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Characteristic integrals and general solution of the Ferapontov-Shabat-Yamilov lattice

Dmitry K. Demskoi School of Computing and Mathematics, Charles Sturt University, NSW 2678, Australia ddemskoy@csu.edu.au
Abstract

For the finite (non-periodic) systems obtained from a lattice introduced by Ferapontov and independently by Shabat and Yamilov, we present a quadrature-free general solution and a recurrent formula for the characteristic integrals. The derivation of these formulae relies on the underlying determinantal equations. We illustrate the results using a two-component system.

1 Introduction

The lattice equation

tx2vn=tvnxvn(1vnvn11vn+1vn),\partial^{2}_{tx}v_{n}=\partial_{t}v_{n}\partial_{x}v_{n}\left(\frac{1}{v_{n}-v_{n-1}}-\frac{1}{v_{n+1}-v_{n}}\right), (1)

which we refer to as Ferapontov-Shabat-Yamilov (FSY) lattice, was introduced independently in [1] and [2]. In the work of Shabat and Yamilov, equation (1) was derived as one of the examples in the list of two-dimensional generalisations of the Toda-type lattices. There is a close connection between the latter and the nonlinear Shrödinger-type (NLS) systems: the lattices serve as auto-Bäcklund transformations for the NLS-type systems. Respectively, the two-dimensional generalisations of the Toda-type lattices play a role of auto-Bäcklund transformations of Davey-Stewartson-type systems. It turns out that (1) is compatible with the well-known Ishimori equation which is a two-dimensional generalization of the Heisenberg spin model [3, 4].

In the work of Ferapontov, the lattice (1) emerged in the context of two-component hydrodynamic-type systems in Riemann invariants. It was shown that the characteristic velocities of such systems, related by the Laplace transformation, satisfy lattice (1). Ferapontov also investigated periodic reductions of the corresponding chain of the Laplace transformation and lattice (1).

In regards to the integrability of reductions of lattice equations, normally the periodic boundary conditions, i.e. vn+N=vnv_{n+N}=v_{n}, lead to solitonic equations, whereas finite (non-periodic) reductions, often referred to as cutoff constraints, yield linearisable equations. For hyperbolic lattices like (1), the finite reductions turn out to be Darboux integrable. This type of integrability is characterised by existence of complete sets of integrals along each characteristic direction.

A finite reduction of the lattice (1) corresponding to the boundary condition

v0=0,vN=v_{0}=0,\ \ v_{N}=\infty (2)

was introduced by the author [5] in connection with the determinantal equation

|uututtuxutxuttxuxxutxxuttxx|=0,\left|\begin{array}[]{cccc}u&u_{t}&\ldots&u_{t\ldots t}\\ u_{x}&u_{tx}&\ldots&u_{t\ldots tx}\\ \vdots&\vdots&\ddots&\vdots\\ u_{x\ldots x}&u_{tx\ldots x}&\ldots&u_{t\ldots tx\ldots x}\end{array}\right|=0, (3)

where

utt=tN1u,uxx=xN1u,uttxx=xN1tN1u,etc.u_{t\ldots t}=\partial_{t}^{N-1}u,\,u_{x\ldots x}=\partial_{x}^{N-1}u,\,u_{t\ldots tx\ldots x}=\partial_{x}^{N-1}\partial_{t}^{N-1}u,\,\mbox{etc.}

It was pointed out that the quantities below (see also formula (25))

v1=1u,v2=utx|uutuxutx|,v3=|utxuttxutxxuttxt||uututtuxutxuttxuxxutxxuttxx|,v_{1}=\frac{1}{u},\,v_{2}=\frac{u_{tx}}{\left|\begin{array}[]{ll}u&u_{t}\\ u_{x}&u_{tx}\end{array}\right|},\,v_{3}=\frac{\left|\begin{array}[]{ll}u_{tx}&u_{ttx}\\ u_{txx}&u_{ttxt}\end{array}\right|}{\left|\begin{array}[]{cccc}u&u_{t}&u_{tt}\\ u_{x}&u_{tx}&u_{ttx}\\ u_{xx}&u_{txx}&u_{ttxx}\end{array}\right|},\dots (4)

satisfy lattice (1).

On the other hand, equation (3) is known [6, 7, 8] to be closely related to the two-dimesional Toda lattice in the algebraic form

w0=1,tx2lnwn=wn+1wn1wn2,wN=0, 1<n<N.w_{0}=1,\ \ \displaystyle\partial^{2}_{tx}\ln w_{n}=\frac{w_{n+1}w_{n-1}}{w_{n}^{2}},\ \ w_{N}=0,\ \ 1<n<N. (5)

Specifically, the relationship between the scalar equation (3) and the lattice (5) is realised if we introduce the lattice variables wnw_{n} according to the formula

w1=u,w2=|uutuxutx|,w3=|uututtuxutxuttxuxxutxxuttxx|,\begin{array}[]{l}w_{1}=u,\,w_{2}=\left|\begin{array}[]{ll}u&u_{t}\\ u_{x}&u_{tx}\end{array}\right|,\,w_{3}=\left|\begin{array}[]{cccc}u&u_{t}&u_{tt}\\ u_{x}&u_{tx}&u_{ttx}\\ u_{xx}&u_{txx}&u_{ttxx}\end{array}\right|,\dots\end{array} (6)

i.e. quantities wnw_{n} represent the principal minors of the n×nn\times n matrix corresponding to the determinant in the left-hand side of formula (3).

The boundary condition

v0=a,vN=b,v_{0}=a,\,v_{N}=b, (7)

where a,b=const,a,b=\mbox{const}, is equivalent to (2) due to invariance of the lattice (1) under the Möbius transformation

φn=αvn+βγvn+δ.\varphi_{n}=\frac{\alpha v_{n}+\beta}{\gamma v_{n}+\delta}. (8)

Thus, by choosing the parameters such that (8) becomes

φn=(ab)vnabvn+a,ab,\varphi_{n}=\frac{(a-b)v_{n}}{a-b-v_{n}}+a,\ \ a\neq b, (9)

we observe that

φ0=a,φN=b,\varphi_{0}=a,\ \ \varphi_{N}=b, (10)

provided that vnv_{n} satisfies the condition (2). Furthermore, the degenerate case b=ab=a can be recovered in two steps:

  1. 1.

    Apply the reduction vN1=0v_{N-1}=0 in the system obtained from the condition (2). This implies the homogeneous boundary condition v0=0,vN1=0v_{0}=0,\,v_{N-1}=0;

  2. 2.

    Shift the variables: φn=vn+a.\varphi_{n}=v_{n}+a.

The Darboux integrability of the Toda lattice (5), defined as the existence of complete sets of characteristic integrals, is well-established [9]. Consequently, the lattice (1) with the boundary condition (2), or equivalently (7), is also Darboux integrable. Furthermore, an explicit formula for the characteristic integrals was provided in [5] (see formula (10) therein), where the integrals of (1) were expressed in terms of a single variable, u=1/v1u=1/v_{1}, and its derivatives. This formula yields characteristic integrals for all lattices derived from the scalar equation (3) by introducing lattice variables.

However, a more natural representation of the integrals should involve all lattice variables and avoid mixed derivatives. While such expressions can be derived from the aforementioned formula, the process becomes increasingly computationally expensive as the number of lattice variables grows. The related approaches in [10] and [11], which rely on the system’s linear representation (Lax pair), allow the construction of integrals as coefficients of a factorised differential operator. The drawback of this approach, however, is its labour-intensive nature, as it requires expanding the differential operator to determine its coefficients.

Thus, it would be advantageous to find a direct formula for the integrals that avoids the need to compute additional objects. In the following section, equation (1) will be derived from the determinantal equation (3) ab initio. Subsequently, recurrent formulae for the integrals and the general solutions will be calculated in the variables of the hyperbolic systems obtained by constraining lattice (1) with boundary conditions (2) and (10). In conclusion, we will discuss discrete and semi-discrete analogues of (1) that are related to the determinantal equation (3).

2 Determinantal structure of the FSY lattice

First, we introduce some notation to prepare the ground for a derivation of the lattice (1). Consider a function wnw_{n} defined by the nn-th order determinant

wn(u)=det(aij),w_{n}(u)=\mbox{det}\left(a_{ij}\right), (11)

where

ai+1,j+1=i+juxitj,i,j=1n1.\quad a_{i+1,j+1}=\frac{\partial^{i+j}u}{\partial x^{i}\partial t^{j}},\ \ i,j=1\dots n-1.

Hence, the argument of wnw_{n} is the entry in the top left corner of the determinant. Unless otherwise stated, it will be suppressed, i.e. wn=wn(u).w_{n}=w_{n}(u). In this notation, equation (3) can be re-stated as follows

wN(u)=0.w_{N}(u)=0. (12)

Without any further restrictions, wnw_{n} satisfies the lattice equation

w0=1,tx2lnwn=wn+1wn1wn2w_{0}=1,\ \ \displaystyle\partial^{2}_{tx}\ln w_{n}=\frac{w_{n+1}w_{n-1}}{w_{n}^{2}} (13)

which is infinite in the positive direction. Formula (11) is essentially a definition of new variables wnw_{n} which transform the scalar equation (3) into a chain of hyperbolic equations (13). Imposing the condition wN(u)=constw_{N}(u)=\mbox{const} turns (13) into a Darboux integrable system of PDEs. However, we note that (13) then implies wN+1(u)=0,w_{N+1}(u)=0, thus, without loss of generality we may assume that equation (12) is satisfied.

Jacobi determinantal identity.

We denote the minor of the entry in the pp-th row and qq-th column of the matrix (aij)(a_{ij}) as mpqm_{pq} and the minor obtained from (aij)(a_{ij}) by removing its pp- and qq-th rows as well as rr- and ss-th columns as mpqrsm_{pqrs}. In such notation, the Jacobi determinant identity can be written as follows [12]

mpqrswn=mprmqsmpsmqr.m_{pqrs}w_{n}=m_{pr}m_{qs}-m_{ps}m_{qr}. (14)

When it is necessary to indicate the order of minors mpqm_{pq} and mpqrsm_{pqrs} explicitly, we write mn;pqm_{n;pq} and mn;pqrsm_{n;pqrs} respectively. This notation means that the minors are obtained by deleting rows and columns from the n×nn\times n matrix (aij).(a_{ij}). We will refer to instances of the Jacobi identity by indicating the list of indices (p,q,r,s)(p,q,r,s).

Consider the ratios of the determinants:

Jn;p=mpnwn1,In;p=mnpwn1,p=1,,nJ_{n;p}=\frac{m_{pn}}{w_{n-1}},\ \ I_{n;p}=\frac{m_{np}}{w_{n-1}},\ \ p=1,\ldots,n (15)

with the values for p=np=n and p=0p=0:

Jn;n=In;n=1,Jn;0=In;0=0.J_{n;n}=I_{n;n}=1,\ \ J_{n;0}=I_{n;0}=0.

The quantities Jn;pJ_{n;p} and In;pI_{n;p} are connected by the involution txt\leftrightarrow x. Broadly speaking, they represent characteristic tt- and xx-integrals, respectively. A more precise description is provided below.

Proposition.

[13] The quantities Jn;pJ_{n;p} and In;pI_{n;p} satisfy the equations

tJn;p=wn2wnwn12Jn1;p,\partial_{t}J_{n;p}=\frac{w_{n-2}w_{n}}{w_{n-1}^{2}}J_{n-1;p}, (16)
Jn;p=Jn1;p1xJn1;p+Jn1;pxlnwn1wn2,J_{n;p}=J_{n-1;p-1}-\partial_{x}J_{n-1;p}+J_{n-1;p}\partial_{x}\ln\frac{w_{n-1}}{w_{n-2}}, (17)

and

xIn;p=wn2wnwn12In1;p,\partial_{x}I_{n;p}=\frac{w_{n-2}w_{n}}{w_{n-1}^{2}}I_{n-1;p}, (18)
In;p=In1;p1tIn1;p+In1;ptlnwn1wn2.I_{n;p}=I_{n-1;p-1}-\partial_{t}I_{n-1;p}+I_{n-1;p}\partial_{t}\ln\frac{w_{n-1}}{w_{n-2}}. (19)

Now the connection between the quantities Jn;pJ_{n;p} and In;pI_{n;p} on one hand, and the characteristic integrals of the lattice (5) on the other, is obvious. Indeed, if wn=0w_{n}=0 for some n=N,n=N, then, as follows from (16) and (18), formula (15) gives expressions for the characteristic integrals of equation (3) as well as of the lattice (5), depending on whether wn,w_{n}, present in the formulae are interpreted as determinants or the lattice variables as in (5), i.e.

tJN;p=0,xIN;p=0modwN=0.\partial_{t}J_{N;p}=0,\ \ \partial_{x}I_{N;p}=0\ \ \mbox{mod}\,\,w_{N}=0.

Thus, we have 2N22N-2 integrals which equals the order of equation (3). Additionally, the independence of these integrals is evident from their structure in (15). Indeed, all these integrals have the same order, 2N3,2N-3, yet by construction each integral depends on the unique set of variables. \IfBlankTF1.1

Example 1.

Consider the case N=3.N=3. The scalar equation (3) takes the form

|uututtuxutxuttxuxxutxxuttxx|=0.\left|\begin{array}[]{cccc}u&u_{t}&u_{tt}\\ u_{x}&u_{tx}&u_{ttx}\\ u_{xx}&u_{txx}&u_{ttxx}\end{array}\right|=0. (20)

The respective lattice (5) becomes a system for variables w1w_{1} and w2:w_{2}:

w0=1,tx2lnw1=w2w12,tx2lnw2=0,w3=0.w_{0}=1,\ \ \displaystyle\partial^{2}_{tx}\ln w_{1}=\frac{w_{2}}{w_{1}^{2}},\ \ \partial^{2}_{tx}\ln w_{2}=0,\ \ w_{3}=0. (21)

Formula (15) gives the following expressions for the tt-integrals

J3;1=|uxutxuxxutxx||uutuxutx|,J3;2=|uutuxxutxx||uutuxutx|.J_{3;1}=\frac{\left|\begin{array}[]{ll}u_{x}&u_{tx}\\ u_{xx}&u_{txx}\end{array}\right|}{\left|\begin{array}[]{ll}u&u_{t}\\ u_{x}&u_{tx}\end{array}\right|},\ \ J_{3;2}=\frac{\left|\begin{array}[]{ll}u&u_{t}\\ u_{xx}&u_{txx}\end{array}\right|}{\left|\begin{array}[]{ll}u&u_{t}\\ u_{x}&u_{tx}\end{array}\right|}. (22)

In order to express J3;1J_{3;1} and J3;2J_{3;2} in terms of w1w_{1} and w2w_{2} one can substitute u=w1u=w_{1} and eliminate mixed derivatives using (21). However, a simpler way to calculate them is to use formula (17) which gives

J2;1=J1;0xJ1;1+J1;1xlnw1w0=xlnw1,\begin{array}[]{ll}J_{2;1}&\displaystyle=J_{1;0}-\partial_{x}J_{1;1}+J_{1;1}\partial_{x}\ln\frac{w_{1}}{w_{0}}\\ &=\partial_{x}\ln w_{1},\end{array} (23)

Then the integrals are calculated as follows

J3;1=J2;0xJ2;1+J2;1xlnw2w1=x2lnw1+(lnw1)xxlnw2w1=w1,xxw1+w1,xw2,xw1w2,J3;2=J2;1xJ2;2+J2;2xlnw2w1=xlnw1+xlnw2w1=xlnw2.\begin{array}[]{ll}J_{3;1}&\displaystyle=J_{2;0}-\partial_{x}J_{2;1}+J_{2;1}\partial_{x}\ln\frac{w_{2}}{w_{1}}\\[11.38109pt] &\displaystyle=-\partial_{x}^{2}\ln w_{1}+\left(\ln w_{1}\right)_{x}\partial_{x}\ln\frac{w_{2}}{w_{1}}\\[11.38109pt] &\displaystyle=-\frac{w_{1,xx}}{w_{1}}+\frac{w_{1,x}w_{2,x}}{w_{1}w_{2}},\\[11.38109pt] J_{3;2}&\displaystyle=J_{2;1}-\partial_{x}J_{2;2}+J_{2;2}\partial_{x}\ln\frac{w_{2}}{w_{1}}\\[5.69054pt] &\displaystyle=\partial_{x}\ln w_{1}+\partial_{x}\ln\frac{w_{2}}{w_{1}}\\[5.69054pt] &\displaystyle=\partial_{x}\ln w_{2}.\end{array} (24)

New variables.

Let us introduce a new variable vnv_{n} as the ratio of the determinants

vn=wn1(utx)wn,n1,v_{n}=\frac{w_{n-1}\left(u_{tx}\right)}{w_{n}},\ \ n\geq 1, (25)

or the same vn=ulnwn.v_{n}=\partial_{u}\ln w_{n}. It follows from this definition that

v1=1uv_{1}=\frac{1}{u} (26)

since w1=u.w_{1}=u.

Lemma.

Quantity vnv_{n} satisfies the following equation

tvn=wn1(ux)wn(ut)wn2\partial_{t}v_{n}=-\frac{w_{n-1}\left(u_{x}\right)w_{n}\left(u_{t}\right)}{w_{n}^{2}} (27)
Proof.

Identity (14) with (p,q,r,s)=(1,n+1,1,n+1)(p,q,r,s)=(1,n+1,1,n+1) can be cast into the form

wn1(utx)wn+1=wn(utx)wnwn(ux)wn(ut).w_{n-1}(u_{tx})w_{n+1}=w_{n}(u_{tx})w_{n}-w_{n}(u_{x})w_{n}(u_{t}). (28)

Dividing it by wnwn+1w_{n}w_{n+1} and employing (25) we obtain

vn+1=vn+wn(ux)wnwn(ut)wn+1.v_{n+1}=v_{n}+\frac{w_{n}\left(u_{x}\right)}{w_{n}}\frac{w_{n}\left(u_{t}\right)}{w_{n+1}}. (29)

Setting p=1p=1 in (16)(\ref{recJ}) we can rewrite it as follows

twn1(ux)wn1=wn2(ux)wnwn12.\partial_{t}\frac{w_{n-1}\left(u_{x}\right)}{w_{n-1}}=\frac{w_{n-2}\left(u_{x}\right)w_{n}}{w_{n-1}^{2}}. (30)

Additionally, setting p=1p=1 in (19)(\ref{recI2}) and noting that In1,0=0I_{n-1,0}=0 we get the following equation

twn1(ut)wn=wn1wn(ut)wn2.\partial_{t}\frac{w_{n-1}\left(u_{t}\right)}{w_{n}}=-\frac{w_{n-1}w_{n}\left(u_{t}\right)}{w_{n}^{2}}. (31)

Further, we employ induction on nn. For n=1n=1 equation (27) takes the form t(1/u)=ut/u2\partial_{t}(1/u)=-u_{t}/u^{2} hence satisfied. Differentiating (29) and employing (27), (30) and (31), we get

tvn+1=wn(ux)wn+1(ut)wn+12\partial_{t}v_{n+1}=-\frac{w_{n}\left(u_{x}\right)w_{n+1}\left(u_{t}\right)}{w_{n+1}^{2}}

which is nothing but the upshifted formula (27). ∎

Corollary.

  1. i.

    Due to symmetry txt\leftrightarrow x in the definition of v,v, formula (27) implies the following equation

    xvn=wn1(ut)wn(ux)wn2.\partial_{x}v_{n}=-\frac{w_{n-1}\left(u_{t}\right)w_{n}\left(u_{x}\right)}{w_{n}^{2}}. (32)
  2. ii.

    Additionally, let us state the xx-counterparts of formulae (30) and (31), which will be useful later:

    xwn1(ut)wn1=wn2(ut)wnwn12,xwn1(ux)wn=wn1wn(ux)wn2.\partial_{x}\frac{w_{n-1}\left(u_{t}\right)}{w_{n-1}}=\frac{w_{n-2}\left(u_{t}\right)w_{n}}{w_{n-1}^{2}},\ \ \partial_{x}\frac{w_{n-1}\left(u_{x}\right)}{w_{n}}=-\frac{w_{n-1}w_{n}\left(u_{x}\right)}{w_{n}^{2}}. (33)
  3. iii.

    Multiplying (27) and (32) and then using (29) we can eliminate wn1(ut)wn1(ux)w_{n-1}(u_{t})w_{n-1}(u_{x}) and wn(ut)wn(ux)w_{n}(u_{t})w_{n}(u_{x}) to obtain the formula relating lattice variables vnv_{n} and wnw_{n} [2]

    wn1wn+1wn2=vn,tvn,x(vnvn1)(vn+1vn).\frac{w_{n-1}w_{n+1}}{w_{n}^{2}}=\frac{v_{n,t}v_{n,x}}{\left(v_{n}-v_{n-1}\right)\left(v_{n+1}-v_{n}\right)}. (34)

The following theorem was stated without a proof in [5].

Theorem.

Quantity vnv_{n} satisfies the lattice equation (1) with the left-boundary condition v0=0.v_{0}=0.

Proof.

The case n=1n=1 can be verified directly if we consider (26) and the fact that

v2=utxuutxutux.v_{2}=\frac{u_{tx}}{uu_{tx}-u_{t}u_{x}}.

Further, for n>1,n>1, on differentiating (27) with respect to xx and using (33), we obtain

tx2vn=wn+1wn1wn2(wn(ut)wn(ux)wnwn+1wn1(ut)wn1(ux)wn1wn).\partial^{2}_{tx}v_{n}=\frac{w_{n+1}w_{n-1}}{w_{n}^{2}}\left(\frac{w_{n}(u_{t})w_{n}(u_{x})}{w_{n}w_{n+1}}-\frac{w_{n-1}\left(u_{t}\right)w_{n-1}\left(u_{x}\right)}{w_{n-1}w_{n}}\right). (35)

Then, using formulae (29) and (34) we can eliminate variables wnw_{n} to obtain (1). ∎

3 Formulae for integrals and general solutions of the FSY lattice

Here we discuss the aspects of Darboux integrability of the obtained systems, e.g., the existence of characteristic integrals and solutions depending on arbitrary functions. Given that both systems (1) and (5) have their origin in the scalar equation (3) they inherit its Darboux integrability and the integrals. Hence the integrals (15) will be recalculated in the lattice variables vnv_{n} given by formula (25).

3.1 Recurrent formula for characteristic integrals

Boundary condition (0,)(0,\infty).

Firstly, consider the boundary condition (2). It is convenient to calculate the tt-integrals using the recurrent formula (17). To recalculate them in the lattice variables vnv_{n}, we re-write (34) and make self-substitution:

wn+1wn=wnwn1vn,tvn,x(vn+1vn)(vnvn1)=wn1wn2vn,tvn,xvn1,tvn1,x(vn+1vn)(vnvn1)2(vn1vn2)=m=1nvm,tvm,xv12(vn+1vn)m=1n1(vm+1vm)2,n1.\begin{array}[]{ll}\displaystyle\frac{w_{n+1}}{w_{n}}&\displaystyle=\frac{w_{n}}{w_{n-1}}\cdot\frac{v_{n,t}v_{n,x}}{\left(v_{n+1}-v_{n}\right)\left(v_{n}-v_{n-1}\right)}\\[11.38109pt] &\displaystyle=\frac{w_{n-1}}{w_{n-2}}\cdot\frac{v_{n,t}v_{n,x}v_{n-1,t}v_{n-1,x}}{\left(v_{n+1}-v_{n}\right)\left(v_{n}-v_{n-1}\right)^{2}\left(v_{n-1}-v_{n-2}\right)}\\[11.38109pt] &\dots\\ &\displaystyle=\frac{\displaystyle\prod_{m=1}^{n}v_{m,t}v_{m,x}}{v_{1}^{2}\left(v_{n+1}-v_{n}\right)\displaystyle\prod_{m=1}^{n-1}\left(v_{m+1}-v_{m}\right)^{2}},\ \ n\geq 1.\end{array} (36)

Then, on differentiating and eliminating vm,txv_{m,tx} by means of (1), we obtain

Λn=xlnwn+1wn=v1,xv1+m=1n(vm,xxvm,xvm+1,xvm+1vm)+m=1n1vm,xvm+1vm.\begin{array}[]{ll}\Lambda_{n}&\displaystyle=\partial_{x}\ln\frac{w_{n+1}}{w_{n}}\\ &\displaystyle=-\frac{v_{1,x}}{v_{1}}+\sum_{m=1}^{n}\left(\frac{v_{m,xx}}{v_{m,x}}-\frac{v_{m+1,x}}{v_{m+1}-v_{m}}\right)+\sum_{m=1}^{n-1}\frac{v_{m,x}}{v_{m+1}-v_{m}}.\end{array} (37)

Thus, formula (17) takes the following form

Jn;p=Jn1;p1xJn1;p+Λn2Jn1;p,J_{n;p}=J_{n-1;p-1}-\partial_{x}J_{n-1;p}+\Lambda_{n-2}J_{n-1;p}, (38)

where Λn\Lambda_{n} is given by formula (37).

\IfBlankTF

1.2

Example 2.

Consider equation (20) in variables (25) which implies the condition

v0=0,v3=.v_{0}=0,\,v_{3}=\infty. (39)

Condition (39) turns lattice (1) into the following two-component system

v1,tx=v1,tv1,x(1v11v2v1),v2,tx=v2,tv2,xv2v1.\begin{array}[]{ll}v_{1,tx}&\displaystyle=v_{1,t}v_{1,x}\left(\frac{1}{v_{1}}-\frac{1}{v_{2}-v_{1}}\right),\\[5.69054pt] v_{2,tx}&\displaystyle=\frac{v_{2,t}v_{2,x}}{v_{2}-v_{1}}.\end{array} (40)

The most straightforward way to calculate the integrals of (40) is to use formula (22), in which we must substitute u=1/v1u=1/v_{1} and eliminate the mixed derivatives by means of (40). However, the integrals can be calculated more efficiently by means of formula (38). Recall that Jn,0=0J_{n,0}=0 and Jn,n=1J_{n,n}=1 for any nn. Then, from formulae (37) and (38) we first obtain the auxiliary expression

J2,1=Λ0=v1,xv1.J_{2,1}=\Lambda_{0}=-\frac{v_{1,x}}{v_{1}}. (41)

Further, we have

Λ1=v1,xxv1,xv1,xv1v2,xv2v1\Lambda_{1}=\frac{v_{1,xx}}{v_{1,x}}-\frac{v_{1,x}}{v_{1}}-\frac{v_{2,x}}{v_{2}-v_{1}} (42)

hence the first integral is given by

J3,1=xJ2,1+Λ1J2,1=v1,xxv1v1,x2v12v1,xv1(v1,xxv1,xv1,xv1v2,xv2v1)=v1,xv2,xv1(v2v1).\begin{array}[]{ll}J_{3,1}&=-\partial_{x}J_{2,1}+\Lambda_{1}J_{2,1}\\ &\displaystyle=\frac{v_{1,xx}}{v_{1}}-\frac{v_{1,x}^{2}}{v_{1}^{2}}-\frac{v_{1,x}}{v_{1}}\left(\frac{v_{1,xx}}{v_{1,x}}-\frac{v_{1,x}}{v_{1}}-\frac{v_{2,x}}{v_{2}-v_{1}}\right)\\[11.38109pt] &\displaystyle=\frac{v_{1,x}v_{2,x}}{v_{1}\left(v_{2}-v_{1}\right)}.\end{array} (43)

Lastly, the integral J3,2J_{3,2} reads

J3,2=J2,1+Λ1J2,2=v1,xxv1,x2v1,xv1v2,xv2v1.\begin{array}[]{ll}J_{3,2}&=J_{2,1}+\Lambda_{1}J_{2,2}\\[5.69054pt] &\displaystyle=\frac{v_{1,xx}}{v_{1,x}}-\frac{2v_{1,x}}{v_{1}}-\frac{v_{2,x}}{v_{2}-v_{1}}.\end{array} (44)

Thus, the integrals J3,1J_{3,1} and J3,2J_{3,2} constitute a complete set of integrals for the system (40).

Boundary condition (a,b).(a,b).

Let us quickly discuss how integrals can be re-calculated in the case of the boundary condition (7). Obviously, one can simply make the inverse transformation

vn=φnaφnb,v_{n}=\frac{\varphi_{n}-a}{\varphi_{n}-b}, (45)

where the non-essential constant factor aba-b was suppressed.

However, instead of recalculating the integrals we would rather recalculate formula (37) in variables φn\varphi_{n}. Calculations, similar to (36) and (37), yield the formula

Λn=φ1,xφ1aφn,xφnb+φn+1,xφn+1b+m=1n(φm,xxφm,xφm+1,xφm+1φm)+m=1n1φm,xφm+1φm.\begin{array}[]{ll}\Lambda_{n}&\displaystyle=-\frac{\varphi_{1,x}}{\varphi_{1}-a}-\frac{\varphi_{n,x}}{\varphi_{n}-b}+\frac{\varphi_{n+1,x}}{\varphi_{n+1}-b}\\[5.69054pt] &\displaystyle+\sum_{m=1}^{n}\left(\frac{\varphi_{m,xx}}{\varphi_{m,x}}-\frac{\varphi_{m+1,x}}{\varphi_{m+1}-\varphi_{m}}\right)+\sum_{m=1}^{n-1}\frac{\varphi_{m,x}}{\varphi_{m+1}-\varphi_{m}}.\end{array} (46)
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1.3

Example 3.

Consider the system obtained from (40) by applying (45)

φ1,tx=φ1,tφ1,x(1φ1a1φ2φ1),φ2,tx=φ2,tφ2,x(1φ2φ11bφ2).\begin{array}[]{l}\displaystyle\varphi_{1,tx}=\varphi_{1,t}\varphi_{1,x}\left(\frac{1}{\varphi_{1}-a}-\frac{1}{\varphi_{2}-\varphi_{1}}\right),\\[8.53581pt] \displaystyle\varphi_{2,tx}=\varphi_{2,t}\varphi_{2,x}\left(\frac{1}{\varphi_{2}-\varphi_{1}}-\frac{1}{b-\varphi_{2}}\right).\end{array} (47)

Hence, we assume that

φ0=a,φ3=b.\varphi_{0}=a,\ \ \varphi_{3}=b. (48)

Then, formula (46) yields

J2,1=Λ0=φ1,xφ1bφ1,xφ1a.J_{2,1}=\Lambda_{0}=\frac{\varphi_{1,x}}{\varphi_{1}-b}-\frac{\varphi_{1,x}}{\varphi_{1}-a}.

Further, from the same formula we obtain

Λ1=φ2,xφ2bφ1,xφ1bφ1,xφ1a+φ1,xxφ1,xφ2,xφ2φ1.\Lambda_{1}=\frac{\varphi_{2,x}}{\varphi_{2}-b}-\frac{\varphi_{1,x}}{\varphi_{1}-b}-\frac{\varphi_{1,x}}{\varphi_{1}-a}+\frac{\varphi_{1,xx}}{\varphi_{1,x}}-\frac{\varphi_{2,x}}{\varphi_{2}-\varphi_{1}}. (49)

The integrals are given by

J3,1=xJ2,1+Λ1J2,1=(ab)φ1,xφ2,x(φ1a)(φ2φ1)(φ2b)\begin{array}[]{ll}J_{3,1}&\displaystyle=-\partial_{x}J_{2,1}+\Lambda_{1}J_{2,1}\\[5.69054pt] &\displaystyle=\frac{(a-b)\varphi_{1,x}\varphi_{2,x}}{(\varphi_{1}-a)(\varphi_{2}-\varphi_{1})(\varphi_{2}-b)}\end{array} (50)

and

J3,2=J2,1+Λ1J2,2=2φ1,xφ1a+φ2,xφ2bφ2,xφ2φ1+φ1,xxφ1,x.\begin{array}[]{ll}J_{3,2}&\displaystyle=J_{2,1}+\Lambda_{1}J_{2,2}\\[5.69054pt] &\displaystyle=-\frac{2\varphi_{1,x}}{\varphi_{1}-a}+\frac{\varphi_{2,x}}{\varphi_{2}-b}-\frac{\varphi_{2,x}}{\varphi_{2}-\varphi_{1}}+\frac{\varphi_{1,xx}}{\varphi_{1,x}}.\end{array} (51)
Remark.

System (40), given in the variables

v1=a/p,v2=qv_{1}=-a/p,\ \ v_{2}=q

was shown to be Darboux integrable in [14], in which its integrals and higher symmetries were described. Later, the point-equivalent system (47) was used as an illustrating example in several papers (see e.g. [11, 4]).

3.2 General solutions

The general solution of (3) has a particularly simple form [6], namely

u(t,x)=s=1N1Xs(x)Ts(t),u(t,x)=\sum_{s=1}^{N-1}X_{s}(x)T_{s}(t), (52)

where Ts(t)T_{s}(t) and Xs(x)X_{s}(x) are arbitrary functions of their arguments. Thus, the number of arbitrary functions in it, 2N22N-2, matches the order of equation (3).

Substituting (52) into (25) we obtain the general solution of the lattice (1) with the boundary condition (2):

vn=det(aij)det(bkl),v_{n}=\frac{\mbox{det}\left(a_{ij}\right)}{\mbox{det}\left(b_{kl}\right)}, (53)

where the components of the determinants are given by

aij=s=1N1Xs(i)Ts(j),bkl=s=1N1Xs(k1)Ts(l1),i,j=1,,n1,k,l=1,,n.\begin{array}[]{ll}a_{ij}&\displaystyle=\sum_{s=1}^{N-1}X_{s}^{(i)}T_{s}^{(j)},\ \ b_{kl}=\sum_{s=1}^{N-1}X_{s}^{(k-1)}T_{s}^{(l-1)},\\ &i,j=1,\dots,n-1,\ \ k,l=1,\dots,n.\end{array} (54)

and the derivatives are denoted as follows:

Xs(κ)=dκXdxκ,Ts(μ)=dμTdtμ.X^{(\kappa)}_{s}=\frac{d^{\kappa}X}{dx^{\kappa}},\ \ T^{(\mu)}_{s}=\frac{d^{\mu}T}{dt^{\mu}}. (55)

Hence, formula (53) provides us with the general solution of (1) satisfying condition (2). In order to obtain the general solution satisfying the boundary condition (7) one has to apply transformation (9).

Let us consider the degenerate boundary condition

v0=vN=av_{0}=v_{N}=a (56)

in more detail. Although calculation of integrals in this case is straightforward, the general solution requires a more detailed analysis.

Firstly, we consider the homogeneous condition

v0=vN=0.v_{0}=v_{N}=0. (57)

Comparing it with (25) we see that

wN1(utx)=0.w_{N-1}(u_{tx})=0.

The general solution of the latter equation is given by

u=X0(x)+T0(t)+s=1N2XsTs.u=X_{0}(x)+T_{0}(t)+\sum_{s=1}^{N-2}X_{s}T_{s}. (58)

Substituting (58) in (25) and shifting the result, we get the general solution of (1) satisfying condition (56) in the form

vn=det(αij)det(βkl)+a,v_{n}=\frac{\mbox{det}\left(\alpha_{ij}\right)}{\mbox{det}\left(\beta_{kl}\right)}+a, (59)

where

αij=s=1N2Xs(i)Ts(j),βkl=δk1T0(l1)+δ1lX0(k1)+s=1N2Xs(k1)Ts(l1),i,j=1,,n1,k,l=1,,n.\begin{array}[]{ll}\alpha_{ij}&\displaystyle=\sum_{s=1}^{N-2}X_{s}^{(i)}T_{s}^{(j)},\\ \beta_{kl}&\displaystyle=\delta_{k1}T_{0}^{(l-1)}+\delta_{1l}X_{0}^{(k-1)}+\sum_{s=1}^{N-2}X_{s}^{(k-1)}T_{s}^{(l-1)},\\ &i,j=1,\dots,n-1,\ \ k,l=1,\dots,n.\end{array} (60)

Here, δkl\delta_{kl} is the Kronecker delta:

δkl={1,k=l0,kl\delta_{kl}=\left\{\begin{array}[]{ll}1,&k=l\\ 0,&k\neq l\end{array}\right.
\IfBlankTF

1.4

Example 4.

For system (40), formula (53) gives a general solution in the following form

v1=1T1X1+T2X2,v2=T1X1+T2X2T1X1T2X2T1X2T2X1T2X1T1X2+T2X2T1X1.\begin{array}[]{ll}v_{1}&\displaystyle=\frac{1}{T_{1}X_{1}+T_{2}X_{2}},\\ v_{2}&\displaystyle=\frac{T_{1}^{\prime}X_{1}^{\prime}+T_{2}^{\prime}X_{2}^{\prime}}{T_{1}X_{1}T_{2}^{\prime}X_{2}^{\prime}-T_{1}X_{2}T_{2}^{\prime}X_{1}^{\prime}-T_{2}X_{1}T_{1}^{\prime}X_{2}^{\prime}+T_{2}X_{2}T_{1}^{\prime}X_{1}^{\prime}}.\end{array} (61)

Applying (9), we get a general solution of (47) in the form

φ1=a+ab(ab)(X1T1+X2T2)1,φ2=a+(ab)(T1X1+T2X2)(ab)(X2X1X1X2)(T2T1T1T2)T1X1T2X2.\begin{array}[]{ll}\varphi_{1}&\displaystyle=a+\frac{a-b}{(a-b)(X_{1}T_{1}+X_{2}T_{2})-1},\\[8.53581pt] \varphi_{2}&\displaystyle=a+\frac{(a-b)\big{(}T_{1}^{\prime}X_{1}^{\prime}+T_{2}^{\prime}X_{2}^{\prime}\big{)}}{(a-b)\big{(}X_{2}X_{1}^{\prime}-X_{1}X_{2}^{\prime}\big{)}\big{(}T_{2}T_{1}^{\prime}-T_{1}T_{2}^{\prime}\big{)}-T_{1}^{\prime}X_{1}^{\prime}-T_{2}^{\prime}X_{2}^{\prime}}.\end{array} (62)

Finally, the solution to the system (47) in the degenerate case b=ab=a is obtained from the formula (59)

φ1=a+1T1X1+T0+X0,φ2=a+T1X1T0T1X1T1T0X1+X0T1X1X1T1X0T0X0.\begin{array}[]{ll}\varphi_{1}&\displaystyle=a+\frac{1}{T_{1}X_{1}+T_{0}+X_{0}},\\ \varphi_{2}&\displaystyle=a+\frac{T_{1}^{\prime}X_{1}^{\prime}}{T_{0}T_{1}^{\prime}X_{1}^{\prime}-T_{1}T_{0}^{\prime}X_{1}^{\prime}+X_{0}T_{1}^{\prime}X_{1}^{\prime}-X_{1}T_{1}^{\prime}X_{0}^{\prime}-T_{0}^{\prime}X_{0}^{\prime}}.\end{array} (63)

4 Conclusion

An evident extension of the results presented in this paper concerns the discrete and semi-discrete versions of the FSY lattice (1). To derive these, one can start with the discrete scalar equation (3), where derivatives are replaced by shifts of discrete variables, and introduce new lattice variables in a similar manner, specifically using formula (25). The subsequent calculations rely on the Jacobi identity (14) and largely mirror those presented in this paper.

The resulting equations should exhibit analogous properties. In particular, when the boundary condition (2) is imposed, they become Darboux integrable. Detailed aspects of integrability, such as characteristic integrals and general solutions, will be addressed in a separate publication.

Another direction, concerning finite reductions of the FSY lattice, involves finding exact solutions to integrable models with two spatial dimensions [15, 4]. We anticipate that the formulae for the integrals and general solutions provided in this paper will facilitate progress in addressing these problems.

References

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