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. 2022 Sep 26;85(4):41. doi: 10.1007/s00285-022-01793-5

Scaling relations for auxin waves

Bente Hilde Bakker 1, Timothy E Faver 2, Hermen Jan Hupkes 1,, Roeland M H Merks 3, Jelle van der Voort 1
PMCID: PMC9512763  PMID: 36163567

Abstract

We analyze an ‘up-the-gradient’ model for the formation of transport channels of the phytohormone auxin, through auxin-mediated polarization of the PIN1 auxin transporter. We show that this model admits a family of travelling wave solutions that is parameterized by the height of the auxin-pulse. We uncover scaling relations for the speed and width of these waves and verify these rigorous results with numerical computations. In addition, we provide explicit expressions for the leading-order wave profiles, which allows the influence of the biological parameters in the problem to be readily identified. Our proofs are based on a generalization of the scaling principle developed by Friesecke and Pego to construct pulse solutions to the classic Fermi–Pasta–Ulam–Tsingou model, which describes a one-dimensional chain of coupled nonlinear springs.

Supplementary Information

The online version contains supplementary material available at 10.1007/s00285-022-01793-5.

Keywords: Travelling waves, Polar auxin transport, Up-the-gradient models, Scaling limits, Cross-diffusion, Lattice differential equations

Introduction

Polar auxin transport

The phytohormone auxin is a central player in practically all aspects of the development and growth of plants, for example in phyllotaxis, root development and the initiation of lateral roots, the formation of vascular tissues in stems, the patterning of leaf veins, and flower development (Paque and Weijers 2016). The pattern formation principles underlying these developmental mechanisms have been uncovered to a large part through an intensive cross-talk between experimental approaches and mathematical modeling (Shi and Vernoux 2018; Autran et al. 2021; Cieslak et al. 2021). Auxin is transported between cells and between cells and the cell walls both through diffusion and through transport proteins that are localized at the plasma membrane (PM). Some of these transport proteins, mostly notably several members of the PIN-FORMED family including PIN1 (Adamowski and Friml 2015) are distributed in a polarised manner inside the cells. Such polarised localisation of PINs is coordinated in plant tissue, leading to a directed transport of auxin through plant tissues in a mechanism called polar auxin transport (PAT) (Adamowski and Friml 2015). For example, in fully developed seed plants, auxin is synthesized in leaves, then is transported through the central tissues of the stem and the root towards the root tips, where it redirected along the superficial tissues of the root back to towards the stem and recycled towards the internal tissues of the root (Adamowski and Friml 2015).

Despite new details being uncovered incessantly (see e.g. Verna et al. 2019; Hajný et al. 2020), it is still incompletely understood what mechanisms drive the polarization of PINs inside cells and the coordinated polarization among adjacent cells. In a series of classical experiments, Sachs applied artificial auxin to bean plants, and observed that these become the source of new vascular tissue that then joins the existing vasculature; see e.g. Sachs (1975) and the review (Hajný et al. 2022). These initial observations, together with the discovery of PIN1 and subsequently discovered members of the PIN-FORMED protein family suggested that auxin drives the polarization of its own transporters, and hence the direction of its own transport (reviewed in Merks et al. 2007; Hajný et al. 2022). Initial models aimed to explain the formation of transport channels as observed in Sachs’ experiments. These models therefore assumed that the rate of auxin flux from cell to cell further polarised auxin transport. This positive feedback led to the self-organised formation of auxin transport channels in a process called auxin canalisation. When it was realised that auxin accumulations mark the formation of new leaves at the shoot apex, an alternative model was proposed, in which cells polarised towards the locally increased concentrations of auxin, thus forming self-organised accumulation of auxin (Reinhardt et al. 2003). Mathematical models of the self-organisation of polar auxin transport therefore follow these two broad categories. ‘With-the-gradient’ models formalise the canalisation hypothesis and assume that the rate of cell polarisation depends on the auxin flux towards the relevant neighbour (Mitchison 1980, 1981; Rolland-Lagan and Prusinkiewicz 2005; Rolland-Lagan 2008). ‘Up-the-gradient’ models assume that PIN polarizes in the direction of neighbouring cells at a rate that positively depends on the auxin concentration in that neighbour (Jönsson et al. 2006; Smith et al. 2006). Attempts to reconcile these two seemingly contradicting ideas have followed two broad approaches. The first approach proposed that with-the-gradient and up-the-gradient models act at different positions of the plant or at different stages during development. For example Bayer et al. (2009) proposed that the up-the-gradient model act at superficial tissue layers of the shoot apical meristem where it forms auxin accumulation points leading to the initial of new leaves. The deeper tissue layers could follow the with-the-gradient model channeling auxin away from the auxin accumulation point towards the vascular tissues (Bayer et al. 2009). A similar approach was recently taken to explain the leaf venation patterning in combination with auxin convergence at the edge of the leaf primordium (Holloway and Wenzel 2021). The second approach looked for variants of the with-the-gradient or up-the-gradient models that could explain both auxin canalisation and auxin accumulation depending on the parameter settings. In this line of reasoning Walker et al. have proposed a with-the-gradient hypothesis for phyllotaxis (Walke et al. 2013), whereas one of us has proposed an up-the-gradient hypothesis for canalisation (Merks et al. 2007).

More recent analyses of the role of auxin and PINs in the formation of leaf veins (Verna et al. 2019) put the key role of a feedback between auxin signaling and the polar localisation of PINs into question, and therefore the validity of canalisation hypothesis or its alternatives including the traveling-wave hypothesis (Merks et al. 2007) for formation of vascular tissues. In particular, quadruple mutants strongly reducing functionality of all plasma-membrane-localised PINs, i.e., of all PINs that are responsible for PAT in the leaf veins, show relatively mild venation pattern phenotypes. Further knock-out of PIN6 and PIN8, expressed in the leaf veins but not localised in the PM, thus excluding a role of these PINs in PAT, led to further defects in leaf venation patterning (Verna et al. 2019) identical to those due to a chemical block of auxin transport. Nevertheless, in these mutants the polar ordening of the cells in the vasculature stays intact and supernumerary veins are induced by exogenous application of auxin, showing that auxin can induce veins in absence of polar transport. Using further mutations of auxin sensing proteins, it was found that this PAT-independent vein formation requires auxin sensing and the activity of GNOM, a protein regulating the constitutive recycling of PM-localised proteins, including PINs. How the available mathematical models of auxin-regulated patterning in plants will need to be updated or rejected is a topic of ongoing investigation, but what seems clear at this moment is that such models must involve auxin sensing and coordination of cell polarisation possibly through polar transport of other small chemicals besides auxine [e.g., acidification of the cell walls (Fendrych et al. 2016)], facilitated diffusion (Mitchison 1980) or coordination of polarity through other means such as mechanical signaling as studied in mathematical models of phyllotaxis (Julien et al. 2019) and leaf venation patterning (Kneuper et al. 2020).

In this paper we formally analyse an existing up-the-gradient model for establishment of polar auxin transport during leaf venation patterning (Jönsson et al. 2006; Heisler and Jonsson 2006; Merks et al. 2007). Although this model is a strong oversimplification of the experimental state-of-the-art, which in part invalidates it, it includes (1) auxin sensing, (2) polar transport, and (3) constitutive recycling, and thus likely contains key elements of updated, future models while still retaining the simplicity required for mathematical analysis. Thus, despite clear discrepancies of recent experimental insights with both the up-the-gradient and with-the-gradient models, the insights obtained in a formal analysis as well as the mathematical approaches developed in this work will likely apply to future, updated models of auxin-regulated patterning in plants.

Mathematical motivation

In order to distinguish between the available phenomenological models of auxin-driven pattern formation and the general developmental principles that they represent, mathematical insight into the models’ structure and the models’ solutions will be crucial. This will help pinpoint key differences between the model structures and may uncover potential structural instabilities in the models upon which evolution may have acted, so as to produce new developmental patterning modules (Benítez et al. 2018). From the mathematical side, almost all previous studies have focused on the types of patterns that can be generated by different models once the transitory dynamics have died out. An important example is the study by Van Berkel and coworkers (van Berkel et al. 2013), where a number of models for polar auxin transport are recast into a common mathematical framework that allows them to be compared. A steady state analysis for a general class of active transport models can be found in Draelants et al. (2015), using advanced tools such as snaking from the field of bifurcation theory. Both periodic and stationary patterns are examined in Allen and Ptashnyk (2020), where the authors consider an extended with-the-gradient model. Haskovec and his coworkers derive local and global existence results together with an appropriate continuum limit for their graph-based diffusion model in Haskovec et al. (2019).

Important qualitative examples of the up-the-gradient model are the formation of regularly spaced auxin maximums that lead to the growth of new leaves, as well as the formation of auxin channels that have been hypothesized to precede the formation of veins. Our goal here is to move beyond the well-studied equilibrium settings above and focus instead on understanding the dynamical behavior that leads to these patterns. In particular, we provide a rigorous framework to study a class of wave solutions that underpin the dynamical behaviour associated to up-the-gradient models. Ultimately, we hope that this analytic approach will provide an additional lens through which models of PAT can be examined and compared.

The model

Inspired by Jönsson et al. (2006), Heisler and Jonsson (2006) and Merks et al. (2007), the system we will study is given by

A˙j=TactRj-1Aj-1ka+Aj-1-RjAjka+Aj+Tdiff(Aj+1-2Aj+Aj-1),P˙j=-k1Aj+1kr+Aj+1Pjkm+Pj+αAj,R˙j=k1Aj+1kr+Aj+1Pjkm+Pj, 1.1

posed on the one-dimensional lattice jZ; see Fig. 1. The variable Aj(t) denotes the auxin concentration in cell jZ, while Pj(t) and Rj(t) represent the unpolarized respectively right-polarized PIN1 in this cell. PIN1 is the PIN-variant that is believed to play a central role during auxin-based pattern formation in the shoot apical meristem and during leaf venation patterning (Reinhardt et al. 2003; Jönsson et al. 2006; Smith et al. 2006; Scarpella et al. 2006; Verna et al. 2019), and we therefore consider PIN1 here. However, note that the general structure of this model would apply to other polarised transporter proteins with similar behavior.

Fig. 1.

Fig. 1

Schematic representation of the model (1.1). Black arrows represent transport, red arrows describe polarization and the green dashed arrows indication promotion. In particular, the PIN1 polarization rate correlates positively with the neighbouring auxin concentration, making this a model of ‘up-the-gradient’ type

The parameters appearing in the problem are all strictly positive and labelled in the same manner as in Merks et al. (2007).1 In particular, Tact and Tdiff denote the strengths of the active PIN1-induced rightward auxin transport and its diffusive counterpart, respectively. Unpolarized PIN1 is formed in the presence of auxin at a rate α, while k1 denotes the polarization rate. Finally, ka, kr, and km are the Michaelis constants associated to the active transport of auxin and the polarization of PIN1, which depends on the auxin-concentration in the right-hand neighbouring cell. In particular, this model is of ‘up-the-gradient’ type.

The main difference compared to Merks et al. (2007) is that we are neglecting the presence of left-polarized PIN1 and have set the decay and depolarization rates of PIN1 to zero. Although this step of course imposes a pre-existing polarity on the system, we need to do this for technical reasons that we explain in the sequel. For now we simply point out that we wish to focus our attention on the dynamics of rightward auxin propagation, which takes place on timescales that are much faster than these decay and depolarization processes, and that the results will give novel insight into the full problem.

We will look for solutions of the special type

(Aj,Pj,Rj)(t)=(ϕA,ϕP,ϕR)(j-ct), 1.2

with c>0, in which we impose the limits

limξ-ϕA(ξ)=0,limξ(ϕA,ϕP,ϕR)(ξ)=0; 1.3

see Fig. 2. From a modelling perspective, such solutions represent a pulse of auxin that moves to the right through a one-dimensional row of cells. Ahead of the wave the cells are clear of both polarized and unpolarized PIN, but behind the wavefront a residual amount of PIN is left in the cells, representing the coordinated polarisation of the tissue.

Fig. 2.

Fig. 2

Left: cartoon of the waveprofiles (ϕA,ϕP,ϕR), illustrating the definition of the width w of the auxin-pulse and the limits (1.3). Right: numerical simulation of an auxin pulse passing through cell 25, leaving a residue of (polarized) PIN1. We used the procedure described in Sect. 1.4, with A1(0)=A=0.15. The remaining parameters were fixed as Tact=800, Tdiff=0.15, ka=1, km=kr=100, k1=200 and α=0.1

In reality these residues start to depolarize and decay, which can be included by adding linear decay terms to (1.1). This leads to the expanded system

A˙j=TactRj-1Aj-1ka+Aj-1-RjAjka+Aj+Tdiff(Aj+1-2Aj+Aj-1),P˙j=-k1Aj+1kr+Aj+1Pjkm+Pj+αAj+k2Rj-δPj,R˙j=k1Aj+1kr+Aj+1Pjkm+Pj-k2Rj, 1.4

in which the positive parameters δ and k2 represent the decay and depolarization rate of PIN1, respectively. Mathematically, these terms can be included into our framework provided that the parameters δ and k2 are small compared to the amplitude of the pulses, but we do not pursue this level of generality in the current paper for presentational clarity. Note in any case that in Merks et al. (2007) these parameters were chosen to be orders of magnitude smaller than α and k1.

Travelling waves have played a fundamental role in the analysis of many spatially discrete systems (Kevrekidis 2011; Mallet-Paret 1999; Chen et al. 2008; Hupkes and Sandstede 2010; Keener 1987). They can be seen as a lossless mechanism to transport matter or energy over arbitrary distances. As such, they are interesting in their own right, but they can also be viewed as building blocks to describe more complicated behaviour of nonlinear systems (Aronson and Weinberger 1975, 1978). In the present case for example, one can construct wavetrain solutions to (1.4) by adding a persistent auxin source; see Fig. 3 and Supplementary Video S1. Initially, these solutions can be seen in an approximate sense as a concatenation of the individual auxin pulses that we consider here (Moser 2021). As a consequence of the amplitude variations, small speed differences occur between these pulses which leads to highly interesting collision processes. Due to this type of versatility, travelling waves play an important role in many applications and have been extensively studied in a variety of settings (Sandstede 2002; Kevrekidis 2011; Hochstrasser et al. 1989; Jones et al. 1991).

Fig. 3.

Fig. 3

Six snapshots of a wavetrain simulation for the expanded system (1.4). Higher pulses travel faster than lower pulses, in correspondence with the scaling relations (1.7). These speed differences lead to merge events where even higher pulses are formed, which detach from the bulk. We used the procedure described in Sect. 1.4, taking A1(0)=A=0.0 but adding 0.025 to A˙1(t) to simulate a constant auxin influx at the left boundary. We picked δ=0.1 and k2=0.2, leaving the remaining parameters from Fig. 2 unchanged. The full simulation can be found in supplementary video S1

Main results

Our goal will be to obtain quantitative scaling information concerning the speed and shape of these waves. In particular, we will show rigorously that (1.1) admits a family of travelling wave solutions that are parameterized by the amplitude of the auxin-pulse. In addition, we show that the speed and width of these waves scale with this amplitude via a fractional power law. We state our results in full technical detail in Theorem 6.3 below.

More precisely, we provide an explicit triplet of functions (ϕA,ϕP,ϕR) that satisfy the limits (1.3) and construct solutions to (1.1) of the form

(Aj,Pj,Rj)(t)=(ϵϕA,ϵ1/5ϕP,ϵ2/5ϕR)(ϵ2/5(j-cϵ2/5t))+(O(ϵ17/15),O(ϵ1/3),O(ϵ3/5)), 1.5

for a constant c, which we state exactly in (1.8). Here the limiting profile ϕA is scaled in such a way that ϕAL=1. Upon introducing the heights2

(hA,hP,hR)=(A,P,R) 1.6

associated to the three components of our waves, this choice ensures that the auxin-height hA is equal to the parameter ϵ>0 at leading order. In particular, comparing this to (1.2) we uncover the leading order scaling relations

cchA2/5,wwhA-2/5,hPhPhA1/5,hRhRhA2/5 1.7

for the speed c, width3w and heights of the wave. Here the constant w denotes the width of the limiting profile ϕA, while the other constants are given explicitly by

c=9αk1TactTdiff28kakmkr1/5,hP=69α6ka4km4kr4Tdiff28k14Tact41/10,hR=39αka4k1Tdiff28krkmTact41/5. 1.8

In particular, for a fixed height of the auxin-pulse our results state that the speed and residual PIN1 will increase as the PIN1-production parameter α>0 is increased.

Although our proof requires the parameter ϵ>0 and hence the amplitude of the auxin-pulses to be small, this branch of solutions continues to exist well beyond this asymptotic regime. Indeed, we numerically confirmed the existence (and stability) of these waves by a direct simulation of (1.1) on a row of cells j{1,500}, initialized with Aj(0)=Pj(0)=Rj(0)=0 for 2j500, together with P1(0)=R1(0)=0 and A1(0)=A for some A>0 that we varied between simulations. In order to close the system, we used the Neumann-type condition A0(t)=A1(t) on the left-boundary, together with R0(t)=0 and a sink condition A501(t)=0 on the right. An example of such a simulation can be found in Fig. 2 (right). By varying the initial auxin concentration A, we were able to generate waves with a range of amplitudes. We subsequently numerically computed the speed and width of these waves, which allowed us to confirm the leading order behaviour (1.7); see Fig. 4. In addition, we verified the convergence to the limiting profiles (ϕA,ϕP,ϕR) by comparing the appropriately rescaled numerical waveprofiles; see Fig. 5.

Fig. 4.

Fig. 4

Scaling behaviour of the wavespeed c (left) and the auxin width w (right) against the height hA of the auxin pulse. The dashed lines represent the explicit predictions (1.7). The circles arise from numerical simulations, following the procedure described in Sect. 1.4 with several different values for A. The other parameters were chosen as in Fig. 2

Fig. 5.

Fig. 5

Convergence of the (scaled) profiles ϕA (left), ϕP (center) and ϕR (right) to their limits (ϕA,ϕP,ϕR). To perform the scalings, we wrote hA=ϕAL, compressed space by a factor of hA2/5 and divided the three profiles by the respective factors (hA,hA1/5,hA2/5), in line with the relations (1.7)

Cross-diffusion

From a mathematical perspective, the problem (1.1) is interesting due to its interpretation as a so-called cross-diffusion problem, where the transport coefficient of one component is influenced by one of the other components. Work in this area was stimulated by developments in the modeling of bacterial cell membranes (Shih et al. 2019) and biofilms (Emerenini et al. 2015), where self-organization of biological molecules plays an important role. In the continuum regime, such problems are tough to analyze on account of potential degeneracies in the coefficients. The well-posedness of the underlying problem was analyzed in Sonner et al. (2011), while a numerical method for such problems was developed in Ghasemi et al. (2018).

The key phenomenological assumption behind such models is that particles behave differently when they are isolated compared to when they are part of a cluster. A simplified agent-based approach to capture this mechanism can be found in Johnston et al. (2017), which reduces naturally to a scalar PDE with nonlinear diffusion in the continuum limit. After adding a small regularization term, it is possible to use geometric singular perturbation theory to show that this PDE admits travelling wave solutions (Li et al. 2021). In this setting, the steepness of the wavefronts provides the necessary scale-separation required for rigorous results.

Our approach in this paper proceeds along entirely different lines, using the amplitude of the auxin pulse as a small continuation parameter to construct a family of travelling wave solutions to (1.1). The key insight is that one can extract an effective limiting system by scaling the width and speed of the wave in an appropriate fashion and sending the amplitude to zero. By means of a fixed-point analysis one can show in a rigorous fashion that solutions to this limiting system can be continued to form a family of solutions to the full system.

Relation to FPUT pulses

Our technique is a generalization of the approach developed by Friesecke and Pego (1999) to construct small-amplitude travelling pulse solutions to the Fermi–Pasta–Ulam–Tsingou (FPUT) problem (Fermi et al. 1955; Dauxois 2008)

x¨j=F(xj+1-xj)-F(xj-xj-1),jZ. 1.9

This models an infinite, one-dimensional chain of particles that can only move horizontally and are connected to their nearest neighbours by springs. These springs transmit a force

F(r)=r+r2 1.10

that hence depends nonlinearly on the relative distance r between neighbouring particles; see Friesecke and Pego (1999), Herrmann and Matthies (2015) and Pankov (2005) for the impact of other choices. The FPUT system is well-established as a fundamental model to study the propagation of disturbances through spatially discrete systems, such as granular media, artificial metamaterials, DNA strands, and electrical transmission lines (Brillouin 1953; Kevrekidis 2011).

Looking for a travelling wave in the relative displacement coordinates, one introduces an Ansatz of the form

xj+1(t)-xj(t)=ϕ(j-σt), 1.11

which leads to the scalar functional differential equation of mixed type (MFDE)

σ2ϕ(ξ)=F(ϕ(ξ+1))-2F(ϕ(ξ))+F(ϕ(ξ-1)). 1.12

Following the classic papers by Friesecke in combination with Wattis (Friesecke and Wattis 1994) and Pego (Friesecke and Pego 1999, 2002, 2004a, b), we introduce the scaling

ϕ(ξ)=ϵ2φϵ(ϵξ) 1.13

and write σ=σϵ, which transforms (1.12) into the MFDE

σϵ2ϵ2φϵ=(Sϵ+S-ϵ-2)[φϵ+ϵ2φϵ2]. 1.14

Here the shift operator Sd acts as

(Sdf)(ξ)=f(ξ+d) 1.15

for any dR. Since the symbol Sϵ+S-ϵ-2 represents a discrete Laplacian, we can interpret (1.14) as a wave equation with a nonlinear diffusion term. To some extent, this clarifies the link with our original problem (1.1) and the discussion above.

Applying the Fourier transform to (1.14) with k as the frequency variable, we arrive at

-σϵ2ϵ2k2φ^ϵ(k)=2(cos(ϵk)-1)[φϵ^+ϵ2φϵ2^](k)=-4sin2(ϵk/2)[φϵ^+ϵ2φϵ2^](k). 1.16

Upon introducing the symbol

M~FPUT(ϵ)(k)=4ϵ2sin2(ϵk/2)σϵ2ϵ2k2-4sin2(ϵk/2), 1.17

this can be recast into the compact form

φϵ^(k)=M~FPUT(ϵ)(k)φϵ2^(k). 1.18

Upon choosing the speed

σϵ=1+ϵ23, 1.19

we can exploit the expansion sin2(z/2)=14z2-148z4+O(z6) to obtain the pointwise limit

M~FPUT(ϵ)(k)128+k2,ϵ0. 1.20

Using the fact that (8+k2) is the Fourier symbol for 8-ξ2, this suggests that the relevant system for φϵ in the formal ϵ0 limit is given by

8φ-φ=12φ2, 1.21

which has the nontrivial even solution

φ(ξ)=sech2(2ξ). 1.22

By casting the problem in an appropriate functional analytic framework, one can show that this explicit solution φ can be continued to yield solutions φϵ to (1.14) for small ϵ>0. In this fashion, one establishes the existence of a family of pulse solutions (Friesecke and Pego 1999)

xj+1(t)-xj(t)=ϵ2sech2(2ϵ(j-σϵt))+O(ϵ4). 1.23

Roughly speaking, the main mathematical contribution in this paper is that we show how this analysis can be generalized to the setting of (1.1). The first main obstacle is that this is a multi-component system, which requires us to explicitly reduce the order before a tractable limit can be obtained. The second main obstacle is that the analysis of our Fourier symbol is considerably more delicate, since in our setting the wavespeed c converges to zero instead of one as ϵ0. Indeed, the denominator of M~FPUT(ϵ) above depends only on the product ϵk, while in our case there is a separate dependence on ϵ2k. This introduces a quasi-periodicity into the problem that requires our convergence analysis to carefully distinguish between ‘small’ values of k and several separate regions of ‘large’ k.

The third main difference is that we cannot use formal spectral arguments to analyze the limiting linear operator, which in our case is related to the Bernoulli equation. Instead, we apply a direct solution technique using variation-of-constants formulas. On the one hand this is much more explicit, but on the other hand the resulting estimates are rather delicate on account of the custom function spaces involved.

Discussion

Due to the important organizing role that wave solutions often play in complex systems, scaling information such as (1.7) can be used as the starting point to uncover more general dynamical information concerning models such as (1.1) and related models of polar auxin trasnport. As such, we hope that the ideas we present here will provide a robust analytical tool to analyze different types of models as well. The resulting insights and predictions could help to prioritize competing models on the basis of dynamical experimental observations. Indeed, scaling laws appear to play a role in many aspects of biological systems, such as the structural properties of vascular systems (Razavi et al. 2018), the mass dependence of metabolic rates (West and Brown 2004) and the functional constraints imposed by size (Schmidt-Nielsen and Knut 1984).

Although we have included only right-polarizing PIN in our system, we believe that our techniques can be adapted to cover the full case where also left-polarizing PIN is included. However, the computations rapidly become unwieldy and the limiting system is expected to differ qualitatively. For this reason, we have not chosen to pursue this level of generality in the present paper, as it would only obscure the main ideas behind our framework. One of the main generalizations that we intend to pursue in the future is to study the model in two spatial dimensions. This is motivated by recent numerical observations concerning the formation of auxin channels and their associated PIN polarization under the influence of travelling patterns that are localized in both spatial dimensions (Althuis 2021; Merks et al. 2007).

Notation

We summarize a few aspects of our (mostly standard) notation.

  • If f=f(X) is a differentiable function on R, then we sometimes write f=X[f].

  • If X and Y are normed spaces, then we denote the space of bounded linear operators from X to Y by B(X,Y). We put B(X):=B(X,X).

  • We sometimes abbreviate R+:=(0,) and R-:=(-,0).

The travelling wave problem

Rewriting the original problem (1.1)

We will reduce the problem (1.1) to a system of equations involving only Aj and Pj, and it will be this resulting system on which we make the long wave-scaled travelling wave Ansatz.

Changes of notation

We begin by rewriting (1.1) in a slightly more compressed manner that also exposes more transparently the leading order terms in the nonlinearities. Let δ± be the left and right difference operators that act on sequences (xj) in R via

δ+xj:=xj+1-xjandδ-xj:=xj-xj-1.

Next, for k, xR with k+x0 we have

xk+x=xk-x2k(k+x).

We put

Q1(x,y):=x2yka+x 2.1

and compress

τ1:=Tactkaandτ2:=Tdiff 2.2

to see that our equation for Aj now reads

A˙j=τ2δ+δ-Aj-τ1δ-(RjAj)+τ1δ-Q1(Aj,Rj).

Next, we abbreviate

κ:=k1krkm 2.3

and put

Q2(x,y):=κkry+kmx+xy(kr+x)(km+y)xy 2.4

to see that, the equation for Pj is

P˙j=-κAj+1Pj+αAj+Q2(Aj+1,Pj).

The equation for Rj is updated similarly, and so we have rewritten (1.1) as

A˙j=τ2δ+δ-Aj-τ1δ-(RjAj)+τ1δ-Q1(Aj,Rj),P˙j=-κAj+1Pj+αAj+Q2(Aj+1,Pj),R˙j=κAj+1Pj-Q2(Aj+1,Pj). 2.5

We observe that the equation for Rj depends only on Aj+1 and Pj and therefore can be solved by direct integration. Before we do that, however, we rewrite the new equation for Pj using Duhamel’s formula.

Rewriting the Pj equation

We can view the equation for Pj in (2.5) as a first-order linear differential equation forced by αAj+Q2(Aj+1,Pj), and so we can solve it via the integrating factor method. For f, gL1 and hL we introduce the operators

E(f)(s,t):=exp-κstf(ξ)dξ,s,tR, 2.6
P1(f,g)(t):=α-tE(f)(s,t)g(s)ds, 2.7

and

P2(f,h)(t):=-tE(f)(s,t)Q2(f(s),h(s))ds. 2.8

Recall from (1.3) that we want Pj to vanish at -. The unique solution for Pj in (2.5) that does vanish at - must satisfy

Pj(t)=P1(Aj+1,Aj)(t)+P2(Aj+1,Pj)(t).

Solving the Rj equation

Since, per (1.3), we want Rj to vanish at -, and since we are assuming that each Aj vanishes sufficiently fast at both ± and Pj vanishes at - and remains bounded at +, we may solve for Rj by integrating the third equation in (2.5) from - to t. For f, gL1 and hL, we define more integral operators:

R1(f,g)(t):=κτ1-tf(s)P1(f,g)(s)ds,tR, 2.9
R2(f,g,h)(t):=-t(κf(s)P2(f,g)(s)-Q2(f(s),P1(f,g)(s)+P2(f,h)(s)))ds, 2.10

and

R(f,g,h)(t):=R1(f,g)(t)+R2(f,g,h)(t). 2.11

We have defined P1 and P2 just above, respectively, in (2.7) and (2.8) and Q2 earlier in (2.4). Then the solution to the third equation in (2.5) that vanishes at - is

Rj(t)=R(Aj+1,Aj,Pj)(t)=R1(Aj+1,Aj)(t)+R2(Aj+1,Aj,Pj)(t). 2.12

The final system for Aj and Pj

We rewrite (part of) the Aj equation once more to incorporate the new expression for Rj. For f, gL1 and hL and tR put

N(f,g,h)(t):=τ1Q1(g(t),R(f,g,h)(t))-τ1R2(f,g,h)(t)g(t), 2.13

where we defined Q1 in (2.1). Then Aj must satisfy

A˙j=τ2δ+δ-Aj-δ-(R1(Aj+1,Aj)Aj)+δ-N(Aj+1,Aj,Pj),

and so our system for Aj and Pj is now

A˙j=τ2δ+δ-Aj-δ-(R1(Aj+1,Aj)Aj)+δ-N(Aj+1,Aj,Pj),Pj=P1(Aj+1,Aj)+P2(Aj+1,Pj). 2.14

That is, using the formula (2.12) for Rj in terms of Aj and Pj, we can solve (2.5) if we can solve (2.14).

We will make two changes of variables on (2.14). First, in Sect. 2.2, we make a travelling wave Ansatz for Aj and Pj. We reformulate (2.14) for the travelling wave profiles as the system (2.28) below. Then, in Sect. 3.1, we introduce our long wave scaling on these travelling wave profiles. After numerous adjustments, we arrive at the final system (3.14) for the scaled travelling wave profiles, which we solve in Sect. 6. The reader uninterested in these intermediate stages may wish to proceed directly to Proposition 3.5, which discusses the equivalence of the problem (2.14) for Aj and Pj and the ultimate long wave system (3.42). Of course, our notation must keep up with these changes of variables, and we summarize in Table 1 the evolution of a typical operator’s typesetting across these different problems.

Table 1.

Summary of notational evolution

Symbol Use
R The original problem (2.14)
R~c The travelling wave problem (2.28)
R˘ϵ The preliminary long wave problem (3.14)
Rν The final long wave problem (3.42)
Remark 2.1

The linearization of (2.14) at 0 yields

A˙j=τ2δ+δ-Aj,Pj=Rj=0.

If we follow the discussion after Friesecke and Pego (1999, Thm. 1.1), as well as Faver and Wright (2018, Rem. 2.2), and look for plane wave solutions Aj(t)=eikj-iωt with ω, kR, we find the dispersion relation

-iω=2τ2(cos(k)-1). 2.15

The only real solutions are ω=0 and k2πZ. Previously, in Friesecke and Pego (1999) and Faver and Wright (2018) a nontrivial dispersion relation ω=ω(k) was found by making the same kind of plane wave Ansatz, and the result ‘phase speed’ kω(k)/k had a nonzero maximum cs, which was called the ‘speed of sound.’ These articles then proceeded to look for travelling waves with speed slightly above their respective values of cs; these were ‘supersonic’ waves. For us, ω(k) is identically zero, which suggests that the speed of sound for our auxin problem is 0. Our long wave scaling in Sect. 3.1 analytically justifies this intuition.

The travelling wave Ansatz

We now look for solutions Aj and Pj to (2.14) of the form

Aj=ϕ1(j-ct)andPj=ϕ2(j-ct). 2.16

The profiles ϕ1 and ϕ2 are real-valued functions of a single real variable and cR. The following manipulations will be justified if we assume ϕ1Hq1 and ϕ2W1,; we discuss the exponentially localized Sobolev space Hq1 in Appendix A.3. Working on an exponentially localized space, as opposed to an algebraically weighted space, both allows us to capture precisely certain very fast decay properties and permits us to use some technical results on approximating Fourier multipliers. Furthermore, since we want Pj to vanish at - and be asymptotically constant at +, per the limits (1.3) and the numerical predictions of Fig. 2, we expect that ϕ2 should vanish at + and be asymptotically constant at -.

We will convert the problem (2.14) for Aj and Pj into a nonlocal system for ϕ1 and ϕ2, with c as a parameter. Doing so amounts to little more than changing variables many times in the integral operators defined in Sects. 2.1.2 and 2.1.3 and gives us a host of new integral operators that will constitute the problem for ϕ1 and ϕ2.

In what follows we assume fL1 and gL, so that the operators below are defined in the special cases of f=ϕ1Hq1 and g=ϕ2W1,. First, for x, vR, put

E~c(f)(v,x):=expκcvxf(u+1)du 2.17

and

P~1c(f)(x):=αcxE~c(f)(v,x)f(v)dv. 2.18

Then we use the Ansatz (2.16) and the definition of P1 in (2.7) to find

P1(Aj+1,Aj)(t)=α-texp-κstϕ1(j-cξ+1)dξϕ1(j-cs)ds=P~1c(ϕ1)(j-ct).

Here we have substituted u=j-cξ in the exponential’s integral and then v=j-cs throughout.

Similar substitutions, which we do not discuss, yield the following identities. Put

P~2c(f,g)(x):=1cxE~c(f)(v,x)Q2(f(v+1),g(v))dv, 2.19

so that with P2 defined in (2.8) we have

P2(Aj+1,Pj)(t)=P~2c(ϕ1,ϕ2)(j-ct).

Thus ϕ2 must satisfy

ϕ2=P~1c(ϕ1)+P~2c(ϕ1,ϕ2), 2.20

which indicates that, as expected, ϕ2 should vanish at + and be asymptotically constant at -.

Now we reformulate the equation for Aj, equivalently, for ϕ1. Put

R~1c(f)(x):=κτ1cxf(u+1)P~1c(f)(u)du, 2.21

so that with R1 defined in (2.9) we have

R1(Aj+1,Aj)(t)=R~1c(ϕ1)(j-ct).

Put

R~2c(f,g)(x):=1cx(κf(u+1)P~2c(f,g)(u)-Q2(f(u+1),g(u)))du 2.22

and

R~c(f,g):=R~1c(f)+R~2c(f,g), 2.23

so that with R2 defined in (2.10) and R in (2.11) we have

R2(Aj+1,Aj,Pj)(t)=R~2c(ϕ1,ϕ2)(j-ct)andR(Aj+1,Aj,Pj)(t)=R~c(ϕ1,ϕ2)(j-ct).

Last, put

N~c(f,g)(x):=τ1R~2c(f,g)(x)f(x)-τ1Q1(f(x),R~c(f,g)(x)), 2.24

so that with N defined in (2.13) we have

N(Aj+1,Aj,Pj)(t)=N~c(ϕ1,ϕ2)(j-ct).

For a function f:RR and dR, define, as in (1.15), the shift operator Sd by

(Sdf)(x):=f(x+d). 2.25

This final piece of notation, along with the Eq. (2.20), allows us to convert the problem (2.14) for Aj and Pj into the following nonlocal system for ϕ1 and ϕ2:

-cϕ1=τ2(S1-2+S-1)ϕ1+(S-1-1)(R~1c(ϕ1)ϕ1+N~c(ϕ1,ϕ2)),ϕ2=P~1c(ϕ1)+P~2c(ϕ1,ϕ2). 2.26

The Fourier multiplier structure

We summarize our conventions and definitions for Fourier transforms and Fourier multipliers in Appendix A. If we take the Fourier transform of the equation for ϕ1 in (2.26), we find

(ick+2τ2(cos(k)-1))ϕ^1(k)=(1-e-ik)F[R~1c(ϕ1)ϕ1+N~c(ϕ1,ϕ2)](k).

For kR, we have ick+2τ2(cos(k)-1)=0 if and only if k=0. Consequently, the function

M~c(k):=1-e-ikick+2τ2(cos(k)-1) 2.27

has a removable singularity at 0 and is in fact analytic on R. We therefore define Mc to be the Fourier multiplier with symbol M~c, i.e., Mc satisfies

Mcf^(k)=M~c(k)f^(k).

We discuss some further properties of Fourier multipliers in Appendix A.2. Now the problem (2.26) is equivalent to

ϕ1=Mc(R~1c(ϕ1)ϕ1+N~c(ϕ1,ϕ2))ϕ2=P~1c(ϕ1)+P~2c(ϕ1,ϕ2). 2.28

The long wave problem

The long wave scaling

We now make the long wave Ansatz

ϕ1(x)=ϵψ1(ϵμx),ϕ2(x)=ϵβψ2(ϵμx),andc=ϵγc0. 3.1

We assume, as with ϕ1 and ϕ2, that the scaled profiles satisfy ψ1Hq1 and ψ2W1,. We think of ϵ>0 as small and keep the exponents β, γ, μ>0 arbitrary for now; eventually we will pick

γ=μ=25andβ=15.

The reasoning behind this choice is by no means obvious at this point and will not be for some time; leaving μ, β, and γ arbitrary will allow this choice to appear more naturally (at the cost of temporarily more cumbersome notation).

As we intuited in Remark 2.1, our wave speed is now close to 0, which is the auxin problem’s natural ‘speed of sound’. The parameter c00 affords us some additional flexibility in choosing the wave speed. A properly chosen value of c0 will cause the maximum of the leading-order term of ϕ1 to be ϵ, which will fulfill our promise in Sect. 1.4 that the auxin-height is, to leading order, ϵ. Friesecke and Pego introduce a similar auxiliary parameter into their ϵ-dependent wave speed, see Friesecke and Pego (1999, Eq. (2.5), (2.13)). This parameter allows them to prove that the dependence of their travelling wave profile on wave speed is sufficiently regular in different function spaces, a result needed for their subsequent stability arguments in Friesecke and Pego (2002, 2004a, 2004b). We did not provide this extra parameter in our version (1.19) of the Friesecke–Pego wave speed, but rather we selected it so that the amplitude of the leading order sech2-profile term in (1.22) is 1. Similarly, we will not pursue their depth of wave-speed analysis on our profiles’ dependence on c0.

We convert (2.28) to another nonlocal system for ψ1 and ψ2, which now depends heavily on the parameter ϵ. As before, this process mostly amounts to changing variables in many integrals. For example, we use the definition of P~1c in (2.18) and the Ansatz (3.1) to find

P~1c(ϕ1)(x)=αϵγc0xE~c(ϕ1)(v,x)ϵψ1(ϵμv)dv, 3.2

where, using the definition of E~c in (2.17), we have

E~c(ϕ1)(v,x)=expκϵγc0vxϵψ1(ϵμu+ϵμ)du=expκc0ϵ1-(γ+μ)ϵμvϵμxψ1(U+ϵμ)dU.

Here we have substituted U=ϵμu.

Now for fL1 we put

E(f)(V,X):=expκc0VXf(U)dU,V,XR, 3.3

so that (3.2) becomes

P~1c(ϕ1)(x)=αc0ϵ1-γxE(ϵ1-(γ+μ)Sϵμψ1)(ϵμv,ϵμx)ψ1(ϵμv)dv.

Here Sϵμ is the shift operator defined in (2.25) with d=ϵμ. We substitute again with V=ϵμv and define

P˘1ϵ(f)(X):=αc0XE(ϵ1-(γ+μ)Sϵμf)(V,X)f(V)dV 3.4

to conclude that

P~1c(ϕ1)(x)=ϵ1-(γ+μ)P˘1ϵ(ψ1)(ϵμx).

Similar careful substitutions will allow us to reformulate the integral operators from Sect. 2.2 in terms of the long wave Ansatz. First, however, we define

Q˘1ϵ(X,Y):=X2Yka+ϵXandQ˘2ϵ(X,Y):=κkrY+kmϵ1-βX+ϵXY(kr+ϵX)(km+ϵβY)XY. 3.5

When ϵ0, this definition permits the very convenient factorizations

Q1(ϵX,ϵ1-(γ+μ)Y)=ϵ3-(γ+μ)Q˘1ϵ(X,Y)andQ2(ϵX,ϵβY)=ϵ1+2βQ˘2ϵ(X,Y),

where Q1 was defined in (2.1) and Q2 in (2.4).

Now we work on the travelling wave integral operators. Below we will assume fL1 and gL. Put

P˘2ϵ(f,g)(X):=1c0XE(ϵ1-(γ+μ)Sϵμf)(V,X)Q˘2ϵ(f(V+ϵμ),g(V))dV, 3.6

so that with P~2c defined in (2.19) we have

P~2c(ϕ1,ϕ2)(x)=ϵ1-(γ+μ)+2βP˘2ϵ(ψ1,ψ2)(ϵμx).

This converts the second equation in (2.28) for ϕ2 to

ϵβψ2(ϵμx)=ϵ1-(γ+μ)P˘1ϵ(ψ1)(ϵμx)+ϵ1-(γ+μ)+2βP˘2ϵ(ψ1,ψ2)(ϵμx).

Passing to X=ϵμx, we find that ψ2 must satisfy

ψ2(X)=ϵ1-(γ+μ)-βP˘1ϵ(ψ1)(X)+ϵ1-(γ+μ)+βP˘2ϵ(ψ1,ψ2)(X). 3.7

Now put

R˘1ϵ(f)(X):=κτ1c0XP˘1ϵ(f)(V)f(V+ϵμ)dV, 3.8

so that with R~1c defined in (2.21) we have

R~1c(ϕ1)(x)=ϵ2(1-(γ+μ))R˘1ϵ(ψ1)(ϵμx).

Put

R˘2ϵ(f,g)(X):=1c0X(ϵ1-(γ+μ)κf(V+ϵμ)P˘2ϵ(f,g)(V)-Q˘2ϵ(f(V+ϵμ),g(V)))dV 3.9

and

R˘ϵ(f,g)(X):=ϵ1-(γ+μ)R˘1ϵ(f)(X)+ϵ2βR2ϵ(f,g)(X), 3.10

so that with R~2c defined in (2.22) and R~c defined in (2.23) we have

R~2c(ϕ1,ϕ2)(x)=ϵ1-(γ+μ)+2βR˘2ϵ(ψ1,ψ2)(ϵμx)andR~c(ϕ1,ϕ2)(x)=ϵ1-(γ+μ)R˘ϵ(ψ1,ψ2)(ϵμx).

Finally, put

N˘ϵ(f,g)(X):=τ1R˘2ϵ(f,g)(X)f(X)-ϵ1-2βτ1Q˘1ϵ(f(X),R˘ϵ(f,g)(X)), 3.11

so that with N~c defined in (2.24) we have

N~c(ϕ1,ϕ2)(x)=ϵ2-(γ+μ)+2βN˘ϵ(ψ1,ψ2)(ϵμx).

The definition of scaled Fourier multipliers from (A.3) tells us that, for ϵ>0, Mϵγc0(ϵμ) is the Fourier multiplier satisfying

Mϵγc0(ϵμ)f^(k)=M~ϵγc0(ϵμk)f^(k),

where M~ϵγc0 is defined by taking c=ϵγc0 in (2.27). This converts the first equation in (2.28) for ϕ1 to

ϵψ1(ϵμx)=Mϵγc0(ϵμ)[ϵ2(1-(γ+μ))R˘1ϵ(ψ1)ϵψ1+ϵ2-(γ+μ)+2βN˘ϵ(ψ1,ψ2)](ϵμx).

We factor this to reveal

ψ1(X)=ϵ2(1-(γ+μ))Mϵγc0(ϵμ)[R˘1ϵ(ψ1)ψ1+ϵ-1+γ+μ+2βNϵ(ψ1,ψ2)](X). 3.12

We abbreviate

M˘ϵ:=ϵ2(1-(γ+μ))Mϵγc0(ϵμ) 3.13

to conclude from (3.12) and the prior Eq. (3.7) for ψ2 that the long wave profiles must satisfy

ψ1=M˘ϵ[R˘1ϵ(ψ1)ψ1+ϵ-1+γ+μ+2βN˘ϵ(ψ1,ψ2)]ψ2=ϵ1-(γ+μ+β)P˘1ϵ(ψ1)+ϵ1-(γ+μ)+βP˘2ϵ(ψ1,ψ2). 3.14

We have been tacitly assuming that all of the exponents on powers of ϵ above are nonnegative so that the various ϵ-dependent operators and prefactors are actually defined at ϵ=0. In particular, this demands

1-2β0,-1+γ+μ+2β0,and1-(γ+μ+β)0. 3.15

The formal long wave limit and exponent selection

Our intention is now to take the limit ϵ0 in the Eq. (3.14) for ψ1 and ψ2. Doing so in a way that the limit is both meaningful (i.e., defined and nontrivial) and reflective of what the numerics predict at ϵ=0 will teach us what the exponents μ, γ, and β should be, beyond the requirements of (3.15).

The formal limit on M˘ϵ and the selection of the exponents γ and μ

We want to assign a ‘natural’ definition to M˘0, where M˘ϵ was defined, for ϵ>0, in (3.13). However, we relied above on having ϵ>0 to invoke the scaled Fourier multiplier identity (A.3) that gave us M˘ϵ, and naively setting ϵ=0 in that identity is meaningless. Additionally, we should be careful that the prefactor ϵ2(1-(γ+μ)) in (3.13) does not lead us to define M˘0=0; otherwise, we would have ψ1=0 when ϵ=0, and that is not what the numerics in Fig. 2 predict.

A natural starting point, then, is to study M˘ϵ in the limit ϵ0+, and this amounts to considering the limit of its symbol, whose definition we extract from the definition of M˘ϵ in (3.13) and the definition of the scaled Fourier multiplier in (A.3). Thus, for each kR, we want the limit

limϵ0+ϵ2(1-(γ+μ))M~ϵγc0(ϵμk) 3.16

to exist without being identically zero. The function M~ϵγc0 was defined in (2.27).

To calculate this limit, we first state the Taylor expansions

1-e-iz=iz+iz2N1(z)andcos(z)-1=-z22+iz4N2(z)2τ2 3.17

for zC. The functions N1 and N2 are analytic and uniformly bounded on strips in the sense that

Cq:=supxR|N1(x±iq)|+|N2(x±iq)|< 3.18

for any q>0. The choice of constants on N1 and N2 will permit some useful cancellations later. Then

M~c(k)=ik+ik2N1(k)ick-τ2k2+ik4N2(k)=1+kN1(k)c+iτ2k+k3N2(k),

and so

ϵ2(1-(γ+μ))M~ϵγc0(ϵμk)=ϵ2(1-(γ+μ))1+ϵμkN1(ϵμk)ϵγc0+iτ2ϵμk+ϵ3μk3N2(ϵμk). 3.19

At this point it does not make sense to set ϵ=0, as then the denominator would be identically zero. So, we would like to factor some power of ϵ out of the denominator. Since the first term in the denominator has a factor of ϵγ and the second a factor of ϵμ, we assume γ=μ and remove the power of ϵ from both the first and the second terms. We discuss the choice of γ=μ further in Remark 3.2.

Then

ϵ2(1-(γ+μ))M~ϵγc0(ϵμk)=ϵ2(1-2γ)M~ϵγc0(ϵγk)=ϵ2(1-2γ)-γ1+ϵγkN1(ϵγk)c0+iτ2k+ϵ2γk3N2(ϵγk). 3.20

Pointwise in k we have

limϵ0+1+ϵγkN1(ϵγk)c0+iτ2k+ϵ2γk3N2(ϵγk)=1c0+iτ2k,

and so we want

2(1-2γ)-γ=0

so that the prefactor of ϵ2(1-2γ)-γ in (3.20) does not induce a trivial or undefined limit. Thus we take

γ=μ=25.

Certainly doing so does not contradict any of the inequalities in (3.15), provided that β is chosen appropriately. Moreover, the power of 2/5 agrees with the height-speed-width relations suggested in Fig. 4. And so

limϵ0+ϵ2(1-(γ+μ))M~ϵγc0(ϵμk)=limϵ0+ϵ4/5M~ϵ2/5c0(ϵ2/5k)=1c0+τ2ik.

Put

M~(0)(z):=1c0+iτ2z, 3.21

so M~(0) is analytic on any strip zC||Im(z)|<q for q(0,τ2/c0). Let M(0) be the Fourier multiplier with symbol M~(0).

Lemma A.2 then gives the following properties of M(0); the identities (3.22) are direct calculations with the Fourier transform.

Lemma 3.1

Fix q(0,τ2/c0). Then M(0)B(Hqr,Hqr+1) for all r. More generally, if fH1 and gL2, then

M(0)(c0+τ2X)f=fand(c0+τ2X)M(0)g=g. 3.22

Because of the identities (3.22), we write M(0)=(c0+τ2X)-1. The formal analysis above then leads us to expect

limϵ0+M˘ϵ=M(0)=(c0+τ2X)-1. 3.23

However, we have not yet proved this rigorously by any means.

Remark 3.2

Here is why we take γ=μ when factoring the power of ϵ out of the denominator in (3.19). First, taking γ>μ produces

ϵ2(1-(γ+μ))M~ϵγc0(ϵμk)=ϵ2(1-(γ+μ))-μ1+ϵμkN1(ϵμk)ϵγ-μc0+iτ2k+ϵ2μk3N2(ϵμk)

instead of (3.20). If 2(1-(γ+μ))-μ>0, then the right side above is identically zero at ϵ=0, and so we demand 2(1-(γ+μ))-μ=0; there are many pairs of γ and μ that work here. But then

limϵ0+1+ϵμkN1(ϵμk)ϵγ-μc0+iτ2k+ϵ2μk3N2(ϵμk)=1iτ2k.

This suggests that instead of (3.23), we have

limϵ0+M˘ϵ=(τ2X)-1.

However, this is meaningless: differentiation is not invertible from Hqr to Hqr+1.

Taking γ<μ also does not work. In that case, instead of (3.20) we would have found

ϵ2(1-(γ+μ))M~ϵγc0(ϵμk)=ϵ2(1-(γ+μ))-γ1+ϵμkN1(ϵμk)c0+iτ2ϵμ-γk+ϵ3μ-γk3N2(ϵμk).

Since γ<μ we find

limϵ0+1+ϵμkN1(ϵμk)c0+iτ2ϵμ-γk+ϵ3μ-γk3N2(ϵμk)=1c0.

We would then want 2-3γ-2μ=0 to prevent a nontrivial limit.

Choosing γ and μ appropriately, we conclude that at ϵ=0 the equation for ψ1 from (3.14) formally reduces to

ψ1=1c0R˘10(ψ1)ψ1.

Numerically we expect ψ1(X)>0 for all X when ϵ=0, and so, using the definition of R˘10 from (3.8), we have

c0=R˘10(ψ1)(X)=ακτ1c02XVψ1(W)dWψ1(V)dV.

Differentiating, we find

Xψ1(W)dWψ1(X)=0.

But since ψ1(W)>0 for all W, we cancel the integral factor to find ψ1(X)=0, a contradiction to our numerical predictions.

The formal leading order equation for ψ1

At ϵ=0 the equation for ψ1 in (3.14) becomes (again, formally)

ψ1=M(0)(R˘0(ψ1)ψ1)=(c0+τ2X)-1(R˘0(ψ1)ψ1).

This is equivalent to

c0ψ1+τ2ψ1=R˘0(ψ1)ψ1. 3.24

We will rewrite this equation so that each term is a perfect derivative.

The definition of R˘1ϵ in (3.8), valid for all ϵ, gives

R˘0(ψ1)(X)=ακτ1c02XVψ1(W)dWψ1(V)dV. 3.25

Write

Ψ1(X):=Xψ1(W)dW,

so that Ψ1=-ψ1. The double integral from (3.25) is

XVψ1(W)dWψ1(V)dV=-XΨ1(V)Ψ1(V)dV=-XVΨ12(V)2dV=Ψ1(X)22.

Here we are using the requirement that ψ1Hq1, which implies Ψ1(X)0 as X. Thus

R˘0(ψ1)ψ1=-ακτ12c02Ψ12Ψ1=-ακτ16c02X[Ψ13].

Then (3.24) is equivalent to

τ2Ψ1+c0Ψ1-ακτ16c02X[Ψ13]=0.

We integrate both sides from 0 to and use the aforementioned fact that Ψ1 and its derivatives are required to vanish at to find

τ2Ψ1+c0Ψ1-ακτ16c02Ψ13=0. 3.26

This is a Bernoulli equation, and it has the solution

Ψ1(X)=Σ(X):=6c03ακτ1+6c02exp(2c0X/τ2+θ)1/2. 3.27

Here θR is an arbitrary phase shift. It follows that putting

ψ1(X)=σ(X):=-Σ(X)=(6c03)3/2exp(2c0X/τ2+θ)τ2[ακτ1+6c02exp(2c0X/τ2+θ)]3/2 3.28

solves (3.24).

Remark 3.3

We view the free parameter θ in (3.28) as an artifact of the translation invariance of our original problem (1.1). Friesecke and Pego (1999) do not incorporate a phase shift like θ into their leading order sech2-type KdV solution, since their broader existence result relies on working in spaces of even functions, and phase shifts destroy evenness. We will not need such symmetry in our subsequent arguments (nor could we achieve it, since no translation of σ is even or odd), and so we will leave θ as an arbitrary free parameter and not specify its value. Instead, we will restrain the extra degree of freedom of translation invariance by imposing a certain integral condition, which we make precise in (5.2).

The formal leading order equation for ψ2 and the selection of the exponent β

From our choice of γ=μ=2/5 and the inequalities in (3.15), we need, at the very least,

110β15.

If the strict inequality β<1/5 holds, then at ϵ=0 the equation for ψ2 in (3.14) reduces to the trivial result ψ2=0. This is not at all what we expect numerically from Fig. 2; rather, we anticipate that ψ2 will asymptote to some nonzero constant at .

However, if we instead take β so that

0=1-(γ+μ+β)=15-β,

which is to say,

β=15,

then the equation for ψ2 in (3.14) at ϵ=0 becomes

ψ2=P˘10(ψ1).

Putting

ψ2(X)=ζ(X):=P˘10(σ)(X)=αc0Xσ(V)dV 3.29

therefore solves the leading order equation for ψ2. We really have

ζ(X)=αc0Σ(X)=αc06c03ακτ1+6c02e2c0X/τ2+θ1/2,

where Σ was defined in (3.27).

The final long wave system

With the choices of exponents γ=μ=2/5 and β=1/5, it becomes convenient to introduce the new small parameter

ν:=ϵ2/5 3.30

into the problem (3.14) and then recast that problem more cleanly in terms of ν. First, the long wave Ansatz (3.1) becomes

ϕ1(x)=ν5/2ψ1(νx),ϕ2(x)=ν1/2ψ2(νx),andc=νc0. 3.31

Proceeding very much as in Sect. 3.1, we then define

Q1ν(X,Y):=X2Yka(ka+ν5/2X)andQ2ν(X,Y):=κkrY+kmν2X+ν5/2XY(kr+ν5/2X)(km+ν1/2Y)XY 3.32

for X, YR, while for fL1 and gL, we put

P1ν(f)(X):=αc0XE(ν1/2Sνf)(V,X)f(V)dV, 3.33

where E was defined in (3.3), and

P2ν(f,g)(X):=1c0XE(ν1/2Sνf)(V,X)Q2ν(f(V+ν),g(V))dV, 3.34
R1ν(f)(X):=κτ1c0XP1ν(f)(V)f(V+ν)dV, 3.35
R2ν(f,g)(X):=1c0X(ν1/2κf(V+ν)P2ν(f,g)(V)-Q2ν(f(V+ν),g(V)))dV, 3.36
Rν(f,g)(X):=R1ν(f)(X)+ν1/2R2ν(f,g)(X), 3.37

and

Nν(f,g)(X):=τ1R2ν(f,g)(X)f(X)-ν3/2τ1Q1ν(f(X),Rν(f,g)(X)). 3.38

Remark 3.4

The operators P1ν and R1ν map L1 into L, while P2ν and R2ν map L1×L into L, and Nν maps L1×L into L1. More precisely, we could replace L1 with Hq1 and L with W1, and the preceding statement would still be true; see the estimates in Appendix B.1.

The operator R10 has the especially simple form

R10(f)(X)=ακτ16c02XVf(W)dWf(V)dV 3.39

and therefore is differentiable from L1 to L.

Last, for ν>0, let M(ν) be the Fourier multiplier with symbol

M~(ν)(z):=ν1-e-iνzic0ν2z+2τ2(cos(νz)-1). 3.40

When ν=0 we have already defined M(0) as the Fourier multiplier whose symbol M~(0) is given in (3.21). We will show momentarily in Sect. 4 how M(0) is a good approximation of M(ν) in the operator norm topology, which we formally anticipated in the limit (3.23).

We now summarize the work of this section and the preceding one. In Sect. 2 we reformulated our original problem (1.1) into the more concise structure (2.14) and then made a travelling wave ansatz on this latter system. That led to the travelling wave problem (2.28). In this section, we introduced the long wave Ansatz (3.1) into this travelling wave problem and studied several formal expansions and limits to deduce the ‘correct’ choice of exponents and scalings. With the operators defined above, we can summarize our long wave problem in the following form.

Proposition 3.5

Suppose

Aj(t)=ν5/2ψ1(ν(j-νc0t)),Pj(t)=ν1/2ψ2(ν(j-νc0t)) 3.41

for some ψ1Hq1 and ψ2L, where c0, ν>0 and q(0,c0/τ2). Then Aj and Pj satisfy (2.14) if and only if ψ1 and ψ2 satisfy

ψ1=M(ν)(R1ν(ψ1)ψ1+ν1/2Nν(ψ1,ψ2)),ψ2=P1ν(ψ1)+νP2ν(ψ1,ψ2). 3.42

Moreover, taking

ψ1=σandψ2=ζ=P10(σ),

where σ is defined in (3.28) and ζ is given explicitly in (3.29), solves (3.42) when ν=0.

We will analyze the system (3.42) with a quantitative contraction mapping argument that tracks its dependence on ν. Specifically, we will look for solutions ψ1 and ψ2 to (3.42) that are close to σ and ζ, respectively, when ν is close to 0. We provide the details of this argument in Sect. 6.

Before doing so, we need to understand the behavior of two key operators, on whose good behavior the successful contraction argument will hinge. Our first task, as we mentioned above, is to study how M(0) approximates M(ν), and we do this in Sect. 4. Next, since we are looking for solutions (ψ1,ψ2) to (3.42) that are close to (σ,ζ), it is natural to study the linearization of (3.42) at (σ,ζ) for ν=0. It turns out that we will only need the linearization of the first equation, which is the operator

Tψ:=ψ-M(0)[R10(σ)ψ+(DR10(σ)ψ)σ]. 3.43

We will show in Sect. 5 that T is surjective from Hq1 to Hq1 with a one-dimensional kernel. Restricting T off this kernel will yield an extremely useful bijectivity result.

Analysis of the Fourier multiplier M(ν)

We show that the Fourier multiplier M(ν), whose symbol was defined in (3.40), converges to the multiplier M(0), whose symbol was defined in (3.21). More precisely, we prove the following estimate.

Proposition 4.1

Fix q(0,c0/τ2). There exist νM, CM>0 such that if 0<ν<νM, then

M(ν)-M(0)B(Hq1)CMν1/3.

The proof of this estimate depends on the following lemma, whose proof we give in the remainder of this section.

Lemma 4.2

Let q(0,c0/τ2). There exist CM, νM>0 such that if 0<ν<νM, then the map M~(ν) defined in (3.40) is analytic on the strip U¯q:=zC||Im(z)|q and satisfies

supkR|M~(ν)(k±iq)-M~(0)(k±iq)|<CMν1/3, 4.1

where M~(0) was defined in (3.21).

This lemma allows us to invoke Beale’s result in Lemma A.2 (with r=1 and s=0) to prove Proposition 4.1. Beale’s result depends very much on our working in exponentially weighted Sobolev spaces, and this is another of our reasons for preferring these spaces to algebraically weighted ones.

We will estimate the difference |M~(ν)(z)-M~(0)(z)| over two regimes, one in which z=k±iq is ‘close’ to 0, and the other in which z is ‘far from’ 0. Part of these estimates will involve bounding the denominator of M~(ν) away from zero; this will ensure the analyticity of M~(ν), since it is the quotient of two analytic functions.

To quantify these regimes, we introduce two positive constants p and m; we say that z is ‘close’ to 0 if |z|ν-p and ‘far from’ 0 if |z|>ν-p. The constant m will later control how close the real part of νz is to an integer multiple of 2π, a bound that will be very useful in certain estimates to come. All constants C in the work below are allowed to depend on m, p, and q, but they are always independent of ν and z.

Our estimates will depend on the parameters p and m; once we have all the estimates together, we will choose useful values for p and m. We feel that this approach allows the otherwise nonobvious final values for p and m to emerge very naturally. This strategy of splitting the estimates over regions close to and far from 0 is modeled on the proofs of Faver and Wright (2018, Lem. A.13) and Stefanov and Wright (2020, Lem. 3) and the strategy in Johnson and Wright (2020, App. A.3). Friesecke and Pego Friesecke and Pego (1999, Sec. 3) give a rather different proof of symbol convergence that relies on more knowledge of the poles of M~(ν) than we care to discover.

Estimates for z ‘close to’ 0

In this regime we fix |z|ν-p. We recall the Taylor expansions

1-e-iz=iz+iz2N1(z)andcos(z)-1=-z22+iz4N2(z)2τ2

from (3.17), as well as the estimate

Cq:=supxR|N1(x±iq)|+|N2(x±iq)|<.

Now we can write

M~(ν)(z)=1+νzN1(νz)c0+τ2iz+ν2z3N2(νz).

With this expression we find the following equality

M~(ν)(z)-M~0(z)=Iν(z)+IIν(z),

where

Iν(z):=c0νzN1(νz)-ν2z3N2(νz)(c0+τ2iz+ν2z3N2(νz))(c0+iτ2z) 4.2

and

IIν(z):=iτ2νz2N1(νz)(c0+τ2iz+ν2z3N2(νz))(c0+iτ2z). 4.3

We work on the denominators. We use the reverse triangle inequality to find

|(c0+τ2iz-2τ2iν2z3N2(νz))(c0+τ2iz)||c0-τ2q-2τ2ν2|z|3|N2(νz)|||c0-τ2q|.

As q(0,c0/τ2), we have |c0-τ2q|>0. Also, since |z|ν-p, we have ν2|z|3ν2-3p. If we take

0<p<23 4.4

and assume ν(0,ν1), where

ν1:=min1,|c0-τ2q|4Cqτ21/(2-3p), 4.5

then

|c0-τ2q-ν2|z|3|N2(νz)|||c0-τ2q|2. 4.6

In particular,

|c0-τ2q-2τ2ν2|z|3|N2(νz)|||c0-τ2q||c0-τ2q|22, 4.7

and this inequality guarantees that M~(ν) is defined (and analytic) for |z|ν-p and |Im(z)|<q. Then we use (4.7) to estimate Iν(z) from (4.2) as

|Iν(z)|Cν1-p+Cν2-3p.

Next, we use (4.6) to estimate IIν(z) from (4.3) as

|IIν(z)|Cν1-p|z||c0+iτ2z|.

Setting z=x±iq we note

|z|2|c0+iτ2z|2=x2+q2(c0±τ2q)2+τ22x2x2+q2(c0-τ2q)2+τ22x2.

We know

D:=supxRx2+q2(c0-τ2q)2+c02x2<,

and thus

|IIν(z)|Cν1-p.

We conclude

|M~(ν)(z)-M~(0)(z)||Iν(z)|+|IIν(z)|C(ν1-p+ν2-3p). 4.8

As we required p(0,2/3), the final estimate contains only positive powers of ν. Since we will always consider 0<ν<ν1 in the future, the definition of ν1 in (4.5) ensures 0<ν<1 in the following regimes.

Estimates for z ‘far from’ 0

In this regime we assume |z|>νp. Take

ν2<minν1,τ22c01/p, 4.9

with ν1 defined in (4.5), so that if 0<ν<ν2, then |z|>c0/τ2. With the reverse triangle inequality we find

|M~(0)(z)|1||c0|-|τ2z||<1τ2ν-p-c0<2τ2νp. 4.10

Consequently, it suffices in this regime to show that M~(ν) is bounded by a multiple of some power of ν. It will be convenient now to rewrite M~(ν) as

M~(ν)(z)=νM~1(ν)(z)M~2(ν)(z),

where

M~1(ν)(z):=1-e-iνzandM~2(ν)(z):=ic0ν2z+2τ2(cos(νz)-1). 4.11

The analyticity of M~(ν) for |z|>νp will follow if we bound M~2(ν) away from zero here.

The presence of the factor cos(νz)-1 in the denominator of M~(ν) suggests that the behavior of this function may be different when Re(νz) is ‘close’ to an integer multiple of 2π and when it is not. For this reason, we expand z=x±iq and let nZ be the unique integer such that |νx-2πn|π. We consider three cases on the behavior of νx and n.

Estimates for Re(νz) ‘close to’ a nonzero integer multiple of 2π

In this regime we assume |νx-2πn|νm with n0.

We first rewrite the numerator as

M~1(ν)(z)=1-e-i(νx-2πn)+e-iνx(1-e±νq).

Since the map ye-iy is uniformly Lipschitz on R we have

|1-e-i(νx-2πn)||νx-2πn|νm.

Since the map ye-y is locally Lipschitz on R we have, if we take 0<ν<ν3 with

ν3:=minν2,1q 4.12

and ν2 defined in (4.9), the estimate

|1-e±νq|νq.

Then

|M~1(ν)(z)|νm+νqC(νm+ν). 4.13

We remark that we did not need n0 here, although we will momentarily.

We now turn to the denominator, M2(ν)(z). Using the identity

cos(a+bi)=cos(a)cosh(b)-isin(a)sinh(b) 4.14

for a,bR we find

Im(M~1(ν)(z))=c0ν2x-2τ2sin(νx)sinh(νq).

We estimate

|Im(M~1(ν)(z))|C(ν|n|-ν|νx-2nπ|-|sin(νx-2nπ)||sinh(νq)|)

We control the three terms on the right as follows. First, |n|1. Next, we are in the regime |νx-2nπ|νm. Finally, we have

|sin(νx-2nπ)||νx-2nπ|νmand|sinh(νq)|2|νq|,

since |νq|1. We thus find

|Im(M~2(ν)(z))|C(ν-νm+1).

Now that we have the numerator and the denominator bounded, we can conclude

|M~(ν)(z)|Cννm+νν-νm+1=Cνm+ν1-νmCνm. 4.15

Here we need to assume

0<m<1. 4.16

Estimates for Re(νz) ‘close to’ 0

In this regime we assume |νx|νm; in particular, we are taking n=0. We will need the following bound on the cosine, which is a consequence of an elementary argument with Taylor’s theorem.

Lemma 4.3

Let Q0. There exist C1,Q, C2,Q>0 such that if ZC with |Z|C1,Q and |Im(Z)|Q, then

|cos(Z)-1|C2,Q|Z|2.

In particular, if Q=0, then C1,0>π.

We use the reverse triangle inequality on M~2(ν) from (4.11) to find

|M~2(ν)(z)|2τ2|cos(νz)-1|-c0ν2q-c0ν2|x|. 4.17

Take 0<ν<νM, where

νM<minν3,1q1/(1-m),C1,q21/m, 4.18

with ν3 defined in (4.12), to find

|νz|νm+νz2νm<C1,q.

Lemma 4.3 then guarantees

|cos(νz)-1|C|νz|2Cν2-2p.

Finally, since |x|νm-1 in this regime we use the bound (4.17) to conclude

|M~2(ν)(z)|C(ν2-2p-ν2-νm+1).

We remark that the derivation of the estimate (4.13) only assumed |νx-2πn|νm and did not rely on having n0. So it is still valid here, and we conclude

|M~(ν)(z)|Cννm+νν2-2p-ν2-νm+1=Cνm+2p-1+ν2p1-ν2p-νm+2p-1C(νm+2p-1+ν2p). 4.19

Here we are assuming

01-2p<min{1,m}. 4.20

Estimates for Re(νz) ‘far from’ a nonzero integer multiple of 2π

In this regime we assume |νx-2πn|>νm. We do not perform separate work on n=0 and n0.

Via (4.14) we find

Re(M2(ν)(z))=-c0ν2q+2τ2(cos(νx-2nπ)-1)+2τ2cos(νx)(cosh(νq)-1).

We estimate

|Re(M2(ν)(z))|C(|cos(νx-2nπ)-1|-|cos(νx)||cosh(νq)-1|-ν2).

Now we use Lemma 4.3 with Q=0 to bound

|cos(νx-2nπ)-1|C|νz-2nπ|2Cν2m.

Also, a routine Lipschitz estimate on the hyperbolic cosine gives

|cos(νx)||cosh(νq)-1|Cν2

since |νq|1. We thus find

|Re(M2(ν)(z))|C(ν2m-ν2).

As we are assuming 0<m<1 from (4.16), this is a positive lower bound.

Finally, we bound the numerator M~1ν(z) crudely as |M~1(ν)(z)|C for all zC with |Im(z)|=q. This follows from the boundedness of ZeiZ on strips. We conclude

|M~(ν)(z)|<Cνν2m-ν2Cν1-2m. 4.21

This is a positive bound if we now require

0<m<12. 4.22

Overall estimates

Suppose 0<ν<νM, where νM was specified in (4.18). We conclude from (4.8) that

sup|Im(z)|=q|z|ν-p|M~(ν)(z)-M~(0)(z)|C(ν1-p+ν2-3p) 4.23

and, by combining (4.10), (4.15), (4.19), and (4.21), that

sup|Im(z)|=q|z|>ν-p|M~(ν)(z)-M~(0)(z)|Cνp+Cmax{νm,νm+2p-1+ν2p,ν1-2m}. 4.24

Additionally, we need, per (4.4), and (4.20), and (4.22), the exponents p and m to satisfy

0<p<23,0<m<12,and0<1-2p<min{1,m}. 4.25

There are many possible choices of p and m that will satisfy (4.25). Purely for convenience, we elect to take m=1/3 and then p=1/2. We combine (4.23) and (4.24) to conclude the estimate (4.1).

Analysis of the linearization T

The operator

Tψ=ψ-M(0)[R10(σ)ψ+(DR10(σ)ψ)σ] 5.1

is the linearization of the first equation in our long wave-scaled travelling wave problem (3.42) at (ψ1,ψ2)=(σ,ζ) and ν=0. We recall that the symbol of the Fourier multiplier M(0) was defined in (3.21) and the operator R10 was defined in (3.39).

We will work with T defined on the following subspace of Hq1:

Hq,01:=fHq1|0f(W)dW=0. 5.2

We norm Hq,01 with the Hq1-norm. In Lemma 5.2 below we show that the kernel of T in Hq1 is spanned by σ. Restricting T to Hq,01 removes this kernel and guarantees injectivity. We will then prove that T is surjective onto Hq1 and so conclude the following result.

Proposition 5.1

For q(0,c0/τ2), the operator T:Hq,01Hq1 is invertible with bounded inverse.

The linearization at the limiting localized solution appears as a key operator in numerous FPUT problems, including (Friesecke and Pego 1999; Faver and Wright 2018; Hoffman and Wright 2017), and the invertibility of this operator is a property essential to the development of the right fixed point formula for the given problem. Our treatment of the invertibility of T is rather different from the analogous inversions in those papers, as the problem Tf=g is really a linearized Bernoulli equation in disguise, rather than the linearized KdV travelling wave profile equation. In particular, solving Tf=g amounts to studying a first-order linear problem, which we can solve explicitly with an integrating factor. In doing so, we avoid the more abstract spectral theory that controls the second-order KdV linearizations (see, e.g., Friesecke and Pego (1999, Lem. 4.2)).

It will be convenient to abbreviate

q:=c0τ2, 5.3

and in the following we always assume 0<q<q.

The proof of Proposition 5.1

We will reformulate the equation Tf=g in a very convenient manner, which we summarize in Lemma 5.2 below. This lemma will be the key to deducing the injectivity and surjectivity of T.

First, for hHq1, we introduce the operator

(Af)(X):=Xh(W)dW, 5.4

so that

h=-X[Ah]. 5.5

Then hHq,01 if and only if hHq1 and (Af)(0)=0. We will show that the equation Tf=g for f, gHq1 is equivalent to a statement about Af and Ag, which we give precisely in Lemma 5.2.

The following steps are quite similar to the derivation of the Bernoulli solution σ in Sect. 3.2.2. From the definition of T in (5.1), we have Tf=g if and only if

(c0+τ2X)f-R10(σ)f+(DR10(σ)f)σ=g. 5.6

From the definition of R10 in (3.39), we find

(DR0(σ)f)(X)=XWσ(V)dVf(W)dW+XWf(V)dVσ(W)dW. 5.7

Since g, σHq1, and since we seek fHq1, we abbreviate

F:=Af,G:=Ag,andΣ:=Aσ. 5.8

Then (5.6) is equivalent to

τ2F(X)-c0F(X)-ακτ1c02F(X)XΣ(W)Σ(W)dW-ακτ1c02Σ(X)X(Σ(W)F(W)+F(W)Σ(W))dW=-c0G(X)-τ2G(X). 5.9

Although it may not be apparent at first glance, every term in this equation is a perfect derivative. First, since Σ and F must vanish at +, we have

XΣ(W)Σ(W)dW=-Σ(X)22

and

X(Σ(W)F(W)+F(W)Σ(W))dW=-Σ(X)F(X).

Hence (5.9) really is

τ2F-c0F+ακτ1c02FΣ22+ΣΣF=-c0G-τ2G, 5.10

where

FΣ22+ΣΣF=12X[Σ2F].

So, we deduce that F and G must satisfy

-τ2F-c0F+ακτ1c02XΣ2F2=-c0G-τ2G. 5.11

Since both F and G must vanish at +, we may integrate (5.11) to find

τ2F+c0F-ακτ1c02Σ2F2LF=c0G+τ2G. 5.12

The operator L defined above is the linearization of the Bernoulli equation (3.26) at its solution Σ, and so

0=LΣ=L(-σ). 5.13

The operator L, or, more precisely, τ2-1L, is also a first-order linear differential operator, and so we can solve (5.12) with an integrating factor. Namely, let P satisfy

P=c0τ2-ακτ12c02τ2Σ2. 5.14

Then F solves (5.12) if and only if

F(X)=F(0)eP(0)-P(X)+σ(X)0XeP(W)(qG(W)+G(W))dW. 5.15

In particular, any solution H to LH=0 must be a scalar multiple of e-P(·), and so, by (5.13), σ is also a scalar multiple of e-P(·). Consequently, we can rewrite (5.15) as

F(X)=F(0)σ(0)σ(X)+σ(X)0XqG(W)+G(W)σ(W)dW. 5.16

Conversely, if F satisfies (5.16), then we may undo all of the work above to see that f:=-F solves Tf=g. Using the identities (5.8), we can recast this result in terms of the original functions f and g.

Lemma 5.2

For gHq1, define

(Hg)(X):=q(Ag)(X)-g(X) 5.17

and

(Kg)(X):=σ(X)0X(Hg)(W)σ(W)dW. 5.18

Then fHq1 satisfies Tf=g if and only if

(Af)(X)=(Af)(0)σ(0)σ(X)+(Kg)(X). 5.19

In particular, a function fHq,01 satisfies Tf=g if and only if

(Af)(X)=(Kg)(X). 5.20

The identity (5.20) allows to prove the bijectivity of T:Hq,01Hq1. The proof of injectivity is very easy. If Tf=0 for some fHq,01, then (5.20) implies Af=0, and so the identity (5.5) gives f=0. Observe that if we were working on all of Hq1, then (5.19) tells us that T would have a one-dimensional kernel in Hq1 spanned by σ. But since (Aσ)(0)=-σ(0)0, we have σHq,01.

Toward surjectivity, suppose Tf=g for some fHq,01 and gHq1. Then (5.5) and (5.20) imply

f=-X[Kg]=:Sg. 5.21

That is, we expect T-1=S. Now we make this rigorous.

Lemma 5.3

The operator S, defined in (5.21), is a bounded linear operator from Hq1 to Hq,01 that satisfies TSg=g for all gHq1.

Proof

Let gHq1. In part (i) of Lemma 5.4 below we show that σ=-ρσ for a certain function ρL. Then the definition of K in (5.18) gives

Sg=ρ(Kg)-Hg, 5.22

and the definition of H in (5.17) shows

X[Sg]=ρ(Kg)-ρ(Sg)+qg+g. 5.23

We claim there is a constant C, independent of g, such that

ρ(Kg)Lq2CgHq1 5.24

and

SgLq2CgHq1 5.25

Since ρL, the identities (5.22) and (5.23) show that S is a bounded operator on Hq1. We prove the estimate (5.24) in Sect. 5.2.1 below and the estimate (5.25) in Sect. 5.2.2.

To show both that SgHq,01 and that taking f=Sg satisfies (5.20), we first use the definition of A in (5.4) to compute

(ASg)(X)=(Kg)(X)-limB(Kg)(B). 5.26

We claim that

limB(Kg)(B)=0. 5.27

Indeed, since SgHq1, we know that Sg vanishes at infinity; so does Hg by the definition of H in (5.17). However, ρ(X)q0 as X by part (iii) of Lemma 5.4 below. The first equality in (5.22) then forces the limit (5.27) to be true.

Thus

(ASg)(X)=(Kg)(X). 5.28

In particular,

(ASg)(0)=(Kg)(0)=0

by the definition of K in (5.18). Consequently, SgHq,01, and so (5.28) shows that f=Sg satisfies (5.20). This implies T(Sg)=g.

Auxiliary results for the proof of Lemma 5.3

We first study some properties of σ and its derivative.

Lemma 5.4

  • (i)

    There exists ρL such that σ=-ρσ.

  • (ii)
    There exist ς1+, ς2+, ϱ+L(R+), ς1-, ς2-, ϱ-L(R-), and C1, C2R such that
    1σ(X)=C1eqX+e-qXς1+(X),X>0C2e-2qX+ς1-(X),X<0, 5.29
    σ(X)=C1-1e-qX+e-3qXς2+(X),X>0C2-1e2qX+e4qXς2-(X),X<0, 5.30
    and
    ρ(X)=q+e-qXϱ+(X),X>0-2q+eqXϱ-(X),X<0. 5.31
  • (iii)
    There is C3>0 such that
    |ρ(X)|C3e-q|X| 5.32
    for all XR.

Proof

  • (i)
    Recall that σ=-Σ, where Σ satisfies the Bernoulli equation (3.26). That is,
    σ=-Σ=c0τ2Σ-ακτ16c02τ2Σ3.
    Then
    σ=c0τ2Σ-ακτ12c02τ2Σ2Σ=ακτ12c02τ2Σ2-c0τ2σ.
    Put
    ρ=c0τ2-ακτ12c02τ2Σ2. 5.33
    By the definition of Σ in (3.27), we have ρL. Note, incidentally, that ρ must be a scalar multiple of P from (5.14).
  • (ii)
    The expansions (5.30) and (5.29) follow directly from the formula for σ in (3.28). The expansion (5.31) follows from the definition of ρ in (5.33) and the definition of Σ in (3.27), which gives
    limXΣ(X)2=0andlimX-Σ(X)2=3c0τ2=3q.
  • (iii)

    This is a direct consequence of (5.33).

We will also need estimates on A and H.

Lemma 5.5

There is C>0 such that

AgL+HgLCgHq1 5.34

for all gHq1.

Proof

We use the definition of A in (5.4) to bound

|(Ag)(X)|fL1CfHq1

by the embedding of Hq1 into L1, which we discuss in Appendix A.3. The estimate for H then follows from the triangle inequality.

In the following we again recall that 0<q<q.

The proof of the estimate (5.24)

We first use the definition of K in (5.18) and the estimates (5.32) on ρ and (5.34) on Hg to bound

|ρ(X)(Kg)(X)|CgHq1e-q|X|σ(X)0XdWσ(W).

If X>0, we use the estimates (5.30) on σ(X) and (5.29) on 1/σ(W) to bound

σ(X)0XdWσ(W)Ce-qX0XeqWdWC.

If X<0, we use the negative versions of these estimates to bound

σ(X)0XdWσ(W)Ce2qXX0e-2qWC.

We conclude

|ρ(X)(Kg)(X)|CgHq1e-q|X|

for all X. Since 0<q<q, this gives ρ(Kg)Lq2CgHq1.

The proof of the estimate (5.25)

It suffices to find C>0 such that for all gHq1, we have

SgLq2(R+)+SgLq2(R-)CgHq1.

We will rewrite (Sg)(X) in different ways for X>0 and X<0 to exploit the different decay rates of σ at + and -.

First suppose X>0. The formula (5.22) for Sg, the formula (5.18) for K and the expansions in Lemma 5.4 allow us to write

(Sg)(X)=(C1-1qe-qX+e-2qXς3+(X))0X(C1eqW+e-qWς1+(W))(Hg)(W)dW-(Hg)(X),

where ς3+L(R+). We expand this to give

(Sg)(X)=j=14(Sj+g)(X),

where

(S1+g)(X):=qe-qX0XeqW(Hg)(W)dW-(Hg)(X)(S2+g)(X):=C1-1qe-qX0Xe-qWς1+(W)(Hg)(W)dW(S3+g)(X):=C1e-2qXς3+(X)0XeqW(Hg)(W)dW(S4+g)(X):=e-2qXς3+(X)0Xe-qWς1+(W)(Hg)(W)dW.

The estimate (5.34) from Lemma 5.5 allows us to bound the last three terms with

|(S2+g)(X)|+|(S4+g)(X)|Ce-qXHgL0Xe-qWCe-qXgHq1 5.35

and

|(S3+g)(X)|Ce-2qXHgL0XeqWCe-qXgHq1. 5.36

To control S1+g, we first integrate by parts:

0XeqW(Hg)(W)dW=eqX(Hg)(X)-(Hg)(0)q-1q0XeqW(Hg)(W)dW.

The definition of H in (5.17) gives

0XeqW(Hg)(W)dW=-0XeqW(qg(W)+g(W))dW=-0XW[eqWg(W)]dW=g(0)-eqXg(X). 5.37

It follows that

(S1+g)(X)=-e-qX(Hg)(0)-e-qXg(0)+g(X). 5.38

We apply Lemma 5.5 to the factor (Hg)(0) and use the Sobolev embedding to estimate g(0), so that

|(S1+g)(X)|Ce-qXgHq1+|g(X)|.

Since 0<q<q, the estimates (5.35) and (5.36) and the identity (5.38) give

eqX|(Sg)(X)|Ce(q-q)XgHq1+eqX|g(X)|

for X>0, from which the bound

SgLq2(R+)CgHq1

follows.

Now suppose X<0. Using the expansions in Lemma 5.4 valid for X<0, we rewrite

(Sg)(X)=(2qC2-1e2qX+e3qXς3-(X))X0(C2e-2qW+ς1-(W))(Hg)(W)-(Hg)(X),

where ς3-L(R-). We expand this as

(Sg)(X)=j=14(Sj-g)(X),

where

(S1-g)(X):=2qe2qXX0e-2qW(Hg)(W)dW-(Hg)(X)(S2-g)(X):=2qC2-1e2qXX0ς1-(W)(Hg)(W)dW(S3-g)(X):=C2e3qXς3-(X)X0e-2qW(Hg)(W)dW(S4-g)(X):=e3qXς3-(X)X0ς1-(W)(Hg)(W)dW.

We crudely estimate the last three terms as

|(S2-g)(X)|+|(S3-g)(X)|+|(S4-g)(X)|Ce2qX|X|HgLCeqXgHq1. 5.39

For the first term, we integrate by parts to find

X0e-2qW(Hg)(W)dW=e-2qX(Hg)(X)-(Hg)(0)2r-12qX0e-2qW(qg(W)+g(W))dW.

The difference compared to (5.37) in our treatment of S1+g is that we no longer have a perfect derivative as the integrand on the right; this is an consequence of the different asymptotic behavior of ρ and σ at - compared to +, as specified in Lemma 5.4. Thus

(S1-g)(X)=-(Hg)(0)e2qX+I[g](X), 5.40

where

I[g](X):=-e2qXX0e-2qW(rg(W)+g(W))dW.

To control this integral term, we will use the following lemma, whose proof we defer to Sect. 5.2.3.

Lemma 5.6

There exists C>0 such that

-0e2XX0e-Wh(W)dW2dXChL2 5.41

for all hL2.

Since qg+gLq2, we can write

qg(X)+g(X)=e-q|X|h(X)

for some hL2. Then

-0e-2qX|I[g](X)|2dX=-0e2(2q-q)XX0e-(2q-q)Wh(W)dW2dX=1(2q-q)2-0e2UU0e-VhV2q-qdV2dU.

Applying Lemma 5.6, we obtain

I[g]Lq2(R-)Ch·2q-qL2Ce-q|·|(eq|·|h)L2CgHq1.

All together, we use the estimates (5.39) and the identity (5.40) to bound

|(Sg)(X)|CeqXgHq1+|I[g](X)|,

from which we obtain

SgLq2(R-)CgHq1.

The proof of Lemma 5.6

Put

W:=(X,W,Y)R3|-<X0,XW0,XY0,

so that, after using the triangle inequality, the integral in (5.41) is bounded by

J:=-0e2XX0e-W|h(W)|dW2dX=We2Xe-We-Y|h(W)h(Y)|dYdWdX.

Next, put

W1:=(X,W,Y)R3|-<XW,WY0,-<W0

and

W2:=(X,W,Y)R3|-<XY,YW0,-<Y0,

so W=W1W2 and W1W2 has measure zero. Then

J=J1+J2,

where

J1:=W1e2Xe-We-Y|h(W)h(Y)|dYdWdX

and

J2:=W2e2Xe-We-Y|h(W)h(Y)|dYdWdX.

Since the integrands are symmetric in W and Y, it suffices to show

J1C-0|h(X)|2dX.

Change variables to obtain

J1=-0W0-We2XdXe-We-Y|h(W)h(Y)|dYdW=12-0W0eWe-Y|h(W)h(Y)|dYdW.

Now we estimate

4|J1|J12+J13, 5.42

where

J12:=-0W0eWe-Y|h(W)|2dYdWandJ13:=-0W0eWe-Y|h(Y)|2dYdW.

We first evaluate

J12=-0W0e-YdYeW|h(W)|2dW=-0(1-eW)|h(W)|2dW.

Since W0 we have |1-eW|2, and so

J122-0|h(W)|2dWChL22. 5.43

Next, we change variables in J13 to find

J13=-0-YeWdWe-Y|h(Y)|2dY=-0|h(Y)|2dYhL22. 5.44

Combining the decomposition (5.42) and the estimates (5.43) and (5.44) gives

|J1|ChL22,

as desired.

Analysis of the long wave problem

The perturbation Ansatz for the long wave problem (3.42)

Throughout this section we keep q(0,c0/τ2) fixed. We make the perturbation Ansatz

ψ1=σ+η1andψ2=ζ+η2 6.1

for the long wave problem (3.42). Here η1Hq,01, which was defined in (5.2), and η2W1,. We abbreviate

η=(η1,η2)X:=Hq,01×W1,,

where X has the norm

ηX:=η1Hq1+η2W1,.

The Ansatz (6.1) solves the system (3.42) if and only if η1 and η2 solve

Tη1=k=15V1kν(η),η2=k=13V2kν(η), 6.2

where T was defined in (3.43) and the V-operators are given by

V11ν(η):=(M(ν)-M(0))[R1ν(σ+η1)(σ+η1)],V12ν(η):=M(0)[(R1ν(σ+η1)-R10(σ+η1))(σ+η1)],V13ν(η):=M(0)[(R10(σ+η1)-R10(σ)-DR10(σ)η1)σ],V14ν(η):=M(0)[(R10(σ+η1)-R10(σ))η1],V15ν(η):=ν1/2M(0)Nν(σ+η1,ζ+η2) 6.3

and

V21ν(η):=P1ν(σ+η1)-P10(σ+η1),V22ν(η):=P10(σ+η1)-ζ,V23ν(η):=νP2ν(σ+η1,ζ+η2). 6.4

We recall that the symbol of M(ν) was defined in (3.40) and the symbol of M(0) in (3.21). The operator R1ν was defined in (3.35), the operator Nν in (3.38), the operator P1ν in (3.33) and the operator P2ν in (3.34).

Due to Proposition 5.1, the first equation in (6.2) is equivalent to

η1=T-1k=15V1kν(η)=:N1ν(η). 6.5

Subsequently, η1 and η2 solve (6.2) if and only if

η2=V21ν(η)+V22ν(N1ν(η))+V23ν(η)=:N2ν(η). 6.6

We have replaced η1 with its fixed point expression (6.5) in V22ν for the sake of better estimates later; see Appendix B.2.7 for a more precise discussion. Finally, set

Nν(η):=(N1ν(η),N2ν(η)), 6.7

so Nν maps X to X. More precisely, this follows from the mapping estimates in Appendix B.3. We conclude that the problem (6.2) is equivalent to the fixed point problem

η=Nν(η), 6.8

which we now solve.

The solution of the fixed point problem (6.8)

For r>0, we define the ball

B(r):=ηX|ηXr.

We prove the following estimates in Appendix B; their verifications are routine, but detailed, so we do not present them here.

Proposition 6.1

There exist C, ν>0 such that if 0<ν<ν then the following hold.

  • (i)

    If ηB(Cν1/3), then Nν(η)B(Cν1/3).

  • (ii)
    If η, η`B(Cν1/3), then
    Nν(η)-Nν(η`)X12η-η`X.

Proposition 6.1 then guarantees that Nν is a contraction on B(Cν1/3) for each 0<ν<ν, and so Banach’s fixed point theorem gives the following solution to (6.2).

Proposition 6.2

Let C, ν>0 be as in Proposition 6.1. For each 0<ν<ν, there exists a unique ηνB(Cν1/3) such that ην=Nν(ην).

The existence of the perturbation terms ην enables us to conclude our main results, which are paraphrased nontechnically in (1.5).

Theorem 6.3

Let α, κ, τ1, τ2>0, q(0,c0/τ2), and θR. Define the leading-order profile terms

ϕA(X):=66c09/2τ2exp(2c0X/τ2+θ)[ακτ1+6c02exp(2c0X/τ2+θ)]3/2,ϕP(X):=((6c0)1/2α)1[ακτ1+6c02exp(2c0X/τ2+θ)/τ2)]1/2,

and

ϕR(X):=(3ακc0)1ακτ1+6c02exp(2c0X/τ2+θ)/τ2).

There exists ϵ>0 such that for each 0<ϵ<ϵ, there are ϕAϵHq1C and ϕPϵ, ϕRϵW1,C with the following properties.

  • (i)
    Let
    Aj(t)=ϵϕA(ϵ2/5(j-ϵ2/5c0t))+ϵ17/15ϕAϵ(ϵ2/5(j-ϵ2/5c0t)),Pj(t)=ϵ1/5ϕP(ϵ2/5(j-ϵ2/5c0t))+ϵ1/3ϕPϵ(ϵ2/5(j-ϵ2/5c0t)),
    and
    Rj(t)=ϵ2/5ϕR(ϵ2/5(j-ϵ2/5c0t))+ϵ3/5ϕRϵ(ϵ2/5(j-ϵ2/5c0t)).
    Then the triple (Aj,Pj,Rj) solves (1.1).
  • (ii)
    The remainder terms ϕAϵ, ϕPϵ, and ϕRϵ satisfy
    sup0<ϵ<ϵϕAϵHq1+ϕPϵW1,+ϕRϵW1,<.
  • (iii)
    The functions ϕPϵ and ϕRϵ vanish exponentially fast at + and are asymptotically constant at - in the following sense: there exist Pϵ, RϵR such that
    sup0<ϵ<ϵ|Pϵ|+supX0eqX|ϕPϵ(X)|+supX0e-qX|ϕPϵ(X)-Pϵ|<
    and
    sup0<ϵ<ϵ|Rϵ|+supX0eqX|ϕRϵ(X)|+supX0e-qX|ϕRϵ(X)-Rϵ|<.

Proof

Write the solution of (6.8), which exists due to Proposition 6.2, as ην=(η1ν,η2ν). Define

ψ1ν:=σ+η1νandψ2ν:=ζ+η2ν. 6.9

By the discussion at the start of Sect. 6.1, the pair (ψ1ν,ψ2ν) then solves the system (3.42).

Now take

Aj(t)=ν5/2ψ1ν(ν(j-νc0t))andPj(t)=ν1/2ψ2ν(ν(j-νc0t)).

This is the scaled travelling wave ansatz from (3.41), and so Proposition 3.5 guarantees that Aj and Pj thus defined solve the simplified system (2.14). Let Rj be given by (2.12). Then the discussion in Sect. 2.1 shows that Aj, Pj and Rj together solve our original problem (1.1).

Next, we use the identity ϵ=ν5/2 from (3.30) to reintroduce the original long wave parameter ϵ into the solutions. The expansions in (i) and the estimates in (ii) above then follow from (6.9) and the estimates in Proposition 6.2. The exact formulas for the leading order terms follow from the definitions of σ in (3.28) and ζ in (3.29). The asymptotics of part (iii) follow from the definition of ζ, the fixed point property η2ν=N2ν(ην) and the definition of N2ν in (6.6), and the definition of Rj from (2.12).

Finally, to obtain the smoothness of the solutions, we first note that σ, ζC. Next, crude estimates on the symbol of the Fourier multiplier M(ν), which we omit, allow us to invoke Lemma A.2 to conclude M(ν)B(Hqr,Hqr+1) for each ν0 and r0; we make no claim about uniform estimates in ν here. This smoothing property of M(ν), as well as the smoothing properties of the integral operators that compose N2ν, show that if ηCr×C2, then Nν(η)Cr+1×Cr+1. By bootstrapping, we obtain ηνC×C.

In order to achieve the normalization ϕAL=1, as discussed in Sect. 1.4, we need to use the explicit choice

c0=9ακτ1τ2281/5=:c, 6.10

as employed in (1.5). From (6.10), we obtain

ϕPL=6ακτ11/29ακτ1τ2281/10andϕRL=3τ19ακτ1τ2281/5. 6.11

Substituting the abbreviations (2.2) and (2.3) into the quantities in (6.10) and (6.11) then leads to the identities (1.8). This completes the rigorous derivation of the main results that we discussed more informally in Sect. 1.4.

Supplementary Information

Below is the link to the electronic supplementary material.

Acknowledgements

We acknowledge support from the Netherlands Organization for Scientific Research (NWO) (Grants 639.032.612, HJH, TEF; 865.17.004, RM)

Appendix A. Fourier analysis

A.1. The Fourier transform

We use the following conventions for Fourier transforms. If fL1, then its Fourier transform is

F[f](k)=f^(k):=12π-f(x)e-ikxdx,

and its inverse Fourier transform is

graphic file with name 285_2022_1793_Equ402_HTML.gif

A.2. Fourier multipliers on Sobolev spaces

For integers r0, we denote by Hr=Hr(R) the usual Sobolev space of all r-times weakly differentiable functions whose weak derivatives are square-integrable.

Our fundamental operator on Sobolev spaces is the Fourier multiplier. The following result above is standard; see, e.g., Faver (2018, Lem. D.2.1).

Lemma A.1

Let M~:RC be measurable and suppose

NM~(r,s):=supkR|M~(k)|(1+k2)(r-s)/2<.

Then the Fourier multiplier M with symbol M~ defined by

Mf:=F-1[M~f^], A.1

i.e., by Mf^(k)=M~(k)f^(k), is a bounded operator from Hr to Hs, and

MB(Hr,Hs)=NM~(r,s). A.2

We also need a convenient expression for ‘scaled’ Fourier multipliers. If f is a function on R and νR\{0}, let f(ν·) be the ‘scaled’ map xf(νx). Now let M be the Fourier multiplier with symbol M~ and define M~(ν)(k):=M~(νk). Let M(ν) be the Fourier multiplier with symbol M~(ν). Then standard scaling properties of the Fourier transform imply that

M[f(ν·)](x)=(M(ν)f)(νx). A.3

A.3. Fourier multipliers on weighted Sobolev spaces

We frequently work with weighted Sobolev spaces. For qR, let

Hqr:=fHqr|eq|·|fHr.

We norm this space by

fHqr:=eq|·|fHr,

and, see Faver (2018, App. C), this norm is equivalent to

fj=0req|·|xj[f]L2.

We put Lq2:=Hq0. The Cauchy–Schwarz inequality guarantees that Lq2 embeds into L1:

fL1=e-q|·|(eq|·|f)L1e-|q·|L2eq|·|fL2CqfLq2.

Finally, if IR is an interval, we sometimes denote by Lq2(I) the set of all measurable functions f:IC such that

Ie2q|X||f(X)|2dX<.

Since HqrHr, any Fourier multiplier defined on Hr is defined on Hqr. A variation on a result of Beale (1980, Lem. 5.1) gives sufficient conditions for a Fourier multiplier on Hqr to map into another weighted space Hqs.

Lemma A.2

(Beale) Fix q>0 and let

U¯q:=zC||Im(z)|q.

Let M~ be analytic on U¯q. Suppose there exist s0 and C, r0>0 such that if zU¯q and r0<|z|, then

|M~(z)|C|Re(z)|(s-r).

Then the Fourier multiplier M with symbol M~, defined by (A.1), is a bounded operator from Hqr to Hqs and

MB(Hqr,Hqs)supkR|(1+k2)(s-r)/2M~(k±iq)|.

Appendix B. The Proof of Proposition 6.1

Our proof depends on the following lemma, which we prove in the subsequent parts of this appendix.

Lemma B.1

Let νM>0 be as in Proposition 4.1. There exist CN, ρN>0 such that if 0<ν<νM and η1Hq1, η`1Hq1, η2Hq1, η`2Hq1ρN, then the following hold.

  • (i)

    Nν(η)XCN(ν1/3+ηX2).

  • (ii)

    Nν(η)-Nν(η`)XCN(ν1/3+ηX+η`X)η-η`X.

Assuming this lemma to be true, we define

C:=CNandν:=12minνM,1,1(1+C2)6,164C6(1+2C)6,ρN.

Take 0<ν<ν and η, η`B(Cν). Then by part (i) of Lemma B.1 we have

Nν(η)XCN(ν1/3+ηX2)C[C(1+C2)ν1/6]ν1/3Cν1/3.

This proves part (i) of Proposition 6.1. Next, part (ii) of that lemma gives

Nν(η)-Nν(η`)XCN(ν1/3+2CNν1/6)η-η`XC(1+2C)ν1/6η-η`X12η-η`X.

This proves part (ii) of Proposition 6.1.

In the remainder of this appendix, we first give some essential auxiliary estimates in Appendix B.1. Then we prove the Lipschitz estimates of part (ii) of Proposition 6.1 in Appendix B.2. Finally, using in part these Lipschitz estimates, we prove in Appendix B.3 the mapping estimates from part (i) of the proposition.

B.1. Auxiliary estimates

Throughout this appendix we will frequently obtain estimates in terms of the L1- or L-norms of a function fHq1. Afterwards we can use the embedding of Lq2 into L1 and the corresponding inequalities

fL1CfLq2CfHq1

for fHq1, as well as the Sobolev embedding, to turn these L1- and L-estimates into Hq1 estimates. For brevity, we will omit those details.

We will also use the operator A defined in (5.4); we recall

(Af)(X)=Xf(W)dW

for fHq1, so that

f=-X[Af]andAfLCfL1.

Last, we will use the shift operator Sν, which satisfies

(Sνf)(X)=f(X+ν)

for any function f defined on R and any νR.

The operator A and the definitions of our fundamental operators P1ν in (3.33) and R1ν in (3.35) allow us to rewrite

P1ν(f)(X)=αc0A[E(ν1/2Sνf)(·,X)f](X)

and

R1ν(f)(X)=αc02τ1XA[E(ν1/2Sνf)(·,V)f](V)(Sνf)(V)dV.

Now we begin our estimates on E, P1ν, and R1ν in earnest.

Lemma B.2

There exists C>0 such that if fL1, f`L11, then the following hold.

  • (i)

    |E(f)(V,X)-E(f`)(V,X)|Cf-f`L1 for all V, XR.

  • (ii)

    |E(f)(V,X)|C for all V, XR.

Proof
  • (i)
    Since
    κc0VXf(U)dUκc0fL1
    for all V, XR, a local Lipschitz estimate on the exponential yields C>0 such that if fL1, f`L11, then
    |E(f)(V,X)-E(f`)(V,X)|CVXf(U)dU-VXf`(U)dUCf-f`L1.
  • (ii)

    Since E(0)=0, this follows from part (i) by taking f`=0.

The following lemma guarantees that P1ν maps Hq1 to W1,, among other results.

Lemma B.3

There exists C>0 such that if 0ν<1 and f, f`Hq1 with fHq1, f`Hq11, then the following hold.

  • (i)

    P1ν(f)-P1ν(f`)LC(ν1/2fHq1+1)f-f`Hq1.

  • (ii)

    P1ν(f)LCfHq1.

  • (iii)

    P1ν(f)-P10(f)LCν1/2fHq12.

  • (iv)

    X[P1ν(f)-P10(f)]LCν1/2fHq12.

  • (v)

    (P1ν(f)-P10(f))-(P1ν(f`)-P10(f`))LCν1/2(fHq1+f`Hq1)f-f`Hq1.

  • (vi)

    X[P1ν(f)-P10(f)])-(X[P1ν(f`)-P10(f`)]LCν1/2(fHq1+f`Hq1)f-f`Hq1.

Proof

As we mentioned earlier, in most cases we will conclude bounds in terms of L- or L1-norms, which then immediately yield the Hq1-bounds stated above.

  • (i)
    We have
    P1ν(f)(X)-P1ν(f`)(X)=I1ν(f,f`)(X)+I2ν(f,f`)(X),
    where
    I1ν(f,f`)(X):=αc0X(E(ν1/2Sνf)(V,X)-E(ν1/2Sνf`)(V,X))f(V)dV
    and
    I2ν(f,f`)(X):=αc0XE(ν1/2Sνf`)(V,X)(f(V)-f`(V))dV.
    We use part (i) of Lemma B.2 to bound
    |E(ν1/2Sνf)(V,X)-E(ν1/2Sνf`)(V,X)|Cν1/2Sνf-Sνf`L1=Cν1/2f-f`L1 B.1
    for all V, XR. Thus
    |I1ν(f,f`)(X)|Cν1/2f-f`L1X|f(V)|dVCν1/2f-f`L1fL1
    for all XR.
    Next, we use part (ii) of Lemma B.2 to bound
    |I2ν(f,f`)(X)|CX|f(V)-f`(V)|dVCf-f`L1.
  • (ii)

    Since Pν(0)=0, this follows from part (i) by taking f`=0.

  • (iii)
    We have
    P1ν(f)(X)-P10(f)(X)=αc0X(E(ν1/2Sνf)(V,X)-1)f(V)dV. B.2
    Since
    E(ν1/2Sνf)(V,X)-1=E(ν1/2Sνf)(V,X)-E(0)(V,X),
    we may use part (i) of Lemma B.2 to bound
    |E(ν1/2Sνf)(V,X)-1|Cν1/2SνfL1=Cν1/2fL1. B.3
    Thus
    |P1ν(f)(X)-P10(f)(X)|Cν1/2fL1X|f(V)|dVCν1/2fL12.
  • (iv)
    We first differentiate under the integral and use the condition E(g)(X,X)=1, apparent from the definition of E in (3.3) and valid for all integrable g and XR, to calculate
    X[P1ν(f)](X)=-αc0f(X)+αc02ν1/2XE(ν1/2Sνf)(V,X)f(V+ν)f(V)dV.
    Then
    X[P1ν(f)-P10(f)](X)=αc02ν1/2XE(ν1/2Sνf)(V,X)f(V+ν)f(V)dV. B.4
    Part (ii) of Lemma B.2 then guarantees
    X[P1ν(f)-P10(f)]LCν1/2fLfL1.
  • (v)
    We use (B.2) to write
    (P1ν(f)-P10(f))-(P1ν(f`)-P10(f`))=I3ν(f,f`)+I4ν(f,f`),
    where
    I3ν(f,f`)(X):=αc0X(E(ν1/2Sνf)(V,X)-E(ν1/2Sνf`)(V,X))f(V)dV
    and
    I4ν(f,f`)(X):=αc0X(E(ν1/2Sνf`)(V,X)-1)(f(V)-f`(V))dV.
    We use (B.1) to estimate
    |I3ν(f,f`)(X)|Cν1/2f-f`L1X|f(V)|dVCν1/2fL1f-f`L1.
    We use (B.3) to estimate
    |I3ν(f,f`)(X)|Cν1/2f`L1X|f(V)-f`(V)|dVCν1/2f`L1f-f`L1.
  • (vi)
    Using (B.4), we have
    X[P1ν(f)-P10(f)](X)-X[P1ν(f`)-P10(f`)](X)=αc02ν1/2X[E(ν1/2Sνf)(V,X)f(V+ν)f(V)-E(ν1/2Sνf`)(V,X)f`(V+ν)f`(V)]dV.
    The estimate follows in a manner analogous to the proof of part (v) above, so we omit the details.

The next lemma guarantees that R1ν maps Hq1 to W1,.

Lemma B.4

There exists C>0 such that if 0ν<1 and fHq1, f`Hq11, then the following hold.

  • (i)

    Rν(f)LCfHq12.

  • (ii)

    X[Rν(f)]LCfHq12.

  • (iii)

    Rν(f)-Rν(f`)LC(ν1/2+fHq1+f`Hq1)f-f`Hq1.

  • (iv)

    X[Rν(f)-Rν(f`)]LC(ν1/2+fHq1+f`Hq1)f-f`Hq1

  • (v)

    Rν(f)-R10(f)LCν1/2fHq12.

  • (vi)

    (Rν(f)-R10(f))-(Rν(f`)-R10(f`))LC(ν1/2+fHq1+f`Hq1)f-f`Hq1.

  • (vii)

    Rν(f)-R10(f)LCν1/2fHq12.

Proof

Throughout we will use the inequality

Rν(f)LP1ν(f)(Sνf)L1.

As before, we stop when we have bounds in terms of L1- or L-norms.

  • (i)
    We use part (ii) of Lemma B.3 to bound
    Rν(f)L=CP1ν(f)(Sνf)L1CP1ν(f)LSνfL1CfL12.
  • (ii)
    We have
    X[Rν(f)]=-αc02τ1P1ν(f)(Sνf),
    thus
    X[Rν(f)]LCP1ν(f)(Sνf)LCP1ν(f)LfHq1CfHq12
    by the Sobolev embedding and part (ii) of Lemma B.3.
  • (iii)
    We use parts (i) and (ii) of Lemma B.3 to bound
    Rν(f)-Rν(f`)LC(P1ν(f)-P1ν(f))fL1+CP1ν(f`)(Sν(f-f`))L1CP1ν(f)-P1ν(f`)LfL1+CP1ν(f`)LSν(f-f`)L1C(ν1/2fL1+1)fL1f-f`L1+Cf`L1f-f`L1.
  • (iv)
    We have
    X[Rν(f)-Rν(f`)]=αc02τ1P1ν(f`)(Sνf`)-αc02τ1P1ν(f)(Sνf),
    thus
    X[Rν(f)-Rν(f`)]LC(P1ν(f)-P1ν(f`))f`L+CP1ν(f`)(Sν(f-f`))L.
    We use part (i) of Lemma B.3 and the Sobolev embedding to estimate
    (P1ν(f)-P1ν(f`))f`LP1ν(f)-P1ν(f`)LfHq1C(ν1/2fL1+1)fHq1f-f`L1
    and part (ii) of Lemma B.3 and the Sobolev embedding to estimate
    P1ν(f`)(Sν(f-f`))LCP1ν(f`)Lf-f`LCfL1f-f`Hq1.
  • (v)
    We first estimate
    Rν(f)-R10(f)LCP1ν(f)(Sνf)-P10(f)fL1C(P1ν(f)-P10(f))(Sνf)L1+CP10(f)(Sνf-f)L1.
    Then part (iii) of Lemma B.3 gives
    (P1ν(f)-P10(f))(Sνf)L1P1ν(f)-P10(f)LSνfL1Cν1/2fL13.
    Next, part (ii) of Lemma B.3 implies
    P10(f)(Sνf-f)L1P10(f)LSνf-fL1CfL1(Sν-1)fL1.
    Since fHq1, we have
    (Sν-1)fL1Cq(Sν-1)fLq2.
    It follows from Faver and Wright (2018, Lem. A.11) that
    (Sν-1)fLq2CνfHq1.
  • (vi)
    We estimate
    (Rν(f)-R10(f))-(Rν(f`)-R10(f`))LC(P1ν(f)(Sνf)-P10(f)f)-(Pν(f`)(Sνf`)-P10(f`)f`)L1C(P1ν(f)-P1ν(f`))(Sνf)L1+CP1ν(f`)(Sν(f-f`))L1+C(P10(f)-P10(f`))f`L1+CP10(f)(f-f`)L1.
    We use part (ii) of Lemma B.3 to bound
    P1ν(f`)(Sν(f-f`))L1+P10(f)(f-f`)L1P1ν(f`LSν(f-f`)L1+P10(f)Lf-f`L1CfL1f-f`L1.
    We use part (i) of Lemma B.3 to bound
    (P1ν(f)-P1ν(f`))(Sνf)L1+(P10(f)-P10(f`))f`L1P1ν(f)-P1ν(f`)LSνfL1+P10(f)-P10(f`)Lf`L1C(ν1/2fL1+1)fL1f-f`L1+Cf`L1f-f`L1.
  • (vii)

    We use part (vi) with f`=0.

Finally, we present estimates on the operators Nν defined in (3.38) and P2ν from (3.34).

Lemma B.5

There exist C, ρ0>0 such that if 0ν<1, then the following hold.

  • (i)
    If f, f`Hq1 and g, g`W1, with fHq1+gW1,ρ0 and f`Hq1+g`W1,ρ0, then
    Nν(f,g)-Nν(f`,g`)Lq2+P2ν(f,g)-P2ν(f`,g`)Hq1C(ν1/2+fHq1+f`Hq1+gW1,+g`W1,)(f-f`Hq1+g-g`W1,).
  • (ii)
    If fHq1 and gW1, with fHq1+gW1,ρ0, then
    Nν(f,g)Lq2+P2ν(f,g)W1,C.
Proof

Part (ii) follows from part (i) since Nν(0,0)=P2ν(0,0)=0. The proof of the Lipschitz estimates in part (i) follows exactly the strategies deployed above, and we would learn almost nothing new from seeing its argument, so we omit that. The one difference here is that Nν and P2ν incorporate the maps Q1ν and Q2ν, which were defined in (3.32) and which are really rational functions from R2 to R. A glance at the formulas for Q1ν and Q2ν provides ρQ>0 such that if 0<ν<1, then Q1ν and Q2ν are defined and smooth on the ball (X,Y)R2||X|+|Y|ρQ. By taking fHq1+gW1,ρ0 for some small ρ0>0, we can guarantee that the compositions involving Q1ν and Q2ν with f, g, and other operators acting on f and g are all defined and satisfy tame Lipschitz estimates.

B.2. Lipschitz estimates

We first prove the Lipschitz estimates undergirding part (ii) of Lemma B.1, which we then use to prove the mapping estimates in part (i). From (6.7), we have Nν=(N1ν,N2ν), where N1ν was defined in (6.5) and N2ν in (6.6). Using these definitions and the boundedness of the operator T-1 from Proposition 5.1, we can prove part (ii) of Lemma B.1 if we show

k=15(V1kν(η)-V1kν(η`)Hq1)+(V21ν(η)-V21ν(η`)W1,)+V23ν(η)-V23ν(η`)W1,)CRν(η,η`),

where

Rν(η,η`):=(ν1/3+η1Hq1+η`1Hq1+η2W1,+η`2W1,)(η1-η1`Hq1+η2-η`2W1,).

The terms V1kν were defined in (6.3) and V2kν in (6.4).

B.2.1. Lipschitz estimates on V11ν

We use the estimate on M(ν)-M(0) from Proposition 4.1 to obtain

V11ν(η)-V11ν(η`)Hq1Cν1/3(Rν(σ+η1)-Rν(σ+η`1))(σ+η`1)Hq1+Cν1/3Rν(σ+η1)(η1-η`1)Hq1.

We first estimate

(Rν(σ+η1)-Rν(σ+η`1))(σ+η`1)Hq1X[Rν(σ+η1)-Rν(σ+η`1)](σ+η`1)Lq2+(Rν(σ+η1)-Rν(σ+η`1))X[σ+η`1]Lq2,

where

X[Rν(σ+η1)-Rν(σ+η`1)](σ+η`1)Lq2X[Rν(σ+η1)-R1ν(σ+η`1)]Lσ+η`1Lq2C(ν1/2+η1Hq1+η`1Hq1)η1-η`1Hq1

by part (iv) of Lemma B.4 and

(R1ν(σ+η1)-R1ν(σ+η`1))X[σ+η`1]Lq2,R1ν(σ+η1)-R1ν(σ+η`1)LX[σ+η`1]Lq2C(ν1/2+η1Hq1+η`1Hq1)η1-η`1Hq1

by part (iii) of Lemma B.4.

Next we estimate

R1ν(σ+η1)(η1-η`1)Hq1X[R1ν(σ+η1)](η1-η`1)Lq2+R1ν(σ+η1)X[η1-η`1]Lq2,

where

X[R1ν(σ+η1)](η1-η`1)Lq2X[R1ν(σ+η1)]Lη1-η`1Lq2Cσ+η1Hq12η1-η`1Hq1Cη1-η`1Hq1

by part (ii) of Lemma B.4 and

R1ν(σ+η1)X[η1-η`1]Lq2R1ν(σ+η1)LX[η1-η`1]Lq2Cσ+η1Hq12η1-η`1Hq1Cη1-η`1Hq12.

by part (i) of Lemma B.4.

B.2.2. Lipschitz estimates on V12ν

We use the smoothing property of M(0) from Lemma 3.1 to bound

V12ν(η)-V12ν(η`)Hq1C[(R1ν(η1)-R10(η1))-(R1ν(η`1)-R10(η`1))](σ+η1)Lq2+C(R1ν(η`1)-R10(η`1))(η1-η`1)Lq2.

Call the two Lq2-norm terms above I and II. We estimate

I(R1ν(η1)-R10(η1))-(R1ν(η`1)-R10(η`1))Lσ+η1Lq2C(ν1/2+η1Hq1+η`1Hq1)η1-η`1Hq1.

by part (vi) of Lemma B.4 and

IIR1ν(η`1)-R10(η`1)Lη1-η`1Lq2Cν1/2η`1Hq1η1-η`1Hq1

by part (vii) of Lemma B.4.

B.2.3. Lipschitz estimates on V13ν

We use again the smoothing property of M(0) to bound

V13ν(η)-V13ν(η`)Hq1C(R10(σ+η1)-R10(σ)-DR10(σ)η1)σLq2CR10(σ+η1)-R10(σ)-DR10(σ)η1LσLq2.

Next we will use the following ‘difference of squares’ estimate, which is proved using the fundamental theorem of calculus. We thank J. Douglas Wright for pointing out this lemma to us.

Lemma B.6

Let X and Y be Banach spaces with ZX open and convex and with 0Z. Let fC1(Z,Y) with Df(0)=0, and suppose

LipZ(Df):=supx,x`Zxx`Df(x)-Df(x`)B(X,Y)x-x`X<.

Then

f(x)-f(x`)Y12LipZ(Df)(xX+x`X)x-x`X.

We apply this lemma to f(η1):=R10(σ)η1)-R10(σ)-DR10(σ)η1, which is infinitely differentiable as a map from Hq1 to W1, by Remark 3.4, to conclude

R10(σ+η1)-R10(σ)-DR10(σ)η1LC(η1Hq1+η`1Hq1)η1-η`1Hq1.
B.2.4. Lipschitz estimates on V14ν

We smooth with M(0) once more, and then we use the fundamental theorem of calculus and the smoothness of R10 to rewrite

V14ν(η)-V14ν(η`)Hq1CILq2+CIILq2,

where

I:=01(DR10(σ+sη1)-DR10(σ+sη`1))dsη12

and

II:=01DR10(σ+sη`1)ds(η1+η`1)(η1-η`1).

Then

ILq201(DR10(σ+sη1)-DR10(σ+sη`1))dsLη1Lq2

and

IILq201DR10(σ+sη`1)dsLη1+η`1Lη1-η`1Lq2.

We conclude

ILq2Cη1Hq1η1-η`1Hq1

via a Lipschitz estimate on DR10 and

IILq2C(η1Hq1+η`1Hq1)η1-η`1Hq1

via the boundedness of DR10.

B.2.5. Lipschitz estimates on V15ν

We smooth with M(0) to estimate

V15ν(η)-V15ν(η`)Hq1Cν1/2Nν(σ+η1,ζ+η2)-Nν(σ+η`1,ζ+η`2)Lq2.

The desired estimate then follows from part (i) of Lemma B.5.

B.2.6. Lipschitz estimates on V21ν

This is a direct application of parts (v) and .(vi) of Lemma B.3.

B.2.7. Lipschitz estimates on V22νN1ν

We have

V22ν(N1ν(η))(X)=P10(σ+N1ν(η))(X)-P10(σ)(X)=αc0XN1ν(η)(V)dV. B.5

The desired Lipschitz estimate on V22ν then follows at once from the Lipschitz estimate

N1ν(η)-N1ν(η`)Hq1CRν(η,η`),

which we proved in Appendix B.2.1 through B.2.5. Without having substituted N1ν(η) for η1 in the process of defining N2ν in (6.6), we would have only a useless O(1) estimate here.

B.2.8. Lipschitz estimates on V23ν

This is a direct application of part (i) of Lemma B.5.

B.3. Mapping estimates

We prove the mapping estimates that deliver part (i) of Lemma B.1 and rely mostly on the preceding Lipschitz estimates. Due to the boundedness of T-1, it suffices to show

k=15V1kν(η)Hq1+V21ν(η)W1,+V23ν(η)W1,C(ν1/3+η1Hq12+η2W1,2).
B.3.1. Mapping estimates on V11ν

We estimate

V11ν(η)Hq1V11ν(η)-V11ν(0)Hq1+V11ν(0)Hq1,

where

V11ν(η)-V11ν(0)Hq1Cν1/3η1Hq12

by the Lipschitz estimates in Appendix B.2.1 and

V11ν(0)Hq1=(M(ν)-M(0))[R1ν(σ)σ]Hq1Cν1/3

by Proposition 4.1.

B.3.2. Mapping estimates on V12ν

We estimate

V12ν(η)Lq2V12ν(η)-V12ν(0)Lq2+V12ν(0)Lq2,

where

V12ν(η)-V12ν(0)Lq2C

by the Lipschitz estimates in Appendix B.2.1 and

V12ν(0)Lq2=(R1ν(σ)-R10(σ))σLq2R1ν(σ)-R10(σ)LσLq2Cν1/2

by part (vii) of Lemma B.4.

B.3.3. Mapping estimates on V13ν

Because V13ν(0)=0, these follow from the Lipschitz estimates for V13ν that we developed above in Appendix B.2.3.

B.3.4. Mapping estimates on V14ν

Because V14ν(0)=0, these follow from the Lipschitz estimates for V14ν that we developed above in Appendix B.2.3.

B.3.5. Mapping estimates on V15ν

The estimates are analogous to those in Appendix B.3.1, except now we use Lemma B.5 instead of the Lipschitz estimates in Appendix B.2.1.

B.3.6. Mapping estimates on V21ν

These estimates follow directly from parts (iii) and (iv) of Lemma B.3.

B.3.7. Mapping estimates on V22νN1ν

We obtain these estimates by first rewriting V22νN1ν via the identity (B.5) and then using the mapping estimates on N1ν developed in Appendices B.3.1 through B.3.5.

B.3.8. Mapping estimates on V23ν

This estimate follows from part (ii) of Lemma B.5.

Data availability statement

The datasets generated during the current study are available from the corresponding author on reasonable request.

Declarations

Conflict of interest

The authors have no relevant financial or non-financial interests to disclose.

Footnotes

1

For presentation purposes, the parameters L and r appearing in Merks et al. (2007) have been set to unity.

2

Here we use the abbreviation A=supj,t|Aj(t)| and its analogues for P and R.

3

We define the width of the auxin pulse as the distance between the two points where the pulse attains 5% of its maximum value.

Publisher's Note

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Contributor Information

Bente Hilde Bakker, Email: b.h.bakker@math.leidenuniv.nl.

Timothy E. Faver, Email: tfaver1@kennesaw.edu

Hermen Jan Hupkes, Email: hhupkes@math.leidenuniv.nl.

Roeland M. H. Merks, Email: merksrmh@math.leidenuniv.nl

Jelle van der Voort, Email: jelvoort@live.nl.

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Associated Data

This section collects any data citations, data availability statements, or supplementary materials included in this article.

Supplementary Materials

Data Availability Statement

The datasets generated during the current study are available from the corresponding author on reasonable request.


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