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28 March 2026

29 Pages

N-Triple-Pole Solitons in Matrix NLS Systems: Inverse Scattering Transform Under Nonzero Boundary Conditions

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School of Information Engineering, Zhejiang Ocean University, Zhoushan 316022, China
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Author to whom correspondence should be addressed.
This article belongs to the Section B: Mathematics

Abstract

This work presents the first systematic development of the inverse scattering transform for matrix nonlinear Schrödinger equations in the case where the discrete spectrum has triple poles, under nonzero boundary conditions at infinity. These systems arise physically as reductions modeling spinor Bose-Einstein condensates with hyperfine spin F = 1 and find applications in nonlinear optics. A uniformization variable is employed to map the underlying Riemann surface to the complex plane, enabling a complete characterization of the analyticity, symmetries, and asymptotic behaviors of the Jost functions and scattering data. Extending the established framework for simple and double poles, we show that rank   P ( x , t , z n ) = 3 requires a third-order zero of det   a ( z ) at z = z n , while rank   P ( x , t , z n ) = 2 necessitates a fourth-order zero—a nontrivial feature absent in lower-order cases. The discrete spectrum for both rank configurations is fully characterized, and the full singular behavior near a triple pole is derived, respecting the quartet symmetry z n , z n * , v k 0 2 / z n , v k 0 2 / z n * imposed by the nonzero boundary conditions. Solving the resulting matrix Riemann-Hilbert problem with triple poles yields the potential reconstruction formula and, in the reflectionless case, explicit expressions for general N-triple-pole soliton solutions, with a detailed example for N = 1 presented to illustrate the construction.

1. Introduction

Quantum mechanics, a cornerstone of modern physics, emerged from the inability of classical theory to describe microscopic systems. While quantum fluctuations are generally suppressed in the limit of a large number of particles, leading to classical behavior, genuine macroscopic quantum phenomena are rare. A prominent exception is the Bose–Einstein condensate (BEC). In recent decades, BEC systems have been widely explored from both theoretical and experimental perspectives [1,2,3,4,5,6,7,8].
In 1961, Gross and Pitaevskii independently formulated the mean-field theory for a dilute atomic gas BEC, resulting in the Gross–Pitaevskii (GP) equation
i ℏ ∂ ∂ t Ψ ( r , t ) = − ℏ 2 ∇ 2 2 m + V ext ( r ) + Q | Ψ |     2 Ψ ( r , t ) ,
where Ψ ( r , t ) is the condensate wave function, V ext ( r ) is the external trapping potential, Q = 4 π N ℏ a s / m is the coupling constant (with N the particle number, m the atomic mass, and a s the s-wave scattering length), and | Ψ |     2 denotes the atomic density.
Under homogeneous or trap-free conditions, the GP equation reduces to the standard nonlinear Schrödinger (NLS) equation. Subsequent advances in optical trapping techniques have liberated the internal spin degrees of freedom, spurring extensive research on multicomponent BEC [9,10,11]. In the mean-field description that neglects collisions and thermal clouds, two interacting condensates can be modeled by a pair of coupled GP equations:
i ℏ ∂ Ψ 1 ∂ t = − ℏ 2 2 m 1 ∂ 2 ∂ x 2 + V 1 + Q 11 Ψ 1 2 + Q 12 Ψ 2 2 Ψ 1 , i ℏ ∂ Ψ 2 ∂ t = − ℏ 2 2 m 2 ∂ 2 ∂ x 2 + V 2 + Q 21 Ψ 1 2 + Q 22 Ψ 2 2 Ψ 2 ,
where Q i j = 2 π ℏ 2 a i j / A μ i j , with a i j being the three-dimensional scattering length, μ i j = m i m j ( m i + m j ) the reduced mass, and A the cross-sectional area of the cigar-shaped BEC. Here, m i is the atomic mass in component i, V i the external trapping potential, and N i = ∫ − ∞ ∞ Ψ i 2 d x the number of atoms in component i.
In 1998, the group of W. Ketterle realized a Bose-Einstein condensate by confining 23Na atomic gas with a single focused infrared laser beam as an optical dipole trap—a pioneering experimental achievement. The spin-exchange interactions among atoms give rise to rich spin textures and hyperfine structures within the condensate, leading to the distinct phenomenon known as a spinor BEC. The dynamics of a spinor BEC with three hyperfine states confined in an optical dipole trap is governed by a three-component coupled GP equation [12,13]:
i ℏ ∂ ϕ 1 ∂ t = − ℏ 2 2 m ∂ 2 ϕ 1 ∂ x 2 + c ¯ 0 + c ¯ 2 ϕ 1 2 + ϕ 0 2 ϕ 1 + c ¯ 0 − c ¯ 2 ϕ − 1 2 ϕ 1 + c ¯ 2 ϕ − 1 * ϕ 0 2 , i ℏ ∂ ϕ 0 ∂ t = − ℏ 2 2 m ∂ 2 ϕ 0 ∂ x 2 + c ¯ 0 + c ¯ 2 ϕ 1 2 + ϕ − 1 2 ϕ 0 + c ¯ 0 ϕ 0 2 ϕ 0 + 2 c ¯ 2 ϕ 0 * ϕ 1 ϕ − 1 , i ℏ ∂ ϕ − 1 ∂ t = − ℏ 2 2 m ∂ 2 ϕ − 1 ∂ x 2 + c ¯ 0 + c ¯ 2 ϕ − 1 2 + ϕ 0 2 ϕ − 1 + c ¯ 0 − c ¯ 2 ϕ 1 2 ϕ − 1 + c ¯ 2 ϕ 1 * ϕ 0 2 ,
here c ¯ 0 and c ¯ 2 represent the mean-field and spin-exchange interaction strengths, respectively.
After nondimensionalization, this system reduces to a focusing-type matrix NLS equation. More generally, in the homogeneous case, an F = 1 spinor BEC is modeled by the matrix NLS equation
i Q t + Q x x − 2 v Q Q † Q = 0 2 × 2 , v = ± 1 ,
for appropriate interaction coefficients. Here, Q ( x , t ) is a 2 × 2 complex matrix-valued function, Q † denotes its Hermitian conjugate, and 0 2 × 2 is the 2 × 2 zero matrix [14,15]. In this work we consider the generalized matrix NLS equation
i Q t + Q x x − 2 Q R Q = 0 2 × 2 , R = Σ Q † Ω ,
where Ω and Σ are 2 × 2 Hermitian matrices whose specific choices determine the type of nonlinearity (focusing, defocusing, or mixed sign), as shown below. In the following, we refer to Equation (5) as the matrix NLS equation.
Under the gauge transformation [16]
Q ( x , t ) → Q ( x , t ) e ∓ 2 i k 0 2 t ,
where k 0 > 0 , Equation (5) becomes the equivalent form
i Q t + Q x x − 2 ( Q R Q − v k 0 2 I 2 ) = 0 2 × 2 ,
where I 2 is the 2 × 2 identity matrix. Depending on the sign parameter v, Equation (5) admits four distinct types of reductions, often categorized as follows:
  • Case 1: (defocusing, Σ = Ω = diag ( 1 , 1 ) )
i q 1 t + q 1 x x − 2 q 1 q 1 2 + 2 q 0 2 − 2 q 0 2 q − 1 * = 0 , i q 0 t + q 0 x x − 2 q 0 ( q − 1 2 + q 0 2 + q 1 2 ) − 2 q − 1 q 0 * q 1 = 0 , i q − 1 t + q − 1 x x − 2 q − 1 ( q − 1 2 + 2 q 0 2 ) − 2 q 0 2 q 1 * = 0 .
  • Case 2: (focusing, Σ = − Ω = diag ( 1 , 1 ) )
i q 1 t + q 1 x x + 2 q 1 ( q 1 2 + 2 q 0 2 ) + 2 q 0 2 q − 1 * = 0 , i q 0 t + q 0 x x + 2 q 0 ( q − 1 2 + q 0 2 + q 1 2 ) + 2 q − 1 q 0 * q 1 = 0 , i q − 1 t + q − 1 x x + 2 q − 1 ( q − 1 2 + 2 q 0 2 ) + 2 q 0 2 q 1 * = 0 .
  • Case 3: (mixed sign(i), Σ = Ω = diag ( 1 , − 1 ) )
i q 1 t + q 1 x x − 2 q 1 q 1 2 − 2 q 0 2 − 2 q 0 2 q − 1 * = 0 , i q 0 t + q 0 x x − 2 q 0 ( q − 1 2 − q 0 2 + q 1 2 ) + 2 q − 1 q 0 * q 1 = 0 , i q − 1 t + q − 1 x x − 2 q − 1 ( q − 1 2 − 2 q 0 2 ) − 2 q 0 2 q 1 * = 0 .
  • Case 4: (mixed sign(ii), Σ = − Ω = diag ( 1 , − 1 ) )
i q 1 t + q 1 x x + 2 q 1 ( q 1 2 − 2 q 0 2 ) + 2 q 0 2 q − 1 * = 0 , i q 0 t + q 0 x x + 2 q 0 ( q − 1 2 − q 0 2 + q 1 2 ) − 2 q − 1 q 0 * q 1 = 0 , i q − 1 t + q − 1 x x + 2 q − 1 ( q − 1 2 − 2 q 0 2 ) + 2 q 0 2 q 1 * = 0 .
Here, v = 1 corresponds to Cases 1 and 3, while v = − 1 corresponds to Cases 2 and 4.
Cases 1 and 2 (the defocusing and focusing reductions) have been studied extensively [17,18,19]. Complete soliton solutions for the mixed-sign vector NLS equation have also been reported under zero and nonzero boundary conditions [20,21,22]. However, the matrix case is fundamentally different. In the context of BEC, the signs of the coupling constants reflect those of the s-wave scattering lengths governing intraspecies and interspecies atomic interactions. Consequently, the nonlinear integrable equations in Cases 3 and 4 do not correspond to a physically valid model for three-component F = 1 spinor BEC, unlike Cases 1 and 2. Instead, they find application in other physical settings, notably in nonlinear optics and in models of four-component fermionic condensates [23,24,25,26,27].

1.1. Motivation

The inverse scattering transform (IST) provides a powerful framework for solving integrable nonlinear evolution equations by linearizing them into a spectral problem. Recently, Ortiz and Prinari [28] systematically developed the IST and constructed simple-pole solutions for the matrix NLS Equation (5) under nonzero boundary conditions (NZBCs) at infinity. Subsequently, the IST for Equation (5) with both zero boundary conditions (ZBCs) and NZBCs, accounting for double zeros in the analytic scattering coefficients, was investigated in Ref. [29]. However, the case of triple poles—corresponding to higher-order spectral degeneracies and more intricate soliton dynamics—has remained largely unexplored. Constructing triple-pole solutions demands a more delicate analysis, including refined regularization and residue calculus within the associated Riemann-Hilbert (RH) problem. These solutions not only provide a stringent test of the completeness and robustness of the IST framework, but also reveal deeper algebraic structures inherent in the integrable hierarchy.
The extension from double to triple poles in the matrix setting introduces essential new features absent in scalar or vector counterparts. Most notably, there exists a forced correspondence between the order of zeros of det   a ( z ) and the rank of the matrix P ( x , t , z n ) —a feature already present at the double-pole level, but whose explicit realization at third order requires a systematic characterization. Specifically, as we show in this work:
  • rank   P ( x , t , z n ) = 3 requires a third-order zero of det   a ( z ) at z = z n ;
  • rank   P ( x , t , z n ) = 2 requires a fourth-order zero of det   a ( z ) at z = z n .
These rank configurations give rise to distinct residue conditions and norming constant structures, which must be carefully derived and incorporated into the RH problem.
Furthermore, the physical relevance of NZBCs cannot be overstated. They describe systems with nontrivial backgrounds, such as multicomponent BEC in external potentials or light propagation in inhomogeneous media—settings where zero boundary conditions are no longer applicable. Thus, extending the IST to matrix NLS equations with triple poles under NZBCs is both mathematically necessary and physically meaningful.
The IST is ideally suited for triple-pole solitons in the matrix NLS equation under NZBCs. First, IST systematically characterizes the discrete spectrum through analytic scattering coefficients: the order of zeros of det   a ( z ) directly dictates the pole structure, enabling rigorous treatment of higher-order poles via Laurent expansions. Second, the matrix nature is encoded in the scattering data—the rank of P ( x , t , z n ) emerges from linear dependence among Jost functions at the eigenvalue, revealing a correspondence between spectral degeneracy and eigenfunction structure inaccessible to purely algebraic methods. Third, NZBCs introduce a Riemann surface and continuous spectrum, seamlessly handled via a uniformization variable and the associated RH problem. This approach yields explicit soliton solutions in the reflectionless case, as well as spectral properties, trace formulae, and long-time asymptotics—offering a comprehensive understanding beyond mere solution construction.

1.2. Structure of This Paper

This paper is organized as follows. Section 2 reviews the direct scattering problem for Equation (6) under NZBCs, with emphasis on the characterization of the discrete spectrum for triple poles. We derive the associated residue conditions and norming constants for the two distinct cases: rank   P ( x , t , z n ) = 2 and rank   P ( x , t , z n ) = 3 . Section 3 formulates the inverse problem as a matrix RH problem. Solving this RH problem in the reflectionless case yields the potential reconstruction formula and explicit expressions for general N-triple-pole soliton solutions. A detailed example for N = 1 is presented in the Appendix A. Concluding remarks and directions for future research are given in Section 4.

2. Direct Scattering Problem

The direct scattering problem under NZBCs for systems with poles of different orders shares a common framework, differing principally in the characterization of the discrete spectrum. The direct scattering theory for the matrix NLS equation with NZBCs is well established for simple and double poles [28,29]; we therefore only briefly recall the essential elements before turning to the novel features associated with triple poles.

2.1. Lax Pair, Riemann Surface, and Uniformization Coordinate

Equation (6) admits the following Lax pair formulation:
φ x = U φ , φ t = V φ ,
where
U = − i k σ 4 + Q ˜ , V = − 2 i k 2 σ 4 + 2 k Q ˜ + i σ 4 ( Q ˜ x − Q ˜ 2 + v k 0 2 I 4 ) ,
and
Q ˜ = 0 2 × 2 Q R 0 2 × 2 , Q = q 1 ( x , t ) q 0 ( x , t ) q 0 ( x , t ) q − 1 ( x , t ) , σ 4 = I 2 0 2 × 2 0 2 × 2 − I 2 ,
with R = Σ Q † Ω as in (5), and I 4 denotes the 4 × 4 identity matrix. We consider Equation (6) under constant NZBCs:
Q ( x , t ) → Q ± , x → ± ∞ .
The anticommutation relation Q ˜ σ 4 = − σ 4 Q ˜ can be directly verified. Taking the limit x → ± ∞ and imposing the boundary condition (14) yields the asymptotic spectral problem
φ x = U ± φ , U ± = − i k σ 4 + Q ˜ .
From the boundary condition (14), it follows that
Q ˜ ± 2 = v k 0 2 I 4 , Q ˜ ± = 0 2 × 2 Q ± R ± 0 2 × 2 ,
and consequently,
Q ± R ± = R ± Q ± = v k 0 2 I 2 .
The eigenvalues of U ± and V ± are ± i λ and ± 2 i k λ , respectively. To uniformize the two-sheeted Riemann surface, we introduce the variable
z = k + λ ,
where λ is defined by λ 2 = k 2 − v k 0 2 . The branch points of the Riemann surface are therefore at k = ± v k 0 2 .
For Cases 1 and 3 ( v = 1 ), we parametrize
k − k 0 = r 1 e i θ 1 , k + k 0 = r 2 e i θ 2 ,
which leads to the definition of λ ( k ) on the two sheets:
λ ( k ) = r 1 r 2 e i ( θ 1 + θ 2 ) / 2 , C I , − r 1 r 2 e i ( θ 1 + θ 2 ) / 2 , C I I ,
where 0 < θ 1 < π and − π < θ 2 < π . C I and C I I denoten the first and second sheets of the Riemann surface, respectively. Thus, one has
k = 1 2 z + k 0 2 z , λ = 1 2 z − k 0 2 z .
Under Equation (21), the first sheet C I is mapped conformally onto the upper half-plane D + = { z ∈ C : Im z > 0 } , while the second sheet C I I is mapped onto the lower half-plane D − = { z ∈ C : Im z < 0 } . A neighbourhood of k = ∞ on either sheet corresponds to a neighbourhood of either z = 0 or z = ∞ , depending on the sign of Im λ .
For Cases 2 and 4 ( v = − 1 ), we employ the parametrization
k − i k 0 = r 1 e i θ 1 , k + i k 0 = r 2 e i θ 2 ,
with − π 2 < θ 1 , θ 2 < 3 π 2 . The function λ ( k ) is then given by
λ ( k ) = r 1 r 2 e i ( θ 1 + θ 2 ) / 2 , C I , − r 1 r 2 e i ( θ 1 + θ 2 ) / 2 , C I I ,
and the relations inverse to Equation (18) become
k = 1 2 z − k 0 2 z , λ = 1 2 z + k 0 2 z .
In this case, the branch cut on the Riemann surface is mapped onto the circle C 0 = { z ∈ C : | z | = k 0 } . The first sheet C I corresponds to the exterior of C 0 ( | z | > k 0 ), while the second sheet C I I corresponds to its interior ( | z | < k 0 ). The points at infinity map as z ( ∞ I ) = ∞ and z ( ∞ I I ) = 0 . The regions D + and D − are now defined by the sign of ( | z | 2 − k 0 2 ) Im z :
D + = { z ∈ C : ( | z | 2 − k 0 2 ) Im z > 0 } , D − = { z ∈ C : ( | z | 2 − k 0 2 ) Im z < 0 } .
These correspond to Im λ > 0 and Im λ < 0 , respectively.

2.2. Jost Functions and Analyticty

The asymptotic eigenvector matrices are given by
X ± = I 4 − i z σ 4 Q ˜ ± ,
which, by construction, satisfy
U ± X ± = − i λ X ± σ 4 .
From this definition, one finds det   X ± ( z ) = ( 2 λ λ + k ) 2 = ( γ ( z ) ) 2 , where γ ( z ) = 1 − v k 0 2 z 2 . The inverse is given by
X ± − 1 ( z ) = 1 γ ( z ) ( I 4 + i z σ 4 Q ˜ ± ) .
We note that γ ( z ) (and hence X ± ( z ) ) is singular at the branch points: z = ± k 0 for v = 1 , and z = ± i k 0 for v = − 1 ; these points are excluded from the analysis.
The Jost solutions are defined as the following matrix-valued functions satisfying the asymptotic conditions:
Φ ( x , t , z ) = ( ϕ ( x , t , z ) , ϕ ¯ ( x , t , z ) ) , Ψ ( x , t , z ) = ( ψ ¯ ( x , t , z ) , ψ ( x , t , z ) ) .
Here, ϕ , ϕ ¯ and ψ , ψ ¯ are each 4 × 2 matrix functions. Their defining asymptotic behaviors (as x → ± ∞ ) are:
ϕ ( x , t , z ) ∼ I 2 i z R − e − i θ ( x , t , z ) , ϕ ¯ ( x , t , z ) ∼ − i z Q − I 2 e i θ ( x , t , z ) , x → − ∞ ,
ψ ( x , t , z ) ∼ I 2 i z R + e − i θ ( x , t , z ) , ψ ¯ ( x , t , z ) ∼ − i z Q + I 2 e i θ ( x , t , z ) , x → + ∞ ,
where θ ( x , t , z ) = λ ( x + 2 k t ) . Consequently, the full matrix solutions Φ and Ψ satisfy the asymptotic conditions
Φ ( x , t , z ) = X − ( z ) e − i θ ( x , t , z ) σ 4 + o ( 1 ) , x → − ∞ ,
Ψ ( x , t , z ) = X + ( z ) e − i θ ( x , t , z ) σ 4 + o ( 1 ) , x → + ∞ .
It is standard to introduce the modified Jost functions, which remove the essential asymptotic oscillations:
( M ( x , t , z ) , M ¯ ( x , t , z ) ) = Φ ( x , t , z ) e i θ ( x , t , z ) σ 4 , ( N ¯ ( x , t , z ) , N ( x , t , z ) ) = Ψ ( x , t , z ) e i θ ( x , t , z ) σ 4 .
From Equations (27)–(29) and (32), their asymptotic behaviors follow directly:
( M ( x , t , z ) , M ¯ ( x , t , z ) ) ∼ X − , x → − ∞ , ( N ¯ ( x , t , z ) , N ( x , t , z ) ) ∼ X + , x → + ∞ .
For v = 1 , the continuous spectrum in the original k-plane is Σ k = R ∖ [ − k 0 , k 0 ] , which corresponds to Σ z = R in the uniformized z-plane. For v = − 1 , we have Σ k = R ∪ i [ − k 0 , k 0 ] and Σ z = R ∪ C 0 .
The Jost functions satisfy the following Volterra integral equations, derived from the equivalent Lax pair:
( M ( x , t , z ) , M ¯ ( x , t , z ) ) = X − + ∫ − ∞ x X − e i λ ( y − x ) σ ^ 4 [ X − − 1 Δ Q ˜ ( y , t ) ( M ( y , t , z ) , M ¯ ( y , t , z ) ) ] d y , ( N ¯ ( x , t , z ) , N ( x , t , z ) ) = X + + ∫ ∞ x X + e i λ ( y − x ) σ ^ 4 [ X + − 1 Δ Q ˜ ( y , t ) ( N ¯ ( y , t , z ) , N ( y , t , z ) ) ] d y ,
where Δ Q ± = Q − Q ± for x → ± ∞ , and σ ^ 4 denotes the operator that acts on a 4 × 4 matrix A as σ ^ 4 A = [ σ 4 , A ] = σ 4 A − A σ 4 . These integral equations imply the analyticity properties:
M ( x , t , z ) , N ( x , t , z ) ∈ H ( D + ) , M ¯ ( x , t , z ) , N ¯ ( x , t , z ) ∈ H ( D − ) .
Here, H ( D ± ) denotes the set of analytic (holomorphic) functions on D ± .

2.3. Scattering Matrix and Reflection Coefficients

Since the Lax matrices are traceless, t r ( U ) = t r ( V ) = 0 , the determinants of the fundamental solutions are independent of x and t. One finds
det Φ ( x , t , z ) = det Ψ ( x , t , z ) = det X ± = ( γ ( z ) ) 2 .
Being fundamental solutions of the scattering problem, Φ and Ψ are related by a constant (in x and t) scattering matrix S ( z ) :
Φ ( x , t , z ) = Ψ ( x , t , z ) S ( z ) , S ( z ) = a ( z ) b ¯ ( z ) b ( z ) a ¯ ( z ) , z ∈ Σ z .
Here, a ( z ) , b ( z ) , a ¯ ( z ) , b ¯ ( z ) are 2 × 2 matrix-valued functions, and the unimodularity condition det S ( z ) = 1 holds. Expanding Equation (36) column-wise yields the linear relations
ϕ = ψ b + ψ ¯ a , ϕ ¯ = ψ a ¯ + ψ ¯ b ¯ .
Using these relations and Equation (35), one can express the determinants of the scattering coefficients as Wronskian ratios:
det a ( z ) = W r ( ϕ , ψ ) W r ( ψ ¯ , ψ ) = det ( ϕ , ψ ) ( γ ( z ) ) 2 ,
det a ¯ ( z ) = W r ( ϕ ¯ , ψ ¯ ) W r ( ψ ¯ , ψ ) = det ( ψ ¯ , ϕ ¯ ) ( γ ( z ) ) 2 .
From the analyticity properties of the Jost functions and the Volterra integral Equation (34), it follows that a ( z ) and det a ( z ) can be analytically extended to the region D + , while a ¯ ( z ) and det a ¯ ( z ) can be analytically extended to D − .
Reflection coefficients are defined by
ρ ( z ) = b ( z ) a − 1 ( z ) , ρ ¯ ( z ) = b ¯ ( z ) a ¯ − 1 ( z ) , z ∈ Σ 0 ,
where Σ 0 = Σ z ∖ { branch points } . Using Equation (37) and the definitions of the modified Jost functions (32), one derives the following relations:
M ( x , t , z ) a − 1 ( z ) = N ¯ ( x , t , z ) + e 2 i θ ( x , t , z ) N ( x , t , z ) ρ ( z ) , M ¯ ( x , t , z ) a ¯ − 1 ( z ) = N ( x , t , z ) + e − 2 i θ ( x , t , z ) N ¯ ( x , t , z ) ρ ¯ ( z ) .
Consequently, M ( x , t , z ) a − 1 ( z ) is meromorphic in the upper half-plane D + , and M ¯ ( x , t , z ) a ¯ − 1 ( z ) is meromorphic in the lower half-plane D − , with poles occurring at the zeros of det a ( z ) and det a ¯ ( z ) , respectively.

2.4. Symmetries

Due to the specific matrix structure of the potential and the imposed boundary conditions, the Jost functions and scattering data inherit three fundamental symmetries. We present their implications in turn.
  • First symmetry (Hermitian conjugation):  ( k , λ ) → ( k * , λ * )
The Jost functions satisfy the involution property
Φ ( x , t , z ) − 1 = 1 γ ( z ) J v Φ † ( x , t , z * ) J v , Ψ ( x , t , z ) − 1 = 1 γ ( z ) J v Ψ † ( x , t , z * ) J v ,
where the constant matrix J v is defined by
J v = Ω − 1 2 × 2 2 × 2 − Σ .
Consequently, the scattering matrix and reflection coefficients obey
S − 1 ( z ) = J v S † ( z * ) J v , ρ ¯ ( z ) = Ω − 1 ρ † ( z * ) Σ − 1 .
If we denote the blocks of the inverse scattering matrix as
S − 1 ( z ) = c ¯ ( z ) d ( z ) d ¯ ( z ) c ( z ) ,
then expanding Equation (44) yields the following relations between the block entries:
c ¯ ( z ) = Ω − 1 a † ( z * ) Ω − 1 , c ( z ) = Σ a ¯ † ( z * ) Σ , d ( z ) = − Ω − 1 b † ( z * ) Σ , d ¯ ( z ) = − Σ b ¯ † ( z * ) Ω − 1 .
Furthermore, the determinants satisfy the conjugation relation
det a ¯ ( z ) = det a † ( z * ) = det a ( z * ) * , z ∈ D − .
  • Second symmetry:  ( k , λ ) → ( k , − λ )
For z ∈ Σ z , the Jost functions transform as
Φ ( x , t , z ) = − i z Φ ( x , t , v k 0 2 / z ) σ 4 Q ˜ − , Ψ ( x , t , z ) = − i z Ψ ( x , t , v k 0 2 / z ) σ 4 Q ˜ + ,
leading to the scattering matrix symmetry
S ( v k 0 2 / z ) = σ 4 Q ˜ + S ( z ) Q ˜ − − 1 σ 4 .
The reflection coefficients consequently satisfy
ρ ( v k 0 2 / z ) = − R + ρ ¯ ( z ) Q + − 1 , ρ ¯ ( v k 0 2 / z ) = − Q + ρ ( z ) R + − 1 .
  • Third symmetry (transposition):  Q → Q T
For z ∈ Σ z , the Jost functions obey the symplectic-like identity
Φ T ( x , t , z ) σ ^ 2 Φ ( x , t , z ) = Ψ T ( x , t , z ) σ ^ 2 Ψ ( x , t , z ) = γ ( z ) σ ^ 2 ,
where
σ ^ 2 = 0 2 × 2 − i I 2 i I 2 0 2 × 2 .
This implies a corresponding symmetry for the scattering matrix and reflection coefficients:
S − 1 ( z ) = σ ^ 2 S T ( z ) σ ^ 2 ,
and
ρ T ( z ) = ρ ( z ) , ρ ¯ T ( z ) = ρ ¯ ( z ) , ρ ¯ ( z ) = Σ ρ * ( z * ) Ω .

2.5. Asymptotics

The asymptotic expansions of the modified Jost functions as z → ∞ are derived by substituting the WKB-type ansatz into the Lax pair equations. For z ∈ D + and z ∈ D − , we obtain respectively:
M ( x , t , z ) = I 2 + i z ∫ − ∞ x [ Q ( x ′ , t ) R ( x ′ , t ) − v k 0 2 I 2 ] d x ′ + O ( 1 / z 2 ) i z R ( x , t ) + O ( 1 / z 2 ) , z ∈ D + ,
M ¯ ( x , t , z ) = − i z Q ( x , t ) + O ( 1 / z 2 ) I 2 − i z ∫ − ∞ x [ R ( x ′ , t ) Q ( x ′ , t ) − v k 0 2 I 2 ] d x ′ + O ( 1 / z 2 ) , z ∈ D − ,
and
N ¯ ( x , t , z ) = I 2 + i z ∫ x ∞ [ Q ( x ′ , t ) R ( x ′ , t ) − v k 0 2 I 2 ] d x ′ + O ( 1 / z 2 ) i z R ( x , t ) + O ( 1 / z 2 ) , z ∈ D − ,
N ( x , t , z ) = − i z Q ( x , t ) + O ( 1 / z 2 ) I 2 − i z ∫ x ∞ [ R ( x ′ , t ) Q ( x ′ , t ) − v k 0 2 I 2 ] d x ′ + O ( 1 / z 2 ) , z ∈ D + .
Similarly, the asymptotic behaviors as z → 0 are found to be
M ( x , t , z ) = v Q R − / k 0 2 + O ( z ) i R − / z + O ( 1 ) , M ¯ ( x , t , z ) = − i Q − / z + O ( 1 ) v R Q − / k 0 2 + O ( z ) ,
N ¯ ( x , t , z ) = v Q R + / k 0 2 + O ( z ) i R + / z + O ( 1 ) , N ( x , t , z ) = − i Q + / z + O ( 1 ) v R Q + / k 0 2 + O ( z ) .
Substituting the above asymptotics into the scattering relation (36) yields the large- and small-z behaviour of S ( z ) :
S ( z ) = I 4 + O ( 1 / z ) , z → ∞ ,
and
S ( z ) = v k 0 2 Q + R − 0 2 × 2 0 2 × 2 R + Q − , z → 0 .

2.6. Discrete Spectrum and Residue Conditions

The discrete spectrum consists of the zeros of the analytic scattering coefficients. In this work, we focus on the case where det a ( z ) possesses a triple zero at z = z n . From the symmetry relation (47), it follows that such zeros do not appear in isolation but rather in quartets:
det a ( z n ) = 0 ⇔ det a ¯ ( z n * ) = 0 ⇔ det a ¯ ( v k 0 2 / z n ) = 0 ⇔ det a ( v k 0 2 / z n * ) = 0 .
Consequently, the discrete spectrum is defined as the set
Z = z n , z n * , v k 0 2 / z n , v k 0 2 / z n * n = 1 N .
To avoid spectral singularities on the continuous spectrum Σ z , we assume det a ( z ) ≠ 0 and det a ¯ ( z ) ≠ 0 for all z ∈ Σ z . To characterize the discrete eigenvalues, it is convenient to introduce the auxiliary 4 × 4 matrices
P ( x , t , z ) = ( ϕ ( x , t , z ) , ψ ( x , t , z ) ) , P ¯ ( x , t , z ) = ( ψ ¯ ( x , t , z ) , ϕ ¯ ( x , t , z ) ) .
As is proved in [30], for a discrete eigenvalue z n ∈ D + ∩ Z , the rank of P ( x , t , z n ) is directly linked to the rank of the scattering block a ( z ) . Specifically:
  • rank   P ( x , t , z n ) = 2 if and only if rank   a ( z ) = 0 (i.e., a ( z n ) = 0 2 × 2 );
  • rank   P ( x , t , z n ) = 3 if and only if rank   a ( z ) = 1 .
Analogous statements hold for the conjugate eigenvalue z n * ∈ D − ∩ Z and the matrix P ¯ .
  • Case of rank   P ( x , t , z n ) = 3
Let α ( z ) and α ¯ ( z ) denote the adjugate matrices of a ( z ) and a ¯ ( z ) , respectively. Since z n is a triple zero of det a ( z ) , we have the linear dependence
ϕ ( x , t , z n ) α ( z n ) = ψ ( x , t , z n ) c n ,
where c n is a nonzero 2 × 2 matrix. To capture the higher-order pole contributions, we differentiate Equation (65) with respect to the spectral parameter z (denoted by a prime) and obtain
( ϕ ( z n ) α ( z n ) ) ′ = ψ ′ ( z n ) c n + ψ ( z n ) d n , ( ϕ ( z n ) α ( z n ) ) ″ = ψ ″ ( z n ) c n + 2 ψ ′ ( z n ) d n + ψ ( z n ) e n ,
where d n , e n are additional 2 × 2 matrices (higher-order scattering data). Using the relation M = Φ e i θ and N from Equation (32), these relations become
( M ( x , t , z n ) α ( z n ) ) ′ = e 2 i θ ( z n ) [ N ′ ( z n ) c n + N ( z n ) ( d n + 2 i θ ′ ( z n ) c n ) ] , ( M ( x , t , z n ) α ( z n ) ) ″ = e 2 i θ ( z n ) [ N ( z n ) ( e n + 4 i θ ′ ( z n ) d n + 2 i θ ″ ( z n ) c n − 4 c n ( θ ′ ( z n ) ) 2 ) + N ″ ( z n ) c n + N ′ ( z n ) ( 2 d n + 4 i θ ′ ( z n ) c n ) ] .
To simplify notation, we write M ( x , t , z ) as M ( z ) in the remainder of this paper. To find the singular part of M ( z ) a − 1 ( z ) = M ( z ) α ( z ) det a ( z ) near z = z n , we consider the function
g ( z ) = ( z − z n ) 3 M ( z ) α ( z ) det a ( z ) ,
where is analytic at z n . Expanding both numerator and denominator in Taylor series, we have
det a ( z ) = 1 3 ! ( det a ) ‴ ( z n ) ( z − z n ) 3 + 1 4 ! ( det a ) ( 4 ) ( z n ) ( z − z n ) 4 + ⋯ ,
and
M ( z ) α ( z ) = M α + ( M α ) ′ ( z − z n ) + 1 2 ! ( M α ) ″ ( z − z n ) 2 + 1 3 ! ( M α ) ‴ ( z − z n ) 3 + ⋯ ,
where M α ≡ M ( z n ) α ( z n ) . Substituting these expansions into g ( z ) and simplifying gives the Taylor expansion of g ( z ) :
g ( z ) = P − 3 [ M ( z ) a − 1 ( z ) ] + P − 2 [ M ( z ) a − 1 ( z ) ] ( z − z n ) + Res [ M ( z ) a − 1 ( z ) ] ( z − z n ) 2 + O ( ( z − z n ) 3 ) .
Here, Res [ M ( z ) a − 1 ( z ) ] , P − 2 [ M ( z ) a − 1 ( z ) ] and P − 3 [ M ( z ) a − 1 ( z ) ] denote the coefficients of ( z − z n ) , ( z − z n ) 2 and ( z − z n ) 3 in the Laurent expansion of M ( z ) a − 1 ( z ) , respectively. The coefficients are obtained from the standard formulas for Taylor coefficients:
Res z = z n [ M ( z ) a − 1 ( z ) ] = 1 2 ! g ″ ( z n ) = 1 2 ! lim z → z n d 2 d z 2 ( z − z n ) 3 M ( z ) α ( z ) det a ( z ) , P − 2 z = z n [ M ( z ) a − 1 ( z ) ] = lim z → z n d d z ( z − z n ) 3 M ( z ) α ( z ) det a ( z ) , P − 3 z = z n [ M ( z ) a − 1 ( z ) ] = lim z → z n ( z − z n ) 3 M ( z ) α ( z ) det a ( z ) .
Evaluating these limits yields
Res z = z n [ M ( z ) a − 1 ( z ) ] = [ − 3 ( M ( z ) α ( z ) ) ′ ( det a ) ( 4 ) ( z ) 2 ( ( det a ) ‴ ( z ) ) 2 + 3 M ( z ) α ( z ) ( ( det a ) ( 4 ) ( z ) ) 2 8 ( ( det a ) ‴ ( z ) ) 3 − 3 M ( z ) α ( z ) ( det a ) ( 5 ) ( z ) 10 ( ( det a ) ‴ ( z ) ) 2 + 3 ( M ( z ) α ( z ) ) ″ ( det a ) ‴ ( z ) ] z = z n , P − 2 z = z n [ M ( z ) a − 1 ( z ) ] = − 3 M ( z ) α ( z ) ( det a ) ( 4 ) ( z ) 2 ( ( det a ) ‴ ( z ) ) 2 + 6 ( M ( z ) α ( z ) ) ′ ( det a ) ‴ ( z ) z = z n , P − 3 z = z n [ M ( z ) a − 1 ( z ) ] = 6 M ( z ) α ( z ) ( det a ) ‴ ( z ) z = z n .
To express these conditions in a compact and useful form, we define the following constant matrices derived from the scattering data and the previously introduced matrices c n , d n , e n
A n = 6 c n det a ‴ ( z n ) , B n = 2 d n − c n ( det a ) ( 4 ) ( z n ) 2 ( det a ) ‴ ( z n ) 3 ( det a ) ‴ ( z n ) , C n = ( ( det a ) ( 4 ) ( z n ) ) 2 8 ( ( det a ) ‴ ( z n ) ) 2 − d n c n − 1 ( det a ) ( 4 ) ( z n ) 2 ( det a ) ‴ ( z n ) − ( det a ) ( 5 ) ( z n ) 10 ( det a ) ‴ ( z n ) + e n c n − 1 3 ( det a ) ‴ ( z n ) .
Substituting the above constant matrices and Equation (67) into Equation (73), we obtain
Res z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) [ 1 2 N ″ ( z n ) A n + N ′ ( z n ) B n + 2 i θ ′ A n + N ( z n ) C n + 2 i θ ′ B n + ( i θ ″ − 2 ( θ ′ ) 2 ) A n ] , P − 2 z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) N ′ ( z n ) A n + N ( z n ) ( B n + 2 i θ ′ A n ) , P − 3 z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) N ( z n ) A n .
Furthermore, we combine the above equations with the phase derivatives to define the norming constants:
C n , 1 = C n + 2 i θ ′ B n + ( i θ ″ − 2 ( θ ′ ) 2 ) A n , C n , 2 = B n + 2 i θ ′ A n , C n , 3 = A n .
In terms of these constants, the singular behavior of M ( z ) a − 1 ( z ) takes its final, compact form:
Res z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) 1 2 N ″ ( z n ) C n , 3 + N ′ ( z n ) C n , 2 + N ( z n ) C n , 1 , P − 2 z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) N ′ ( z n ) C n , 3 + N ( z n ) C n , 2 , P − 3 z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) N ( z n ) C n , 3 .
An entirely analogous derivation for the conjugate pole z = z n * ∈ D − ∩ Z provides the corresponding singular behavior for M ¯ ( z ) a ¯ − 1 ( z ) . The results are structurally identical to (73) under the substitutions M → M ¯ , α → α ¯ , det a ( z ) → det a ¯ ( z ) , and evaluation at z = z n *
Res z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = [ 3 M ¯ ( z ) α ¯ ( z ) ( ( det a ¯ ) ( 4 ) ( z ) ) 2 8 ( ( det a ¯ ) ‴ ( z ) ) 3 − 3 ( M ¯ ( z ) α ¯ ( z ) ) ′ ( det a ¯ ) ( 4 ) ( z ) 2 ( ( det a ¯ ) ‴ ( z ) ) 2 − 3 M ¯ ( z ) α ¯ ( z ) ( det a ¯ ) ( 5 ) ( z ) 10 ( ( det a ¯ ) ‴ ( z ) ) 2 + 3 ( M ¯ ( z ) α ¯ ( z ) ) ″ ( det a ¯ ) ‴ ( z ) ] z = z n * , P − 2 z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = − 3 M ¯ ( z ) α ¯ ( z ) ( det a ¯ ) ( 4 ) ( z ) 2 ( ( det a ¯ ) ‴ ( z ) ) 2 + 6 ( M ¯ ( z ) α ¯ ( z ) ) ′ ( det a ¯ ) ‴ ( z ) z = z n * , P − 3 z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = 6 M ¯ ( z ) α ¯ ( z ) ( det a ¯ ) ‴ ( z ) z = z n * .
These lead to the definition of the norming constants C ¯ n , 1 , C ¯ n , 2 , C ¯ n , 3 , defined exactly as in (74) but with c n , d n , e n replaced by their conjugate counterparts c ¯ n , d ¯ n , e ¯ n . The derivatives of det a replaced by those of det a ¯ evaluated at z = z n * , and θ ′ ( z n ) , θ ″ ( z n ) replaced by θ ′ ( z n * ) , θ ″ ( z n * ) . The final compact form is then:
Res z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z n * ) 1 2 N ¯ ″ ( z n * ) C ¯ n , 3 + N ¯ ′ ( z n * ) C ¯ n , 2 + N ¯ ( z n * ) C ¯ n , 1 , P − 2 z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z n * ) [ N ¯ ′ ( z n * ) C ¯ n , 3 + N ¯ ( z n * ) C ¯ n , 2 ] , P − 3 z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z n * ) N ¯ ( z n * ) C ¯ n , 3 .
By symmetry (49), the points z ^ n = v k 0 2 / z n * and z ¯ ^ = v k 0 2 / z n also belong to the discrete spectrum. At these points, there exist 2 × 2 matrices c ^ n and c ¯ ^ n (and corresponding higher-order constants d ^ n , e ^ n , d ¯ ^ n , e ¯ ^ n ) that satisfy relations analogous to Equations (65) and (66). The singular behaviour of M a − 1 and M ¯ a ¯ − 1 at these points can be obtained by applying the same derivative formulas and symmetry transformations. And thus, we can obtain the corresponding residue conditions:
Res z = z ^ n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z ^ n ) 1 2 N ″ ( z ^ n ) C ^ n , 3 + N ′ ( z ^ n ) C ^ n , 2 + N ( z ^ n ) C ^ n , 1 , P − 2 z = z ^ n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z ^ n ) [ N ′ ( z ^ n ) C ^ n , 3 + N ( z ^ n ) C ^ n , 2 ] , P − 3 z = z ^ n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z ^ n ) N ( z ^ n ) C ^ n , 3 ,
and
Res z = z ^ n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z ^ n * ) 1 2 N ¯ ″ ( z ^ n * ) C ¯ ^ n , 3 + N ¯ ′ ( z ^ n * ) C ¯ ^ n , 2 + N ¯ ( z ^ n * ) C ¯ ^ n , 1 , P − 2 z = z ^ n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z ^ n * ) [ N ¯ ′ ( z ^ n * ) C ¯ ^ n , 3 + N ¯ ( z ^ n * ) C ¯ ^ n , 2 ] , P − 3 z = z ^ n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z ^ n * ) N ¯ ( z ^ n * ) C ¯ ^ n , 3 ,
where
A ^ n = 6 c ^ n det a ‴ ( z ^ n ) , B ^ n = 2 d ^ n − c ^ n ( det a ) ( 4 ) ( z ^ n ) 2 ( det a ) ‴ ( z ^ n ) 3 ( det a ) ‴ ( z ^ n ) , C ^ n = ( ( det a ) ( 4 ) ( z ^ n ) ) 2 8 ( ( det a ) ‴ ( z ^ n ) ) 2 − d ^ n c ^ n − 1 ( det a ) ( 4 ) ( z ^ n ) 2 ( det a ) ‴ ( z ^ n ) − ( det a ) ( 5 ) ( z ^ n ) 10 ( det a ) ‴ ( z ^ n ) + e ^ n c ^ n − 1 3 ( det a ) ‴ ( z ^ n ) , C ^ n , 1 = C ^ n + 2 i θ ′ B ^ n + ( i θ ″ − 2 ( θ ′ ) 2 ) A ^ n , C ^ n , 2 = B ^ n + 2 i θ ′ A ^ n , C ^ n , 3 = A ^ n ,
and the definition of norming constants C ¯ ^ n , 1 , C ¯ ^ n , 2 , C ¯ ^ n , 3 , defined exactly as in Equation (80) but with c ^ n , d ^ n , e ^ n replaced by their conjugate counterparts c ¯ ^ n , d ¯ ^ n , e ¯ ^ n . The derivatives of det a replaced by those of det a ¯ evaluated at z = z ^ n * , and θ ′ ( z ^ n ) , θ ″ ( z ^ n ) replaced by θ ′ ( z ^ n * ) , θ ″ ( z ^ n * ) .
The symmetry z → v k 0 2 / z induces relations between the norming constants at the symmetric points. After a careful computation (detailed in Appendix B), we obtain the following expressions for the norming constants:
C ^ n , 1 = 1 ( z n * ) 2 R + C ¯ n , 1 R + − 2 ( z n * ) 3 R + ( C ¯ n , 2 − i θ ′ ( z n * ) C ¯ n , 3 ) R + + 3 ( z n * ) 4 R + C ¯ n , 3 R + , C ^ n , 2 = 1 ( z n * ) 2 R + C ¯ n , 2 R + − 3 ( z n * ) 3 R + C ¯ n , 3 R + , C ^ n , 3 = 1 ( z n * ) 2 R + C ¯ n , 3 R + .
II.
Case of rank   P ( x , t , z n ) = 2
This case corresponds to rank   a ( z n ) = 0 , i.e., a ( z n ) = 0 2 × 2 (and similarly a ¯ ( z n * ) = 0 2 × 2 ). Consequently, the Jost functions are linearly dependent at the eigenvalue:
ϕ ( x , t , z n ) = ψ ( x , t , z n ) b n , ϕ ¯ ( x , t , z n * ) = ψ ¯ ( x , t , z n * ) b ¯ n ,
where b n and b ¯ n are nonsingular 2 × 2 matrices.
A crucial subtlety must be addressed. If det a ( z ) possessed only a third-order zero at z n , the meromorphic matrix function M a − 1 would exhibit at most a double pole. To obtain a genuine triple pole—the central object of this paper, a stronger condition is indispensable: det a ( z ) must have a fourth-order zero at z = z n . We therefore introduce the function
f ( z ) = ( z − z n ) 4 M ( z ) α ( z ) det a ( z ) ,
where is analytic at z n . Expanding both numerator and denominator in Taylor series gives
det a ( z ) = 1 4 ! ( det a ) ( 4 ) ( z n ) ( z − z n ) 4 + 1 5 ! ( det a ) ( 5 ) ( z n ) ( z − z n ) 5 + ⋯ ,
and
M ( z ) α ( z ) = M α + ( M α ) ′ ( z − z n ) + 1 2 ! ( M α ) ″ ( z − z n ) 2 + 1 3 ! ( M α ) ‴ ( z − z n ) 3 + 1 4 ! ( M α ) ( 4 ) ( z − z n ) 4 + ⋯ .
Substituting these expansions into Equation (83) and simplifying yields the Taylor expansion of f ( z ) :
f ( z ) = P − 4 [ M ( z ) a − 1 ( z ) ] + P − 3 [ M ( z ) a − 1 ( z ) ] ( z − z n ) + P − 2 [ M ( z ) a − 1 ( z ) ] ( z − z n ) 2 + Res [ M ( z ) a − 1 ( z ) ] ( z − z n ) 3 + O ( ( z − z n ) 4 ) .
Here, Res [ M ( z ) a − 1 ( z ) ] , P − 2 [ M ( z ) a − 1 ( z ) ] , P − 3 [ M ( z ) a − 1 ( z ) ] and P − 4 [ M ( z ) a − 1 ( z ) ] denote the coefficients of ( z − z n ) , ( z − z n ) 2 , ( z − z n ) 3 and ( z − z n ) 4 in the Laurent expansion of M ( z ) a − 1 ( z ) , respectively. The coefficients are obtained from the standard formulas for Taylor coefficients:
Res z = z n [ M ( z ) a − 1 ( z ) ] = 1 3 ! lim z → z n d 3 d z 3 ( z − z n ) 4 M ( z ) α ( z ) det a ( z ) , P − 2 z = z n [ M ( z ) a − 1 ( z ) ] = 1 2 ! lim z → z n d 2 d z 2 ( z − z n ) 4 M ( z ) α ( z ) det a ( z ) , P − 3 z = z n [ M ( z ) a − 1 ( z ) ] = lim z → z n d d z ( z − z n ) 4 M ( z ) α ( z ) det a ( z ) , P − 4 z = z n [ M ( z ) a − 1 ( z ) ] = lim z → z n ( z − z n ) 4 M ( z ) α ( z ) det a ( z ) .
After a straightforward (though lengthy) computation, the singular part of M a − 1 at z = z n can again be cast into the compact form (74), but the norming constants C n , 1 , C n , 2 and C n , 3 are now defined by more elaborate expressions that involve b n , d n , e n and the derivatives of det a ( z ) up to sixth order. Explicitly,
Res z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) 1 2 N ″ ( z n ) C n , 3 + N ′ ( z n ) C n , 2 + N ( z n ) C n , 1 , P − 2 z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) [ N ′ ( z n ) C n , 3 + N ( z n ) C n , 2 ] , P − 3 z = z n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z n ) N ( z n ) C n , 3 , P − 4 z = z n [ M ( z ) a − 1 ( z ) ] = 0 4 × 2 .
The auxiliary constants are constructed from the matrices b n , d n , e n and the derivatives of det a ( z )
A n = 24 b n α ′ ( z n ) ( det a ) ( 4 ) ( z n ) , B n = d n b n − 1 − ( det a ) ( 5 ) ( z n ) 5 ( det a ) ( 4 ) ( z n ) , C n = 12 b n α ″ ( z n ) ( det a ) ( 4 ) ( z n ) , D n = 1 2 e n b n − 1 − ( det a ) ( 6 ) ( z n ) 30 ( det a ) ( 4 ) ( z n ) , E n = 4 b n α ‴ ( z n ) ( det a ) ( 4 ) ( z n ) .
The norming constants for the triple-pole (fourth-order zero) case are then defined by
C n , 1 = A n 2 i θ ′ ( z n ) − ( det a ) ( 5 ) ( z n ) 5 ( det a ) ( 4 ) ( z n ) B n + i θ ″ ( z n ) − 2 ( θ ′ ( z n ) ) 2 + D n + C n ( B n + 2 i θ ′ ( z n ) ) + E n , C n , 2 = A n B n + 2 i θ ′ ( z n ) + C n , C n , 3 = A n .
The corresponding quantities for the conjugate pole z n * are obtained by the usual substitutions ( M , α , det a , z n ) ⟶ ( M ¯ , α ¯ , det a ¯ , z n * ) and θ ⟶ − θ . They take the form
Res z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z n * ) 1 2 N ¯ ″ ( z n * ) C ¯ n , 3 + N ¯ ′ ( z n * ) C ¯ n , 2 + N ¯ ( z n * ) C ¯ n , 1 , P − 2 z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z n * ) [ N ¯ ′ ( z n * ) C ¯ n , 3 + N ¯ ( z n * ) C ¯ n , 2 ] , P − 3 z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z n * ) N ¯ ( z n * ) C ¯ n , 3 , P − 4 z = z n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = 0 4 × 2 ,
where C ¯ n , 1 , C ¯ n , 2 , C ¯ n , 3 are defined analogously to Equation (77) with all quantities replaced by their conjugate counterparts.
Similarly, for z ^ n = v k 0 2 / z n * and z ¯ ^ = v k 0 2 / z n , we have
Res z = z ^ n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z ^ n ) 1 2 N ″ ( z ^ n ) C ^ n , 3 + N ′ ( z ^ n ) C ^ n , 2 + N ( z ^ n ) C ^ n , 1 , P − 2 z = z ^ n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z ^ n ) [ N ′ ( z ^ n ) C ^ n , 3 + N ( z ^ n ) C ^ n , 2 ] , P − 3 z = z ^ n [ M ( z ) a − 1 ( z ) ] = e 2 i θ ( z ^ n ) N ( z ^ n ) C ^ n , 3 , P − 4 z = z ^ n [ M ( z ) a − 1 ( z ) ] = 0 4 × 2 ,
and
Res z = z ^ n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z ^ n * ) 1 2 N ¯ ″ ( z ^ n * ) C ¯ ^ n , 3 + N ¯ ′ ( z ^ n * ) C ¯ ^ n , 2 + N ¯ ( z ^ n * ) C ¯ ^ n , 1 , P − 2 z = z ^ n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z ^ n * ) [ N ¯ ′ ( z ^ n * ) C ¯ ^ n , 3 + N ¯ ( z ^ n * ) C ¯ ^ n , 2 ] , P − 3 z = z ^ n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = e − 2 i θ ( z ^ n * ) N ¯ ( z ^ n * ) C ¯ ^ n , 3 , P − 4 z = z ^ n * [ M ¯ ( z ) a ¯ − 1 ( z ) ] = 0 4 × 2 ,
where
A ^ n = 24 b ^ n α ′ ( z ^ n ) ( det a ) ( 4 ) ( z ^ n ) , B ^ n = d ^ n b ^ n − 1 − ( det a ) ( 5 ) ( z ^ n ) 5 ( det a ) ( 4 ) ( z ^ n ) , C ^ n = 12 b ^ n α ″ ( z ^ n ) ( det a ) ( 4 ) ( z ^ n ) , D ^ n = 1 2 e ^ n b ^ n − 1 − ( det a ) ( 6 ) ( z ^ n ) 30 ( det a ) ( 4 ) ( z ^ n ) , E ^ n = 4 b ^ n α ‴ ( z ^ n ) ( det a ) ( 4 ) ( z ^ n ) ,
and
C ^ n , 1 = A ^ n ( 2 i θ ′ ( z ^ n ) − ( det a ) ( 5 ) ( z ^ n ) 5 ( det a ) ( 4 ) ( z ^ n ) ) B ^ n + i θ ″ ( z ^ n ) − 2 ( θ ′ ( z ^ n ) ) 2 + D ^ n + C ^ n ( B ^ n + 2 i θ ′ ( z ^ n ) ) + E ^ n , C ^ n , 2 = A ^ n ( B ^ n + 2 i θ ′ ( z ^ n ) ) + C ^ n , C ^ n , 3 = A ^ n .
The norming constants C ¯ ^ n , 1 , C ¯ ^ n , 2 , C ¯ ^ n , 3 are defined analogously to the case rank   P ( x , t , z n ) = 3 . By calculation, we obtain the symmetry of the norming constant.
C ^ n , 1 = 1 ( z n * ) 2 R + C ¯ n , 1 R + − 2 ( z n * ) 3 R + ( C ¯ n , 2 − i θ ′ ( z n * ) C ¯ n , 3 ) R + + 3 ( z n * ) 4 R + C ¯ n , 3 R + , C ^ n , 2 = 1 ( z n * ) 2 R + C ¯ n , 2 R + − 3 ( z n * ) 3 R + C ¯ n , 3 R + , C ^ n , 3 = 1 ( z n * ) 2 R + C ¯ n , 3 R + .
The derivation is provided in Appendix B. We find the symmetries of the norming constants coincide with those in Equation (81).

3. Inverse Scattering Problem

3.1. Riemann-Hilbert Problem

The inverse problem is formulated as a matrix RH problem for sectionally meromorphic functions. We introduce the following sectionally meromorphic matrices:
μ + ( x , t , z ) = ( M a − 1 , N ) , μ − ( x , t , z ) = ( N ¯ , M ¯ a ¯ − 1 ) ,
where μ ± ( x , t , z ) are analytic in D ± , respectively, except at the discrete eigenvalues where they possess poles. From the scattering relation (36), these matrices satisfy the following jump condition across the contour Σ z :
μ − ( x , t , z ) = μ + ( x , t , z ) ( I 4 − G ( x , t , z ) ) ,
with the jump matrix G ( x , t , z ) given by
G ( x , t , z ) = 0 2 × 2 − e − 2 i θ ( x , t , z ) ρ ¯ ( z ) e 2 i θ ( x , t , z ) ρ ( z ) ρ ( z ) ρ ¯ ( z ) .
The asymptotic behaviour of μ ± ( z ) follows directly from the expansions of the modified Jost functions and scattering coefficients obtained in Section 2.5. As z → ∞ (in the respective half-plane),
μ ± = I 4 + o ( 1 / z ) ,
while as z → 0 ,
μ ± = − i z σ 4 Q ˜ + + o ( 1 ) .
To obtain an explicit integral representation for the solution, we regularize the RH problem by subtracting the pole contributions. Define ξ j = z j for j = 1 , 2 , … , N , and ξ j = z ^ j − N for j = N + 1 , N + 2 , … , 2 N , encompassing all discrete eigenvalues in D + . The contribution from the poles of M a − 1 is explicitly subtracted from μ + . Applying the Cauchy projection operator to the regularized RH problem then yields the following integral equation for N ¯ ( z ) :
N ¯ ( z ) = I 2 i z R + + ∑ j = 1 2 N Res z = z j ( M a − 1 ) z − ξ j + ∑ j = 1 2 N P − 2 z = z j ( M a − 1 ) z − ξ j 2 + ∑ j = 1 2 N P − 3 z = z j ( M a − 1 ) z − ξ j 3 + 1 2 π i ∫ Σ z e 2 i θ ( ξ ) N ( ξ ) ρ ( ξ ) ξ − ( z − i 0 ) d ξ ,
where the residues and pole coefficients are given by Equations (75) and (88). Similarly, an integral equation for N ( z ) is obtained by considering the poles of M ¯ a ¯ − 1 in D − :
N ( z ) = − i z Q + I 2 + ∑ j = 1 2 N Res z = z j * ( M ¯ a ¯ − 1 ) z − ξ j * + ∑ j = 1 2 N P − 2 z = z j * ( M ¯ a ¯ − 1 ) z − ξ j * 2 + ∑ j = 1 2 N P − 3 z = z j * ( M ¯ a ¯ − 1 ) z − ξ j * 3 − 1 2 π i ∫ Σ z e − 2 i θ ( ξ ) N ¯ ( ξ ) ρ ¯ ( ξ ) ξ − ( z + i 0 ) d ξ .
Here, ξ j * = z j * for j = 1 , 2 , … , N , and ξ j * = z ^ j − N * for j = N + 1 , N + 2 , … , 2 N . The corresponding constants C j , i , C ^ j , i , C ¯ j , i , C ¯ ^ j , i ( i = 1 , 2 , 3 ) are defined in Section 2.6.
The potential Q ( x , t ) is reconstructed from the large-z asymptotics of the solution to the RH problem. Comparing the O ( z − 1 ) term in the expansion of (102) or (103) with the asymptotic Formula (57) yields:
Q ( x , t ) = Q + + i ∑ j = 1 2 N e − 2 i θ ( ξ j * ) 1 2 N ¯ j , 2 u p ( ξ j * ) C ¯ j , 3 + N ¯ j , 1 u p ( ξ j * ) C ¯ j , 2 + N ¯ j , 0 u p ( ξ j * ) C ¯ j , 1 + 1 π ∫ Σ z e − 2 i θ ( x , t , ξ ) N ¯ u p ( x , t , ξ ) ρ ¯ ( ξ ) d ξ ,
R ( x , t ) = R + − i ∑ j = 1 2 N e 2 i θ ( ξ j ) 1 2 N j , 2 d n ( ξ j ) C j , 3 + N j , 1 d n ( ξ j ) C j , 2 + N j , 0 d n ( ξ j ) C j , 1 + 1 π ∫ Σ z e 2 i θ ( x , t , ξ ) N d n ( x , t , ξ ) ρ ( ξ ) d ξ .
In Equations (102) and (103), we have used the block decomposition N ( x , t ) = ( N u p , N d n ) T and N ¯ ( x , t ) = ( N ¯ u p , N ¯ d n ) T , where the superscripts up and dn denote the upper and lower 2 × 2 blocks, respectively. The coefficients N j , k and N ¯ j , k are defined as the derivatives of these blocks at the discrete eigenvalues:
N n , 0 ( x , t ) = N ( x , t , z n ) , N ¯ n , 0 ( x , t ) = N ¯ ( x , t , z n * ) , N n , 1 ( x , t ) = ( ∂ N / ∂ z ) ( x , t , z n ) , N ¯ n , 1 ( x , t ) = ( ∂ N ¯ / ∂ z ) ( x , t , z n * ) , N n , 2 ( x , t ) = ( ∂ 2 N / ∂ z 2 ) ( x , t , z n ) , N ¯ n , 2 ( x , t ) = ( ∂ 2 N ¯ / ∂ z 2 ) ( x , t , z n * ) .
The symmetry relations for the potential, R = Σ Q † Ω , together with the asymptotic behaviors N d n ( x , t , z ) ∼ I 2 and N ¯ u p ( x , t , z ) ∼ I 2 as x → ∞ , impose constraints on the norming constants. By comparing the structures of the reconstruction Formulas (102) and (103), we deduce the following symmetry:
C ¯ j , n = Ω − 1 C j , n † Σ − 1 , n = 1 , 2 , 3 , j = 1 , ⋯ , 2 N .
If, in addition, the potential satisfies the transposition reduction Q ( x , t ) = Q T ( x , t ) (equivalently R ( x , t ) = R T ( x , t ) ), the norming constants inherit the symmetry:
C ¯ j , n = C ¯ j , n T , C j , n = C j , n T , n = 1 , 2 , 3 , j = 1 , ⋯ , 2 N .

3.2. Reflectionless Case and N-Triple-Pole Soliton Solutions

In the reflectionless case, where the reflection coefficients vanish ( ρ ( z ) = ρ ¯ ( z ) = 0 2 × 2 ), the RH problem simplifies considerably. The integral terms in Equations (102) and (103) vanish, reducing the problem to a closed algebraic system for the eigenfunctions. Focusing on the upper blocks ( u p -components), we obtain the following system:
N ¯ u p ( z ) = I 2 + ∑ j = 1 2 N e 2 i θ ( ξ j ) 1 2 N j , 2 u p ( x , t ) C j , 3 + N j , 1 u p ( x , t ) C j , 2 + N j , 0 u p ( x , t ) C j , 1 z − ξ j + ∑ j = 1 2 N e 2 i θ ( ξ j ) ( N j , 1 u p ( x , t ) C j , 3 + N j , 0 u p ( x , t ) C j , 2 ) z − ξ j 2 + ∑ j = 1 2 N e 2 i θ ( ξ j ) N j , 0 u p ( x , t ) C j , 3 z − ξ j 3 ,
and
N u p ( z ) = − i z Q + + ∑ j = 1 2 N e − 2 i θ ( ξ j * ) 1 2 N ¯ j , 2 u p ( x , t ) C ¯ j , 3 + N ¯ j , 1 u p ( x , t ) C ¯ j , 2 + N ¯ j , 0 u p ( x , t ) C ¯ j , 1 z − ξ j * + ∑ j = 1 2 N e − 2 i θ ( ξ j * ) ( N ¯ j , 1 u p ( x , t ) C ¯ j , 3 + N ¯ j , 0 u p ( x , t ) C ¯ j , 2 ) z − ξ j * 2 + ∑ j = 1 2 N e − 2 i θ ( ξ j * ) N ¯ j , 0 u p ( x , t ) C ¯ j , 3 z − ξ j * 3 .
Here, for brevity, we have written N j , k u p = N j , k u p ( x , t ) and similarly for N ¯ j , k u p .
Theorem 1.
(General N-triple-pole soliton solution). In the reflectionless case, the general N-triple-pole soliton solution of the matrix NLS Equation (6) under nonzero boundary conditions is reconstructed via
Q ( x , t ) = Q + + i ∑ n = 1 2 N e − 2 i θ ( ξ n * ) 1 2 N ¯ n , 2 u p ( ξ n * ) C ¯ n , 3 + N ¯ n , 1 u p ( ξ n * ) C ¯ n , 2 + N ¯ n , 0 u p ( ξ n * ) C ¯ n , 1 .
The functions N ¯ j , 2 u p ( x , t ) , N ¯ j , 1 u p ( x , t ) and N ¯ j , 0 u p ( x , t ) are determined by solving the linear algebraic system formed by evaluating Equation (108) at the points z = ξ k * for k = 1 , … , 2 N .
A detailed example for the fundamental case N = 1 is presented in the Appendix A.

4. Discussion

In this paper, we have systematically developed the inverse scattering transform for the matrix NLS equation under NZBCs, focusing on the case where the discrete spectrum contains triple poles. Two distinct scenarios arise from the rank of the matrix P ( x , t , z n ) : the case rank   P ( x , t , z n ) = 3 requires a third-order zero of det a ( z ) at z = z n , while rank   P ( x , t , z n ) = 2 necessitates a fourth-order zero. For each case, we derived the corresponding residue conditions and established the symmetries of the associated norming constants, thereby completing the discrete spectral analysis for triple poles. Solving the resulting matrix RH problem in the reflectionless case yielded explicit closed-form expressions for the general N-triple-pole soliton solutions.
The extension from double to triple poles in the matrix setting is by no means a mere parameter adjustment. The matrix structure introduces a forced correspondence between the order of zeros of det a ( z ) and the rank of the eigenfunction matrix P ( x , t , z n ) —a feature already present at the double-pole level, but whose explicit realization at third order requires:
  • handling third-order poles in the matrix Riemann–Hilbert problem under two distinct reduction classes;
  • deriving Laurent coefficients up to order three for both admissible rank cases ( rank   P = 2 , 3 );
  • constructing norming constants C n , 1 , C n , 2 , C n , 3 that absorb all higher-order scattering data;
  • respecting the quartet symmetry z n , z n * , v k 0 2 / z n , v k 0 2 / z n * imposed by the boundary conditions.
Building on these results, several directions merit further investigation. First, a natural extension is to establish a unified framework for constructing soliton solutions with arbitrary-order poles under nonzero boundary conditions. Such an extension would complete the hierarchy of higher-order poles within the IST formalism and reveal deeper algebraic structures inherent in integrable systems. Second, the long-time asymptotics of solutions in the presence of higher-order discrete spectra constitutes a challenging yet important problem. The RH formalism established herein provides an ideal starting point for this endeavor, following the seminal work of Deift-Zhou and subsequent developments [31,32,33,34].
Beyond these mathematical generalizations, the matrix NLS equation under NZBCs is not merely a mathematical abstraction—it is the mean-field model for F = 1 spinor BEC in the homogeneous trap-free regime, and also arises in the description of four-wave mixing processes in nonlinear optics. Equation (6) can be reduced to two-component or even scalar NLS systems via appropriate parameter choices, retaining significant physical content—from optical spatiotemporal solitons to effective descriptions of bilayer graphene [35]. These connections provide fertile ground for further interdisciplinary exploration. In particular, Cases 3 and 4—though not directly applicable to F = 1 condensates—also warrant attention. They find important applications in other physical contexts, such as multicolor optical solitons and models of superconducting phenomena [35]. Elucidating these connections and investigating the role of triple-pole structures in such systems would constitute a valuable extension of the present work.

Author Contributions

Conceptualization, G.Z. and Y.Z.; methodology, Y.Z.; software, Z.H.; validation, Y.Z., Z.H. and H.Z.; formal analysis, Y.Z.; investigation, Y.Z.; resources, G.Z.; data curation, Z.H.; writing—original draft preparation, Y.Z.; writing—review and editing, G.Z.; visualization, Z.H.; supervision, G.Z.; project administration, G.Z.; funding acquisition, G.Z. All authors have read and agreed to the published version of the manuscript.

Funding

This work is supported by Zhejiang Provincial Natural Science Foundation of China (Grant No. LQN25A010010), the Guangdong Basic and Applied Basic Research Foundation (Grant No. 2024A1515013106), and the National Natural Science Foundation of China (Grant Nos. 12471239 and 11871446).

Data Availability Statement

The original contributions presented in this study are included in the article. Further inquiries can be directed to the corresponding author.

Conflicts of Interest

The authors declare no conflicts of interest.

Appendix A. Explicit Example for N = 1

This appendix demonstrates the application of the general theory developed in Section 2 and Section 3 to the simplest nontrivial case N = 1 . Its purpose is twofold: first, to show how the abstract IST formalism yields a concrete solution; and second, to provide a complete algebraic framework that interested readers can use as a starting point for further analytical or numerical investigation, including the generation of soliton profiles.
For N = 1 , the discrete spectrum consists of a quartet of eigenvalues: Z = { z 1 , z 1 * , z ^ 1 , z ^ 1 * } , with z ^ 1 = v k 0 2 / z 1 * and z ^ 1 * = v k 0 2 / z 1 . The solution is constructed from Theorem 1 (Equation (110) in the main text), which for N = 1 simplifies to the following explicit expression for Q ( x , t ) :
Q ( x , t ) = Q + + i ∑ n = 1 2 e − 2 i θ ( ξ n * ) 1 2 N ¯ n , 2 u p ( ξ n * ) C ¯ n , 3 + N ¯ n , 1 u p ( ξ n * ) C ¯ n , 2 + N ¯ n , 0 u p ( ξ n * ) C ¯ n , 1 ,
where ( ξ 1 , ξ 2 ) = ( z 1 , z ^ 1 ) and ( ξ 1 * , ξ 2 * ) = ( z 1 * , z ^ 1 * ) . The unknown functions N ¯ n , k u p ( n = 1 , 2 ;   k = 0 , 1 , 2 ) are determined by solving a linear algebraic system obtained from the eigenfunction relations (108) and (109). Substituting Equation (108) into (109) yields the following compact form:
N ¯ j , k ( ξ n * ) = A i + N ¯ 1 , 2 ( ξ 1 * ) D i + N ¯ 2 , 2 ( ξ 2 * ) E i + N ¯ 1 , 1 ( ξ 1 * ) F i + N ¯ 2 , 1 ( ξ 2 * ) G i + N ¯ 1 , 0 ( ξ 1 * ) H i + N ¯ 2 , 0 ( ξ 2 * ) K i ,
where j = 1 , 2 ; k = 0 , 1 , 2 ; i = 1 , 2 , 3 , 4 , 5 , 6 . The coefficients A i , D i , E i , F i , G i , H i and K i are defined below:
  • X n = I 2 , n = 1 , 0 2 × 2 , n = 2 , Y n = 0 2 × 2 , n = 1 , I 2 , n = 2 ,
  • A n = I 2 − i Q + ∑ j = 1 2 N e 2 i θ ( ξ j ) ξ j ( z n * − ξ j ) C j , 1 + C j , 2 ( z n * − ξ j ) + C j , 3 ( z n * − ξ j ) 2 − C j , 2 ξ j − C j , 3 ξ j ( z n * − ξ j ) + C j , 3 ξ j 2 , A s = i Q + ∑ j = 1 2 N e 2 i θ ( ξ j ) ξ j z s − 2 * − ξ j 2 [ C j , 1 + 2 C j , 2 z s − 2 * − ξ j + 3 C j , 3 z s − 2 * − ξ j 2 − C j , 2 ξ j + C j , 3 ξ j 2 − 2 C j , 3 ξ j z s − 2 * − ξ j ] ,
  • A t = − i Q + ∑ j = 1 2 N e 2 i θ ( ξ j ) ξ j ( z t − 4 * − ξ j ) 3 [ 2 C j , 1 + 6 C j , 2 ( z t − 4 * − ξ j ) + 12 C j , 3 ( z t − 4 * − ξ j ) 2 − 2 C j , 2 ξ j + C j , 3 ξ j 2 − 6 C j , 3 ξ j ( z t − 4 * − ξ j ) ] ,
  • F n = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) ( z n * − ξ j ) ( ξ j − z 1 * ) [ C 2 ¯ + C 3 ¯ ξ j − z 1 * C j , 1 + C j , 2 z n * − ξ j + C j , 3 z n * − ξ j 2 − 1 ( ξ j − z 1 * ) C 2 ¯ + 2 C 3 ¯ ξ j − z 1 * C j , 2 + C j , 3 z n * − ξ j + 1 ( ξ j − z 1 * ) 2 C 2 ¯ + 3 C 3 ¯ ξ j − z 1 * C j , 3 ] ,
  • F s = − X s − 2 + ∑ j = 1 2 N − e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) z s − 2 * − ξ j 2 ξ j − z 1 * [ C ¯ 2 + C ¯ 3 ξ j − z 1 * C j , 1 + 2 C j , 2 z s − 2 * − ξ j + 3 C j , 3 z s − 2 * − ξ j 2 − 1 ξ j − z 1 * C ¯ 2 + 2 C ¯ 3 ξ j − z 1 * C j , 2 + 2 C j , 3 z s − 2 * − ξ j + 1 ξ j − z 1 * 2 C ¯ 2 + 3 C ¯ 3 ξ j − z 1 * C j , 3 ] ,
  • F t = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) z t − 4 * − ξ j 3 ξ j − z 1 * [ C ¯ 2 + C ¯ 3 ξ j − z 1 * 2 C j , 1 + 6 C j , 2 z t − 4 * − ξ j + 12 C j , 3 z t − 4 * − ξ j 2 − 1 ( ξ j − z 1 * ) C ¯ 2 + 2 C ¯ 3 ξ j − z 1 * 2 C j , 2 + 6 C j , 3 z t − 4 * − ξ j + 1 ξ j − z 1 * 2 2 C ¯ 2 + 6 C ¯ 3 ξ j − z 1 * C j , 3 ] ,
  • G n = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) ( z n * − ξ j ) ( ξ j − z ^ 1 * ) [ C ¯ ^ 2 + C ¯ ^ 3 ξ j − z ^ 1 * C j , 1 + C j , 2 z n * − ξ j + C j , 3 z n * − ξ j 2 − 1 ( ξ j − z ^ 1 * ) C ¯ ^ 2 + 2 C ¯ ^ 3 ξ j − z ^ 1 * C j , 2 + C j , 3 z n * − ξ j + 1 ξ j − z ^ 1 * 2 C ¯ ^ 2 + 3 C ¯ ^ 3 ξ j − z ^ 1 * C j , 3 ] ,
  • G s = − Y s − 2 + ∑ j = 1 2 N − e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) z s − 2 * − ξ j 2 ( ξ j − z ^ 1 * ) [ C ¯ ^ 2 + C ¯ ^ 3 ξ j − z ^ 1 * C j , 1 + 2 C j , 2 z s − 2 * − ξ j + 3 C j , 3 z s − 2 * − ξ j 2 − 1 ( ξ j − z ^ 1 * ) C ¯ ^ 2 + 2 C ¯ ^ 3 ξ j − z ^ 1 * C j , 2 + 2 C j , 3 z s − 2 * − ξ j + 1 ξ j − z ^ 1 * 2 C ¯ ^ 2 + 3 C ¯ ^ 3 ξ j − z ^ 1 * C j , 3 ] ,
  • G t = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) ( z t − 4 * − ξ j ) 3 ( ξ j − z 1 ^ * ) [ C ¯ ^ 2 + C ¯ ^ 3 ξ j − z ^ 1 * 2 C j , 1 + 6 C j , 2 z t − 4 * − ξ j + 12 C j , 3 z t − 4 * − ξ j 2 − 1 ( ξ j − z ^ 1 * ) C ¯ ^ 2 + 2 C ¯ ^ 3 ξ j − z ^ 1 * 2 C j , 2 + 6 C j , 3 z t − 4 * − ξ j + 1 ξ j − z ^ 1 * 2 2 C ¯ ^ 2 + 6 C ¯ ^ 3 ξ j − z ^ 1 * C j , 3 ] ,
  • D n = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) ( z n * − ξ j ) ( ξ j − z 1 * ) C ¯ 3 2 [ C j , 1 + C j , 2 z n * − ξ j + C j , 3 z n * − ξ j 2 + 1 ξ j − z 1 * 2 C j , 3 − 1 ξ j − z 1 * C j , 2 + C j , 3 z n * − ξ j ] ,
  • D s = ∑ j = 1 2 N − e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) z s − 2 * − ξ j 2 ( ξ j − z 1 * ) C 3 ¯ 2 [ C j , 1 + 2 C j , 2 z s − 2 * − ξ j + 3 C j , 3 z s − 2 * − ξ j 2 + 1 ξ j − z 1 * 2 C j , 3 − 1 ξ j − z 1 * C j , 2 + 2 C j , 3 z s − 2 * − ξ j ] ,
  • D t = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) z t − 4 * − ξ j 3 ( ξ j − z 1 * ) C ¯ 3 [ C j , 1 + 3 C j , 2 z t − 4 * − ξ j + 6 C j , 3 z t − 4 * − ξ j 2 + 1 ξ j − z 1 * 2 C j , 3 − 1 ξ j − z 1 * C j , 2 + 3 C j , 3 z t − 4 * − ξ j ] − X t − 4 ,
  • E n = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) ( z n * − ξ ^ j ) ( ξ j − z ^ 1 * ) C ¯ ^ 3 2 [ C j , 1 + C j , 2 z n * − ξ j + C j , 3 z n * − ξ j 2 + 1 ξ j − z ^ 1 * 2 C j , 3 − 1 ξ j − z ^ 1 * C j , 2 + C j , 3 z n * − ξ j ] ,
  • E s = ∑ j = 1 2 N − e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) z s − 2 * − ξ j 2 ( ξ j − z ^ 1 * ) C ¯ ^ 3 2 [ C j , 1 + 2 C j , 2 z s − 2 * − ξ j + 3 C j , 3 z s − 2 * − ξ j 2 + 1 ξ j − z ^ 1 * 2 C j , 3 − 1 ξ j − z ^ 1 * C j , 2 + 2 C j , 3 z s − 2 * − ξ j ] ,
  • E t = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( ξ 1 * ) ) z t − 4 * − ξ j 3 ( ξ j − z ^ 1 * ) C ¯ ^ 3 [ C j , 1 + 3 C j , 2 z t − 4 * − ξ j + 6 C j , 3 z t − 4 * − ξ j 2 + 1 ξ j − z ^ 1 * 2 C j , 3 − 1 ξ j − z ^ 1 * C j , 2 + 3 C j , 3 z t − 4 * − ξ j ] − Y t − 4 ,
  • H n = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) ( z n * − ξ j ) ( ξ j − z 1 * ) [ 1 ( ξ j − z 1 * ) 2 C 1 ¯ + 3 C 2 ¯ ξ j − z 1 * + 6 C 3 ¯ ( ξ j − z 1 * ) 2 C j , 3 + C 1 ¯ + C 2 ¯ ξ j − z 1 * + C 3 ¯ ( ξ j − z 1 * ) 2 C j , 1 + C j , 2 z n * − ξ j + C j , 3 ( z n * − ξ j ) 2 − 1 ( ξ j − z 1 * ) C 1 ¯ + 2 C 2 ¯ ξ j − z 1 * + 3 C 3 ¯ ( ξ j − z 1 * ) 2 C j , 2 + C j , 3 z n * − ξ j ] − X n ,
  • H s = ∑ j = 1 2 N − e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) z s − 2 * − ξ j 2 ξ j − z 1 * [ 1 ξ j − z 1 * 2 C ¯ 1 + 3 C ¯ 2 ξ j − z 1 * + 6 C ¯ 3 ξ j − z 1 * 2 C j , 3 + C ¯ 1 + C ¯ 2 ξ j − z 1 * + C ¯ 3 ξ j − z 1 * 2 C j , 1 + 2 C j , 2 z s − 2 * − ξ j + 3 C j , 3 z s − 2 * − ξ j 2 − 1 ξ j − z 1 * C ¯ 1 + 2 C ¯ 2 ξ j − z 1 * + 3 C ¯ 3 ξ j − z 1 * 2 C j , 2 + 2 C j , 3 z s − 2 * − ξ j ] ,
  • H t = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z 1 * ) ) z t − 4 * − ξ j 3 ξ j − z 1 * [ 2 ξ j − z 1 * 2 C 1 ¯ + 3 C 2 ¯ ξ j − z 1 * + 6 C 3 ¯ ξ j − z 1 * 2 C j , 3 + C 1 ¯ + C 2 ¯ ξ j − z 1 * + C 3 ¯ ξ j − z 1 * 2 2 C j , 1 + 6 C j , 2 z t − 4 * − ξ j + 12 C j , 3 z t − 4 * − ξ j 2 − 1 ξ j − z 1 * C 1 ¯ + 2 C 2 ¯ ξ j − z 1 * + 3 C 3 ¯ ξ j − z 1 * 2 2 C j , 2 + 6 C j , 3 z t − 4 * − ξ j ] ,
  • K n = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) ( z n * − ξ j ) ( ξ j − z ^ 1 * ) [ 1 ( ξ j − z ^ 1 * ) 2 C ¯ ^ 1 + 3 C ¯ ^ 2 ξ j − z ^ 1 * + 6 C ¯ ^ 3 ( ξ j − z ^ 1 * ) 2 C j , 3 + C ¯ ^ 1 + C ¯ ^ 2 ξ j − z ^ 1 * + C ¯ ^ 3 ( ξ j − z ^ 1 * ) 2 C j , 1 + C j , 2 z n * − ξ j + C j , 3 ( z n * − ξ j ) 2 − 1 ( ξ j − z ^ 1 * ) C ¯ ^ 1 + 2 C ¯ ^ 2 * ξ j − z ^ 1 * + 3 C ¯ ^ 3 ( ξ j − z ^ 1 * ) 2 C j , 2 + C j , 3 z n * − ξ j ] − Y n ,
  • K s = ∑ j = 1 2 N − e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) z s − 2 * − ξ j 2 ξ j − z ^ 1 * [ 1 ξ j − z ^ 1 * 2 C ¯ ^ 1 + 3 C ¯ ^ 2 ξ j − z ^ 1 * + 6 C ¯ ^ 3 ξ j − z ^ 1 * 2 C j , 3 + C ¯ ^ 1 + C ¯ ^ 2 ξ j − z ^ 1 * + C ¯ ^ 3 ξ j − z ^ 1 * 2 C j , 1 + 2 C j , 2 z s − 2 * − ξ j + 3 C j , 3 z s − 2 * − ξ j 2 − 1 ξ j − z ^ 1 * C ¯ ^ 1 + 2 C ¯ ^ 2 ξ j − z ^ 1 * + 3 C ¯ ^ 3 ξ j − z ^ 1 * 2 C j , 2 + 2 C j , 3 z s − 2 * − ξ j ] ,
  • K t = ∑ j = 1 2 N e 2 i ( θ ( ξ j ) − θ ( z ^ 1 * ) ) z t − 4 * − ξ j 3 ξ j − z ^ 1 * [ 2 ξ j − z ^ 1 * 2 C ¯ ^ 1 + 3 C ¯ ^ 2 ξ j − z ^ 1 * + 6 C ¯ ^ 3 ξ j − z ^ 1 * 2 C j , 3 + C ¯ ^ 1 + C ¯ ^ 2 ξ j − z ^ 1 * + C ¯ ^ 3 ξ j − z ^ 1 * 2 2 C j , 1 + 6 C j , 2 z t − 4 * − ξ j + 12 C j , 3 z t − 4 * − ξ j 2 − 1 ξ j − z ^ 1 * C ¯ ^ 1 + 2 C ¯ ^ 2 ξ j − z ^ 1 * + 3 C ¯ ^ 3 ξ j − z ^ 1 * 2 2 C j , 2 + 6 C j , 3 z t − 4 * − ξ j ] ,
  • where n = 1 , 2 ; s = 3 , 4 ; t = 5 , 6 . Applying the elimination method to Equation (A2) yields
L m N ¯ 2 , 2 ( ξ 2 * ) + M m N ¯ 1 , 1 ( ξ 1 * ) + P m N ¯ 2 , 1 ( ξ 2 * ) + Q m N ¯ 1 , 0 ( ξ 1 * ) + R m N ¯ 2 , 0 ( ξ 2 * ) = S m , M q N ¯ 1 , 1 ( ξ 1 * ) + P q N ¯ 2 , 1 ( ξ 2 * ) + Q q N ¯ 1 , 0 ( ξ 1 * ) + R q N ¯ 2 , 0 ( ξ 2 * ) = S q , T l N ¯ 2 , 1 ( ξ 2 * ) + U l N ¯ 1 , 0 ( ξ 1 * ) + V l N ¯ 2 , 0 ( ξ 2 * ) = W l , U p N ¯ 1 , 0 ( ξ 1 * ) + V p N ¯ 2 , 0 ( ξ 2 * ) = W p , V r N ¯ 2 , 0 ( ξ 2 * ) = W r ,
where the coefficients L m , M m , P m , Q m , R m , S m , M q , P q , Q q , R q , S q , T l , U l , V l , W l , U p , V p , W p , V r , and W r are obtained through a sequential elimination process:
  • L m = E m + 1 − D m + 1 D 1 − 1 E 1 , M m = F m + 1 − D m + 1 D 1 − 1 F 1 , P m = G m + 1 − D m + 1 D 1 − 1 G 1 ,
  • Q m = H m + 1 − D m + 1 D 1 − 1 H 1 , R m = K m + 1 − D m + 1 D 1 − 1 K 1 , S m = − A m + 1 + D m + 1 D 1 − 1 A 1 ,
  • M q = M q − 4 − L q − 4 L 1 − 1 M 1 , P q = P q − 4 − L q − 4 L 1 − 1 P 1 , R q = R q − 4 − L q − 4 L 1 − 1 R 1 ,
  • Q q = Q q − 4 − L q − 4 L 1 − 1 Q 1 , S q = S q − 4 − L q − 4 L 1 − 1 S 1 , W l = S l + 6 − M l + 6 M 6 − 1 S 6 ,
  • U l = Q l + 6 − M l + 6 M 6 − 1 Q 6 , T l = P l + 6 − M l + 6 M 6 − 1 P 6 , V l = R l + 6 − M l + 6 M 6 − 1 R 6 ,
  • U p = U p − 2 − T p − 2 T 1 − 1 U 1 , V p = V p − 2 − T p − 2 T 1 − 1 V 1 , W p = W p − 2 − T p − 2 T 1 − 1 W 1 ,
  • V r = V r − 1 − U r − 1 U 4 − 1 V 4 , W r = W r − 1 − U r − 1 U 4 − 1 W 4 ,
  • ( m = 1 , 2 , 3 , 4 , 5 ; q = 6 , 7 , 8 , 9 ; l = 1 , 2 , 3 ; p = 4 , 5 ; r = 6 ). Solving the system (A3) yields the unknown functions:
N ¯ 1 , 0 u p z 1 * = U 4 − 1 W 4 − V 4 X 1 , N ¯ 1 , 1 u p z 1 * = M 6 − 1 S 6 − R 6 X 1 − Q 6 X 2 − P 6 X 3 , N ¯ 1 , 2 u p z 1 * = D 1 − 1 − A 1 − K 1 X 1 − H 1 X 2 − G 1 X 3 − F 1 X 4 − E 1 X 5 , N ¯ 2 , 0 u p z ^ 1 * = V 6 − 1 W 6 , N ¯ 2 , 1 u p z ^ 1 * = T 1 − 1 W 1 − V 1 X 1 − U 1 X 2 , N ¯ 2 , 2 u p z ^ 1 * = L 1 − 1 S 1 − R 1 X 1 − Q 1 X 2 − P 1 X 3 − M 1 X 4 .
Finally, substituting the solutions (A4) back into Equation (A1) provides the complete, explicit expression for the single triple-pole soliton potential Q ( x , t ) . While the fully expanded form is too lengthy to display here, the systematic derivation above fully elucidates the structure of the solution and provides a clear theoretical foundation for further analytical or numerical study.

Appendix B. Symmetry Relations for Norming Constants

In this appendix, we collect the explicit relations between norming constants at the symmetric points z ^ n = v k 0 2 / z n * and z ¯ ^ = v k 0 2 / z n and those at the original eigenvalues z n and z n * . The derivations follow from the symmetry transformations Equations (48) and (49) and are straightforward but lengthy. All equation numbers are prefixed with B.

Appendix B.1. Relations for the Rank-3 Case

We begin by introducing norming constants at the symmetric point z → v k 0 2 / z . In analogy with Equations (65) and (66), we define c ^ n , d ^ n , e ^ n via
ϕ ( z ^ n ) α ( z ^ n ) = ψ ( z ^ n ) c ^ n , ϕ ¯ ( z ^ n * ) α ¯ ( z ^ n * ) = ψ ¯ ( z ^ n * ) c ¯ ^ n ,
together with the higher-order relations
ϕ z ^ n α z ^ n ′ = ψ ′ z ^ n c ^ n + ψ z ^ n d ^ n , ϕ z ^ n α z ^ n ″ = ψ ″ z ^ n c ^ n + 2 ψ ′ z ^ n d ^ n + ψ z ^ n e ^ n ,
and analogous formulas for the conjugates.
Using the symmetry (48) and the relations between the adjugate matrices obtained from Equation (49), we have
α ( z n ) = v k 0 2 cof ( R − ) α ¯ ( z ^ n * ) cof ( Q + ) , α ¯ ( z n * ) = v k 0 2 cof ( Q − ) α ( z ^ n ) cof ( R + ) , α ( z ^ n ) = v k 0 2 cof ( R − ) α ¯ ( z n * ) cof ( Q + ) , α ¯ ( z ^ n * ) = v k 0 2 cof ( Q − ) α ( z ^ n ) cof ( R + ) ,
where cof ( Q ± ) and cof ( R ± ) denote the adjugate matrices of Q ± and R ± , respectively. Now we express ϕ ( z n ) α ( z n ) , in two different ways. On one hand, using Equations (48) and (A5),
ϕ z n α ( z n ) = i z n ϕ ¯ ( z ^ n * ) R − α z n = i v z n k 0 2 ϕ ¯ ( z ^ n * ) R − cof ( R − ) α ¯ ( z ^ n * ) cof ( Q + ) .
Applying Equation (A7) to replace α ( z ) and noting that R − cof ( R − ) = det R − I 2 , we obtain
ϕ ( z n ) α ( z n ) = i v det R − k 0 2 z n ψ ¯ ( z ^ n * ) c ¯ ^ n cof ( Q + ) .
On the other hand, from Equations (48) and (65),
ϕ ( z n ) α ( z n ) = ψ ( z n ) c n = − i z n ψ ¯ ( z ^ n * ) Q + c n .
Comparing Equations (A9) and (A10) yields
c ¯ ^ n = − v k 0 2 det Q + det R − Q + c n Q + .
Similarly, by Equations (48), (A5) and (A7), we can obtain
c ^ n = − v k 0 2 det Q − det R + R + c ¯ n R + .
Following the same procedure and using the differentiated relations (A6) together with (66), we derive
d ¯ ^ n = − v k 0 2 det Q + det R − Q + d n Q + , d ^ n = − v k 0 2 det Q − det R + R + d ¯ n R + , e ¯ ^ n = − v k 0 2 det Q + det R − Q + e n Q + , e ^ n = − v k 0 2 det Q − det R + R + e ¯ n R + .
Next, we need the relations between the determinants of the scattering matrices and their derivatives. By Equations (49) and (A7), we have
det a ( z ^ n ) = det Q + det R − k 0 4 det a ¯ ( z n * ) , det a ¯ z ^ n * = det Q − det R + k 0 4 det a z n .
Differentiating these identities repeatedly with respect to z and evaluating at the relevant points yield the following connections:
( det a ) ‴ ( z ^ n ) = − v ( z n * ) 6 k 0 10 det Q + det R − ( det a ¯ ) ‴ ( z n * ) , ( det a ¯ ) ‴ ( z ^ n * ) = − v ( z n ) 6 k 0 10 det Q − det R + ( det a ) ‴ ( z n ) ,
( det a ) ( 4 ) ( z ^ n ) = 12 ( z n * ) 7 k 0 12 det Q + det R − ( det a ¯ ) ‴ ( z n * ) + ( z n * ) 8 k 0 12 det Q + det R − ( det a ¯ ) ( 4 ) ( z n * ) , ( det a ¯ ) ( 4 ) ( z ^ n * ) = 12 ( z n ) 7 k 0 12 det Q − det R + ( det a ) ‴ ( z n ) + ( z n ) 8 k 0 12 det Q − det R + ( det a ) ( 4 ) ( z n ) ,
and
( det a ) ( 5 ) ( z ^ n ) = [ − v z 10 k 0 14 det Q + det R − ( det a ¯ ) ( 5 ) ( z ) − 20 v z 9 k 0 14 det Q + det R − ( det a ¯ ) ( 4 ) ( z ) − 120 v z 8 k 0 14 det Q + det R − ( det a ¯ ) ‴ ( z ) ] z = z n * , ( det a ¯ ) ( 5 ) ( z ^ n * ) = [ − v z 10 k 0 14 det Q − det R + ( det a ) ( 5 ) ( z ) − 20 v z 9 k 0 14 det Q − det R + ( det a ) ( 4 ) ( z ) − 120 v z 8 k 0 14 det Q − det R + ( det a ) ‴ ( z ) ] z = z n .
By Equation (80), we finally obtain the following symmetry relations for A ^ n and A ¯ ^ n :
A ^ n = − 6 v k 0 2 R + c ¯ n R + k 0 10 − v ( z n * ) 6 det Q − det R + det Q + det R − ( det a ¯ ) ‴ ( z n * ) = 1 ( z n * ) 2 R + A ¯ n R + , A ¯ ^ n = − 6 v k 0 2 Q + c n Q + k 0 10 − v ( z n ) 6 det Q − det R + det Q + det R − ( det a ¯ ) ‴ ( z n ) = 1 ( z n ) 2 Q + A n Q + ,
noting that det Q ± det R ± = k 0 4 . It follows similarly that
B ^ n = 6 k 0 10 v z 6 det Q + det R − ( det a ¯ ) ‴ ( z ) [ R + c ¯ n R + [ 12 z 7 ( det a ¯ ) ‴ ( z ) + z 8 ( det a ¯ ) ( 4 ) ( z ) ] 4 z 6 det Q − det R + ( det a ¯ ) ‴ ( z ) + v k 0 2 R + d ¯ n R + det Q − det R + ] z = z n * = 1 ( z n * ) 2 R + B ¯ n R + − 3 ( z n * ) 3 R + A ¯ n R + , B ¯ ^ n = 6 k 0 10 v z 6 det Q + det R − ( det a ¯ ) ‴ ( z ) [ Q + c n Q + [ 12 z 7 ( det a ¯ ) ‴ ( z ) + z 8 ( det a ¯ ) ( 4 ) ( z ) ] 4 z 6 det Q − det R + ( det a ¯ ) ‴ ( z ) + v k 0 2 Q + d n Q + det Q − det R + ] z = z n = 1 ( z n ) 2 Q + B n Q + − 3 ( z n ) 3 Q + A n Q + ,
and
C ^ n = ( ( det a ) ( 4 ) ( z ^ n ) ) 2 16 ( ( det a ) ‴ ( z ^ n ) ) 2 − d ^ n c ^ n − 1 ( det a ) ( 4 ) ( z ^ n ) 4 ( det a ) ‴ ( z ^ n ) − ( det a ) ( 5 ) ( z ^ n ) 20 ( det a ) ‴ ( z ^ n ) + e ^ n c ^ n − 1 2 6 ( det a ) ‴ ( z ^ n ) = 1 ( z n * ) 2 R + C ¯ n R + − 2 ( z n * ) 3 R + B ¯ n R + + 3 ( z n * ) 4 R + A ¯ n R + , C ¯ ^ n = ( ( det a ¯ ) ( 4 ) ( z ^ n * ) ) 2 16 ( ( det a ¯ ) ‴ ( z ^ n * ) ) 2 − d ¯ ^ n c ¯ ^ n − 1 ( det a ¯ ) ( 4 ) ( z ^ n * ) 4 ( det a ¯ ) ‴ ( z ^ n * ) − ( det a ¯ ) ( 5 ) ( z ^ n * ) 20 ( det a ¯ ) ‴ ( z ^ n * ) + e ¯ ^ n c ¯ ^ n − 1 2 6 ( det a ¯ ) ‴ ( z ^ n * ) = 1 ( z n ) 2 Q + C n Q + − 2 ( z n ) 3 Q + B n Q + + 3 ( z n ) 4 Q + A n Q + .
Substituting the above equations into Equation (80), one has
C ^ n , 1 = 1 ( z n * ) 2 R + C ¯ n , 1 R + − 2 ( z n * ) 3 R + ( C ¯ n , 2 − i θ ′ ( z n * ) C ¯ n , 3 ) R + + 3 ( z n * ) 4 R + C ¯ n , 3 R + , C ^ n , 2 = 1 ( z n * ) 2 R + C ¯ n , 2 R + − 3 ( z n * ) 3 R + C ¯ n , 3 R + , C ^ n , 3 = 1 ( z n * ) 2 R + C ¯ n , 3 R + .

Appendix B.2. Relations for the Rank-2 Case

We now perform an analogous analysis for the case rank   P = 2 . At the symmetric points we introduce c ^ n , d ^ n , e ^ n via
ϕ ( x , t , z ^ n ) = ψ ( x , t , z ^ n ) b ^ n , ϕ ¯ ( x , t , z ^ n * ) = ψ ¯ ( x , t , z ^ n * ) b ¯ ^ n ,
and the corresponding higher-order relations
ϕ ′ z ^ n = ψ ′ z ^ n b ^ n + ψ z ^ n d ^ n , ϕ ″ z ^ n = ψ ″ z ^ n b ^ n + 2 ψ ′ z ^ n d ^ n + ψ z ^ n e ^ n .
Using the symmetry (48) together with (A22), we can relate ϕ ( z n ) and ψ ( z n ) to quantities at the symmetric points:
ϕ ( x , t , z n ) = i z n ϕ ¯ ( x , t , z ^ n * ) R − = i z n ψ ¯ ( x , t , z ^ n * ) b ¯ ^ n R − .
On the other hand, from Equation (82),
ϕ ( x , t , z n ) = ψ ( x , t , z n ) b n = − i z n ψ ¯ ( x , t , z ^ n * ) Q + b n .
By comparing these two results, we obtain
b ¯ ^ n = − v k 0 2 Q + b n Q − .
Similarly, by Equations (48), (82), and (A22), we have
b ^ n = − v k 0 2 R + b ¯ n R − .
From Equation (82), it follows that
ϕ ′ ( z n ) = − i ( z n ) 2 ψ ¯ ( z ^ n * ) b ¯ ^ n R − + i z n − v k 0 2 ( z n ) 2 ψ ¯ ′ ( z ^ n * ) b ¯ ^ n + ψ ¯ ( z ^ n * ) d ¯ ^ n R − = i ( z n ) 2 ψ ¯ ( z ^ n * ) Q + b n − i z n ψ ¯ ′ ( z ^ n * ) v k 0 2 ( z n ) 2 Q + b n − i z n ψ ¯ ( z ^ n * ) Q + d n ,
and
ϕ ″ ( z n ) = 2 i ( z n ) 3 ψ ¯ ( z ^ n * ) b ¯ ^ n R − − 2 i ( z n ) 2 − v k 0 2 ( z n ) 2 ψ ¯ ′ ( z ^ n * ) b ¯ ^ n + ψ ¯ ( z ^ n * ) d ¯ ^ n R − + i z n ( 2 ψ ¯ ′ ( z ^ n * ) d ¯ ^ n + ψ ¯ ″ ( z ^ n * ) b ¯ ^ n + ψ ¯ ( z ^ n * ) e ¯ ^ n ) R − = 2 i ( z n ) 2 ψ ¯ ( z ^ n * ) Q + d n − 2 i z n ψ ¯ ′ ( z ^ n * ) v k 0 2 ( z n ) 2 Q + d n − i z n ψ ¯ ( z ^ n * ) Q + e n + − 2 i ( z n ) 3 ψ ¯ ( z ^ n * ) + 2 i ( z n ) 2 ψ ¯ ′ ( z ^ n * ) − i z n ψ ¯ ″ ( z ^ n * ) Q + b n .
From the above equations, we obtain that
d ¯ ^ n = − v k 0 2 Q + d n Q − , d ^ n = − v k 0 2 R + d ¯ n R − , e ¯ ^ n = − v k 0 2 Q + e n Q − , e ^ n = − v k 0 2 R + e ¯ n R − .
By Equation (A17), we derive
( det a ) ( 6 ) ( z ^ n ) = [ 1300 z 9 k 0 16 det Q + det R − ( det a ¯ ) ‴ ( z ) + 300 z 10 k 0 16 det Q + det R − ( det a ¯ ) ( 4 ) ( z ) + 30 z 11 k 0 16 det Q + det R − ( det a ¯ ) ( 5 ) ( z ) + z 12 k 0 16 det Q + det R − ( det a ¯ ) ( 6 ) ( z ) ] z = z n * , ( det a ¯ ) ( 5 ) ( z ^ n * ) = [ 1300 z 9 k 0 16 det Q − det R + ( det a ) ‴ ( z ) + 300 z 10 k 0 16 det Q − det R + ( det a ) ( 4 ) ( z ) + 30 z 11 k 0 16 det Q − det R + ( det a ) ( 5 ) ( z ) + z 12 k 0 16 det Q − det R + ( det a ) ( 6 ) ( z ) ] z = z n .
Differentiating Equation (A7) with respect to z gives
α ′ ( z ^ n ) = − ( z n * ) 2 k 0 4 cof ( R − ) α ¯ ′ ( z n * ) cof ( Q + ) , α ″ ( z ^ n ) = 2 ( z n * ) 3 v k 0 6 cof ( R − ) α ¯ ′ ( z n * ) cof ( Q + ) + ( z n * ) 4 v k 0 6 cof ( R − ) α ¯ ″ ( z n * ) cof ( Q + ) , α ‴ ( z ^ n ) = − 6 ( z n * ) 4 k 0 8 cof ( R − ) α ¯ ′ ( z n * ) cof ( Q + ) − 6 ( z n * ) 5 k 0 8 cof ( R − ) α ¯ ″ ( z n * ) cof ( Q + ) − ( z n * ) 6 k 0 8 cof ( R − ) α ¯ ‴ ( z n * ) cof ( Q + ) .
Using the definitions in Equation (94) and the above derivations, we conclude that
A ^ n = R + A ¯ n R + ( z n * ) 2 , B ^ n = B ¯ n − 4 z n * , C ^ n = R + C ¯ n R + ( z n * ) 2 + R + A ¯ n R + ( z n * ) 3 , D ^ n = D ¯ n − 10 ( z n * ) 2 − ( det a ¯ ) ( 5 ) ( z n * ) z n * ( det a ¯ ) ( 4 ) ( z n * ) , E ^ n = R + E ¯ n R + ( z n * ) 2 + 2 R + C ¯ n R + ( z n * ) 3 + R + A ¯ n R + ( z n * ) 4 .
Substituting the above expressions into Equation (95) yields the symmetry of the norming constant:
C ^ n , 1 = 1 ( z n * ) 2 R + C ¯ n , 1 R + − 2 ( z n * ) 3 R + ( C ¯ n , 2 − i θ ′ ( z n * ) C ¯ n , 3 ) R + + 3 ( z n * ) 4 R + C ¯ n , 3 R + , C ^ n , 2 = 1 ( z n * ) 2 R + C ¯ n , 2 R + − 3 ( z n * ) 3 R + C ¯ n , 3 R + , C ^ n , 3 = 1 ( z n * ) 2 R + C ¯ n , 3 R + .

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