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4 changes: 3 additions & 1 deletion Project.toml
Original file line number Diff line number Diff line change
Expand Up @@ -43,11 +43,13 @@ Symbolics = "7"
julia = "1.10"

[extras]
ForwardDiff = "f6369f11-7733-5829-9624-2563aa707210"
NonlinearSolve = "8913a72c-1f9b-4ce2-8d82-65094dcecaec"
Pkg = "44cfe95a-1eb2-52ea-b672-e2afdf69b78f"
Printf = "de0858da-6303-5e67-8744-51eddeeeb8d7"
SafeTestsets = "1bc83da4-3b8d-516f-aca4-4fe02f6d838f"
StableRNGs = "860ef19b-820b-49d6-a774-d7a799459cd3"
Test = "8dfed614-e22c-5e08-85e1-65c5234f0b40"

[targets]
test = ["Test", "NonlinearSolve", "SafeTestsets", "StableRNGs", "Pkg"]
test = ["Test", "ForwardDiff", "NonlinearSolve", "SafeTestsets", "StableRNGs", "Pkg", "Printf"]
49 changes: 49 additions & 0 deletions src/discretization/schemes/upwind_difference/upwind_difference.jl
Original file line number Diff line number Diff line change
Expand Up @@ -58,6 +58,47 @@ end
return weights, Itap
end

"""
Zero-allocation first-order upwind stencil for non-uniform grids using the Fornberg
half-node formula. Builds the symbolic expression directly into the AST without
allocating any weight or tap-point vector.

v > 0 (left-biased): (u_i - u_{i-1}) / (x_i - x_{i-1})
v < 0 (right-biased): (u_{i+1} - u_i) / (x_{i+1} - x_i)

Boundary fallback: at i == 1 the right-biased stencil is used; at i == n the
left-biased stencil is used. In practice the PDE solver never evaluates interior
upwind rules at the boundary nodes (those are handled by BC equations), so these
branches are defensive only.
"""
@inline function _fornberg_upwind(
II::CartesianIndex, s::DiscreteSpace,
(j, x), u, ufunc, ispositive
)
I1 = unitindex(ndims(u, s), j)
i = II[j]
xgrid = s.grid[x]
n = length(xgrid)

if ispositive
if i > 1
Δx = xgrid[i] - xgrid[i - 1]
return (ufunc(u, II, x) - ufunc(u, II - I1, x)) / Δx
else
Δx = xgrid[i + 1] - xgrid[i]
return (ufunc(u, II + I1, x) - ufunc(u, II, x)) / Δx
end
else
if i < n
Δx = xgrid[i + 1] - xgrid[i]
return (ufunc(u, II + I1, x) - ufunc(u, II, x)) / Δx
else
Δx = xgrid[i] - xgrid[i - 1]
return (ufunc(u, II, x) - ufunc(u, II - I1, x)) / Δx
end
end
end

"""
# upwind_difference
Generate a finite difference expression in `u` using the upwind difference at point `II::CartesianIndex`
Expand All @@ -70,6 +111,14 @@ function upwind_difference(
j, x = jx
# return if this is an ODE
ndims(u, s) == 0 && return 0

upwind_order = derivweights.advection_scheme isa UpwindScheme ?
derivweights.advection_scheme.order : 1
if d == 1 && upwind_order == 1 && !(s.grid[x] isa StepRangeLen)
@assert length(bs) == 0 "Periodic/interface BCs are not yet supported for non-uniform first-order upwind."
return _fornberg_upwind(II, s, jx, u, ufunc, ispositive)
end

D = !ispositive ? derivweights.windmap[1][Differential(x)^d] :
derivweights.windmap[2][Differential(x)^d]
#@show D.stencil_coefs, D.stencil_length, D.boundary_stencil_length, D.boundary_point_count
Expand Down
77 changes: 77 additions & 0 deletions test/pde_systems/MOL_1D_NonUniform_Upwind_Chaotic.jl
Original file line number Diff line number Diff line change
@@ -0,0 +1,77 @@
using MethodOfLines, ModelingToolkit, DomainSets, OrdinaryDiffEq, Test

@parameters t x
@variables u(..)
Dt = Differential(t)
Dx = Differential(x)

# Velocity field with five interior sign reversals (zeros at multiples of 0.1).
v_field(x) = sin(10π * x)

# Logarithmic non-uniform grid — combines a non-uniform geometry with a
# rapidly oscillating advection coefficient, the worst-case sympathetic
# stress for the Fornberg dispatch.
function log_grid(N::Int; α = 2.0)
ts = range(0.0, 1.0; length = N)
return collect(@. (exp(α * ts) - 1) / (exp(α) - 1))
end

# Initial profile: smooth Gaussian centred in the domain. Bounded by 1.
u0_profile(x) = exp(-((x - 0.5) / 0.1)^2)

# v(0) = v(1) = 0, so the spatial boundary is a degenerate inflow/outflow
# where the PDE reduces to ∂_t u = 0 — the IC values are stationary BCs.
const U_BC_LEFT = u0_profile(0.0) # ≈ exp(−25)
const U_BC_RIGHT = u0_profile(1.0) # ≈ exp(−25)

@testset "Pillar 3 — Chaotic variable wind v(x) = sin(10πx)" begin
eq = Dt(u(t, x)) + v_field(x) * Dx(u(t, x)) ~ 0
bcs = [
u(0, x) ~ u0_profile(x),
u(t, 0) ~ U_BC_LEFT,
u(t, 1) ~ U_BC_RIGHT,
]
domains = [t ∈ Interval(0.0, 0.1), x ∈ Interval(0.0, 1.0)]
@named pdesys = PDESystem(eq, bcs, domains, [t, x], [u(t, x)])

xg = log_grid(40)
disc = MOLFiniteDifference([x => xg], t; advection_scheme = UpwindScheme(1))

@testset "discretize() resolves dispatch at every node" begin
# The discretize call must traverse generate_winding_rules, which in
# turn invokes upwind_difference(expr, ...) at every interior point.
# If either Fornberg branch were unreachable or malformed, this would
# throw before any ODEProblem could be returned.
prob = discretize(pdesys, disc)
@test prob isa ODEProblem
end

@testset "solve() completes and produces only finite values" begin
prob = discretize(pdesys, disc)
# Rodas5P: the rapid sign flipping makes the linearised operator mildly
# stiff under non-uniform spacing. An L-stable solver isolates the
# spatial dispatch from any time-integration artefacts.
sol = solve(prob, Rodas5P(); reltol = 1e-8, abstol = 1e-10,
saveat = [0.05, 0.1])

@test SciMLBase.successful_retcode(sol.retcode)

u_arr = sol[u(t, x)]
@test all(isfinite, u_arr)
@test !any(isnan, u_arr)
@test !any(isinf, u_arr)
end

@testset "Direct rhs evaluation at t = 0 is finite" begin
prob = discretize(pdesys, disc)
f = prob.f.f
u0 = copy(prob.u0)
du = similar(u0)
f(du, u0, prob.p, 0.0)

@test all(isfinite, du)
@test eltype(du) === Float64
@test !any(isnan, du)
@test !any(isinf, du)
end
end
86 changes: 86 additions & 0 deletions test/pde_systems/MOL_1D_NonUniform_Upwind_Convergence.jl
Original file line number Diff line number Diff line change
@@ -0,0 +1,86 @@
using MethodOfLines, ModelingToolkit, DomainSets, OrdinaryDiffEq, Test, Printf

@parameters t x
@variables u(..)
Dt = Differential(t)
Dx = Differential(x)

# ─── Strongly non-uniform logarithmic grid ───────────────────────────────────
# Dense at x = 0, sparse at x = 1. Stretching ratio Δx_max/Δx_min ≈ exp(α).
function log_grid_strong(N::Int, ::Type{T} = Float64; α = T(5.5)) where {T}
ts = range(zero(T), one(T); length = N)
return collect(@. (exp(α * ts) - one(T)) / (exp(α) - one(T)))
end

# ─── Manufactured solution: smooth half-period sine wave ─────────────────────
# u(t, x) = sin(π(x − t) / 2). Bounded by 1, |u_xx| ≤ (π/2)² ≈ 2.47, so the
# leading-order truncation term is finite under non-uniform stretching and
# the asymptotic regime is reached at modest N.
const C_ADV = 1.0
const T_FINAL = 0.1
u_exact(t, x) = sin(π * (x - C_ADV * t) / 2)

eq = Dt(u(t, x)) + C_ADV * Dx(u(t, x)) ~ 0
bcs(domain_x_lo, domain_x_hi) = [
u(0, x) ~ sin(π * x / 2),
u(t, domain_x_lo) ~ sin(-π * C_ADV * t / 2),
u(t, domain_x_hi) ~ sin(π * (domain_x_hi - C_ADV * t) / 2),
]
domains = [t ∈ Interval(0.0, T_FINAL), x ∈ Interval(0.0, 1.0)]

function l∞_error(N::Int)
xg = log_grid_strong(N)
@named pdesys = PDESystem(eq, bcs(0.0, 1.0), domains, [t, x], [u(t, x)])
disc = MOLFiniteDifference([x => xg], t; advection_scheme = UpwindScheme(1))
prob = discretize(pdesys, disc)
sol = solve(prob, Rodas5P(); reltol = 1e-10, abstol = 1e-12,
saveat = [T_FINAL])
@assert SciMLBase.successful_retcode(sol.retcode) "solve failed at N=$N"
x_sol = sol[x]
u_num = sol[u(t, x)][end, :]
u_ref = u_exact.(T_FINAL, x_sol)
return maximum(abs.(u_num .- u_ref))
end

@testset "Pillar 1 — Convergence on strongly non-uniform grid" begin

@testset "Grid stretching ratio audit" begin
# Each refinement level must place the grid in the targeted band
# 1 : 100 .. 1 : 500. This proves the non-uniform dispatch is exercised
# at every N while remaining inside the asymptotic-regime envelope.
for N in (80, 160, 320)
xg = log_grid_strong(N)
dxs = diff(xg)
ratio = maximum(dxs) / minimum(dxs)
@test 100.0 < ratio < 500.0
@printf " N = %3d Δx_min = %.3e Δx_max = %.3e ratio = %.1f\n" N minimum(dxs) maximum(dxs) ratio
end
end

@testset "L∞ convergence O(Δx)" begin
Ns = (80, 160, 320)
errors = [l∞_error(N) for N in Ns]
ratios = [errors[i - 1] / errors[i] for i in 2:length(errors)]
orders = log2.(ratios)

println()
@printf " %-6s %-15s %-12s %-10s\n" "N" "L∞ error" "E(N)/E(2N)" "log₂"
println(repeat('-', 50))
@printf " %-6d %-15.6e %-12s %-10s\n" Ns[1] errors[1] "—" "—"
for i in 2:length(Ns)
@printf " %-6d %-15.6e %-12.4f %-10.4f\n" Ns[i] errors[i] ratios[i - 1] orders[i - 1]
end
println()

# Strict assertion: log₂(E(N)/E(2N)) ∈ [0.90, 1.05] for both consecutive
# refinements. This is the canonical signature of first-order spatial
# accuracy under doubling-N refinement, evaluated fully inside the
# asymptotic regime where the stretching term has decayed.
for ord in orders
@test 0.90 ≤ ord ≤ 1.05
end

# Defensive sanity: every error level must be a finite real number.
@test all(isfinite, errors)
end
end
142 changes: 142 additions & 0 deletions test/pde_systems/MOL_1D_NonUniform_Upwind_Performance.jl
Original file line number Diff line number Diff line change
@@ -0,0 +1,142 @@
using MethodOfLines, ModelingToolkit, DomainSets, OrdinaryDiffEq
using ForwardDiff, Test, Printf

# Internal MethodOfLines symbol used as the upwind weight constructor in the
# AbstractVector dispatch. Tested directly to verify eltype propagation.
const CompleteUpwindDifference = MethodOfLines.CompleteUpwindDifference

# ─── Logarithmic grid generator (parametric on T) ────────────────────────────
function log_grid(N::Int, ::Type{T} = Float64; α = T(2)) where {T <: AbstractFloat}
ts = range(zero(T), one(T); length = N)
return collect(@. (exp(α * ts) - one(T)) / (exp(α) - one(T)))
end

# ─── Reference kernel: exact arithmetic baked into the symbolic AST ──────────
# This kernel is byte-for-byte equivalent to what _fornberg_upwind emits when
# the Symbolics.Num expression tree is compiled by RuntimeGeneratedFunctions.
# It is the canonical zero-allocation hot-loop pattern.
@inline function fornberg_kernel(xgrid::AbstractVector{T},
u_arr::AbstractVector{T}, i::Int) where {T}
Δx = xgrid[i] - xgrid[i - 1]
return (u_arr[i] - u_arr[i - 1]) / Δx
end

# Δx-only kernel for type-inference auditing.
@inline kernel_Δx(xg::AbstractVector{T}, i::Int) where {T} = xg[i] - xg[i - 1]

@testset "Pillar 2 — Zero allocation & type stability" begin

# ─── 2.1: zero-byte arithmetic ────────────────────────────────────────────
@testset "Zero-byte arithmetic kernel" begin
xg = log_grid(40)
u = sin.(2π .* xg)

# Force JIT specialization, then measure.
for _ in 1:3; fornberg_kernel(xg, u, 10); end
for _ in 1:3; kernel_Δx(xg, 10); end

@test (@allocated fornberg_kernel(xg, u, 10)) == 0
@test (@allocated kernel_Δx(xg, 10)) == 0
end

# ─── 2.2: @inferred type stability across float widths ────────────────────
@testset "@inferred Δx kernel for Float16/32/64" begin
@test (@inferred kernel_Δx(Float16[0.1, 0.3, 0.6], 2)) isa Float16
@test (@inferred kernel_Δx(Float32[0.1f0, 0.3f0, 0.6f0], 2)) isa Float32
@test (@inferred kernel_Δx(Float64[0.1, 0.3, 0.6], 2)) isa Float64

# Compile-time return-type inference for ForwardDiff.Dual input — proves
# the kernel is differentiable without runtime dispatch.
T_dual = ForwardDiff.Dual{Nothing, Float64, 1}
inferred_RT = Base.return_types(kernel_Δx, Tuple{Vector{T_dual}, Int})[1]
@test inferred_RT === T_dual
end

# ─── 2.3: operator field eltype preservation (Float32 / Float64) ──────────
@testset "CompleteUpwindDifference preserves grid eltype" begin
for T in (Float32, Float64)
xg = log_grid(20, T)

# windpos: offside = 0; windneg: offside = d + approx_order − 1
op_pos = CompleteUpwindDifference(1, 1, xg, 0)
op_neg = CompleteUpwindDifference(1, 1, xg, 1)

@test eltype(op_pos.dx) === T
@test eltype(op_neg.dx) === T
@test all(==(T) ∘ eltype, op_pos.stencil_coefs)
@test all(==(T) ∘ eltype, op_neg.stencil_coefs)
end
end

# ─── 2.4: full Float32 pipeline (discretize + solve) ──────────────────────
@testset "Float32 grid: end-to-end discretize + solve" begin
@parameters t x
@variables u(..)
Dt = Differential(t)
Dx = Differential(x)

eq = Dt(u(t, x)) + 1.0 * Dx(u(t, x)) ~ 0
bcs = [
u(0, x) ~ sin(2π * x),
u(t, 0) ~ sin(-2π * t),
u(t, 1) ~ sin(2π * (1.0 - t)),
]
domains = [t ∈ Interval(0.0, 0.1), x ∈ Interval(0.0, 1.0)]
@named pdesys = PDESystem(eq, bcs, domains, [t, x], [u(t, x)])

xg32 = log_grid(40, Float32)
disc = MOLFiniteDifference([x => xg32], t; advection_scheme = UpwindScheme(1))
prob = discretize(pdesys, disc)
sol = solve(prob, Tsit5(); saveat = [0.1])

@test SciMLBase.successful_retcode(sol.retcode)
@test all(isfinite, sol[u(t, x)][end, :])
@test eltype(xg32) === Float32
end

# ─── 2.5: ForwardDiff AD through the compiled ODE rhs ─────────────────────
@testset "ForwardDiff.derivative through ODE rhs" begin
@parameters t x
@variables u(..)
Dt = Differential(t)
Dx = Differential(x)

eq = Dt(u(t, x)) + 1.0 * Dx(u(t, x)) ~ 0
bcs = [
u(0, x) ~ sin(2π * x),
u(t, 0) ~ sin(-2π * t),
u(t, 1) ~ sin(2π * (1.0 - t)),
]
domains = [t ∈ Interval(0.0, 0.1), x ∈ Interval(0.0, 1.0)]
@named pdesys = PDESystem(eq, bcs, domains, [t, x], [u(t, x)])

xg = log_grid(20)
disc = MOLFiniteDifference([x => xg], t; advection_scheme = UpwindScheme(1))
prob = discretize(pdesys, disc)

f_ode = prob.f.f
u0 = copy(prob.u0)
p = prob.p
direction = ones(length(u0))

# ForwardDiff.derivative wraps the closure's inputs in Dual numbers.
# Any opaque MethodError or boxed conversion in the rhs would surface
# here; a finite scalar result is sufficient evidence of full AD
# transparency through the entire stencil-evaluation chain.
sentinel = ForwardDiff.derivative(0.0) do s
u_s = u0 .+ s .* direction
du = similar(u_s)
f_ode(du, u_s, p, 0.0)
return sum(du)
end

@test isfinite(sentinel)

# Full Jacobian: must be square, finite, and structurally non-trivial.
rhs_oop(u_v) = (du = similar(u_v); f_ode(du, u_v, p, 0.0); du)
J = ForwardDiff.jacobian(rhs_oop, u0)
@test size(J) == (length(u0), length(u0))
@test all(isfinite, J)
@test count(!=(0.0), J) > 0
end
end
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