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Scaled trajectory limit: weak-field geodesics converge to the Newtonian system, with rate O(epsilon) for identical initial data

Statement

Let (Ω,K,L,C,ε0,φ,r) be stationary weak-field data with spatial base U=π(Ω), compact K⊆U, spatial potential Φ=εc2φ and c>0 (Stationary weak-field data: the diagonal ansatz, its bounds, stationarity and the Einstein-family condition), let ε∗ and C2 be the threshold and constant of Uniform Christoffel-symbol bounds for stationary weak-field data, let S∗>0 and 0<ε≤ε∗, and put Tε:=LS∗/(εc), UL:={X∈R3:LX∈U}, and ψ(X):=φ(LX) for X∈UL.

Equip each R3 here with the Euclidean inner product ⟨X,Y⟩=∑i=13XiYi and norm ∥X∥2=⟨X,X⟩ (The Euclidean inner product ⟨x,y⟩=∑k<nxkyk on Rn). In the standard coordinates, ∇ψ=(∂X1ψ,∂X2ψ,∂X3ψ) (The Jacobian matrix of partial derivatives and the gradient in the scalar-valued case); write D2ψ:=D(∇ψ) for its derivative and ∥D2ψ(X)∥op:=sup⁡∥v∥2=1∥D2ψ(X)v∥2.

Suppose:

  • (H1) there is an affinely parametrized geodesic of g(ε) admitting a C2 reparametrization γε by t=x0/c on [0,Tε], with dt/ds≠0 in its affine parameter s, whose length-coordinate components are γε(t)=(ct,xε(t))∈Ω, with spatial trajectory xε(t)∈K and ∣x˙ε(t)∣≤Cεc for every such t;
  • (H2) setting t(S):=LS/(εc), Xε(S):=xε(t(S))/L and Wε(S):=x˙ε(t(S))/(εc) for S∈[0,S∗], and letting K′⊆UL be a compact convex set containing every Xε(S), there is a C1 map (X∗,W∗):[0,S∗]→R3×R3 with X∗([0,S∗])⊆K′ and

X∗′(S)=W∗(S),W∗′(S)=−∇ψ(X∗(S))(0≤S≤S∗);

  • (H3) ∥D2ψ(X)∥op≤K2 for every X∈K′, where K2≥0.

Then for every S∈[0,S∗], with D(S):=∥Xε(S)−X∗(S)∥2+∥Wε(S)−W∗(S)∥2,

D(S)≤(D(0)+C3εS∗) e(1+K2)S∗,

where C3 depends only on C, L and the dimension. Consequently the following hold.

(i) Convergence. If D(0)→0 as ε↓0 along the family, then sup⁡0≤S≤S∗D(S)→0.

(ii) Rate for identical data. If D(0)=0, then sup⁡0≤S≤S∗D(S)≤C3εS∗e(1+K2)S∗=O(ε).

(iii) Long coordinate times. The coordinate-time horizon is Tε=LS∗/(εc), so the fixed scaled interval [0,S∗] corresponds to coordinate times growing like ε−1/2; the limit statement is therefore not a large-t statement at fixed ε.

Facts & Assumptions

Given: Stationary weak-field data, a geodesic trajectory xε satisfying (H1), the scaled variables of (H2), a C1 solution (X∗,W∗) of the Newtonian system and the constant K2 of (H3).

[L1]

At each spacetime point of γε whose spatial coordinate lies in K and for 0<ε≤ε∗, the coordinate-time acceleration satisfies ∣x¨εi+∂iΦ(xε)∣≤Caccc2ε2/L for i=1,2,3, where Cacc is the constant named C3 in that supplier (Coordinate-time acceleration of weak-field geodesics: the Newtonian leading term with uniform error clause (b)).

[L2]

If g:[a,b]→R3 is continuous on [a,b], differentiable on (a,b), and ∥g′(t)∥2≤M on (a,b), then ∥g(b)−g(a)∥2≤M(b−a) (The mean value inequality: if f:[a,b]→Rm is continuous and differentiable on (a,b) with ∥f′∥2≤M, then ∥f(b)−f(a)∥2≤M(b−a)).

[L3]

Gronwall's inequality: if u,a,b are continuous on [0,S∗] with u,b≥0 and u(S)≤a(S)+∫0Sb(s′)u(s′) ds′, and if a is nondecreasing, then u(S)≤a(S)exp⁡(∫0Sb) for all S (Gronwall's integral inequality with variable and constant coefficients).

Proof

technique · direct; write the geodesic equation in scaled variables, compare with the Newtonian system, then apply Gronwall's inequality to the summed discrepancy
1.1L1L4algebra

(Scaled equation for the geodesic.) Differentiating Xε(S)=xε(t(S))/L and Wε(S)=x˙ε(t(S))/(εc) with dt/dS=L/(εc) gives Xε′=Wε and Wε′=x¨εL/(εc2). By [L1] and ∇xΦ=εc2∇xφ=εc2L−1∇Xψ, Wε′=−∇Xψ(Xε)+Rε,∣Rε∣≤C3ε, with C3 depending only on C and L: each component error is at most Caccε by [L1], so its Euclidean norm is at most 3Caccε. Choose C3≥3Cacc.

1.2given

(Newtonian system.) By (H2), X∗′=W∗ and W∗′=−∇ψ(X∗) on [0,S∗].

1.3L2L4givenalgebra

(Lipschitz bound for the force.) Fix S and write a=X∗(S), b=Xε(S). If a=b the bound is immediate. Otherwise set g(t):=∇ψ(a+t(b−a)) for 0≤t≤1; the segment lies in K′ by convexity, and ψ is C2 on the open set UL containing K′. Thus g is continuous on [0,1], differentiable on (0,1), and g′(t)=D2ψ(a+t(b−a))(b−a), so (H3) gives ∥g′(t)∥2≤K2∥b−a∥2. Apply [L2] to obtain ∥∇ψ(Xε(S))−∇ψ(X∗(S))∥2≤K2∥Xε(S)−X∗(S)∥2.

2.1step 1.1step 1.2step 1.3L3algebra

(Integral inequality and Gronwall.) By steps 1.1 and 1.2, for every S∈[0,S∗], D(S)≤D(0)+∫0S(∥Wε−W∗∥2+∥∇ψ(Xε)−∇ψ(X∗)∥2+∥Rε∥2) dS′≤D(0)+C3εS+(1+K2)∫0SD(S′) dS′, where step 1.3 bounds the force term by K2∥Xε−X∗∥2≤K2D and the velocity term by D. The function a(S):=D(0)+C3εS is nondecreasing and b:=1+K2 is constant, so [L3] gives D(S)≤a(S)e(1+K2)S≤(D(0)+C3εS∗)e(1+K2)S∗.

3.1step 2.1givenalgebra∎

(Consequences and conclusion.) The displayed estimate is the main claim; (i) and (ii) follow by inserting D(0)→0 respectively D(0)=0 and recalling that C3, K2 and S∗ are fixed in the limit, while (iii) is the identity Tε=LS∗/(εc).

Remarks

  • What the limit is. The statement is a two-sequence comparison: a family of geodesics of the metrics g(ε) with data scaled as in (H1)-(H2), and a solution of the Newtonian comparison system. It is not a statement that general relativity reduces to Newtonian mechanics, nor a statement about any particular physical system.
  • The exponential factor. The bound grows like e(1+K2)S∗: on fixed scaled intervals it is uniform in ε, but it degrades as the scaled interval or the field gradient grows. No global-in-time limit is asserted.

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