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A posteriori error estimates of spectral method for the fractional optimal control problems with non-homogeneous initial conditions

  • In this paper we consider an optimal control problem governed by a space-time fractional diffusion equation with non-homogeneous initial conditions. A spectral method is proposed to discretize the problem in both time and space directions. The contribution of the paper is threefold: (1) A discussion and better understanding of the initial conditions for fractional differential equations with Riemann-Liouville and Caputo derivatives are presented. (2) A posteriori error estimates are obtained for both the state and the control approximations. (3) Numerical experiments are performed to verify that the obtained a posteriori error estimates are reliable.

    Citation: Xingyang Ye, Chuanju Xu. A posteriori error estimates of spectral method for the fractional optimal control problems with non-homogeneous initial conditions[J]. AIMS Mathematics, 2021, 6(11): 12028-12050. doi: 10.3934/math.2021697

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  • In this paper we consider an optimal control problem governed by a space-time fractional diffusion equation with non-homogeneous initial conditions. A spectral method is proposed to discretize the problem in both time and space directions. The contribution of the paper is threefold: (1) A discussion and better understanding of the initial conditions for fractional differential equations with Riemann-Liouville and Caputo derivatives are presented. (2) A posteriori error estimates are obtained for both the state and the control approximations. (3) Numerical experiments are performed to verify that the obtained a posteriori error estimates are reliable.



    The subject of fractional calculus has gained considerable popularity and importance during the past three decades, due to, on one side, its well-recognized applicability in diverse and widespread fields of science and engineering, and on the other side, its attractive complementary of the integer order calculus in mathematical sciences. Interested reader in fractional calculus and fractional partial differential equations (FPDEs) can refer to [1,2,3].

    In recent years the research of optimal control problem governed by FPDEs has formed a hot topic not only in theoretical investigation, but also in numerical methods. In [4,5] the authors discussed the wellposedness of optimal control problem governed by time fractional diffusion equation with control constraint and state constraint, respectively. The authors in [6,7,8,9] studied the finite element method for optimal control problem governed by the fractional Laplace equation, the prior error estimate and the posterior error estimate were derived. A spectral Galerkin approximation of optimal control problem governed by Riesz fractional differential equation was investigated in [10]. The integral definition of the fractional Laplacian and a linear-quadratic optimal control problem for the fractional heat equation with control constraints were analyzed in [11]. Finite element method for optimal control problem for a fractional semilinear PDE with control constraints was studied in [12]. Numerical method for solving a class of fractional optimal control problems with canonical equality and inequality constraints was considered in [13,14]. Li et al. [15] presented a numerical method for solving nonlinear fractional optimal control problems with multiple states and controls. A spectral optimization methods for the time fractional diffusion inverse problem was discussed in [16]. Spectral Galerkin approximation of time fractional optimal control problems with integral constraint on the state was studied in [17]. Du et al. [18] studied the optimal control problem of fractional diffusion equations based on the finite difference fast projection gradient algorithm. Wu and Huang [19] introduced a time parallel algorithm to solve the optimal control problem of fractional diffusion equation in order to reduce the computation time. Also we refer the interested reader in optimal control problem for FPDEs to see [20,21,22,23,24,25] and its references for some recent works in the subject.

    To the best of our knowledge, only few attempts have been made to develop the posteriori error estimation for problems involving fractional derivative, especially the one for optimal control problem governed by FPDEs. An a posteriori error analysis for an optimal control problem involving the fractional Laplacian was introduced in [7]. An a posteriori error estimator for PDE constrained optimization problem involving a nondifferentiable cost functional, fractional diffusion, and control-constraints was proposed and analyzed in [26]. In an earlier work of Ye and Xu [27], a posteriori error estimates for spectral method was carried out for the fractional optimal control problem governed by the time fractional diffusion equation with Riemann-Liouville fractional derivative. It is known within the community of fractional calculus that with the Riemann-Liouville definition, only homogeneous conditions (under an integral form) is possible. As an extension of the above mentioned paper [27], in this work we shall mainly be interested in a posteriori error estimates for the fractional optimal control problem with non-homogeneous conditions. As we are going to see, the non-homogeneous case presents a considerable difference on the solution property, and introduces additional non-trivial difficulties into the analysis of the a posteriori error of the optimal control problem.

    The literature reports several definitions for the fractional derivative, including the expressions derived by Riemann-Liouville, Caputo, Riesz, Riesz-Caputo, Grunwald-Letnikov, Hadamard, and so on. Although the way to impose suitable initial conditions for different definitions has been discussed in the literature, there are still some issues need to be clarified. We will focus on the initial value problem for Riemann-Liouville and Caputo fractional differential equations in Section 2, where some new initial conditions are derived. Besides, as compared to the posteriori error analysis in [27], the presence of a singular term tα in the right hand side of the state equation associated to the non-homogeneous initial condition leads to additional difficulties. Hence special techniques such as Embedding Theorem should be adopt to achieve reliable a posteriori error estimator.

    The rest of this paper is organized as follows. In Section 2, we discuss the issue about the initial condition for Riemann-Liouville and Caputo fractional ordinary differential equation, and propose a consistent way to impose the "well-defined" initial condition. The formulation of the optimal control problem with non-homogeneous initial conditions and the optimality conditions are presented in Section 3. Section 4 describes the spectral discretization of the optimal control problem. In Section 5, we establish the main result on the posteriori error analysis for the considered problem. Numerical experiment is presented in Section 6, showing that the posteriori error estimates are reliable. Some concluding remarks are given at the end of the paper.

    In this section we discuss the issue how to correctly impose initial conditions for the time fractional differential equations involving Riemann-Liouville and Caputo fractional derivatives, respectively.

    Let I=(0,T),T>0. We begin with the following fractional differential equation:

    RDαtu(t)=f(t),  tI, (2.1)

    where RDαt is the Riemann-Liouville fractional differential operator of order α given by

    RDαtv(t)=ddtI1αtv(t)=1Γ(1α)ddtt0v(τ)(tτ)αdτ,  tI.

    The following initial condition of integral form

    limt0I1αtu(t)=u0 (2.2)

    for a given u0 should be provided to guarantee the uniqueness of the solution, where 0<α<1, Iαt is the Riemann-Liouville fractional integral operator of order α defined by

    Iαtv(t)=1Γ(α)t0v(τ)(tτ)1αdτ.

    In fact, a direct calculation using [3, Lemma 5.2] gives the expression of the solution to (2.1):

    u(t)=tα1Γ(α)limt0+I1αtu(t)+1Γ(α)t0f(τ)dτ(tτ)1α. (2.3)

    Clearly, the solution uniquely exists subject to the condition (2.2). This is in agreement with the common sense in two extreme cases: α1 and α0. In the former case, it was shown [1]:

    1Γ(1α)t0u(τ)dτ(tτ)αu(t),   α1. (2.4)

    Thus the Eq (2.1) becomes

    u(t)=f(t),  tI,

    and the initial condition (2.2) becomes

    u(0)=u0. (2.5)

    In the latter case, i.e., α0, it can be easily verified from (2.3) that u(t)f(t) for integrable f.

    One of the main inconveniences with the Eq (2.1) is that there will be not much choice in imposing a well-defined initial condition u0 for 0<α<1. In fact, it has been shown in [28] the following lemma.

    Lemma 2.1. [28] If  0<α<1/2,uL2(I), or if  1/2α<1, uHs(I), α1/2<s<1/2, then it holds

    limt0I1αtu(t)=0.

    This means there will not be a solution in L2(I) for 0<α<1/2 or in Hs(I),α1/2<s<1/2 for 1/2α<1 if u00. In other words, the initial condition (2.2) has to be homogeneous if we want a reasonably regular solution.

    In order to be able to use non-homogeneous initial conditions, a common practice is to consider the fractional equation with Caputo derivative as follows:

    CDαtu(t)=f(t),  tI, (2.6)

    where CDαt is the Caputo differential operator defined by

    CDαtv(t)=1Γ(1α)t0v (τ)(tτ)αdτ,  tI.

    It has been widely believed that the Eq (2.6) subject to the standard form of the initial condition

    u(0)=u0 (2.7)

    is well-posed. However, this may not be true if we are interested in weak solutions or even singular solutions. For example, if we consider the right hand side function f(t)=tδ1/2L2(I),δ>0, it is not difficult to check that the Eq (2.6) admits a unique solution

    u(t):=Γ(δ+12)Γ(α+δ+12)tα+δ1/2,

    which belongs to Hα+δε(I) for any ε>0, but has non finite values at t=0 for 0<α<1/2,0<δ<1/2α. In fact the initial condition (2.7) can only be made sense for fHδ(I) with δ>1/2α.

    For the purpose to impose the initial condition in a consistent way and allow for weaker solutions, we propose to consider the fractional differential equation under Riemann-Liouville definition:

    RDαtu(t)=f(t)+u0tαΓ(1α),  0<α<1. (2.8)

    It is seen in the above equation that an "initial condition" is imposed in a weak sense in the right hand side, similar to the Neumann condition for a second order elliptic problem. This is motivated by the relationship

    CDαtv(t)=RDαtv(t)v(0)tαΓ(1α),

    which is true for all functions v such that all terms in the above identity are well-defined. A direct computation shows that the Eq (2.8) subject to the initial condition

    limt0I1αtu(t)=0

    leads to the solution

    u(t)=1Γ(α)t0f(τ)dτ(tτ)1α+1Γ(α)u0Γ(1α)t0ταdτ(tτ)1α=1Γ(α)t0f(τ)dτ(tτ)1α+u0.

    Inspired by the discussion in the previous section, we are interested in an optimal control problem governed by the space-time fractional diffusion equation (STFDE) with non-homogeneous initial condition under the form:

    R0αtu(x,t) Raβxu(x,t)=f(x,t)+q(x,t)+u0(x)tαΓ(1α),(x,t)Λ×I,u(a,t)=u(b,t)=0,tI,limt0I1αtu(x,t)=0,xΛ, (3.1)

    where 0<α<1,1<β<2, Λ=(a,b),I=(0,T),T>0.

    We first introduce some notations that will be used throughout the paper. In all that follows, we use the expression AB to denote AcB with c being a generic positive constant. For a domain O, which may be Λ,I or Ω=Λ×I, we recall that L2(O),Hs(O), and Hs0(O) stand for the usual Sobolev spaces, equipped with the norms 0,O and s,O respectively. Let X be the Sobolev space with norm X, we introduce the space

    Hs(I;X):={vL2(I;X)|v(,t)XHs(I)},

    endowed with the norm:

    vHs(I;X):=v(,t)Xs,I.

    Particularly, when X stands for Hμ(Λ) or Hμ0(Λ), the norm of the space Hs(I;X) will be denoted by μ,s,Ω.

    Hereafter, in cases where no confusion would arise, the domain symbols I,Λ,Ω may be dropped from the notations.

    We now consider the following optimal control problem:

    minq{g(u)+h(q)}, (3.2a)

    where g and h are given convex functionals, the state variable u is the solution of STFDE (3.1), and the control variable q satisfies

    IΛq(x,t)dxdt0. (3.2b)

    In order to formulate the weak form of the state Eq (3.1), we recall the state space

    Bs,σ(Ω)=Hs(I,L2(Λ))L2(I,Hσ0(Λ)), s>0,σ>0,

    endowed with the norm

    vBs,σ(Ω)=(v2Hs(I,L2(Λ))+v2L2(I,Hσ(Λ)))12,

    which can be found in Li and Xu [28]. Then we have the following weak formulation of the state Eq (3.1): given q,fL2(Ω),u0L2(Λ), find uBα2,β2(Ω), such that

    A(u,v)=(f+q,v)Ω+(u0(x)tαΓ(1α),v)Ω,   vBα2,β2(Ω) (3.3)

    with the bilinear form A(,) being defined by

    A(u,v):=(R0α2tu, Rtα2Tv)Ω(Raβ2xu, Rxβ2bv)Ω.

    Here, R0α2t and Rtα2T respectively denote the left and right Riemann-Liouville fractional derivative of order α2, Raβ2x and Rxβ2b respectively denote the left and right Riemann-Liouville fractional derivative of order β2.

    It has been shown in [28] that the following continuity and coercivity hold

    A(u,v)uBα2,β2(Ω)vBα2,β2(Ω),  A(v,v)v2Bα2,β2(Ω),  u,vBα2,β2(Ω),

    and the problem (3.3) is well-posed.

    Let K denote the admissible set associated to the constraints (3.2b) as

    K:={qL2(Ω):Ωq(x,t)dxdt0},

    and let

    J(q,u):=g(u)+h(q), (q,u)K×Bα2,β2(Ω), (3.4)

    then the optimal control problem (3.2) reads: find (q,u(q))K×Bα2,β2(Ω), such that

    J(q,u(q))=min(q,u)K×Bα2,β2(Ω)J(q,u)  subjectto(3.3). (3.5)

    Assume that the functional g() is bounded below, and h(q)+ as q0,Ω+, it is known (see, e.g., [29,30]) that the optimal control problem (3.5) admits a unique solution (q,u(q))K×Bα2,β2(Ω).

    The well-posedness of the state equation ensures the existence of a control-to-state mapping qu=u(q) defined through (3.3). Then the optimal control problem (3.5) equivalently can be rewritten in the following form: find qK, such that

    J(q)=minqKJ(q) (3.6)

    for the reduced functional J(q):=J(q,u(q)) over L2(Ω).

    The first order necessary optimality conditions for (3.6) take the form

    J(q)(δqq)0,  δqK, (3.7)

    with

    J(q)(ζ)=(h(q)+z(q),ζ)Ω,  q,ζK,

    which is proved in the following lemma.

    Lemma 3.1. It holds

    J(q)(ζ)=(h(q)+z(q),ζ)Ω,  ζL2(Ω), (3.8)

    where z(q)=z is the solution of the following adjoint state equation

    tαTz(x,t) Rxβbz(x,t)=g(u),(x,t)Ω, (3.9)
    z(x,T)=0,xΛ, (3.10)
    z(a,t)=z(b,t)=0,tI, (3.11)

    with tαT (0<α<1) denoting the right Caputo fractional derivative.

    Proof. The proof of this lemma is very close to that given for Lemma 2.1 in [21], but for the reader's convenience, we therefore give the details as follows. It is apparent from the chain rule that

    J(q)(ζ)=(g(u(q)))(ζ)+h(q)(ζ)=Ωg(u(q))u(q)(ζ)dxdt+Ωh(q)ζdxdt. (3.12)

    We now in a position to compute u(q)(ζ). For simplicity, let δu denote the derivative of u=u(q) in the direction ζ, that is

    δu(x,t):=u(q)(ζ)=limε0u(q+εζ)u(q)ε.

    Then it is readily seen that δu is the solution of the following problem:

    {R0αtδu Raβxδu=ζ,(x,t)Ω,δu(a,t)=δu(b,t)=0,tI,I1αtδu(x,0)=0,xΛ. (3.13)

    To prove (3.8), we multiply each side of (3.9) by δu, then integrate the resulted equation on the domain Ω to yield

    Ωg(u)δudxdt=Ω(tαTz Rxβbz)δudxdt. (3.14)

    Taking into account the boundary conditions in (3.13) and (3.11), by means of the fractional integration by parts demonstrated in [28], it holds

    Ω Rxβbzδudxdt=Ωz Raβxδudxdt. (3.15)

    Once again we use the fractional integration by parts to find

    ΩtαTzδudxdt=Ωz R0αtδudxdtΛ(I1αtδu(x,T)z(x,T)I1αtδu(x,0)z(x,0))dx. (3.16)

    Noticing the terminal condition in (3.10) and the initial condition in (3.13), we get

    ΩtαTzδudxdt=Ωz R0αtδudxdt. (3.17)

    Finally, combining (3.14), (3.15), and (3.17), we obtain

    Ωg(u)δudxdt=Ω(R0αtδuRaβxδu)zdxdt=Ωζzdxdt. (3.18)

    This, together with (3.12), leads to (3.8).

    The weak form of (3.9)–(3.11) reads: find zBα2,β2(Ω), such that

    A(φ,z)=(g(u),φ)Ω,   φBα2,β2(Ω). (3.19)

    Following the same idea as for the problem (3.3), it can be proved that (3.19) admits a unique solution zBα2,β2(Ω) for any given uBα2,β2(Ω).

    In what follows we will need the mapping qu(q)z(q), where for any given q, u(q) is defined by (3.3), and once u(q) is known, z(q) is defined by (3.19).

    We define the polynomial space

    P0M(Λ):=PM(Λ)Hβ20(Λ),  SL:=P0M(Λ)PN(I)Bα2,β2(Ω),

    where PM and PN respectively denote the space of polynomials with degree no more than M and N, L stands for the parameter pair (M,N).

    Then we arrive at the spectral approximation to the state Eq (3.3) as follows: find uL(q)SL such that

    A(uL(q),vL)=(f+q,vL)Ω+(u0(x)tαΓ(1α),vL)Ω,  vLSL. (4.1)

    According to [28], the above discrete state equation admits a unique solution. The following estimate, also derived in [28], will be used in the analysis later on.

    Lemma 4.1. [28] For any qL2(Ω), let u(q) be the solution of (3.3), uL(q) be the solution of (4.1). Suppose uHα2(I;Hμ(Λ))Hν(I;Hβ20(Λ)), 0<α<1,1<β<2,ν>1,μ1, then we have

    u(q)uL(q)Bα2,β2(Ω)Nνuβ2,ν+Nα2νu0,ν+Mμuμ,α2+Mβ2μuμ,0. (4.2)

    We now define the semidiscrete optimal problem: find qK, such that

    JL(q)=minqKJL(q), (4.3)

    where for qL2(Ω) we set JL(q):=J(q,uL(q)) with uL(q) being defined in (4.1). The unique solution q of problem (4.3) is characterized by the variational inequality

    JL(q)(δqq)0,   δqK, (4.4)

    where similar as Eq (3.8)

    JL(q)(ϕ)=(h(q)+zL(q),ϕ)Ω, q,ϕK. (4.5)

    The above semidiscrete adjoint state zL(q)SL is the solution of the following problem:

    A(φL,zL(q))=(g(uL(q)),φL)Ω,   φLSL. (4.6)

    By defining the following finite dimensional subspace for the control variable:

    KL=K(PM(Λ)PN(I)),

    we arrive at the full discrete optimal control problem: find qLKL, such that

    JL(qL)=minqLKLJL(qL), (4.7)

    where the unique solution qL satisfies the first order optimality condition

    JL(qL)(δqqL)0,  δqKL. (4.8)

    In order to obtain the posteriori error estimates for the spectral approximation (4.7), we need some approximation operators and their approximation properties. Let r and s be two real numbers such that rn+12,0sr, there exits an operator Πs,0r,N:HrHs0PNHs0, such that, for any φHσHs0 with σr, we have [31]

    φΠs,0r,NφmcNmσφσ,  0mr. (5.1)

    Let ΠN be the L2-orthogonal projection operator from L2(I) onto PN(I). Equivalently, it means that, for any function vL2(I), ΠNv belongs to PN(I) and satisfies

    (ΠNvv,wN)I=0, wNPN(I).

    Then for any nonnegative real number m, the following estimate holds

    ΠNvv0,INmvm,I,  vHm(I),m0. (5.2)

    The L2-orthogonal projector ΠM in Λ is defined similarly.

    We now proceed to analyze the approximation error of the proposed space-time spectral method. The proof of the main result will be accomplished with a series of lemmas which we present below.

    Lemma 5.1. If g() is convex, and h() is strictly convex such that

    (h(p)h(q),pq)Ωcpq20,Ω,  p,qL2(Ω).

    Then for all p,qL2(Ω), we have

    J(p)(pq)J(q)(pq)cpq20,Ω. (5.3)

    Proof. The proof of this result is quite similar to that given for Lemma 4.2 in [21] and so is omitted.

    Lemma 5.2. Let q and qL denote the solutions of the problems (3.6) and (4.7) respectively. Assume that g() is convex, h() is strictly convex, and h(qL)H1(I,H1(Λ)). Then there holds:

    qqL0,Ωξ+zL(qL)z(qL)0,Ω, (5.4)

    where

    ξ=N1h(qL)0,1,Ω+M1h(qL)1,0,Ω,

    zL(qL) and z(qL) are respectively the solutions of (4.6) and (3.19) associated to qL.

    Proof. Using (3.7), (5.3) and (4.8), we can show that for arbitrary pLKL,

    cqqL20,ΩJ(q)(qqL)J(qL)(qqL)J(qL)(qqL)=JL(qL)(qLq)J(qL)(qqL)+JL(qL)(qqL)=JL(qL)(qLpL)+JL(qL)(pLq)(h(qL)+z(qL),qqL)Ω+(h(qL)+zL(qL),qqL)ΩJL(qL)(pLq)+(zL(qL)z(qL),qqL)Ω=(zL(qL)+h(qL),pLq)Ω+(zL(qL)z(qL),qqL)Ω. (5.5)

    Furthermore, by taking pL=ΠNΠMq, we have

    (zL(qL)+h(qL),pLq)Ω=(h(qL),ΠNΠMqq)Ω=(h(qL)ΠNΠMh(qL),ΠNΠMqq)Ω=(h(qL)ΠNΠMh(qL),qLq)Ω. (5.6)

    By substituting (5.6) into (5.5), and using the Young inequality, we get

    cqqL20,Ω(h(qL)ΠNΠMh(qL),qLq)Ω+(zL(qL)z(qL),qqL)ΩCεh(qL)ΠNΠMh(qL)20,Ω+εqLq20,Ω+CεzL(qL)z(qL)20,Ω+εqLq20,Ω,

    where ε>0 is a sufficient small constant. Then, we choose ε=c4 to derive

    c2qqL20,ΩCεh(qL)ΠNΠMh(qL)20,Ω+CεzL(qL)z(qL)20,Ω. (5.7)

    Finally, by using the approximation estimate (5.2) we obtain (5.4).

    Remark 5.1. The above results can be simplified in the case where the cost functional is quadratic, i.e.,

    g(u)=12Ω(uˉu)2dxdt,  h(q)=12Ωq2dxdt,

    where ˉu is a given observation data. In this case, we have

    (zL(qL)+h(qL),pLq)Ω=(zL(qL)+qL,ΠNΠMqq)Ω=0.

    Hence (5.4) is reduced to

    qqL0,ΩzL(qL)z(qL)0,Ω.

    Lemma 5.3. Let qL denote the solution of (4.7) with the associated discrete state uL(qL) and adjoint state zL(qL). Assume g() is Lipschitz continuous. Then it holds

    zL(qL)z(qL)Bα2,β2(Ω)η1+uL(qL)u(qL)0,Ω, (5.8)

    where

    η1=(Nα2+Mβ2) RtαTzL(qL) RxβbzL(qL)g(uL(qL))0,Ω.

    Proof. Let us first denote ez=zL(qL)z(qL), eLz=ΠNΠβ2,0β2,MezSL. It follows from (3.19) and (4.6) that

    A(eLz,ez)=(g(uL(qL))g(u(qL)),eLz)Ω.

    Using (3.3), (3.19), (4.1), and (4.6), we obtain

    zL(qL)z(qL)2Bα2,β2(Ω)A(ez,ez)=A(ezeLz,ez)+A(eLz,ez)=A(ezeLz,zL(qL))A(ezeLz,z(qL))+A(eLz,ez)=( R0α2t(ezeLz), Rtα2TzL(qL))Ω( Raβ2x(ezeLz), Rxβ2bzL(qL))Ω(g(u(qL)),ezeLz)Ω+(g(uL(qL))g(u(qL)),eLz)Ω=(ezeLz, RtαTzL(qL))Ω(ezeLz, RxβbzL(qL))Ω(g(u(qL)),ezeLz)Ω+(g(uL(qL))g(u(qL)),eLzez)Ω+(g(uL(qL))g(u(qL)),ez)Ω=(ezeLz, RtαTzL(qL) RxβbzL(qL))Ω+(g(uL(qL)),eLzez)Ω+(g(uL(qL))g(u(qL)),ez)Ω=(ezeLz, RtαTzL(qL) RxβbzL(qL)g(uL(qL)))Ω+(g(uL(qL))g(u(qL)),ez)ΩezeLz0,ΩRtαTzL(qL) RxβbzL(qL)g(uL(qL))0,Ω+g(uL(qL))g(u(qL))0,Ωez0,ΩezeLz0,ΩRtαTzL(qL) RxβbzL(qL)g(uL(qL))0,Ω+uL(qL)u(qL)0,Ωez0,Ω. (5.9)

    Notice that both zL(qL) and z(qL) are in Bα2,β2(Ω), which means ezHα2(I,L2(Λ)) and ezL2(I,Hβ20(Λ)), thus it follows from the approximation estimates (5.1) and (5.2):

    ezeLz0,ΩezΠNez0,Ω+ΠNezΠNΠβ2,0β2,Mez0,ΩezΠNez0,Ω+(ΠNId)(ezΠβ2,0β2,Mez)0,Ω+ezΠβ2,0β2,Mez0,ΩezΠNez0,Ω+ezΠβ2,0β2,Mez0,ΩNα2ez0,α2,Ω+Mβ2ezβ2,0,Ω(Nα2+Mβ2)ezBα2,β2(Ω), (5.10)

    where Id denotes the identity operator. Plugging (5.10) into (5.9) yields (5.8).

    Lemma 5.4. Let qL denote the solution of (4.7) with the associated discrete state uL(qL) and adjoint state zL(qL). Then we have

    uL(qL)u(qL)Bα2,β2(Ω)η2+η3, (5.11)

    where

    η2=(Mβ2+Nα2) R0αtuL(qL) RaβxuL(qL)fqL0,Ω,η3=(Mβ2+Nγ)1Γ(1α)u00,Λ(11αsT1αs)1s.

    Here, γ=α4,s=42+α if 0<α<12, and γ=1α4,s=41+3α if 12α<1.

    Proof. We follow the argument similar to the one used in the previous lemma. Set eu=uL(qL)u(qL), and let eLu=ΠNΠβ2,0β2,MeuSL. Then it follows from (3.3) and (4.1) that A(eu,eLu)=0, and consequently,

    uL(qL)u(qL)2Bα2,β2(Ω)A(eu,eu)=A(eu,eueLu)=A(uL(qL),eueLu)A(u(qL),eueLu)=( R0αtuL(qL) RaβxuL(qL)fqL,eueLu)Ω+(u0(x)tαΓ(1α),eLueu)Ω. (5.12)

    On one hand, we have

    ( R0αtuL(qL) RaβxuL(qL)fqL,eueLu)Ω R0αtuL(qL) RaβxuL(qL)fqL0,ΩeueLu0,Ω R0αtuL(qL) RaβxuL(qL)fqL0,Ω(Nα2eu0,α2,Ω+Mβ2euβ2,0,Ω) R0αtuL(qL) RaβxuL(qL)fqL0,Ω(Nα2+Mβ2)euBα2,β2(Ω). (5.13)

    On the other hand,

    (u0(x)tαΓ(1α),eLueu)Ω=1Γ(1α)ItαΛu0(x)(eLueu)dxdt1Γ(1α)Itαu0(x)0,ΛeLueu0,Λdt1Γ(1α)u0(x)0,ΛtαLs(I)eLueuLs(I;L2(Λ)), (5.14)

    where 1s+1s=1. A simple calculation gives

    tαLs(I)=(11αs(T1αslimt0t1αs))1s,

    which is bounded for any fixed T and α(0,1) if and only if s<1α. Furthermore, it holds

    eLueuLs(I;L2(Λ))euΠNeuLs(I;L2(Λ))+euΠβ2,0β2,MeuLs(I;L2(Λ)). (5.15)

    By the error estimate for the L2-projector ΠN in Ls norm, s>2 (see (5.4.16) in [32]), we have

    euΠNeuLs(I;L2(Λ))NγeuWγ,s(I;L2(Λ)), γ0,

    where Wγ,s(I) is the classic Sobolev space defined on I. It can be checked [33] that when γα2 and γ1s1α2,

    Hα2(I)Wγ,s(I).

    Hence, if 0<α<12, we take

    s=42+α,s=42+α,γ=α4, (5.16)

    and if 12α<1, we set

    s=41+3α,s=43(1α),γ=1α4. (5.17)

    As a result, it holds for the above chosen parameters that

    euΠNeuLs(I;L2(Λ))Nγeu0,α2,ΩNγeuBα2,β2(Ω). (5.18)

    Furthermore, we have

    euΠβ2,0β2,MeuLs(I;L2(Λ))=euΠβ2,0β2,Meu0,ΛLs(I)Mβ2euβ2,ΛLs(I)Mβ2euBα2,β2(Ω). (5.19)

    By substituting (5.18) and (5.19) into (5.15), we obtain

    eLueuLs(I;L2(Λ))(Mβ2+Nγ)euBα2,β2(Ω). (5.20)

    Taking (5.14) into consideration, we get

    (u0(x)tαΓ(1α),eLueu)Ωη3euBα2,β2(Ω). (5.21)

    Plugging (5.13) and (5.21) back into (5.12) gives (5.11).

    With the help of the preceding three lemmas we can now prove the following main result.

    Theorem 5.1. Let q be the solution of (3.6) with the associated state u(q) and adjoint state z(q). qL is the solution of (4.7) with the associated discrete state uL(qL) and adjoint state zL(qL). Under the assumptions in Lemmas 5.2, 5.3, and 5.4, the following estimate holds:

    qqL0,Ω+u(q)uL(qL)Bα2,β2(Ω)+z(q)zL(qL)Bα2,β2(Ω)η, (5.22)

    where η=ξ+η1+η2+η3, with ξ,η1,η2, and η3 being defined in Lemmas 5.2-5.4.

    Proof. We begin with estimating qqL0,Ω. According to (5.4), it suffices to estimate zL(qL)z(qL)0,Ω. Combining (5.8) and (5.11) we obtain

    zL(qL)z(qL)Bα2,β2(Ω)η1+uL(qL)u(qL)0,Ωη1+η2+η3. (5.23)

    Using the above estimate, inequality 0,ΩBα2,β2(Ω), and Lemma 5, we get

    qqL0,Ωξ+η1+η2+η3. (5.24)

    It follows from (3.3) and (3.19) that u(q)u(qL) satisfies

    A(u(q)u(qL),v)=(qqL,v),   vBα2,β2(Ω), (5.25)

    and z(q)z(qL) satisfies

    A(φ,z(q)z(qL))=(g(u(q))g(u(qL)),φ),   φBα2,β2(Ω). (5.26)

    Taking v=u(q)u(qL) in (5.25) gives

    u(q)u(qL)Bα2,β2(Ω)qqL0,Ω. (5.27)

    Furthermore, using the triangle inequalities and (5.11), we get

    u(q)uL(qL)Bα2,β2(Ω)u(q)u(qL)Bα2,β2(Ω)+u(qL)uL(qL)Bα2,β2(Ω)qqL0,Ω+η2+η3. (5.28)

    Similarly, taking φ=z(q)z(qL) in (5.26) we have

    z(q)z(qL)Bα2,β2(Ω)g(u(q))g(u(qL))0,Ω.

    In view of the Lipschitz continuity of g(), we obtain

    z(q)z(qL)Bα2,β2(Ω)u(q)u(qL)0,Ωu(q)u(qL)Bα2,β2(Ω)qqL0,Ω. (5.29)

    It follows from (5.23), (5.29) and the triangle inequality:

    z(q)zL(qL)Bα2,β2(Ω)z(q)z(qL)Bα2,β2(Ω)+z(qL)zL(qL)Bα2,β2(Ω)qqL0,Ω+η1+η2+η3. (5.30)

    Finally, combining (5.24), (5.28) and (5.30) gives (5.22).

    Remark 5.2. In Theorem 5.1, we have obtained an a posteriori upper bound, expressed by the reliable indicator η, which will be checked in our numerical experiments. For the time being we are unable to derive an optimal estimate. As for the classical elliptic and parabolic equations, we guess such an optimal estimate will have to make use of some Jacobi-weighted Sobolev spaces and polynomial inverse inequalities. We leave this issue for future work.

    We carry out in this section a series of numerical experiments and present results to validate the obtained error estimates. We use the projection gradient optimization algorithm proposed in [27] to solve the optimization problem. In all the calculations, we take Λ=(1,1),T=1, and

    g(u)=12Ω(uˉu)2dxdt,  h(q)=12Ωq2dxdt.

    We consider the problem (3.2) with the exact analytical solutions as follows

    u(q)=sinπxcosπt, z(q)=sinπxsinπ(1t), q=max{0,¯z(q)}z(q).

    The right-hand side function f and the observation state ˉu are numerically calculated through (3.3) and (3.19) using u(q),z(q), and q.

    We first investigate the impact of the initial guess on the convergence of the projection gradient optimization algorithm. We start by considering q(0)=25q. In Figure 1, we present the convergence history of the gradient of the objective function versus the iteration number with M=18,N=18,α=0.6,β=1.6. We see that the iterative method converges within a dozen iterations. We then take q(0) to be constant c with c=0 or 15, and repeat the same computation as the previous test. The result is given in Figure 2. These results seem to tell that the initial guess has no significant effects on the convergence of the projection gradient iterative algorithm. In the following, the initial guess is set to 0.

    Figure 1.  Convergence history of the gradient of the objective function for q(0)=25q.
    Figure 2.  Convergence history of the gradient of the objective function for q(0)=c.

    Next we check the convergence behavior of numerical solutions with respect to the polynomial degrees M. In Figures 3 to 5, we plot the errors as functions of the polynomial degrees M with α=0.6,N=20 for β=1.2,1.6,1.9. The errors show an exponential decay, since in this semi-log representation one observes that the error variations are essentially linear versus the degrees of polynomial.

    Figure 3.  Errors of u,z,q versus M with N=20,α=0.6,β=1.2.
    Figure 4.  Errors of u,z,q versus M with N=20,α=0.6,β=1.6.
    Figure 5.  Errors of u,z,q versus M with N=20,α=0.6,β=1.9.

    We then investigate the temporal errors, that is, for fix M, we check the convergence behavior of numerical solutions with respect to the polynomial degrees N in time direction. In Figures 6 to 8, we plot the errors as functions of N with β=1.6,M=20 for three values α=0.2,0.6,0.9. The straight line of the error curves indicates that the convergence in time is also exponential.

    Figure 6.  Errors of u,z,q versus N with M=20,α=0.6,β=1.6.
    Figure 7.  Errors of u,z,q versus N with M=20,α=0.9,β=1.6.
    Figure 8.  Errors of u,z,q versus N with M=20,α=0.2,β=1.6.

    In order to validate the a posteriori error estimate, we compare the error indicator η defined in (5.22) and the real error of the numerical solution measured by:

    e:=qqL0,Ω+u(q)uL(qL)Bα2,β2(Ω)+z(q)zL(qL)Bα2,β2(Ω).

    These two errors are compared in Figures 9 and 10 as functions of M(=N) for different α and β. We observe that the indicator η has almost the same exponential decay rate as the real error e. Also observed in the figures is that the a posteriori error is an upper bound. This is consistent with the theoretical results.

    Figure 9.  Performance of the error indicator η with M=N,α=0.6,β=1.6.
    Figure 10.  Performance of the error indicator η with M=N,α=0.3,β=1.4.

    In the present work, we have first discussed the commonly used initial conditions for differential equations involving Riemann-Liouville and Caputo derivatives, and proposed a consistent way to impose the non-homogeneous initial condition. Then an optimal control problem governed by the space-time fractional diffusion equation with non-homogeneous initial conditions was investigated. A posteriori upper bound was derived for the space-time spectral approximation. Numerical experiment has been carried out to confirm the theoretical results. In a future work, we will focus on the efficiency of the error estimates, i.e. a posteriori error lower bound, to obtain equivalent a posteriori error estimates for the considered optimal control problems. It will be also interesting to look for a strategy that allows to approximate the optimal control problem with adaptive spectral method.

    The research of X. Y. Ye was partially supported by the Natural Science Foundation of Fujian Province of China (Grants 2020J01703), Scientific Research Foundation of Jimei University of China (Grants ZP2020062 and ZP2020054), Foundation of Fujian Provincial department of education (Grants JAT190326). The research of C. J. Xu is partially supported by NSFC grant 11971408, NNW2018-ZT4A06 project.

    The authors declared that they have no conflicts of interest to this work.



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