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Article

Applications of Haar Wavelet-Finite Difference Hybrid Method and Its Convergence for Hyperbolic Nonlinear Schrödinger Equation with Energy and Mass Conversion

1
Department of Mathematics, Hanshan Normal University, Chaozhou 515041, China
2
Department of Mathematics, University of Swabi, Swabi 23200, Pakistan
3
Department of Basic Sciences, University of Engineering and Technology Peshawar, Peshawar 25000, Pakistan
4
Department of Mathematics and Statistics, Macquarie University, Sydney, NSW 2109, Australia
5
Department of Mathematics, FATA University, Darra Adam Khel 26100, Pakistan
6
Department of Computer Engineering, Biruni University, Istanbul 34025, Turkey
7
Section of Mathematics, International Telematic University Uninettuno, Corso Vittorio Emanuele II, 39, 00186 Roma, Italy
*
Author to whom correspondence should be addressed.
Submission received: 4 October 2021 / Revised: 4 November 2021 / Accepted: 11 November 2021 / Published: 23 November 2021
(This article belongs to the Special Issue Recent Advances in Solar Energy Collectors: Models and Applications)

Abstract

:
This article is concerned with the numerical solution of nonlinear hyperbolic Schr o ¨ dinger equations (NHSEs) via an efficient Haar wavelet collocation method (HWCM). The time derivative is approximated in the governing equations by the central difference scheme, while the space derivatives are replaced by finite Haar series, which transform it to full algebraic form. The experimental rate of convergence follows the theoretical statements of convergence and the conservation laws of energy and mass are also presented, which strengthens the proposed method to be convergent and conservative. The Haar wavelets based on numerical results for solitary wave shape of | φ | are discussed in detail. The proposed approach provides a fast convergent approximation to the NHSEs. The reliability and efficiency of the method are illustrated by computing the maximum error norm and the experimental rate of convergence for different problems. Comparisons are performed with various existing methods in recent literature and better performance of the proposed method is shown in various tables and figures.

1. Introduction

The nonlinear hyperbolic Schr o ¨ dinger equation govern most scientific and physical processes, and they play an essential role in nonlinear optics, Biomolecular dynamics, plasma physics, and water waves. Because finding the exact solution to these types of NHSEs is difficult due to the nonlinear term, numerical methods are an alternative method of determining their solution. In this paper, we considered the following NHSEs [1]
2 φ τ 2 2 φ s 2 + μ 1 2 φ τ s i μ 2 φ τ i μ 3 φ s + μ 4 φ + μ 5 | φ | 2 φ = 0 , a s b , 0 τ T ,
with the initial and boundary conditions
φ ( s , 0 ) = I 1 ( s ) , φ ( s , 0 ) τ = I 2 ( s )
φ ( a , τ ) = B 1 ( τ ) , φ ( b , τ ) = B 2 ( τ ) .
In the above equations I 1 , I 2 , B 1 , and B 2 are known functions, i 2 = 1 and φ is the only unknown complex function, which is to be determined. The above NHSEs (1) have a lot of application in physics, such as Langmuir wave packet estimation in plasma physics [2], modeling of planar light bullets [3] and non-relativistic limit of the Klein-Gordon equation [4]. The two important properties of Equations (1)–(3) are the energy and mass conservation. The NHSEs (1)–(3) preserve the following expressions for total energy and total mass, which have been proved in [1]:
  • Energy invariant
    E ( τ ) : = a b φ τ 2 + φ s 2 + i μ 3 φ φ s ¯ + μ 4 φ 2 + μ 5 2 φ 4 d s = E ( 0 ) .
  • Mass invariant
    Q ( τ ) : = a b φ τ φ ¯ φ τ ¯ φ μ 1 φ φ s ¯ i μ 2 | φ | 2 d s = Q ( 0 ) .
Due to the above mentioned applications, different numerical techniques have been developed to solve the important NHSEs. These numerical technique are finite difference method [5,6,7,8,9], spline collocation methods [10] Galerkin method [11], Fourier pseudospectral method [12] and Multi-symplectic integrator [1]. The nonconservative scheme [5] may not handle the nonlinear blow up phenomena easily and the conservative schemes are presented to minimize these issues [7,9]. Some recent contributions are also reported in [13,14,15].
Recently, the research has been focused on the Haar wavelet application in the investigation and analysis of different problems in applied sciences. The different algorithms, based on weak and strong formulations, are the meshless wavelet method [16], the Daubechies wavelet-based method [17], the wavelet Galerkin method [18], and the wavelet collocation methods [19,20].A thorough introduction of the wavelets schemes for partial differential equations (PDEs) is given in [21]. Different scientific and engineering phenomena have been represented in the forms of ordinary differential equations (ODEs), integro-differential equations, and PDEs, which have been solved by Haar wavelets in the references [22,23,24,25,26,27,28,29,30,31,32,33,34,35,36,37]. A further development of the Haar wavelet is related to the solution of challenging fractional differential and integral equations [38,39,40,41,42]. The latest contribution on Haar wavelets is presented in [43] for the identification of software piracy.
The Haar wavelets have been used as an innovative and excellent mathematical tool for signal processing in physics and communication research [44] as well as in digital image/video processing and compression [45,46]. The Haar wavelet, like the finite difference approach, may convert PDEs into an algebraic system of equations, resulting in a well-conditioned number for the resulting system. This is the beauty of Haar wavelet in dealing with ill-conditioned problems in this way.
Haar wavelets based algorithms have also been reported to solve hyperbolic type PDEs. In [47], a linear hyperbolic PDE has been solved with Haar wavelet operational matrix method. In [48], the Haar wavelets were used to approximate the term 3 φ ( s , τ ) τ s 2 in order to get the numerical solution in the unit interval [ 0 , 1 ] using a transformation that converted the governing equation into system of PDEs. A Haar wavelet-finite difference hybrid method has been applied to the nonlinear parabolic Schr o ¨ dinger equations in [20,49,50].
In this paper, the potential of the Haar wavelet is further applied to the NHSEs along with the theoretical convergence, which is supported by our numerical results in the interval [ a , b ] . Finite-difference and Haar wavelets are used to discretize the time and space derivatives, respectively. Because the Haar functions are discontinuous, the approximation begins with the highest order derivatives in the model equation. The unknown solution can be found by integrating the series further. A system of algebraic equations can be easily solved by introducing these approximations in Equation (1). The next sections go into the details of the suggested method.
The paper is composed as follows. Section 2 is focused on the definitions of the Haar functions and their integrals. Section 3 presents the suggested numerical scheme. In Section 4, the convergence analysis is discussed. In Section 5, numerical findings are highlighted in details and in the last section, the concluding remarks are drawn.

2. Haar Functions

A generalized representation of the Haar functions is defined as
h i ( s ) = 1 for s [ ζ 1 ( i ) , ζ 2 ( i ) ) , 1 for s [ ζ 2 ( i ) , ζ 3 ( i ) ) , 0 elsewhere ,
where
ζ 1 ( i ) = a + ( b a ) k m , ζ 2 ( i ) = a + ( b a ) ( k + 0.5 ) m , ζ 3 ( i ) = a + ( b a ) ( k + 1 ) m .
Here m = 2 j , j = 0 , 1 , , represents the level of the wavelet, k = 0 , 1 , , m 1 is the translation parameter, and i = m + k + 1 . We note that i 2 . We define
h 1 ( s ) = 1 for s [ a , b ] , 0 elsewhere ,
which is also known as the mother wavelet. Due to the numerical estimation, we acknowledge a maximum estimation J of the entity j that expresses the level of the Haar wavelet in the earlier definition and J is then called the supreme level of resolution. We also introduced the integer M = 2 J . To keep the derivations simple, we intend to introduce some notations for the following integrals for i = 2 , 3 , 4 ,
p i , 1 ( s ) = a s h i ( s ) d s = 0 for s < ζ 1 ( i ) , s ζ 1 ( i ) for s [ ζ 1 ( i ) , ζ 2 ( i ) ) , s ζ 1 ( i ) 2 ( s ζ 2 ( i ) ) for s [ ζ 2 ( i ) , ζ 3 ( i ) ) , s ζ 1 ( i ) 2 ( s ζ 2 ( i ) ) + ( s ζ 3 ( i ) ) for s ζ 3 ( i ) ,
p i , 2 ( s ) = a s p i , 1 ( s ) d s = 0 for s < ζ 1 ( i ) , 1 2 ( s ζ 1 ( i ) ) 2 for s [ ζ 1 ( i ) , ζ 2 ( i ) ) , 1 2 [ ( s ζ 1 ( i ) ) 2 2 ( s ζ 2 ( i ) ) 2 ] for s [ ζ 2 ( i ) , ζ 3 ( i ) ) , 1 2 [ ( s ζ 1 ( i ) ) 2 2 ( s ζ 2 ( i ) ) 2 + ( s ζ 3 ( i ) ) 2 ] for s ζ 3 ( i ) ,
and
C = a b p i , 1 ( s ) d s = ( b a ) 2 4 m 2 = b a 2 j + 1 2 .
As p i , 1 ( s ) is increasing in the interval [ ζ 1 ( i ) , ζ 2 ( i ) ) and decreasing in the interval [ ζ 2 ( i ) , ζ 3 ( i ) ) but the maximum value is at ζ 2 ( i ) . Hence
max s ( p i , 1 ( s ) ) = p i , 1 ( ζ 2 ( i ) ) = b a 2 m = b a 2 j + 1 .
It is worth noting that the following formula has been validated in [51]
max s ( p i , 2 ( s ) ) = ( b a ) 2 4 m 2 = b a 2 j + 1 2 .

3. Haar Approximation

In this section, we consider Haar wavelets as a basic part of our numerical technique for spatial discretization. In order to construct the HWCM proposed in this paper, we consider the following form of Equation (1) [10]
2 φ τ 2 2 φ s 2 + i φ τ + λ | φ | 2 φ = 0 ,
where λ is constant. Due to discontinuity of the Haar functions, we start approximating the second order derivative with respect to s in Equation (10) by Haar functions as
2 φ ( s , τ ) s 2 = i = 1 λ i ( τ ) h i ( s ) .
Integrating Equation (11) w.r.t s, from a to s,
φ ( s , τ ) s = φ ( a , τ ) s + i = 1 λ i ( τ ) p i , 1 ( s ) .
Integrating Equation (12) w.r.t s, from a to b,
φ ( a , τ ) s = φ ( b , τ ) φ ( a , τ ) b a i = 1 λ i ( τ ) C b a ,
where C is given by Equation (7). By Equations (12) and (13), we obtain
φ ( s , τ ) s = w ¯ 0 ( τ ) + i = 1 λ i ( τ ) h ¯ i ( s ) ,
where w ¯ 0 ( τ ) = φ ( b , τ ) φ ( a , τ ) b a and h ¯ i ( s ) = p i , 1 ( s ) C b a . Again, by partially integrating Equation (14) w.r.t s, from a to s, we get
φ ( s , τ ) = w ˜ 0 ( s , τ ) + i = 1 λ i ( τ ) h ˜ i ( s ) ,
where w ˜ 0 ( s , τ ) = φ ( a , τ ) + ( s a ) w ¯ 0 ( τ ) , and h ˜ i ( s ) = ( p i , 2 ( s ) ( s a ) C b a .
If τ n 1 is the current time level, τ n and τ n + 1 is the consecutive next time levels, then using central difference approximation for time derivatives and introducing the following linearized θ -weighted scheme to Equation (10), we get
φ ( s , τ n + 1 ) 2 φ ( s , τ n ) + φ ( s , τ n 1 ) Δ τ 2 θ 2 φ ( s , τ n + 1 ) s 2 ( 1 θ ) 2 φ ( s , τ n ) s 2 + i φ ( s , τ n + 1 ) φ ( s , τ n 1 ) 2 Δ τ + λ | φ ( s , τ n ) | 2 φ ( s , τ n + 1 ) + φ ( s , τ n 1 ) 2 + O ( Δ τ 2 ) = 0 .
Using θ = 1 in Equation (17), we get the well known implicit method to the NHSE
φ ( s , τ n + 1 ) 2 φ ( s , τ n ) + φ ( s , τ n 1 ) Δ τ 2 2 φ ( s , τ n + 1 ) s 2 + i φ ( s , τ n + 1 ) φ ( s , τ n 1 ) 2 Δ τ + λ | φ ( s , τ n ) | 2 φ ( s , τ n + 1 ) + φ ( s , τ n 1 ) 2 + O ( Δ τ 2 ) = 0 .
To find the numerical solution based on the sum of finite Haar wavelet, we define
φ M ( s , τ ) = w ˜ 0 ( s , τ ) + i = 1 2 M λ i ( τ ) h ˜ i ( s ) .
Similarly, by intercepting the finite terms of Equations (11) and (14), we get
φ M ( s , τ ) s = w ¯ 0 ( τ ) + i = 1 2 M λ i ( τ ) h ¯ i ( s ) , 2 φ M ( s , τ ) s 2 = i = 1 2 M λ i ( τ ) h i ( s ) .
The relationship between exact and approximate representations are
φ ( s , τ ) = φ M ( s , τ ) + E M ( s , τ ) , where E M ( s , τ ) = i = 2 M + 1 λ i ( τ ) h ˜ i ( s ) , φ ( s , τ ) s = φ M ( s , τ ) s + E M ( s , τ ) s , where E M ( s , τ ) s = i = 2 M + 1 λ i ( τ ) h ¯ i ( s ) ,
and
2 φ ( s , τ ) s 2 = 2 φ M ( s , τ ) s 2 + 2 E M ( s , τ ) s 2 , where 2 E M ( s , τ ) s 2 = i = 2 M + 1 λ i ( τ ) h i ( s ) .
The exact form of Equation (18) employing the Haar wavelet is now as follows
φ ( s , τ n + 1 ) 2 φ ( s , τ n ) + φ ( s , τ n 1 ) Δ τ 2 2 φ ( s , τ n + 1 ) s 2 + i φ ( s , τ n + 1 ) φ ( s , τ n 1 ) 2 Δ τ + λ | φ ( s , τ n ) | 2 φ ( s , τ n + 1 ) + φ ( s , τ n 1 ) 2 = E M H ( s , τ ) + O ( Δ τ 2 ) ,
where E M H ( s , τ ) is the Haar wavelet truncation error term, which is defined as
E M H ( s , τ ) = E M ( s , τ n + 1 ) 2 E M ( s , τ n ) + E M ( s , τ n 1 ) Δ τ 2 + 2 E M ( s , τ n + 1 ) s 2 i E M ( s , τ n + 1 ) E M ( s , τ n 1 ) 2 Δ τ λ | E M ( s , τ n ) | 2 E M ( s , τ n + 1 ) + E M ( s , τ n 1 ) 2 .
Dropping all the error terms E M H ( s , τ ) + O ( Δ τ 2 ) and using the collocation points s l = a + ( b a ) ( l 0.5 ) 2 M , l = 1 , 2 , , 2 M , we have
φ ( s l , τ n + 1 ) 2 φ ( s l , τ n ) + φ ( s l , τ n 1 ) Δ τ 2 2 φ ( s l , τ n + 1 ) s 2 + i φ ( s l , τ n + 1 ) φ ( s l , τ n 1 ) 2 Δ τ + λ | φ ( s l , τ n ) | 2 φ ( s l , τ n + 1 ) + φ ( s l , τ n 1 ) 2 = 0 .
Now defining
φ ˜ M , l n : = w ˜ 0 ( s l , τ n ) + i = 1 2 M λ i M , n h ˜ i ( s l ) , φ ˜ M , l n s : = w ¯ 0 ( τ n ) + i = 1 2 M λ i M , n h ¯ i ( s l ) , 2 φ ˜ M , l n s 2 : = i = 1 2 M λ i M , n h i ( s l ) ,
we get
φ ˜ M , l n + 1 2 φ ˜ M , l n + φ ˜ M , l n 1 Δ τ 2 2 φ ˜ M , l n + 1 s 2 + i φ ˜ M , l n + 1 φ ˜ M , l n 1 2 Δ τ + λ φ ˜ M , l n 2 φ ˜ M , l n + 1 + φ ˜ M , l n 1 2 = 0 .
Putting Equation (24) in Equation (25), we get a system of 2 M equations with 2 M unknowns, which can be easily solved for λ i ’s i.e.,
λ i M , n + 1 1 + i Δ τ 2 + λ Δ τ 2 2 φ ˜ M , l n 2 h ˜ i ( s l ) Δ τ 2 h i ( s l ) = 2 φ ˜ M , l n + i Δ τ 2 λ Δ τ 2 2 φ ˜ M , l n 2 1 φ ˜ M , l 1 + i Δ τ 2 + λ Δ τ 2 2 φ ˜ M , l n 2 w ˜ 0 ( s l , τ n ) .
By using λ i ’s in Equation (24), it is possible to obtain the desired numerical solution. To interpolate the solution at any point s, we define the formula below
φ ˜ M n + 1 ( s ) : = w ˜ 0 ( s , τ n + 1 ) + i = 1 2 M λ i M , n + 1 h ˜ i ( s ) ,
then φ ˜ M n + 1 ( s ) φ ( s , τ n + 1 ) .

4. Convergence Analysis

This section is dedicated to the rate of convergence when φ ( s , τ P ) is approximated by the numerical method described in Section 3. Let 0 = τ 0 < τ 1 < τ P = T be the partitioned of [ 0 , T ] and P denotes a positive integer.
Theorem 1.
“Assume that φ τ , 2 φ τ 2 , φ s , 2 φ s 2 , 3 φ s 3 exist and are bounded in [ a , b ] × [ 0 , T ] . For any M = 2 J , J = 0 , 1 , 2 , , and p = 0 , 1 , P , where P is a positive integer, if φ ˜ M p ( s ) is the Haar wavelet solution and φ ( s , τ p ) is the exact solution then
max 0 p P φ ( . , τ p ) φ ˜ M p L ( a , b ) O 1 M 2 + O ( Δ τ 2 ) , as J and P ,
where Δ τ = max 0 p P 1 ( τ p + 1 τ p ) and L ( a , b ) represents the infinity-norm in the interval (a,b)”.
Proof. 
For p = 1 , 2 , , P we have
φ ( . , τ p ) φ ˜ M p L ( a , b ) E M L ( a , b ) + φ M ( . , τ p ) φ ˜ M p L ( a , b ) ,
where E M L ( a , b ) is defined as
E M L ( a , b ) : = φ ( . , τ p ) φ M ( . , τ p ) L ( a , b ) = max s i = 2 M + 1 λ i h ˜ i ( s ) .
It is shown in ([51] Equation (18)) that λ i β / 2 j + 1 . In fact, it can be shown that | λ i | β / 2 j + 1 (which should also have been required in [51]). Therefore
E M L ( a , b ) β i = 2 M + 1 1 2 j + 1 max s h ˜ i ( s ) .
By using successively Equation (16), the triangle inequality, Equations (7) and (9), we obtain
E M L ( a , b ) β i = 2 M + 1 1 2 j + 1 max s ( p i , 2 ( s ) | + max s | ( s a ) C b a 2 β ( b a ) 2 i = 2 M + 1 1 2 j + 1 3 2 β ( b a ) 2 j = J + 1 k = 0 2 j 1 1 2 j + 1 3 = β ( b a ) 2 j = J + 1 1 2 j + 1 2 β ( b a ) 2 3 1 2 J + 1 2 = O 1 M 2 .
The second part φ M ( . , τ p ) φ ˜ M p L ( a , b ) is the error due to the time iteration where we used central difference approximation, which is second order accurate in time, i.e., φ M ( . , τ p ) φ ˜ M p O ( Δ τ 2 ) . □

5. Test Cases

The HWCM is implemented by computing the results of various numerical test problems. We employed the second-order central difference for time discretization, and we generally want to expose the effect of spatial discretization by our results. The maximum error norms have been used for accuracy measurements, which are defined as;
E = max 1 l 2 M | φ ( s l , τ P ) φ ˜ M , l P | , E R e = max 1 l 2 M | Re ( φ ( s l , τ P ) ) Re ( φ ˜ M , l P ) | , E I m = max 1 l 2 M | Im ( φ ( s l , τ P ) ) Im ( φ ˜ M , l P ) | .
The important property in solving the NHSEs are the discrete conservation laws. To verify the HWCM we have calculated Equations (4) and (5) in the following way
E ( τ ) : = a b φ τ 2 + φ s 2 + i μ 3 φ φ s ¯ + μ 4 φ 2 + μ 5 2 φ 4 d s 1 2 M i = 0 2 M ( D ( s i ) 2 + φ ˜ M n + 1 ( s i ) s 2 + i μ 3 φ ˜ M n + 1 ( s i ) φ ˜ M n + 1 ( s i ) s ¯ + μ 4 φ ˜ M n + 1 ( s i ) 2 + μ 5 2 φ ˜ M n + 1 ( s i ) 4 ) , Q ( τ ) : = a b φ τ φ ¯ φ τ ¯ φ μ 1 φ φ s ¯ i μ 2 | φ | 2 d s 1 2 M i = 0 2 M [ D ( s i ) φ ˜ M n + 1 ( s i ) ¯ D ( s i ) ¯ φ ˜ M n + 1 ( s i ) μ 1 φ ˜ M n + 1 ( s i ) φ ˜ M n + 1 ( s i ) s ¯ i μ 2 | φ ˜ M n + 1 ( s i ) | 2 ] ,
where D ( s i ) = φ ˜ M n + 1 ( s i ) φ ˜ M n 1 ( s i ) 2 Δ τ .
Problem 1.
We consider the following linear form of Equation (1)
2 φ τ 2 2 φ s 2 + i φ τ + φ = 0 , 0 s 2 π , 0 τ T .
with the initial conditions
φ ( s , 0 ) = e i s , φ ( s , 0 ) τ = i e i s
and boundary conditions
φ ( 0 , τ ) = e i τ , φ ( 2 π , τ ) = e i ( 2 π + τ ) .
The exact solution is φ ( s , τ ) = e i ( s + τ ) .
The aim of presenting this linear case is to check and evaluate the accuracy, efficiency and the performance of this proposed Haar wavelet conservative scheme. In Table 1, to check the spatial convergence of the HWCM, we set Δ τ = 0.0001 for various values of M. It was discovered that the theoretical and experimental rates of convergence for the space variable are in good agreement, and the CUP times demonstrate the program’s efficiency and speed of calculation.
Problem 2.
We consider the following nonlinear type of Equation (1) [11]
2 φ τ 2 2 φ s 2 + i φ τ 2 | φ | 2 φ = 0 , 50 s 50 , 0 τ T .
The exact solution is
φ ( s , τ ) = A sech ( K s ) e i Θ τ ,
where A = | K | and Θ = 1 2 ( 1 ± 1 4 K 2 ) . The boundary and initial conditions can be obtained from the exact solution. In our calculations we have considered K = 1 4 and Θ = 1 2 3 4 . Further details can be found in [11].
The reason we designed this example is to show the advantage of HWCM. To examine the error bounds, we analyzed the spatial and temporal discretization errors of the proposed method separately. To test the spatial convergence of the HWCM, we set Δ τ = 0.0001 for various values of M and discovered that the theoretical and experimental rates of convergence for the space variable are in good agreement. To study the discretization error in time, we fixed M for different values of Δ τ .
Problem 3.
Finally, consider the following form of NHSE
2 φ τ 2 2 φ s 2 + i φ τ + | φ | 2 φ = 0 , 40 s 40 , 0 τ T .
with the initial conditions
φ ( s , 0 ) = ( 1 + i ) s e 10 ( 1 s ) 2 , φ ( s , 0 ) τ = 0 ,
and homogeneous boundary conditions φ ( 40 , τ ) = 0 = φ ( 40 , τ ) .
This problem is challenging due to the blow up phenomena of the soliton wave and has been considered in many papers as a practical problem [1,11,12] which has no exact solution. In Figure 3 the soliton wave is presented at different T, where the propagation of soliton is clearly seen as time increases. From this figure, one can examine that the soliton wave translates and converts into some lower waves quickly, and more ripples get up with the progression of wave. As the time T 5 , the single soliton is split into more than one small solitons and moves violently. In Table 2 and Table 3 the discrete conservation law are given for different T and Δ τ by fixing M. From these table it can be easy to conclude that the HWCM can simulate the conservation of energy and mass in Equation (28) very well, respectively.

6. Discussion

Different NHSEs are solved by the HWCM proposed in this paper for different time and space intervals. The real and imaginary part of the numerical solution are compared with the exact solution in Figure 1, Figure 2 and with the Galerkin method in Table 4, where the same order of accuracy has been obtained for a lesser number of collocation points than the Galerkin method. In the theorem it is proved that the proposed method is second order accurate in space discretization, which is supported by the numerical results and verified by calculating the experimental rate of convergence (see Table 1 and Table 5). The various results obtained by the proposed methods are compared with exact solutions as well as other existing methods. The propagation of soliton wave towards boundary from the origin is clearly shown in Figure 3 at a different final time, which is the important part while studying the Schr o ¨ dinger equation. The conservation laws for energy and mass are preserved in Table 2, Table 3, Table 6 and Table 7. The experimental rate of convergence and the maximum absolute errors are displayed in Table 1 and Table 5. A comparison of HWCM is performed with other well known methods in Table 4 for a linear case and in Figure 4 for a nonlinear challenging case as well, which shows better performance of the HWCM.

7. Conclusions

In this work, we have proposed the HWCM for the numerical solution of second-order NHSEs with wave operator. In different figures, it is shown that the propagating soliton waves are accurately captured by the proposed method and the HWCM has also been used to solve nonlinear problems with the blowup phenomena. The proposed HWCM preserves the energy as well as the mass, which have been highlighted for various examples. In different tables, the experimental rate of convergence is in line with the theoretical rate of convergence. The L error norm and the rate of convergence show that the proposed numerical method is accurate and applicable to solve NHSEs. Through the implementation of HWCM on different types of nonlinear equations and based on the above numerical experiments, we may conclude that the proposed HWCM is practical, time-efficient, and effective for solving NHSEs numerically. Due to the high potential achievements of the HWCM, the current scheme can be implemented to 2D and coupled NHSEs. These topics are the focus of our forthcoming work.

Author Contributions

Conceptualization, M.A. (Muhammad Ahsan) and M.A. (Masood Ahmad); methodology, M.A. (Muhammad Ahsan), M.N. and M.A. (Masood Ahmad); software, I.A. and H.A.; validation, M.A. (Muhammad Ahsan), X.L. (Xiaoling Liu) and X.L. (Xuan Liu); formal analysis, M.A. (Muhammad Ahsan) and I.A.; investigation, H.A. and M.A. (Masood Ahmad); resources, X.L. (Xiaoling Liu) and X.L. (Xuan Liu); data curation, M.A. (Masood Ahmad) and M.A. (Muhammad Ahsan); writing—original draft preparation, M.A. (Muhammad Ahsan); writing—review and editing, M.A. (Muhammad Ahsan) and I.A.; visualization, M.A. (Masood Ahmad), H.A. and M.N.; supervision, M.A. (Masood Ahmad); project administration, X.L. (Xiaoling Liu) and X.L. (Xuan Liu); funding acquisition, X.L. (Xiaoling Liu). All authors have read and agreed to the published version of the manuscript.

Funding

This research was supported by Characteristic innovation project of Guangdong Provincial Department of Education under No. 2017KTSCX124.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

We wish to acknowledge the anonymous referees whose suggestions have helped improve the quality of our paper.

Conflicts of Interest

The authors declare no conflict of interest.

Nomenclature

ODEsordinary differential equations
PDEspartial differential equation equations
NHSEsnonlinear hyperbolic Schr o ¨ dinger equations
HWCMHaar wavelet collocation method
φ unknown complex function
sspace variable
τ time variable
E ( τ ) energy invariant
Q ( τ ) mass invariant
w ¯ 0 ( τ ) function of variable τ
w ˜ 0 ( s , τ ) function of variables τ and s
μ i constant parameter, where i = 1 , 2 , 3 , 4 and 5
h i ( s ) Haar wavelet function
a , ζ 1 , ζ 2 , ζ 3 and bsome real numbers
p i , 1 ( s ) integral of h i ( s ) from a to s
p i , 2 ( s ) integral of p i , 1 ( s ) from a to s
Cintegral of p i , 1 ( s ) from a to b
λ i unknown Haar wavelet coefficients
i 1
2M number of collocation points
s l  collocation points
Δ τ  time discretisizing unit
I 1 , I 2 , B 1 and B 2  given known functions
L ( a , b )  infinity-norm in the interval (a,b)
φ M ( s , τ )  Haar wavelet representation of φ
φ ˜ M n + 1 ( s )  approximate numerical value of φ
E M ( s , τ )  error term due to Haar wavelet approximation
E M H ( s , τ )  Haar wavelet truncation error term
O ( Δ τ 2 )  truncation error due to time discretization
P positive integer
p all positive integer up to P
Re real part
Im imaginary part
E  infinity error
E R e  maximum absolute error of real part
E I m  maximum absolute error of imaginary part

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Figure 1. The solution and the absolute error at M = 128 , T = 1 and Δ τ = 0.001 for Test Problem 2.
Figure 1. The solution and the absolute error at M = 128 , T = 1 and Δ τ = 0.001 for Test Problem 2.
Energies 14 07831 g001
Figure 2. Profile of the numerical solutions at M = 128 and Δ τ = 0.01 with different T for Test Problem 2.
Figure 2. Profile of the numerical solutions at M = 128 and Δ τ = 0.01 with different T for Test Problem 2.
Energies 14 07831 g002
Figure 3. The profile of soliton wave at various T with M = 128 and Δ τ = 0.01 for Test Problem 3.
Figure 3. The profile of soliton wave at various T with M = 128 and Δ τ = 0.01 for Test Problem 3.
Energies 14 07831 g003aEnergies 14 07831 g003b
Figure 4. Comparison of propagating soliton obtained form different methods for Test Problem 3.
Figure 4. Comparison of propagating soliton obtained form different methods for Test Problem 3.
Energies 14 07831 g004
Table 1. The numerical results at Δ τ = 0.0001 , and T = 1 for Test Problem 1. Theoretical rate of convergence is 2 (see Theorem 1).
Table 1. The numerical results at Δ τ = 0.0001 , and T = 1 for Test Problem 1. Theoretical rate of convergence is 2 (see Theorem 1).
M E Experimental Rate of ConvergenceCPU Time (Second Unit)
1 1.3468 × 10 1 -0.5020
2 2.9363 × 10 2 2.1975 1.2312
4 9.7614 × 10 3 1.5888 2.4447
8 2.5647 × 10 3 1.9283 6.9728
16 6.3987 × 10 4 2.0029 13.2555
Table 2. Conservation laws at various time levels with M = 32 and Δ τ = 0.01 for Test Problem 3.
Table 2. Conservation laws at various time levels with M = 32 and Δ τ = 0.01 for Test Problem 3.
T E Q
0.10.0004634221899000.000519664924343i
0.20.0004590116485890.000502983303627i
0.30.0004504554560480.000479539412998i
0.40.0004356979043020.000453609233561i
0.50.0004136343485050.000429562779666i
0.60.0003850222784160.000410899419094i
0.70.0003528379665130.000399558520828i
0.80.0003218892037780.000395661494238i
0.90.0002977372551760.000397719510978i
10.0002852219720770.000403216918935i
Table 3. Conservation laws at various time steps with M = 8 and T = 1 for Test Problem 3.
Table 3. Conservation laws at various time steps with M = 8 and T = 1 for Test Problem 3.
Δ τ E Q
0.0050.0000000000656640.00000000094289i
0.0010.0000000000657230.00000000094345i
0.00050.0000000000657300.00000000094353i
0.00010.0000000000657360.00000000094358i
Table 4. Comparison of different methods at Δ τ = 0.001 and T = π 2 for Test Problem 1.
Table 4. Comparison of different methods at Δ τ = 0.001 and T = π 2 for Test Problem 1.
HWCMGalerkin Method ( p 0 ) [11]Galerkin Method ( p 1 ) [11]
N = 2 M E Re E Im N E Re E Im E Re E Im
16 2.38 × 10 2 2.16 × 10 2 20 2.09 × 10 1 2.09 × 10 1 3.79 × 10 2 3.79 × 10 2
32 4.21 × 10 3 8.95 × 10 3 40 8.69 × 10 2 8.69 × 10 2 5.05 × 10 3 5.05 × 10 3
64 1.73 × 10 3 5.81 × 10 3 80 4.11 × 10 2 4.11 × 10 2 1.31 × 10 3 1.31 × 10 3
Table 5. The numerical results at Δ τ = 0.0001 , and T = 1 for Test Problem 2. Theoretical rate of convergence is 2 (see Theorem 1).
Table 5. The numerical results at Δ τ = 0.0001 , and T = 1 for Test Problem 2. Theoretical rate of convergence is 2 (see Theorem 1).
M E Experimental Rate of Convergence
1 9.9872 × 10 2 -
2 2.9424 × 10 2 1.7630
4 7.9739 × 10 3 1.8836
8 1.9021 × 10 3 2.0676
16 4.7361 × 10 4 2.0058
Table 6. Error norms and conservation laws at various time level with M = 128 and Δ τ = 0.001 for Test Problem 1.
Table 6. Error norms and conservation laws at various time level with M = 128 and Δ τ = 0.001 for Test Problem 1.
T E Re E Im E E Q
0.1 9.8864 × 10 4 1.0506 × 10 3 1.0541 × 10 3 2.249906963054199 1.999664635386422 i
0.2 9.5558 × 10 4 9.9005 × 10 4 9.9772 × 10 4 2.249936145461749 1.999568078806202 i
0.3 9.0241 × 10 4 9.5549 × 10 4 9.7158 × 10 4 2.249924837045404 1.999483611315301 i
0.4 8.3248 × 10 4 8.9079 × 10 4 9.0917 × 10 4 2.249851076414263 1.999387185040249 i
0.5 7.5063 × 10 4 7.9955 × 10 4 8.1870 × 10 4 2.249705208726114 1.999267565085404 i
0.6 7.9987 × 10 4 7.1485 × 10 4 9.7909 × 10 4 2.249488431902245 1.999123715667415 i
0.7 8.3409 × 10 4 7.6764 × 10 4 1.1246 × 10 3 2.249209466191778 1.998958893217779 i
0.8 8.2634 × 10 4 9.4861 × 10 4 1.2538 × 10 3 2.248882302999423 1.998777677883512 i
0.9 7.7745 × 10 4 1.1220 × 10 3 1.3646 × 10 3 2.248524815729122 1.998585531996365 i
1 7.0575 × 10 4 1.2804 × 10 3 1.4550 × 10 3 2.248157302414185 1.998388782032106 i
Table 7. Error norms and conservation laws at various M with T = 1 and Δ τ = 0.01 for Test Problem 2.
Table 7. Error norms and conservation laws at various M with T = 1 and Δ τ = 0.01 for Test Problem 2.
M E Re E Im E E Q
8 4.5530 × 10 3 1.5323 × 10 3 4.8039 × 10 3 0.000948069171383 0.000232841089347 i
16 6.0002 × 10 3 2.2329 × 10 3 6.4022 × 10 3 0.000985139322483 0.000254685053319 i
32 6.7727 × 10 3 2.7085 × 10 3 7.2942 × 10 3 0.000991057419645 0.000255807453310 i
64 6.9416 × 10 3 2.8066 × 10 3 7.4875 × 10 3 0.000992332262253 0.000256101948732 i
128 6.9769 × 10 3 2.8255 × 10 3 7.5273 × 10 3 0.000992632417626 0.000256178051069 i
256 6.9852 × 10 3 2.8299 × 10 3 7.5367 × 10 3 0.000992706293238 0.000256197214486 i
512 6.9872 × 10 3 2.8309 × 10 3 7.5390 × 10 3 0.000992724689529 0.000256202013479 i
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Liu, X.; Ahsan, M.; Ahmad, M.; Nisar, M.; Liu, X.; Ahmad, I.; Ahmad, H. Applications of Haar Wavelet-Finite Difference Hybrid Method and Its Convergence for Hyperbolic Nonlinear Schrödinger Equation with Energy and Mass Conversion. Energies 2021, 14, 7831. https://0-doi-org.brum.beds.ac.uk/10.3390/en14237831

AMA Style

Liu X, Ahsan M, Ahmad M, Nisar M, Liu X, Ahmad I, Ahmad H. Applications of Haar Wavelet-Finite Difference Hybrid Method and Its Convergence for Hyperbolic Nonlinear Schrödinger Equation with Energy and Mass Conversion. Energies. 2021; 14(23):7831. https://0-doi-org.brum.beds.ac.uk/10.3390/en14237831

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Liu, Xuan, Muhammad Ahsan, Masood Ahmad, Muhammad Nisar, Xiaoling Liu, Imtiaz Ahmad, and Hijaz Ahmad. 2021. "Applications of Haar Wavelet-Finite Difference Hybrid Method and Its Convergence for Hyperbolic Nonlinear Schrödinger Equation with Energy and Mass Conversion" Energies 14, no. 23: 7831. https://0-doi-org.brum.beds.ac.uk/10.3390/en14237831

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