ − 1 2 − 1 − 1 2 ) ∈ R d × d . L_d =
\begin{pmatrix}
2 & -1 \\
-1 & 2 & -1 \\
& \ddots& \ddots& \ddots\\
& & -1 & 2 & -1 \\
& & & -1 & 2
\end{pmatrix}
\in\mathbb{R}^{d\times d}. L d = 2 − 1 − 1 2 ⋱ − 1 ⋱ − 1 ⋱ 2 − 1 − 1 2 ∈ R d × d .
The diffusion matrix is
Σ d a l = 0.4 diag ( 1 , 2 − 2 , … , d − 2 ) , ∑ r = 1 d ∣ Σ d a l e r ∣ 2 / 3 ≤ 0.4 2 / 3 ζ ( 4 / 3 ) . \Sigma_d^{\mathrm{al}} = 0.4\operatorname{diag}(1,2^{-2},\ldots,d^{-2}),\qquad\sum_{r=1}^{d}\left|\Sigma_d^{\mathrm{al}}e_r\right|^{2/3}\le0.4^{2/3}\zeta(4/3). Σ d al = 0.4 diag ( 1 , 2 − 2 , … , d − 2 ) , r = 1 ∑ d Σ d al e r 2/3 ≤ 0. 4 2/3 ζ ( 4/3 ) .
The model satisfies Assumptions 2.1 and 2.2 with τ = 1 \tau= 1 τ = 1 : ∥ L d ∥ 2 ≤ 4 \lVert L_d\rVert_2 \le4 ∥ L d ∥ 2 ≤ 4 , the higher derivative operator norms of the componentwise sine are at most one, and the quadratic payoff has common derivative bounds. The displayed column bound verifies Assumption 2.3. For the rotated model we set
Σ d r o t = Σ d a l H d , \Sigma_d^{\mathrm{rot}}=\Sigma_d^{\mathrm{al}}H_d, Σ d rot = Σ d al H d ,
where d d d is a power of two and H d H_d H d is the normalized Sylvester Hadamard matrix defined recursively by
H 1 = ( 1 ) , H 2 d = 1 2 ( H d H d H d − H d ) . H_1=(1),\qquad H_{2d}=\frac{1}{\sqrt{2}}
\begin{pmatrix}
H_d & H_d \\
H_d & -H_d
\end{pmatrix}. H 1 = ( 1 ) , H 2 d = 2 1 ( H d H d H d − H d ) .
Then H d H d T = I d H_dH_d^{\mathsf{T}} = I_d H d H d T = I d , and hence
Σ d r o t ( Σ d r o t ) T = Σ d a l ( Σ d a l ) T . \Sigma_d^{\mathrm{rot}}\left(\Sigma_d^{\mathrm{rot}}\right)^{\mathsf{T}} = \Sigma_d^{\mathrm{al}}\left(\Sigma_d^{\mathrm{al}}\right)^{\mathsf{T}}. Σ d rot ( Σ d rot ) T = Σ d al ( Σ d al ) T .
The two Euler–Maruyama schemes therefore have the same law. On the other hand,
∑ r = 1 d ∣ Σ d r o t e r ∣ 2 = 0.4 d 1 / 2 ( ∑ j = 1 d j − 4 ) 1 / 2 ⟶ ∞ . \sum_{r=1}^{d}\left|\Sigma_d^{\mathrm{rot}}e_r\right|_2 = 0.4d^{1/2}\left(\sum_{j=1}^{d}j^{-4}\right)^{1/2} \longrightarrow\infty. r = 1 ∑ d Σ d rot e r 2 = 0.4 d 1/2 ( j = 1 ∑ d j − 4 ) 1/2 ⟶ ∞.
Thus the column norms are not even uniformly ℓ 1 \ell^1 ℓ 1 -summable in d d d , and the summability condition is no longer satisfied as d → ∞ d \to\infty d → ∞ . The QMC rule depends on the Gaussian coordinate representation, and the rotation spreads the dominant noise directions over all coordinates.
Figure 5 compares the aligned and rotated representations using the same slices. Panels (a)–(b) fix m = 64 m = 64 m = 64 and use d = 4 , 16 , 64 d = 4, 16, 64 d = 4 , 16 , 64 ; panels (c)–(d) fix d = 16 d = 16 d = 16 and use m = 64 , 256 , 1024 m = 64, 256, 1024 m = 64 , 256 , 1024 . The MC error levels are comparable between the aligned and rotated representations. For Σ d a l \Sigma_d^{\mathrm{al}} Σ d al , median-of-thirteen has smaller RMSE than MC and approaches the n − 0.8 n^{-0.8} n − 0.8 reference rate at large budgets. Its error does not visibly deteriorate as either m m m or d d d increases, consistent with Corollary 3.3 . For Σ d r o t \Sigma_d^{\mathrm{rot}} Σ d rot , the advantage of QMC over MC is pronounced at d = 4 d = 4 d = 4 but largely disappears at d = 16 d = 16 d = 16 and d = 64 d = 64 d = 64 , where the QMC and MC errors are comparable. At fixed d = 16 d = 16 d = 16 , increasing m m m has little effect on the QMC error. These results illustrate that rotating Σ \Sigma Σ as in Remark 3.4 so that Assumption 2.3 holds preserves the target expectation and can substantially improve the efficiency of the lattice estimators.
Figure 5. Dimension and time-step comparisons for the aligned and rotated representations. (a) Aligned, fixed m = 64 m = 64 m = 64 . (b) Rotated, fixed m = 64 m = 64 m = 64 . (c) Aligned, fixed d = 16 d = 16 d = 16 . (d) Rotated, fixed d = 16 d = 16 d = 16 . The underlying Euler laws are identical at common ( d , m ) (d,m) ( d , m ) , whereas the QMC coordinate representations differ.
Conclusion
We studied randomly shifted rank-1 lattice rules for computing expectations of solutions to SDEs with a constant diffusion matrix. Using the Euler–Maruyama scheme and Brownian bridge construction, we established almost first-order sampling error bounds. A rooted-tree expansion of the mixed derivatives yields summability estimates uniform in the number of time steps. These estimates give an O ( N − 1 + ε ) O(N^{-1+\varepsilon}) O ( N − 1 + ε ) mean absolute error for a single random lattice rule and an L q L^q L q error of the same order for the median estimator, with admissible q > 1 q>1 q > 1 . We also identified conditions for error bounds uniform in the state and Brownian path dimensions. The numerical experiments demonstrate the advantage of median lattice estimators over Monte Carlo and their stability under time grid refinement. Under the diffusion-column summability condition, the observed convergence also remains stable as the state and Brownian path dimensions increase.
The current bounds retain a dependence on the time horizon T T T , which limits their use in assessing long-time computations. Addressing this dependence by identifying conditions for error bounds uniform in T T T is one direction for future work. Another is to develop methods whose sampling errors decay faster than O ( N − 1 ) O(N^{-1}) O ( N − 1 ) . Together, these directions would extend QMC approximation of SDE expectations to longer time horizons and higher convergence orders.
Proof of the recursive state-derivative expansions
Proof of Lemma 4.2. Fix the input z z z . We first consider u = { j } u=\{j\} u = { j } . Applying (4.3) to (4.4) and then using X i , { j } h = Y i , { j } + ξ j ( t i ) X^h_{i,\{j\}}=Y_{i,\{j\}}+\xi_j(t_i) X i , { j } h = Y i , { j } + ξ j ( t i ) gives
Y i + 1 , { j } = Y i , { j } + h D x b ( t i , X t i h ) [ X i , { j } h ] = Y i , { j } + h D x b ( t i , X t i h ) [ Y i , { j } + ξ j ( t i ) ] = Ω i Y i , { j } + h D x b ( t i , X t i h ) [ ξ j ( t i ) ] , Y 0 , { j } = 0. (74) \begin{aligned}
Y_{i+1,\{j\}} &= Y_{i,\{j\}}+hD_xb(t_i,X^h_{t_i})[X^h_{i,\{j\}}]\\
&=Y_{i,\{j\}}+hD_xb(t_i,X^h_{t_i})[Y_{i,\{j\}}+\xi_j(t_i)]\\
&=\Omega_iY_{i,\{j\}}+hD_xb(t_i,X^h_{t_i})[\xi_j(t_i)],\qquad Y_{0,\{j\}}=0. \tag*{(74)}
\end{aligned} Y i + 1 , { j } = Y i , { j } + h D x b ( t i , X t i h ) [ X i , { j } h ] = Y i , { j } + h D x b ( t i , X t i h ) [ Y i , { j } + ξ j ( t i )] = Ω i Y i , { j } + h D x b ( t i , X t i h ) [ ξ j ( t i )] , Y 0 , { j } = 0. (74)
Since P i + 1 , i ′ = Ω i P i , i ′ P_{i+1,i'}=\Omega_iP_{i,i'} P i + 1 , i ′ = Ω i P i , i ′ for i ′ < i i'<i i ′ < i and P i + 1 , i = I d d x P_{i+1,i}=\mathrm{Id}_{d_x} P i + 1 , i = Id d x , induction on i i i gives
Y i , { j } = ∑ i ′ = 0 i − 1 P i , i ′ h D x b ( t i ′ , X t i ′ h ) [ ξ j ( t i ′ ) ] . (75) Y_{i,\{j\}}=\sum_{i'=0}^{i-1}P_{i,i'}hD_xb(t_{i'},X^h_{t_{i'}})[\xi_j(t_{i'})]. \tag*{(75)} Y i , { j } = i ′ = 0 ∑ i − 1 P i , i ′ h D x b ( t i ′ , X t i ′ h ) [ ξ j ( t i ′ )] . (75)
This proves (4.6).
Next let ∣ u ∣ ≥ 2 |u|\ge2 ∣ u ∣ ≥ 2 . Applying (4.3) to (4.4) gives
Y i + 1 , u = Y i , u + h ∑ ρ ∈ P ( u ) D x ∣ ρ ∣ b ( t i , X t i h ) [ X i , v h : v ∈ ρ ] = Y i , u + h D x b ( t i , X t i h ) [ X i , u h ] + h ∑ ρ ∈ P ( u ) ∣ ρ ∣ ≥ 2 D x ∣ ρ ∣ b ( t i , X t i h ) [ X i , v h : v ∈ ρ ] = Ω i Y i , u + h ∑ ρ ∈ P ( u ) ∣ ρ ∣ ≥ 2 D x ∣ ρ ∣ b ( t i , X t i h ) [ X i , v h : v ∈ ρ ] , Y 0 , u = 0. (76) \begin{aligned}
Y_{i+1,u}&=Y_{i,u}+h\sum_{\rho\in\mathcal{P}(u)}D_x^{|\rho|}b(t_i,X^h_{t_i})[X^h_{i,v}:v\in\rho]\\
&=Y_{i,u}+hD_xb(t_i,X^h_{t_i})[X^h_{i,u}]+h\sum_{\substack{\rho\in\mathcal{P}(u)\\|\rho|\ge2}}D_x^{|\rho|}b(t_i,X^h_{t_i})[X^h_{i,v}:v\in\rho]\\
&=\Omega_iY_{i,u}+h\sum_{\substack{\rho\in\mathcal{P}(u)\\|\rho|\ge2}}D_x^{|\rho|}b(t_i,X^h_{t_i})[X^h_{i,v}:v\in\rho],\qquad Y_{0,u}=0. \tag*{(76)}
\end{aligned} Y i + 1 , u = Y i , u + h ρ ∈ P ( u ) ∑ D x ∣ ρ ∣ b ( t i , X t i h ) [ X i , v h : v ∈ ρ ] = Y i , u + h D x b ( t i , X t i h ) [ X i , u h ] + h ρ ∈ P ( u ) ∣ ρ ∣ ≥ 2 ∑ D x ∣ ρ ∣ b ( t i , X t i h ) [ X i , v h : v ∈ ρ ] = Ω i Y i , u + h ρ ∈ P ( u ) ∣ ρ ∣ ≥ 2 ∑ D x ∣ ρ ∣ b ( t i , X t i h ) [ X i , v h : v ∈ ρ ] , Y 0 , u = 0. (76)
where the last equality uses X i , u h = Y i , u X^h_{i,u}=Y_{i,u} X i , u h = Y i , u . The same induction, again using P i + 1 , i ′ = Ω i P i , i ′ P_{i+1,i'}=\Omega_iP_{i,i'} P i + 1 , i ′ = Ω i P i , i ′ and P i + 1 , i = I d d x P_{i+1,i}=\mathrm{Id}_{d_x} P i + 1 , i = Id d x , yields
Y i , u = ∑ i ′ = 0 i − 1 P i , i ′ h ∑ ρ ∈ P ( u ) ∣ ρ ∣ ≥ 2 D x ∣ ρ ∣ b ( t i ′ , X t i ′ h ) [ X i ′ , v h : v ∈ ρ ] . (77) Y_{i,u}=\sum_{i'=0}^{i-1}P_{i,i'}h\sum_{\substack{\rho\in\mathcal{P}(u)\\|\rho|\ge2}}D_x^{|\rho|}b(t_{i'},X^h_{t_{i'}})[X^h_{i',v}:v\in\rho]. \tag*{(77)} Y i , u = i ′ = 0 ∑ i − 1 P i , i ′ h ρ ∈ P ( u ) ∣ ρ ∣ ≥ 2 ∑ D x ∣ ρ ∣ b ( t i ′ , X t i ′ h ) [ X i ′ , v h : v ∈ ρ ] . (77)
To rewrite (A.4), fix ρ ∈ P ( u ) \rho\in\mathcal{P}(u) ρ ∈ P ( u ) with ∣ ρ ∣ ≥ 2 |\rho| \ge2 ∣ ρ ∣ ≥ 2 . For S ⊆ sing ( ρ ) S \subseteq\operatorname{sing}(\rho) S ⊆ sing ( ρ ) , with sing ( ρ ) \operatorname{sing}(\rho) sing ( ρ ) defined in (5) , set
π S : = ρ ∖ { { j } : j ∈ S } . \pi_S := \rho\setminus\{\{j\}: j \in S\}. π S := ρ ∖ {{ j } : j ∈ S } .
By multilinearity,
D x ∣ ρ ∣ b ( t i ′ , X t i ′ h ) [ X i ′ , v h : v ∈ ρ ] = D x ∣ ρ ∣ b ( t i ′ , X t i ′ h , ( ( Y i ′ , { j } + ξ j ( t i ′ ) ) j ∈ sing ( ρ ) , ( Y i ′ , v ) v ∈ ρ , ∣ v ∣ ≥ 2 ) ) = ∑ S ⊆ sing ( ρ ) D x ∣ S ∣ + ∣ π S ∣ b ( t i ′ , X t i ′ h ) [ ( ξ j ( t i ′ ) ) j ∈ S , ( Y i ′ , v ) v ∈ π S ] . \begin{aligned}
D_x^{|\rho|}b(t_{i^\prime},X_{t_{i^\prime}}^h)[X_{i^\prime,v}^h:v\in\rho]
=
D_x^{|\rho|}b\left(t_{i^\prime},X_{t_{i^\prime}}^h,\left((Y_{i^\prime,\{j\}}+\xi_j(t_{i^\prime}))_{j\in\operatorname{sing}(\rho)},(Y_{i^\prime,v})_{v\in\rho,\ |v|\ge2}\right)\right) \\
&=
\sum_{S\subseteq\operatorname{sing}(\rho)}
D_x^{|S|+|\pi_S|}b(t_{i^\prime},X_{t_{i^\prime}}^h)
\left[(\xi_j(t_{i^\prime}))_{j\in S},(Y_{i^\prime,v})_{v\in\pi_S}\right].
\end{aligned} D x ∣ ρ ∣ b ( t i ′ , X t i ′ h ) [ X i ′ , v h : v ∈ ρ ] = D x ∣ ρ ∣ b ( t i ′ , X t i ′ h , ( ( Y i ′ , { j } + ξ j ( t i ′ ) ) j ∈ sing ( ρ ) , ( Y i ′ , v ) v ∈ ρ , ∣ v ∣ ≥ 2 ) ) = S ⊆ sing ( ρ ) ∑ D x ∣ S ∣ + ∣ π S ∣ b ( t i ′ , X t i ′ h ) [ ( ξ j ( t i ′ ) ) j ∈ S , ( Y i ′ , v ) v ∈ π S ] .
We note that π S ∈ P ( u ∖ S ) \pi_S\in\mathcal{P}(u\setminus S) π S ∈ P ( u ∖ S ) and ∣ S ∣ + ∣ π S ∣ = ∣ ρ ∣ ≥ 2 |S|+|\pi_S|=|\rho|\ge2 ∣ S ∣ + ∣ π S ∣ = ∣ ρ ∣ ≥ 2 . Conversely, every S ⊆ u S\subseteq u S ⊆ u and π ∈ P ( u ∖ S ) \pi\in\mathcal{P}(u\setminus S) π ∈ P ( u ∖ S ) satisfying ∣ S ∣ + ∣ π ∣ ≥ 2 |S|+|\pi|\ge2 ∣ S ∣ + ∣ π ∣ ≥ 2 uniquely determine ρ = { { j } : j ∈ S } ∪ π \rho=\{\{j\}:j\in S\}\cup\pi ρ = {{ j } : j ∈ S } ∪ π and the corresponding choices in the multilinear expansion. Reindexing the finite sum in (A.4) therefore gives (50) .
Finally, (8) and submultiplicativity give
∥ Ω i ∥ 2 ≤ 1 + h B 1 , ∥ P i , i ′ ∥ 2 ≤ ( 1 + h B 1 ) i − i ′ − 1 ≤ e B 1 T , \|\Omega_i\|_2\le1+hB_1,\qquad\|P_{i,i^\prime}\|_2\le(1+hB_1)^{i-i^\prime-1}\le e^{B_1T}, ∥ Ω i ∥ 2 ≤ 1 + h B 1 , ∥ P i , i ′ ∥ 2 ≤ ( 1 + h B 1 ) i − i ′ − 1 ≤ e B 1 T ,
including the empty product. This proves (51) .
A tree expansion for the derivative majorant
This appendix establishes the estimate for D m , u D_{m,u} D m , u stated in Proposition 4.3. We first derive an expansion of ∂ u F m \partial_uF_m ∂ u F m that separates the direct Brownian bridge inputs from the state derivatives. We then use labelled rooted trees to track the terms generated by repeatedly substituting the recursive expansions in Lemma 4.2. After estimating the value of each tree and counting the compatible tree structures, we sum over the admissible time assignments and complete the proof of Proposition 4.3.
Payoff-derivative expansion
The following lemma separates the endpoint inputs that enter the payoff derivative directly from the state derivatives that will be expanded recursively.
Lemma B.1. For nonempty u ⊆ [ s ] u\subseteq[s] u ⊆ [ s ] , the payoff derivative is
∂ u F m = ∑ E ⊆ u ∩ E w ∑ π ∈ P ( u ∖ E ) D x ∣ E ∣ + ∣ π ∣ g ( X t m h ) [ ( ξ j ( T ) ) j ∈ E , ( Y m , v ) v ∈ π ] . (78) \partial_uF_m=
\sum_{E\subseteq u\cap\mathcal{E}_w}
\sum_{\pi\in\mathcal{P}(u\setminus E)}
D_x^{|E|+|\pi|}g(X_{t_m}^h)
\left[(\xi_j(T))_{j\in E},(Y_{m,v})_{v\in\pi}\right]. \tag*{(78)} ∂ u F m = E ⊆ u ∩ E w ∑ π ∈ P ( u ∖ E ) ∑ D x ∣ E ∣ + ∣ π ∣ g ( X t m h ) [ ( ξ j ( T ) ) j ∈ E , ( Y m , v ) v ∈ π ] . (78) where E w \mathcal{E}_w E w is defined in (16) .
Proof. The partition chain rule [14 Theorem 1] gives
∂ u F m = ∑ ρ ∈ P ( u ) D x ∣ ρ ∣ g ( X t m h ) [ X m , v h : v ∈ ρ ] . \partial_uF_m=
\sum_{\rho\in\mathcal{P}(u)}
D_x^{|\rho|}g(X_{t_m}^h)[X_{m,v}^h:v\in\rho]. ∂ u F m = ρ ∈ P ( u ) ∑ D x ∣ ρ ∣ g ( X t m h ) [ X m , v h : v ∈ ρ ] .
As in the proof of Lemma 4.2, expand the singleton factors by multilinearity. For ρ ∈ P ( u ) \rho\in\mathcal{P}(u) ρ ∈ P ( u ) and E ⊆ sing ( ρ ) E\subseteq\operatorname{sing}(\rho) E ⊆ sing ( ρ ) , set
π E : = ρ ∖ { { j } : j ∈ E } . \pi_E:=\rho\setminus\{\{j\}:j\in E\}. π E := ρ ∖ {{ j } : j ∈ E } .
Then
∂ u F m = ∑ ρ ∈ P ( u ) ∑ E ⊆ sing ( ρ ) D x ∣ E ∣ + ∣ π E ∣ g ( X t m h ) [ ( ξ j ( T ) ) j ∈ E , ( Y m , v ) v ∈ π E ] . \partial_uF_m=
\sum_{\rho\in\mathcal{P}(u)}
\sum_{E\subseteq\operatorname{sing}(\rho)}
D_x^{|E|+|\pi_E|}g(X_{t_m}^h)
\left[(\xi_j(T))_{j\in E},(Y_{m,v})_{v\in\pi_E}\right]. ∂ u F m = ρ ∈ P ( u ) ∑ E ⊆ sing ( ρ ) ∑ D x ∣ E ∣ + ∣ π E ∣ g ( X t m h ) [ ( ξ j ( T ) ) j ∈ E , ( Y m , v ) v ∈ π E ] .
Any term with E ⊈ u ∩ E w E\not\subseteq u\cap\mathcal{E}_w E ⊆ u ∩ E w vanishes, since it contains some j ∈ E ∩ J m j\in E\cap\mathcal{J}_m j ∈ E ∩ J m and ξ j ( T ) = 0 \xi_j(T)=0 ξ j ( T ) = 0 . Reindexing the remaining terms by
ρ = { { j } : j ∈ E } ∪ π \rho=\{\{j\}:j\in E\}\cup\pi ρ = {{ j } : j ∈ E } ∪ π
gives (B.1).
Rooted-tree representation
We encode the repeated substitutions of Lemma 4.2 into (B.1) by finite rooted trees, using the standard terminology of Levin [13 Section 4.2] . The root represents one summand in (B.1), while each nonroot vertex y y y is associated with an occurrence of a state derivative Y i , v Y_{i,v} Y i , v . The edges record how the state derivatives in (B.1) are recursively expanded using Lemma 4.2 . We now make this representation precise.
Definition B.2. For ∅ ≠ u ⊆ [ s ] \varnothing\ne u \subseteq[s] ∅ = u ⊆ [ s ] , a labelled payoff tree T \mathcal{T} T has a payoff root y ∗ y_* y ∗ and drift vertices y ≠ y ∗ y \ne y_* y = y ∗ . The root carries a direct label set S ( y ∗ ) = E ⊆ u ∩ E w S(y_*) = E \subseteq u \cap\mathcal{E}_w S ( y ∗ ) = E ⊆ u ∩ E w , while each drift vertex carries a direct label set S ( y ) S(y) S ( y ) , possibly empty. These sets are pairwise disjoint and satisfy
u = ⋃ y ∈ T S ( y ) . u = \bigcup_{y \in\mathcal{T}} S(y). u = y ∈ T ⋃ S ( y ) .
The root-only tree is included; in this case E = u E = u E = u . For a nonroot vertex y y y , let pa ( y ) \operatorname{pa}(y) pa ( y ) denote its parent. For every vertex y y y , let ch ( y ) \operatorname{ch}(y) ch ( y ) denote its set of children, and define
c y : = ∣ ch ( y ) ∣ . (79) c_y := \lvert\operatorname{ch}(y) \rvert. \tag*{(79)} c y := ∣ ch ( y )∣ . (79)
At every drift vertex require
( ∣ S ( y ) ∣ , c y ) = ( 1 , 0 ) or ∣ S ( y ) ∣ + c y ≥ 2. (80) \bigl(\lvert S(y) \rvert,c_y\bigr) = (1,0) \quad\text{or} \quad\lvert S(y) \rvert+ c_y \ge2. \tag*{(80)} ( ∣ S ( y )∣ , c y ) = ( 1 , 0 ) or ∣ S ( y )∣ + c y ≥ 2. (80)
Thus S ( y ) ≠ ∅ S(y) \ne\varnothing S ( y ) = ∅ for every drift leaf y y y . The children of a vertex are unordered, so permuting them does not produce a new labelled tree. Let T ( u ) \mathcal{T}(u) T ( u ) denote the set of these trees, and let V ( T ) \mathcal{V}(\mathcal{T}) V ( T ) denote the vertex set of T \mathcal{T} T .
Definition B.3. Fix T ∈ T ( u ) \mathcal{T} \in\mathcal{T}(u) T ∈ T ( u ) . A time assignment is a family i = ( i y ) y ∈ V ( T ) i = (i_y)_{y \in\mathcal{V}(\mathcal{T})} i = ( i y ) y ∈ V ( T ) in
R m ( T ) = { ( i y ) ∈ { 0 , … , m } ∣ V ( T ) ∣ : i y ∗ = m , i y < i pa ( y ) for every y ∗ ≠ y ∈ V ( T ) } . \mathcal{R}_m(\mathcal{T}) = \left\{(i_y) \in\{0,\ldots,m\}^{\lvert\mathcal{V}(\mathcal{T})\rvert} : i_{y_*} = m,\quad i_y < i_{\operatorname{pa}(y)} \text{ for every } y_* \ne y \in\mathcal{V}(\mathcal{T})\right\}. R m ( T ) = { ( i y ) ∈ { 0 , … , m } ∣ V ( T )∣ : i y ∗ = m , i y < i pa ( y ) for every y ∗ = y ∈ V ( T ) } .
Definition B.4. Fix T ∈ T ( u ) \mathcal{T} \in\mathcal{T}(u) T ∈ T ( u ) and i ∈ R m ( T ) i \in\mathcal{R}_m(\mathcal{T}) i ∈ R m ( T ) . Evaluate its drift vertices from the leaves toward the root by setting
V y = P i pa ( y ) , i y h x ∣ S ( y ) ∣ + c y b ( t i y , X t i y h ) [ ( ξ j ( t i y ) ) j ∈ S ( y ) , ( V y ′ ) y ′ ∈ ch ( y ) ] . (81) V_y = P_{i_{\operatorname{pa}(y)},i_y}h_x^{\lvert S(y)\rvert+c_y}b(t_{i_y},X_{t_{i_y}}^h)\left[(\xi_j(t_{i_y}))_{j \in S(y)},(V_{y'})_{y' \in\operatorname{ch}(y)}\right]. \tag*{(81)} V y = P i pa ( y ) , i y h x ∣ S ( y )∣ + c y b ( t i y , X t i y h ) [ ( ξ j ( t i y ) ) j ∈ S ( y ) , ( V y ′ ) y ′ ∈ ch ( y ) ] . (81)
For a leaf y y y , ch ( y ) = ∅ \operatorname{ch}(y) = \varnothing ch ( y ) = ∅ , so c y = 0 c_y = 0 c y = 0 and the family ( V y ′ ) y ′ ∈ ch ( y ) (V_{y'})_{y' \in\operatorname{ch}(y)} ( V y ′ ) y ′ ∈ ch ( y ) is empty. The value of the payoff tree is
G ( T , i ) = D x ∣ E ∣ + c y ∗ g ( X t m h ) [ ( ξ j ( T ) ) j ∈ E , ( V y ′ ) y ′ ∈ ch ( y ∗ ) ] . (82) \mathcal{G}(\mathcal{T},i) = D_x^{\lvert E\rvert+c_{y_*}}g(X_{t_m}^h)\left[(\xi_j(T))_{j \in E},(V_{y'})_{y' \in\operatorname{ch}(y_*)}\right]. \tag*{(82)} G ( T , i ) = D x ∣ E ∣ + c y ∗ g ( X t m h ) [ ( ξ j ( T ) ) j ∈ E , ( V y ′ ) y ′ ∈ ch ( y ∗ ) ] . (82)
Since the derivatives of b b b and g g g are symmetric, G ( T , i ) \mathcal{G}(\mathcal{T},i) G ( T , i ) is independent of the ordering of the children. The following lemma identifies ∂ u F m \partial_u F_m ∂ u F m with the sum of these tree values.
Lemma B.5. For ∅ ≠ u ⊆ [ s ] \varnothing\ne u \subseteq[s] ∅ = u ⊆ [ s ] , we have
∂ u F m = ∑ T ∈ T ( u ) ∑ i ∈ R m ( T ) G ( T , i ) . (83) \partial_u F_m = \sum_{\mathcal{T} \in\mathcal{T}(u)}\sum_{i \in\mathcal{R}_m(\mathcal{T})}\mathcal{G}(\mathcal{T},i). \tag*{(83)} ∂ u F m = T ∈ T ( u ) ∑ i ∈ R m ( T ) ∑ G ( T , i ) . (83)
Proof. Construction of the labelled tree and its time assignment. Repeatedly substitute Lemma 4.2 whenever a state derivative Y i , v Y_{i,v} Y i , v with i ≥ 1 i \ge1 i ≥ 1 appears in (B.1), and distribute the resulting finite sums. Each newly generated state derivative has a strictly smaller time index. Hence, after at most m m m generations, every branch contains no state derivative Y i , v Y_{i,v} Y i , v with i ≥ 1 i \ge1 i ≥ 1 . We remove every term containing a factor Y 0 , v Y_{0,v} Y 0 , v , since Y 0 , v = 0 Y_{0,v} = 0 Y 0 , v = 0 . The remaining choices are complete in the sense that no state derivative remains, so all terminal vector arguments are direct inputs ξ j ( t ) \xi_j(t) ξ j ( t ) .
Let C m , u \mathcal{C}_{m,u} C m , u denote the finite set of these complete expansion choices, and let val ( χ ) \operatorname{val}(\chi) val ( χ ) be the fully expanded scalar term corresponding to χ ∈ C m , u \chi\in\mathcal{C}_{m,u} χ ∈ C m , u . Then
∂ u F m = ∑ χ ∈ C m , u val ( χ ) . (84) \partial_u F_m=\sum_{\chi\in\mathcal{C}_{m,u}}\operatorname{val}(\chi). \tag*{(84)} ∂ u F m = χ ∈ C m , u ∑ val ( χ ) . (84)
Fix χ ∈ C m , u \chi\in\mathcal{C}_{m,u} χ ∈ C m , u . We construct from χ \chi χ a labelled payoff tree T \mathcal{T} T and a time assignment i \boldsymbol{i} i . First consider the summand of (B.1) selected by χ \chi χ . It is indexed by
E ⊆ u ∩ E w , π ∈ P ( u ∖ E ) . E\subseteq u\cap E_w,\qquad\pi\in\mathcal{P}(u\setminus E). E ⊆ u ∩ E w , π ∈ P ( u ∖ E ) .
Create the payoff root y ∗ y_* y ∗ , set S ( y ∗ ) = E S(y_*)=E S ( y ∗ ) = E and i y ∗ = m i_{y_*}=m i y ∗ = m . For each v ∈ π v\in\pi v ∈ π , create a distinct child y y y of y ∗ y_* y ∗ and set Y ( y ) : = Y m , v \mathrm{Y}(y):=Y_{m,v} Y ( y ) := Y m , v . So ∣ ch ( y ∗ ) ∣ = ∣ π ∣ |\operatorname{ch}(y_*)|=|\pi| ∣ ch ( y ∗ ) ∣ = ∣ π ∣ . We extend the notation Y ( y ) \mathrm{Y}(y) Y ( y ) recursively below. The summand selected by χ \chi χ at the payoff root can then be written as
D x ∣ S ( y ∗ ) ∣ + c y ∗ g ( X t m h [ ( ξ j ( T ) ) j ∈ S ( y ∗ ) , ( Y ( y ) ) y ∈ ch ( y ∗ ) ] ) . (85) D_x^{|S(y_*)|+c_{y_*}}g\left(X_{t_m}^h\left[(\xi_j(\mathcal{T}))_{j\in S(y_*)},(\mathrm{Y}(y))_{y\in\operatorname{ch}(y_*)}\right]\right). \tag*{(85)} D x ∣ S ( y ∗ ) ∣ + c y ∗ g ( X t m h [ ( ξ j ( T ) ) j ∈ S ( y ∗ ) , ( Y ( y ) ) y ∈ ch ( y ∗ ) ] ) . (85)
If π = ∅ \pi=\varnothing π = ∅ , no drift vertex is introduced and the tree consists only of the payoff root.
Suppose that Y ( y ) = Y i , v \mathrm{Y}(y)=Y_{i,v} Y ( y ) = Y i , v with i ≥ 1 i\geq1 i ≥ 1 for a drift vertex y y y . Then i pa ( y ) = i i_{\operatorname{pa}(y)}=i i pa ( y ) = i . We distinguish two cases. If v = { j } v=\{j\} v = { j } , the expansion choice χ \chi χ selects a summand of (49) , indexed by 0 ≤ i ′ < i 0\leq i'<i 0 ≤ i ′ < i , namely
P i , i ′ h D x b ( t i ′ , X t i ′ h ) [ ξ j ( t i ′ ) ] . P_{i,i'}hD_xb(t_{i'},X_{t_{i'}}^h)[\xi_j(t_{i'})]. P i , i ′ h D x b ( t i ′ , X t i ′ h ) [ ξ j ( t i ′ )] .
We set i y = i ′ i_y=i' i y = i ′ , S ( y ) = { j } S(y)=\{j\} S ( y ) = { j } . This summand requires no further expansion, so no child is attached to y y y . Hence c y = 0 c_y=0 c y = 0 , ( ∣ S ( y ) ∣ , c y ) = ( 1 , 0 ) (|S(y)|,c_y)=(1,0) ( ∣ S ( y ) ∣ , c y ) = ( 1 , 0 ) , and y y y is a leaf. If ∣ v ∣ ≥ 2 |v|\geq2 ∣ v ∣ ≥ 2 , the expansion choice χ \chi χ selects a summand of (50) , indexed by
0 ≤ i ′ < i , S ⊆ v , π ∈ P ( v ∖ S ) , ∣ S ∣ + ∣ π ∣ ≥ 2. 0\leq i'<i,\qquad S\subseteq v,\qquad\pi\in\mathcal{P}(v\setminus S),\qquad|S|+|\pi|\geq2. 0 ≤ i ′ < i , S ⊆ v , π ∈ P ( v ∖ S ) , ∣ S ∣ + ∣ π ∣ ≥ 2.
This summand is
P i , i ′ h D x ∣ S ∣ + ∣ π ∣ b ( t i ′ , X t i ′ h [ ( ξ j ( t i ′ ) ) j ∈ S , ( Y i , v ′ ) v ′ ∈ π ] ) . (86) P_{i,i'}hD_x^{|S|+|\pi|}b\left(t_{i'},X_{t_{i'}}^h\left[(\xi_j(t_{i'}))_{j\in S},(Y_{i,v'})_{v'\in\pi}\right]\right). \tag*{(86)} P i , i ′ h D x ∣ S ∣ + ∣ π ∣ b ( t i ′ , X t i ′ h [ ( ξ j ( t i ′ ) ) j ∈ S , ( Y i , v ′ ) v ′ ∈ π ] ) . (86)
Set i y = i ′ i_y=i' i y = i ′ and S ( y ) = S S(y)=S S ( y ) = S . For each v ′ ∈ π v'\in\pi v ′ ∈ π , create a distinct child w w w of y y y and set Y ( w ) : = Y i ′ , v ′ \mathrm{Y}(w):=Y_{i',v'} Y ( w ) := Y i ′ , v ′ . Thus c y = ∣ π ∣ c_y=|\pi| c y = ∣ π ∣ and ∣ S ( y ) ∣ + c y ≥ 2 |S(y)|+c_y\geq2 ∣ S ( y ) ∣ + c y ≥ 2 , while y y y is a leaf exactly when π = ∅ \pi=\varnothing π = ∅ . Moreover, for a retained term, i y = 0 i_y=0 i y = 0 forces π = ∅ \pi=\varnothing π = ∅ , since every term containing a factor Y 0 , v ′ Y_{0,v'} Y 0 , v ′ has been removed. In both cases, i y < i = i pa ( y ) i_y<i=i_{\operatorname{pa}(y)} i y < i = i pa ( y ) , and the local summand selected by χ \chi χ at y y y can be written uniformly as
P i pa ( y ) , i y h D x ∣ S ( y ) ∣ + c y b ( t i y , X t i y h [ ( ξ j ( t i y ) ) j ∈ S ( y ) , ( Y ( w ) ) w ∈ ch ( y ) ] ) . (87) P_{i_{\operatorname{pa}(y)},i_y}hD_x^{|S(y)|+c_y}b\left(t_{i_y},X_{t_{i_y}}^h\left[(\xi_j(t_{i_y}))_{j\in S(y)},(\mathrm{Y}(w))_{w\in\operatorname{ch}(y)}\right]\right). \tag*{(87)} P i pa ( y ) , i y h D x ∣ S ( y ) ∣ + c y b ( t i y , X t i y h [ ( ξ j ( t i y ) ) j ∈ S ( y ) , ( Y ( w ) ) w ∈ ch ( y ) ] ) . (87)
Applying the same rule recursively to every new child completes the construction of T \mathcal{T} T and i \boldsymbol{i} i from χ \chi χ .
Admissibility and preservation of values. We first verify that T ∈ T ( u ) \mathcal{T}\in\mathcal{T}(u) T ∈ T ( u ) , i ∈ R m ( T ) \boldsymbol{i}\in\mathcal{R}_m(\mathcal{T}) i ∈ R m ( T ) . The two alternatives in the construction above give (B.3). If Y ( y ) = Y i , v \mathrm{Y}(y)=Y_{i,v} Y ( y ) = Y i , v , let T y \mathcal{T}_y T y denote the subtree of T \mathcal{T} T rooted at y y y . Induction over T y \mathcal{T}_y T y gives
v = ⋃ ˙ w ∈ V ( T y ) S ( w ) . (88) v=\mathop{\dot{\bigcup}}_{w\in V(\mathcal{T}_y)}S(w). \tag*{(88)} v = ⋃ ˙ w ∈ V ( T y ) S ( w ) . (88)
Applying this identity to the children of the payoff root and recalling their association with the state-derivative factors in the selected summand of (B.1), we obtain
u = ⋃ ˙ w ∈ V ( T ) S ( w ) . u=\mathop{\dot{\bigcup}}_{w\in V(\mathcal{T})}S(w). u = ⋃ ˙ w ∈ V ( T ) S ( w ) .
Together with i y ∗ = m i_{y_*}=m i y ∗ = m and the strict time inequalities, this proves that the construction yields T ∈ T ( u ) \mathcal{T} \in\mathcal{T}(u) T ∈ T ( u ) and i ∈ R m ( T ) i \in\mathcal{R}_m(\mathcal{T}) i ∈ R m ( T ) .
It remains to prove val ( χ ) = G ( T , i ) \operatorname{val}(\chi)=\mathcal{G}(\mathcal{T},i) val ( χ ) = G ( T , i ) . For every drift vertex y y y , we claim that recursively applying Lemma 4.2 to the state-derivative factors in (B.10), with summands selected according to χ \chi χ , yields V y V_y V y . We prove this by induction from the leaves toward the root.
For a leaf y y y , ch ( y ) = ∅ \operatorname{ch}(y)=\varnothing ch ( y ) = ∅ , so the claim follows directly by comparing (B.10) with (B.4). For a nonleaf vertex y y y , each state-derivative factor Y ( w ) Y(w) Y ( w ) in (B.10) is associated with a child w w w . By the construction and the induction hypothesis, the term selected by χ \chi χ in the expansion of Y ( w ) Y(w) Y ( w ) equals V w V_w V w . By multilinearity, the selected term at y y y is therefore obtained by replacing each Y ( w ) Y(w) Y ( w ) in (B.10) with V w V_w V w , which gives (B.4).
Applying the same argument to (B.8) and comparing with (B.5) gives
val ( χ ) = G ( T , i ) . (89) \operatorname{val}(\chi)=\mathcal{G}(\mathcal{T},i). \tag*{(89)} val ( χ ) = G ( T , i ) . (89)
This identity holds directly in the root-only case.
Inverse construction. Conversely, fix T ∈ T ( u ) \mathcal{T} \in\mathcal{T}(u) T ∈ T ( u ) and i ∈ R m ( T ) i \in\mathcal{R}_m(\mathcal{T}) i ∈ R m ( T ) . For every drift vertex y y y , recall that T y \mathcal{T}_y T y denotes the subtree of T \mathcal{T} T rooted at y y y , and define its coordinate set by
v ( y ) : = ⋃ w ∈ V ( T y ) S ( w ) . (90) v(y):=\bigcup_{w\in V(\mathcal{T}_y)} S(w). \tag*{(90)} v ( y ) := w ∈ V ( T y ) ⋃ S ( w ) . (90)
The child coordinate sets are nonempty and pairwise disjoint by (B.3) and the disjointness of the direct label sets. For every vertex y y y , set
π y : = { v ( w ) : w ∈ ch ( y ) } . \pi_y:=\{v(w):w\in\operatorname{ch}(y)\}. π y := { v ( w ) : w ∈ ch ( y )} .
At the payoff root, E = S ( y ∗ ) E=S(y_*) E = S ( y ∗ ) and π = π y ∗ \pi=\pi_{y_*} π = π y ∗ determine a unique summand of (B.1). At a drift vertex y y y , the associated derivative is Y i pa ( y ) , v ( y ) Y_{i_{\operatorname{pa}(y)},v(y)} Y i pa ( y ) , v ( y ) and π y ∈ P ( v ( y ) ∖ S ( y ) ) \pi_y \in\mathcal{P}(v(y)\setminus S(y)) π y ∈ P ( v ( y ) ∖ S ( y )) . If ( ∣ S ( y ) ∣ , c y ) = ( 1 , 0 ) (|S(y)|,c_y)=(1,0) ( ∣ S ( y ) ∣ , c y ) = ( 1 , 0 ) , then v ( y ) = S ( y ) v(y)=S(y) v ( y ) = S ( y ) is a singleton, which together with i y i_y i y determines a unique summand of (49) . Otherwise ∣ v ( y ) ∣ ≥ ∣ S ( y ) ∣ + c y ≥ 2 |v(y)|\ge|S(y)|+c_y\ge2 ∣ v ( y ) ∣ ≥ ∣ S ( y ) ∣ + c y ≥ 2 , so S ( y ) S(y) S ( y ) , π y \pi_y π y , and i y < i pa ( y ) i_y<i_{\operatorname{pa}(y)} i y < i pa ( y ) select a unique summand of (50) .
The strict time inequalities force every vertex at time zero to be a leaf, so no recovered summand contains a factor Y 0 , v Y_{0,v} Y 0 , v . These local choices therefore form a complete choice χ ∈ C m , u \chi\in\mathcal{C}_{m,u} χ ∈ C m , u .
Verification of the bijection. First, let ( T , i ) (\mathcal{T},i) ( T , i ) be constructed from χ \chi χ . Comparing (B.11) with (B.13) gives v ( y ) = v v(y)=v v ( y ) = v whenever Y ( y ) = Y i , v Y(y)=Y_{i,v} Y ( y ) = Y i , v . Since i = i pa ( y ) i=i_{\operatorname{pa}(y)} i = i pa ( y ) , we have Y ( y ) = Y i pa ( y ) , v ( y ) Y(y)=Y_{i_{\operatorname{pa}(y)},v(y)} Y ( y ) = Y i pa ( y ) , v ( y ) . Thus the inverse construction recovers the same associated derivatives. Applying the root and drift-vertex construction rules recursively recovers the same selected summands, hence the original χ \chi χ .
Conversely, fix ( T , i ) (\mathcal{T},i) ( T , i ) and let χ \chi χ be obtained by the inverse construction. The same vertex-by-vertex comparison shows that the forward construction applied to this χ \chi χ returns the original pair ( T , i ) (\mathcal{T},i) ( T , i ) . Thus the two constructions are mutually inverse and give a bijection.
Combining this bijection with (B.12) and (B.7) proves (B.6).
Tree counts and coefficient bounds
We establish three technical lemmas controlling the size, weighted count, and coefficients of trees with a fixed direct partition.
For a labelled payoff tree T ∈ T ( u ) \mathcal{T}\in\mathcal{T}(u) T ∈ T ( u ) , define its global direct partition by
Π ( T ) : = { S ( y ) : y ∈ V ( T ) ∖ { y ∗ } , S ( y ) ≠ ∅ } . \Pi(\mathcal{T}):=\{S(y):y\in V(\mathcal{T})\setminus\{y_*\},\ S(y)\ne\varnothing\}. Π ( T ) := { S ( y ) : y ∈ V ( T ) ∖ { y ∗ } , S ( y ) = ∅ } .
By Definition B.2, Π ( T ) ∈ P ( u ∖ S ( y ∗ ) ) \Pi(\mathcal{T}) \in\mathcal{P}(u \setminus S(y_*)) Π ( T ) ∈ P ( u ∖ S ( y ∗ )) . Throughout this subsection, fix E ⊆ u ∩ E w E \subseteq u \cap E_w E ⊆ u ∩ E w such that u ˉ : = u ∖ E ≠ ∅ \bar{u} := u \setminus E \ne\varnothing u ˉ := u ∖ E = ∅ , and fix π ∈ P ( u ˉ ) \pi\in\mathcal{P}(\bar{u}) π ∈ P ( u ˉ ) . Define
Γ ( E , π ) : = { T ∈ T ( u ) : S ( y ∗ ) = E , Π ( T ) = π } . \Gamma(E,\pi) := \{\mathcal{T} \in\mathcal{T}(u) : S(y_*) = E,\ \Pi(\mathcal{T}) = \pi\}. Γ ( E , π ) := { T ∈ T ( u ) : S ( y ∗ ) = E , Π ( T ) = π } .
Write
n π : = ∣ π ∣ = ∣ Π ( T ) ∣ for T ∈ Γ ( E , π ) . n_\pi:= |\pi| = |\Pi(\mathcal{T})| \quad\text{for } \mathcal{T} \in\Gamma(E,\pi). n π := ∣ π ∣ = ∣Π ( T ) ∣ for T ∈ Γ ( E , π ) .
Lemma B.6. Let T ∈ Γ ( E , π ) \mathcal{T} \in\Gamma(E,\pi) T ∈ Γ ( E , π ) and define
n ∅ : = ∣ { y ∈ V ( T ) ∖ { y ∗ } : S ( y ) = ∅ } ∣ . (91) n_{\varnothing} := |\{y \in\mathcal{V}(\mathcal{T}) \setminus\{y_*\} : S(y) = \varnothing\}|. \tag*{(91)} n ∅ := ∣ { y ∈ V ( T ) ∖ { y ∗ } : S ( y ) = ∅ } ∣. (91) Then
n ∅ ≤ n π − 1 , ∣ V ( T ) ∣ = n π + n ∅ + 1 ≤ 2 n π . n_{\varnothing} \le n_\pi- 1,\qquad|\mathcal{V}(\mathcal{T})| = n_\pi+ n_{\varnothing} + 1 \le2n_\pi. n ∅ ≤ n π − 1 , ∣ V ( T ) ∣ = n π + n ∅ + 1 ≤ 2 n π . Moreover,
c ( T ) : = ∏ y ∈ V ( T ) c y ! ≤ n π ! . (92) c(\mathcal{T}) := \prod_{y \in\mathcal{V}(\mathcal{T})} c_y! \le n_\pi!. \tag*{(92)} c ( T ) := y ∈ V ( T ) ∏ c y ! ≤ n π ! . (92) Proof. There are n π + n ∅ + 1 n_\pi+ n_{\varnothing} + 1 n π + n ∅ + 1 vertices and n π + n ∅ n_\pi+ n_{\varnothing} n π + n ∅ edges. Each edge joins a child to its parent, so ∑ y ∈ V ( T ) c y = n π + n ∅ \sum_{y \in\mathcal{V}(\mathcal{T})} c_y = n_\pi+ n_{\varnothing} ∑ y ∈ V ( T ) c y = n π + n ∅ . By (B.3), if y ≠ y ∗ y \ne y_* y = y ∗ and S ( y ) = ∅ S(y) = \varnothing S ( y ) = ∅ , then c y ≥ 2 c_y \ge2 c y ≥ 2 . Since u ˉ ≠ ∅ \bar{u} \ne\varnothing u ˉ = ∅ , c y ∗ ≥ 1 c_{y_*} \ge1 c y ∗ ≥ 1 . Consequently
n π + n ∅ = ∑ y ∈ V ( T ) c y ≥ 2 n ∅ + 1 , n ∅ ≤ n π − 1. n_\pi+ n_{\varnothing} = \sum_{y \in\mathcal{V}(\mathcal{T})} c_y \ge2n_{\varnothing} + 1,\qquad n_{\varnothing} \le n_\pi- 1. n π + n ∅ = y ∈ V ( T ) ∑ c y ≥ 2 n ∅ + 1 , n ∅ ≤ n π − 1. We then prove an auxiliary bound valid for every finite rooted tree S \mathcal{S} S , without imposing the conditions defining T \mathcal{T} T . Let L ( S ) L(\mathcal{S}) L ( S ) denote its number of leaves. We claim that ∏ y ∈ V ( S ) c y ! ≤ L ( S ) ! \prod_{y \in\mathcal{V}(\mathcal{S})} c_y! \le L(\mathcal{S})! ∏ y ∈ V ( S ) c y ! ≤ L ( S )! . We argue by induction on the number of vertices. For the one-vertex tree, the root has no children and is itself a leaf, so both sides equal 1 1 1 . For the induction step, let the root have c ≥ 1 c \ge1 c ≥ 1 child subtrees S 1 , … , S c \mathcal{S}_1,\ldots,\mathcal{S}_c S 1 , … , S c , with respective leaf counts L 1 , … , L c ≥ 1 L_1,\ldots,L_c \ge1 L 1 , … , L c ≥ 1 . Applying the induction hypothesis to these subtrees gives
∏ y ∈ V ( S ) c y ! = c ! ∏ a = 1 c ∏ y ′ ∈ V ( S a ) c y ′ ! ≤ c ! ∏ a = 1 c L a ! ≤ ( ∑ a = 1 c L a ) ! = L ( S ) ! . \prod_{y \in\mathcal{V}(\mathcal{S})} c_y! = c! \prod_{a=1}^{c} \prod_{y' \in\mathcal{V}(\mathcal{S}_a)} c_{y'}! \le c! \prod_{a=1}^{c} L_a! \le\left(\sum_{a=1}^{c} L_a\right)! = L(\mathcal{S})!. y ∈ V ( S ) ∏ c y ! = c ! a = 1 ∏ c y ′ ∈ V ( S a ) ∏ c y ′ ! ≤ c ! a = 1 ∏ c L a ! ≤ ( a = 1 ∑ c L a ) ! = L ( S )! . The second inequality holds because, for L a ≥ 1 L_a \ge1 L a ≥ 1 , the multinomial coefficient ( ∑ a L a ) ! / ∏ a L a ! (\sum_a L_a)!/\prod_a L_a! ( ∑ a L a )! / ∏ a L a ! is at least its value c ! c! c ! at L 1 = ⋯ = L c = 1 L_1 = \cdots= L_c = 1 L 1 = ⋯ = L c = 1 : increasing L j L_j L j multiplies it by ( ∑ a L a + 1 ) / ( L j + 1 ) ≥ 1 (\sum_a L_a + 1)/(L_j + 1) \ge1 ( ∑ a L a + 1 ) / ( L j + 1 ) ≥ 1 . Finally, apply this auxiliary bound to T \mathcal{T} T . Since u ˉ ≠ ∅ \bar{u} \ne\varnothing u ˉ = ∅ , the payoff root is not a leaf. By (B.3), every drift leaf has a nonempty label set. Thus all leaves are drift vertices with nonempty label sets, and their number L ∗ L_* L ∗ is at most n π n_\pi n π . Hence
∏ y ∈ V ( T ) c y ! ≤ L ∗ ! ≤ n π ! , \prod_{y \in\mathcal{V}(\mathcal{T})} c_y! \le L_* ! \le n_\pi!, y ∈ V ( T ) ∏ c y ! ≤ L ∗ ! ≤ n π ! , which proves (B.15).
Lemma B.7. With c ( T ) c(\mathcal{T}) c ( T ) defined in (B.15), we have
∑ T ∈ Γ ( E , π ) c ( T ) ≤ 64 n π n π ! . (93) \sum_{\mathcal{T} \in\Gamma(E,\pi)} c(\mathcal{T}) \le64^{n_\pi} n_\pi!. \tag*{(93)} T ∈ Γ ( E , π ) ∑ c ( T ) ≤ 6 4 n π n π ! . (93) Proof. Temporarily order the children at each vertex. Since sibling subtrees carry pairwise disjoint nonempty coordinate sets, each T \mathcal{T} T admits exactly c ( T ) c(\mathcal{T}) c ( T ) such orderings.
By Lemma B.6, there are at most 2 n π 2n_\pi 2 n π vertices. By the classical Catalan enumeration of plane rooted trees [5 Section I.5] , the number of ordered rooted shapes with n n n vertices is
Cat n − 1 = 1 n ( 2 n − 2 n − 1 ) ≤ 4 n − 1 . \operatorname{Cat}_{n-1}=\frac{1}{n}\binom{2n-2}{n-1}\leq4^{n-1}. Cat n − 1 = n 1 ( n − 1 2 n − 2 ) ≤ 4 n − 1 .
For each shape, the root carries E E E ; choose the n π n_\pi n π other vertices carrying nonempty direct sets in ( n − 1 n π ) \binom{n-1}{n_\pi} ( n π n − 1 ) ways and assign the distinct blocks of π \pi π in n π ! n_\pi! n π ! ways. The subtree coordinate sets determine all local partitions, so no further choices are needed. Including inadmissible choices only enlarges the bound. Thus
∑ T ∈ Γ ( E , π ) c ( T ) ≤ n π ! ∑ n = n π + 1 2 n π 4 n − 1 ( n − 1 n π ) ≤ n π ! ∑ n = 1 2 n π 8 n − 1 = n π ! 8 2 n π − 1 7 ≤ 64 n π n π ! . \sum_{\mathcal{T}\in\Gamma(E,\pi)}c(\mathcal{T})\leq n_\pi!\sum_{n=n_\pi+1}^{2n_\pi}4^{n-1}\binom{n-1}{n_\pi}\leq n_\pi!\sum_{n=1}^{2n_\pi}8^{n-1}=n_\pi!\frac{8^{2n_\pi}-1}{7}\leq64^{n_\pi}n_\pi!. T ∈ Γ ( E , π ) ∑ c ( T ) ≤ n π ! n = n π + 1 ∑ 2 n π 4 n − 1 ( n π n − 1 ) ≤ n π ! n = 1 ∑ 2 n π 8 n − 1 = n π ! 7 8 2 n π − 1 ≤ 6 4 n π n π ! .
Lemma B.8. For T ∈ Γ ( E , π ) \mathcal{T}\in\Gamma(E,\pi) T ∈ Γ ( E , π ) and i ∈ R m ( T ) i\in\mathcal{R}_m(\mathcal{T}) i ∈ R m ( T ) , define
i T ( j ) : = i y for the unique y ∈ V ( T ) with j ∈ S ( y ) , j ∈ u ˉ . i_{\mathcal{T}}(j):=i_y\quad\text{for the unique }y\in\mathcal{V}(\mathcal{T})\text{ with }j\in S(y),\qquad j\in\bar{u}. i T ( j ) := i y for the unique y ∈ V ( T ) with j ∈ S ( y ) , j ∈ u ˉ . Recall from Assumption 2.1 that
B n = B 0 B 1 n ( n ! ) τ , G n = G 0 G 1 n ( n ! ) τ , n ≥ 1. B_n=B_0B_1^n(n!)^\tau,\qquad G_n=G_0G_1^n(n!)^\tau,\qquad n\geq1. B n = B 0 B 1 n ( n ! ) τ , G n = G 0 G 1 n ( n ! ) τ , n ≥ 1. Define
K T : = G ∣ E ∣ + c y ∗ ∏ j ∈ E ∣ ξ j ( T ) ∣ 2 ∏ y ∈ V ( T ) ∖ { y ∗ } e B 1 T T B ∣ S ( y ) ∣ + c y . K_{\mathcal{T}}:=G_{|E|+c_{y_*}}\prod_{j\in E}|\xi_j(\mathcal{T})|_2\prod_{y\in\mathcal{V}(\mathcal{T})\setminus\{y_*\}}e^{B_1T_{\mathcal{T}}B_{|S(y)|+c_y}}. K T := G ∣ E ∣ + c y ∗ j ∈ E ∏ ∣ ξ j ( T ) ∣ 2 y ∈ V ( T ) ∖ { y ∗ } ∏ e B 1 T T B ∣ S ( y ) ∣ + c y . Then we have,
e − β g ∣ X t m h ∣ 2 ∣ G ( T , i ) ∣ ≤ K T h ∣ V ( T ) ∣ − 1 ∏ j ∈ u ˉ ∣ ξ j ( t i T ( j ) ) ∣ 2 (94) e^{-\beta_g|X^h_{t_m}|_2|\mathcal{G}(\mathcal{T},i)|\leq K_{\mathcal{T}}h^{|\mathcal{V}(\mathcal{T})|-1}\prod_{j\in\bar{u}}|\xi_j(t_{i_{\mathcal{T}}(j)})|_2} \tag*{(94)} e − β g ∣ X t m h ∣ 2 ∣ G ( T , i ) ∣ ≤ K T h ∣ V ( T ) ∣ − 1 ∏ j ∈ u ˉ ∣ ξ j ( t i T ( j ) ) ∣ 2 (94) Moreover, there exists C c n t ≥ 1 C_{\mathrm{cnt}}\geq1 C cnt ≥ 1 , depending only on T T T , B 0 B_0 B 0 , B 1 B_1 B 1 , G 0 G_0 G 0 , G 1 G_1 G 1 , τ \tau τ , such that
∑ T ∈ Γ ( E , π ) K T ≤ C c n t ∣ u ∣ + n π ( ∣ E ∣ ! ) τ ∏ j ∈ E ( T σ j ) ( n π ! ) τ ∏ S ∈ π ( ∣ S ∣ ! ) τ . (95) \sum_{\mathcal{T}\in\Gamma(E,\pi)}K_{\mathcal{T}}\leq C_{\mathrm{cnt}}^{|u|+n_\pi}(|E|!)^\tau\prod_{j\in E}(\sqrt{T}\,\sigma_j)(n_\pi!)^\tau\prod_{S\in\pi}(|S|!)^\tau. \tag*{(95)} T ∈ Γ ( E , π ) ∑ K T ≤ C cnt ∣ u ∣ + n π ( ∣ E ∣ ! ) τ j ∈ E ∏ ( T σ j ) ( n π ! ) τ S ∈ π ∏ ( ∣ S ∣ ! ) τ . (95)
Proof. By (B.4), (2.4), and (4.8), every drift vertex satisfies
∣ V y ∣ 2 ≤ h e B 1 T T B ∣ S ( y ) ∣ + c y ∏ j ∈ S ( y ) ∣ ξ j ( t i y ) ∣ 2 ∏ w ∈ ch ( y ) ∣ V w ∣ 2 . |V_y|_2\leq h e^{B_1T_{\mathcal{T}}}B_{|S(y)|+c_y}\prod_{j\in S(y)}|\xi_j(t_{i_y})|_2\prod_{w\in\operatorname{ch}(y)}|V_w|_2. ∣ V y ∣ 2 ≤ h e B 1 T T B ∣ S ( y ) ∣ + c y j ∈ S ( y ) ∏ ∣ ξ j ( t i y ) ∣ 2 w ∈ ch ( y ) ∏ ∣ V w ∣ 2 .
At the payoff root, (B.5) and (2.5) give
e − β g ∣ X t m h ∣ 2 ∣ G ( T , i ) ∣ ≤ G ∣ E ∣ + c y ∗ ∏ j ∈ E ∣ ξ j ( T ) ∣ 2 ∏ w ∈ ch ( y ∗ ) ∣ V w ∣ 2 . e^{-\beta_g|X^h_{t_m}|_2|\mathcal{G}(\mathcal{T},i)|\leq G_{|E|+c_{y_*}}\prod_{j\in E}|\xi_j(\mathcal{T})|_2\prod_{w\in\operatorname{ch}(y_*)}|V_w|_2.} e − β g ∣ X t m h ∣ 2 ∣ G ( T , i ) ∣ ≤ G ∣ E ∣ + c y ∗ ∏ j ∈ E ∣ ξ j ( T ) ∣ 2 ∏ w ∈ ch ( y ∗ ) ∣ V w ∣ 2 .
Recursively substituting the drift bounds into the root bound gives
\begin{aligned}
e^{-\beta_g|X^h_{t_m}|_2|\mathcal{G}(\mathcal{T},i)|
&\leq G_{|E|+c_{y_*}}\prod_{j\in E}|\xi_j(\mathcal{T})|_2
\prod_{y\in\mathcal{V}(\mathcal{T})\setminus\{y_*\}}
\left(he^{B_1T_{\mathcal{T}}}B_{|S(y)|+c_y}\prod_{j\in S(y)}|\xi_j(t_{i_y})|_2\right)\\
&=K_{\mathcal{T}}h^{|\mathcal{V}(\mathcal{T})|-1}
\prod_{y\in\mathcal{V}(\mathcal{T})\setminus\{y_*\}}\prod_{j\in S(y)}|\xi_j(t_{i_y})|_2\\
&=K_{\mathcal{T}}h^{|\mathcal{V}(\mathcal{T})|-1}
\prod_{j\in\bar{u}}|\xi_j(t_{i_{\mathcal{T}}(j)})|_2.
\end{aligned}}
This proves (B.17).
For the coefficient sum, put n y = ∣ S ( y ) ∣ n_y = |S(y)| n y = ∣ S ( y ) ∣ and let n ∅ n_{\varnothing} n ∅ count drift vertices with empty direct sets. Then
n y ∗ = ∣ E ∣ , ∑ y ∈ V ( T ) n y = ∣ u ∣ , ∑ y ∈ V ( T ) c y = ∣ V ( T ) ∣ − 1 = n π + n ∅ . n_{y_*} = |E|,\qquad\sum_{y\in V(\mathcal{T})} n_y = |u|,\qquad\sum_{y\in V(\mathcal{T})} c_y = |V(\mathcal{T})|-1 = n_\pi+n_{\varnothing}. n y ∗ = ∣ E ∣ , y ∈ V ( T ) ∑ n y = ∣ u ∣ , y ∈ V ( T ) ∑ c y = ∣ V ( T ) ∣ − 1 = n π + n ∅ .
Define
R ( E ) : = ( ∣ E ∣ ! ) τ ∏ j ∈ E ∣ ξ j ( T ) ∣ 2 = ( ∣ E ∣ ! ) τ ∏ j ∈ E ( τ σ j ) . R(E) := (|E|!)^\tau\prod_{j\in E} |\xi_j(\mathcal{T})|_2 = (|E|!)^\tau\prod_{j\in E}(\sqrt{\tau}\,\sigma_j). R ( E ) := ( ∣ E ∣ ! ) τ j ∈ E ∏ ∣ ξ j ( T ) ∣ 2 = ( ∣ E ∣ ! ) τ j ∈ E ∏ ( τ σ j ) .
At every vertex y y y ,
( ( n y + c y ) ! ) τ ≤ 2 τ ( n y + c y ) ( n y ! ) τ ( c y ! ) τ . ((n_y+c_y)!)^\tau\le2^{\tau(n_y+c_y)}(n_y!)^\tau(c_y!)^\tau. (( n y + c y )! ) τ ≤ 2 τ ( n y + c y ) ( n y ! ) τ ( c y ! ) τ .
Expanding the coefficient bounds and applying this inequality gives
K T = G 0 G 1 n y ∗ + c y ∗ ( ( n y ∗ + c y ∗ ) ! ) τ ∏ j ∈ E ∣ ξ j ( T ) ∣ 2 ∏ y ∈ V ( T ) ∖ { y ∗ } e B 1 T B 0 B 1 n y + c y ( ( n y + c y ) ! ) τ ≤ G 0 G 1 n y ∗ + c y ∗ 2 τ ( n y ∗ + c y ∗ ) ( n y ∗ ! ) τ ( c y ∗ ! ) τ ∏ j ∈ E ∣ ξ j ( T ) ∣ 2 × ∏ y ∈ V ( T ) ∖ { y ∗ } e B 1 T B 0 B 1 n y + c y 2 τ ( n y + c y ) ( n y ! ) τ ( c y ! ) τ = R ( E ) G 0 ( e B 0 B 1 T B 0 ) n π + n ∅ G 1 n y ∗ + c y ∗ B 1 ∑ y ∈ V ( T ) ∖ { y ∗ } ( n y + c y ) × ( 2 τ ) ∑ y ∈ V ( T ) ( n y + c y ) ∏ S ∈ π ( ∣ S ∣ ! ) τ c ( T ) τ . \begin{aligned}
K_{\mathcal{T}} & = G_0G_1^{n_{y_*}+c_{y_*}}((n_{y_*}+c_{y_*})!)^\tau\prod_{j\in E}|\xi_j(\mathcal{T})|_2 \prod_{y\in V(\mathcal{T})\setminus\{y_*\}}e^{B_1TB_0}B_1^{n_y+c_y}((n_y+c_y)!)^\tau\\
& \le G_0G_1^{n_{y_*}+c_{y_*}}2^{\tau(n_{y_*}+c_{y_*})}(n_{y_*}!)^\tau(c_{y_*}!)^\tau\prod_{j\in E}|\xi_j(\mathcal{T})|_2 \\
&\qquad{}\times\prod_{y\in V(\mathcal{T})\setminus\{y_*\}}e^{B_1TB_0}B_1^{n_y+c_y}2^{\tau(n_y+c_y)}(n_y!)^\tau(c_y!)^\tau\\
& = R(E)G_0(e^{B_0B_1TB_0})^{n_\pi+n_{\varnothing}}G_1^{n_{y_*}+c_{y_*}}B_1^{\sum_{y\in V(\mathcal{T})\setminus\{y_*\}}(n_y+c_y)} \\
&\qquad{}\times(2^\tau)^{\sum_{y\in V(\mathcal{T})}(n_y+c_y)}\prod_{S\in\pi}(|S|!)^\tau c(\mathcal{T})^\tau.
\end{aligned} K T = G 0 G 1 n y ∗ + c y ∗ (( n y ∗ + c y ∗ )! ) τ j ∈ E ∏ ∣ ξ j ( T ) ∣ 2 y ∈ V ( T ) ∖ { y ∗ } ∏ e B 1 T B 0 B 1 n y + c y (( n y + c y )! ) τ ≤ G 0 G 1 n y ∗ + c y ∗ 2 τ ( n y ∗ + c y ∗ ) ( n y ∗ ! ) τ ( c y ∗ ! ) τ j ∈ E ∏ ∣ ξ j ( T ) ∣ 2 × y ∈ V ( T ) ∖ { y ∗ } ∏ e B 1 T B 0 B 1 n y + c y 2 τ ( n y + c y ) ( n y ! ) τ ( c y ! ) τ = R ( E ) G 0 ( e B 0 B 1 T B 0 ) n π + n ∅ G 1 n y ∗ + c y ∗ B 1 ∑ y ∈ V ( T ) ∖ { y ∗ } ( n y + c y ) × ( 2 τ ) ∑ y ∈ V ( T ) ( n y + c y ) S ∈ π ∏ ( ∣ S ∣ ! ) τ c ( T ) τ .
Here the nonempty drift direct sets are exactly the blocks of π \pi π ; empty sets contribute 0 ! = 1 0! = 1 0 ! = 1 , and the child factorials give ∏ y ∈ V ( T ) ( c y ! ) τ = c ( T ) τ \prod_{y\in V(\mathcal{T})}(c_y!)^\tau= c(\mathcal{T})^\tau ∏ y ∈ V ( T ) ( c y ! ) τ = c ( T ) τ by (B.15). Set
K = max { 1 , G 0 , G 1 , e B 0 B 1 T B 0 , B 1 , 2 τ } . K=\max\{1,G_0,G_1,e^{B_0B_1TB_0},B_1,2^\tau\}. K = max { 1 , G 0 , G 1 , e B 0 B 1 T B 0 , B 1 , 2 τ } .
Since ∑ y ∈ V ( T ) ( n y + c y ) = ∣ u ∣ + n π + n ∅ \sum_{y\in V(\mathcal{T})}(n_y+c_y)=|u|+n_\pi+n_{\varnothing} ∑ y ∈ V ( T ) ( n y + c y ) = ∣ u ∣ + n π + n ∅ and n ∅ ≤ n π − 1 n_{\varnothing}\le n_\pi-1 n ∅ ≤ n π − 1 ,
K T ≤ R ( E ) K 1 + 2 ∣ u ∣ + 3 ( n π + n ∅ ) ∏ S ∈ π ( ∣ S ∣ ! ) τ c ( T ) τ ≤ R ( E ) K 2 ∣ u ∣ + 6 n π ∏ S ∈ π ( ∣ S ∣ ! ) τ c ( T ) τ . K_{\mathcal{T}}\le R(E)K^{1+2|u|+3(n_\pi+n_{\varnothing})}\prod_{S\in\pi}(|S|!)^\tau c(\mathcal{T})^\tau\le R(E)K^{2|u|+6n_\pi}\prod_{S\in\pi}(|S|!)^\tau c(\mathcal{T})^\tau. K T ≤ R ( E ) K 1 + 2∣ u ∣ + 3 ( n π + n ∅ ) S ∈ π ∏ ( ∣ S ∣ ! ) τ c ( T ) τ ≤ R ( E ) K 2∣ u ∣ + 6 n π S ∈ π ∏ ( ∣ S ∣ ! ) τ c ( T ) τ .
Taking C 0 = K 6 C_0=K^6 C 0 = K 6 , we have K 2 ∣ u ∣ + 6 n π ≤ C 0 ∣ u ∣ + n π K^{2|u|+6n_\pi}\le C_0^{|u|+n_\pi} K 2∣ u ∣ + 6 n π ≤ C 0 ∣ u ∣ + n π . Moreover, Lemma B.6 and τ ≥ 1 \tau\ge1 τ ≥ 1 give
c ( T ) τ = c ( T ) τ − 1 c ( T ) ≤ ( n π ! ) τ − 1 c ( T ) . c(\mathcal{T})^\tau=c(\mathcal{T})^{\tau-1}c(\mathcal{T})\le(n_\pi!)^{\tau-1}c(\mathcal{T}). c ( T ) τ = c ( T ) τ − 1 c ( T ) ≤ ( n π ! ) τ − 1 c ( T ) .
Consequently,
K T ≤ C 0 ∣ u ∣ + n π R ( E ) ∏ S ∈ π ( ∣ S ∣ ! ) τ ( n π ! ) τ − 1 c ( T ) . (96) K_{\mathcal{T}}\le C_0^{|u|+n_\pi}R(E)\prod_{S\in\pi}(|S|!)^\tau(n_\pi!)^{\tau-1}c(\mathcal{T}). \tag*{(96)} K T ≤ C 0 ∣ u ∣ + n π R ( E ) S ∈ π ∏ ( ∣ S ∣ ! ) τ ( n π ! ) τ − 1 c ( T ) . (96)
Summing and applying (B.16), we obtain
∑ T ∈ Γ ( E , π ) K T ≤ C 0 ∣ u ∣ + n π R ( E ) ∏ S ∈ π ( ∣ S ∣ ! ) τ ( n π ! ) τ − 1 ∑ T ∈ Γ ( E , π ) c ( T ) ≤ C 0 ∣ u ∣ + n π 64 n π R ( E ) ( n π ! ) τ ∏ S ∈ π ( ∣ S ∣ ! ) τ . \begin{aligned}
\sum_{\mathcal{T}\in\Gamma(E,\pi)}K_{\mathcal{T}}\le C_0^{|u|+n_\pi}R(E)\prod_{S\in\pi}(|S|!)^\tau(n_\pi!)^{\tau-1}\sum_{\mathcal{T}\in\Gamma(E,\pi)}c(\mathcal{T}) \\
&\le C_0^{|u|+n_\pi}64^{n_\pi}R(E)(n_\pi!)^\tau\prod_{S\in\pi}(|S|!)^\tau.
\end{aligned} T ∈ Γ ( E , π ) ∑ K T ≤ C 0 ∣ u ∣ + n π R ( E ) S ∈ π ∏ ( ∣ S ∣ ! ) τ ( n π ! ) τ − 1 T ∈ Γ ( E , π ) ∑ c ( T ) ≤ C 0 ∣ u ∣ + n π 6 4 n π R ( E ) ( n π ! ) τ S ∈ π ∏ ( ∣ S ∣ ! ) τ .
Hence, taking
C c n t = 64 C 0 = 64 K 6 , C_{\mathrm{cnt}}=64C_0=64K^6, C cnt = 64 C 0 = 64 K 6 ,
proves (B.18). This constant depends only on T T T , B 0 B_0 B 0 , B 1 B_1 B 1 , G 0 G_0 G 0 , G 1 G_1 G 1 , τ \tau τ .
Proof of the derivative majorant
Proof of Proposition 4.3. Fix E ⊆ u ∩ E w E \subseteq u \cap E_w E ⊆ u ∩ E w , put u ˉ = u ∖ E \bar{u}=u\setminus E u ˉ = u ∖ E , and fix π ∈ P ( u ˉ ) \pi\in\mathcal{P}(\bar{u}) π ∈ P ( u ˉ ) . If u ˉ ≠ ∅ \bar{u}\ne\varnothing u ˉ = ∅ , put n π = ∣ π ∣ n_\pi=|\pi| n π = ∣ π ∣ . For T ∈ Γ ( E , π ) \mathcal{T}\in\Gamma(E,\pi) T ∈ Γ ( E , π ) , let n ∅ n_{\varnothing} n ∅ be the number of drift vertices with empty direct label sets, as defined in (B.14). Then T \mathcal{T} T has n π + n ∅ n_\pi+n_{\varnothing} n π + n ∅ drift vertices. At each drift vertex y y y put
f y ( i ) = ∏ j ∈ S ( y ) ∣ ξ j ( t i ) ∣ 2 . f_y(i)=\prod_{j\in S(y)}|\xi_j(t_i)|^2. f y ( i ) = j ∈ S ( y ) ∏ ∣ ξ j ( t i ) ∣ 2 .
with the empty product equal to one. Enlarging the admissible times to independent choices gives
h n π + n ∅ ∑ i ∈ R m ( T ) ∏ y ∈ V ( T ) ∖ { y ∗ } f y ( i y ) ≤ ∏ y ∈ V ( T ) ∖ { y ∗ } ( h ∑ i = 0 m − 1 f y ( i ) ) = T n ∅ ∏ S ∈ π η m ( S ) . (97) h^{n_\pi+n_{\varnothing}}\sum_{i\in\mathcal{R}_m(\mathcal{T})}\prod_{y\in V(\mathcal{T})\setminus\{y_*\}}f_y(i_y)
\leq\prod_{y\in V(\mathcal{T})\setminus\{y_*\}}\left(h\sum_{i=0}^{m-1}f_y(i)\right)
=T^{n_{\varnothing}}\prod_{S\in\pi}\eta_m(S). \tag*{(97)} h n π + n ∅ i ∈ R m ( T ) ∑ y ∈ V ( T ) ∖ { y ∗ } ∏ f y ( i y ) ≤ y ∈ V ( T ) ∖ { y ∗ } ∏ ( h i = 0 ∑ m − 1 f y ( i ) ) = T n ∅ S ∈ π ∏ η m ( S ) . (97)
The equality follows because each nonempty direct set S ∈ π S\in\pi S ∈ π contributes η m ( S ) \eta_m(S) η m ( S ) by (4.9), while each empty direct set contributes m h = T mh=T mh = T .
Let C c n t ≥ 1 C_{\mathrm{cnt}}\geq1 C cnt ≥ 1 be the constant in (B.18) and choose
C m a j = max { C c n t max ( 1 , T ) , G 1 max ( 1 , G 0 ) } . C_{\mathrm{maj}}=\max\{C_{\mathrm{cnt}}\max(1,T),G_1\max(1,G_0)\}. C maj = max { C cnt max ( 1 , T ) , G 1 max ( 1 , G 0 )} .
This constant depends only on T T T , B 0 B_0 B 0 , B 1 B_1 B 1 , G 0 G_0 G 0 , G 1 G_1 G 1 , τ \tau τ . Combining (B.17), (B.20), and (B.18) gives
e − β g ∣ X t m h ∣ 2 ∑ T ∈ Γ ( E , π ) ∑ i ∈ R m ( T ) ∣ G ( T , i ) ∣ ≤ ∑ T ∈ Γ ( E , π ) K T h ∣ V ( T ) ∣ − 1 ∑ i ∈ R m ( T ) ∏ y ∈ V ( T ) ∖ { y ∗ } f y ( i y ) ≤ ∏ S ∈ π η m ( S ) ∑ T ∈ Γ ( E , π ) K T T n ∅ ≤ max ( 1 , T ) n π ∏ S ∈ π η m ( S ) ∑ T ∈ Γ ( E , π ) K T ≤ C m a j ∣ u ∣ + n π ( ∣ E ∣ ! ) τ ∏ j ∈ E ( T σ j ) ( n π ! ) τ ∏ S ∈ π ( ∣ S ∣ ! ) τ η m ( S ) . (98) \begin{aligned}
e^{-\beta_g|X^h_{t_m}|_2}\sum_{\mathcal{T}\in\Gamma(E,\pi)}\sum_{i\in\mathcal{R}_m(\mathcal{T})}|\mathcal{G}(\mathcal{T},i)|
&\leq\sum_{\mathcal{T}\in\Gamma(E,\pi)}\mathcal{K}_{\mathcal{T}}h^{|V(\mathcal{T})|-1}\sum_{i\in\mathcal{R}_m(\mathcal{T})}\prod_{y\in V(\mathcal{T})\setminus\{y_*\}}f_y(i_y)\\
&\leq\prod_{S\in\pi}\eta_m(S)\sum_{\mathcal{T}\in\Gamma(E,\pi)}\mathcal{K}_{\mathcal{T}}T^{n_{\varnothing}}\\
&\leq\max(1,T)^{n_\pi}\prod_{S\in\pi}\eta_m(S)\sum_{\mathcal{T}\in\Gamma(E,\pi)}\mathcal{K}_{\mathcal{T}}\\
&\leq C_{\mathrm{maj}}^{|u|+n_\pi}(|E|!)^\tau\prod_{j\in E}(\sqrt{T}\,\sigma_j)(n_\pi!)^\tau\prod_{S\in\pi}(|S|!)^\tau\eta_m(S). \tag*{(98)}
\end{aligned} e − β g ∣ X t m h ∣ 2 T ∈ Γ ( E , π ) ∑ i ∈ R m ( T ) ∑ ∣ G ( T , i ) ∣ ≤ T ∈ Γ ( E , π ) ∑ K T h ∣ V ( T ) ∣ − 1 i ∈ R m ( T ) ∑ y ∈ V ( T ) ∖ { y ∗ } ∏ f y ( i y ) ≤ S ∈ π ∏ η m ( S ) T ∈ Γ ( E , π ) ∑ K T T n ∅ ≤ max ( 1 , T ) n π S ∈ π ∏ η m ( S ) T ∈ Γ ( E , π ) ∑ K T ≤ C maj ∣ u ∣ + n π ( ∣ E ∣ ! ) τ j ∈ E ∏ ( T σ j ) ( n π ! ) τ S ∈ π ∏ ( ∣ S ∣ ! ) τ η m ( S ) . (98)
Here the third inequality uses n ∅ ≤ n π − 1 n_{\varnothing}\leq n_\pi-1 n ∅ ≤ n π − 1 , which gives T n ∅ ≤ max ( 1 , T ) n π T^{n_{\varnothing}}\leq\max(1,T)^{n_\pi} T n ∅ ≤ max ( 1 , T ) n π . The last inequality absorbs max ( 1 , T ) n π \max(1,T)^{n_\pi} max ( 1 , T ) n π into C m a j ∣ u ∣ + n π C_{\mathrm{maj}}^{|u|+n_\pi} C maj ∣ u ∣ + n π .
If u ˉ = ∅ \bar{u}=\varnothing u ˉ = ∅ , then E = u ⊆ E w E=u\subseteq E_w E = u ⊆ E w and the tree consists only of its payoff root. By (2.5),
e − β g ∣ X t m h ∣ 2 ∣ D x ∣ u ∣ g ( X t m h ) [ ξ j ( T ) : j ∈ u ] ∣ ≤ G 0 G 1 ∣ u ∣ ( ∣ u ∣ ! ) τ ∏ j ∈ u ( T σ j ) ≤ C m a j ∣ u ∣ ( ∣ u ∣ ! ) τ ∏ j ∈ u ( T σ j ) . e^{-\beta_g|X^h_{t_m}|_2}\left|D_x^{|u|}g(X^h_{t_m})[\xi_j(T):j\in u]\right|
\leq G_0G_1^{|u|}(|u|!)^\tau\prod_{j\in u}(\sqrt{T}\,\sigma_j)
\leq C_{\mathrm{maj}}^{|u|}(|u|!)^\tau\prod_{j\in u}(\sqrt{T}\,\sigma_j). e − β g ∣ X t m h ∣ 2 D x ∣ u ∣ g ( X t m h ) [ ξ j ( T ) : j ∈ u ] ≤ G 0 G 1 ∣ u ∣ ( ∣ u ∣ ! ) τ j ∈ u ∏ ( T σ j ) ≤ C maj ∣ u ∣ ( ∣ u ∣ ! ) τ j ∈ u ∏ ( T σ j ) .
Thus the final bound in (B.21) also holds for u ˉ = ∅ \bar{u}=\varnothing u ˉ = ∅ , π = ∅ \pi=\varnothing π = ∅ .
Finally, the triangle inequality in (B.6) and the final bound in (B.21) give
e − β g ∣ X t m h ∣ 2 ∣ ∂ u F m ( z ) ∣ ≤ e − β g ∣ X t m h ∣ 2 ∑ E ⊆ u ∩ E w ∑ π ∈ P ( u ∖ E ) ∑ T ∈ Γ ( E , π ) ∑ i ∈ R m ( T ) ∣ G ( T , i ) ∣ ≤ ∑ E ⊆ u ∩ E w ∑ π ∈ P ( u ∖ E ) C m a j ∣ u ∣ + ∣ π ∣ ( ∣ E ∣ ! ) τ ∏ j ∈ E ( T σ j ) ( ∣ π ∣ ! ) τ ∏ S ∈ π ( ∣ S ∣ ! ) τ η m ( S ) = C m a j ∣ u ∣ ∑ E ⊆ u ∩ E w ( ∣ E ∣ ! ) τ ∏ j ∈ E ( T σ j ) ∑ π ∈ P ( u ∖ E ) C m a j ∣ π ∣ ( ∣ π ∣ ! ) τ ∏ S ∈ π ( ∣ S ∣ ! ) τ η m ( S ) . \begin{aligned}
e^{-\beta_g|X^h_{t_m}|_2}|\partial_uF_m(z)|
&\leq e^{-\beta_g|X^h_{t_m}|_2}\sum_{E\subseteq u\cap E_w}\sum_{\pi\in\mathcal{P}(u\setminus E)}\sum_{\mathcal{T}\in\Gamma(E,\pi)}\sum_{i\in\mathcal{R}_m(\mathcal{T})}|\mathcal{G}(\mathcal{T},i)|\\
&\leq\sum_{E\subseteq u\cap E_w}\sum_{\pi\in\mathcal{P}(u\setminus E)}C_{\mathrm{maj}}^{|u|+|\pi|}(|E|!)^\tau\prod_{j\in E}(\sqrt{T}\,\sigma_j)(|\pi|!)^\tau\prod_{S\in\pi}(|S|!)^\tau\eta_m(S)\\
&=C_{\mathrm{maj}}^{|u|}\sum_{E\subseteq u\cap E_w}(|E|!)^\tau\prod_{j\in E}(\sqrt{T}\,\sigma_j)\sum_{\pi\in\mathcal{P}(u\setminus E)}C_{\mathrm{maj}}^{|\pi|}(|\pi|!)^\tau\prod_{S\in\pi}(|S|!)^\tau\eta_m(S).
\end{aligned} e − β g ∣ X t m h ∣ 2 ∣ ∂ u F m ( z ) ∣ ≤ e − β g ∣ X t m h ∣ 2 E ⊆ u ∩ E w ∑ π ∈ P ( u ∖ E ) ∑ T ∈ Γ ( E , π ) ∑ i ∈ R m ( T ) ∑ ∣ G ( T , i ) ∣ ≤ E ⊆ u ∩ E w ∑ π ∈ P ( u ∖ E ) ∑ C maj ∣ u ∣ + ∣ π ∣ ( ∣ E ∣ ! ) τ j ∈ E ∏ ( T σ j ) ( ∣ π ∣ ! ) τ S ∈ π ∏ ( ∣ S ∣ ! ) τ η m ( S ) = C maj ∣ u ∣ E ⊆ u ∩ E w ∑ ( ∣ E ∣ ! ) τ j ∈ E ∏ ( T σ j ) π ∈ P ( u ∖ E ) ∑ C maj ∣ π ∣ ( ∣ π ∣ ! ) τ S ∈ π ∏ ( ∣ S ∣ ! ) τ η m ( S ) .
The right-hand side is independent of z z z . Taking the supremum over z ∈ R s z\in\mathbb{R}^s z ∈ R s proves (4.10). ∩ევნ
Proofs of the auxiliary summability estimates
This appendix proves Lemmas 4.4 and 4.5.
Proof of Lemma 4.4. Fix m ∈ M m \in\mathcal{M} m ∈ M and ∅ ≠ S ⊆ J m \varnothing\ne S \subseteq\mathcal{J}_m ∅ = S ⊆ J m , and put n = ∣ S ∣ n = |S| n = ∣ S ∣ . If ⋂ j ∈ S int ( I j ) = ∅ \bigcap_{j\in S}\operatorname{int}(I_j) = \varnothing ⋂ j ∈ S int ( I j ) = ∅ , then at every grid point t i t_i t i at least one ξ j ( t i ) \xi_j(t_i) ξ j ( t i ) vanishes, since ξ j \xi_j ξ j is zero outside int ( I j ) \operatorname{int}(I_j) int ( I j ) for every j ∈ J m j \in\mathcal{J}_m j ∈ J m . Consequently,
η m ( S ) = h ∑ i = 0 m − 1 ∏ j ∈ S ∣ ξ j ( t i ) ∣ 2 = 0. \eta_m(S) = h \sum_{i=0}^{m-1} \prod_{j\in S} |\xi_j(t_i)|^2 = 0. η m ( S ) = h i = 0 ∑ m − 1 j ∈ S ∏ ∣ ξ j ( t i ) ∣ 2 = 0.
Otherwise choose j ∗ ∈ S j_* \in S j ∗ ∈ S such that ∣ I j ∗ ∣ = min j ∈ S ∣ I j ∣ |I_{j_*}| = \min_{j\in S}|I_j| ∣ I j ∗ ∣ = min j ∈ S ∣ I j ∣ . By (2.15), for j , j ′ ∈ J m j,j' \in\mathcal{J}_m j , j ′ ∈ J m , either int ( I j ) ∩ int ( I j ′ ) = ∅ \operatorname{int}(I_j) \cap\operatorname{int}(I_{j'}) = \varnothing int ( I j ) ∩ int ( I j ′ ) = ∅ , or I j ⊆ I j ′ I_j \subseteq I_{j'} I j ⊆ I j ′ , or I j ′ ⊆ I j I_{j'} \subseteq I_j I j ′ ⊆ I j . Since the intervals indexed by S S S have a nonempty interior intersection, every I j I_j I j , j ∈ S j \in S j ∈ S , contains I j ∗ I_{j_*} I j ∗ . Thus a summand in η m ( S ) \eta_m(S) η m ( S ) can be nonzero only when t i ∈ I j ∗ t_i \in I_{j_*} t i ∈ I j ∗ .
The interval I j ∗ I_{j_*} I j ∗ contains at most 1 + ∣ I j ∗ ∣ / h 1+|I_{j_*}|/h 1 + ∣ I j ∗ ∣/ h grid points. Write ∣ I j ∗ ∣ = T 2 − ℓ ∗ |I_{j_*}| = T2^{-\ell_*} ∣ I j ∗ ∣ = T 2 − ℓ ∗ , where ℓ ∗ ∈ { 0 , … , J − 1 } \ell_* \in\{0,\ldots,J-1\} ℓ ∗ ∈ { 0 , … , J − 1 } . Since h = T 2 − J h=T2^{-J} h = T 2 − J , we have
∣ I j ∗ ∣ ≥ T 2 − ( J − 1 ) = 2 h , h ( 1 + ∣ I j ∗ ∣ h ) = h + ∣ I j ∗ ∣ ≤ 3 2 ∣ I j ∗ ∣ . |I_{j_*}| \ge T2^{-(J-1)} = 2h,\qquad h\left(1+\frac{|I_{j_*}|}{h}\right)=h+|I_{j_*}| \le\frac{3}{2}|I_{j_*}|. ∣ I j ∗ ∣ ≥ T 2 − ( J − 1 ) = 2 h , h ( 1 + h ∣ I j ∗ ∣ ) = h + ∣ I j ∗ ∣ ≤ 2 3 ∣ I j ∗ ∣.
For each j ∈ S j \in S j ∈ S , the height bound in (2.18) gives ∣ ξ j ( t i ) ∣ 2 ≤ σ r ( j ) 2 ∣ I j ∣ 1 / 2 |\xi_j(t_i)|^2 \le\frac{\sigma_{r(j)}}{2}|I_j|^{1/2} ∣ ξ j ( t i ) ∣ 2 ≤ 2 σ r ( j ) ∣ I j ∣ 1/2 . Applying these bounds to the defining sum, we obtain
η m ( S ) = h ∑ i = 0 m − 1 ∏ j ∈ S ∣ ξ j ( t i ) ∣ 2 = h ∑ 0 ≤ i ≤ m − 1 t i ∈ I j ∗ ∏ j ∈ S ∣ ξ j ( t i ) ∣ 2 ≤ h ( 1 + ∣ I j ∗ ∣ h ) ∏ j ∈ S ( σ r ( j ) 2 ∣ I j ∣ 1 / 2 ) ≤ 3 2 ∣ I j ∗ ∣ ∏ j ∈ S ( σ r ( j ) 2 ∣ I j ∣ 1 / 2 ) . \begin{aligned}
\eta_m(S) = h \sum_{i=0}^{m-1} \prod_{j\in S}|\xi_j(t_i)|^2
= h \sum_{\substack{0\le i\le m-1\\t_i\in I_{j_*}}} \prod_{j\in S}|\xi_j(t_i)|^2
\le h\left(1+\frac{|I_{j_*}|}{h}\right)\prod_{j\in S}\left(\frac{\sigma_{r(j)}}{2}|I_j|^{1/2}\right) \\
&\le\frac{3}{2}|I_{j_*}|\prod_{j\in S}\left(\frac{\sigma_{r(j)}}{2}|I_j|^{1/2}\right).
\end{aligned} η m ( S ) = h i = 0 ∑ m − 1 j ∈ S ∏ ∣ ξ j ( t i ) ∣ 2 = h 0 ≤ i ≤ m − 1 t i ∈ I j ∗ ∑ j ∈ S ∏ ∣ ξ j ( t i ) ∣ 2 ≤ h ( 1 + h ∣ I j ∗ ∣ ) j ∈ S ∏ ( 2 σ r ( j ) ∣ I j ∣ 1/2 ) ≤ 2 3 ∣ I j ∗ ∣ j ∈ S ∏ ( 2 σ r ( j ) ∣ I j ∣ 1/2 ) .
This proves (4.11).
We next prove (4.12). Fix an integer n ≥ 1 n \ge1 n ≥ 1 . Recall that each j ∈ J m j \in\mathcal{J}_m j ∈ J m has indices ( ℓ ( j ) , μ ( j ) , r ( j ) ) (\ell(j),\mu(j),r(j)) ( ℓ ( j ) , μ ( j ) , r ( j )) determined by (2.11), with ∣ I j ∣ = T 2 − ℓ ( j ) |I_j|=T2^{-\ell(j)} ∣ I j ∣ = T 2 − ℓ ( j ) . For 0 ≤ ℓ ∗ ≤ J − 1 0\le\ell_*\le J-1 0 ≤ ℓ ∗ ≤ J − 1 and j ∗ ∈ J m j_*\in\mathcal{J}_m j ∗ ∈ J m with ℓ ( j ∗ ) = ℓ ∗ \ell(j_*)=\ell_* ℓ ( j ∗ ) = ℓ ∗ , define
S ℓ ∗ , j ∗ : = { S ⊆ J m : ∣ S ∣ = n , ⋂ j ∈ S int ( I j ) ≠ ∅ , max j ∈ S ℓ ( j ) = ℓ ∗ , j ∗ = min { j ∈ S : ℓ ( j ) = ℓ ∗ } } . \mathcal{S}_{\ell_*,j_*}:=\left\{S\subseteq\mathcal{J}_m:
\ |S|=n,\quad\bigcap_{j\in S}\operatorname{int}(I_j)\ne\varnothing,\quad
\max_{j\in S}\ell(j)=\ell_*,\quad
j_*=\min\{j\in S:\ell(j)=\ell_*\}\right\}. S ℓ ∗ , j ∗ := ⎩ ⎨ ⎧ S ⊆ J m : ∣ S ∣ = n , j ∈ S ⋂ int ( I j ) = ∅ , j ∈ S max ℓ ( j ) = ℓ ∗ , j ∗ = min { j ∈ S : ℓ ( j ) = ℓ ∗ } ⎭ ⎬ ⎫ .
Here, choosing the smallest index j ∗ j_* j ∗ among those at level ℓ ∗ \ell_* ℓ ∗ makes the classes pairwise disjoint. Every n n n -element subset S ⊆ J m S\subseteq\mathcal{J}_m S ⊆ J m with ⋂ j ∈ S int ( I j ) ≠ ∅ \bigcap_{j\in S}\operatorname{int}(I_j)\ne\varnothing ⋂ j ∈ S int ( I j ) = ∅ belongs to exactly one such class; all other n n n -element subsets satisfy η m ( S ) = 0 \eta_m(S)=0 η m ( S ) = 0 . If J = 0 J=0 J = 0 , then J m = ∅ \mathcal{J}_m=\varnothing J m = ∅ and the claimed sum is zero, so below we may assume J ≥ 1 J\ge1 J ≥ 1 .
For S ∈ S ℓ ∗ , j ∗ S\in\mathcal{S}_{\ell_*,j_*} S ∈ S ℓ ∗ , j ∗ , the interval I j ∗ I_{j_*} I j ∗ is shortest. Raising (4.11) to the power ρ \rho ρ and substituting ∣ I j ∣ = T 2 − ℓ ( j ) |I_j|=T2^{-\ell(j)} ∣ I j ∣ = T 2 − ℓ ( j ) gives
η m ( S ) ρ ≤ ( 3 / 2 ) ρ 2 − n ρ σ r ( j ∗ ) ρ ∣ I j ∗ ∣ 3 ρ / 2 ∏ j ∈ S ∖ { j ∗ } σ r ( j ) ρ ∣ I j ∣ ρ / 2 = ( 3 / 2 ) ρ 2 − n ρ T ρ ( n + 2 ) / 2 σ r ( j ∗ ) ρ 2 − 3 ρ ℓ ∗ / 2 ∏ j ∈ S ∖ { j ∗ } σ r ( j ) ρ 2 − ρ ℓ ( j ) / 2 . (99) \begin{aligned}
\eta_m(S)^\rho\le(3/2)^\rho2^{-n\rho} \sigma_{r(j_*)}^\rho|I_{j_*}|^{3\rho/2}
\prod_{j\in S\setminus\{j_*\}}\sigma_{r(j)}^\rho|I_j|^{\rho/2} \\
&= (3/2)^\rho2^{-n\rho}T^{\rho(n+2)/2}\sigma_{r(j_*)}^\rho
2^{-3\rho\ell_*/2}\prod_{j\in S\setminus\{j_*\}}\sigma_{r(j)}^\rho2^{-\rho\ell(j)/2}. \tag*{(99)}
\end{aligned} η m ( S ) ρ ≤ ( 3/2 ) ρ 2 − n ρ σ r ( j ∗ ) ρ ∣ I j ∗ ∣ 3 ρ /2 j ∈ S ∖ { j ∗ } ∏ σ r ( j ) ρ ∣ I j ∣ ρ /2 = ( 3/2 ) ρ 2 − n ρ T ρ ( n + 2 ) /2 σ r ( j ∗ ) ρ 2 − 3 ρ ℓ ∗ /2 j ∈ S ∖ { j ∗ } ∏ σ r ( j ) ρ 2 − ρ ℓ ( j ) /2 . (99)
To bound the sum over S ∈ S ℓ ∗ , j ∗ S\in\mathcal{S}_{\ell_*,j_*} S ∈ S ℓ ∗ , j ∗ of the products in (C.1), define the list
A ℓ ∗ : = ( σ 1 ρ , … , σ d w ρ , 2 − ρ / 2 σ 1 ρ , … , 2 − ρ / 2 σ d w ρ , … , 2 − ρ ℓ ∗ / 2 σ 1 ρ , … , 2 − ρ ℓ ∗ / 2 σ d w ρ ) . \mathcal{A}_{\ell_*}:=(\sigma_1^\rho,\ldots,\sigma_{d_w}^\rho,
2^{-\rho/2}\sigma_1^\rho,\ldots,2^{-\rho/2}\sigma_{d_w}^\rho,
\ldots,
2^{-\rho\ell_*/2}\sigma_1^\rho,\ldots,2^{-\rho\ell_*/2}\sigma_{d_w}^\rho). A ℓ ∗ := ( σ 1 ρ , … , σ d w ρ , 2 − ρ /2 σ 1 ρ , … , 2 − ρ /2 σ d w ρ , … , 2 − ρ ℓ ∗ /2 σ 1 ρ , … , 2 − ρ ℓ ∗ /2 σ d w ρ ) .
Write N ℓ ∗ = d w ( ℓ ∗ + 1 ) N_{\ell_*}=d_w(\ell_*+1) N ℓ ∗ = d w ( ℓ ∗ + 1 ) and denote the entries of A ℓ ∗ A_{\ell_*} A ℓ ∗ by α q \alpha_q α q , 1 ≤ q ≤ N ℓ ∗ 1\le q\le N_{\ell_*} 1 ≤ q ≤ N ℓ ∗ . Define
e n − 1 ( A ℓ ∗ ) : = ∑ 1 ≤ q 1 < ⋯ < q n − 1 ≤ N ℓ ∗ ∏ i = 1 n − 1 α q i , e 0 ( A ℓ ∗ ) = 1. e_{n-1}(A_{\ell_*}):=\sum_{1\le q_1<\cdots<q_{n-1}\le N_{\ell_*}}\prod_{i=1}^{n-1}\alpha_{q_i},\qquad e_0(A_{\ell_*})=1. e n − 1 ( A ℓ ∗ ) := 1 ≤ q 1 < ⋯ < q n − 1 ≤ N ℓ ∗ ∑ i = 1 ∏ n − 1 α q i , e 0 ( A ℓ ∗ ) = 1.
The sum is zero when n − 1 > N ℓ ∗ n-1>N_{\ell_*} n − 1 > N ℓ ∗ .
For each 0 ≤ ℓ ≤ ℓ ∗ 0\le\ell\le\ell_* 0 ≤ ℓ ≤ ℓ ∗ , let I ℓ ∗ I_\ell^* I ℓ ∗ be the unique dyadic interval of length T 2 − ℓ T2^{-\ell} T 2 − ℓ containing I j ∗ I_{j_*} I j ∗ . For S ∈ S ℓ ∗ , j ∗ S\in\mathcal{S}_{\ell_*,j_*} S ∈ S ℓ ∗ , j ∗ , every j ∈ S j\in S j ∈ S with ℓ ( j ) = ℓ \ell(j)=\ell ℓ ( j ) = ℓ satisfies I j = I ℓ ∗ I_j=I_\ell^* I j = I ℓ ∗ . By (2.11) and (2.15), exactly d w d_w d w indices j ∈ J m j\in\mathcal{J}_m j ∈ J m have support I ℓ ∗ I_\ell^* I ℓ ∗ , with pairwise distinct values r ( j ) r(j) r ( j ) ranging over { 1 , … , d w } \{1,\ldots,d_w\} { 1 , … , d w } . For each j ∈ S ∖ { j ∗ } j\in S\setminus\{j_*\} j ∈ S ∖ { j ∗ } , define q ( j ) : = d w ℓ ( j ) + r ( j ) q(j):=d_w\ell(j)+r(j) q ( j ) := d w ℓ ( j ) + r ( j ) . By the definition of A ℓ ∗ A_{\ell_*} A ℓ ∗ ,
α q ( j ) = σ r ( j ) ρ 2 − ρ ℓ ( j ) / 2 . \alpha_{q(j)}=\sigma_{r(j)}^\rho2^{-\rho\ell(j)/2}. α q ( j ) = σ r ( j ) ρ 2 − ρ ℓ ( j ) /2 .
Each position q q q determines ( ℓ , r ) (\ell,r) ( ℓ , r ) , which together with I ℓ ∗ I_\ell^* I ℓ ∗ uniquely determines j j j by (2.11) and (2.15). Thus the position set { q ( j ) : j ∈ S ∖ { j ∗ } } \{q(j):j\in S\setminus\{j_*\}\} { q ( j ) : j ∈ S ∖ { j ∗ }} uniquely determines S ∈ S ℓ ∗ , j ∗ S\in\mathcal{S}_{\ell_*,j_*} S ∈ S ℓ ∗ , j ∗ . Summing over all ( n − 1 ) (n-1) ( n − 1 ) -element subsets of positions therefore only enlarges the sum. Hence
∑ S ∈ S ℓ ∗ , j ∗ ∏ j ∈ S ∖ { j ∗ } σ r ( j ) ρ 2 − ρ ℓ ( j ) / 2 ≤ e n − 1 ( A ℓ ∗ ) . (100) \sum_{S\in\mathcal{S}_{\ell_*,j_*}}\prod_{j\in S\setminus\{j_*\}}\sigma_{r(j)}^\rho2^{-\rho\ell(j)/2}\le e_{n-1}(A_{\ell_*}). \tag*{(100)} S ∈ S ℓ ∗ , j ∗ ∑ j ∈ S ∖ { j ∗ } ∏ σ r ( j ) ρ 2 − ρ ℓ ( j ) /2 ≤ e n − 1 ( A ℓ ∗ ) . (100)
Note that
∑ j ∗ ∈ J m ℓ ( j ∗ ) = ℓ ∗ σ r ( j ∗ ) ρ = ∑ μ = 0 2 ℓ ∗ − 1 ∑ r = 1 d w σ r ρ = 2 ℓ ∗ Θ ρ . (101) \sum_{\substack{j_*\in\mathcal{J}_m\\ \ell(j_*)=\ell_*}}\sigma_{r(j_*)}^\rho
=\sum_{\mu=0}^{2^{\ell_*}-1}\sum_{r=1}^{d_w}\sigma_r^\rho
=2^{\ell_*}\Theta_\rho. \tag*{(101)} j ∗ ∈ J m ℓ ( j ∗ ) = ℓ ∗ ∑ σ r ( j ∗ ) ρ = μ = 0 ∑ 2 ℓ ∗ − 1 r = 1 ∑ d w σ r ρ = 2 ℓ ∗ Θ ρ . (101)
Using (C.1), (C.2), and (C.3), we obtain
∑ S ⊂ J m ∣ S ∣ = n η m ( S ) ρ = ∑ ℓ ∗ = 0 J − 1 ∑ j ∗ ∈ J m ℓ ( j ∗ ) = ℓ ∗ ∑ S ∈ S ℓ ∗ , j ∗ η m ( S ) ρ ≤ ( 3 / 2 ) ρ 2 − n ρ T ρ ( n + 2 ) / 2 Θ ρ ∑ ℓ ∗ = 0 J − 1 2 ( 1 − 3 ρ / 2 ) ℓ ∗ e n − 1 ( A ℓ ∗ ) . \begin{aligned}
\sum_{\substack{S\subset\mathcal{J}_m\\ |S|=n}}\eta_m(S)^\rho
=\sum_{\ell_*=0}^{J-1}\sum_{\substack{j_*\in\mathcal{J}_m\\ \ell(j_*)=\ell_*}}\sum_{S\in\mathcal{S}_{\ell_*,j_*}}\eta_m(S)^\rho\\
&\le(3/2)^\rho2^{-n\rho T^\rho(n+2)/2}\Theta_\rho\sum_{\ell_*=0}^{J-1}2^{(1-3\rho/2)\ell_*}e_{n-1}(A_{\ell_*}).
\end{aligned} S ⊂ J m ∣ S ∣ = n ∑ η m ( S ) ρ = ℓ ∗ = 0 ∑ J − 1 j ∗ ∈ J m ℓ ( j ∗ ) = ℓ ∗ ∑ S ∈ S ℓ ∗ , j ∗ ∑ η m ( S ) ρ ≤ ( 3/2 ) ρ 2 − n ρ T ρ ( n + 2 ) /2 Θ ρ ℓ ∗ = 0 ∑ J − 1 2 ( 1 − 3 ρ /2 ) ℓ ∗ e n − 1 ( A ℓ ∗ ) .
Moreover,
e n − 1 ( A ℓ ∗ ) ≤ 1 ( n − 1 ) ! ( ∑ q = 1 N ℓ ∗ α q ) n − 1 = 1 ( n − 1 ) ! ( Θ ρ ∑ ℓ = 0 ℓ ∗ 2 − ρ ℓ / 2 ) n − 1 . (102) e_{n-1}(A_{\ell_*})\le\frac{1}{(n-1)!}\left(\sum_{q=1}^{N_{\ell_*}}\alpha_q\right)^{n-1}
=\frac{1}{(n-1)!}\left(\Theta_\rho\sum_{\ell=0}^{\ell_*}2^{-\rho\ell/2}\right)^{n-1}. \tag*{(102)} e n − 1 ( A ℓ ∗ ) ≤ ( n − 1 )! 1 q = 1 ∑ N ℓ ∗ α q n − 1 = ( n − 1 )! 1 ( Θ ρ ℓ = 0 ∑ ℓ ∗ 2 − ρ ℓ /2 ) n − 1 . (102)
Consequently,
∑ S ⊂ J m ∣ S ∣ = n η m ( S ) ρ ≤ ( 3 / 2 ) ρ 2 − n ρ T ρ ( n + 2 ) / 2 Θ ρ ( n − 1 ) ! ∑ ℓ ∗ = 0 J − 1 2 ( 1 − 3 ρ / 2 ) ℓ ∗ ( Θ ρ ∑ ℓ = 0 ℓ ∗ 2 − ρ ℓ / 2 ) n − 1 ≤ ( 3 / 2 ) ρ 2 − n ρ T ρ ( n + 2 ) / 2 Θ ρ ( n − 1 ) ! ( ∑ ℓ ∗ = 0 ∞ 2 ( 1 − 3 ρ / 2 ) ℓ ∗ ) ( Θ ρ ∑ ℓ = 0 ∞ 2 − ρ ℓ / 2 ) n − 1 = ( 3 / 2 ) ρ 2 − n ρ T ρ ( n + 2 ) / 2 Θ ρ n ( 1 − 2 1 − 3 ρ / 2 ) ( 1 − 2 − ρ / 2 ) n − 1 ( n − 1 ) ! . \begin{aligned}
\sum_{\substack{S\subset\mathcal{J}_m\\ |S|=n}}\eta_m(S)^\rho
\le\frac{(3/2)^\rho2^{-n\rho T^\rho(n+2)/2}\Theta_\rho}{(n-1)!}
\sum_{\ell_*=0}^{J-1}2^{(1-3\rho/2)\ell_*}
\left(\Theta_\rho\sum_{\ell=0}^{\ell_*}2^{-\rho\ell/2}\right)^{n-1} \\
&\le\frac{(3/2)^\rho2^{-n\rho T^\rho(n+2)/2}\Theta_\rho}{(n-1)!}
\left(\sum_{\ell_*=0}^{\infty}2^{(1-3\rho/2)\ell_*}\right)
\left(\Theta_\rho\sum_{\ell=0}^{\infty}2^{-\rho\ell/2}\right)^{n-1} \\
&=\frac{(3/2)^\rho2^{-n\rho T^\rho(n+2)/2}\Theta_\rho^n}
{(1-2^{1-3\rho/2})(1-2^{-\rho/2})^{n-1}(n-1)!}.
\end{aligned} S ⊂ J m ∣ S ∣ = n ∑ η m ( S ) ρ ≤ ( n − 1 )! ( 3/2 ) ρ 2 − n ρ T ρ ( n + 2 ) /2 Θ ρ ℓ ∗ = 0 ∑ J − 1 2 ( 1 − 3 ρ /2 ) ℓ ∗ ( Θ ρ ℓ = 0 ∑ ℓ ∗ 2 − ρ ℓ /2 ) n − 1 ≤ ( n − 1 )! ( 3/2 ) ρ 2 − n ρ T ρ ( n + 2 ) /2 Θ ρ ( ℓ ∗ = 0 ∑ ∞ 2 ( 1 − 3 ρ /2 ) ℓ ∗ ) ( Θ ρ ℓ = 0 ∑ ∞ 2 − ρ ℓ /2 ) n − 1 = ( 1 − 2 1 − 3 ρ /2 ) ( 1 − 2 − ρ /2 ) n − 1 ( n − 1 )! ( 3/2 ) ρ 2 − n ρ T ρ ( n + 2 ) /2 Θ ρ n .
Both geometric series converge since ρ > 2 / 3 \rho>2/3 ρ > 2/3 . To make the constant explicit, set
C ρ , T ′ = 2 − ρ T ρ / 2 1 − 2 − ρ / 2 , C ρ , T ′ ′ = ( 3 / 2 ) ρ T ρ ( 1 − 2 − ρ / 2 ) 1 − 2 1 − 3 ρ / 2 , C ρ , T = C ρ , T ′ max { 1 , C ρ , T ′ ′ } . C'_{\rho,T}=\frac{2^{-\rho T^\rho/2}}{1-2^{-\rho/2}},\qquad
C''_{\rho,T}=\frac{(3/2)^\rho T^\rho(1-2^{-\rho/2})}{1-2^{1-3\rho/2}},\qquad
C_{\rho,T}=C'_{\rho,T}\max\{1,C''_{\rho,T}\}. C ρ , T ′ = 1 − 2 − ρ /2 2 − ρ T ρ /2 , C ρ , T ′′ = 1 − 2 1 − 3 ρ /2 ( 3/2 ) ρ T ρ ( 1 − 2 − ρ /2 ) , C ρ , T = C ρ , T ′ max { 1 , C ρ , T ′′ } .
The last bound is C ρ , T ′ ′ C ρ , T ′ n Θ ρ n / ( n − 1 ) ! C''_{\rho,T}C'_{\rho,T}{}^n\Theta_\rho^n/(n-1)! C ρ , T ′′ C ρ , T ′ n Θ ρ n / ( n − 1 )! . Since n ≥ 1 n\ge1 n ≥ 1 , we have C ρ , T ′ ′ C ρ , T ′ n Θ ρ n ≤ C ρ , T n Θ ρ n C''_{\rho,T}C'_{\rho,T}{}^n\Theta_\rho^n\le C_{\rho,T}^n\Theta_\rho^n C ρ , T ′′ C ρ , T ′ n Θ ρ n ≤ C ρ , T n Θ ρ n . The constant C ρ , T C_{\rho,T} C ρ , T depends only on ρ , T \rho,T ρ , T . Taking the supremum over m ∈ M m\in\mathcal{M} m ∈ M proves (4.12).
Proof of Lemma 4.5. Fix 2 / 3 < ρ < 1 / τ 2/3<\rho<1/\tau 2/3 < ρ < 1/ τ and κ > 0 \kappa>0 κ > 0 . Similarly to (C.4),
Υ E ( κ ) = ∑ ℓ = 0 d w κ ℓ T ρ ℓ / 2 ( ℓ ! ) τ ρ ∑ E ⊆ E w ∣ E ∣ = ℓ ∏ j ∈ E σ j ρ ≤ ∑ ℓ = 0 ∞ ( κ T ρ / 2 Θ ρ ) ℓ ( ℓ ! ) τ ρ − 1 = : Υ ∗ E ( κ ) . (103) \Upsilon^{\mathcal{E}}(\kappa)=\sum_{\ell=0}^{d_w}\kappa^{\ell}T^{\rho\ell/2}(\ell!)^{\tau\rho}\sum_{\substack{E\subseteq\mathcal{E}_w\\ |E|=\ell}}\prod_{j\in E}\sigma_j^{\rho}\leq\sum_{\ell=0}^{\infty}\left(\kappa T^{\rho/2}\Theta_\rho\right)^{\ell}(\ell!)^{\tau\rho-1}=:\Upsilon^{\mathcal{E}}_{*}(\kappa). \tag*{(103)} Υ E ( κ ) = ℓ = 0 ∑ d w κ ℓ T ρ ℓ /2 ( ℓ ! ) τ ρ E ⊆ E w ∣ E ∣ = ℓ ∑ j ∈ E ∏ σ j ρ ≤ ℓ = 0 ∑ ∞ ( κ T ρ /2 Θ ρ ) ℓ ( ℓ ! ) τ ρ − 1 =: Υ ∗ E ( κ ) . (103)
For the detail inputs, Lemma 4.4 yields
Υ m J ( κ ) : = ∑ ∅ ≠ D ⊆ J m κ ∣ D ∣ ( ∣ D ∣ ! ) τ ρ η m ( D ) ρ = ∑ n ≥ 1 κ n ( n ! ) τ ρ ∑ D ⊆ J m ∣ D ∣ = n η m ( D ) ρ ≤ ∑ n ≥ 1 ( κ C ρ , T Θ ρ ) n n ( n ! ) τ ρ − 1 = : Υ ∗ J ( κ ) . \begin{aligned}
\Upsilon^{\mathcal{J}}_m(\kappa):=\sum_{\varnothing\ne D\subseteq\mathcal{J}_m}\kappa^{|D|}(|D|!)^{\tau\rho}\eta_m(D)^\rho=\sum_{n\geq1}\kappa^n(n!)^{\tau\rho}\sum_{\substack{D\subseteq\mathcal{J}_m\\ |D|=n}}\eta_m(D)^\rho\\
&\leq\sum_{n\geq1}\left(\kappa C_{\rho,T}\Theta_\rho\right)^n n(n!)^{\tau\rho-1}=:\Upsilon^{\mathcal{J}}_{*}(\kappa).
\end{aligned} Υ m J ( κ ) := ∅ = D ⊆ J m ∑ κ ∣ D ∣ ( ∣ D ∣ ! ) τ ρ η m ( D ) ρ = n ≥ 1 ∑ κ n ( n ! ) τ ρ D ⊆ J m ∣ D ∣ = n ∑ η m ( D ) ρ ≤ n ≥ 1 ∑ ( κ C ρ , T Θ ρ ) n n ( n ! ) τ ρ − 1 =: Υ ∗ J ( κ ) .
If Θ ρ > 0 \Theta_\rho>0 Θ ρ > 0 , the ratios of consecutive terms in Υ ∗ E ( κ ) \Upsilon^{\mathcal{E}}_{*}(\kappa) Υ ∗ E ( κ ) and Υ ∗ J ( κ ) \Upsilon^{\mathcal{J}}_{*}(\kappa) Υ ∗ J ( κ ) are κ T ρ / 2 Θ ρ ( ℓ + 1 ) τ ρ − 1 \kappa T^{\rho/2}\Theta_\rho(\ell+1)^{\tau\rho-1} κ T ρ /2 Θ ρ ( ℓ + 1 ) τ ρ − 1 and κ C ρ , T Θ ρ ( 1 + 1 / n ) ( n + 1 ) τ ρ − 1 \kappa C_{\rho,T}\Theta_\rho(1+1/n)(n+1)^{\tau\rho-1} κ C ρ , T Θ ρ ( 1 + 1/ n ) ( n + 1 ) τ ρ − 1 , respectively. Both tend to zero since τ ρ < 1 \tau\rho<1 τ ρ < 1 , so both series converge for every κ > 0 \kappa>0 κ > 0 . If Θ ρ = 0 \Theta_\rho=0 Θ ρ = 0 , then Υ ∗ E ( κ ) = 1 \Upsilon^{\mathcal{E}}_{*}(\kappa)=1 Υ ∗ E ( κ ) = 1 and Υ ∗ J ( κ ) = 0 \Upsilon^{\mathcal{J}}_{*}(\kappa)=0 Υ ∗ J ( κ ) = 0 .
Every nonempty S ⊆ [ s ] S\subseteq[s] S ⊆ [ s ] has a unique decomposition S = D ∪ ˙ E S=D\mathbin{\dot\cup}E S = D ∪ ˙ E , with D ⊆ J m D\subseteq\mathcal{J}_m D ⊆ J m and E ⊆ E w E\subseteq\mathcal{E}_w E ⊆ E w . The endpoint bound ∣ ξ j ( t i ) ∣ 2 ≤ T σ j |\xi_j(t_i)|^2\leq\sqrt{T}\,\sigma_j ∣ ξ j ( t i ) ∣ 2 ≤ T σ j for j ∈ E j\in E j ∈ E , together with m h = T mh=T mh = T , gives
η m ( D ∪ E ) = h ∑ i = 0 m − 1 ( ∏ j ∈ D ∣ ξ j ( t i ) ∣ 2 ) ( ∏ j ∈ E ∣ ξ j ( t i ) ∣ 2 ) ≤ { η m ( D ) ∏ j ∈ E ( T σ j ) , D ≠ ∅ , T ∏ j ∈ E ( T σ j ) , D = ∅ . \eta_m(D\cup E)=h\sum_{i=0}^{m-1}\left(\prod_{j\in D}|\xi_j(t_i)|^2\right)\left(\prod_{j\in E}|\xi_j(t_i)|^2\right)\leq\begin{cases}\eta_m(D)\prod_{j\in E}(\sqrt{T}\,\sigma_j),&D\ne\varnothing,\\[6pt]T\prod_{j\in E}(\sqrt{T}\,\sigma_j),&D=\varnothing.\end{cases} η m ( D ∪ E ) = h i = 0 ∑ m − 1 j ∈ D ∏ ∣ ξ j ( t i ) ∣ 2 j ∈ E ∏ ∣ ξ j ( t i ) ∣ 2 ≤ ⎩ ⎨ ⎧ η m ( D ) ∏ j ∈ E ( T σ j ) , T ∏ j ∈ E ( T σ j ) , D = ∅ , D = ∅ .
The inequality ( ∣ D ∣ + ∣ E ∣ ∣ D ∣ ) ≤ 2 ∣ D ∣ + ∣ E ∣ \binom{|D|+|E|}{|D|}\leq2^{|D|+|E|} ( ∣ D ∣ ∣ D ∣ + ∣ E ∣ ) ≤ 2 ∣ D ∣ + ∣ E ∣ gives, with κ ′ = 2 τ ρ κ \kappa'=2^{\tau\rho}\kappa κ ′ = 2 τ ρ κ ,
κ ∣ D ∣ + ∣ E ∣ ( ( ∣ D ∣ + ∣ E ∣ ) ! ) τ ρ ≤ ( κ ′ ) ∣ D ∣ ( ∣ D ∣ ! ) τ ρ ( κ ′ ) ∣ E ∣ ( ∣ E ∣ ! ) τ ρ . \kappa^{|D|+|E|}((|D|+|E|)!)^{\tau\rho}\leq(\kappa')^{|D|}(|D|!)^{\tau\rho}(\kappa')^{|E|}(|E|!)^{\tau\rho}. κ ∣ D ∣ + ∣ E ∣ (( ∣ D ∣ + ∣ E ∣ )! ) τ ρ ≤ ( κ ′ ) ∣ D ∣ ( ∣ D ∣ ! ) τ ρ ( κ ′ ) ∣ E ∣ ( ∣ E ∣ ! ) τ ρ .
Summing over D ≠ ∅ D\ne\varnothing D = ∅ and all E E E gives
∑ ∅ ≠ D ⊆ J m ∑ E ⊆ E w κ ∣ D ∣ + ∣ E ∣ ( ( ∣ D ∣ + ∣ E ∣ ) ! ) τ ρ η m ( D ∪ E ) ρ ≤ [ ∑ ∅ ≠ D ⊆ J m ( κ ′ ) ∣ D ∣ ( ∣ D ∣ ! ) τ ρ η m ( D ) ρ ] [ ∑ E ⊆ E w ( κ ′ ) ∣ E ∣ ( ∣ E ∣ ! ) τ ρ ∏ j ∈ E ( T σ j ) ρ ] = Υ m J ( κ ′ ) Υ E ( κ ′ ) . \begin{aligned}
\sum_{\varnothing\ne D\subseteq\mathcal{J}_m}\sum_{E\subseteq\mathcal{E}_w}\kappa^{|D|+|E|}((|D|+|E|)!)^{\tau\rho}\eta_m(D\cup E)^\rho\\
&\leq\left[\sum_{\varnothing\ne D\subseteq\mathcal{J}_m}(\kappa')^{|D|}(|D|!)^{\tau\rho}\eta_m(D)^\rho\right]\left[\sum_{E\subseteq\mathcal{E}_w}(\kappa')^{|E|}(|E|!)^{\tau\rho}\prod_{j\in E}(\sqrt{T}\,\sigma_j)^\rho\right] \\
&=\Upsilon^{\mathcal{J}}_m(\kappa')\Upsilon^{\mathcal{E}}(\kappa').
\end{aligned} ∅ = D ⊆ J m ∑ E ⊆ E w ∑ κ ∣ D ∣ + ∣ E ∣ (( ∣ D ∣ + ∣ E ∣ )! ) τ ρ η m ( D ∪ E ) ρ ≤ ∅ = D ⊆ J m ∑ ( κ ′ ) ∣ D ∣ ( ∣ D ∣ ! ) τ ρ η m ( D ) ρ E ⊆ E w ∑ ( κ ′ ) ∣ E ∣ ( ∣ E ∣ ! ) τ ρ j ∈ E ∏ ( T σ j ) ρ = Υ m J ( κ ′ ) Υ E ( κ ′ ) .
For D = ∅ D=\varnothing D = ∅ , the condition S ≠ ∅ S\ne\varnothing S = ∅ requires E ≠ ∅ E\ne\varnothing E = ∅ , and
∑ ∅ ≠ E ⊆ E w κ ∣ E ∣ ( ∣ E ∣ ! ) τ ρ η m ( E ) ρ ≤ T ρ ∑ ∅ ≠ E ⊆ E w κ ∣ E ∣ ( ∣ E ∣ ! ) τ ρ ∏ j ∈ E ( T σ j ) ρ = T ρ ( Υ E ( κ ) − 1 ) . \begin{aligned}
\sum_{\varnothing\ne E\subseteq\mathcal{E}_w}\kappa^{|E|}(|E|!)^{\tau\rho}\eta_m(E)^\rho\leq T^\rho\sum_{\varnothing\ne E\subseteq\mathcal{E}_w}\kappa^{|E|}(|E|!)^{\tau\rho}\prod_{j\in E}(\sqrt{T}\,\sigma_j)^\rho\\
&=T^\rho\left(\Upsilon^{\mathcal{E}}(\kappa)-1\right).
\end{aligned} ∅ = E ⊆ E w ∑ κ ∣ E ∣ ( ∣ E ∣ ! ) τ ρ η m ( E ) ρ ≤ T ρ ∅ = E ⊆ E w ∑ κ ∣ E ∣ ( ∣ E ∣ ! ) τ ρ j ∈ E ∏ ( T σ j ) ρ = T ρ ( Υ E ( κ ) − 1 ) .
Combining these two contributions yields
Υ m ( κ ) ≤ Υ m J ( κ ′ ) Υ E ( κ ′ ) + T ρ ( Υ E ( κ ) − 1 ) ≤ Υ ∗ J ( κ ′ ) Υ ∗ E ( κ ′ ) + T ρ ( Υ ∗ E ( κ ) − 1 ) < ∞ . \begin{aligned}
\Upsilon_m(\kappa)\leq\Upsilon^{\mathcal{J}}_m(\kappa')\Upsilon^{\mathcal{E}}(\kappa')+T^\rho\left(\Upsilon^{\mathcal{E}}(\kappa)-1\right) \\
&\leq\Upsilon^{\mathcal{J}}_{*}(\kappa')\Upsilon^{\mathcal{E}}_{*}(\kappa')+T^\rho\left(\Upsilon^{\mathcal{E}}_{*}(\kappa)-1\right)<\infty.
\end{aligned} Υ m ( κ ) ≤ Υ m J ( κ ′ ) Υ E ( κ ′ ) + T ρ ( Υ E ( κ ) − 1 ) ≤ Υ ∗ J ( κ ′ ) Υ ∗ E ( κ ′ ) + T ρ ( Υ ∗ E ( κ ) − 1 ) < ∞.
Together with Υ E ( κ ) ≤ Υ ∗ E ( κ ) \Upsilon^{\mathcal{E}}(\kappa)\leq\Upsilon^{\mathcal{E}}_{*}(\kappa) Υ E ( κ ) ≤ Υ ∗ E ( κ ) , this proves the lemma with
C Υ ( κ , ρ , τ , T ; Θ ρ ) : = Υ ∗ E ( κ ) + Υ ∗ J ( κ ′ ) Υ ∗ E ( κ ′ ) + T ρ ( Υ ∗ E ( κ ) − 1 ) . C_{\Upsilon}(\kappa,\rho,\tau,T;\Theta_\rho):=\Upsilon^{\mathcal{E}}_{*}(\kappa)+\Upsilon^{\mathcal{J}}_{*}(\kappa')\Upsilon^{\mathcal{E}}_{*}(\kappa')+T^\rho\left(\Upsilon^{\mathcal{E}}_{*}(\kappa)-1\right). C Υ ( κ , ρ , τ , T ; Θ ρ ) := Υ ∗ E ( κ ) + Υ ∗ J ( κ ′ ) Υ ∗ E ( κ ′ ) + T ρ ( Υ ∗ E ( κ ) − 1 ) .
Every term in the defining series is nonnegative and nondecreasing in κ \kappa κ and Θ ρ \Theta_\rho Θ ρ . Hence this constant depends only on κ , ρ , τ , T , Θ ρ \kappa,\rho,\tau,T,\Theta_\rho κ , ρ , τ , T , Θ ρ and is nondecreasing in both κ \kappa κ and Θ ρ \Theta_\rho Θ ρ .
Proofs of the weighted Gaussian norm estimates
Proof of Lemma 5.1. For each 1 ≤ r ≤ d w 1 \le r \le d_w 1 ≤ r ≤ d w and 0 ≤ ℓ < J 0 \le\ell< J 0 ≤ ℓ < J , define
M ℓ , r : = max j ∈ J m ℓ ( j ) = ℓ , r ( j ) = r ∣ z j ∣ . M_{\ell,r} := \max_{\substack{j \in\mathcal{J}_m\\ \ell(j)=\ell,\ r(j)=r}} |z_j|. M ℓ , r := j ∈ J m ℓ ( j ) = ℓ , r ( j ) = r max ∣ z j ∣.
For fixed 0 ≤ ℓ < J 0 \le\ell< J 0 ≤ ℓ < J , 1 ≤ r ≤ d w 1 \le r \le d_w 1 ≤ r ≤ d w , and 0 ≤ i ≤ m 0 \le i \le m 0 ≤ i ≤ m , (19) and (20) give
∣ { j ∈ J m : ℓ ( j ) = ℓ , r ( j ) = r , ξ j ( t i ) ≠ 0 } ∣ ≤ 1. \left|\left\{j \in\mathcal{J}_m : \ell(j)=\ell,\ r(j)=r,\ \xi_j(t_i) \ne0\right\}\right| \le1. ∣ { j ∈ J m : ℓ ( j ) = ℓ , r ( j ) = r , ξ j ( t i ) = 0 } ∣ ≤ 1.
Hence, by (21) and (22) ,
∣ Σ W t i ( z ) ∣ 2 ≤ ∑ r = 1 d w ∣ ξ r ( t i ) ∣ 2 ∣ z r ∣ + ∑ ℓ = 0 J − 1 ∑ r = 1 d w ∑ j ∈ J m ℓ ( j ) = ℓ , r ( j ) = r ∣ ξ j ( t i ) ∣ 2 ∣ z j ∣ ≤ T ∑ r = 1 d w σ r ∣ z r ∣ + T 2 ∑ ℓ = 0 J − 1 ∑ r = 1 d w σ r 2 − ℓ / 2 M ℓ , r = T ∑ r = 1 d w σ r ( ∣ z r ∣ + 1 2 ∑ ℓ = 0 J − 1 2 − ℓ / 2 M ℓ , r ) . (104) \begin{aligned}
|\Sigma W_{t_i}(z)|_2
&\le\sum_{r=1}^{d_w} |\xi_r(t_i)|_2 |z_r|
+ \sum_{\ell=0}^{J-1}\sum_{r=1}^{d_w}
\sum_{\substack{j\in\mathcal{J}_m\\\ell(j)=\ell,\ r(j)=r}}
|\xi_j(t_i)|_2 |z_j| \\
&\le\sqrt{T}\sum_{r=1}^{d_w}\sigma_r|z_r|
+ \frac{\sqrt{T}}{2}\sum_{\ell=0}^{J-1}\sum_{r=1}^{d_w}
\sigma_r 2^{-\ell/2}M_{\ell,r} \\
&= \sqrt{T}\sum_{r=1}^{d_w}\sigma_r
\left(|z_r|+\frac{1}{2}\sum_{\ell=0}^{J-1}2^{-\ell/2}M_{\ell,r}\right). \tag*{(104)}
\end{aligned} ∣Σ W t i ( z ) ∣ 2 ≤ r = 1 ∑ d w ∣ ξ r ( t i ) ∣ 2 ∣ z r ∣ + ℓ = 0 ∑ J − 1 r = 1 ∑ d w j ∈ J m ℓ ( j ) = ℓ , r ( j ) = r ∑ ∣ ξ j ( t i ) ∣ 2 ∣ z j ∣ ≤ T r = 1 ∑ d w σ r ∣ z r ∣ + 2 T ℓ = 0 ∑ J − 1 r = 1 ∑ d w σ r 2 − ℓ /2 M ℓ , r = T r = 1 ∑ d w σ r ( ∣ z r ∣ + 2 1 ℓ = 0 ∑ J − 1 2 − ℓ /2 M ℓ , r ) . (104)
The same bound holds for max 0 ≤ i ≤ m ∣ Σ W t i ( z ) ∣ 2 \max_{0\le i\le m}|\Sigma W_{t_i}(z)|_2 max 0 ≤ i ≤ m ∣Σ W t i ( z ) ∣ 2 . The telescoped Euler recursion and the drift bound in (10) give
∣ X t i h ( z ) ∣ 2 ≤ ∣ x 0 ∣ 2 + K 0 T + max 0 ≤ i ′ ≤ m ∣ Σ W t i ′ ( z ) ∣ 2 + B 1 h ∑ i ′ = 0 i − 1 ∣ X t i ′ h ( z ) ∣ 2 . |X^h_{t_i}(z)|_2 \le|x_0|_2+K_0T+\max_{0\le i'\le m}|\Sigma W_{t_{i'}}(z)|_2+B_1h\sum_{i'=0}^{i-1}|X^h_{t_{i'}}(z)|_2. ∣ X t i h ( z ) ∣ 2 ≤ ∣ x 0 ∣ 2 + K 0 T + 0 ≤ i ′ ≤ m max ∣Σ W t i ′ ( z ) ∣ 2 + B 1 h i ′ = 0 ∑ i − 1 ∣ X t i ′ h ( z ) ∣ 2 .
Discrete Gronwall yields
max i ∣ X t i h ( z ) ∣ 2 ≤ e B 1 T ( ∣ x 0 ∣ 2 + K 0 T + max i ∣ Σ W t i ( z ) ∣ 2 ) . (105) \max_i |X^h_{t_i}(z)|_2
\le e^{B_1T}\left(|x_0|_2+K_0T+\max_i|\Sigma W_{t_i}(z)|_2\right). \tag*{(105)} i max ∣ X t i h ( z ) ∣ 2 ≤ e B 1 T ( ∣ x 0 ∣ 2 + K 0 T + i max ∣Σ W t i ( z ) ∣ 2 ) . (105)
In the following moment estimates, evaluate these quantities at z = Z ( u ) z=Z^{(u)} z = Z ( u ) . Set
λ 0 : = 2 β g e B 1 T T Θ 1 ( 2 + 1 2 ) . \lambda_0:=2\beta_g e^{B_1T}\sqrt{T}\Theta_1\left(2+\frac{1}{\sqrt{2}}\right). λ 0 := 2 β g e B 1 T T Θ 1 ( 2 + 2 1 ) .
Then (62) gives 2 α 0 − λ 0 = 2 2\alpha_0-\lambda_0=2 2 α 0 − λ 0 = 2 , and each coordinate satisfies
E e λ 0 ∣ Z j ( u ) ∣ ≤ K α 0 ( λ 0 ) : = max ( 2 e λ 0 2 / 2 , 2 α 0 2 α 0 − λ 0 ) = max ( 2 e λ 0 2 / 2 , α 0 ) . \mathbb{E}e^{\lambda_0|Z_j^{(u)}|}
\le K_{\alpha_0}(\lambda_0)
:=\max\left(2e^{\lambda_0^2/2},\frac{2\alpha_0}{2\alpha_0-\lambda_0}\right)
=\max\left(2e^{\lambda_0^2/2},\alpha_0\right). E e λ 0 ∣ Z j ( u ) ∣ ≤ K α 0 ( λ 0 ) := max ( 2 e λ 0 2 /2 , 2 α 0 − λ 0 2 α 0 ) = max ( 2 e λ 0 2 /2 , α 0 ) .
Since (15) gives 2 ℓ 2^\ell 2 ℓ indices with ℓ ( j ) = ℓ \ell(j)=\ell ℓ ( j ) = ℓ and r ( j ) = r r(j)=r r ( j ) = r , we have
E e λ 0 M ℓ , r ≤ ∑ j ∈ J m ℓ ( j ) = ℓ , r ( j ) = r E e λ 0 ∣ Z j ( u ) ∣ ≤ 2 ℓ K α 0 ( λ 0 ) . \mathbb{E}e^{\lambda_0M_{\ell,r}}
\le\sum_{\substack{j\in\mathcal{J}_m\\\ell(j)=\ell,\ r(j)=r}}
\mathbb{E}e^{\lambda_0|Z_j^{(u)}|}
\le2^\ell K_{\alpha_0}(\lambda_0). E e λ 0 M ℓ , r ≤ j ∈ J m ℓ ( j ) = ℓ , r ( j ) = r ∑ E e λ 0 ∣ Z j ( u ) ∣ ≤ 2 ℓ K α 0 ( λ 0 ) .
Assume Θ 1 > 0 \Theta_1>0 Θ 1 > 0 , with Θ 1 \Theta_1 Θ 1 defined in (11) . Define the weights
w r = σ r Θ 1 ( 2 + 1 2 ) , w ℓ , r = σ r 2 − ℓ / 2 2 Θ 1 ( 2 + 1 2 ) . w_r=\frac{\sigma_r}{\Theta_1\left(2+\frac{1}{\sqrt{2}}\right)},\qquad
w_{\ell,r}=\frac{\sigma_r2^{-\ell/2}}{2\Theta_1\left(2+\frac{1}{\sqrt{2}}\right)}. w r = Θ 1 ( 2 + 2 1 ) σ r , w ℓ , r = 2 Θ 1 ( 2 + 2 1 ) σ r 2 − ℓ /2 .
Since 1 + 1 2 ∑ ℓ ≥ 0 2 − ℓ / 2 = 2 + 1 2 1+\frac{1}{2}\sum_{\ell\ge0}2^{-\ell/2}=2+\frac{1}{\sqrt{2}} 1 + 2 1 ∑ ℓ ≥ 0 2 − ℓ /2 = 2 + 2 1 , we have
ω : = ∑ r = 1 d w w r + ∑ ℓ = 0 J − 1 ∑ r = 1 d w w ℓ , r = 1 + 1 2 ∑ ℓ = 0 J − 1 2 − ℓ / 2 2 + 1 2 ≤ 1. \omega:=\sum_{r=1}^{d_w}w_r+\sum_{\ell=0}^{J-1}\sum_{r=1}^{d_w}w_{\ell,r}=\frac{1+\frac{1}{2}\sum_{\ell=0}^{J-1}2^{-\ell/2}}{2+\frac{1}{\sqrt{2}}}\le1. ω := r = 1 ∑ d w w r + ℓ = 0 ∑ J − 1 r = 1 ∑ d w w ℓ , r = 2 + 2 1 1 + 2 1 ∑ ℓ = 0 J − 1 2 − ℓ /2 ≤ 1.
Put w ∗ = 1 − ω w_* = 1-\omega w ∗ = 1 − ω . Then λ 0 w r = 2 β g e B 1 T T σ r \lambda_0w_r=2\beta_g e^{B_1T}\sqrt{T}\,\sigma_r λ 0 w r = 2 β g e B 1 T T σ r and λ 0 w ℓ , r = 2 β g e B 1 T T σ r 2 − ℓ / 2 / 2 \lambda_0w_{\ell,r}=2\beta_g e^{B_1T}\sqrt{T}\,\sigma_r2^{-\ell/2}/2 λ 0 w ℓ , r = 2 β g e B 1 T T σ r 2 − ℓ /2 /2 . Omitting zero weights, generalized Hölder gives
E exp { 2 β g e B 1 T T ∑ r = 1 d w σ r ( ∣ Z r ( u ) ∣ + 1 2 ∑ ℓ = 0 J − 1 2 − ℓ / 2 M ℓ , r ) } = E [ ∏ r = 1 d w ( e λ 0 ∣ Z r ( u ) ∣ ) w r ∏ ℓ = 0 J − 1 ∏ r = 1 d w ( e λ 0 M ℓ , r ) w ℓ , r ] ≤ ∏ r = 1 d w ( E e λ 0 ∣ Z r ( u ) ∣ ) w r ∏ ℓ = 0 J − 1 ∏ r = 1 d w ( E e λ 0 M ℓ , r ) w ℓ , r ≤ K α 0 ( λ 0 ) ω 2 ∑ ℓ = 0 J − 1 ∑ r = 1 d w ℓ w ℓ , r ≤ K α 0 ( λ 0 ) exp { log 2 4 + 2 ∑ ℓ = 0 J − 1 ℓ 2 − ℓ / 2 } ≤ K α 0 ( λ 0 ) exp { log 2 4 + 2 ∑ ℓ = 0 ∞ ℓ 2 − ℓ / 2 } = K α 0 ( λ 0 ) 2 4 + 3 2 4 + 2 . \begin{aligned}
\mathbb{E}\exp\left\{2\beta_g e^{B_1T}\sqrt{T}\sum_{r=1}^{d_w}\sigma_r\left(\lvert Z_r^{(u)}\rvert+\frac{1}{2}\sum_{\ell=0}^{J-1}2^{-\ell/2}M_{\ell,r}\right)\right\}
&=\mathbb{E}\left[\prod_{r=1}^{d_w}\left(e^{\lambda_0\lvert Z_r^{(u)}\rvert}\right)^{w_r}\prod_{\ell=0}^{J-1}\prod_{r=1}^{d_w}\left(e^{\lambda_0M_{\ell,r}}\right)^{w_{\ell,r}}\right]\\
&\le\prod_{r=1}^{d_w}\left(\mathbb{E}e^{\lambda_0\lvert Z_r^{(u)}\rvert}\right)^{w_r}\prod_{\ell=0}^{J-1}\prod_{r=1}^{d_w}\left(\mathbb{E}e^{\lambda_0M_{\ell,r}}\right)^{w_{\ell,r}}\\
&\le K_{\alpha_0}(\lambda_0)^{\omega}2^{\sum_{\ell=0}^{J-1}\sum_{r=1}^{d_w}\ell w_{\ell,r}}\\
&\le K_{\alpha_0}(\lambda_0)\exp\left\{\frac{\log2}{4+\sqrt{2}}\sum_{\ell=0}^{J-1}\ell2^{-\ell/2}\right\}\\
&\le K_{\alpha_0}(\lambda_0)\exp\left\{\frac{\log2}{4+\sqrt{2}}\sum_{\ell=0}^{\infty}\ell2^{-\ell/2}\right\}
=K_{\alpha_0}(\lambda_0)2^{\frac{4+3\sqrt{2}}{4+\sqrt{2}}}.
\end{aligned} E exp { 2 β g e B 1 T T r = 1 ∑ d w σ r ( ∣ Z r ( u ) ∣ + 2 1 ℓ = 0 ∑ J − 1 2 − ℓ /2 M ℓ , r ) } = E [ r = 1 ∏ d w ( e λ 0 ∣ Z r ( u ) ∣ ) w r ℓ = 0 ∏ J − 1 r = 1 ∏ d w ( e λ 0 M ℓ , r ) w ℓ , r ] ≤ r = 1 ∏ d w ( E e λ 0 ∣ Z r ( u ) ∣ ) w r ℓ = 0 ∏ J − 1 r = 1 ∏ d w ( E e λ 0 M ℓ , r ) w ℓ , r ≤ K α 0 ( λ 0 ) ω 2 ∑ ℓ = 0 J − 1 ∑ r = 1 d w ℓ w ℓ , r ≤ K α 0 ( λ 0 ) exp { 4 + 2 log 2 ℓ = 0 ∑ J − 1 ℓ 2 − ℓ /2 } ≤ K α 0 ( λ 0 ) exp { 4 + 2 log 2 ℓ = 0 ∑ ∞ ℓ 2 − ℓ /2 } = K α 0 ( λ 0 ) 2 4 + 2 4 + 3 2 .
Here we used ω ≤ 1 \omega\le1 ω ≤ 1 , K α 0 ( λ 0 ) ≥ 1 K_{\alpha_0}(\lambda_0)\ge1 K α 0 ( λ 0 ) ≥ 1 , ∑ r = 1 d w σ r = Θ 1 \sum_{r=1}^{d_w}\sigma_r=\Theta_1 ∑ r = 1 d w σ r = Θ 1 , and ∑ ℓ ≥ 0 ℓ 2 − ℓ / 2 = 4 + 3 2 \sum_{\ell\ge0}\ell2^{-\ell/2}=4+3\sqrt{2} ∑ ℓ ≥ 0 ℓ 2 − ℓ /2 = 4 + 3 2 . Define
C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) : = exp { 2 β g e B 1 T ( ∣ x 0 ∣ 2 + K 0 T ) } K α 0 ( λ 0 ) 2 4 + 3 2 4 + 2 < ∞ . (106) C_{\mathrm{aux}}(\lvert x_0\rvert_2,\Theta_1):=\exp\left\{2\beta_g e^{B_1T}(\lvert x_0\rvert_2+K_0T)\right\}K_{\alpha_0}(\lambda_0)2^{\frac{4+3\sqrt{2}}{4+\sqrt{2}}}<\infty. \tag*{(106)} C aux (∣ x 0 ∣ 2 , Θ 1 ) := exp { 2 β g e B 1 T (∣ x 0 ∣ 2 + K 0 T ) } K α 0 ( λ 0 ) 2 4 + 2 4 + 3 2 < ∞. (106)
Combining (D.1), (D.2), and the preceding estimate gives
sup m ∈ N sup u ∈ [ s ] E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) . \sup_{m\in\mathbb{N}}\sup_{u\in[s]}\mathbb{E}e^{2\beta_g\lvert X_{t_m}^{h}(Z^{(u)})\rvert_2}\le C_{\mathrm{aux}}(\lvert x_0\rvert_2,\Theta_1). m ∈ N sup u ∈ [ s ] sup E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ C aux (∣ x 0 ∣ 2 , Θ 1 ) .
If Θ 1 = 0 \Theta_1=0 Θ 1 = 0 , then Σ = 0 \Sigma=0 Σ = 0 , and (D.2) directly gives E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ exp { 2 β g e B 1 T ( ∣ x 0 ∣ 2 + K 0 T ) } \mathbb{E}e^{2\beta_g\lvert X_{t_m}^{h}(Z^{(u)})\rvert_2}\le\exp\left\{2\beta_g e^{B_1T}(\lvert x_0\rvert_2+K_0T)\right\} E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ exp { 2 β g e B 1 T (∣ x 0 ∣ 2 + K 0 T ) } , so the same bound follows from (D.3) with λ 0 = 0 \lambda_0=0 λ 0 = 0 . Both entries of the maximum defining K α 0 ( λ 0 ) K_{\alpha_0}(\lambda_0) K α 0 ( λ 0 ) are nondecreasing in Θ 1 \Theta_1 Θ 1 . Hence (D.3) is nondecreasing in ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 and Θ 1 \Theta_1 Θ 1 .
Proof of Lemma 5.2. Let Z ( u ) Z^{(u)} Z ( u ) be as defined in Lemma 5.1. By (44) , ∣ ∂ u F m ( z ) ∣ ≤ D m , u e β g ∣ X t m h ( z ) ∣ 2 \lvert\partial_uF_m(z)\rvert\le\mathcal{D}_{m,u}e^{\beta_g\lvert X_{t_m}^{h}(z)\rvert_2} ∣ ∂ u F m ( z )∣ ≤ D m , u e β g ∣ X t m h ( z ) ∣ 2 . Jensen’s inequality and α 0 ≥ 1 \alpha_0\ge1 α 0 ≥ 1 give
S u ( F m ) 2 ≤ ∫ R s ∣ ∂ u F m ( z ) ∣ 2 ϕ − u ( z − u ) ∏ j ∈ u e − 2 α 0 ∣ z j ∣ d z ≤ α 0 − ∣ u ∣ D m , u 2 E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ D m , u 2 E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ C a u x ( ∣ x 0 ∣ 2 , Θ 1 ) D m , u 2 . \begin{aligned}
S_u(F_m)^2
&\le\int_{\mathbb{R}^s}\lvert\partial_uF_m(z)\rvert^2\phi_{-u}(z_{-u})\prod_{j\in u}e^{-2\alpha_0\lvert z_j\rvert}\,dz\\
&\le\alpha_0^{-\lvert u\rvert}\mathcal{D}_{m,u}^2\mathbb{E}e^{2\beta_g\lvert X_{t_m}^{h}(Z^{(u)})\rvert_2}
\le\mathcal{D}_{m,u}^2\mathbb{E}e^{2\beta_g\lvert X_{t_m}^{h}(Z^{(u)})\rvert_2}\\
&\le C_{\mathrm{aux}}(\lvert x_0\rvert_2,\Theta_1)\mathcal{D}_{m,u}^2.
\end{aligned} S u ( F m ) 2 ≤ ∫ R s ∣ ∂ u F m ( z ) ∣ 2 ϕ − u ( z − u ) j ∈ u ∏ e − 2 α 0 ∣ z j ∣ d z ≤ α 0 − ∣ u ∣ D m , u 2 E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ D m , u 2 E e 2 β g ∣ X t m h ( Z ( u ) ) ∣ 2 ≤ C aux (∣ x 0 ∣ 2 , Θ 1 ) D m , u 2 .
The last inequality uses Lemma 5.1. Taking square roots proves (63) .
Moment bounds and the Euler bias
Here X t x X_t^x X t x and X ~ t i x \widetilde{X}_{t_i}^{x} X t i x denote, respectively, the solution of the SDE (1.1) and its Euler–Maruyama approximation (2) , both with initial state x x x . Throughout, h = T / m h=T/m h = T / m .
Lemma E.1. For every v > 0 v > 0 v > 0 ,
E exp ( v sup t ≤ T ∣ Σ W t ∣ 2 2 ) ≤ 5 exp ( v 2 T ( 1 + ∥ Σ ∥ H S 2 ) ) . (107) \mathbb{E}\exp\left(v\sup_{t\leq T}|\Sigma W_t|_2^2\right)\leq5\exp\left(v^2T(1+\|\Sigma\|_{\mathrm{HS}}^2)\right). \tag*{(107)} E exp ( v t ≤ T sup ∣Σ W t ∣ 2 2 ) ≤ 5 exp ( v 2 T ( 1 + ∥Σ ∥ HS 2 ) ) . (107) In particular, this bound is uniform in d x , d w d_x,d_w d x , d w under Assumption 2.3, since then ∥ Σ ∥ H S 2 ≤ M 2 / 3 3 \|\Sigma\|_{\mathrm{HS}}^2\leq M_{2/3}^3 ∥Σ ∥ HS 2 ≤ M 2/3 3 by (2.9).
Proof. The case Σ = 0 \Sigma=0 Σ = 0 is immediate. By orthogonal diagonalization of Σ Σ ⊤ \Sigma\Sigma^\top Σ Σ ⊤ , the process Σ W \Sigma W Σ W has the same law as an orthogonal image of ( ς r W ~ r ) r = 1 rank ( Σ ) (\varsigma_r\widetilde W_r)_{r=1}^{\operatorname{rank}(\Sigma)} ( ς r W r ) r = 1 rank ( Σ ) , where ς r > 0 \varsigma_r>0 ς r > 0 are the nonzero singular values of Σ \Sigma Σ , ∑ r = 1 rank ( Σ ) ς r 2 = ∥ Σ ∥ H S 2 \sum_{r=1}^{\operatorname{rank}(\Sigma)}\varsigma_r^2=\|\Sigma\|_{\mathrm{HS}}^2 ∑ r = 1 rank ( Σ ) ς r 2 = ∥Σ ∥ HS 2 , and the W ~ r \widetilde W_r W r are independent one-dimensional Brownian motions. This identity holds for the whole process, since the centered Gaussian covariances agree. Thus sup t ≤ T ∣ Σ W t ∣ 2 2 \sup_{t\leq T}|\Sigma W_t|_2^2 sup t ≤ T ∣Σ W t ∣ 2 2 has the same distribution as sup t ≤ T ∑ r = 1 rank ( Σ ) ς r 2 W ~ r ( t ) 2 \sup_{t\leq T}\sum_{r=1}^{\operatorname{rank}(\Sigma)}\varsigma_r^2\widetilde W_r(t)^2 sup t ≤ T ∑ r = 1 rank ( Σ ) ς r 2 W r ( t ) 2 . Writing W ‾ r = sup t ≤ T ∣ W ~ r ( t ) ∣ \overline W_r=\sup_{t\leq T}|\widetilde W_r(t)| W r = sup t ≤ T ∣ W r ( t ) ∣ , we have
sup t ≤ T ∑ r = 1 rank ( Σ ) ς r 2 W ~ r ( t ) 2 ≤ ∑ r = 1 rank ( Σ ) ς r 2 W ‾ r 2 . \sup_{t\leq T}\sum_{r=1}^{\operatorname{rank}(\Sigma)}\varsigma_r^2\widetilde W_r(t)^2\leq\sum_{r=1}^{\operatorname{rank}(\Sigma)}\varsigma_r^2\overline W_r^2. t ≤ T sup r = 1 ∑ rank ( Σ ) ς r 2 W r ( t ) 2 ≤ r = 1 ∑ rank ( Σ ) ς r 2 W r 2 . Convexity of the exponential, with weights ς r 2 / ∥ Σ ∥ H S 2 \varsigma_r^2/\|\Sigma\|_{\mathrm{HS}}^2 ς r 2 /∥Σ ∥ HS 2 , gives
E exp ( c ∑ r = 1 rank ( Σ ) ς r 2 W ‾ r 2 ) ≤ ∑ r = 1 rank ( Σ ) ς r 2 ∥ Σ ∥ H S 2 E e c ∥ Σ ∥ H S 2 W ‾ r 2 = E e c ∥ Σ ∥ H S 2 W ‾ 1 2 . \mathbb{E}\exp\left(c\sum_{r=1}^{\operatorname{rank}(\Sigma)}\varsigma_r^2\overline W_r^2\right)\leq\sum_{r=1}^{\operatorname{rank}(\Sigma)}\frac{\varsigma_r^2}{\|\Sigma\|_{\mathrm{HS}}^2}\mathbb{E}e^{c\|\Sigma\|_{\mathrm{HS}}^2\overline W_r^2}=\mathbb{E}e^{c\|\Sigma\|_{\mathrm{HS}}^2\overline W_1^2}. E exp c r = 1 ∑ rank ( Σ ) ς r 2 W r 2 ≤ r = 1 ∑ rank ( Σ ) ∥Σ ∥ HS 2 ς r 2 E e c ∥Σ ∥ HS 2 W r 2 = E e c ∥Σ ∥ HS 2 W 1 2 . The reflection principle [15 Theorem 2.21] gives P ( W ‾ 1 > u ) ≤ 4 e − u 2 / ( 2 T ) \mathbb{P}(\overline W_1>u)\leq4e^{-u^2/(2T)} P ( W 1 > u ) ≤ 4 e − u 2 / ( 2 T ) . Hence
E e a W ‾ 1 2 ≤ 1 + 8 a ∫ 0 ∞ u e − ( 1 / ( 2 T ) − a ) u 2 d u < ∞ , 0 < a < 1 / ( 2 T ) . \mathbb{E}e^{a\overline W_1^2}\leq1+8a\int_0^\infty ue^{-(1/(2T)-a)u^2}\,du<\infty,\qquad0<a<1/(2T). E e a W 1 2 ≤ 1 + 8 a ∫ 0 ∞ u e − ( 1/ ( 2 T ) − a ) u 2 d u < ∞ , 0 < a < 1/ ( 2 T ) . For 0 < a ≤ 1 / ( 4 T ) 0<a\leq1/(4T) 0 < a ≤ 1/ ( 4 T ) , the right-hand side is at most 1 + 4 a / ( 1 / ( 2 T ) − a ) ≤ 5 1+4a/(1/(2T)-a)\leq5 1 + 4 a / ( 1/ ( 2 T ) − a ) ≤ 5 . Take c = [ 4 T ( 1 + ∥ Σ ∥ H S 2 ) ] − 1 c=[4T(1+\|\Sigma\|_{\mathrm{HS}}^2)]^{-1} c = [ 4 T ( 1 + ∥Σ ∥ HS 2 ) ] − 1 . Then c ∥ Σ ∥ H S 2 ≤ 1 / ( 4 T ) c\|\Sigma\|_{\mathrm{HS}}^2\leq1/(4T) c ∥Σ ∥ HS 2 ≤ 1/ ( 4 T ) , so the preceding display gives
E exp ( c sup t ≤ T ∣ Σ W t ∣ 2 2 ) ≤ 5. \mathbb{E}\exp\left(c\sup_{t\leq T}|\Sigma W_t|_2^2\right)\leq5. E exp ( c t ≤ T sup ∣Σ W t ∣ 2 2 ) ≤ 5. Using v y ≤ c y 2 + v 2 / ( 4 c ) vy\leq cy^2+v^2/(4c) v y ≤ c y 2 + v 2 / ( 4 c ) proves (E.1). All these inequalities use scalar constants independent of the rank.
Lemma E.2. Under Assumption 2.1, (1.1) has a unique global strong solution. Define
C X ( ∣ x ∣ 2 , ∥ Σ ∥ H S ) : = e B 1 T ( ∣ x ∣ 2 + K 0 T + 2 T ∥ Σ ∥ H S ) . (108) C_X(|x|_2,\|\Sigma\|_{\mathrm{HS}}):=e^{B_1T}\left(|x|_2+K_0T+2\sqrt{T}\|\Sigma\|_{\mathrm{HS}}\right). \tag*{(108)} C X ( ∣ x ∣ 2 , ∥Σ ∥ HS ) := e B 1 T ( ∣ x ∣ 2 + K 0 T + 2 T ∥Σ ∥ HS ) . (108) Then
( E sup t ≤ T ∣ X t x ∣ 2 2 ) 1 / 2 ≤ C X ( ∣ x ∣ 2 , ∥ Σ ∥ H S ) . (109) \left(\mathbb{E}\sup_{t\leq T}|X_t^x|_2^2\right)^{1/2}\leq C_X(|x|_2,\|\Sigma\|_{\mathrm{HS}}). \tag*{(109)} ( E t ≤ T sup ∣ X t x ∣ 2 2 ) 1/2 ≤ C X ( ∣ x ∣ 2 , ∥Σ ∥ HS ) . (109) For v > 0 v>0 v > 0 , define
C exp ( v , ∥ Σ ∥ H S ) : = 10 exp ( v e B 1 T K 0 T + v 2 e 2 B 1 T T ( 1 + ∥ Σ ∥ H S 2 ) ) . (110) C_{\exp}(v,\|\Sigma\|_{\mathrm{HS}}):=10\exp\left(ve^{B_1T}K_0T+v^2e^{2B_1T}T(1+\|\Sigma\|_{\mathrm{HS}}^2)\right). \tag*{(110)} C e x p ( v , ∥Σ ∥ HS ) := 10 exp ( v e B 1 T K 0 T + v 2 e 2 B 1 T T ( 1 + ∥Σ ∥ HS 2 ) ) . (110) For every m ∈ M m\in\mathcal{M} m ∈ M ,
E e v sup t ≤ T ∣ X t x ∣ 2 2 + E e v max i ≤ m ∣ X ~ t i x ∣ 2 2 ≤ C exp ( v , ∥ Σ ∥ H S ) e v e B 1 T ∣ x ∣ 2 . (111) \mathbb{E}e^{v\sup_{t\leq T}|X_t^x|_2^2}+\mathbb{E}e^{v\max_{i\leq m}|\widetilde X_{t_i}^x|_2^2}\leq C_{\exp}(v,\|\Sigma\|_{\mathrm{HS}})e^{ve^{B_1T}|x|_2}. \tag*{(111)} E e v s u p t ≤ T ∣ X t x ∣ 2 2 + E e v m a x i ≤ m ∣ X t i x ∣ 2 2 ≤ C e x p ( v , ∥Σ ∥ HS ) e v e B 1 T ∣ x ∣ 2 . (111)
Proof. Existence and uniqueness follow from global spatial Lipschitz continuity, linear growth, and Borel time dependence; see [24 Theorem 7.1] . Put A = ∣ x ∣ 2 + K 0 T + sup t ≤ T ∣ Σ W t ∣ 2 A=|x|_2+K_0T+\sup_{t\le T}|\Sigma W_t|_2 A = ∣ x ∣ 2 + K 0 T + sup t ≤ T ∣Σ W t ∣ 2 . The integral equation, the telescoped Euler recursion, and the continuous and discrete Gronwall inequalities give
max { sup t ≤ T ∣ X t x ∣ 2 , max i ≤ m ∣ X ~ t i x ∣ 2 } ≤ e B 1 T A \max\left\{\sup_{t\le T}|X_t^x|_2,\max_{i\le m}|\widetilde{X}_{t_i}^x|_2\right\}\le e^{B_1T}A max { t ≤ T sup ∣ X t x ∣ 2 , i ≤ m max ∣ X t i x ∣ 2 } ≤ e B 1 T A
on the same Brownian path. Doob’s L 2 L^2 L 2 inequality gives ∥ sup t ≤ T ∣ Σ W t ∣ 2 ∥ L 2 ≤ 2 T ∥ Σ ∥ H S \left\|\sup_{t\le T}|\Sigma W_t|_2\right\|_{L^2}\le2\sqrt{T}\|\Sigma\|_{\mathrm{HS}} sup t ≤ T ∣Σ W t ∣ 2 L 2 ≤ 2 T ∥Σ ∥ HS , which proves (E.3). The left side of (E.5) is bounded by
2 e ν e B 1 T ( ∣ x ∣ 2 + K 0 T ) E e ν e B 1 T sup t ≤ T ∣ Σ W t ∣ 2 . 2e^{\nu e^{B_1T}(|x|_2+K_0T)}\mathbb{E}e^{\nu e^{B_1T}\sup_{t\le T}|\Sigma W_t|_2}. 2 e ν e B 1 T ( ∣ x ∣ 2 + K 0 T ) E e ν e B 1 T s u p t ≤ T ∣Σ W t ∣ 2 .
Applying (E.1) with ν e B 1 T \nu e^{B_1T} ν e B 1 T proves (E.5) with the choice (E.4).
For the following two proofs, couple the solution X X X of (1.1) and its Euler–Maruyama approximation X h X^h X h in (2.20) using the same Brownian motion W W W . Define
C p a y ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) : = G 0 G 1 2 C exp ( 2 β g , ∥ Σ ∥ H S ) exp ( β g e B 1 T ∣ x 0 ∣ 2 ) . (112) C_{\mathrm{pay}}(|x_0|_2,\|\Sigma\|_{\mathrm{HS}}):=G_0G_1\sqrt{2C_{\exp}(2\beta_g,\|\Sigma\|_{\mathrm{HS}})}\exp\left(\beta_g e^{B_1T}|x_0|_2\right). \tag*{(112)} C pay ( ∣ x 0 ∣ 2 , ∥Σ ∥ HS ) := G 0 G 1 2 C e x p ( 2 β g , ∥Σ ∥ HS ) exp ( β g e B 1 T ∣ x 0 ∣ 2 ) . (112)
The first derivative bound in (2.5) gives
∣ g ( y ) − g ( x ) ∣ ≤ G 0 G 1 ∣ y − x ∣ 2 ( e β g ∣ x ∣ 2 + e β g ∣ y ∣ 2 ) . |g(y)-g(x)|\le G_0G_1|y-x|_2\left(e^{\beta_g|x|_2}+e^{\beta_g|y|_2}\right). ∣ g ( y ) − g ( x ) ∣ ≤ G 0 G 1 ∣ y − x ∣ 2 ( e β g ∣ x ∣ 2 + e β g ∣ y ∣ 2 ) .
Cauchy–Schwarz and (E.5) imply
∣ I m − I ∣ ≤ G 0 G 1 ∥ X T − X t m h ∥ L 2 [ ( E e 2 β g ∣ X T ∣ 2 ) 1 / 2 + ( E e 2 β g ∣ X t m h ∣ 2 ) 1 / 2 ] ≤ C p a y ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) ∥ X T − X t m h ∥ L 2 . (113) \begin{aligned}
|\mathcal{I}_m-\mathcal{I}|&\le G_0G_1\|X_T-X_{t_m}^h\|_{L^2}\left[\left(\mathbb{E}e^{2\beta_g|X_T|_2}\right)^{1/2}+\left(\mathbb{E}e^{2\beta_g|X_{t_m}^h|_2}\right)^{1/2}\right]\\
&\le C_{\mathrm{pay}}(|x_0|_2,\|\Sigma\|_{\mathrm{HS}})\|X_T-X_{t_m}^h\|_{L^2}. \tag*{(113)}
\end{aligned} ∣ I m − I ∣ ≤ G 0 G 1 ∥ X T − X t m h ∥ L 2 [ ( E e 2 β g ∣ X T ∣ 2 ) 1/2 + ( E e 2 β g ∣ X t m h ∣ 2 ) 1/2 ] ≤ C pay ( ∣ x 0 ∣ 2 , ∥Σ ∥ HS ) ∥ X T − X t m h ∥ L 2 . (113)
Proof of Theorem 3.6. Define
C i n c ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) : = T [ K 0 + B 1 C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) ] + ∥ Σ ∥ H S . (114) C_{\mathrm{inc}}(|x_0|_2,\|\Sigma\|_{\mathrm{HS}}):=\sqrt{T}\left[K_0+B_1C_X(|x_0|_2,\|\Sigma\|_{\mathrm{HS}})\right]+\|\Sigma\|_{\mathrm{HS}}. \tag*{(114)} C inc ( ∣ x 0 ∣ 2 , ∥Σ ∥ HS ) := T [ K 0 + B 1 C X ( ∣ x 0 ∣ 2 , ∥Σ ∥ HS ) ] + ∥Σ ∥ HS . (114)
For s ∈ [ t i , t i + 1 ] s\in[t_i,t_{i+1}] s ∈ [ t i , t i + 1 ] , the integral equation, Itô’s isometry, (E.3), and s − t i ≤ T s-t_i\le T s − t i ≤ T give
∥ X s − X t i ∥ L 2 ≤ ∫ t i s ( K 0 + B 1 ∥ X t ′ ∥ L 2 ) d t ′ + ∥ Σ ∥ H S ( s − t i ) 1 / 2 ≤ C i n c ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) ( s − t i ) 1 / 2 . \begin{aligned}
\|X_s-X_{t_i}\|_{L^2}&\le\int_{t_i}^{s}(K_0+B_1\|X_{t'}\|_{L^2})\,\mathrm{d}t'+\|\Sigma\|_{\mathrm{HS}}(s-t_i)^{1/2}\\
&\le C_{\mathrm{inc}}(|x_0|_2,\|\Sigma\|_{\mathrm{HS}})(s-t_i)^{1/2}.
\end{aligned} ∥ X s − X t i ∥ L 2 ≤ ∫ t i s ( K 0 + B 1 ∥ X t ′ ∥ L 2 ) d t ′ + ∥Σ ∥ HS ( s − t i ) 1/2 ≤ C inc ( ∣ x 0 ∣ 2 , ∥Σ ∥ HS ) ( s − t i ) 1/2 .
Split b ( s , X s ) − b ( t i , X t i ) b(s,X_s)-b(t_i,X_{t_i}) b ( s , X s ) − b ( t i , X t i ) into b ( s , X s ) − b ( s , X t i ) b(s,X_s)-b(s,X_{t_i}) b ( s , X s ) − b ( s , X t i ) and b ( s , X t i ) − b ( t i , X t i ) b(s,X_{t_i})-b(t_i,X_{t_i}) b ( s , X t i ) − b ( t i , X t i ) . The spatial Lipschitz bound and (3.4) then yield
∥ b ( s , X s ) − b ( t i , X t i ) ∥ L 2 ≤ B 1 ∥ X s − X t i ∥ L 2 + L ~ t ( 1 + ∥ X t i ∥ L 2 ) ( s − t i ) 1 / 2 ≤ [ B 1 C i n c ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) + L ~ t ( 1 + C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) ) ] ( s − t i ) 1 / 2 . \begin{aligned}
\|b(s,X_s)-b(t_i,X_{t_i})\|_{L^2}&\le B_1\|X_s-X_{t_i}\|_{L^2}+\widetilde{L}_t(1+\|X_{t_i}\|_{L^2})(s-t_i)^{1/2}\\
&\le\left[B_1C_{\mathrm{inc}}(|x_0|_2,\|\Sigma\|_{\mathrm{HS}})+\widetilde{L}_t(1+C_X(|x_0|_2,\|\Sigma\|_{\mathrm{HS}}))\right](s-t_i)^{1/2}.
\end{aligned} ∥ b ( s , X s ) − b ( t i , X t i ) ∥ L 2 ≤ B 1 ∥ X s − X t i ∥ L 2 + L t ( 1 + ∥ X t i ∥ L 2 ) ( s − t i ) 1/2 ≤ [ B 1 C inc ( ∣ x 0 ∣ 2 , ∥Σ ∥ HS ) + L t ( 1 + C X ( ∣ x 0 ∣ 2 , ∥Σ ∥ HS )) ] ( s − t i ) 1/2 .
Let E i = X t i − X t i h E_i=X_{t_i}-X_{t_i}^h E i = X t i − X t i h . Subtracting the Euler recursion from the integral equation gives
E j = h ∑ i < j [ b ( t i , X t i ) − b ( t i , X t i h ) ] + ∑ i < j ∫ t i t i + 1 [ b ( s , X s ) − b ( t i , X t i ) ] d s . E_j=h\sum_{i<j}\left[b(t_i,X_{t_i})-b(t_i,X_{t_i}^h)\right]+\sum_{i<j}\int_{t_i}^{t_{i+1}}\left[b(s,X_s)-b(t_i,X_{t_i})\right]\,\mathrm{d}s. E j = h i < j ∑ [ b ( t i , X t i ) − b ( t i , X t i h ) ] + i < j ∑ ∫ t i t i + 1 [ b ( s , X s ) − b ( t i , X t i ) ] d s .
Discrete Gronwall applied pathwise implies
max j ≤ m ∣ E j ∣ 2 ≤ e B 1 T ∑ i = 0 m − 1 ∫ t i t i + 1 ∣ b ( s , X s ) − b ( t i , X t i ) ∣ 2 d s . \max_{j\le m}|E_j|_2\le e^{B_1T}\sum_{i=0}^{m-1}\int_{t_i}^{t_{i+1}}|b(s,X_s)-b(t_i,X_{t_i})|_2\,\mathrm{d}s. j ≤ m max ∣ E j ∣ 2 ≤ e B 1 T i = 0 ∑ m − 1 ∫ t i t i + 1 ∣ b ( s , X s ) − b ( t i , X t i ) ∣ 2 d s .
Define
C s t r , 1 / 2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) : = 2 3 e B 1 T T T [ B 1 C i n c ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) + L ~ t ( 1 + C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) ) ] , C_{\mathrm{str},1/2}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}}) := \frac{2}{3}e^{B_1T}T\sqrt{T}\left[B_1C_{\mathrm{inc}}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}})+\widetilde{L}_t\left(1+C_X(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}})\right)\right], C str , 1/2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) := 3 2 e B 1 T T T [ B 1 C inc ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) + L t ( 1 + C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) ) ] ,
C b i a s , 1 / 2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) : = C p a y ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) C s t r , 1 / 2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) . (115) C_{\mathrm{bias},1/2}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}}) := C_{\mathrm{pay}}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}})C_{\mathrm{str},1/2}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}}). \tag*{(115)} C bias , 1/2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) := C pay ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) C str , 1/2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) . (115)
Taking L 2 L^2 L 2 norms and using Minkowski’s inequality gives
∥ max j ≤ m ∣ E j ∣ 2 ∥ L 2 ≤ e B 1 T [ B 1 C i n c ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) + L ~ t ( 1 + C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) ) ] × ∑ i = 0 m − 1 ∫ t i t i + 1 ( s − t i ) 1 / 2 d s = C s t r , 1 / 2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) m − 1 / 2 . \begin{aligned}
\left\lVert\max_{j\le m}|E_j|_2\right\rVert_{L^2}
\le e^{B_1T}\left[B_1C_{\mathrm{inc}}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}})+\widetilde{L}_t\left(1+C_X(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}})\right)\right]
\times\sum_{i=0}^{m-1}\int_{t_i}^{t_{i+1}}(s-t_i)^{1/2}\,\mathrm{d}s \\
&= C_{\mathrm{str},1/2}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}})m^{-1/2}.
\end{aligned} j ≤ m max ∣ E j ∣ 2 L 2 ≤ e B 1 T [ B 1 C inc ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) + L t ( 1 + C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) ) ] × i = 0 ∑ m − 1 ∫ t i t i + 1 ( s − t i ) 1/2 d s = C str , 1/2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) m − 1/2 .
This proves (38) . Applying (E.7) gives ∣ I m − I ∣ ≤ C b i a s , 1 / 2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) m − 1 / 2 \lvert\mathcal{I}_m-\mathcal{I}\rvert\le C_{\mathrm{bias},1/2}(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}})m^{-1/2} ∣ I m − I ∣ ≤ C bias , 1/2 ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) m − 1/2 and proves (39) . Under the additional hypotheses in (ii), the model constants, ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 and L ~ t \widetilde{L}_t L t have common bounds, and (13) gives ∥ Σ ∥ H S 2 ≤ M 2 / 3 3 \lVert\Sigma\rVert_{\mathrm{HS}}^2\le M_{2/3}^3 ∥ Σ ∥ HS 2 ≤ M 2/3 3 , hence ∥ Σ ∥ H S ≤ M 2 / 3 3 / 2 \lVert\Sigma\rVert_{\mathrm{HS}}\le M_{2/3}^{3/2} ∥ Σ ∥ HS ≤ M 2/3 3/2 . The constants in (E.2), (E.4), (E.6), (E.8), and (E.9) are nondecreasing in ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 and ∥ Σ ∥ H S \lVert\Sigma\rVert_{\mathrm{HS}} ∥ Σ ∥ HS . Thus the dimension-uniform constants are obtained by evaluating (E.9) at ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) = ( R 0 , M 2 / 3 3 / 2 ) (\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})=(R_0,M_{2/3}^{3/2}) (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) = ( R 0 , M 2/3 3/2 ) .
Proof of Theorem 3.7. Let E i = X t i − X t i h E_i=X_{t_i}-X^h_{t_i} E i = X t i − X t i h . The additive noise cancels in the error recursion, giving
E i + 1 = E i + h [ b ( t i , X t i ) − b ( t i , X t i h ) ] + R i , (116) E_{i+1}=E_i+h\left[b(t_i,X_{t_i})-b(t_i,X^h_{t_i})\right]+R_i, \tag*{(116)} E i + 1 = E i + h [ b ( t i , X t i ) − b ( t i , X t i h ) ] + R i , (116)
R i = ∫ t i t i + 1 [ b ( s , X s ) − b ( t i , X t i ) ] d s . R_i=\int_{t_i}^{t_{i+1}}\left[b(s,X_s)-b(t_i,X_{t_i})\right]\,\mathrm{d}s. R i = ∫ t i t i + 1 [ b ( s , X s ) − b ( t i , X t i ) ] d s .
Split the integrand in R i R_i R i into b ( s , X s ) − b ( t i , X s ) b(s,X_s)-b(t_i,X_s) b ( s , X s ) − b ( t i , X s ) and b ( t i , X s ) − b ( t i , X t i ) b(t_i,X_s)-b(t_i,X_{t_i}) b ( t i , X s ) − b ( t i , X t i ) . Applying Itô’s formula to the fixed function b ( t i , ⋅ ) b(t_i,\cdot) b ( t i , ⋅ ) and then stochastic Fubini gives R i = A i + M i R_i=A_i+M_i R i = A i + M i , where
A i = ∫ t i t i + 1 [ b ( s , X s ) − b ( t i , X s ) ] d s + ∫ t i t i + 1 ( t i + 1 − t ′ ) ( D x b ( t i , X t ′ ) b ( t ′ , X t ′ ) + 1 2 ∑ r = 1 d w D x 2 b ( t i , X t ′ ) [ Σ e r , Σ e r ] ) d t ′ , A_i=\int_{t_i}^{t_{i+1}}\left[b(s,X_s)-b(t_i,X_s)\right]\,\mathrm{d}s
+\int_{t_i}^{t_{i+1}}(t_{i+1}-t')\left(D_xb(t_i,X_{t'})b(t',X_{t'})+\frac{1}{2}\sum_{r=1}^{d_w}D_x^2b(t_i,X_{t'})[\Sigma e_r,\Sigma e_r]\right)\,\mathrm{d}t', A i = ∫ t i t i + 1 [ b ( s , X s ) − b ( t i , X s ) ] d s + ∫ t i t i + 1 ( t i + 1 − t ′ ) ( D x b ( t i , X t ′ ) b ( t ′ , X t ′ ) + 2 1 r = 1 ∑ d w D x 2 b ( t i , X t ′ ) [ Σ e r , Σ e r ] ) d t ′ ,
M i = ∫ t i t i + 1 ( t i + 1 − t ′ ) D x b ( t i , X t ′ ) Σ d W t ′ . M_i=\int_{t_i}^{t_{i+1}}(t_{i+1}-t')D_xb(t_i,X_{t'})\Sigma\,\mathrm{d}W_{t'}. M i = ∫ t i t i + 1 ( t i + 1 − t ′ ) D x b ( t i , X t ′ ) Σ d W t ′ .
The bounded first and second spatial derivatives and Lemma E.2 justify these formulas by localization; the stochastic integrand is square integrable. The operator-norm bounds give
∥ ∑ r = 1 d w D x 2 b ( t i , X t ′ ) [ Σ e r , Σ e r ] ∥ 2 ≤ B 2 ∥ Σ ∥ H S 2 , (117) \left\lVert\sum_{r=1}^{d_w}D_x^2b(t_i,X_{t'})[\Sigma e_r,\Sigma e_r]\right\rVert_2\le B_2\lVert\Sigma\rVert_{\mathrm{HS}}^2, \tag*{(117)} r = 1 ∑ d w D x 2 b ( t i , X t ′ ) [ Σ e r , Σ e r ] 2 ≤ B 2 ∥ Σ ∥ HS 2 , (117)
∥ D x b ( t i , X t ′ ) Σ ∥ H S 2 ≤ B 1 2 ∥ Σ ∥ H S 2 . (118) \lVert D_xb(t_i,X_{t'})\Sigma\rVert_{\mathrm{HS}}^2\le B_1^2\lVert\Sigma\rVert_{\mathrm{HS}}^2. \tag*{(118)} ∥ D x b ( t i , X t ′ ) Σ ∥ HS 2 ≤ B 1 2 ∥ Σ ∥ HS 2 . (118)
Thus (40) , linear growth of b b b , Minkowski’s inequality, and (E.3) imply the bound below. Define
C A ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) : = 1 2 ( L t + B 1 K 0 + 1 2 B 2 ∥ Σ ∥ H S 2 ) + 1 2 ( L t + B 1 2 ) C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) . (119) C_A(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}}):=\frac{1}{2}\left(L_t+B_1K_0+\frac{1}{2}B_2\lVert\Sigma\rVert_{\mathrm{HS}}^2\right)+\frac{1}{2}(L_t+B_1^2)C_X(|x_0|_2,\lVert\Sigma\rVert_{\mathrm{HS}}). \tag*{(119)} C A ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) := 2 1 ( L t + B 1 K 0 + 2 1 B 2 ∥ Σ ∥ HS 2 ) + 2 1 ( L t + B 1 2 ) C X ( ∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) . (119)
Then
∥ A i ∥ L 2 ≤ h 2 2 ( L t + B 1 K 0 + 1 2 B 2 ∥ Σ ∥ H S 2 ) + h 2 2 ( L t + B 1 2 ) ( E sup t ≤ T ∣ X t ∣ 2 2 ) 1 / 2 ≤ C A ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) h 2 . (120) \lVert A_i\rVert_{L^2} \le\frac{h^2}{2}\left(L_t+B_1K_0+\frac{1}{2}B_2\lVert\Sigma\rVert_{\mathrm{HS}}^2\right)+\frac{h^2}{2}\left(L_t+B_1^2\right)\left(\mathbb{E}\sup_{t\le T}\lvert X_t\rvert_2^2\right)^{1/2}
\le C_A(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})h^2. \tag*{(120)} ∥ A i ∥ L 2 ≤ 2 h 2 ( L t + B 1 K 0 + 2 1 B 2 ∥ Σ ∥ HS 2 ) + 2 h 2 ( L t + B 1 2 ) ( E t ≤ T sup ∣ X t ∣ 2 2 ) 1/2 ≤ C A (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) h 2 . (120)
The partial sums of M i M_i M i form a square-integrable martingale at the grid points. Itô’s isometry, orthogonality of its increments, and (E.12) give
E ∣ ∑ i = 0 m − 1 M i ∣ 2 2 ≤ B 1 2 ∥ Σ ∥ H S 2 ∑ i = 0 m − 1 ∫ t i t i + 1 ( t i + 1 − t ′ ) 2 d t ′ = B 1 2 ∥ Σ ∥ H S 2 T 3 h 2 . \mathbb{E}\left\lvert\sum_{i=0}^{m-1}M_i\right\rvert_2^2\le B_1^2\lVert\Sigma\rVert_{\mathrm{HS}}^2\sum_{i=0}^{m-1}\int_{t_i}^{t_{i+1}}(t_{i+1}-t')^2\,\mathrm{d}t'=\frac{B_1^2\lVert\Sigma\rVert_{\mathrm{HS}}^2T}{3}h^2. E i = 0 ∑ m − 1 M i 2 2 ≤ B 1 2 ∥ Σ ∥ HS 2 i = 0 ∑ m − 1 ∫ t i t i + 1 ( t i + 1 − t ′ ) 2 d t ′ = 3 B 1 2 ∥ Σ ∥ HS 2 T h 2 .
Doob’s inequality therefore yields
∥ max j ≤ m ∣ ∑ i < j M i ∣ 2 ∥ L 2 ≤ 2 B 1 ∥ Σ ∥ H S T 3 h . (121) \left\lVert\max_{j\le m}\left\lvert\sum_{i<j}M_i\right\rvert_2\right\rVert_{L^2}\le2B_1\lVert\Sigma\rVert_{\mathrm{HS}}\sqrt{\frac{T}{3}}\,h. \tag*{(121)} j ≤ m max i < j ∑ M i 2 L 2 ≤ 2 B 1 ∥ Σ ∥ HS 3 T h . (121)
Summing (E.10) and using the spatial Lipschitz bound, discrete Gronwall gives
max j ≤ m ∣ E j ∣ 2 ≤ e B 1 T max j ≤ m ∣ ∑ i < j ( A i + M i ) ∣ 2 . \max_{j\le m}\lvert E_j\rvert_2\le e^{B_1T}\max_{j\le m}\left\lvert\sum_{i<j}(A_i+M_i)\right\rvert_2. j ≤ m max ∣ E j ∣ 2 ≤ e B 1 T j ≤ m max i < j ∑ ( A i + M i ) 2 .
Since the maximum of the partial sums of A i A_i A i is bounded by ∑ i ∣ A i ∣ 2 \sum_i\lvert A_i\rvert_2 ∑ i ∣ A i ∣ 2 , estimates (E.14) and (E.15) give the following choices:
C s t r ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) : = e B 1 T [ T C A ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) + 2 B 1 ∥ Σ ∥ H S T 3 ] , C b i a s ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) : = T C p a y ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) C s t r ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) . (122) \begin{aligned}
C_{\mathrm{str}}(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})&:=e^{B_1T}\left[TC_A(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})+2B_1\lVert\Sigma\rVert_{\mathrm{HS}}\sqrt{\frac{T}{3}}\right],\\
C_{\mathrm{bias}}(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})&:=TC_{\mathrm{pay}}(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})C_{\mathrm{str}}(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}}). \tag*{(122)}
\end{aligned} C str (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) C bias (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) := e B 1 T [ T C A (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) + 2 B 1 ∥ Σ ∥ HS 3 T ] , := T C pay (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) C str (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) . (122)
Indeed,
∥ max j ≤ m ∣ E j ∣ 2 ∥ L 2 ≤ C s t r ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) h . (123) \left\lVert\max_{j\le m}\lvert E_j\rvert_2\right\rVert_{L^2}\le C_{\mathrm{str}}(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})h. \tag*{(123)} j ≤ m max ∣ E j ∣ 2 L 2 ≤ C str (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) h . (123)
Combining (E.17) with (E.7) and h = T / m h=T/m h = T / m gives
∣ I m − I ∣ ≤ C b i a s ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) m − 1 , \lvert\mathcal{I}_m-\mathcal{I}\rvert\le C_{\mathrm{bias}}(\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})m^{-1}, ∣ I m − I ∣ ≤ C bias (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) m − 1 ,
which proves (i).
For (ii), Assumption 2.2 bounds the model constants and ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 uniformly in d x , d w d_x,d_w d x , d w , while Assumption 2.3 and (2.9) give ∥ Σ ∥ H S ≤ M 2 / 3 3 / 2 \lVert\Sigma\rVert_{\mathrm{HS}}\le M_{2/3}^{3/2} ∥ Σ ∥ HS ≤ M 2/3 3/2 . For fixed common model bounds and L t L_t L t , the constants in (E.13) and (E.16) are nondecreasing in ∣ x 0 ∣ 2 \lvert x_0\rvert_2 ∣ x 0 ∣ 2 and ∥ Σ ∥ H S \lVert\Sigma\rVert_{\mathrm{HS}} ∥ Σ ∥ HS . Thus the dimension-uniform constants are obtained by evaluating (E.16) at ( ∣ x 0 ∣ 2 , ∥ Σ ∥ H S ) = ( R 0 , M 2 / 3 3 / 2 ) (\lvert x_0\rvert_2,\lVert\Sigma\rVert_{\mathrm{HS}})=(R_0,M_{2/3}^{3/2}) (∣ x 0 ∣ 2 , ∥ Σ ∥ HS ) = ( R 0 , M 2/3 3/2 ) . □
Acknowledgement The work of Josef Dick was supported in part by a grant of access to OpenAI models through the ChatGPT for Academic Researchers program. The work of Ziyang Ye was supported by the China Scholarship Council program (Project ID: 202606210192).
Declaration of generative AI use The authors used ChatGPT 6 Astra for literature searches, exploratory development, and the preparation of portions of the exposition and LaTeX source. All mathematical arguments, calculations, references, and conclusions were independently checked and verified by the authors, who take full responsibility for the contents of the paper.
Lean 4 formalization. A Lean 4 formalization of Theorem 3.1 , Corollary 3.3 , Theorem 3.6 , and Theorem 3.7 is available at https://github.com/ZiyangYe2000/Lattice4SDE-Lean. The formalization is carried out under Assumptions 2.1, 2.2, and 2.3. It uses Lemmas 2.5 and E.2 , as well as standard stochastic and distributional identities, as external inputs. A complete account of these inputs is provided in the repository blueprint. The project can be checked by running lake build.