Research article Special Issues

Hopf bifurcation control of the ML neuron model with Hc bifurcation type

  • It is shown that many neurological diseases are caused by the changes of firing patterns induced by bifurcations. Therefore, the bifurcation control may provide a potential therapeutic method of these neurodegenerative diseases. In this paper, we investigate the Hopf bifurcation control of the Morris-Lecar (ML) model with Homoclinic (Hc) bifurcation type by introducing a dynamic state-feedback control. The results indicate that the linear term can change the ML model from Hc bifurcation type to SNIC bifurcation type without changing the firing patterns. The cooperation of linear and cubic term can transform the ML model from the Hc bifurcation type to the Hopf bifurcation type, resulting in the transformation of firing patterns from type I to type II. Besides, we utilize the Poincare Birkhoff (PB) normal form method to derive the analytical expression of the bifurcation stability index for the controlled ML model with Hc bifurcation type, and the results show that the cubic term can regulate the criticality of the Hopf bifurcation. Numerical simulation results are consistent with the theoretical analysis.

    Citation: Qinghua Zhu, Meng Li, Fang Han. Hopf bifurcation control of the ML neuron model with Hc bifurcation type[J]. Electronic Research Archive, 2022, 30(2): 615-632. doi: 10.3934/era.2022032

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  • It is shown that many neurological diseases are caused by the changes of firing patterns induced by bifurcations. Therefore, the bifurcation control may provide a potential therapeutic method of these neurodegenerative diseases. In this paper, we investigate the Hopf bifurcation control of the Morris-Lecar (ML) model with Homoclinic (Hc) bifurcation type by introducing a dynamic state-feedback control. The results indicate that the linear term can change the ML model from Hc bifurcation type to SNIC bifurcation type without changing the firing patterns. The cooperation of linear and cubic term can transform the ML model from the Hc bifurcation type to the Hopf bifurcation type, resulting in the transformation of firing patterns from type I to type II. Besides, we utilize the Poincare Birkhoff (PB) normal form method to derive the analytical expression of the bifurcation stability index for the controlled ML model with Hc bifurcation type, and the results show that the cubic term can regulate the criticality of the Hopf bifurcation. Numerical simulation results are consistent with the theoretical analysis.



    In this paper, we introduce a numerical method based on the spectral collocation method to solve nonlinear fractional quadratic integral equations

    y(x)=a(x)+f(x,y(x))Γ(α)x0(xt)α1g(t,y(t))dt,    α(0,1],   x[0,1], (1.1)

    where Γ() is the gamma function, y(x) is the unknown function and a:[0,1]R is a given function. The functions f and g satisfy the following conditions:

    (1) The functions f, g: [0,1]×RR in (1.1) are continuous and bounded functions with

    M1:=sup(x,y)[0,1]×R|f(x,y)|,   M2:=sup(x,y)[0,1]×R|g(x,y)|.

    (2) The functions f and g satisfy the Lipschitz condition with respect to the second variable, i.e., there exist constants L1>0 and L2>0 such that, for all (x,y1) and (x,y2), we have

    |f(x,y1)f(x,y2)|L1|y1y2|,
    |g(x,y1)g(x,y2)|L2|y1y2|.

    Integral equations are used to model some practical physical problems in the theory of radiative transfer, kinetic theory of gases, neutron transport, and traffic theory [12,17,28,30,33]. Also, some applications in the load leveling problem of energy systems, airfoils and optimal control problems can be found in [24,25,39,40,41]. Existence and uniqueness theorems and some other properties of quadratic integral equations have been studied in [6,16,17,19,48]. So far, various numerical methods for solving quadratic integral equations have been introduced: Adomian decomposition method [17,18,60], repeated trapezoidal methods [18], modified hat functions method [37], piecewise linear functions method [38], Chebyshev cardinal functions method [27], etc.

    Spectral methods are a class of reliable techniques in solving various mathematical modeling of real-life phenomena. The general framework of these methods is based on approximating the solutions of the problems using a finite series of orthogonal polynomials as ciξi, where ξi are called basis functions and can be considered as Legendre, Chebyshev, Hermit, Jacobi polynomials and so on. Spectral methods have been developed to solve various types of fractional differential equations, such as [1,8,14,21,23,44,53,55,59]. The spectral collocation method is a powerful approach that provides high accuracy approximations for the solutions of both linear and nonlinear problems provided that these solutions are sufficiently smooth [9,11,22,58]. The spectral collocation methods based on some extended class of B-spline functions and finite difference formulation have been investigated to find the approximate solutions of time fractional partial differential equations [2,3,4,32,50]. In the last years, the extension of spectral methods based on fractional order basis functions have been developed for solving fractional differential and integral problems [5,20,29,35,52,56,57]. In these works, the authors constructed the fractional order basis functions by writing xxγ, (0<γ<1) in the standard basis functions.

    The Chelyshkov orthogonal polynomials were introduced in [10] and then used to solve various classes of differential and integral equations, mixed functional integro-differential equations [43], weakly singular integral equations [46,52], nonlinear Volttera-Hammerstian integral equations [7], multi-order fractional differential equations [51], two-dimensional Fredholm-Volterra integral equation [49], systems of fractional delay differential equations [36], Volterra-Hammerstein delay integral equations [47]. Some properties of Chelyshkov polynomials can be listed as follows:

    ● The Chelyshkov polynomials CN,n(x) can be expressed in terms of the Jacobi polynomials P(γ,δ)m(x) [9] by the following relation

    CN,n(x)=(1)NnxnP(0,2n+1)Nn(2x1)=Nj=n(1)jn(Nnjn)(N+j+1Nn)xj,  n=0,...N. (1.2)

    In the set {CN,n(x)}Nn=0, every member has degree N with Nn simple roots. Hence, for every N if the roots of the polynomial CN,0(x) are chosen as collocation points, then an accurate numerical collocation method can be derived (for more details see [10]).

    ● The Chelyshkov polynomials (1.2) are orthogonal on the interval [0,1] with respect to the weight function w(x)=1, i.e.,

    10CN,i(x)CN,j(x)dx={0,           ij,12i+1,   i=j.

    About the structure of numerical methods in solving the fractional quadratic integral equations there are various researches, however some of them have not considered the singular behavior of the solutions. Most of these methods that were considered lie in the class of spectral methods and attempt to solve the problem via integer-order polynomial basis. Nevertheless, the obtained numerical solutions do not provide good approximations, and hence the convergence rates of the obtained numerical solutions are not be acceptable. Therefore, these methods cannot be considered as a comprehensive tool in solving fractional integral equations of the form of Eq (1.1) due to the singular behavior of their solutions. These disadvantages motivated us to overcome this drawback by developing a spectral method based on proper basis functions such that covers both smooth and non-smooth solutions of Eq (1.1). In this paper, we introduce a spectral collocation method via implementing a sequence of fractional-order Chelyshkov polynomials as basis functions to produce the numerical solution of Eq (1.1) regarding the singular behavior of the exact solution. These polynomials are constructed by writing xxγ, (0<γ<1) in the standard Chelyshkov polynomials [10]; i.e.,

    ˆCN,n,γ(x):=CN,n,γ(xγ),   n=0,...,N,

    which have both integer and non-integer powers. In this paper, we first convert the Eq (1.1) into a system of integral equation with linear integral operator. Then, the numerical method is implemented to reduce this problem to a set of nonlinear algebraic equations. This allows us to determine the approximate solution of the Eq (1.1) with a high order of accuracy versus results of other numerical methods based on standard orthogonal basis functions.

    The contribution of this paper can be summarized as follows:

    ● In Theorems 4.1 and 4.2, we construct the operational matrices of fractional integration and multiplication based on fractional-order Chelyshkov polynomials with a simple calculative technique that is easy to implement in computer programming.

    ● The upper bound for the error vectors of the operational matrices is discussed in Theorems 4.4 and 4.5.

    ● The proposed numerical method is applied to an equivalent system of integral equations of the form (5.3), which includes a linear integral terms, to reduce the problem to a system of algebraic equations. This method is based on using simple operational matrix techniques so that, unlike other methods, it does not require any discretization, linearization, or perturbation (see Section 5).

    ● The approximate solution is expressed as a linear combination of fractional order terms of the form xiγ such that overcomes the drawback of the poor rate of convergence of the method. The accuracy of the method for solving the Eq (1.1) with non-smooth solutions is confirmed through theoretical and numerical results.

    ● The convergence analysis and numerical stability of the method are investigated.

    The content of this paper is organized as follows: Section 2 contains some necessary definitions that are used in the rest of the paper. The fractional order Chelyshkov polynomials and their properties are investigated in Section 3. The operational matrices of integration and product of the fractional order Chelyshkov polynomials are derived in Section 4. In Section 5, we explain the application of operational matrices with spectral collocation method to obtain the numerical solution of Eq (1.1). The convergence analysis of the method is studied in Section 6. In Section 7, some numerical results are presented to illustrate the accuracy and efficiency of the method. Section 8 is devoted to conclusion and future works.

    In this section, we recall some preliminary results which will be needed throughout the paper. With the development of theories of fractional derivatives and integrals, many definitions appear, such as Riemann-Liouville [45], which are described as follows:

    For uL1[a,b], the Riemann-Liouville fractional integral of order γR+0:=R+{0} is defined as

    Jγau(x)=1Γ(γ)xa(xt)γ1u(t)dt,     γ0. (2.1)

    For γ=0, set J0a:=I, the identity operator. Let u(x)=(xa)β for some β>1 and γ>0. Then

    Jγau(x)=Γ(β+1)Γ(γ+β+1)(xa)γ+β. (2.2)

    Let m=α, the operator Dαa defined by

    Dγau(x)=DmJmγau(x), (2.3)

    is called the Riemann-Liouville fractional differential operator of order γ. For γ=0, set D0a:=I, the identity operator. The Caputo fractional differential operator of order n is defined by

    Dγau(x)=Dγa[u(x)Tm1[u(x);a]], (2.4)

    whenever Dγa[u(x)Tm1[u(x);a]] exists, where Tm1[u(x);a] denotes the Taylor polynomial of degree m1 of the function u around the point a. In the case m=0 define Tm1[u(x);a]:=0. Under the above conditions it is easy to show that,

    Dγau(x)=Jmγau(m)(x). (2.5)

    For more details, see [13,45].

    Theorem 2.1. [42] (Generalized Taylor's formula). Suppose that Dkγ0u(x)C(0,1] for k=0,1,..., N+1. Then, we can write

    u(x)=Ni=0xiγΓ(iγ+1)Diγ0u(0+)+x(N+1)γΓ((N+1)γ+1)D(N+1)γ0u(ξ), (2.6)

    with 0<ξx, x(0,1]. Also, we have

    |u(x)Ni=0xiγΓ(iγ+1)Diγ0u(0+)|MγΓ((N+1)γ+1), (2.7)

    provided that |D(N+1)γ0u(ξ)|Mγ.

    This section includes the definition of fractional Chelyshkov polynomials (FCHPs) and some of its essential properties that will be used in the next sections. The FCHPs on the interval [0,1] are defined as [52]

    ˆCN,n,γ(x)=Nj=n(1)jn(Nnjn)(N+j+1Nn)xjγ,  0<γ<1, n=0,1,...,N. (3.1)

    These polynomials are orthogonal with respect to the weight function w(x)=xγ1:

    <ˆCN,i,γ(x),ˆCN,q,γ(x)>:=10ˆCN,i,γ(x)ˆCN,j,γ(x)w(x)dx={0,           ij,1γ(2i+1),    i=j. (3.2)

    For N=5, we have

    ˆC5,0,γ(x)=6105xγ+560x2γ1260x3γ+1260x4γ462x5γˆC5,1,γ(x)=35xγ280x2γ+756x3γ840x4γ+330x5γˆC5,2,γ(x)=56x2γ252x3γ+360x4γ165x5γˆC5,3,γ(x)=36x3γ90x4γ+55x5γˆC5,4,γ(x)=10x4γ11x5γˆC5,5,γ(x)=x5γ.

    It is shown that, every member in the set {ˆC5,i,γ(x)} has degree 5γ. Figure 1 shows the graphs of these polynomials for γ=12 on the interval [0,1].

    Figure 1.  Plots of ˆC5,i,γ(x) for i=0,...,5 and γ=12.

    Lemma 3.1. The fractional order Chelyshkov polynomial ˆCN,0,γ(x), has precisely N zeros in the form x1γi fori=1,...,N, where xi are zeros of the standard Chelyshkov polynomialCN,0(x) defined in (1.2).

    Proof. The Chelyshkov polynomial CN,0(x) can be written as

    CN,0(x)=(xx1)(xx2)...(xxN).

    Changing the variable x=tγ, yields

    ˆCN,0,γ(t)=(tγx1)(tγx2)...(tγxN),

    so, the zeros of ˆCN,0,γ(t) are

    ti=(xi)1γ,  i=1,...,N.

    Let MN=span{ˆCN,0,α(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x)} be a subspace of the Hilbert space L2[0,1]. Since MN is a finite dimensional space, for every uL2[0,1] there exists a unique best approximation uNMN such that

    uuN2uv2,  vMN,

    and there exist unique coefficients a0,a1,...,aN, such that

    uN(x)=Nn=0anˆCN,n,γ(x)=ˆΦT(x)A=ATˆΦ(x), (3.3)

    where

    A=[a0,a1,...,aN]T,    ˆΦ(x)=[ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x)]T (3.4)

    and

    an=(2n+1)γ10u(x)ˆCN,n,γ(x)w(x)dx. (3.5)

    Lemma 3.2. Suppose that Dkγ0uC(0,1] for k=0,1,...,N, and uN is the bestapproximation of u defined by (3.3). Then, we have

    limNuuN2=0,

    provided that |D(N+1)γ0u(ξ)|Mγ.

    Proof. From Theorem 2.1, we have

    |u(x)Ni=0xiγΓ(iγ+1)Diγ0u(0+)|Mγx(N+1)γΓ((N+1)γ+1). (3.6)

    Due to the fact that uNMN is the best approximation of u, we obtain

    uuN22uNi=0xiγΓ(iγ+1)Diγ0u(0+)22M2γ(Γ((N+1)γ+1))210x2(N+1)γw(x)dx=M2γ(Γ((N+1)γ+1))2(2N+3)γ. (3.7)

    This yields

    limNuˆuN2=0.

    Corollary 3.1. From Lemma 3.2, for the approximate solution uN(x) (3.3), we have the following error bound

    uˆuN2=O(1(Γ((N+1)γ+1))(2N+3)γ). (3.8)

    In this section, we obtain the operational matrix of fractional integration ˆΦ(x) and the one of the product of vectors ˆΦ(x) and ˆΦT(x). These operational matrices have major role in reducing the Eq (1.1) to a system of algebraic equations.

    Theorem 4.1. Let ˆΦ(x) be the FCHPs vector defined in (3.4) and suppose γ(0,1]. Then,

    Jα0ˆΦ(x)PˆΦ(x),

    with P is the (N+1)×(N+1) fractional integral operational matrix and is given by

    P=[Θ(0,0)Θ(0,1)Θ(0,N)Θ(1,0)Θ(1,1)Θ(1,N)Θ(N,0)Θ(N,1)Θ(N,N)],

    where

    Θ(n,k)=Nj=n(1)jn(Nnjn)(N+j+1Nn)Γ(jγ+1)Γ(jγ+α+1)ξj,k, (4.1)

    and

    ξj,k=γ(2k+1)Nl=k(1)lk(j+l+1)γ+α(Nklk)(N+l+1Nk).

    Proof. According to the definition of fractional integral (2.1), we have

    Jα0ˆCN,n,γ(x)=Nj=n(1)jn(Nnjn)(N+j+1Nn)Jα0xjγ=Nj=n(1)jn(Nnjn)(N+j+1Nn)Γ(jγ+1)Γ(jγ+α+1)xjγ+α. (4.2)

    Now, by approximating xjγ+α in terms of ˆΦ(x), we have

    xjγ+αNk=0ξj,kˆCN,k,γ(x), (4.3)

    where

    ξj,k=γ(2k+1)10xjγ+αˆCN,k,γ(x)w(x)dx=γ(2k+1)Nl=k(1)lk(Nklk)(N+l+1Nk)10x(j+l+1)γ+α1dx=γ(2k+1)Nl=k(1)lk(j+l+1)γ+α(Nklk)(N+l+1Nk). (4.4)

    Therefore, we derive from (4.2) and (4.3) that

    Jα0ˆCN,n,γ(x)=Nk=0(Nj=n(1)jn(Nnjn)(N+j+1Nn)Γ(jγ+1)Γ(jγ+α+1)ξj,k)ˆCN,k,γ(x)=Nk=0Θ(n,k)ˆCN,k,γ(x). (4.5)

    This leads to the desired result.

    Theorem 4.2. If V=[v0,v1,...,vN]T, then

    ˆΦ(x)ˆΦT(x)VˆVˆΦ(x), (4.6)

    where

    ˆV=[ˆvi,j]Ni,j=0,   ˆvi,j:=Nl=0vlμi,l,j, (4.7)

    and vl, μi,l,j will be introduced through the proof.

    Proof. Let

    ˆΦ(x)ˆΦT(x)V=[Nj=0vjˆCN,0,γ(x)ˆCN,j,γ(x)Nj=0vjˆCN,1,γ(x)ˆCN,j,γ(x)Nj=0vjˆCN,N,γ(x)ˆCN,j,γ(x)]. (4.8)

    By approximating ˆCN,i,γ(x)ˆCN,j,γ(x) in terms of ˆΦ(x), we have

    ˆCN,i,γ(x)ˆCN,j,γ(x)Nk=0μi,j,kˆCN,k,γ(x), (4.9)

    where

    μi,j,k=γ(2k+1)10ˆCN,i,γ(x)ˆCN,j,γ(x)ˆCN,k,γ(x)w(x)dx. (4.10)

    On the other hand, we can write ˆΦ(x)=DˆX(x), where ˆX(x)=[1,xγ,...,xNγ]T and D is an upper triangular coefficient matrix (see [51] for details). Let Di denote the i-th row of D. Therefore, we achieve

    μi,j,k=γ(2k+1)10ˆCN,i,γ(x)ˆCN,j,γ(x)ˆCN,k,γ(x)w(x)dx=γ(2k+1)10DiˆX(x)ˆXT(x)DTjˆCN,k,γ(x)w(x)dx=Di(γ(2k+1)10ˆX(x)ˆXT(x)ˆCN,k,γ(x)w(x)dx)DTj=DiKDTj, (4.11)

    where K is the (N+1)×(N+1) matrix given by

    [K]r,s=γ(2k+1)10x(r+s)γˆCN,k,γ(x)w(x)dx=γ(2k+1)Nl=k(1)lk(Nklk)(N+l+1Nk)10x(r+s+l+1)γ1dx=(2k+1)Nl=k(1)lkr+s+l+1(Nklk)(N+l+1Nk), (4.12)

    for r,s,k=0,...,N. From (4.8) and (4.9), we obtain

    Nj=0vjˆCN,i,γ(x)ˆCN,j,γ(x)Nj=0vj(Nk=0μi,j,kˆCN,k,γ(x))=Nk=0(Nj=0vjμi,j,k)ˆCN,k,γ(x)=Nk=0ˆvi,kˆCN,k,γ(x), (4.13)

    for i=0,1,...,N. This leads to the desired result.

    Now, we find the upper bound for the error vector of the operational matrix P defined in Theorem 4.1. To this end, first we state the following theorems:

    Theorem 4.3. [31]Suppose that H is a Hilbert space and U=span{u1,u2...,uN} is a closed subspace of H. Let u be an arbitrary element in H and uU be the unique best approximation to uH. Then,

    uu22=G(u,u1,u2,...,uN)G(u1,u2,...,uN),

    where

    G(u,u1,u2,...,uN)=|<u,u><u,u1><u,uN><u1,u><u1,u1><u1,uN><uN,u><uN,u1><uN,uN>|.

    Theorem 4.4. Let

    EI,α(x)=Jα0ˆΦ(x)PˆΦ(x),

    be the error vector of the operational matrix P defined in Theorem 4.1. Then,

    ej,α2Ni=j(Njij)(N+i+1Nj)Γ(iγ+1)Γ(iγ+α+1)(G(xiγ+α,ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x))G(ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x)))1/2

    and

    EI,α20, (4.14)

    where ej,α(x) is the j-th component of EI,α(x) and EI,α2:=(jej,α22)12.

    Proof. We have

    ej,α(x)=Ni=j(1)ij(Njij)(N+i+1Nj)Γ(iγ+1)Γ(iγ+α+1)(xiγ+αNk=0ξk,iˆCN,k,γ(x)), (4.15)

    for j=0,1,...,N. From Theorem 4.3, we can write

    xiγ+αNk=0ξk,iˆCN,k,γ(x)2=(G(xiγ+α,ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x))G(ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x)))1/2. (4.16)

    From (4.15) and (4.16), we obtain

    ej,α2Ni=j(Njij)(N+i+1Nj)Γ(iγ+1)Γ(iγ+α+1)(G(xiγ+α,ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x))G(ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x)))1/2. (4.17)

    By considering the above results and Lemma 3.2, we can conclude that

    EI,α20,   N.

    Theorem 4.5. Let

    EP,α(x)=ˆΦ(x)ˆΦT(x)VˆVˆΦ(x),

    be the error vector of the operational matrix of ˆV defined in Theorem 4.2. Then, a similar proof for EP,α2 can be obtained, since from (4.9) and Theorem 4.3, we have

    ˆCN,i,γ(x)ˆCN,j,γ(x)Nk=0μi,j,kˆCN,k,γ(x)2=(G(ˆCN,i,γ(x)ˆCN,j,γ(x),ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x))G(ˆCN,0,γ(x),ˆCN,1,γ(x),...,ˆCN,N,γ(x)))1/2.

    For example, for N=5, α=γ=12, the following upper bound for components of EI,12(x) can be achieved:

    e0,1222.3639×101,  e1,1221.6885×101,  e2,1228.4424×102,e3,1222.8141×102,  e4,1225.6283×103,  e5,1225.1166×104. 

    Hence,

    EI,1/2(x)[2.3639×1011.6885×1018.4424×1022.8141×1025.6283×1035.1166×104].

    By using the definition of Riemann-Liouville fractional integral in (2.1) we can rewrite the Eq (1.1) in the form

    y(x)=a(x)+f(x,y(x))Jα0g(x,y(x)). (5.1)

    Based on the implicit collocation method [15], let

    w1(x)=f(x,y(x)),   w2(x)=g(x,y(x)). (5.2)

    From Eqs (5.1) and (5.2), we have

    {w1(x)=f(x,a(x)+w1(x)Jα0w2(x)),w2(x)=g(x,a(x)+w1(x)Jα0w2(x)), (5.3)

    The integral operator in (5.3) is linear and therefore application of the operational matrices becomes straightforward. The functions w1(x) and w2(x) can be approximated as follows

    {w1(x)wN,1(x)=Ni=0wi,1ˆCN,i,γ(x)=ˆΦT(x)W1,w2(x)wN,2(x)=Ni=0wi,2ˆCN,i,γ(x)=ˆΦT(x)W2, (5.4)

    where Wi=[wi,0,wi,1,...,wi,N]T are the unknown coefficient vectors for i=1,2. By applying Theorems 4.1 and 4.2, we get

    w1(x)Jα0w2(x)WT1ˆΦ(x)Jα0ˆΦT(x)W2WT1ˆΦ(x)ˆΦT(x)PTW2ˆΦT(x)ˆWT1PTW2. (5.5)

    From (5.4) and (5.5), the system (5.3) can be written as follows:

    {ˆΦT(x)W1f(x,a(x)+ˆΦT(x)ˆWT1PTW2),ˆΦT(x)W2g(x,a(x)+ˆΦT(x)ˆWT1PTW2). (5.6)

    By collocating Eq (5.6) at the points ˆxi=x1γi, the zeros of ˆCN+1,0,γ(x), we obtain the following system of nonlinear algebraic equations

    {ˆΦT(^xi)W1=f(^xi,a(^xi)+ˆΦT(^xi)ˆWT1PTW2),ˆΦT(^xi)W2=g(^xi,a(^xi)+ˆΦT(^xi)ˆWT1PTW2). (5.7)

    This nonlinear system can be solved for the unknown vectors W1 and W2. We employed the "fsolve" command in Maple for solving this system. Finally, the approximate solution of the Eq (1.1) is obtained as follows:

    yN(x)=a(x)+wN,1(x)Jα0wN,2(x). (5.8)

    We present the algorithm of the method which is used to solve the numerical examples:

    Algorithm:

    Input: The numbers α, γ; the functions a(.), f(.,.) and g(.,.).

    Step 1. Choose N and construct the vector basis ˆΦ using relation (3.1).

    Step 2. Compute the operational matrices P and ˆV using Theorems 4.1 and 4.2.

    Step 3. Compute the relation (5.5).

    Step 4. Generate ˆxi for i=0,...,N, the roots of ˆCN+1,0,γ(x) (5.5).

    Step 5. Construct the nonlinear system of algebraic Eq (5.7) by using the nodes ˆxi.

    Step 6. Solve the system obtained in Step 5 to determine the vectors W1 and W2.

    Output: The approximate solution (5.8).

    In this section, we investigate the convergence of the proposed method in the space L2[0,1].

    Theorem 6.1. Assume that wi(x) and wi,N(x) are the exact and approximate solutions of Problems (5.3) and (5.6), respectively, and that Conditions (1) and (2) are satisfied. Then,

    limNei2=0,   i=1,2,

    provided that

    0<(L1+L2)M1<1,    0<(L1+L2)M2<1, (6.1)

    in which ei,N:=wiwi,N are called the error functions.

    Proof. By subtracting (5.6) from (5.3) and using Condition (2), we get

    {|e1,N(x)|L1|w1(x)Jα0w2(x)ˆΦT(x)ˆWT1PTW2|,|e2,N(x)|L2|w1(x)Jα0w2(x)ˆΦT(x)ˆWT1PTW2|. (6.2)

    The Relation (6.2) can be written as

    {|e1,N(x)|L1|w1(x)Jα0w2(x)w1,N(x)Jα0w2,N(x)|+L1|Eα(x)|,|e2,N(x)|L2|w1(x)Jα0w2(x)w1,N(x)Jα0w2,N(x)|+L2|Eα(x)|, (6.3)

    where

    Eα(x)=w1,N(x)Jα0w2,N(x)ˆΦT(x)ˆWT1PTW2.

    From Theorems 4.4 and 4.5, we can conclude that Eα20 as N. Using Condition (1) and the Cauchy-Schwarz inequality, we get

    |w1(x)Jα0w2(x)w1,N(x)Jα0w2,N(x)||w1(x)Jα0w2(x)w1(x)Jα0w2,N(x)+w1(x)Jα0w2,N(x)w1,N(x)Jα0w2,N(x)||w1(x)||Jα0w2(x)Jα0w2,N(x)|+|w1(x)w1,N(x)||Jα0w2,N(x)|M1|Jα0e2,N(x)|+|e1,N(x)||Jα0w2(x)|+|e1,N(x)||Jα0e2,N(x)|M1e2,N2+M2|e1,N(x)|+|e1,N(x)|e22, (6.4)

    therefore, from (6.3) and (6.4), we can write

    {e1,N2L1M1e2,N2+L1M2e1,N2+L1e1,N2,Ne2,N2,e2,N2L2M1e2,N2+L2M2e1,N2+L2e1,N2e2,N2. (6.5)

    By ignoring the term e1e22 in (6.5), we obtain

    e1,N2,N+e2,N2(L1M1+L2M1)e2,N2+(L1M2+L2M2)e1,N2,

    which yields

    (1L1M2L2M2)e1,N2+(1L1M1L2M1)e2,N20.

    Now according to inequalities expressed in (6.1), the proof is complete.

    Theorem 6.2. Suppose that y(x) and yN(x) are the exact solution and approximate solution of Eq (1.1), respectively and that Conditions (1), (2) and Relation (6.1) hold. Then, we have

    limNyyN2=0. (6.6)

    Proof. By subtracting (5.8) from (5.1), we get

    y(x)yN(x)=w1(x)Jα0w2(x)wN,1(x)Jα0wN,2(x).

    Therefore, from Theorem 6.1 we can conclude that (6.6) is valid.

    In this section, we provide some numerical examples to illustrate the efficiency and accuracy of the method. All calculations are performed in Maple 2018. The results are compared to the ones obtained using spectral collocation based on standard Chelyshkov basis polynomials (γ=1) [43], Taylor-collocation method [54] and Chebyshev cardinal functions method [27]. The computational error norm (EN2) is calculated in order to test the accuracy of the method as:

    EN(x):=|y(x)yN(x)|,
    EN2:=Ni=0E2N(xi)N,     (xi=ih,  Nh=1).

    To investigate the numerical stability of the method, we solve the perturbed Eq (1.1) of the form

    y(x)=aϵ(x)+fϵ(x,y(x))Γ(α)x0(xt)α1gϵ(t,y(t))dt,    x[0,1],

    with ϵ=103,106,109.

    Example 7.1. Consider the fractional quadratic integral equation

    y(x)=115sin(x)(πxBesselJ(1,x)15)+y(x)20Γ(1/2)x0(xt)12y(t)dt, (7.1)

    in which BesselJ(,) denotes the Bessel function of the first kind. The exact solution of this problem is y(x)=sin(x). In Table 1, the EN2-errors for γ=14,12 and γ=1 (standard Chelyshkov polynomials [43]) are given, and also the CPU-times are computed. From this table, we see that fractional order basis functions get approximate solutions with higher accuracy than the integer order basis functions.

    Table 1.  Comparison of the EN2-error for different values of γ in Example 7.1.
    γ=14 CPU-Time γ=12 CPU-Time γ=1 CPU-Time
    N=3 2.391962×104 1.326s 1.866606×106 1.124s 2.172051×104 0.811s
    N=5 7.866499×107 2.387s 7.046119×108 2.169s 6.374901×105 1.872s
    N=7 3.493808×108 5.180s 4.002629×1010 4.602s 2.764246×105 4.742s
    N=9 3.942763×109 10.031s 1.252167×1012 9.220s 1.465058×105 8.549s
    N=11 6.300361×1012 21.762s 2.556736×1015 19.984s 8.758143×106 17.316s

     | Show Table
    DownLoad: CSV

    Table 2 presents a comparison between the numerical results given by our method and the ones obtained using Taylor-collocation method [54] and Chebyshev cardinal functions method [27].

    Table 2.  The EN2-error of the our method and [27,54] for Example 7.1.
    Our method (γ=12) Taylor-collocation method [54] Chebyshev cardinal functions method [27]
    N=3 1.866606×106 8.022061×104 -
    N=5 7.046119×108 2.793213×104 5.457252×105
    N=7 4.002629×1010 1.433133×104 3.071930×105
    N=9 1.252167×1012 8.802562×105 1.672349×105
    N=11 2.556736×1015 5.997519×105 8.332697×106

     | Show Table
    DownLoad: CSV

    Figure 2 shows that the spectral accuracy of our method with γ=12 is achieved because the semi-logarithmic representation of the errors has almost similar behavior with the test line (dash-dot line). This line is the semi-logarithmic graph of exp(N).

    Figure 2.  The EN2-errors for different values of N in Example 7.1 with γ=12 (solid lines) and γ=1 (dashed lines).

    In Table 3, we solved the perturbed problem with ϵ=103,106,109 to investigate the stability of our method. The obtained numerical results in this example confirm the high-order rate of convergence and stability of the proposed method, as well as the agreement with the obtained theoretical results.

    Table 3.  The EN2-error of perturbed problem of Example 7.1.
    ϵ N=5 CPU-Time N=9 CPU-Time
    103 7.077009×108 2.246s 1.257245×1012 9.297s
    106 7.046150×108 2.184s 1.252172×1012 9.157s
    109 7.046119×108 2.262s 1.252167×1012 9.220s

     | Show Table
    DownLoad: CSV

    Example 7.2. Consider the fractional quadratic integral equation

    y(x)=x3+140x12+xy(x)5Γ(α)x0(xt)α1ty2(t)dt.

    The exact solution for α=1 is y(x)=x3.

    In this example, we study the applicability of the proposed method when the exact solution does not exist. Table 4 shows the numerical results for N=10 and various values of α, γ. From these results, it is seen that the approximate solution converges to the exact solution as α1. The semi-log representation of errors for different values of N with α=γ=1 confirm the spectral (exponential) rate of convergence of our method in Figure 3.

    Table 4.  The obtained approximate solutions for α=0.7,0.8,0.9,0.95 with γ=α and N=10 in Example 7.2.
    α x x=0.2 x=0.4 x=0.6 x=0.8 x=1 CPU-Time
    γ=α=0.70 8.000000548×103 6.400060857×102 2.160655858×101 5.137819785×101 1.024852816 15.210s
    γ=α=0.80 8.000000046×103 6.400035132×102 2.160379087×101 5.130438155×101 1.014435189 15.319s
    γ=α=0.90 8.000000093×103 6.400015092×102 2.160165000×101 5.124608263×101 1.006347436 15.585s
    γ=α=0.95 8.000000050×103 6.400006977×102 2.160077126×101 5.122168920×101 1.002985209 15.070s
    Exa. sol (α=1) 8.000000000×103 6.400000000×102 2.160000000×101 5.120000000×101 1.0000000000 -

     | Show Table
    DownLoad: CSV
    Figure 3.  The EN2-errors for different values of N in Example 7.2 with α=γ=1.

    Obtaining the analytical solution for integral equations is limited to a certain class of them. Therefore, it is required to derive appropriate numerical methods to solve them. A numerical method based on spectral collocation method is presented for solving nonlinear fractional quadratic integral equations. We used a new (fractional order) version of orthogonal Chelyshkov polynomials as basis functions. Also, the convergence of the method is investigated. The numerical results show the accuracy of the proposed method. Utilizing the new non-integer basis functions produces numerical results with high accuracy. The proposed method for problems on a large interval was not considered. As future work, this limitation may be considered by dividing the domain of the problem into sub-domains and applying the numerical method on them [26,34]. Also, this method can be applied to other kinds of integral equations such as cordial integral equations of quadratic type, quadratic integral equations systems and delay quadratic integral equations.

    The authors declare no conflict of interest.



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