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4.3 Amplitude Equations

As discussed in the previous chapters, a linear stability analysis reveals that the unselective state z(x) = 0 becomes unstable for r ≥ 0 and modes on the critical circle |k|= kc start to grow. Directly after spontaneous symmetry breaking, when |z(x)|is still small compared to its asymptotic value reached at t→ ∞, the nonlinearity N3[z]can be neglected and the dynamics is controlled by the linear terms. As shown in Chapter 3 the emerging pattern can then be approximated by a random superposition of modes and its statistics is expected to be Gaussian.

What can we tell about the dynamics at later times when the nonlinearities become important and the modes start to compete? In particular, what can we say about the attractors? For small values of the control parameterr �1, i.e. in theweakly nonlinear regime, solutions to the full dynamics can be approximated by planforms,

z(x) =N−1

j=0

Ajeikjx, |kj|=kc,

consisting of a linear superposition of discrete modes on the critical circle. Thereby the full dynamics Eq.(4.2) of the field z(x) is projected onto the finite dimensional subspace spanned by the amplitudes Aj resulting in amplitude equations, a set of coupled nonlinear differential equations describing the dynamics of the amplitudes Aj. Here we derive the amplitude equations for the dynamics Eq.(4.2). In the subsequent sections we then perform a stability analysis of their stationary solutions in order to identify sets of stable patterns. The perturbation theoretical analysis presented follows the treatise of [58] and [34].

The spectrum of L0 is given by λ(k) =−(kc2k2)2 and attains its maximum at k=|kc|, where it is zero. Therefore, modes on the critical circle reside in the kernel of the linear operator L0. Since one is interested in the dynamics in a small neighbourhood above the bifurcation point r = 0one introduces a small parameter γ ≥0 and assumes that the solutionz(x, t) andr can both be expanded into a power series in γ,

r = r1γ+r2γ2+r3γ3+. . .

z(x, t) = z1(x, t)γ+z2(x, t)γ2+z3(x, t)γ3+. . . . (4.7) In general this will be the case when the solution z(x, t) bifurcates from the homogeneous state in a continuous way. Note that the intrinsic time scale τ = r−1 diverges at the bifurcation point, which means that forr→0 the dynamics ofz(x, t) is becoming arbitrarily slow, a phenomenon which is known as critical slowing down and which can be compensated by considering the dynamics on a slow time scale,

T =r t.

Expressed in rescaled time units the dynamics Eq.(4.2) becomes r

∂Tz(x) =F[z(x)] (4.8)

and no longer exhibits any critical slowing down. We combine the ansatz (4.7) with the rescaled

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dynamics Eq.(4.8) and obtain

0 = L0zr∂Tz+rz+r�Mz¯+N3[z]

= γ(L0z1) +γ2(r1z1+L0z2r1Tz1+r1�Mz¯1) + (4.9) +γ3(L0z3+r1z2+r2z1r1Tz2r2Tz1+r1�Mz¯2+r2�Mz¯1+N3(z1, z1,z¯1)) +

4(L0z4+r1z3+r2z2+r3z1r1Tz3r2Tz2r3Tz1+r1�Mz¯3+r2�Mz¯2+r3�Mz¯1 + +N3(z2, z1,z¯1) +N3(z1, z2,z¯1) +N3(z1, z1,z¯3))

5(L0z5+. . .) +. . .

Equation (4.9) can only be fulfilled when the terms inside the brackets vanish for every order in γ. This implies conditions of the form

L0zi =r.h.s. (4.10)

wherei denotes the order of the term and the right hand side only depends on zj with j < i.

The set of equations (4.10) can be solved in ascending order when the solvability conditions are met, i.e. when the right hand side is orthogonal to the kernel of the adjoint operator L0 . In our case L0 is formally self-adjoint and the kernels ofL0 and L0 are identical. For the first order in γ we have the condition

L0z1= 0

which implies thatz1(x, T)∈kerL0. The kernel ofL0 is spanned by all Fourier modeseikcx on the critical circle (and by the secular terms kcxeikcx, which are unbounded and thus irrelevant in our present context). The second order term yields to

L0z2 =r1(−z1+Tz1�Mz¯1)

from which we conclude that r1 = 0, which is the only way to fulfill the compatibility condition, since the term in the brackets resides in the kernel of L0. The compatibility condition applied to the third order term

L0z3=−r2z1+r2Tz1r2�Mz¯1+N3(z1, z1,z¯1) yields a dynamical equation forz1,

Tz1 =z1+�Mz¯1PcN3(z1, z1,z¯1) (4.11) where we setr2 = 1andPc is the projection operator onto the kernel ofL0. The planform ansatz

z1(x) =2n1

j=0

Aj(T)eikjx,

which consists of a superposition on 2n modes kj = kc(cosαj,sinαj) on the critical circle, where we require that to each mode also its antiparallel mode is in the set, in combination with Eq.(4.11), yields a set ofamplitude equations

A˙j =Aj+�e4iαjA¯j+

k,l,m

AkAlA¯me−ikjxPjN3(eikkx, eiklx, e−ikmx) (4.12)

4.3 Amplitude Equations where Pj denotes the projection onto the Fourier modeeikj and j denotes the index of the mode antiparallel to modej with the corresponding wavevectorkj=−kj.

Next we show that many terms in the triple sum of Eq.(4.12) do not contribute due to symmetry.

As a result, the general form of the amplitude equations can be reduced to A˙j =Aj+�A¯j−e4iαj

2n−1 k=0

gjk|Ak|2Aj

2n−1 k=0

fjkAkAkA¯j− (4.13) with real valued and symmetric matricesgjkandfjk which determine the coupling and competition between modes. They can be expressed in terms of angle-dependent interaction functions g(α) and f(α), which are obtained from the nonlinearityN3[z](cf.[58, 30, 22]).

Due to the projection operatorPj only termsN3(eikkx, eiklx, eikmx) are contributing in which the wave vectors add up to kj, i.e.

kk+klkm =kj.

Since all wave vectors have the same length this condition requires kk=kj, kl=km

or

kk=km, kl =kj

or

kk=−kl:=kl−, km =−kj :=kj

such that Eq.(4.12) becomes

A˙j = Aj +�e4iαjA¯j+

k�=j

Aj|Ak|2e−ikjxPjN3(eikjx, eikkx, e−ikkx) +

+

k�=j

Aj|Ak|2eikjxPjN3(eikkx, eikjx, eikkx) +

+

k�=j,j

AkAkA¯je−ikjxPjN3(e−ikkx, eikkx, eikjx) +Aj|Aj|2eikjxPjN3(eikjx, eikjx, eikjx)

which can be brought into the form of Eq.(4.13) by setting

gjk = −eikjxPjN3(eikjx, eikkx, eikkx) +eikjxPjN3(eikkx, eikjx, eikkx) fjk = −1

2

e−ikjxPjN3(e−ikkx, eikkx, eikjx) +e−ikjxPjN3(eikkx, e−ikkx, eikjx)

forj �=kand

gjj = −eikjxPjN3(eikjx, eikjx, eikjx) fjj = 0

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for the diagonal elements. For an isotropic system, which we assume here, the matrix elements gjk and fjk only depend on the angle difference α = |αkαj| of the Fourier modes kj = kc(cosαj,sinαj). Therefore they can be expressed in terms of the continuous functions

g(α) =eik0xP N3(eik0x, eih(α)x, eih(α)x) +eik0xP N3(eih(α)x, eik0x, eih(α)x)(4.14) f(α) = −1

2

e−ik0xP N3(e−ih(α)x, eih(α)x, eik0x) +e−ik0xP N3(eih(α)x, e−ih(α)x, eik0x)

wherek0=kc(1,0)andh(α) =kc(cosα,sinα). From the definition (4.14) follows thatg(α) = g(α+2π)andf(α) =f(α+π). However, for the particular nonlinearity considered here, Eq.(4.5),

g(α) =g(α+π), (4.15)

which is due to the fact thatN3[z]belongs to the class ofpermutation symmetric models satisfying N3(zj, zk, zl) =N3(zl, zj, zk) (see[22]). The coupling coefficients are given by

gjk = (1−1

2δjk)g(|αkαj|) (4.16) and

fjk = (1−δjkδjk)f(|αkαj|). (4.17) For the nonlinearity Eq.(4.5) one obtains

g(α) =g+ (2−g)e(α) (4.18)

and

f(α) = 1

2g(α) (4.19)

withe(α) = 2 exp(σ2kc2) cosh(σ2k2ccosα).

The amplitude equations can be derived from the energy functional

E = −

2n−1 j=0

AjA¯j+�(AjAj−e−4iαj+ ¯AjA¯j−e4iαj) (4.20)

+1 2

2n−1 j=0

2n−1 k=0

gjk|Aj|2|Ak|2+fjkAjAjA¯kA¯k

and written as a gradient descent

A˙j =−δE δA¯j

In the following sections we identify classes of stationary solutions of the amplitude equations (4.13) and determine their stability criteria.