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Effective transform-expansions algorithm for solving non-linear fractional multi-pantograph system

  • This study presents a new and attractive analytical approach to treat systems with fractional multi-pantograph equations. We introduce the solution as a rapidly-converging series using the Laplace residual power series technique. This method controls the range of convergence and can be easily programmed to find many terms of the series coefficients by computer software. To show the efficiency and strength of the proposed method, we compare the results obtained in this study with those of the Homotopy analysis method and the residual power series technique. Furthermore, two exciting applications of fractional non-homogeneous pantograph systems are discussed in detail and solved numerically. We also present graphical simulations and analyses of the obtained results. Finally, we conclude that the obtained approximate solutions are very close to the exact solutions with a slight difference.

    Citation: Ahmad Qazza, Rania Saadeh, Osama Ala'yed, Ahmad El-Ajou. Effective transform-expansions algorithm for solving non-linear fractional multi-pantograph system[J]. AIMS Mathematics, 2023, 8(9): 19950-19970. doi: 10.3934/math.20231017

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  • This study presents a new and attractive analytical approach to treat systems with fractional multi-pantograph equations. We introduce the solution as a rapidly-converging series using the Laplace residual power series technique. This method controls the range of convergence and can be easily programmed to find many terms of the series coefficients by computer software. To show the efficiency and strength of the proposed method, we compare the results obtained in this study with those of the Homotopy analysis method and the residual power series technique. Furthermore, two exciting applications of fractional non-homogeneous pantograph systems are discussed in detail and solved numerically. We also present graphical simulations and analyses of the obtained results. Finally, we conclude that the obtained approximate solutions are very close to the exact solutions with a slight difference.



    Recently, fractional differential or integral equations and their applications have attracted great interest due to their significant role in describing and justifying various phenomena, for example, chaos synchronization, mechanical systems, image processing, earthquake modeling, wave propagation phenomena, control theory [1,2,3,4,5], artificial intelligence, machine learning, and deep learning in different branches of science and engineering [6,7]. In addition, systems of fractional differential equations (DEs) are a suitable tool for modeling nonlinear dynamical systems [8,9]. The fractional delay DEs are thought to be a potent tool for modeling a variety of natural phenomena, such as the model of HIV infection [10], fractional-order chaotic delayed systems [11], some automatic control systems with feedback [12], etc.

    Delay DEs have various applications in different fields, such as industrial, biological, chemical, electronic and transport systems [13,14,15,16]. One of the most common types of delay DEs is the pantograph equation, which was used by Ockendon and Tayler [15] to study the collection of electric current via an electric locomotive pantograph, hence the name. The pantograph equation is given by the following DE:

    ρ(τ)=φ(τ,ρ(τ),ρ(δτ)),τ0,ρ(0)=ω,

    where 0<δ<1,m=1,2,,k.

    The multi-pantograph differential equation [17,18,19], which is an extension of the pantograph equation and has the following form:

    ρ(τ)=φ(τ,ρ(τ),ρ(δ1τ),ρ(δ2τ),,ρ(δkτ)),τ0,ρ(0)=ω,

    where 0<δm<1,m=1,2,,k, has many applications in electrodynamics, number theory, astrophysics, control of ships, probability theory, physics, engineering, economics, chemistry, nonlinear dynamical systems, cell growth, chemical kinetics, electronic systems, infectious diseases, medicine, control problems and quantum mechanics [10,11,12,13,14,15,16,20,21,22]. The multi-pantograph differential equation involves a system with a temporal delay, and the behavior of the known variable at any given point in the previous states dictates how the unknown variable will behave.

    Widatalla and Koroma [16] and other researchers [23,24,25] proposed the following system of multi-pantograph equations and gave an approximate solution to it by different methods:

    ρ'r(τ)=σrρr(τ)+φr(τ,ρi(τ),ρj(γjτ)),ρr(0)=ωr,r=1,2,3,m,

    where i and j{1,2,3,m}, ωr, σr, γjR, such that 0<σr<1, and φr are functions of τ,ρi(τ), and ρj(γjτ). This system is considered one of the most important kinds of delay DEs that can describe various kinds of applications in engineering, physics and pure and applied mathematics, such as electronic systems, quantum mechanics and dynamical systems among others.

    Because many natural phenomena involve information from the past or memory, researchers saw the use of the fractional derivative as a tool to study the phenomenon in the moments leading up to the moment of its onset [26,27,28,29,30,31,32,33,34]. Thus, the fractional delay DEs are originally classical DEs that are reformulated by substituting the fractional derivative instead of the classical one for the abovementioned purpose. Therefore, the authors in [35,36,37] reformulated the above system by replacing the classical derivatives with fractional derivatives in the Caputo sense as follows and introduced approximate solutions to it through various methods:

    Dαρr(τ)=σrρr(τ)+φr(τ,ρi(τ),ρj(γjτ)), (1)

    subject to

    ρr(0)=ωr,r=1,2,3,m, (2)

    where Dα,α(0,1] is the Caputo-fractional derivative operator, and as with all models of fractional equations, the fractional derivative describes the motion memory in the system and provides an exceptional understanding of the behavior of various dynamical systems.

    Unfortunately, for the fractional multi-pantograph system (FMPS), like the different fractional models, it is difficult to provide an exact solution, and it may be impossible most of the time. Therefore, researchers resort to providing approximate solutions using analytical or numerical methods. Lately, many scholars have extensively researched and proposed numerous analytical and numerical approaches to investigate solutions of fractional equations, such as the variational iteration method [38], reproducing kernel method [39], Adomian decomposition method [40], fractional difference method [41], Homotopy perturbation method [42], Homotopy analysis method [35,43], sine-Gordon expansion method [44], artificial neural network methods [45], gradient-based optimization approach [36], fractional differential transform method [37], residual power series technique (RPST) [35,46,47] and other methods [48,49].

    The RPST is an effective analytical method to set the power series solution coefficients for the ordinary and partial DEs. It is based on creating a series solution for numerous linear and nonlinear DEs and provides a convergent series solution without the need for linearization, discretization, or perturbation. Although old-fashioned, the Laplace transform (LT) is still used to solve various classes of linear DE [49]. Unfortunately, it cannot be utilized directly to solve nonlinear DE. Some analytical methods have been modified by exploiting the Laplace transform to simplify its working mechanisms, such as the Laplace Homotopy perturbation [26], Laplace Adomian decomposition method [27], Laplace Homotopy analysis method [28] and He-Laplace method [29].

    Recently, on the same approach, El-Ajou and his research team employed the LT in the RPST to simplify the tactic of determining the series solution coefficients for some DEs of fractional order, such as the nonlinear time-fractional dispersive PDEs, Lane-Emden equations, multi-dimensional time-fractional Navier-Stokes system, Fisher's equation and logistic system model among others [30,31,32,33,34]. This employment led to the facilitation and acceleration of determining the coefficients process compared with the RPST. The new approach is called the Laplace residual power series technique (LRPST). The mechanism of the new technique depends on transforming the equation into a Laplace space and then creating a series solution for the new equation. Due to the properties of the LT, the series solution is in the form of the fractional Laurent series [30]. Series coefficients are determined using the concept of limit at infinity instead of the fractional derivative used in the RPST. Operating the inverse LT on the obtained Laurent series gives the series solution to the original equation.

    The RPST and LRPST present a solution to the DE in a series form. Therefore, the result is supposed to be identical in both methods. But what distinguishes the LRPST from the RPST is the ease of obtaining the series coefficients. The RPST requires the calculation of the fractional derivative to the residual function in each step of determining the coefficients steps. In contrast, the LRPST needs to calculate the limit at infinity when specifying the coefficients. The Caputo derivative is one of the non-local derivatives that need improper integration calculation, and it takes a long time as we progress in the steps of the solution, even when using computer software. Calculating the limit at infinity is much simpler and does not take much time compared to calculating the improper integrals.

    Indeed, for the systems (1) and (2), its exact solution is not known yet, and all the solutions given by the previous methods are approximate solutions whose accuracy varies from one method to another. On the other hand, literature doesn't addresses the LRPST for solving systems of fractional DEs to the extent of our knowledge. Therefore, in this paper, we seek to apply the new approach, LRPST [35,50], in creating an accurate analytical series solution to another class of fractional DEs, the FMPS given in (1) and (2). In addition, we look to show the ease, speed, and efficiency of the proposed method to obtain accurate solutions by comparing it with the previous results obtained by other techniques, such as the Homotopy analysis method and the RPST.

    The rest of the presented study is structured as follows: In Section 2, we offer some basic definitions and theorems related to fractional power series. Section 3 discusses the suggested method to construct a series solution to the FMPS. In Section 4, we offer two applications with numerical simulations of MPEs. We summarize and discuss the obtained results in the final section.

    Various definitions of the fractional derivative were pointed out previously, such as Hadamard, Riemann Liouville, Caputo, Atangana-Baleanu, Caputo-Fabrizio, conformable, and Riesz definitions. Caputo's view of the fractional derivative is still the most used among other points of view as it has a physical significance in various models and has diverse theorems concerning the expansion of the functions, which is absent from other definitions. Moreover, there is an agreement that Caputo's definition satisfies the fractional derivative conditions. Consequently, during this work, we are interested in considering Caputo's concept, which is defined as follows [51]:

    Dαρ(τ)={1Γ(να)τ0(τζ)υα1ρ(υ)(ζ)dζ,υ1<α<υ,0ζ<τ,ρ(υ)(τ),α=υ. (3)

    Next, we introduce some basic definitions, lemmas and facts essential to constructing the Laplace residual power series solution (LRPSS) for the FMPS.

    Some significant properties of the Caputo-fractional derivative are Dα(κ)=0, κ is a constant, and Dατ(τη)=Γ(η+1)Γ(η+1α)τηα,τ0, η>1,υ1<αυ, vN. For more details, the reader is advised to refer to [51].

    Definition 1. [49] Assume that a function ρ(τ) is specified for τ0. The LT of ρ(τ) is designated and given by:

    P(s)=[ρ(τ)]=0esτρ(τ)dτ. (4)

    Whereas, the inverse LT of P(s) is encoded and defined as:

    ρ(τ)=1[P(s)]=μ+iμiesτP(s)ds,μ=Re(s). (5)

    Lemma 1. [30] Let ρ(τ) be a function of exponential order β and piecewise continuous function on [0,). Then,

    i) limssP(s)=ρ(0),

    ii) [Dαρ(τ)]=sαP(s)υn=0sαn1ρ(n)(0),υ1<α<υ,

    iii) [Dkαρ(τ)]=skαP(s)υn=0s(kn)α1Dnατρ(τ),0<α<1,

    where, P(s)=[ρ(τ)] and Dkα=DαDαDα (k -times).

    Theorem 1. [46] Assume that ρ(τ) can be expressed in fractional power series (FPS) of radius R around τ=0 as:

    ρ(τ)=n=0σnτnα,0<α1,0τ<R. (6)

    If Dnαρ(τ) is continuous on (0,R),n=0,1,2,, then the coefficients σn 's of the above series are provided by

    σn=Dnαρ(0)Γ(nα+1),n=0,1,2,. (7)

    The next theorem describes the coefficients of the Laurent series expansion (LSE), which is the best tool for constructing the LRPS of a given fractional DE in the Laplace space.

    Theorem 2. [29] Assume that ρ(τ) can be stated in terms of the FPS, and assume that Dnαρ(τ) is continuous on (0,R),n=0,1,2,. If P(s)=[ρ(τ)], then P(s) has the following fractional LSE:

    P(s)=n=0Dnαρ(0)snα+1, (8)

    where 0<α1,s>0, and n=0,1,2,.

    The ensuing theorem provides the essential convergence conditions of the LSE.

    Theorem 3.[29] Assume that P(s)=[ρ(τ)] has a fractional LSE. If |s[D(n+1)αρ(τ)|γ, on 0<sβ where 0<α1, and nN, then the remainder of the fractional LSE (Rn(s)) satisfies

    |Rn(s)|γs(n+1)α+1,0<sβ. (9)

    This section introduces the LRPST to construct a series solution to the FMPS. We present the method as a seven-step algorithm. Each step includes mathematical procedures and the facts that explain the process.

    Step 1. Operate the LT on each equation in (1) and use part (ii) of Lemma 1 to get

    sαPr(s)sα1ρr(0)=σrPr(s)+[φr(s,1[Pi(s)],1γj1[Pj(sγj)])], (10)

    for i,j{1,2,,m}, and r=1,2,,m.

    Step 2. Use the conditions (2) with some simplification to rewrite (10) as follows:

    Pr(s)=ωrs+σrsαPr(s)+1sα[φr(s,1[Pi(s)],1γj1[Pj(sγj)])], (11)

    Step 3. Assume that the LRPSS of (1) and (2) have the following LSE:

    Pr(s)=ωrs+n=1hr,nsnα+1,s>0,r=1,,m. (12)

    So, the k th truncated series of Pr(s) will be as follows:

    Pr,k(s)=ωrs+kn=1hr,nsnα+1,s>0,r=1,,m. (13)

    Step 4. For every r=1,2,,m, define the Laplace residual functions of (11) as:

    Resr(s)=Pr(s)ωrsσrsαPr(s)1sα[φr(s,1[Pi(s)],1γj1[Pj(sγj)])], (14)

    and the k th Laplace residual functions as:

    Resr,k(s)=Pr,k(s)ωrsσrsαPr,k(s)1sα[φr(s,1[Pi,k(s)],1γj1[Pj,k(sγj)])]. (15)

    In this regard, the following facts related to the Laplace residual functions and the k th Laplace residual functions must be mentioned, which are considered basic tools in determining the coefficients of the LSE in (12) [30]:

    limkResr,k(s)=Resr(s), for s>0, r=1,2,,m.

    Resr(s)=0, for s>0, r=1,2,,m.

    limsskα+1Resr(s)=0,for  α,s>0,r=1,2,,m,k=0,1,2,. (16)

    limsskα+1Resr,k(s)=0, for α,s>0, r=1,2,,m, k=0,1,2,.

    Step 5. To determine the value of the coefficient hr,k in the LSE (12) for r=1,2,,m and k=1,2,, substitute the k th truncated series, Pr,k(s), into the k th Laplace residual functions, Resr,n(s) to obtain

    Resr,k(s)=kn=1hr,nsnα+1σrsαPr,k(s)1sα[φr(s,1[ωis+kn=1hi,nsnα+1],1γj1[γjωjs+kn=1hj,n(γj)nα+1snα+1])]. (17)

    Step 6. Substitute (17) into fact (16) and solve the result equation iteratively for k=1,2, and r=1,2,,m. The solution of resultant equations gives the values of the coefficients of the LSE (12).

    Step 7. Substitute the obtained values of the coefficients, hr,k, into the k th truncated series (13) and operate the inverse LT on the resultant truncated LSE to obtain the k th approximate LRPSS to the systems (1) and (2).

    In the next section, we apply the algorithm described above in detail in two applications. To ensure the accuracy of the obtained results, we use two kinds of errors, the residual error (EαResr,k), and the exact error (EαExtr), which are given, respectively, as follows:

    EαResr,k=|Dαρr,k(τ)σrρr,k(τ)φk(τ,ρi,m(τ),ρj,m(γjτ))|,r=1,2,,m,k=1,2,. (18)
    EαExtr=|ρr(τ)ρr,k(τ)|,r=1,2,,m. (19)

    In this section, we test the proposed method through two applications. The first is a nonhomogeneous FMPS, and the second is a homogeneous FMPS.

    Application 4.1. [35] Consider the following nonhomogeneous FMPS:

    Dαρ1(τ)ρ1(τ)+ρ2(τ)ρ1(τ2)=eταeτα2,
    Dαρ2(τ)+ρ1(τ)+ρ2(τ)+ρ2(τ2)=eτα2+eτα, (20)

    subject to

    ρ1(0)=1,ρ2(0)=1. (21)

    Solution: To get the solution of (20) and (21) by LRPST, we first expand the exponential functions in (20) using the expansion of the standard exponential function

    ex=1+x1!+x22!+x33!+.

    Thus, Eq (20) becomes

    Dαρ1(τ)ρ1(τ)+ρ2(τ)ρ1(τ2)+(3τα23τ2α8+3τ3α165τ4α128+11τ5α12807τ6α5120)=0,
    Dαρ2(τ)+ρ1(τ)+ρ2(τ)+ρ2(τ2)(2+τα2+5τ2α8+7τ3α48+17τ4α384+31τ5α3840+13τ6α9216)=0. (22)

    Now, applying LT to each equation in (22) and using the condition (21), we obtain

    P1(s)1sP1(s)sα+P2(s)sα2P1(2s)sα+1sα(3Γ(α+1)2sα+13Γ(2α+1)8s2α+1+3Γ(3α+1)16s3α+15Γ(4α+1)128s4α+1+11Γ(5α+1)1280s5α+17Γ(6α+1)5120s6α+1)=0,
    P2(s)1s+P1(s)sα+P2(s)sα+2P2(2s)sα1sα(2s+Γ(α+1)2sα+1+5Γ(2α+1)8s2α+1+7Γ(3α+1)48s3α+1+17Γ(4α+1)384s4α+1+31Γ(5α+1)3840s5α+1+13Γ(6α+1)9216s6α+1)=0. (23)

    According to the previous section, the k th truncated series of the supposed series solution of the systems (20) and (21) is given as:

    P1,k(s)=1s+kn=1h1,nsnα+1,P2,k(s)=1s+kn=1h2,nsnα+1. (24)

    Consequently, the k th Laplace residual functions of (23) can be defined as:

    Res1,k(s)=P1,k(s)1sP1,k(s)sα+P2,k(s)sα2P1,k(2s)sα+1sα(3Γ(α+1)2sα+13Γ(2α+1)8s2α+1+3Γ(3α+1)16s3α+15Γ(4α+1)128s4α+1+11Γ(5α+1)1280s5α+17Γ(6α+1)5120s6α+1),
    Res2,k(s)=P2,k(s)1s+P1,k(s)sα+P2,k(s)sα+2P2,k(2s)sα1sα(2s+Γ(α+1)2sα+1+5Γ(2α+1)8s2α+1+7Γ(3α+1)48s3α+1+17Γ(4α+1)384s4α+1+31Γ(5α+1)3840s5α+1+13Γ(6α+1)9216s6α+1). (25)

    By substituting k=1 in (25), the first Laplace residual function will be as:

    Res1,1(s)=h1,1sα+1h1,1s2α+1+h2,1s2α+11sα+1h1,12αs2α+1+3Γ(α+1)2s2α+13Γ(2α+1)8s3α+1+3Γ(1+3α)16s4α+15Γ(1+4α)128s5α+1+11Γ(1+5α)1280s6α+17Γ(1+6α)5120s7α+1,
    Res2,1(s)=h2,1sα+1+h1,1s2α+1+h2,1s2α+1+1sα+1+h2,12αs2α+1Γ(α+1)2s2α+15Γ(2α+1)8s3α+17Γ(1+3α)48s4α+117Γ(1+4α)384s5α+131Γ(5α+1)3840s6α+113Γ(6α+1)9216s7α+1. (26)

    By multiplying each equation in (26) by sα+1, we get the following new system:

    sα+1Res1,1(s)=h1,11h1,1sα+h2,1sαh1,12αsα+3Γ(α+1)2sα3Γ(2α+1)8s2α+3Γ(3α+1)16s3α5Γ(4α+1)128s4α+11Γ(5α+1)1280s5α7Γ(6α+1)5120s6α,
    sα+1Res2,1(s)=h2,1+1+h1,1sα+h2,1sα+h2,12αsαΓ(α+1)2sα5Γ(2α+1)8s2α7Γ(3α+1)48s3α17Γ(4α+1)384s4α31Γ(5α+1)3840s5α13Γ(6α+1)9216s6α. (27)

    Taking the limit as s goes to infinity in (27) gives h1,1=1 and h2,1=1.

    By repeating the previous procedure for k=2,3,4,5, and 6, we can simply obtain the following coefficients:

    h1,2=(2+12α3Γ(α+1)2)  and  h2,2=(12α+Γ(α+1)2). (28)
    h1,3=18α+1(8+2α+4+23α+42α+2(3+4α+1)Γ(α+1)+3(2)3αΓ(1+2α)),
    h2,3=221α23α+(122α1)Γ(α+1)+58Γ(2α+1), (29)
    h1,6=(8+2114α+2111α+32110α+229α+5217α+216α+3(2)25α+22α+215α+416α+414α+412α+41α+81α12Γ(1+2α)249α(9+21+5α+9(2)1+9α+161+α3)Γ(1+3α)+6Γ(1+α)32114αΓ(1+α)2112αΓ(1+α)2110αΓ(1+α)229αΓ(1+α)3217αΓ(1+α)214αΓ(1+α)223αΓ(1+α)212αΓ(1+α)211αΓ(1+α)28αΓ(1+α)+26αΓ(1+α)725αΓ(1+α)229αΓ(1+2α)227αΓ(1+2α)+3(2)25αΓ(1+2α)+3225αΓ(1+2α)+28αΓ(1+2α)5412αΓ(1+2α)+3814αΓ(1+2α)1192Γ(1+4α)+5275αΓ(1+4α)11Γ(1+5α)1280),
    h2,6=(2815α15(3840+1529+2α+(15)211+7α(15)29+8α(15)210+13α+(15)45+6α+(15)45+7α+(15)83+α+(15)322+α+(15)5121+α+(15)10241+α+(15)27+α(121+2α+22+3α21+4α+321+5α(3)21+6α+22+7α+(3)21+8α21+9α+23+10α22+11α+41+7α+81+4α)Γ(1+α)(15)82+α(5+21+4α+521+7α+21+9α)αΓ(2α)+1528+11ααΓ(3α)+10542+3ααΓ(3α)(15)321+2ααΓ(3α)4526+11αΓ(1+2α)1544+3αΓ(1+2α)(15)83+5αΓ(1+2α)(15)162+3αΓ(1+2α)152561+αΓ(1+2α)+(35)321+3αΓ(1+3α)8521+10αΓ(1+4α)582+5αΓ(1+4α)+31215αΓ(1+5α)).

    Therefore, the fractional Laurent series solution of (23) can be expressed as

    P1(s)=1s+1sα+1+(2+12α3Γ(α+1)2)1s2α+1+18α+1s3α+1(8+2α+4+23α+42α+2(3+4α+1)Γ(α+1)+38αΓ(1+2α))+,
    P2(s)=1s1sα+1+(12α+Γ(α+1)2)1s2α+1+1s3α+1(221α23α+(122α1)Γ(1+α)+58Γ(1+2α))+. (30)

    To obtain the series solution to the systems (20) and (21), we apply the inverse LT to (30), and then we get

    ρ1(τ)=1+(2+12α3Γ(α+1)2)ταΓ(α+1)+18α+1(8+2α+4+23α+42α+2(3+4α+1)Γ(α+1)+3(2)3αΓ(2α+1))τ2αΓ(2α+1)+,
    ρ2(τ)=1+(12α+Γ(α+1)2)ταΓ(α+1)(2+12α1+123α(1122α+1)Γ(α+1)58Γ(2α+1))τ2αΓ(2α+1)+. (31)

    Putting α=1 in (31) gives the solution of (20) and (21) in the following form:

    ρ1(τ)=1+τ+τ22+τ38+,
    ρ2(τ)=1τ+τ22τ38+,

    which are the expansions of the exact solutions ρ1(τ)=eτ, ρ2(τ)=eτ.

    To verify the accuracy of the solution obtained in Eq (31) and to clarify the effect of changing α value on the behavior of the solution, some illustrations have been drawn in Figures 1-4. Figures 1(a) and 2(a). show comparisons between the 6th approximate solution given in (31) and the exact solution of the systems (20) and (21) at α=1. The results indicate a great agreement between the two solutions in the period [0,3].

    Figure 1.  The graph of (a) the exact solution, ρ1(τ)=eτ and the 6th approximate solution, ρ1,6(τ) at α=1, (b) ρ1,6(τ) at α=1,0.7,0.5.
    Figure 2.  The graph of (a) the exact solution, ρ2(τ)=eτ and the 6th approximate solution, ρ2,6(τ) at α=1, (b) ρ2,6(τ) at α=1,0.7,0.5.
    Figure 3.  The exact error of (a) the 6th approximate solution, ρ1,6(τ) (b) the 6th approximate solution, ρ2,6(τ) at α=1.
    Figure 4.  The graphs of the 6th approximate solution of the systems (20) and (21) when α=1 : Dotted Line: LRPST solution, Dashed Dotted Line: HAM (=1) solution, Solid Line: Exact solution. (a) ρ1,6(τ), (b) ρ2,6(τ).

    Figures 1(b) and 2(b) show the behavior of the systems (20) and (21) solution with different values of α, which are 0.5, 0.7 and 1. It can be seen from the figure that as the value of α changes, the level of motion represented by the dependent variables in FMPS changes more or less.

    Since we have the exact solution for the systems (20) and (21) at α=1, we introduce in Figure 3 the exact error of the 6th approximation for the solution given in (31) and it appears to be mathematically acceptable.

    In Figure 4, we make a comparison between the solution obtained by LRPST and the solution obtained by HAM with the exact solution at α=1. It is evident from the figure that the LRPSS is more compatible with the exact solution than with the HAM solution.

    For further analysis of the solution that we obtained in Application 4.1, we consider two types of errors, the exact errors, EαExt1 and EαExt2, and the residual errors, EαRes1 and EαRes2 of the approximate solution in (31) which are defined, respectively, as:

    EαExt1=|ρ1(τ)ρ1,k(τ)|,
    EαExt2=|ρ2(τ)ρ2,k(τ)|,
    EαRes1=|Dαρ1,k(τ)ρ1,k(τ)+ρ2,k(τ)ρ1,k(τ2)eτ+eτ/2|,
    EαRes2=|Dαρ2,k(τ)+ρ1,k(τ)+ρ2,k(τ)+ρ2,k(τ2)eτeτ/2|.

    Tables 1 and 2 confirm numerically the accuracy of the solution we obtained by calculating the exact and residual errors of the approximate solution in (31) at α=1 and 0.5. In addition, they present comparisons between the new solution and the previous solutions obtained by the RPST and HAM methods. The tables show the agreement between the results obtained from LRPST and RPST, which proves the proposed method's efficiency andthat LRPST is much easier and faster to program and performs calculations. Moreover, we can see from the tables that LRPST is better than HAM: the solution obtained from LRPST converges faster to the exact solution, and the error is slightly smaller than the errors obtained using HAM.

    Table 1.  The exact, Eα=1Ext1(τ) and the residual, Eα=0.5Res1(τ) errors of ρ1,6(τ)..
    Eα=1Ext1(τ) Eα=0.5Res1(τ)
    t LRPST HAM (=1) RPST LRPST HAM (=1) RPST
    0.0 0 0 0 0 0 0
    0.2 2.60461×109 2.91038×108 2.60461×109 8.88889×108 9.66713×107 8.88889×108
    0.4 3.42086×107 3.85358×106 3.42086×107 5.68889×106 5.94783×105 5.68889×106
    0.6 6.00039×106 6.75053×105 6.00039×106 6.47999×105 6.51337×104 6.47999×105
    0.8 4.61729×105 5.18636×104 4.61729×105 3.64089×104 3.51558×103 3.64089×104
    1.0 2.26273×104 253712×103 2.26273×104 1.38889×103 1.28713×102 1.38889×103

     | Show Table
    DownLoad: CSV
    Table 2.  The exact, Eα=1Ext2(τ) and the residual, Eα=0.5Res2(τ) errors of ρ2,6(τ).
    Eα=1Ext2(τ) Eα=0.5Res2(τ)
    t LRPST HAM (=1) RPST LRPST HAM (=1) RPST
    0.0 0 0 0 0 0 0
    0.2 2.47757×109 3.62052×108 2.47757×109 8.88889×108 1.27079×106 8.88889×108
    0.4 3.09519×107 4.55603×106 3.09519×107 5.68889×106 8.01156×105 5.68889×106
    0.6 5.16391×106 7.66634×105 5.16391×106 6.47999×105 8.98412×104 6.47999×105
    0.8 3.77914×105 5.65864×104 3.77914×105 3.64089×104 4.96166×103 3.64089×104
    1.0 1.76114×104 2.65956×103 1.76114×104 1.38889×103 1.85716×102 1.38889×103

     | Show Table
    DownLoad: CSV

    Application 4.2. [35] Consider the following homogeneous FMPS:

    Dαρ1(τ)+ρ1(τ)+eταcos(τα2)ρ2(τ2)+2e3τα4cos(τα2)sin(τα4)ρ1(τ4)=0,
    Dαρ2(τ)eταρ21(τ2)+ρ22(τ2)=0, (32)

    subject to

    ρ1(0)=1,ρ2(0)=0, (33)

    which has an exact solution in the case of α=1 as follows:

    ρ1(τ)=eτcosτ,ρ2(τ)=sinτ.

    Solution: As in the previous application, apply LT to every equation in (32) to get

    P1(s)1s+P1(s)sα+1sα[eταcos(τα2)21[P2(2s)]]+1sα[2e3τα4cos(τα2)sin(τα4)41[P1(4s)]]=0,
    P2(s)1sα[eτα(1[2P1(2s)])2]+1sα[(1[2P2(2s)])2]=0. (34)

    Depending on our approach taken in Section 3, assume that the k th approximate series solutions of (34) have the following expansions:

    P1,k(s)=1s+kn=1h1,nsnα+1,P2,k(s)=1s+kn=1h2,nsnα+1. (35)

    Therefore, the k th Laplace residual functions of (34) are as follows:

    Res1,k(s)=P1,k(s)1sP1,k(s)sα+1sα[eταcos(τα2)21[P2,k(2s)]]+1sα[2e3τα4cos(τα2)sin(τα4)41[P1,k(4s)]]=0,
    Res2,k(s)=P2,k(s)1sα[eτα(1[2P1,k(2s)])2]+1sα[(1[2P2,k(2s)])2]=0. (36)

    As in the previous example, recursively, we substitute k=1,2, into (36), multiply each equation in it by skα+1, and then take the limit as s to find the coefficients of series solution in (35) as follows:

    h1,1=1,
    h2,1=1,
    h1,2=(12α21Γ(α+1)),
    h2,2=(21α+Γ(α+1)),
    h1,3=18α+1(1+213α+2α+(1222α)Γ(1+α)+(1+21+α)Γ(12+α)2π+38Γ(1+2α)),
    h2,3=12Γ(1+2α)+8α(2+21+α21+4αΓ(12+α)π2αΓ(1+α)),
    h1,4=(1+216α215α213α2α12Γ(1+α)8α2Γ(1+2α)212απ(4+21+3α+4α)Γ(12+α)38Γ(1+2α)796Γ(1+3α)+413απΓ(1+3α)Γ(12+α)3(2)32α(1+2α)Γ(1+3α)Γ(1+α)215α(1+2α+41+α)Γ(1+3α)Γ(1+2α)+25αΓ(1+α)((1+8α)Γ(1+2α)+8αΓ(1+3α))Γ(1+2α)),
    h2,4=(216α(2+4α8α)215αΓ(1+α)+8α(1+21+α)πΓ(12+α)2αΓ(1+3α)Γ(1+α)+8αΓ(1+α)+3(2)23αΓ(1+2α)+16Γ(1+3α)+4αΓ(1+3α)Γ2(1+α)8α(321+α+2αΓ(1+α))Γ(1+3α)Γ(1+2α)214α(3+2α)Γ(1+3α)Γ(1+α)Γ(1+2α)).

    Thus, we can express the 5th approximate series solution of (34) as:

    P1(s)=1s1sα+1+(112αΓ(α+1)2)1s2α+1+h1,3s3α+1+h1,4s4α+1,
    P2(s)=1sα+1(21αΓ(α+1))1s2α+1+h2,3s3α+1+h2,4s4α+1. (37)

    To get the solution of the system (32) and (33) in the original space, we apply the inverse LT to (37) to get

    ρ1(τ)=1ταΓ(1+α)+(112αΓ(α+1)2)τ2αΓ(1+2α)+h1,3τ3αΓ(1+3α)+h1,4τ4αΓ(1+4α),
    ρ2(τ)=ταΓ(1+α)+(21α+Γ(1+α))τ2αΓ(1+2α)+h2,3τ3αΓ(1+3α)+h2,4τ4αΓ(1+4α). (38)

    We can verify that at α=1, the 5th approximate series solution in (38) becomes as follows:

    ρ61(τ)=1τ+τ33τ46+τ530,
    ρ62(τ)=ττ36+τ5120, (39)

    that coincide with the first six terms of the expansion of the exact solutions.

    Likewise, in this application, the solution that we obtained was analyzed to verify its accuracy by reviewing some graphs and numerical tables. Figures 5(a) and 6(a) show the high agreement between the approximate and exact solution when α=1. Figures 5(b) and 6(b) present the solution in (38) at different values of α, which are 0.5, 0.7 and 1. The curves show that the movement of the particle changes by increasing or decreasing according to the change in the value of α. This confirms what we mentioned earlier: The value of α affects the movement. Figure 7 shows the exact error of the fifth approximation for the solution given in (39) and it seems to be very acceptable mathematically in the period shown.

    Figure 5.  The graphs of (a) the exact solution, ρ1(τ) and the 5th approximate solution, ρ1,5(τ) at α=1, (b) the 5th approximate solution, ρ1,5(τ) at different values of α (α=1,0.7,0.5) using the LRPST.
    Figure 6.  The graphs of (a) the exact solution, ρ2(τ) and the 5th approximate solution, ρ2,5(τ) at α=1, (b) the 5th approximate solution, ρ2,5(τ) at different values of α (α=1,0.7,0.5) using the LRPST.
    Figure 7.  The exact error of (a) the 5th approximate solution, ρ1,5(τ), (b) the 5th approximate solution, ρ2,5(τ) at α=1.

    In the following two tables, Tables 3 and 4, we present two types of errors, exact and residual, related to Application 4.2 for the present approximation and previous approximations prepared by the RPST and HAM methods.

    Table 3.  The exact, Eα=1Ext1(τ) and the residual, Eα=0.5Res1(τ) errors of ρ1,6(τ).
    Eα=1Ext1(τ) Eα=0.5Res1(τ)
    t LRPST HAM(=1) RPST LRPST HAM(=1) RPST
    0.0 0 0 0 0 0 0
    0.2 1.93×108 6.44×108 1.93×108 4.40×104 3.94×104 4.40×104
    0.4 2.35×106 3.79×106 2.35×106 5.40×103 3.72×103 5.40×103
    0.6 3.82×105 3.98×105 3.82×105 2.10×102 1.40×102 2.10×102
    0.8 2.72×104 2.07×104 2.72×104 3.60×102 3.59×102 3.60×102
    1.0 1.23×103 7.38×104 1.23×103 1.09×101 7.49×102 1.09×101

     | Show Table
    DownLoad: CSV
    Table 4.  The exact, Eα=1Ext2(τ) and the residual, Eα=0.5Res2(τ) errors of ρ2,6(τ).
    Eα=1Ext2(τ) Eα=0.5Res2(τ)
    t LRPST HAM(=1) RPST LRPST HAM(=1) RPST
    0.0 0 0 0 0 0 0
    0.2 2.53×109 7.97×1010 2.53×109 2.35×103 3.96×103 2.35×103
    0.4 3.24×107 1.19×107 3.24×107 1.99×102 3.39×102 1.99×102
    0.6 5.52×106 2.40×106 5.52×106 6.90×102 1.20×101 6.90×102
    0.8 4.12×105 2.14×105 4.12×105 1.65×101 2.95×101 1.65×101
    1.0 1.95×104 1.22×104 1.95×104 3.26×101 5.94×101 3.26×101

     | Show Table
    DownLoad: CSV

    The residual errors, EαRes1 and EαRes2, of the approximation in (38) are defined as:

    EαRes1=|Dαρ1,k(τ)+ρ1,k(τ)+eταcos(τα2)ρ2,k(τ2)+2e3τα4cos(τα2)sin(τα4)ρ1,k(τ4)|,
    EαRes2=|Dαρ2,k(τ)eταρ21,k(τ2)+ρ22,k(τ2)|.

    The results in the two tables indicate a perfect match between the results of the methods LRPST and RPST, while the new results are much better than those obtained by the HAM method. Also, we can see from the tables that the LRPST solution converges faster to the exact solution. Although the solution resulting from the methods LRPST and RPST are identical, the steps of the solution using the LRPST are easier and faster to reach the required solution.

    The main goal of this article is to test the applicability of LRPST to solve the FMPS and to determine its efficiency in creating an accurate solution for it. The results indicate the applicability of the proposed method and provide analytical series solutions for the FMPS that are compatible with the exact solutions. Comparisons of the obtained approximate solutions with those previously obtained by HAM or RPST confirm the efficiency of the presented method. Furthermore, the results we got are consistent with those of RPST. It is worth noting that the calculations used in the LRPST were faster and more straightforward compared to the RPST calculations. This is because it is easier to calculate the limit at infinity compared to calculating the Caputo-fractional derivative that we need many times in each step of the RPST. Accordingly, we conclude that LRPST is a powerful and effective method characterized by simplicity and high accuracy in creating analytical series solutions that converge with accurate FMPS solutions. On the other hand, it can be noted that the software (Mathematica 13) was used in calculating symbolic and numerical quantities in this work and that the time taken for the calculation was short compared to other methods.

    As is known, all approximate methods for solving differential equations, whether analytical or numerical, have limits and controls that prevent their application to all equations. The LRPST, like other analytical methods, has conditions when applied that can be summarized in the following points:

    • All of the theories related to LRPST are related to Caputo's definition. If it is used to solve fractional DEs with another fractional derivative concept, the theorems in Section 2 must be reformulated to conform to the new characterization.

    • All functions used in the DEs to be solved must meet the conditions of the Laplace transform.

    • The solution of the target equation plus all its terms must be expandable as a fractional power series.

    Therefore, if all these conditions are met in the DE, the LRPST can solve it. Otherwise, the method fails.

    Based on the foregoing statement, it can be said that there is a need for more research and work to develop the method used to meet the requirements of other types of differential and integral equations, whether they are fractional or integer orders such as nonlinear diffusion-convection fractional equation [32,52], Klien-Gordon equation, Volterra integral equations [53,54] and other equations [55].

    The authors declare they have not used Artificial Intelligence (AI) tools in the creation of this article.

    The authors express their gratitude to the dear referees, who wish to remain anonymous, and the editor for their helpful suggestions.

    The authors declare no conflict of interest.



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