Int ro d uct io n to asym pt o tic tech niq ue s fo r sto ... · Int ro d uct io n to asym pt o tic...

36
Introduction to asymptotic techniques for stochastic systems with multiple time-scales Eric Vanden-Eijnden Courant Institute

Transcript of Int ro d uct io n to asym pt o tic tech niq ue s fo r sto ... · Int ro d uct io n to asym pt o tic...

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Introduction to asymptotic techniques forstochastic systems with multiple time-scales

Eric Vanden-Eijnden

Courant Institute

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Motivating examples

Consider the ODE{

X = −Y 3 + sin(πt) + cos(√

2πt) X(0) = x

Y = −ε−1(Y −X) Y (0) = y.(1)

If ε # 1, Y is very fast and it will adjust rapidly to the current valueof X, i.e. we will have

Y = X + O(ε) at all times.

Then the equation for X reduces to

X = −X3 + sin(πt) + cos(√

2πt). (2)

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! " # $ % & ' (!"

!!)&

!

!)&

"

")&

#

#)&

The solution of (1) when ε = 0.05 and we took Xt=0 = 2, Yt=0 = −1.X is shown in blue, and Y in green. Also shown in red is the solutionof the limiting equation (2).

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In contrast, consider the SDE{

X = −Y 3 + sin(πt) + cos(√

2πt), Xt=0 = x

Y = −ε−1(Y −X) + ε−1/2W , Yt=0 = y.(3)

The equation for Y at fixed X = x defines an Ornstein-Uhlenbeckprocess whose equilibrium probability density is

ρ(y|x) =e−(y−x)2

√π

.

The limiting equation is obtained by averaging the right hand-side ofthe equation for X in (3) with respect to this density:

X = −X3 − 32X + sin(πt) + cos(

√2πt), X0 = x. (4)

Note the new term −32α2X due to the noise in (3).

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! " # $ % & ' (!$

!#

!"

!

"

#

$

%

The solution of (3) with Xt=0 = 2, Yt=0 = −1 when ε = 10−3. X isshown in blue, and Y in green. Also shown in red is the solution ofthe limiting equation (4). Notice how noisy Y is.

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Singular perturbations techniques for Markov processes

Consider the system{

X = f(X, Y ), Xt=0 = x ∈ Rn

Y = ε−1g(X, Y ), Yt=0 = y ∈ Rm.(5)

Assume that the equation for Y at fixed X = x defines an Markovprocess which is ergodic for every x with respect to the probabilitydistribution

dµx(y)

If

F (x) =∫

Rm

f(x, y)dµx(y) exists

then in the limit as ε → 0 the evolution for X solution of (5) isgoverned by

X = F (X) X(0) = x. (6)

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Derivation. Let L be the infinitesimal generator of the Markov pro-cess generated by (5)

limt→0+

1

t

(Ex,yφ(Xt, Yt)− φ(x, y)

)= (Lφ)(x, y) (7)

Then L = L0 + ε−1L1, and u(x, y, t) = Ex,yφ(Y, X) satisfies the back-ward Kolmogorov equation

∂u

∂t= L0u + ε−1L1u, u|t=0 = φ (8)

Look for a solution in the form of

u = u0 + εu1 + O(ε2) (9)

so that limε→0 u = u0.

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Inserting (9) into (8) and equating equal powers in ε leads to thehierarchy of equations

L1u0 = 0,

L1u1 =∂u0

∂t− L0u0,

L1u2 = · · ·

(10)

The first equation tells that u0 belong to the null-space of L1. As-suming that for every x, L1 is the generator of an ergodic Markovprocess with equilibrium distribution µx(y), this null-space is spannedby functions constant in y, i.e. u0 = u0(x, t).

Since the null-space of L1 is non-trivial, the next equations eachrequires a solvability condition, namely that their right hand-side be-longs to the range of L1.

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To see what this solvability condition actually is, take the expectationof both sides of the second equation in (10) with respect to dµx(x).This gives

0 =∫

Rm

dµx(y)(∂u0

∂t− L0u0

)(11)

Explicitly, (11) is∂u0

∂t= F (x) ·∇xu0 (12)

where

F (x) =∫

Rm

f(x, y)dµx(y) (13)

(12) is the backward Kolmogorov equation of (6).

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Remark: Computing the expectation with respect to µx(y) in prac-tice. We have

(eL1tφ)(x, y) →∫

Rm

φ(x, y)dµx(y) as t →∞

In other words, if u(x, y, t) satisfies

∂u

∂t= L1u, u|t=0 = φ

so that formally u(x, y, t) = (eL1tφ)(x, y), we have

limt→∞

u(x, y, t) =∫

Rm

φ(x, y)dµx(y)

But since u(x, y, t) = Eyφ(Y x) where

Y x = g(x, Y x)

it follows that∫

Rm

φ(x, y)dµx(y) = limt→∞

Eyφ(Y xt )

= limT→∞

1

T

∫ T

0φ(Y x

t )dt

(14)

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Example: the Lorenz 96 (L96) model

L96 consists of K slow variables Xk coupled to J ×K fast variablesYj,k whose evolution is governed by

Xk = −Xk−1(Xk−2 −Xk+1)−Xk + Fx +hx

J

J∑

j=1

Yj,k

Yj,k =1

ε

(−Yj+1,k(Yj+2,k − Yj−1,k)− Yj,k + hyXk

).

(15)

We will study (15) with Fx = 10, hx = −0.8, hy = 1, K = 9, J = 8,and two values of ε: ε = 1/128 and ε = 1/1024.

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2 3 4 5 6 7 8-5

0

5

10

15

20

-5

0

5

10

15

Fig. 1. Typical time-series of the slow (black line) and fast (grey line) modes; K = 9,J = 8, ε = 1/128. The subplot displays a typical snapshot of the slow and fast modesat a given time.

3.1 Properties of the system and existence of a limiting dynamics

In the parameter setting that we use, the solutions of (19) are chaotic. Typicaltime-series of a slow variable Xk and a fast variable Yj,k in the associated sub-sector are shown in figure 1; the subplot displays a snapshot of the amplitudeof the modes at a given time. The chaotic behavior can be inferred from thehigh sensitivity of the system to perturbations in the initial conditions, andfurther quantified by the statistical tests described next.

The numerical experiments show that the solutions of (19) settle on an attrac-tor. One way to visualize (part of) this attractor is to look at the marginalprobability density functions (PDFs) of the slow variable Xk (any k since thePDFs are all identical by symmetry) shown in figure 2. The mixing characterof the dynamics can be inferred from the decay in time of the auto-correlationfunctions (ACFs) defined as (assuming ergodicity)

Ck,k′(t) = limT→∞

1

T

∫ T

0(Xk(t + s) − X)(Xk′(s) − X)ds, (20)

where

X = limT→∞

1

T

∫ T

0Xkdt, (21)

and similarly for the fast variables – see figure 3. The ACFs of the slow modesXk can be fit with great precision by

Ck,k(t) ≈ C0 cos(ωt)e−νt, (22)

17

Typical time-series of the slow (black line) and fast (grey line) modes;K = 9, J = 8, ε = 1/128. The subplot displays a typical snapshot ofthe slow and fast modes at a given time.

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-10 -5 0 5 10 150

0.025

0.05

0.075

0.1

0.125

Fig. 2. PDF of the slow variable; K = 9, J = 8, black line: ε = 1/128, grey line:ε = 1/1024. The insensitivity in ε of the PDFs indicates that the slow variableshave already converged close to their limiting behavior when ε = 1/128.

with appropriate ν, ω, and C0 ≈ Ck,k(0).

Even though there is a separation of time-scales between the slow evolution ofthe Xk’s and the fast evolution of the Yj,k’s since ε = 1/128, such separationis not obviously apparent from the correlation functions of these modes. Inparticular, figure 3 shows that, after a short transient decay, the correlationfunction of Yj,k decays and oscillates with about the same rate and frequencyas the correlation function of Xk. In fact this short transient decay, whichbecomes shorter and shorter as ε is decreased, is the only signature on theACFs that Yj,k is faster. This feature should be taken as a warning againstsimple procedure to identify fast modes based on computing their correlationtime – here, the correlation time of the Yj,k’s are comparable to the one ofXk and, in particular, independent of ε. In fact, the unambiguous test todetermine if the Y ′

j,ks are fast is to compute their ACFs at fixed X = x (i.e.compute the ACFs of the variables Zj,k’s solution of (23) below). These ACFsdecay on a O(ε)-time-scale.

Next we check the existence of a limiting dynamics for the Xk’s as ε → 0.A necessary condition is that marginal PDFs and correlations functions havea limit as ε → 0. This is consistent with the numerical experiments – seefigures 2 and 3 and compare black and grey lines. This also indicates that thevalue we take, ε = 1/128, is small enough so that the statistical propertiesof the slow variables Xk are very close to their limit. Now, the existence ofa limit for the law of the Xk’s as ε → 0 is necessary but not sufficient inorder that these variables also have a limiting dynamics. For this we need to

18

PDF of the slow variable; K = 9, J = 8, black line: ε = 1/16,grey line: ε = 1/1024. The insensitivity in ε of the PDFs indicatesthat the slow variables have already converged close to their limitingbehavior when ε = 1/16.

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0 5 10 15 20 25 30-5

0

5

10

15

20

0 0.0125 0.025 0.0375 0.053

4

5

6

7

Fig. 3. ACFs of the slow (thick line) and fast (thin line) variables; K = 9, J = 8,black line: ε = 1/128, grey line: ε = 1/1024. The insensitivity in ε of the ACFsfor the slow modes indicates that the slow variables have already converged closeto their limiting behavior when ε = 1/128. The subplot is the zoom-in of the maingraph which shows the transient decay of the ACFs of the fast modes becomingfaster as ε is decreased: this is the only signature in the ACFs of the fact that theYj,k’s are faster.

check the ergodicity of the fast modes at fixed Xk = xk, – i.e. the solution ofthe following equation corresponding to the equation (4) which we use in themicro-solver of the multiscale scheme:

Zj,k(x) =1

ε

(

−Zj+1,k(x)(Zj+2,k(x) − Zj−1,k(x)) − Zj,k(x) + Fy + hyxk

)

. (23)

Figure 4 shows the PDF of

hx

J

J∑

j=1

Zj,k(x) (24)

for some typical values of x. This is the quantity whose average gives theeffective forcing. The PDFs of (24) are robust against variations in initialconditions for Zj,k which confirm the ergodicity of (23). It is however worthnoting how different these PDFs look for different x, which indicates that theback reaction of the slow variables Xk on the fast ones Yj,k is significant inL96. This can also be seen in the time-series shown in figure 1: for some valuesof Xk, the fast variables are locked, whereas they vary widely for other valuesof Xk.

19

ACFs of the slow (thick line) and fast (thin line) variables; ε = 1/128,grey line: ε = 1/1024. The subplot is the zoom-in of the main graphwhich shows the transient decay of the ACFs of the fast modesbecoming faster as ε is decreased: this is the only signature in theACFs of the fact that the Yj,k’s are faster.

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-3 -2.5 -2 -1.5 -1 -0.5 00

1

2

3

4

Fig. 4. Typical PDFs of the coupling term (hx/J)∑J

j=1 Zj,k(x) for various valuesof x. These PDFs are robust against variations in the initial conditions for (23)indicating that the dynamics of the fast modes conditional on the slow ones beingfixed is ergodic. Notice however how different these PDFs look: this indicates thatthe feedback of the slow variables Xk on the fast ones Yj,k is significant in L96.

3.2 Direct-solvers versus the multiscale scheme

For the direct-solver we use the classical fourth-order Runge-Kutta methodwith time-step δt. We need to take δt = 2−11 at most for stability, and atthis value of δt we achieve reasonable accuracy (i.e. eyeball insensitivity ofthe results on the figures under further refinement of δt and changes in initialconditions). Thus, the direct simulation has a cost, taken as the number oftime-steps of the fast variables per unit of time, given by

cost(direct) = !1/δt" = 211 = 2048. (25)

To compute the PDFs and the correlation functions of the slow variables weuse a total window of averaging of T = 218. The PDFs are computed from thetime-series by bin-counting. The correlation functions are computed by directsummation:

Ck,k′(m∆t) =1

M − m

M−m∑

m′=1

Xk(m′∆t)Xk′((m′ + m)∆t) − X2, (26)

where

X =1

M

M∑

m=1

Xk(m∆t), (27)

20

Typical PDFs of the coupling term (hx/J)∑J

j=1 Zj,k(x) for variousvalues of x. These PDFs are robust against variations in the initialconditions indicating that the dynamics of the fast modes conditionalon the slow ones being fixed is ergodic.

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0 5 10 15 20 25 30-5

0

5

10

15

20

-10 -5 0 5 10 150

0.025

0.05

0.075

0.1

0.125

Fig. 5. Comparison between the ACF obtained via the multiscale scheme (blackline) and via the direct-solver with ε = 1/128 (full grey line); K = 9, J = 8. Thecurves are so closed that it is difficult to distinguish them. The subplot displaysthe PDF of the slow mode obtained via the multiscale scheme (black line) andvia the direct-solver with ε = 1/128 (full grey line). Here ∆t = 2−7 = 1/128,N1 = 1, and R = 1. Thus cost(multiscale) = 27 = 128 and the multiscale scheme iscost(direct)/cost(multiscale) = 24 = 16 times more efficient than the direct-solver.Also shown in dashed grey are the corresponding ACF and PDF produced by thetruncated dynamics where the coupling of the slow modes Xk with the fast ones,Yj,k, is artificially switched off. The discrepancy indicates that the effect of the fastmodes on the slow ones is significant in L96.

functions of the slow variables. Figure 5 shows a run with ∆t = 2−7 = 1/128,N1 = 1, and R = 1, for which cost(multiscale) = 27 = 128, and hence the mul-tiscale scheme is cost(direct)/cost(multiscale) = 24 = 16 times more efficientthan the direct-solver. And this happens even though the time series for Xk

that we generate with the multiscale scheme is much smaller than the one wegenerate in the direct simulations, since Xk is sampled every macro-time-step∆t in the former case, and every micro-time-step δt in the latter case. Thissimply means that even though the sample from the direct-solver is much big-ger, it is not more significant statistically due to the large correlation betweenthe slow variables at successive time-steps δt.

3.3 Effective forcing

The results of the last subsection clearly show that the forcing does not needto be computed accurately at each macro-time-step (which is the case sincewe can take R = 1) for the multiscale scheme to apply, as anticipated from

22

Comparison between the ACFs and PDFs; black line: limiting dy-namics; full grey line: ε = 1/128. Also shown in dashed grey are thecorresponding ACF and PDF produced by the truncated dynamicswhere the coupling of the slow modes Xk with the fast ones, Yj,k, isartificially switched off.

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Fig. 7. Black points: scatterplot of the forcing F (x) produced by the multi-scale scheme (R = 4096). Grey points: scatter plot of the bare coupling term(hx/J)

∑Jj=1 Zj,k(x) produced by the direct-solver when ε = 1/128. K = 9,

J = 8. The width of the cloud obtained via the multiscale scheme indicates thatFk(x) ≈ F (xk) is a rather bad approximation. In contrast, the width of the cloudobtained via the direct-solver is more difficult to interpret since it is also due tostatistical fluctuation.

without wasting time evaluating Fk(x) in regions that are not visited by thedynamics anyway). On the other hand, one may think of making additionalassumptions about Fk(x), the simplest of which being that it only depends onthe slow variable xk it corresponds to, i.e. Fk(x) ≈ F (xk) – the next naturalapproximation would be to assume that Fk(x) ≈ F (xk−1, xk) (using the factthat the slow variables sustain wave propagating primarily from left to right),and so on. Testing Fk(x) ≈ F (xk) is elementary since it amounts to verifyingthat the scatter-plot of Fk(X) versus Xk defines a function. Such a scatter-plot is shown in figure 7, which clearly shows that Fk(x) ≈ F (xk) is a badapproximation. Also shown is the scatter-plot of the bare forcing, which is evenwider since (hx/J)

∑Jj=1 Yj,k is (for all practical purposes at least) a random

quantity – the width of the cloud now corresponds to statistical fluctuations in(hx/J)

∑Jj=1 Yj,k which arise independently on whether its conditional average

Fk(x) depends or not on xk only. This indicates that the multiscale scheme isuseful in checking assumptions on the effective forcing which are more difficultto verify from direct numerical simulations due to statistical fluctuations.

24

Black points: scatterplot of the forcing F (x) in the limiting dynamics.Grey points: scatter plot of the bare coupling term (hx/J)

∑Jj=1 Yj,k(x)

when ε = 1/128.

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Diffusive time-scales

Suppose that

F (x) =∫

Rm

f(x, y)dµx(y) = 0. (16)

Then the limiting equation on the O(1) time-scale is trivial, X = 0,and the interesting dynamics arises on the diffusive time-scale O(ε−1).

Consider then{

X = ε−1f(X, Y ), Xt=0 = x ∈ Rn

Y = ε−2g(X, Y ), Yt=0 = y ∈ Rm.(17)

Proceeding as before we arrive at the following limiting equationwhen ε → 0:

X = b(X) + σ(X) Wt, (18)

where

(Lφ)(x) ≡ b(x) ·∇xφ(x) + 12(σσT)(x) : ∇x∇xφ(x)

=∫ ∞

0dt

Rm

dµx(y)f(x, y) ·∇x(Eyf(x, Y x

t ) ·∇xφ(x)) (19)

and

Y x = g(x, Y x)

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Derivation. The backward Kolmogorov equation for u(x, y, t) =Ex,yf(X) is now

∂u

∂t= ε−1L0u + ε−2L1u.

Inserting the expansion u = u0 + εu1 + ε2u2 + O(ε2) (we will have togo one order in ε higher than before) in this equation now gives

L1u0 = 0,

L1u1 = −L0u0,

L1u2 =∂u0

∂t− L0u1,

L1u3 = · · ·

(20)

The first equation tells that u0(x, y, t) = u0(x, t).

The solvability condition for the second equation is satisfied by as-sumption because of (16). Therefore this equation can be formallysolved as

u1 = −L−11 L2u0.

Inserting this expression in the third equation in (20) and consideringthe solvability condition for this equation, we obtain the limitingequation for u0:

∂u0

∂t= Lu0, (21)

where

L =∫

Rm

dµx(y)L0L−11 L0.

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To see what this equation is explicitly, notice that −L−11 g(y) is the

steady state solution of

∂v

∂t= L1v + g(y).

The solution of this equation with the initial condition v(y,0) = 0can be represented by Feynman-Kac formula as

v(y, t) = Ey

∫ t

0g(Y x

s )ds,

Therefore

−L−11 g(y) = Ey

∫ ∞

0g(Y x

t )dt,

and the operator L in the limiting backward Kolmogorov equa-tion (21) is (19).

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Example: the Lorenz 96 (L96) model

Consider

Xk = −ε (Xk−1(Xk−2 −Xk+1) + Xk) +hx

J

J∑

j=1

(Yj,k+1 − Yj,k−1

)

Yj,k =1

ε

(−Yj+1,k(Yj+2,k − Yj−1,k)− Yj,k + Fy

)+ hyXk,

(22)

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0 100 200 300 400 5000

1

2

3

4

5

6

7

-10 -5 0 5 100

0.05

0.1

0.15

0.2

Fig. 14. ACFs and PDFs (subplot) of the slow variable Xk evolving under (57).Grey line: ε = 1/256; full black line: ε = 1/128; dashed black line: ε = 1/128 withtime rescaled as t → 2t consistent with (56). The near perfect match confirms thatevolution of Xk converges to some limiting dynamics on the O(1/ε) time-scale.

is satisfied. Indeed, the conditional measure entering (51) does not depend onx since the equation used in the microsolver is

Zj,k =1

ε(−Zj+1,k(Zj+2,k − Zj−1,k) − Zj,k + Fy) . (58)

In addition the statistics of Zj,k does not depend on k by periodicity andtherefore the conditional averages of Yj,k+1 and Yj,k−1 at x fixed are the same,and the correspond term involving their difference in (57) cancels to leadingorder.

We study (57) by the multiscale scheme described above by performing twosimulations with J = 2, K = 4, Fy = 10, hx = −0.8, Hy = 1, and ε = 1/256and 1/128, and comparing the solution using the proper rescaling of time givenin (56). The results are displayed on figure 14 and show the almost perfectagreement in PDFs and ACFs. The simulation with ε = 1/128 is performedwith a micro-time-step which is twice as big as the one used in the simulationwith ε = 1/256 and therefore corresponds to an efficiency gain ratio of 2.Notice that, in the present situation, the use of the multiscale scheme can bebypassed since the dependency in ε is explicit in (57). But this need not be thecase, and the poor man’s multiscale scheme used here can be straightforwardlygeneralized to systems such as the one considered in section 5 which containhidden slow variables.

38

ACFs and PDFs (subplot) of the slow variable Xk evolving under(22). Grey line: ε = 1/256; full black line: ε = 1/128; dashed blackline: ε = 1/128 with time rescaled as t → 2t. The near perfect matchconfirms that evolution of Xk converges to some limiting dynamicson the O(1/ε) time-scale.

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Coupled truncated Burgers-Hopf (TBH). I. Stable periodic orbits

X1 =1

εb1X2Y1 + aY1(R2 − (X2

1 + X22))− bX2(α + (X2

1 + X22)),

X2 =1

εb2X1Y1 + ax2(R2 − (X2

1 + X22)) + bX1(α + (X2

1 + X22)),

Yk = −Reik

2

p+q+k=0

U∗pU∗

q +1

εb3δ1,kX1X2,

Zk = −Imik

2

p+q+k=0

U∗pU∗

q ,

where Uk = Yk + iZk.

Truncated system: stable periodic orbit (limit cycle)

(X1(t), X2(t)) = R (cosωt, sinωt) with frequency ω = b(α + R2).

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NB: Truncated Burgers (Majda & Timofeyev, 2000)

Fourier-Galerkin truncation of the inviscid Burgers-Hopf equation,ut + 1

2(u2)x = 0:

Uk = −ik

2

k+p+q=0

|p|,|q|≤Λ

U∗pU∗

q , |k| < Λ

Features common with many complex systems. In particular:

• Display deterministic chaos.• Ergodic on E =

∑k |Uk|2.

• Scaling law for the correlation functions with tk ≈ O(k−1).

Here: Used as a model for unresolved modes.Couple truncated Burgers with two resolved variables.

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X1 =1

εb1X2Y1 + aY1(R2 − (X2

1 + X22))− bX2(α + (X2

1 + X22)),

X2 =1

εb2X1Y1 + ax2(R2 − (X2

1 + X22)) + bX1(α + (X2

1 + X22)),

Yk = −Reik

2

p+q+k=0

U∗pU∗

q +1

εb3δ1,kX1X2,

Zk = −Imik

2

p+q+k=0

U∗pU∗

q ,

Limiting SDEs:

X1 = b1b2X1 + N1X1X22 + σ1X2W (t)

+ aX1(R2 − (X21 + X2

2))− bX2(α + (X21 + X2

2)),

X2 = b1b2X2 + N2X2X21 + σ2X1W (t)

+ aX2(R2 − (X21 + X2

2)) + bX1(α + X21 + X2

2)),

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−1 0 1

−1

0

1

(a)

x1

x 2

−1 0 1

−1

0

1

(b)

Contour plots of the joint probability density for the climate variablesX1 and X2; (a) deterministic system with 102 variables; (b) limitSDE. There only remains a ghost of the limit cycle.

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−2 0 20

0.5

1

1.5

2

2.5

3(c)

−2 0 20

0.5

1

1.5

2

2.5

3(d)

−2 0 20

0.5

1

1.5

2

2.5

3(a)

x1

PDF

of x

1

−2 0 20

0.5

1

1.5

2

2.5

3(b)

PDF

of x

1

PDF

of x

2

PDF

of x

2

DNS Reduced model

DNS Reduced model

x1

x2 x2

Marginal PDFs of X1 and X2 for the simulations of the full deter-ministic system with 102 variables (DNS) and the limit SDE.

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0 20 40 60 80−0.4−0.2

00.20.40.60.8

(a)

t

corr

of x

10 20 40 60 80

−0.4−0.2

00.20.40.60.8

(b)

0 20 40 60 80−0.2−0.1

00.10.20.30.4

(c)

0 20 40 60 800.4

0.6

0.8

1

(d)

t

tt

corr

of x

2

cros

s co

rr of

x1, x

2

K 2(t)Two-point statistics for X1 and X2; solid lines - deterministic systemwith 102 degrees of freedom; dashed lines - limit SDE; (a), (b)correlation functions of X1 and X2, respectively; (c) cross-correlationfunction of X1 and X2; (d) normalized correlation of energy,

K2(t) =〈X2

2(t)X22(0)〉

〈X22〉2 + 2〈X2(t)X2(0)〉2

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Coupled truncated Burgers-Hopf (TBH). II. Multiple equilibria

X =1

εb1Y1Z1 + λ(1− αx2)x,

Yk = −Reik

2

p+q+k=0

U∗pU∗

q +1

εb2δ1,kXZk,

Zk = −Imik

2

p+q+k=0

u∗pu∗q +

1

εb3δ1,kXYk,

Limiting SDE:

X = −γX + σW (t) + λ(1− αX2)X

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−2 0 20

0.2

0.4

0.6(a)

x

PDF

of x

−2 0 20

0.2

0.4

0.6(b)

−2 0 20

0.2

0.4

0.6(c)

λ = 1.2 λ = 0.5 λ=0.15

PDF of X for the simulations of the deterministic model (solid lines)and the limit SDE (dashed lines) in three regimes, λ = 1.2, 0.5, 0.15.

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0 5 10 150

0.5

1(a)

t

corr

of x

0 5 10 150.4

0.6

0.8

1

1.2(d)

K(t)

0 5 10 150

0.5

1(b)

0 5 10 150.4

0.6

0.8

1

1.2(e)

0 5 10 150

0.5

1(c)

0 5 10 150.4

0.6

0.8

1

1.2(f)

t

λ =1.2

λ =1.2 λ =0.5

λ =0.5 λ =0.15

λ =0.15

Two-point statistics of X in three regimes, λ = 1.2, 0.5, 0.15 for thedeterministic equations (solid lines) and limit SDE (dashed lines) (a),(b), (c) correlation function of x; (d), (e), (f) correlation of energy,K(t), in x.

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Generalizations

Let Zt ∈ S be the sample path of a continuous-time Markov processwith generator

L = L0 + ε−1L1

and assume that L1 has several ergodic components indexed by x ∈ S′

with equilibrium distribution

µx(z)

Then, as ε → 0 there exists a limiting on S′ with generator

L = EµxL0

Similar results available on diffusive time-scales.

Can be applied to SDEs, Markov chains (i.e. discrete state-space),deterministic systems (periodic or chaotic), etc.

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Other situations with limiting dynamics?

Consider {Xt = f(Xt, Yt),Yt = g(Xt, Yt),

(23)

and denote by ϕ(X[0,t]) the solution of the equation for Y at time tassuming that Xt is known on [0, t]

Observe that ϕ(X[0,t]) is a functional of {Xs, s ∈ [0, t]}.

Then Xt satisfies the closed equation

Xt = f(Xt, ϕ(X[0,t])) (24)

In general, Xt is not Markov!

It becomes Markov when Yt is faster, or ...?

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Other possibility: Weak coupling

The system

Xt =

1

N

N∑

n=1

f(Xt, Ynt ),

Y nt = g(Xt, Y n

t ), (all the Y nt coupled only via Xt)

may have a limit behavior as N → ∞ which is the same as the limitbehavior as

Xt = f(Xt, Yt),

Yt =1

εg(Xt, Yt),

when ε → 0.

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Asymptotic techniques for singularly perturbed Markov processes:

R. Z. Khasminsky, On Stochastic Processes Defined by Differential Equations with aSmall Parameter, Theory Prob. Applications, 11:211–228, 1966.

R. Z. Khasminsky, A Limit Theorem for the Solutions of Differential Equations withRandom Right-Hand Sides, Theory Prob. Applications, 11:390–406, 1966.

T. G. Kurtz, Semigroups of conditioned shifts and approximations of Markov processes,Annals of Probability, 3:618–642, 1975.

G. Papanicolaou, Some probabilistic problems and methods in singular perturbations,Rocky Mountain J. Math, 6:653–673, 1976.

M. I. Freidlin and A. D. Wentzell, Random perturbations of dynamical systems, 2ndedition, Springer-Verlag, 1998.

Effective dynamics in L96:

E. N. Lorenz, Predictability – A problem partly solved, pp. 1–18 in: ECMWF SeminarProceedings on Predictability, Reading, United Kingdom, ECMWF, 1995.

C. Rodenbeck, C. Beck, H. Kantz, Dynamical systems with time scale-separation:averaging, stochastic modeling, and central limit theorems, pp. 187–209 in: Stochas-tic Climate Models, P. Imkeller, J.-S. von Storch eds., Progress in Probability 49,Birkhauser Verlag, Basel, 2001.

I. Fatkullin and E. Vanden-Eijnden, A computational strategy for multiscale systemswith applications to Lorenz 96 model, J. Comp. Phys. 200:605–638, 2004.

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(Coupled) TBH:

A. J. Majda and I. Timofeyev, Remarkable statistical behavior for truncated Burgers-Hopf dynamics, Proc. Nat. Acad. Sci. USA, 97:12413–12417, 2000.

A. J. Majda and I. Timofeyev, Statistical mechanics for truncations of the Burgers-Hopf equation: a model for intrinsic stochastic behavior with scaling, Milan Journalof Mathematics, 70(1):39–96, 2002.

A. J. Majda, I. Timofeyev, and E. Vanden-Eijnden, Systematic strategies for stochasticmode reduction in climate. J. Atmos. Sci., 60(14):1705–1722, 2003.

A. J. Majda, I. Timofeyev, and E. Vanden-Eijnden, Stochastic models for selectedslow variables in large deterministic systems, Nonlinearity, 19:769–794, 2006.