Research article

Factors Associated with Asthma ED Visit Rates among Medicaid-enrolled Children: A Structural Equation Modeling Approach

  • Background: Asthma is one of the leading causes of emergency department visits and school absenteeism among school-aged children in the United States, but there is significant
    local-area variation in emergency department visit rates, as well as significant differences across racial-ethnic groups. Analysis: We first calculated emergency department (ED) visit rates among Medicaid-enrolled children age 5–12 with asthma using a multi-state dataset. We then performed exploratory factor analysis using over 226 variables to assess whether they clustered around three county-level conceptual factors (socioeconomic status, healthcare capacity, and air quality) thought to be associated with variation in asthma ED visit rates. Measured variables (including ED visit rate as the outcome of interest) were then standardized and tested in a simple conceptual model through confirmatory factor analysis. Results: County-level (contextual) variables did cluster around factors declared a priori in the conceptual model. Structural equation models connecting the ED visit rates to socioeconomic status, air quality, and healthcare system professional capacity factors (consistent with our conceptual framework) converged on a solution and achieved a reasonable goodness of fit on confirmatory factor analysis. Conclusion: Confirmatory factor analysis offers an approach for quantitatively testing conceptual models of local-area variation and racial disparities in
    asthma-related emergency department use.

    Citation: Luceta McRoy, George Rust, Junjun Xu. Factors Associated with Asthma ED Visit Rates among Medicaid-enrolled Children: A Structural Equation Modeling Approach[J]. AIMS Medical Science, 2017, 4(1): 71-82. doi: 10.3934/medsci.2017.1.71

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  • Background: Asthma is one of the leading causes of emergency department visits and school absenteeism among school-aged children in the United States, but there is significant
    local-area variation in emergency department visit rates, as well as significant differences across racial-ethnic groups. Analysis: We first calculated emergency department (ED) visit rates among Medicaid-enrolled children age 5–12 with asthma using a multi-state dataset. We then performed exploratory factor analysis using over 226 variables to assess whether they clustered around three county-level conceptual factors (socioeconomic status, healthcare capacity, and air quality) thought to be associated with variation in asthma ED visit rates. Measured variables (including ED visit rate as the outcome of interest) were then standardized and tested in a simple conceptual model through confirmatory factor analysis. Results: County-level (contextual) variables did cluster around factors declared a priori in the conceptual model. Structural equation models connecting the ED visit rates to socioeconomic status, air quality, and healthcare system professional capacity factors (consistent with our conceptual framework) converged on a solution and achieved a reasonable goodness of fit on confirmatory factor analysis. Conclusion: Confirmatory factor analysis offers an approach for quantitatively testing conceptual models of local-area variation and racial disparities in
    asthma-related emergency department use.


    In the past few decades, more and more diffusion processes have been shown to not satisfy Fickian laws, such as signal transduction in biological cells, foraging behavior of animals, viscoelastic and viscoplastic flow, and solute migration in groundwater. However, fractional partial differential equations (FPDEs) play a very important role in describing anomalous diffusion Ref. [1,2,3], so in recent years, FPDEs have attracted extensive attention. In this paper, we study one type of time-fractional diffusion equation (TFDE), which can be obtained from the standard diffusion equation by replacing the first-order time derivative with a fractional derivative of order α, 0<α<1.

    {Dαtu(x,t)=uxx(x,t)+f(x,t),(x,t)(0,b)×(0,T],u(x,0)=u0(x),x[0,b],u(0,t)=0),u(b,t)=0,t[0,T]. (1.1)

    Where u0(x) is a smooth function and Dαtu(x,t) is the Caputo fractional derivative defined by Definition 2.1.

    The exact solutions of most fractional differential equations are difficult to obtain analytically, and even if they can be obtained, most of them contain special functions that are difficult to calculate. In recent years, many numerical methods have been proposed. For example, Ref. [4,5] used finite difference to solve the fractional diffusion equation. Yang et al. [6] used the finite volume method to solve the nonlinear fractional diffusion equation. Jin et al. studied the finite element method for solving the homogeneous fractional diffusion equation in [7]. Some scholars have developed meshless methods [8,9,10,11] and spectral methods [12,13,14,15] to solve fractional diffusion equations.

    The reproducing kernel space and its related theories are the ideal spatial framework for function approximation [16,17]. The function approximation in this space has uniform convergence, while the Caputo-type fractional derivative of the approximate function still has uniform convergence. Therefore, the reproducing kernel space is also the ideal spatial framework for the numerical processing of Caputo-type fractional derivatives. Numerical solutions to differential equations based on orthogonal polynomials are commonly used. For example, quartic splines and cubic splines are used, respectively, to solve numerical solutions of differential equations in Ref. [18,19,20]. In Ref. [21,22,23], based on the idea of wavelet, a multi-scale orthonormal basis is constructed in the reproducing kernel space by using piecewise polynomials, and ε-approximate solutions of integer-order differential equations are obtained.

    For TFDE, most methods use the finite difference method to deal with time variables. Due to the non-singularity of fractional differentiation, the difference scheme at the initial time needs to be further transformed. And the results are not ideal; when the step size reaches 0.001, the error is only 105 in Ref. [10]. So, the main motivation of this paper is to obtain the ε-approximation solution of TFDE. By constructing a multiscale orthonormal basis in the multiple reproducing kernel space, a numerical algorithm is designed to obtain the approximate solution of TFDE. In order to avoid the influence of fractional non-singularity, this paper constructs the orthonormal basis by using Legendre polynomials, which can be operated by the property of fractional differentiation. In addition, the method in this paper has a good convergence order.

    The paper is organized as follows: In Section 2, the fundamental definitions are provided, and Legendre polynomials and related spaces are introduced. In Section 3, the ε-approximation solutions are given. In Section 4, convergence analysis and time complexity are presented for the proposed method. In Section 5, numerical solutions for several fractional diffusion equations are presented. The paper concludes by stating the advantages of the method.

    In this section, the Caputo fractional derivative and its properties are introduced. Legendre polynomials and their associated spaces are also discussed. This knowledge will be used when constructing the basis.

    Definition 2.1. The Caputo fractional derivative is defined as follows [24]:

    Dαtu(t)=1Γ(nα)t0(ts)nα1u(n)(s)ds,n=[α]+1,n1<α<n.

    For ease of calculation, a property of the Caputo differential needs to be given here.

    Property 2.1.

    Dα(tγ)={Γ(γ+1)Γ(γ+1α)tγα,γ0,0,γ=0. (2.1)

    Proof. According to the definition of Caputo differentiation, the conclusion can be obtained using integration by parts.

    Legendre polynomials are known to be orthogonal on L2[1,1]. Since the variables being analyzed are often defined in different intervals, it is necessary to transform Legendre polynomials on [0,b]. Legendre polynomials defined on [0, b] are shown below

    l0(x)=1,l1(x)=2xb1,lj+1(x)=2j+1j+1(2xb1)lj(x)jj+1lj1(x),j=1,2,

    Clearly, {lj(x)}j=0 is orthogonal on L2[0,b], and

    bxli(x)lj(x)dx={b2j+1,i=j,0,ij.

    Let pj(x)=2j+1blj(x), {pj(x)}j=0 is an orthonormal basis on L2[0,b].

    Consider Eq (1.1); this section gives the following reproducing kernel space. For convenience, the absolutely continuous function is denoted as AC.

    Definition 2.2. W1[0,T]={u(t)u(0)=0,uisAC,uL2[0,T]}, and

    u,vW1=T0uvdt,u,vW1[0,T].

    If b=T and Tj(t)=pj(t), note that Tj(t)=jk=0cktk. Let

    J0Tj(t)=t0Tj(τ)dτ=jk=0cktk+1k+1.

    Theorem 2.1. {J0Tj(t)}j=0 is an orthonormal basis on W1[0,T].

    Definition 2.3. W2[0,b]={u(x)u(0)=u(b)=0,uisAC,uL2[0,b]}, and

    u,vW2=b0uvdx,u,vW2[0,b].

    Similarly, denote pj(x)=jk=0dkxk. Integrating pj(x) twice yields J20pj(x), if J20pj(x)W2[0,b], then

    J20pj(x)=jk=0dkxk+2bk+1x(k+1)(k+2).

    Obviously, {J20pj(x)}j=0 is an orthonormal basis on W2[0,b].

    Put Ω=[0,b]×[0,T], and let's define the space W(Ω).

    Definition 2.4. W(Ω)={u(x,t)u(x,0)=0,u(0,t)=u(b,t)=0,ux is continuous functions, 3utx2L2(Ω)}.

    Clearly, W(Ω) is an inner product space, and

    u,vW(Ω)=Ω3utx23vtx2dσ,u,vW(Ω).

    Theorem 2.2. If u(x,t),v(x,t)W(Ω), and v(x,t)=v1(x)v2(t), then

    u,vW(Ω)=u,v2W1,v1W2=u,v1W2,v2W1.

    Proof. Clearly,

    u,vW(Ω)=Ω3utx23vtx2dσ=Ωt(2ux2)v2t2v1x2dσ=b02x2(u,v2W1)2v1x2dx=u,v2W1,v1W2.

    Similarly, u,vW(Ω)=u,v1W2,v2W1.

    Note

    ϕij(x,t)=J20pi(x)J0Tj(t),i,j=0,1,2,.

    Theorem 2.3. {ϕij(x,t)}i,j=0 is an orthonormal basis on W(Ω).

    Proof. First of all, orthogonality. For ϕij(x,t),ϕmn(x,t)W(Ω), according to Theorem 2.2,

    ϕij(x,t),ϕmn(x,t)W(Ω)=J20pi(x),J20pm(x)W2J0Tj(t),J0Tj(t)W1={1,i=m,j=n,0,others.

    Second, completeness. uW(Ω), if u,ϕijW(Ω)=0 means u0. In fact, by Theorem 2.4,

    u,ϕijW(Ω)=u,J20pi(x)J0Tj(t)W(Ω)=u,J20pi(x)W2,J0Tj(t)W1=u,J0Tj(t)W1,J20pi(x)W2=0.

    Since {J20pi(x)}i=0 and {J0Tj(t)}j=0 are complete systems of W2[0,b] and W1[0,T], respectively, u,J20pi(x)W2=0 and u,J0Tj(t)W1=0. So u0.

    Let L:W(Ω)L2(Ω),

    Lu=Dαtuuxx.

    Then Eq (1.1) is

    Lu=f. (3.1)

    Theorem 3.1. Operator L is a bounded and linear operator.

    Proof. Clearly, L is linear, and one only needs to prove boundedness. According to Cauchy Schwartz's inequality, we derive that

    LuL2DαtuL2+uxxL2.

    Put K(x,t,y,s)=r(x,y)q(t,s) be the RK function in W(Ω), then

    |uxx|=|u(x,t),2Kx2W(Ω)|=|u(x,t),2r(x,y)x2q(t,s)W(Ω)|2r(x,y)x2q(t,s)W(Ω)uW(Ω). (3.2)

    Similarly

    |ut|q(t,s)tr(x,y)W(Ω)uW(Ω). (3.3)

    By Eq (3.2), there exists positive constants M1 such that

    uxx2L2=Ω(uxx)2dσ2r(x,y)x2q(t,s)2W(Ω)SΩu2W(Ω)=M1u2W(Ω), (3.4)

    where M1=2r(x,y)x2q(t,s)2W(Ω)SΩ, SΩ represents the area of the region Ω.

    By Eq (3.3), there exist positive constants M2,M3, such that

    |Dαtu|=|1Γ(1α)t0(ts)αut(x,s)ds|1Γ(1α)t0(ts)α|ut(x,s)|ds1Γ(1α)t0(ts)αq(t,s)tr(x,y)W(Ω)uW(Ω)dsuW(Ω)Γ(1α)q(t,s)tr(x,y)W(Ω)t0(ts)αdst1αΓ(2α)q(t,s)tr(x,y)W(Ω)uW(Ω)=M2uW(Ω),

    and

    Dαtu2L2=Ω(Dαtu)2dσM22SΩu2W(Ω)=M3u2W(Ω). (3.5)

    From Eqs (3.4) and (3.5), we can get

    LuL2MuW(Ω),

    where M=M1+M3.

    Definition 3.1. uε is named the ε-approximate solution for Eq (3.1), ε>0, if

    Luεf2L2<ε2.

    Ref. [21,22] proved the existence of εapproximate solutions to boundary value problems of linear ordinary differential equations. Using the same method, we can prove that the ε-approximate solution of Eq (3.1) exists.

    Theorem 3.2. ε>0, N1,N2>0, when n1>N1,n2>N2,

    uεn1n2(x,t)=n1i=0n2j=0cijϕij(x,t)

    is the ε-approximate solution of Eq (3.1), where cij satisfies

    n1i=0n2j=0cijLϕij(x,t)f(x,t)2L2=mincijn1i=0n2j=0cijLϕij(x,t)f(x,t)2L2.

    Proof. Let u(x,t) be the solution of Eq (3.1),

    u(x,t)=i=0j=0cijϕij(x,t),

    where cij=u,ϕijW(Ω), and un1n2(x,t)=n1i=0n2j=0cijϕij(x,t).

    Because L is a bounded operator, ε>0, N1,N2>0, when n1>N1,n2>N2,

    uun1n22W(Ω)=i=n1+1j=n2+1cijϕij(x,t)2W(Ω)εL2,

    so

    Luεn1n2f2L2=n1i=0n2j=0cijLϕijf2L2=mindijn1i=0n2j=0dijLϕijf2L2n1i=0n2j=0cijLϕijf2L2Lun1n2Lu2L2L2un1n2u2L2ε.

    From Theorem 3.2, note

    J(c00,c01,c02,,cN1N2)=n1i=0n2j=0cijLϕij(x,t)f(x,t)2L2,

    J is a quadratic form about c=(cij)n1,n2i,j=0, and c=(cij)n1,n2i,j=0 is the minimum value of J. To find c, just need Jcij=0. That is

    Jcij=2n1i=0n2k=0cikLϕij,LϕklL22cijLϕij,fL2,

    so

    n1i=0n2k=0cikLϕij,LϕklL2=Lϕij,fL2. (3.6)

    Put N=(n1+1)×(n2+1), and the N-order matrix A and the N-order vector b,

    A=(Lϕij,LϕklL2)N×N,b=(Lϕij,fL2)N,

    so Eq (3.6) is

    Ac=b. (3.7)

    From Property 2.1,

    Lϕij=Dαtϕij2ϕijx2=J20pi(x)DαtJ0Tj(t)pi(x)J0Tj(t)=J20pi(x)jk=0ckk+1Γ(k+2)tk+1αΓ(k+2α)pi(x)J0Tj(t).

    From Ref. [21], if L is reversible, then Eq (3.7) exists and is unique.

    Let u(x,t) be the exact solution to Eq (3.1), and

    u(x,t)=i=0j=0cijϕij(x,t).

    Fourier truncation of u(x,t) is uN1,N2(x,t), and

    uN1N2(x,t)=N1i=0N2j=0cijϕij(x,t).

    In Ref. [25], if u(m)(x)L2[0,b], then

    uunL2Cnm(mk=min{m,n+1}u(k)2L2)12. (4.1)

    Theorem 4.1. Assume m+nu(x,t)tmxnL2(Ω), then

    u(x,t)uN1(x,t)W(Ω)C1Nm1,u(x,t)uN2(x,t)W(Ω)C2Nn2,

    where C1,C2 are constants.

    Proof. Recalling the definition of W(Ω), we get

    u(x,t)uN1(x,t)2W(Ω)=Ω3(uuN1)tx23(uuN1)tx2dxdt=b0T0t(2(uuN1)x2)t(2(uuN1)x2)dtdx=b02ux22uN1x22W1dx.

    According to Eq (4.1), it follows that

    2ux22uN1x2W1=3ux2t3uN1x2tL2[0,T]C(x)Nm1(mk=min{m,N1+1}u(k+1)xx2L2[0,T])1/2,

    so

    u(x,t)uN1(x,t)2W(Ω)b0C2(x)N2m1(mk=min{m,N1+1}u(k+1)xx2L2[0,T])dxN2m1b0C2(x)(mk=min{m,N1+1}u(k+1)xx2L2[0,T])dxC0N2m1,

    where C0=baC2(x)(mk=min{m,N1+1}u(k+1)xx2L2[0,T])dx. Assume C1=C0; that is

    u(x,t)uN1(x,t)W1C1Nm1.

    Similarly,

    u(x,t)uN2(x,t)W(Ω)C2Nn2.

    Theorem 4.2. Assume m+nw(x,t)tmxnL2(Ω), uεN1N2(x,t) is the approximate solution of Eq (3.1), then

    u(x,t)uεN1N2(x,t)W(Ω)CNγ,

    where C=2M2max{C1,C2}, N=min{N1,N2}, and γ=min{m,n}.

    Proof. We know

    u(x,t)uεN1,N2(x,t)W(Ω)=L1Lu(x,t)uN1,N2(x,t)W(Ω)M2N1i=0j=N1+1cijϕij(x,t)+i=N1+1j=0cijϕij(x,t)W(Ω)=M2(N1i=0j=N1+1c2ij+i=N1+1j=0c2ij),

    where M2=L1L. Moreover,

    u(x,t)uN1(x,t)W(Ω)=i=0j=0cijϕij(x,t)N1i=0j=0cijϕij(x,t)W(Ω)=i=N1+1j=0cijϕij(x,t)W(Ω)=i=N1+1j=0c2ij.
    u(x,t)uN2(x,t)W(Ω)=i=0j=0cijϕij(x,t)i=0N2j=0cijϕij(x,t)W(Ω)=i=0j=N2+1cijϕij(x,t)W(Ω)=i=0j=N2+1c2ij.

    So

    u(x,t)uεN1,N2(x,t)W(Ω)M2(N1i=0j=N1+1c2ij+i=N1+1j=0c2ij)M2(i=0j=N1+1c2ij+i=N1+1j=0c2ij)=M2(u(x,t)uN2(x,t)W(Ω)+u(x,t)uN1(x,t)W(Ω))M2(C1Nm1+C2Nn2)CNγ.

    So, the proposed method is γ-order convergence, and the convergence rate depends on N.

    The proposal of an algorithm requires not only a reliable theory but also the feasibility of calculation. The huge calculation process is costly. Next, the time complexity of the algorithm will be analyzed.

    According to the analysis in Section 3, the complexity of the algorithm depends on Eqs (3.6) and (3.7). Next, the algorithm can be illustrated in four steps, as follows:

    (1) A of Eq (3.7). We know A=(Lϕij,LϕklL2)N×N, and

    Lϕij,LϕklL2=10J20pi(x)J20pk(x)dx10J0Tj(t)J0Tl(t)dt.

    Set the number of multiplications required to compute Lϕij,LϕklL2 as C1, where C1 is constant. Clearly, the computing time needed for A is Num1=C1N2.

    (2) b of Eq (3.7). We know b=(Lϕij,fL2)N×N, and

    Lϕij,fL2=1010J20pi(x)J0Tj(t)dtdx.

    Set the number of multiplications required to compute Lϕij,fL2 as C2, where C1 is constant. Clearly, the computing time needed for b is Num2=C2N.

    (3) We use the Gaussian elimination method to solve Eq (3.7). From my mathematical knowledge, Gaussian elimination requires operations

    Num3=N(N+1)(2N+1))6.

    (4) To the εapproximation solution uεN(x,t), the number of computations is N.

    In summary, the multiplication times of this algorithm in the execution process are

    Num=Num1+Num2+Num3+N=O(N3).

    This section discusses three numerical examples to reveal the accuracy of the proposed algorithm. Compared with Ref. [26,27,28,29], the results demonstrate that our method is remarkably effective. All the results are calculated using the mathematical software Mathematica 13.0.

    In this paper, N=N1×N2 is the number of bases, and eN(x)=|u(x)uN(x)| is the absolute error. MEN denotes the maximum absolute error when the number of bases is N. The convergence order can be calculated as follows:

    C.R.=LogNMmax|eM|max|eN|.

    Example 5.1. Consider the test problem suggested in [26,27]

    {Dαtu(x,t)=uxx(x,t)+f(x,t),(x,t)(0,1)×(0,1],u(x,0)=0,x(0,1),u(0,t)=0,u(1,t)=0,

    where f(x)=3π4Γ(2.5α)x4(x1)t1.5α(20x312x2)t1.5, and the analytical solution is given by u(x,t)=x4(x1)t1.5. The numerical results are shown in Tables 1 and 2. Table 1 shows that when α is 0.5 or 0.8, respectively, our results are better than those in Ref. [26,27]. Meanwhile, we also show the results when α=0.01 and α=0.99 in Table 1 and find that the results are not much different from those when a = 0.5 and a = 0.8, demonstrating the robustness of our method. Table 2 indicates that the absolute error gets better as the number of bases increases. Figures 1 and 2 shows the absolute errors when α=0.01 and α=0.99, respectively. Figures 3 and 4 show the absolute errors at different times when α=0.01 and α=0.99.

    Table 1.  The absolute error of Example 5.1.
    α(t) MEN in [26] MEN in [27] ME36 ME64
    0.5 8.82×104 1.99×104 1.41×105 4.18×106
    0.8 8.50×104 1.87×104 7.16×106 4.61×106
    0.01 1.43×105 4.09×106
    0.99 2.95×105 6.03×106

     | Show Table
    DownLoad: CSV
    Table 2.  C.R. of Example 5.1.
    n α=0.5 C.R. α=0.8 C.R.
    9 8.08×103 7.75×103
    16 6.07×104 4.50 6.12×105 8.41
    25 2.75×105 6.93 2.76×105 1.78
    36 1.41×105 1.83 1.41×105 1.84
    49 8.10×106 1.80 8.04×106 1.82
    64 4.18×106 2.48 4.61×106 2.08

     | Show Table
    DownLoad: CSV
    Figure 1.  Example 5.1, N=64,α=0.01.
    Figure 2.  Example 5.1, N=64,α=0.99.
    Figure 3.  Example 5.1, N=64,α=0.01,t.
    Figure 4.  Example 5.1, N=64,α=0.99,t.

    Example 5.2. We consider the same FDEs as that in [28]

    {Dαtu(x,t)=uxx(x,t)+f(x,t),(x,t)(0,1)×(0,1],u(x,0)=0,x(0,1),u(0,t)=0,u(1,t)=0.

    With f(x,t)=2Γ(3α)t2αsin(2πx)+4π2t2sin(2πx), the exact solution of the problem is given by u(x,t)=t2sin(2πx). Tables 35, respectively, show the comparison of absolute error and convergence order with Ref. [28] when α is 0.2, 0.5, or 0.8. Obviously, the proposed method is superior to Ref. [28]. N×L denotes the number of bases in Ref.[28].

    Table 3.  The MEN and C.R. of Example 5.2, α=0.2,L=10000.
    [28] Our method
    N×L ME C.R. N1×N2 MEN C.R.
    25×L 2.06×106 4.00 4×8 1.95×105
    30×L 1.00×106 4.00 4×10 3.11×107 18.54
    35×L 5.39×107 4.00 4×12 2.72×109 25.99
    40×L 3.15×107 4.01 4×14 3.21×1011 28.79

     | Show Table
    DownLoad: CSV
    Table 4.  The MEN and C.R. of Example 5.2, α=0.5,L=20000.
    [28] Our method
    N×L ME C.R. N1×N2 MEN C.R.
    25×L 2.65×106 4.01 4×8 1.95×105
    30×L 9.96×107 4.03 4×10 3.10×107 18.56
    35×L 5.35×107 4.06 4×12 3.72×109 24.25
    40×L 3.11×107 4.11 4×14 1.29×1010 36.74

     | Show Table
    DownLoad: CSV
    Table 5.  The MEN and C.R. of Example 5.2, α=0.8,L=60000.
    [28] Our method
    N×L ME C.R. N1×N2 MEN C.R.
    25×L 2.03×106 4.13 4×8 1.93×105
    30×L 9.65×107 4.30 4×10 3.08×107 18.54
    35×L 5.04×107 4.61 4×12 3.08×109 24.69
    40×L 2.85×107 5.18 4×14 4.80×1010 13.11

     | Show Table
    DownLoad: CSV

    Example 5.3. Considering the following problem with f(x,t)=Γ(4+α)6sin(πx)+π2t3+αsin(πx)+πt3+αcos(πx) [29]:

    {Dαtu(x,t)=uxx(x,t)ux+f(x,t),(x,t)(0,1)×(0,1],u(x,0)=0,x(0,1),u(0,t)=0,u(1,t)=0.

    The exact solution of the problem is given by u(x,t)=t3+αsin(πx). Table 6 shows the comparison of absolute error and convergence order with Ref. [29] when α is 0.1. Obviously, the proposed method is superior to Ref. [29]. Figures 57 show the absolute errors when α=0.1, α=0.01 and α=0.99 respectively.

    Table 6.  The MEN and C.R. of Example 5.3, α=0.1.
    [29] Our method
    N×L ME C.R. N1×N2 MEN C.R.
    20×20 1.44×103 3×3 1.40×103
    40×40 3.66×104 1.98 5×5 1.83×105 4.01
    80×80 9.15×105 1.98 7×7 2.89×106 3.09
    160×160 2.31×105 1.98 9×9 2.83×107 4.62

     | Show Table
    DownLoad: CSV
    Figure 5.  Example 5.3, N=81,α=0.1.
    Figure 6.  Example 5.3, N=54,α=0.01.
    Figure 7.  Example 5.3, N=54,α=0.99.

    In this paper, an effective numerical algorithm based on Legendre polynomials is proposed for TFDE. Based on Legendre polynomials, an orthonormal basis is constructed in the reproducing kernel spaces W1[0,1] and W2[0,b]. Then we define the multiple reproducing kernel space and develop the orthonormal basis in this space. The ε-approximate solution of TFDE is obtained. From the above analysis and the numerical examples, it is clear that the presented method is successfully employed for solving TFDE. The numerical results show that our method is much more accurate than other algorithms. In this paper, because the orthonormal basis constructed in the binary reproducing kernel space contains power terms, the properties of fractional differentiation can be used to calculate fractional differentiation, so as to eliminate the influence of the non-singularity of fractional differentiation. However, the method presented in this paper is suitable for the case where the initial boundary value condition is 0, and for the non-zero case, it needs to be further simplified to the cases where the initial boundary value condition is 0. We are also trying to design methods for cases where initial boundary values are non-zero.

    Yingchao Zhang: Conceived of the study, designed the study, and proved the convergence of the algorithm; Yingzhen Lin: Reviewed the full text. All authors were involved in writing the manuscript. All authors read and approved the final manuscript.

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

    This study was supported by the Characteristic Innovative Scientific Research Project of Guangdong Province (2023KTSCX181, 2023KTSCX183) and Basic and Applied Basic Research Project Zhuhai City (2320004002520)

    The authors have no conflicts of interest to declare.

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