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Abstract

In this paper, we present a collocation algorithm for numerically treating the time-fractional Kuramoto–Sivashinsky equation (TFKSE). Certain orthogonal polynomials, which are expressed as combinations of Chebyshev polynomials, and their shifted polynomials are introduced. Some new theoretical formulas regarding these polynomials have been developed, including their operational matrices of both integer and fractional derivatives. The derived formulas will be the foundation for designing the proposed numerical algorithm, which relies on converting the governing problem with its underlying conditions into a nonlinear algebraic system, which can be solved using Newton’s iteration technique. A rigorous error analysis for the proposed combined Chebyshev expansion is presented. Some numerical examples are given to ensure the applicability and efficiency of the presented algorithm. These results demonstrate that the proposed algorithm attains superior accuracy with fewer expansion terms.

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1. Introduction

Memory effects and non-local interactions are key features of fractional differential equations (FDEs) that distinguish them from classical differential equations (DEs). These features make FDEs ideal for modelling real-world processes. If your system displays complex dynamical behaviour, anomalous diffusion, or genetic effects, FDEs will be a better fit. Therefore, their significance is growing in numerous domains, including physics, engineering, biology, and finance [1,2]. The fields of viscoelasticity, heat conduction, electromagnetism, and signal processing—all of which can significantly benefit from contemporary computer technology—are where FDEs are utilized in the physical and engineering sciences. For some applications, one can refer to [3,4].

Numerous numerical techniques were followed to treat different types of FDEs. Some of them can be listed as follows:

The series–based methods, such as the Laplace–residual power series method [5], and the fractional power series method [6].

The mesh-based methods, such as the predictor–corrector methods [7,8,9], the three–step Adams–Bashforth scheme [10], the spatial sixth-order finite-difference scheme [11], and the spectral element approach [12].

The wavelets and semi-analytic methods, such as Hahn–wavelets collocation method [13], the Fibonacci-wavelets operational-matrix technique [14], and the spectral method in [15].

The neural method, such as the Chebyshev neural-network scheme [16].

A hybrid numerical approach that mixes more than one method, such as the method in [17] that combines the Gauss quadrature rule and finite difference scheme.

Chebyshev polynomials (CPs) play a crucial role in several branches of applied mathematics. They are important in numerical analysis and approximation theory. The first four types of CPs are most often used because of the intuitive trigonometric formulas associated with them. Several publications, both recent and old, use these polynomials in several applications. The authors of [18] created some differentiation matrices of CPs for handling certain nonlinear DEs. In [19], certain modified third-kind CPs were used to treat the multidimensional hyperbolic telegraph equations. In other publications, various modifications and generalizations of CPs have been introduced and used to treat several DEs. For instance, the sixth kind of CPs was used in [20] to treat some fractional partial FDEs. The eighth kind of CPs was utilized in [21] to treat the nonlinear time-fractional generalized Kawahara equation. A set of unified CPs was constructed and employed in [22] to treat the time-fractional heat DEs. Two generalized kinds of CPs were introduced, respectively, in [23,24] to solve some FDEs.

Spectral methods are popular methods to treat DEs. Such approaches are excellent for solving FDEs and high-order ordinary DEs. Their primary benefit over more conventional numerical approaches is the extreme precision they may attain for smooth problems via exponential or high-order convergence. These techniques provide accurate approximations with few degrees of freedom by expressing the numerical solution using special functions or special polynomials. Spectral methods have found practical applications in many domains, including the modelling of biological systems, fluid dynamics, and quantum physics. One can refer to [25,26,27] for a few examples of spectral methods applications. Collocation, tau, and Galerkin are the three primary spectral approaches. Every method has its characteristics and advantages. The collocation method can be applied to all types of DEs due to its simplicity in application, see for example [28,29,30,31]. The Galerkin method can be applied to linear equations and some non-linear ones, see for instance [32,33,34]. For instance, as demonstrated in [35,36,37], the flexibility of the basis function choices makes the tau technique more adaptable compared to the Galerkin method.

An essential tool for modelling complex spatiotemporal dynamics like turbulence and chaos is the fourth-order nonlinear partial differential equation known as the Kuramoto-Sivashinsky equation (KSE). Its development by Yoshiki Kuramoto and Gregory Sivashinsky in the late 1970s was the beginning of its evolution into an indispensable tool in numerous technological and scientific domains. The KSE describes various physical and chemical processes, including chemical reaction-diffusion, plasma instability, problems with viscous flow, growth of flame fronts, and magnetized plasmas [38,39]. Since the KSE and its variants are so important, numerous authors have investigated numerical approaches for handling them using various algorithms. For example, a fractional power series method was presented in [6] to treat the nonlinear KSE. A finite difference scheme was followed in [40] to treat the TFKSE. A kernel smoothing technique was introduced in [41] for the numerical approximation of generalized TFKSEs. Chebyshev cardinal functions were employed in [42] to solve the variable-order fractional version of the two-dimensional equation. Another spline approach was proposed in [43] to treat the fourth-order time-dependent PDEs, including the TFKSE. Certain shifted Morgan–Voyce polynomials were utilized in [44] to treat the TFKSE. Several other methods were employed in [45,46,47,48] for the treatment of these equations.

The employment of the operational matrices of derivatives (OMDs) is pivotal in obtaining numerical solutions of several DEs. The philosophy of the use of these matrices relies on converting the integer and fractional operators into algebraic forms, which enable the reduction of the equation under investigation into a solvable system of equations. This approach decreases the computational cost, making it a powerful technique for treating complex models in applied mathematics, physics, and engineering. The use of OMDs allows various families of orthogonal and non-orthogonal polynomials to be employed in constructing numerical algorithms that are both reliable and versatile. Many publications have been devoted to introducing and employing different OMDs for various DEs. For example, an operational matrix in the Caputo sense was introduced in [49], with applications to fractional models. A matrix approach was followed in [50] for the treatment of a fractional-order computer virus model. The shifted Lucas polynomial collocation scheme, relying on its operational matrix, was presented in [51] for solving the time-fractional FitzHugh–Nagumo equation. An efficient method based on the Chelyshkov operational matrix for the time-space fractional reaction–diffusion equations was developed in [52]. A collocation method employing the fractional-order Lagrange operational matrix was described in [53] for the space-time fractional PDEs. A new operational matrix approach was designed in [54] to solve nonlinear FDEs. Vieta–Fibonacci operational matrices were introduced in [55] to construct spectral solutions for variable-order fractional integro–DEs.

The primary objective of the current paper is to propose a numerical approach that uses the spectral collocation approach to address the TFKSE. To accomplish this, a family of basis functions known as shifted combined Chebyshev polynomials (SCCPs) is presented. The proposed approach can be better designed with the help of specific new formulas that are related to these polynomials.

This paper’s originality is illustrated in the following aspects:

Introducing some new fundamental formulas regarding the combined Chebyshev polynomials (CCPs) and their shifted polynomials.

Establishing new integer and fractional OMDs of these polynomials, which are the fundamental basis for designing the proposed numerical algorithm.

Presenting a rigorous convergence and error analysis of the proposed combined Chebyshev expansion.

The following is the outline for the remainder of the article. An outline of the two main kinds of CPs, along with some key definitions, is provided in the next section. Furthermore, an account of the CCPs and their shifted polynomials is given. Section 3 is dedicated to constructing new formulas for the SCCPs that will be pivotal in our study. Section 4 examines the collocation algorithm developed for handling the TFKSE. In Section 5, the upper bound on the error is provided. In Section 6, some numerical examples are displayed, supported by some comparisons with some other methods. In Section 7, a few last thoughts are reported.

2. Some Essential Definitions and Relations

This section presents some key concepts of fractional calculus. It also presents some features of CPs and their shifted polynomials. In addition, some properties of the CCPs and their shifted polynomials are given.

2.1. Caputo’s Fractional Derivative

Definition 1

([56]). In Caputo’s sense, the fractional-order derivative of ψCk[0,s], where k=ν is defined as:

(1)Dtνψ(s)=1Γ(kν)0s(st)kν1ψ(k)(t)dt,ν>0,s>0,k1<νk,kN.

For Dtν with k1<νk,kN, the relations listed below are valid:

(2)DtνB=0,Bisaconstant,

(3)Dtνsk=0,ifkN0andk<ν,(k)!Γ(kν+1)skν,ifkN0andkν,

where N={1,2,} and N0={0,1,2,}, and ν represents the ceiling function.

Remark 1.

The notation Ck[0,s] denotes the space of functions that are k-times continuously differentiable on the interval [0,s].

2.2. An Overview of CPs

We give here some elementary properties of the first and second kinds of CPs and their shifted polynomials.

The first- and second-kinds of CPs: Tk(x) and Uk(x) are defined as [57])

(4)Tk(x)=cos(kϕ),Uk(x)=sin(k+1)ϕsinϕ,

where ϕ=cos1(x).

Tk(x), and Uk(x) have the following series representations:

(5)Tk(x)=kr=0k2(1)r21+k2r(kr1)!r!(k2r)!xk2r,

(6)Uk(x)=r=0k2(1)r2k2r(kr)!(k2r)!r!xk2r.

The shifted CPs on [0,1] denoted by Tk(x), and Uk(x) can be defined as

(7)Tk(x)=Tk2x1,Uk(x)=Uk2x1,

and they may be expressed as

(8)Tk(x)=kr=0k(1)r22(kr)(2kr1)!(2k2r)!r!xkr,

(9)Uk(x)=r=0k(1)r22(kr)(2kr+1)!(2k2r+1)!r!xkr.

2.3. Combined Chebyshev Polynomials on [1,1]

In [58], Chihara introduced the following orthogonal CCPs on [1,1] defined as

(10)Ck(ξ)(x)=12k1Tk(x)+11ξUk2(x),k0.

Based on the connection formula [57]:

(11)Tk(x)=12Uk(x)Uk2(x),k0,

Ck(ξ)(x) can also be expressed in the following form:

(12)Ck(ξ)(x)=12kUk(x)+12ξUk2(x),k0.

Remark 2.The polynomials Ck(ξ)(x) are extensions of the first and second kinds of CPs, as is evident from the two equations in (10) and (12). To be more specific, we have

(13)Tk(x)=2k1Ck(1)(x),Uk(x)=2kCk(2)(x).

One of the significant formulas of Cj(ξ)(x) is the following three-term recurrence relation [58]:

(14)Cj(ξ)(x)=xCj1(ξ)(x)14Cj2(ξ)(x),j2.

The set of polynomials {Ck(ξ)}k0 are orthogonal on [1,1] with respect to the weight function w(ξ)(x)=1x21ξ(2ξ)x2 in the sense that [59]

(15)11w(ξ)(x)Cm(ξ)(x)Cj(ξ)(x)dx=0,mj,4πξ3,m=j=0,πξ222m1,m=j>0.

2.4. Some Properties of the SCCPs

It is useful to introduce the SCCPs on [0,1] defined as

(16)θi(ξ)(x)=Ci(ξ)(2x1).

These polynomials are orthogonal on [0,1] in the sense that [59]:

(17)01θi(ξ)(x)θj(ξ)(x)w¯(ξ)(x)dx=hi(ξ)δi,j,

where

w¯(ξ)(x)=x(1x)ξ(ξ2)(12x)2+1,hi(ξ)=πξ3,i=0,πξ222i+1,i1.

From (12), by replacing x with (2x1), the SCCPs can be written as combinations of the shifted second kind of CPs as

(18)θj(ξ)(x)=2j(ξ2)ξUj2(x)+Uj(x).

Furthermore, based on the series representation of Uj(x) in (9) along with the combination in (12), they may be represented explicitly as

(19)θi(ξ)(x)=r=0jλr,jxjr,

where

(20)λr,j=(1)j+12j(2jr1)!jrΓj+r12ξ2j22jr+j+(r1)rr2+rπξj!.

The previous power formula can be rewritten in another form as

(21)θi(ξ)(x)=r=0jGr,jxr,

where

(22)Gr,j=(1)1+j2jjjrΓ12r(j+r1)!j+2jr+j2(1+ξ)+r(1+r)(1+ξ)πξj!.

3. Some New Formulas of the CCPs and SCCPs

This section derives some new formulas concerned with the CCPs and SCCPs, which will be pivotal in deriving the suggested numerical scheme. More precisely, the following formulas will be established:

The connection formula between the second kind CPs and the CCPs, that is, we will determine explicitly the connection coefficients Am,i in the following connection formula:

(23)Ui(x)=m=0i2Am,iCi2m(ξ)(x).

Formula (23) will lead immediately to the following connection formula between the shifted second kind Chebyshev polynomials Ui(x) and the SCCPs:

(24)Ui(x)=m=0i2Am,iθi2m(ξ)(x),

only by replacing x by (2x1) in the connection formula (23).

The inversion formula for the series representation for the SCCPs in (19), that is, we will determine explicitly the inversion coefficients Zr,m in the following formula:

(25)xm=r=0mZr,mθmr(ξ)(x),

for every nonnegative integer m.

The high-order derivatives formula for the SCCPs as a combination of their original polynomials, that is, we will derive an expression for Dqθj(ξ)(x) in the following form:

(26)Dqθj(ξ)(x)=m=0jqVjmq,r,j(q)θm(ξ)(x),jq.

The establishment of the OMDs of the SCCPs, that is, we define the vector

(27)θ(ξ)(x)=[θ0(ξ)(x),θ1(ξ)(x),,θN(ξ)(x)]T,

and we will find explicitly the operational matrix of derivatives Vq such that the following identity holds:

(28)dqθ(ξ)(x)dxq=Vqθ(ξ)(x).

The expression of the fractional derivatives of the SCCPs, that is, we will determine the coefficients Qn,j such that for γ(0,1), we have the following expression:

(29)Dtγθj(ξ)(t)=tγn=0jQn,jθn(ξ)(t).

Constructing the operational matrix of fractional derivatives of the SCCPs. It can be constructed from the above fractional derivative expression. In fact, from (29), we can write

(30)dγθ(ξ)(t)dtγ=tγDγθ(ξ)(t),

where Dγ=(Qn,j).

We now proceed to prove our theoretical results that will be pivotal in what follows.

Theorem 1.

Ui(x) are connected with Ci(ξ)(x) by the following formula:

(31) U i ( x ) = m = 0 i 2 ζ i 2 m 2 i 2 m 2 ξ ξ m C i 2 m ( ξ ) ( x ) , i 0 ,

where

(32) ζ j = ξ 2 , j = 0 , 1 , otherwise .

Proof. 

The idea of the proof depends on proving that the right-hand side of (31) satisfies the same recurrence relation of Ui(x) with the same initials. For this end, assume the following polynomials:

(33)ρi(x)=m=0i2ζi2m2i2m2ξξmCi2m(ξ)(x).

Noting that ρ0(1)=1,ρ1(x)=2x, then to prove that (31) holds for i2, it remains to show that the following identity holds:

(34)ηi(x)=ρi+2(x)2xρi+1(x)+ρi(x)=0,i0.

Using Formula (33), ηi(x) can be written in the following form:

(35)ηi(x)=m=0i+22ζi2m+22i2m+22ξξmCi2m+2(ξ)(x)2xm=0i+12ζi2m+12i2m+12ξξmCi2m+1(ξ)(x)+m=0i2ζi2m2i2m2ξξmCi2m(ξ)(x).

We will prove the validity of the following two identities:

(36)η2i(x)=0,η2i+1(x)=0,i0.

It is possible to divide Equation (35) into the following two identities:

(37)η2i(x)=m=0i+1ζ2i2m+222i2m+22ξξmC2i2m+2(ξ)(x)2xm=0iζ2i2m+122i2m+12ξξmC2i2m+1(ξ)(x)+m=0iζ2i2m22i2m2ξξmC2i2m(ξ)(x),

(38)η2i+1(x)=k=0i+122i2k+32ξξkζ2i2k+3C2i2k+3(ξ)(x)2xk=0i+122i2k+22ξξkζ2i2k+2C2i2k+2(ξ)(x)+k=0i22i2k+12ξξkζ2i2k+1C2i2k+1(ξ)(x).

We prove that η2i(x)=0. The proof of η2i+1=0 is similar.

Now, if we make use of the recurrence relation (14) written as

(39)xCj(ξ)(x)=Cj+1(ξ)(x)+14Cj1(ξ)(x),

then Formula (37) turns into following form:

(40)η2i(x)=m=0i+1ζ2i2m+222i2m+22ξξmC2i2m+2(ξ)(x)2m=0iζ2i2m+122i2m+12ξξmC2i2m+2(ξ)(x)+14C2i2m(ξ)(x)+m=0iζ2i2m22i2m2ξξmC2i2m(ξ)(x),

of which the following form is also possible to express:

(41)η2i(x)=m=1iζ2i2m22i2m2ξξm+1C2i2m(ξ)(x)2m=1i1ζ2i2m122i2m12ξξm+1C2i2m(ξ)(x)12m=0iζ2i2m+122i2m+12ξξmC2i2m(ξ)(x)+m=0iζ2i2m22i2m2ξξmC2i2m(ξ)(x).

Now, after some algebraic manipulation, we can write

(42)ηi(x)=m=0iMm,iC2i2m(ξ)(x)+2ξ2ξξi+1ζ1+22+2iζ2i+1+ζ2i+2C2i+2(ξ)(x),

where

(43)Mm,i=2ξ1i(ξ2)ξ,m=i,0,0mi1.

Based on the definition of ζi in (32), it follows that c1=1 and c2i+1=c2i+2=1, and hence the formula of Mm,i leads to

(44)η2i(x)=0.

This ends the proof. □

Corollary 1.

The following is the connection formula between Ui(x) and θi(ξ)(x):

(45) U i ( x ) = m = 0 i 2 ζ i 2 m 2 i 2 m 2 ξ ξ m θ i 2 m ( ξ ) ( x ) .

Proof. 

Equation (45) follows directly from (31) when x is substituted with (2x1). □

The following formula derives the inversion formula of the SCCPs.

Theorem 2.

Let m be any non-negative integer. xm can be expressed in terms of the CCPs as

(46)xm=r=0mZr,mθmr(ξ)(x),

where

(47)Zr,m==0r2(2m+1)!(2+m+1)2mr+1ζmr2ξ1r2(2)!(2+2m+2)!,reven,=0r12(2m+1)!(m2)2mr+1ζmr2ξ112(2+r1)(2+1)!(2+2m+1)!,rodd,

where ζj is as given in (32).

Proof. 

We start from the following inversion formula of Ui(x):

(48)xm=r=0m212m(1+mr)(1+2m)!(2+2mr)!r!Umr(x).

Applying Formula (45) to (48) yields the following formula:

(49)xm=r=0m212m(1+mr)(1+2m)!(2+2mr)!r!k=0mr2ζmr2k2mr2k2ξξkθmr2k(ξ)(x).

Some lengthy manipulations enable one to write the last formula into the following formula:

(50)xm=r=0m2Sr,mθm2r(ξ)(x)+r=0m12S¯r,mθm2r1(ξ)(x),

with

(51)Sr,m==0rζm2r21m2r1+2ξ+r(12+m)(1+2m)!(2)!(22+2m)!,

(52)S¯r,m==0rζm2r12m2r1+2ξ+r(2+m)(1+2m)!(2+1)!(12+2m)!.

Formula (50) may be expressed as

(53)xm=r=0mZr,mθmr(ξ)(x),

with

(54)Zr,m==0r2(2m+1)!(m+12)2mr+1ζmr2ξ1r2(2)!(2m+22)!,reven,=0r12(2m+1)!(m2)2mr+1ζmr2ξ1r12(2+1)!(2m+12)!,rodd.

This ends the proof. □

Theorem 3.

Let j,q be two positive integers with jq. We can write

(55)Dqθj(ξ)(x)=m=0jqVjmq,r,jqθm(ξ)(x),

with

(56)Vm,r,jq=r=0mλr,j(jqr+1)qZmr,jqr,

where λr,j is given in (20), and Zr,m is given in (54).

Proof. 

Differentiating the analytic form in (19) yields the following formula:

(57)Dqθj(ξ)(x)=r=0jqλr,j(jrq+1)qxjrq.

Based on the inversion formula (46), the last equation may be converted into

(58)Dqθj(ξ)(x)=r=0jqλr,j(jrq+1)qt=0jrqZt,jrqθjrqt(ξ)(x),

which can be written alternatively as

(59)Dqθj(ξ)(x)=m=0jqr=0mλr,j(jrq+1)qZmr,jrqθjqm(ξ)(x),

which give Formula (55). □

Remark 3.

Based on the high-order derivative formula of the SCCPs in (55), the OMDS of these polynomials may be deduced. This outcome is given in the following corollary.

Corollary 2.

Assume the following vector:

(60) θ ( ξ ) ( x ) = [ θ 0 ( ξ ) ( x ) , θ 1 ( ξ ) ( x ) , , θ N ( ξ ) ( x ) ] T .

The first-, second-, and fourth-order derivatives of the vector θ(ξ)(x) may be expressed as

(61) d θ ( ξ ) ( x ) d x = U θ ( ξ ) ( x ) , d 2 θ ( ξ ) ( x ) d x 2 = V θ ( ξ ) ( x ) , d 4 θ ( ξ ) ( x ) d x 4 = K θ ( ξ ) ( x ) ,

where U=(Vjm1,r,j1), V=(Vjm2,r,j2), and K=(Vjm4,r,j4) are the OMDS each of order (N+1)2.

For example, the matrices U,V and K take the following form for N=7:

(62)U=00000000ξ0000000040000001ξ4060000002ξ080000(ξ4)ξ+816ξ012+2ξ0100000(ξ2)ξ+44ξ20ξ+2ξ0120016(ξ4)2ξ64ξ2038+1ξ212ξ032+2ξ0140,

(63)V=00000000000000004ξ00000000240000002(ξ5)0480000002+28ξ08000003ξ43+9ξ012(ξ+3)ξ01200000226ξξ2+5026+44ξ016800,

(64)K=00000000000000000000000000000000192ξ000000001920000000192(ξ7)05760000000960(ξ+6)ξ0134400000.

The following theorem is concerned with deriving an expression that computes the fractional derivatives of the SCCPs.

Theorem 4.

For γ(0,1),Dtγθj(ξ)(t) can be expressed as

(65) D t γ θ j ( ξ ) ( t ) = t γ n = 0 j Q n , j θ n ( ξ ) ( t ) ,

where

(66) Q n , j = k = 0 j ( k + 1 ) ! G k + 1 , j Z k n + 1 , k + 1 Γ ( k γ + 2 ) .

Proof. 

Based on (3) together with Formula (21), we can write

(67)Dtγθj(ξ)(t)=tγp=1jp!Gp,jΓ(pγ+1)tp.

Formula (46) turns (67) into the following one:

(68)Dtβθj(ξ)(t)=tγp=1js=0pp!Gp,jZps,pΓ(pγ+1)θs(ξ)(t),

which can be rearranged to give

(69)Dtγθj(ξ)(t)=tγn=0jQn,jθn(ξ)(t),

where

(70)Qn,j=k=0j(k+1)!Gk+1,jZkn+1,k+1Γ(kγ+2).

This completes the proof of this theorem. □

Corollary 3.

The fractional derivative of θ(ξ)(t) can be represented as

(71) d γ θ ( ξ ) ( t ) d t γ = t γ D γ θ ( ξ ) ( t ) ,

where Dγ=(Qn,j).

Proof. 

It is a direct consequence of Formula (65). □

For example, and for the following choices:

γ=12,ξ=3,N=7,

the matrix Dγ takes the following form:

(72)Dγ=000000005π000000010π383π00000015512π38π46415π00000403π6089π185615π261635π000057548π5516π1264445π26167π101776567π00023524π252724π2134445π3618835π203552189π8916802079π001435192π385736π33065π146067π59793401701π891680297π1181603211583π0.

4. Treatment of the TFKSE Using the Collocation Method

In this section, we consider the following TFKSE: [60]:

(73)γζ(σ,t)tγ+a1(σ,t)ζ(σ,t)ζ(σ,t)σ+a2(σ,t)2ζ(σ,t)σ2+a3(σ,t)4ζ(σ,t)σ4=f(σ,t),(σ,t)(0,1)×(0,1],

subject to the following conditions:

(74)ζ(σ,0)=g(σ),

(75)ζ(0,t)=g0(t),ζ(1,t)=g1(t),

(76)ζ(0,t)σ=0,ζ(1,t)σ=0,

or

(77)ζ(σ,0)=g(σ),

(78)ζ(0,t)=g0(t),ζ(1,t)=g1(t),

(79)2ζ(0,t)σ2=0,2ζ(1,t)σ2=0,

where a1(σ,t), a2(σ,t), and a3(σ,t) are real-valued functions of σ and t, a2(σ,t) and a3(σ,t) are connected to the growth of linear stability and surface tension [61], respectively. It is assumed that a1(σ,t), a2(σ,t), a3(σ,t), f(σ,t), g(σ), g0(t), and g1(t) are sufficiently smooth functions.

Now, consider the following space:

(80)WN=span{θm(ξ)(σ)θn(ξ)(t):0m,nN},

and therefore, every function ζN(σ,t)WN may be written as

(81)ζN(σ,t)=m=0Nn=0Nζ^mnθm(ξ)(σ)θn(ξ)(t)=θ(ξ)(σ)Tζ^θ(ξ)(t),

where θ(ξ)(σ) is as given in (60), and ζ^=(ζ^mn)0m,nN is the matrix to be determined with order (N+1)2.

Now, the residual RN(σ,t) of Equation (73) may be expressed as

(82)RN(σ,t)=γζN(σ,t)tγ+a1(σ,t)ζN(σ,t)ζN(σ,t)σ+a2(σ,t)2ζN(σ,t)σ2+a3(σ,t)4ζN(σ,t)σ4f(σ,t).

In virtue of Corollaries 2 and 3, RN(σ,t) may be rewritten in the following form:

(83)RN(σ,t)=θ(ξ)(σ)Tζ^(tγDγθ(ξ)(t))+a1(σ,t)θ(ξ)(σ)Tζ^θ(ξ)(t)(Uθ(ξ)(σ))Tζ^θ(ξ)(t)+a2(σ,t)(Vθ(ξ)(σ))Tζ^θ(ξ)(t)+a3(σ,t)(Kθ(ξ)(σ))Tζ^θ(ξ)(t)f(σ,t).

Applying the collocation method, we may force the residual RN(σ,t) to vanish at suitable collocation nodes σm,tn in order to obtain the expansion coefficients ζ^mn, that is

(84)RNσm,tn=0,1mN3,1nN,

where {(σm,tn):m,n=1,2,,N+1} are the first distinct roots of θN+1(ξ)(x).

In addition, the conditions (74)–(76) lead to the following equations:

(85)θσmTζ^θ(0)=gσm,1mN+1,

(86)θ(0)Tζ^θtn=g0tn,1nN,

(87)θ(1)Tζ^θtn=g1tn,1nN,

(88)(Uθ(0))Tζ^θtn=0,1nN,

(89)(Uθ(1))Tζ^θtn=0,1nN,

while the conditions (77)–(79) lead to the following equations:

(90)θσmTζ^θ(0)=gσm,1mN+1,

(91)θ(0)Tζ^θtn=g0tn,1nN,

(92)θ(1)Tζ^θtn=g1tn,1nN,

(93)(Vθ(0))Tζ^θtn=0,1nN,

(94)(Vθ(1))Tζ^θtn=0,1nN.

To obtain ζ^mn, one can use Newton’s iterative technique to solve the (N+1)2 nonlinear system of equations that is created by Equations (85)–(89) or (90)–(94), in addition to (84).

Remark 4.

It is worth mentioning here that Newton’s method for solving the (N+1)2 nonlinear system of equations is convergent under the following conditions:

Choosing a suitable initial guess ζ^mn=10mn that ensure the convergence.

There is no singular Jacobian while solving the system in (85)–(89) or (90)–(94), in addition to (84).

5. Error Bound

The main aim of this section is to find an estimation of ζ(σ,t)ζN(σ,t), such that ||ζ(σ,t)ζN(σ,t)||0 as N.

Theorem 5.

Let ζN(σ,t)WN be the best approximation of ζ(σ,t). The following inequality holds:

(95) | | ζ ( σ , t ) ζ N ( σ , t ) | | 2 2 N 1 ( ( ξ 1 ) N + ξ ) ξ Γ ( N + 2 ) ,

where s1s2 means that there is a constant ν such that s1νs2.

Proof. 

Since ζN(σ,t)WN is the best approximation of ζ(σ,t); then, we can write the following inequality:

(96)||ζ(σ,t)ζN(σ,t)||||ζ(σ,t)ζ^N(σ,t)||,ζ^N(σ,t)WN.

In addition, (96) holds if ζ^N(σ,t) represents the interpolating polynomial for ζ(σ,t) at points (σi,tj), where σi are the zeros of θi(ξ)(σ), while tj are the zeros of θj(ξ)(t). Now, if we take similar steps as in [62,63], we get

(97)ζ(σ,t)ζ^N(σ,t)=N+1ζ(η,t)σN+1(N+1)!i=0N(σσi)+N+1ζ(σ,μ)tN+1(N+1)!j=0N(ttj)2N+2ζ(η^,μ^)σN+1tN+1((N+1)!)2i=0N(σσi)j=0N(ttj).

where η,η^,μ,μ^[0,1].

Now, we can write

(98)||ζ(σ,t)ζ^N(σ,t)||max(σ,t)ΩN+1ζ(η,t)σN+1||i=0N(σσi)||(N+1)!+max(σ,t)ΩN+1ζ(σ,μ)tN+1||j=0N(ttj)||(N+1)!+max(σ,t)Ω2N+2ζ(η^,μ^)σN+1tN+1||i=0N(σσi)||||j=0N(ttj)||((N+1)!)2.

Since ζ is a smooth function on Ω=[0,1]2, then there exist three constants σ1,σ2 and σ3, such that

(99)max(σ,t)ΩN+1ζ(η,t)σN+1σ1,max(σ,t)ΩN+1ζ(σ,μ)tN+1σ2,max(σ,t)Ω2N+2ζ(η^,μ^)σN+1tN+1σ3.

To minimize the factor ||i=0N(σσi)||, we use the one-to-one mapping σ=12(z+1) between the intervals [1,1] and [0,1] to deduce that

(100)minσi[0,1]maxσ[0,1]i=0N(σσi)=minzi[1,1]maxz[1,1]i=0N12(zzi)=12N+1minzi[1,1]maxz[1,1]i=0N(zzi)=12N+1minzi[1,1]maxz[1,1]CN+1(ξ)(z)CN(ξ)¯,

where CN(ξ)¯=1 is the leading coefficient of CN+1(ξ)(z) and zi are the zeros of CN+1(ξ)(z).

Similarly, the factor ||j=0N(ttj)||, can be minimized by using the one-to-one mapping t=12(t¯+1) between the intervals [1,1] and [0,1] to deduce that

(101)mintj[0,1]maxt[0,1]j=0N(ttj)=12N+1mint¯j[1,1]maxt¯[1,1]CN+1(ξ)(t¯)C(ξ)¯N,

Now, we can write

(102)maxz[1,1]CN+1(ξ)(z)=maxz[1,1]2(N+1)(ξ2)ξUN1(z)+UN+1(z)=2N((ξ1)N+ξ)ξ,

And hence, inequality (99) along with Equations (100)–(102) help us to obtain the following required result:

(103)||ζ(σ,t)ζN(σ,t)||||ζ(σ,t)ζ^N(σ,t)||<σ122N1((ξ1)N+ξ)ξΓ(N+2)+σ222N1((ξ1)N+ξ)ξΓ(N+2)+σ342N1((ξ1)N+ξ)2ξ2Γ(N+2)222N1((ξ1)N+ξ)ξΓ(N+2).

6. Some Numerical Examples

This section presents some numerical examples to ensure the applicability and high accuracy of our proposed algorithm. In addition, comparisons with some other algorithms are presented.

Example 1

([60]). Consider the following equation:

(104)γζ(σ,t)tγ2ζ(σ,t)ζ(σ,t)σ+42ζ(σ,t)σ2+4ζ(σ,t)σ4=f(σ,t),(σ,t)(0,1)×(0,1],

governed by the following conditions:

(105) ζ ( σ , 0 ) = ζ ( 0 , t ) = ζ ( 1 , t ) = ζ ( 0 , t ) σ = ζ ( 1 , t ) σ = 0 ,

where f(σ,t) is selected to meet the the exact solution of (104) given by

(106)ζ(σ,t)=t4σ2σ35σ22+2σ12.

Table 1 and Table 2 present a comparison of L and L2 errors, respectively, between our method at different values of γ with the method in [60]. Table 3 presents the L errors at different values of ξ and γ when N=5. Figure 1 shows the absolute errors (left) and approximate solution (right) at γ=0.2 and ξ=1 when N=5.

Remark 5.

It is noticed from the results of Table 3 that the two cases correspond to the classical CPs, case ξ=1 corresponds to the first kind of CPs, ξ=2 that corresponds to the second kind of CPs, do not always yield the smallest L errors. This demonstrates that our idea to introduce the CCPs and their shifted versions that generalize both the standard first and second kinds of CPs and their shifted versions is significant.

Example 2.

Consider the following equation:

(107) γ ζ ( σ , t ) t γ + σ ζ ( σ , t ) ζ ( σ , t ) σ + σ 2 ζ ( σ , t ) σ 2 + 4 ζ ( σ , t ) σ 4 = f ( σ , t ) , ( σ , t ) ( 0 , 1 ) × ( 0 , 1 ] .

governed by the following conditions:

(108) ζ ( σ , 0 ) = ζ ( 0 , t ) = ζ ( 1 , t ) = 2 ζ ( 0 , t ) σ 2 = 2 ζ ( 1 , t ) σ 2 = 0 ,

where f(σ,t) is selected to meet the exact solution of (107) given by

(109)ζ(σ,t)=t4sin(πσ).

Figure 2 shows the absolute errors (left) and approximate solution (right) at γ=0.2 and ξ=1 when N=18. Table 4 reports the absolute errors and also the CPU times (in seconds) (in seconds) for our numerical method at γ=0.8 and ξ=2 when N=18. Figure 3 shows the absolute errors at different values of N when γ=0.5. Table 5 reports the absolute errors and also the CPU times (in seconds) for our numerical method at γ=0.9 and ξ=2 when N=18.

Example 3

([60]). Consider the following equation:

(110)γζ(σ,t)tγ+e20tζ(σ,t)ζ(σ,t)σ+(1+100σ)2ζ(σ,t)σ2=f(σ,t),(σ,t)(0,1)×(0,1].

governed by the following conditions:

(111)ζ(σ,0)=ζ(0,t)=ζ(1,t)=ζ(0,t)σ=ζ(1,t)σ=0,

where f(σ,t) is selected to meet the exact solution of (110) given by

(112)ζ(σ,t)=t4σ3(1σ)3.

Table 6 presents a comparison of L errors between our method at different values of γ with the method in [60]. Figure 4 shows the absolute errors (left) and approximate solution (right) at γ=0.5 and ξ=4 when N=6. Table 7 reports the absolute errors and also the CPU times (in seconds) for our numerical method when γ=0.3 and ξ=1 when N=5.

Example 4.

Consider the following equation:

(113) γ ζ ( σ , t ) t γ + σ ζ ( σ , t ) ζ ( σ , t ) σ + σ 2 ζ ( σ , t ) σ 2 + 4 ζ ( σ , t ) σ 4 = f ( σ , t ) , ( σ , t ) ( 0 , 1 ) × ( 0 , 1 ] .

governed by the following conditions:

(114) ζ ( σ , 0 ) = ζ ( 0 , t ) = ζ ( 1 , t ) = 2 ζ ( 0 , t ) σ 2 = 2 ζ ( 1 , t ) σ 2 = 0 ,

where f(σ,t) is selected to meet the exact solution of (113) given by

(115) ζ ( σ , t ) = t 4 + α sin ( π σ ) .

Table 8 reports the absolute errors and also the CPU times (in seconds) for our numerical method at γ=0.5 and ξ=1 when N=18. Figure 5 illustrates the absolute errors and approximate solution at γ=0.8 and ξ=3 when N=18.

Remark 6.

The algorithm designed in this paper was suitable for handling Equation (73) in the square domain. The same problem has been solved through other numerical algorithms, such that was those developed in [60]. The numerical results in this section showed the high accuracy and applicability of our algorithm using the combined CPs.

Remark 7.

To handle the problem defined on irregular domains, the method can be extended by employing a suitable curvilinear coordinate transformation, which maps an irregular physical domain into a square domain; however, this requires a comprehensive analysis. We aim to investigate this problem in a separate study in future work.

7. Concluding Remarks

In this work, an efficient collocation framework is analyzed for the numerical solution of the time-fractional Kuramoto–Sivashinsky equation. Certain combined orthogonal polynomials were utilized for this purpose. Some theoretical results of these polynomials, such as the power form representation and their inversion formula, were pivotal in establishing the integer and fractional operational matrices of derivatives. These formulas were essential in designing the numerical algorithm. Through a series of numerical experiments, the method has shown excellent agreement with exact solutions and significant improvements over recently developed algorithms. We expect that other classes of differential equations may be treated using the CCPs. In addition, we aim to introduce other combined orthogonal polynomials and utilize them in numerical analysis. All codes were written and debugged using Mathematica 11 on an HP Z420 Workstation, with an Intel(R) Xeon(R) CPU E5-1620 processor, v2, 3.70 GHz; 16 GB of RAM, DDR3; and 512 GB of storage.

Author Contributions

Conceptualization, W.M.A.-E.; Methodology, W.M.A.-E., M.A.A., N.M.A.A. and A.G.A.; Software, A.G.A.; Validation, W.M.A.-E., N.M.A.A. and A.G.A.; Formal analysis, W.M.A.-E., N.M.A.A. and A.G.A.; Investigation, W.M.A.-E., M.A.A., N.M.A.A. and A.G.A.; Writing—original draft, W.M.A.-E. and M.A.A.; Writing—review & editing, W.M.A.-E. and A.G.A.; Funding acquisition, M.A.A. All authors have read and agreed to the published version of the manuscript.

Data Availability Statement

Data are contained within the article.

Conflicts of Interest

The authors declare no conflicts of interest.

Footnotes

Disclaimer/Publisher’s Note: The statements, opinions and data contained in all publications are solely those of the individual author(s) and contributor(s) and not of MDPI and/or the editor(s). MDPI and/or the editor(s) disclaim responsibility for any injury to people or property resulting from any ideas, methods, instructions or products referred to in the content.

Figures and Tables

Figure 1 The absolute errors (left) and approximate solution (right) of Example 1.

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Figure 2 The absolute errors (left) and approximate solution (right) of Example 2.

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Figure 3 The absolute errors of Example 2 at γ=0.5.

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Figure 4 The absolute errors (left) and approximate solution (right) of Example 3.

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Figure 5 The absolute errors and approximate solution of Example 4 at γ=0.8.

View Image -

Comparison of L errors for Example 1.

γ Method in [60] at Ns=160,Mt=320 Proposed Method at N=5
ξ = 1 ξ = 2 ξ = 3
0.3 4.0055 × 10 12 9.51588 × 10 16 2.24918 × 10 16 1.96003 × 10 16
0.5 7.3038 × 10 12 8.80678 × 10 16 2.29253 × 10 16 2.39325 × 10 16
0.8 5.0390 × 10 11 9.10954 × 10 16 2.2734 × 10 16 2.21425 × 10 16

Comparison of L2 errors for Example 1.

γ Method in [60] at Ns=160,Mt=320 Proposed Method at N=5
ξ = 1 ξ = 2 ξ = 3
0.3 8.2604 × 10 13 2.4914 × 10 15 1.87817 × 10 15 4.21728 × 10 16
0.5 9.0548 × 10 12 2.31524 × 10 16 1.09774 × 10 15 5.44158 × 10 15
0.8 3.1675 × 10 11 2.47329 × 10 16 5.02686 × 10 16 4.70814 × 10 15

L errors for Example 1.

γ ξ = 0.6 ξ = 1 ξ = 1.5 ξ = 2 ξ = 2.5 ξ = 3 ξ = 3.5
0.3 1.62276 × 10 16 9.51588 × 10 16 2.12504 × 10 16 2.24918 × 10 16 1.6694 × 10 16 1.96003 × 10 16 2.25497 × 10 16
0.5 2.30089 × 10 16 8.80678 × 10 16 1.33319 × 10 16 2.29253 × 10 16 2.26395 × 10 16 2.39325 × 10 16 1.71556 × 10 16
0.8 2.30243 × 10 16 9.10954 × 10 16 2.289 × 10 16 2.2734 × 10 16 2.23061 × 10 16 2.21425 × 10 16 1.71799 × 10 16

The absolute errors of Example 2.

σ t = 0.3 CPU Time t = 0.6 CPU Time t = 0.9 CPU Time
0.1 7.17829 × 10 15 6.43166 × 10 14 3.08337 × 10 13
0.2 1.39116 × 10 14 1.24803 × 10 13 5.97689 × 10 13
0.3 1.97793 × 10 14 1.7758 × 10 13 8.49432 × 10 13
0.4 2.43382 × 10 14 2.18783 × 10 13 1.04439 × 10 12
0.5 2.71276 × 10 14 130.876 2.4436 × 10 13 131.048 1.16374 × 10 12 131.204
0.6 2.77382 × 10 14 2.50369 × 10 13 1.18894 × 10 12
0.7 2.57121 × 10 14 2.32731 × 10 13 1.10123 × 10 12
0.8 2.06458 × 10 14 1.8742 × 10 13 8.8346 × 10 13
0.9 1.21465 × 10 14 1.10557 × 10 13 5.19168 × 10 13

The absolute errors of Example 2.

σ t = 0.2 CPU Time t = 0.5 CPU Time t = 0.8 CPU Time
0.1 1.38691 × 10 14 4.51583 × 10 14 2.09416 × 10 13
0.2 2.67414 × 10 14 8.75133 × 10 14 4.05592 × 10 13
0.3 3.76216 × 10 14 1.24317 × 10 13 5.75373 × 10 13
0.4 4.56189 × 10 14 1.52871 × 10 13 7.05769 × 10 13
0.5 4.99646 × 10 14 128.204 1.70336 × 10 13 128.36 7.83984 × 10 13 128.516
0.6 4.99748 × 10 14 1.74034 × 10 13 7.98139 × 10 13
0.7 4.51958 × 10 14 1.6126 × 10 13 7.36244 × 10 13
0.8 3.52986 × 10 14 1.29452 × 10 13 5.88113 × 10 13
0.9 2.01427 × 10 14 7.6085 × 10 14 3.43864 × 10 13

Comparison of L errors for Example 3.

γ Method in [60] at Ns=128,Mt=64 Proposed Method at N=5
ξ = 4 ξ = 6 ξ = 9
0.6 4.2262 × 10 10 5.36161 × 10 17 5.23705 × 10 17 5.91998 × 10 17
0.8 3.9223 × 10 10 2.05108 × 10 16 2.68635 × 10 17 2.4015 × 10 17
0.95 3.3087 × 10 10 5.56566 × 10 17 9.94028 × 10 18 1.01048 × 10 16

The absolute errors of Example 3.

σ t = 0.2 CPU Time t = 0.5 CPU Time t = 0.8 CPU Time
0.1 2.64486 × 10 19 6.77626 × 10 20 2.54788 × 10 18
0.2 7.86047 × 10 19 1.0842 × 10 19 6.93889 × 10 18
0.3 7.45389 × 10 19 3.25261 × 10 19 8.23994 × 10 18
0.4 4.13352 × 10 19 2.1684 × 10 19 9.54098 × 10 18
0.5 5.75982 × 10 19 3.514 0 3.53 1.38778 × 10 17 3.53
0.6 7.04731 × 10 19 6.50521 × 10 19 1.64799 × 10 17
0.7 1.15196 × 10 18 7.58942 × 10 19 1.77809 × 10 17
0.8 1.05032 × 10 18 8.67362 × 10 19 1.47451 × 10 17
0.9 1.999 × 10 19 4.47233 × 10 19 4.71628 × 10 18

The absolute errors of Example 4.

σ t = 0.3 CPU Time t = 0.6 CPU Time t = 0.9 CPU Time
0.1 1.29728 × 10 10 1.46848 × 10 10 9.63238 × 10 10
0.2 2.46753 × 10 10 2.7931 × 10 10 1.83216 × 10 9
0.3 3.39616 × 10 10 3.84417 × 10 10 2.52169 × 10 9
0.4 3.99227 × 10 10 4.51879 × 10 10 2.96434 × 10 9
0.5 4.19752 × 10 10 131.47 4.75101 × 10 10 131.626 3.1168 × 10 9 131.783
0.6 3.99187 × 10 10 4.51818 × 10 10 2.96418 × 10 9
0.7 3.3955 × 10 10 3.84318 × 10 10 2.52143 × 10 9
0.8 2.46683 × 10 10 2.79214 × 10 10 1.83191 × 10 9
0.9 1.29681 × 10 10 1.4679 × 10 10 9.63091 × 10 10

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