Abstract
We introduce a family of stochastic models motivated by the study of nonequilibrium steady states of fluid equations. These models decompose the deterministic dynamics of interest into fundamental building blocks, i.e., minimal vector fields preserving some fundamental aspects of the original dynamics. Randomness is injected by sequentially following each vector field for a random amount of time. We show under general conditions that these random dynamics possess a unique, ergodic invariant measure and converge almost surely to the original, deterministic model in the small noise limit. We apply our construction to the Lorenz-96 equations, often used in studies of chaos and data assimilation, and Galerkin approximations of the 2D Euler and Navier–Stokes equations. An interesting feature of the models developed is that they apply directly to the conservative dynamics and not just those with excitation and dissipation.
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Notes
See Definition 1.1.
A vector field is complete if its flow curve starting from any point exists for all time.
We use calligraphic \(\mathcal {C}^k\) for k-times continuously differentiable maps throughout to avoid confusion with constants which are often denoted by normal script C (for example, the constants \(C_{jk}\) in 2D Euler).
Throughout this paper analytic means real-analytic.
f(h) is o(g(h)) when \(h \rightarrow 0\) if \(\lim f(h)/g(h)=0\) as \(h \rightarrow 0\). f(h) is O(g(h)) when \(h \rightarrow 0\) if \(\lim |f(h)/g(h)| \in (0,\infty )\).
This equation should be interpreted as an equation on measures or, equivalently, as holding in the weak sense. In other words, the left and right side are equal when integrated against any compactly supported, smooth test function.
As in the proof of Proposition 5.2, the continuity equation is intended here in the weak sense.
Recall that for each index \(k\in \mathbb {Z}_N^2\), we have two real coordinates \(a_k\) and \(b_k\).
Recall a generic point is one with all coordinates nonzero; see Definition 6.4.
Note that the same result can trivially be obtained if \((l,h)\not \in \mathcal A(q)\) setting \(\tau _-^{\iota (m)}=0\).
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Acknowledgements
All authors thank the National Science Foundation grant NSF-DMS-1613337 for partial support during this project. AA also gratefully acknowledges the partial support of NSF-CCF-1934964, and OM also thanks NSF-DMS-2038056 for partial support during this project. JCM thanks David Herzog and Brendan Williamson for discussions at the start of these investigations. JCM thanks the hospitality and support of the Institute for Advanced Study, where this manuscript was completed. We also thank the referees for their insightful comments which improved both the form and the content of this paper.
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Appendices
Appendix A. Convergence Lemmas
1.1 A.1. Semigroups, norms, and bounds
In this subsection we elaborate on the semigroup framework of Sect. 4. The notation and results are used extensively in the proofs of Lemmas 4.2 and 4.6, which are given in Sects. A.2 and A.4, respectively.
Fix a \(\mathcal {V}\)-orbit \(\mathcal {X}\). The \(\mathcal {C}^2\) assumption implies the \(V_k\), which act on functions f via \(V_kf(x)=Df(x)V_k(x)\), are linear operators from \(\mathcal {C}^2(\mathcal {X})\) to \(\mathcal {C}^1(\mathcal {X})\) and from \(\mathcal {C}^1(\mathcal {X})\) to \(\mathcal {C}(\mathcal {X})\). It also implies the semigroups \(\{S_t\}_{t\ge 0}\) and \(\{\widetilde{S}^{(k)}_t\}_{t\ge 0}\) defined in (4.2) and (4.3) are linear operators on \(\mathcal {C}^k(\mathcal {X})\) for \(k\le 2\). Our aim now is to obtain bounds on norms of compositions of these random semigroups. For \(i\le j\) define \(\Phi ^{(i,j)}_{h\tau }:=\varphi ^{(j)}_{h\tau _j}\circ \cdots \circ \varphi ^{(i)}_{h\tau _i}\) and \(\widetilde{S}^{(i,j)}_{h\tau }:=\widetilde{S}^{(i)}_{h\tau }\cdots \widetilde{S}^{(j)}_{h\tau }\). Note \(\widetilde{S}^{(i,j)}_{h\tau }\) acts on functions f via
So for any \(f\in \mathcal {C}(\mathcal {X})\) with \(\Vert f\Vert _\infty =1\), we have
and hence \(\Vert \widetilde{S}^m_{h\tau }\Vert _{0\rightarrow 0}=1\). Next, let \(\varphi =\varphi ^{(k)}\) for arbitrary k. Then
and so
and
In particular, \(\Vert D\varphi _t(x)\Vert \le 1 + C_*\int _0^t \Vert D\varphi _s(x)\Vert ds\) for all x in \(\mathcal {X}\) and Grönwall’s inequality implies
where here and throughout \(C_*\) is the constant from (4.1) corresponding to \(\mathcal {X}\). Similarly, since \(\Vert D^2V\left( D\varphi ,D\varphi \right) \Vert \le \Vert D^2V\Vert \Vert D\varphi \Vert ^2\le C_*\Vert D\varphi \Vert ^2\),
and Grönwall implies
Note (A.1) and (A.2) hold uniformly over all \(\varphi ^{(k)}\). Thus, for \(f\in C^1(\mathcal {X})\) with \(\Vert f\Vert _1=1\),
where the first inequality follows from submultiplicity and the second from (A.1). Similarly,
together with (A.1) and (A.2) gives
Therefore
The above computations prove
Lemma A.1
For any \(h>0\) and \(i\le j\), we have \(\Vert \widetilde{S}^{(i,j)}_{h\tau }\Vert _{0\rightarrow 0}=1\) as well as
In particular, \(\left\Vert \widetilde{S}^{(i,j)}_{h\tau }\right\Vert _{\ell \rightarrow \ell }\le \left( 1+C_*h\sum _{k=i}^j\tau _k\right) e^{3C_*h\sum _{k=i}^j \tau _k}\) for all \(\ell \le 2\).
Note that under the \(\mathcal {C}^2\) assumption \(\widetilde{S}^{(i,j)}_{h\tau }\) can also be regarded as a linear operator from \(\mathcal {C}^2( \mathcal {X})\) to \(\mathcal {C}^1( \mathcal {X})\). So since \(\{f\in \mathcal {C}^2(\mathcal {X}) : \Vert f\Vert _2=1\}\) is a subset of \(\{f\in \mathcal {C}^1(\mathcal {X}) : \Vert f\Vert _1=1\}\), we have
We also have the following corollary of Lemma A.1.
Corollary A.2
Fix \(i\le j\) and set \(m:=j-i+1\). For all \(\ell \le 2\) and polynomial \(p:\mathbb {R}^m_+\rightarrow \mathbb {R}\) there exists \(h_*>0\) such that for all \(h<h_*\),
Proof
Writing \(t=(t_i,\dots ,t_j)\) and \(dt=dt_i\cdots dt_j\), we have
which is finite for all \(h < h_*:=(3C_*)^{-1}\).\(\square \)
1.2 A.2. Proof of Lemma 4.2
We highlight the steps of the proof with italicized font.
Variation of constants. We begin by differentiating \(\widetilde{S}_{h\tau }\) in h:
Next, commute \(\widetilde{S}^{(1,k-1)}_{h\tau }\) and \(V_k\) via \([\widetilde{S}^{(1,k-1)}_{h\tau }, V_k]:=\widetilde{S}^{(1,k-1)}_{h\tau }V_k-V_k\widetilde{S}^{(1,k-1)}_{h\tau }\) to get
where \(V_\tau :=\sum _{k=1}^n \tau _kV_k\) and \(E_{h\tau }:=\sum _{k=1}^n \tau _k[\widetilde{S}^{(1,k-1)}_{h\tau }, V_k]\widetilde{S}^{(k,n)}_{h\tau }\). So, by variation of constants,
Call \(S_{h-r}(V_\tau -V)\widetilde{S}_{r\tau }\) error term 1 and \(S_{h-r}E_{r\tau }\) error term 2. These terms will be treated separately in what follows. First however, we invoke variation of constants again to get an expression for \([\widetilde{S}^{(1,k-1)}_{r\tau }, V_k]\) that will be used to control error term 2. Differentiating in r gives
The second equality follows from commuting \(\widetilde{S}^{(1,j-1)}_{h\tau }\) and \(V_j\) as before, and the third follows from the identity \([XY,Z]=X[Y,Z]+[X,Z]Y\). So, by variation of constants,
Note \(\Vert e^{(r-s)\sum _{j=1}^{k-1}\tau _jV_j}\Vert _{0\rightarrow 0}=1\). So, by Corollary A.2 the integrands above satisfy
and
for some C. Therefore
for some new constant C (we will often absorb arbitrary constants into existing ones).
Error term 1. Rewrite error term 1 as
where \(\mathcal {A}_1\) and \(\mathcal {A}_2\) are the first and second sums in the preceding expression. The second equality is obtained by adding and subtracting the identity I as follows:
Notice \(\widetilde{S}^{(1,k-1)}_{r\tau }\widetilde{S}^{(k+1,n)}_{r\tau }\) does not depend on \(\tau _k\). So, since the \(\tau _i\) are independent with mean 1,
For the second sum, Taylor expanding \(r\mapsto e^{r\tau _kV_k}\) about \(r=0\) with remainder gives
for some \(r_*\in [0,r]\). Therefore
and by Lemma A.1 and Corollary A.2,
for some \(C>0\). Combining Equations (A.8), (A.9), and (A.10) gives
Error term 2. Recall error term 2 is \(S_{h-r}E_{r\tau }:=\sum _{k=1}^n \tau _kS_{h-r}[\widetilde{S}^{(1,k-1)}_{r\tau }, V_k]\widetilde{S}^{(k,n)}_{r\tau }\). So, we have that
Note \([\widetilde{S}^{(1,k-1)}_{r\tau },V_k]\) is independent of \(\tau _k\). So, by (A.7) Corollary A.2,
for some \(C>0\).
Final step. Combining (A.5), (A.11), and (A.12) and absorbing constants into C, we have
\(\square \)
1.3 A.3. Concentration of the sum of exponential random variables
The proof of Lemma 4.6 will itself use two lemmas.
Lemma A.3
Let \(\{\tau _k\}_{k=1}^\infty \) be iid exponential with mean 1. For any \(m\in \mathbb {N}\), \(K>0\) and \(\beta >1\),
Proof
Note if \(\tau \sim \text {Exp}(1)\) then \(\mathbb {E}(e^{\tau /2})=2\). So, by Markov’s inequality and independence,
\(\square \)
Lemma A.4
Let \(\{\tau _k\}_{k=1}^\infty \) be iid exponential with mean 1. For any \(m\in \mathbb {N}\) and \(K\in (0,1)\),
Proof
Fix m. For any \(\gamma \in (0,1)\),
The inequality is Markov’s inequality and the equality immediately after the inequality follows from independence together with \(\mathbb {E}[\exp (\alpha \tau )]=(1-\alpha )^{-1}\) for any \(\alpha \in (-1,1)\). The other steps are all algebraic manipulations. By Taylor’s theorem with remainder there exists \(\gamma _1\in (-\gamma ,0)\) such that
where the inequality follows since \(\gamma _1<0\). Therefore
Similarly,
So combining with the first computation of this proof and taking \(\gamma =K\) gives
\(\square \)
1.4 A.4. Proof of Lemma 4.6
Fix \(t>0\). The argument is similar to that of Lemma 4.2.
Variation of constants. Fix \(m\in \mathbb {N}\). Since \(\widetilde{S}^m_{h\tau }=\exp (h\tau _1V_1)\cdots \exp (h\tau _{mn}V_{mn})\),
where the second equality is obtained by commuting \(\widetilde{S}^{(1,k-1)}_{h\tau }\) and \(V_k\), and the third by replacing \(\tau _k\) with \(\tau _k-1+1\). So, setting \(E_{h\tau }^{(m)}:=\sum _{k=1}^{mn}\tau _k[\widetilde{S}^{(1,k-1)}_{h\tau }, V_k]\widetilde{S}^{(k,mn)}_{h\tau }\), variation of constants implies
Therefore, since \(\Vert S_{m(h-r)}\Vert _{0\rightarrow 0}=1\),
Let \(I_1(h)\) and \(I_2(h)\) denote the first and second integrals, respectively. Then for any \(\varepsilon >0\),
We consider the two probabilities on the right, called the first and second probabilities, separately.
First probability. Note \(\sum _{k=1}^{mn}(\tau _k-1)V_k=\sum _{k=1}^n\sum _{j=1}^m (\tau _j^{(k)}-1)V_k\) where \(\tau ^{(k)}_j:=\tau _{(j-1)n+k}\). So
and together with Lemma A.1 and Equation (A.3),
Therefore
The second inequality follows from a union bound together with the fact that for any nonnegative random variables \(X_k\) and constant c, \(\{\sum _{k=1}^n X_k>c\}\subseteq \cup _{k=1}^n \{X_k>c/n\}\). Set
for arbitrary \(\alpha >0\) and note that
Therefore
Set \(h=t/m^2\). By Lemma A.4 for all \(\varepsilon >0\) such that \(K:=\varepsilon (2C_*tn)^{-1}e^{-C_*n\alpha }<1\),
And by Lemma A.3,
where \(K':=\alpha /t\). Therefore
for some positive constant C independent of m.
Second probability. Recall \(E_{r\tau }^{(m)}:=\sum _{k=1}^{mn}\tau _k[\widetilde{S}^{(1,k-1)}_{r\tau }, V_k]\widetilde{S}^{(k,mn)}_{r\tau }\). Also, from Equation (A.6),
Lemma A.1 together with \(\Vert [V_j,V_k]\Vert _{2\rightarrow 0} \le \Vert V_j\Vert _{1\rightarrow 0}\Vert V_k\Vert _{2\rightarrow 1}+\Vert V_k\Vert _{1\rightarrow 0}\Vert V_j\Vert _{2\rightarrow 1}\le 2C_*^2\) give
Also,
together with Lemma A.1 gives
Therefore for any \(0\le r\le h\),
for some \(C>0\). So, we have that
For arbitrary \(\alpha >0\), set
Then taking \(h=t/m^2\) as before,
for some \(C'>0\) where \(K=(\varepsilon (2t^2C(1+C\alpha )e^{C\alpha })^{-1})^{1/2}\), \(K'=Kn^{-1}\), \(K''=\alpha (nt)^{-1}\), and the second-to-last last inequality follows from Lemma A.3. Combining (A.15), (A.16), and (A.17) and taking \(h=t/m^2\) we therefore have that for all \(\varepsilon \) sufficiently small,
for some constant \(C''>0\) independent of m. So, we have that
\(\square \)
Appendix B. Controllability Lemmas
Combining the partial results obtained above we show the existence of transformations implementing the steps listed at the beginning of the section:
Lemma B.1
If \(q^{(0)}\) in \(\mathcal {Q}_0\) is nondegenerate, then there exists \(M_1\) and a sequence of transition times and interaction triples \(\{ \iota (m),\tau (m)\}_{m = 1}^{M_1}\) such that \(\Phi _{\tau (M_1)}^{\iota (M_1)}\circ \dots \circ \Phi _{\tau (1)}^{\iota (1)} (q^{(0)}) = q^{(1)}\) as in (6.17).
Proof
If (6.17) is satisfied by \(q^{(0)}\) we simply set \(M_1 = 0\), \(q^{(1)} = q^{(0)}\). If not, by nondegeneracy there exists a sequence of triples \(\{\iota (m)\}_{m=1}^{M}\) with \(\iota (m) = {\varvec{j}}(m){\varvec{k}}(m){\varvec{\ell }}(m)\) such that \(\mathcal A_0 := \mathcal A(q^{(0)})\) and \( \mathcal A_m = \mathcal A_{m-1} \oplus {\varvec{\ell }}(m)\) with \(\{(0,1,+),(1,0,+),(j^*,-)\}\subset \mathcal A_{M}\). We notice that all steps of this procedure satisfy, upon possibly reordering the indices within each triple, either the conditions of Lemma 6.11 (b) or of Lemma 6.12, so we sequentially choose \(\tau (m) = \tau _+^{\iota (m)}\) from those lemmas.
To activate coordinate \((1,1,-)\) – if this was not already done in the previous procedure – we start with component \(b_{j^*} \ne 0\) for \(|j^*|\ne 1\) and consider a nearest neighbors path \(\{\ell (n)\}_{n=1}^{M'}\) in \(\mathbb Z_N^2\) connecting \(j^*\) to (1, 1) without performing any step on the axes. It is easy to see that such path can be realized through repeated application of Lemma 6.11 (b) by choosing for the n-th step the triples \(\iota (n) = (0,1,+)(\ell (n),-)(\ell (n)\pm (0,1),-)\) or \(\iota (n) = (1,0,+)(\ell (n),-)(\ell (n)\pm (1,0),-)\) for vertical and horizontal steps respectively.
Finally, coordinates \((1,0,-)\) and \((0,1,-)\) can be activated by applying Lemma 6.13 to the triples \((1,0,-)(0,1,+)(1,1,-)\) and \((1,0,+)(0,1,-)(1,1,-)\) respectively, while \((1,1,+)\) is activated by (b) by interchanging the type of modes \((1,1,-)\) and \((1,0,+)\) (or \((0,1,+)\)) in \(\iota (M')\) from the previous paragraph to \((1,1,+)\) and \((1,0,-)\) (or \((0,1,-)\)).\(\square \)
Lemma B.2
Let \(q^{(1)}\) be a nondegenerate point in \(\mathcal {Q}_0\) satisfying (6.17). Then there exists \(M_2\) and a sequence of interacting triples and transition times \(\{\iota (m),\tau (m)\}_{m = 1}^{M_2}\) such that \(\Phi _{\tau (M_2)}^{\iota (M_2)}\circ \dots \circ \Phi _{\tau (1)}^{\iota (1)} (q^{(1)}) = q^{(2)}\) is a nondegenerate point in \(\mathcal {Q}_0\) satisfying (6.18) and (6.19).
Proof
In this part of the proof, we only consider interactions involving triples \(\iota (m)\) of the form
By Lemma 6.11 (a), if \(|j|<|k|<|\ell |\) and \((0,1),(l,h) \in \mathcal A(q)\) there exists \(\tau (m) = \tau _-^{\iota (m)}\) such that defining \(\mathcal A_m = \mathcal A(\varphi ^{\iota (m)}_{\tau (m)}(q))\) we have \((l,h) \not \in \mathcal A_m\) and \((0,1) \in \mathcal A_m\) (and similarly for (1, 0)).Footnote 10 Note that while a triple as above satisfies by assumption that \(|j|<|k|<|\ell |\) and at least two of its coordinates are nonvanishing, it does not, in general, satisfy (6.24). However, assuming that q does not satisfy (6.24), by Lemma 6.12 and setting \(\iota ' = (1,0)(0,1)(1,1)\), there exists \(\tau ^{\iota '}\) such that \( |q_{(1,0)}| \ne |(\Phi _{\tau ^{\iota '}}^{\iota '}(q))_{(1,0)}| >0\). Since none of the coordinates in \(\mathbb Z_N^2\setminus \{(1,0)(0,1)(1,1)\}\) are affected by this operation, \((\Phi _{\tau ^{\iota '}}^{\iota '}(q))\) satisfies (6.24) and Lemma 6.11 can be applied to this state.
To conclude the proof we identify a sequence of triples \(\iota (m) = (j(m),k(m),\ell (m))\in \mathcal I\) of the form (B.1) such that for \(\mathcal A_0 = \mathcal A(q^{(1)}) \subseteq \mathbb Z_N^2\times \{+,-\}\)
A possible such sequence is given by triples of the form
to remove the vertical column of \(\mathbb Z_N^2\) (which cannot interact with (0, 1)), followed by
where importantly the set of transitions for each l is ordered. The above transformation zeroes all coefficients except those in the set \(\{(1,1),(0,1),(1,0)\}\cup \{(l,N)~:~l \in (-N,\dots , N)\}\). We further remove the coefficients from \(\{(l,N)~:~l \in (-N+1,\dots , N-1)\}\) by sequentially applying Lemma 6.11 to the ordered sequence of interacting triples
and then
It is easy to check that each transition in the above construction sequentially satisfies the assumptions of Lemma 6.11 (a), and that once a mode has been removed from \(\mathcal A\) it will not interact again in this procedure. The fact that (6.19) holds follows from (6.17) and that in an interacting triple \(\iota = {\varvec{j} \varvec{k} \varvec{\ell }}\) with \(|j|<|k|<|l|\) both modes \({\varvec{j}}\) and \({\varvec{\ell }}\) are in \(\mathcal A\) at the end of the interaction by \(\tau _-^\iota \).\(\square \)
Lemma B.3
Let \(q^{(2)}\) be a nondegenerate point in \(\mathcal {Q}_0\) satisfying (6.18) and (6.19). Then there exists \(M_3\) and a sequence of interacting triples and transition times \(\{\iota (m),\tau (m)\}_{m = 1}^{M_3}\) such that \(\Phi _{\tau (M_3)}^{\iota (M_3)}\circ \dots \circ \Phi _{\tau (1)}^{\iota (1)} (q^{(2)}) = q^{(3)}\) is a nondegenerate point in \(\mathcal {Q}_0\) satisfying (6.20) and (6.21).
Since it may not be possible to “transfer” the content of e.g., mode \((-N,N)\) to \((-N+1,N)\) through one single interaction with mode (1, 0) – and therefore it won’t be possible to transfer the amplitude of mode \((-N,N)\) to (N, N) in one single “pass” – we proceed to prove that, through a sequence of interactions, we can transfer a finite and \(q_{(-N,N)}\)-independent amount of energy from mode \((-N,N)\) to (N, N). Therefore, the transfer of amplitude from mode \((-N,N)\) to (N, N) may be accomplished by repeating this sequence of interactions sufficiently many times.
The following corollary of Lemma 6.12 will be instrumental for the proof of Lemma B.3:
Corollary B.4
Let \(q_{(1,1)}, b_{{(1,1)}} \ne 0\) then for any \(q,q'\) with \(q_{\varvec{j}}=q_{\varvec{j}}'\) for all \(|j|>1\) there exist a sequence \(\{\iota (m), \tau (m)\}_{m=1}^4\) such that \(\Phi _{\tau (4)}^{\iota (4)} \circ \dots \circ \Phi _{\tau (1)}^{\iota (1)} (q) = q'\).
Proof of Lemma B.3
The desired result follows upon showing that for any \(i \in \{-N,\dots ,N\}\), setting \({\varvec{\ell }}= (-i,N,\chi ), {\varvec{\ell }}' = {(i,N,\chi ')}\) for \(\chi , \chi ' \in \{-,+\}\) there exists \(M_{{\varvec{\ell }}, {\varvec{\ell }}'}\) and a sequence of triples and interaction times \(\{\iota (m)\), \(\tau (m)\}_{m = 1}^{M_{{\varvec{\ell }}, {\varvec{\ell }}'}}\) such that for any q satisfying \(\bigcup _{|i'| < i}\{(i',N,+),{(i',N,-)}\} \cap \mathcal A(q) = \emptyset \) and \(q' = \Phi _{\tau (M_{{\varvec{\ell }}, {\varvec{\ell }}'})}^{\iota (M_{{\varvec{\ell }}, {\varvec{\ell }}'})}\circ \dots \circ \Phi _{\tau (1)}^{\iota (1)}(q)\) we have
and for \({\varvec{k}}\in \{{\varvec{\ell }}, {\varvec{\ell }}'\}\), \(\text {sign}(q_{\varvec{k}}) = \text {sign}(q_{\varvec{k}}')\) holds if \(q_{\varvec{k}}' \ne 0\) (recalling our choice of notation \(\text {sign}(0)=+1\)). Indeed, if \(\text {sign}(b_{{(N,N)}})\ge 0\) we sequentially apply the above result to the pairs
Otherwise, when \(\text {sign}(b_{{(N,N)}})=-1\) we first apply the above result to \({\varvec{\ell }}={(N,N,-)}\), \({\varvec{\ell }}'={(-N,N,-)}\) and then proceed as in the previous case.
We prove the result above by induction on \(i \in \{0,\dots ,N\}\). The proof for \(i \le 0\) is analogous.
Base case (\(i=0: (0,N,\chi )\rightarrow (0,N,\chi ')\)): If \({\varvec{\ell }}= {\varvec{\ell }}'\) there is nothing to show. We proceed to consider the case \({\varvec{\ell }}= (0,N,+)\), \({\varvec{\ell }}'={(0,N,-)}\), as the converse follows by analogous arguments. In this case, for a sufficiently small \(\varepsilon >0\) we consider the interactions \(\iota = (1,0,+)(0,N,+)(1,N,+)\) and \(\iota '= {(1,0,-)}{(0,N,-)}(1,N,+)\), running the corresponding flow maps by a small amount of time \(\tau (\varepsilon )\), \(\tau '(\varepsilon )\) such that \((\Phi _{\tau '(\varepsilon )}^{\iota '} \circ \Phi _{\tau (\varepsilon )}^\iota (q)_{{(0,N,-)}})^2 = b_{{(0,N)}}^2+\varepsilon \). We then apply Corollary B.4 to the coordinates \((1,0,+),{(1,0,-)}\) to return them in the initial configuration. Note that the existence of a uniform \(\varepsilon >0\) such that the transitions above can be performed in a single pair of interactions (and therefore the finiteness of the total number of interactions required to perform the desired transformation) follows from the fact that \(b_{{(0,N)}}\) is nondecreasing and the continuity of the dynamics together with Lemma 6.11.
Induction step (\(i>0: (-i,N,\chi )\rightarrow (i,N,\chi ')\)): We consider two possibilities for q: a) there exists \(q''\) with \(|a_{(1,0)}''| \in [|a_{(1,0)}|/2,|a_{(1,0)}| ]\), \(q_{(-i,N,\chi )}''=0\) and for \(\iota '' = (1,0,+)(-i+1,N,\chi )(-i,N,\chi )\)
or b) such \(q''\) does not exist.
In case a) the state \(q''\) can be reached by letting \(\iota = (1,0,+)(-i+1,N,\chi )(-i,N,\chi )\) interact for a finite amount of time \(\tau \) from Lemma 6.11 (c). Then, by the induction assumption there is a sequence of triples and interaction times allowing to reach a state \(q'''\) with \(q_{(-i+1,N,\chi )}''' = 0\), \(q_{(i-1,N,\chi ')}''' = q_{(-i+1,N,\chi )}''\) and \(q_{\varvec{j}}''' = q_{\varvec{j}}''\) for all other \(j \in \mathbb Z_N^2\). The desired state can then be reached by application of Lemma 6.11 (a) to the triple \(\iota = (1,0,+)(i-1,N,\chi ')(i,N,\chi ')\) . We proceed to check that the final state satisfies (B.2). Because modes \(j \not \in \{(-i,N), \dots , (i,N), (1,0)\}\) did not interact in the procedure above for such \({\varvec{j}}\) we must have that \(q_{\varvec{j}}= q_{\varvec{j}}'\). The fact that for \(j \in \{(-i,N), \dots , (i-1,N)\) \(q_{\varvec{j}}' = 0\) follows by construction and the induction assumption. It remains to check that \(|a_{(1,0)}'| = |a_{(1,0)}|\). Since the only modes affected by the above transformation are \((-i,N,\chi ),(i,N\chi '),(1,0,+)\), this follows directly by conservation of energy and enstrophy:
In case b) we proceed to show that case a) can be reached with a finite number of interactions. More specifically if condition a) is not satisfied we let the triple \(\iota '' = (-i,N,\chi )(-i+1,N, \chi )(1,0, +)\) for \(\chi \in \{+,-\}\) interact as described by Lemma 6.11 for a time \(\tau ''\) to reach a nondegenerate point \(q''\) in \(\mathcal {Q}_0\) with \(q_{\varvec{j}}'' = q_{\varvec{j}}\) for \({\varvec{j}}\not \in \{(-i,N, \chi ),(-i+1,N,\chi ),(1,0,+)\}\), \(a_{(1,0)}'' = a_{(1,0)}/2\) and \(q_{(-i,N,\chi )}'',q_{(-i+1,N,\chi )}''\) satisfying the conservation laws
so that \( (q_{(-i,N,\chi )}'')^2 = (q_{(-i,N,\chi )})^2 - C_{N,i} (q_{(1,0)})^2 \) for \(C_{N,i} = \frac{3}{4} \frac{N^2+i^2}{i^2-(i-1)^2} ( N^2+(i-1)^2-1)\). We see that a positive, \(q_{(1,0,+)}\)-dependent amplitude is removed from \((q_{(-i,N,\chi )})^2\). Again applying the induction step and Lemma 6.11 (a) to transfer, respectively, the amplitude from \({(-i+1,N,\chi )}\) to \({(i-1,N, \chi ')}\) and from \({(i-1,N,\chi ')}\) to \({(i,N,\chi ')}\) we reach the state \(q'\) with \(q_{\varvec{j}}= q_{\varvec{j}}'\) for modes \(j \not \in \{(-i,N), \dots , (i,N), (1,0)\}\) (since these modes either vanish in both cases or they did not interact). Further, by conservation of energy and enstrophy, we have that
so that \(|q_{(1,0,+)}''| = |q_{(1,0,+)}|\). This shows that the amplitude \(C_{N,i} (q_{(1,0,+)})^2\) subtracted to \(q_{(-i,N,\chi )}\) is constant at each cycle, showing by boundedness of \(q_{(-i,N,\chi )}\) that with a finite number of iterations as the one described above we can reach state a), concluding the proof.\(\square \)
Lemma B.5
Let \(q^{(3)}\) be a nondegenerate point in \(\mathcal {Q}_0\) satisfying (6.20) and (6.21). Then there exists \(M_4\) and a sequence of interacting triples and transition times \(\{\iota (m),\tau (m)\}_{m = 1}^{M_4}\) such that \(\Phi _{\tau (M_4)}^{\iota (M_4)}\circ \dots \circ \Phi _{\tau (1)}^{\iota (1)} (q^{(3)}) = q^*\) is a nondegenerate point in \(\mathcal {Q}_0\) satisfying (6.15).
Proof
We start the proof by applying Corollary B.4 to transform the state \(q^{(3)}\) into \(q = \Phi _{\tau (1)}(q^{(3)})\) satisfying \(q_{\varvec{j}}^{(3)} = q_{\varvec{j}}\) for all \(|j|>1\) and \(a_{(0,1)}=b_{{(0,1)}}=b_{{(1,0})}=a_{(1,0)}>0\). Throughout this proof, we refer to states q such that \(q_{(i,i',\chi )} = q_{(i',i,\chi )}\) for all \(i,i' \in (0,\dots , N)\), \(\chi \in \{+,-\}\) as symmetric.
We then proceed to transfer the amplitude from \(a_{(1,1)}\) to \(b_{(2,1)}, b_{(1,2)}\) by transforming q into another symmetric state \(q'\) with \({(2,1,-)}, {(1,2,-)} \in \mathcal A(q')\) and \((1,1,+) \not \in \mathcal A(q')\). This can be done by letting triples \(\iota (2) = {(1,0,-)}(1,1,+){(2,1,-)}\in \mathcal I\) and \(\iota (3) = {(0,1,-)}(1,1,+){(1,2,-)}\in \mathcal I\) interact, and choosing the interaction times \(\tau , \tau '(\tau )\) such that \(\Phi _{\tau '(\tau )}^{\iota (3)}\circ \Phi _{\tau }^{\iota (2)}(q)_{(1,1 ,+)}=0\). Further, we note that the difference \(b_{{(1,2)}}'-b_{{(2,1)}}'\) is negative for \(\tau =0\), positive for \(\tau '(\tau )=0\) and is continuous in \(\tau \), so there must exist \(\tau ^*\) such that \(b_{{(1,2)}}'=b_{{(2,1)}}'\). To show that \(q'\) is symmetric it only remains to show that \(b_{{(1,0)}}' = b_{{(0,1)}}'\). This follows from the conservation laws:
where
Next, we let the triples \(\iota (4) = (1,0,-)(0,1,+)(1,1,-)\) and \(\iota (5) = (0,1,-)(1,0,+)(1,1,-)\) interact. By Lemma 6.12 there exists an interaction time such that the initial state \(q'\) is mapped to \(q''\) with \(b_{{(1,0)}}'' = b_{{(0,1)}}'' = 0\) and \(a_{{(1,0)}}'' = a_{{(0,1)}}'' > 0\), so that \({(1,0,-)}, {(0,1,-)}\not \in \mathcal A(q'')\).
We then proceed to transfer the amplitude from modes \({(1,2,-)}\) and \({(2,1,-)}\) to \({(2,2,-)}\). This is done letting triples \(\iota (6) = (1,0,+){(1,2,-)}{(2,2,-)}\) and \(\iota (7) = (0,1,+){(2,1,-)}{(2,2,-)}\) interact until the modes \({(2,1,-)},{(1,2,-)}\) are depleted, as proved in Lemma 6.11. The symmetry of the final state \(q'''\) is again a consequence of the conservation laws:
Summarizing, we have reached a symmetric state \(q''' = \Phi _{\tau (7)}^{\iota (7)}\circ \dots \circ \Phi _{\tau (2)}^{\iota (2)}(q)\) with
The desired result then follows immediately if we can show that we can transfer the amplitude of mode \((i-1,i-1,-)\) to \((i,i,-)\) for \(i\in (2,\dots , N)\) while preserving the fact that \(a_{(1,0)}' = a_{(0,1)}'\). We show this by considering, sequentially, the interaction triples
More specifically, we consider the family of endpoints
where \(\tau _-^{\iota }\) is defined in Lemma 6.11 (a). By construction, this sequence implies that \(a_{(i-1,i-1)}''= a_{(i-1,i)}''= a_{(i,i-1)}''=0\) and \(a_{(i,i)}''\ne 0\). It remains to prove that \(a_{(1,0)}'' = a_{(0,1)}''\). As a composition of continuous functions, \(q''(t)\) is continuous in t and therefore so is \(\Delta q(t) = a_{(1,0)}''(t) - a_{(0,1)}''(t)\). Further, since by symmetry \(a_{(1,0)}''(0) = a_{(0,1)}''(\tau _-^{\iota (4i)})\), we must have \(\textrm{sign}( \Delta q(0)) = -\textrm{sign}(\Delta q(\tau _-^{\iota _1})) \). This implies the existence of \(\tau (4i) \in [0,\tau _-^{\iota _1}]\) with \(\Delta q(0)=0\), concluding the proof.\(\square \)
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Agazzi, A., Mattingly, J.C. & Melikechi, O. Random Splitting of Fluid Models: Unique Ergodicity and Convergence. Commun. Math. Phys. 401, 497–549 (2023). https://doi.org/10.1007/s00220-023-04645-5
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DOI: https://doi.org/10.1007/s00220-023-04645-5