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Research article

Optimal control for a phase field model of melting arising from inductive heating

  • Received: 02 June 2021 Accepted: 08 September 2021 Published: 08 October 2021
  • MSC : 35K55, 35Q60, 49J20, 49K20

  • Due to its unique performance of high efficiency, fast heating speed and low power consumption, induction heating is widely and commonly used in many applications. In this paper, we study an optimal control problem arising from a metal melting process by using a induction heating method. Metal melting phenomena can be modeled by phase field equations. The aim of optimization is to approximate a desired temperature evolution and melting process. The controlled system is obtained by coupling Maxwell's equations, heat equation and phase field equation. The control variable of the system is the external electric field on the local boundary. The existence and uniqueness of the solution of the controlled system are showed by using Galerkin's method and Leray-Schauder's fixed point theorem. By proving that the control-to-state operator P is weakly sequentially continuous and Fréchet differentiable, we establish an existence result of optimal control and derive the first-order necessary optimality conditions. This work improves the limitation of the previous control system which only contains heat equation and phase field equation.

    Citation: Zonghong Xiong, Wei Wei, Ying Zhou, Yue Wang, Yumei Liao. Optimal control for a phase field model of melting arising from inductive heating[J]. AIMS Mathematics, 2022, 7(1): 121-142. doi: 10.3934/math.2022007

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  • Due to its unique performance of high efficiency, fast heating speed and low power consumption, induction heating is widely and commonly used in many applications. In this paper, we study an optimal control problem arising from a metal melting process by using a induction heating method. Metal melting phenomena can be modeled by phase field equations. The aim of optimization is to approximate a desired temperature evolution and melting process. The controlled system is obtained by coupling Maxwell's equations, heat equation and phase field equation. The control variable of the system is the external electric field on the local boundary. The existence and uniqueness of the solution of the controlled system are showed by using Galerkin's method and Leray-Schauder's fixed point theorem. By proving that the control-to-state operator P is weakly sequentially continuous and Fréchet differentiable, we establish an existence result of optimal control and derive the first-order necessary optimality conditions. This work improves the limitation of the previous control system which only contains heat equation and phase field equation.



    As a fairly new processing technology, induction heating is widely and commonly used in many applications, for example, induction melting, induction heat treatment, and so on (see [1]). The similar mathematical model is described by partial differential equations (see [2]). The metal materials is heated by the eddy current which is produced by electromagnetic induction. The solid phase of the material begins to melt when the temperature achieves its melting point.

    In this paper, we use bold letter represents a vector or vector function in three space dimensions. For convenience, a product space Bn is often simply written as B, such as, L2(Ω):=[L2(Ω)]3. Suppose that a fixed time T>0 is given and a metal material occupies a bounded C2-domain ΩR3. The electric filed E and the magnetic field H in Ω satisfy the Maxwell's equations (see[3,4]):

    {εEt+σE(x,t)=×H,(x,t)QT,μHt+×E=0,(x,t)QT,

    where QT=Ω×(0,T], ε, μ and σ are the electric permittivity, magnetic permeability, and electric conductivity, respectively. Since the induction material is highly conductive, the displacement current Jd=εE is very weak in comparison with the eddy currents Je=σE and is negligible (ε=0) [5]. Hence, Maxwell's equations become a single system with respect to H(x,t):

    μHt+×[ρ×H]=0,(x,t)QT,

    where ρ=1σ represents the electric resistivity, the permeability μ=μ1iμ2, μ1>0,μ2>0 is a complex constant.

    During the heating process, the local density of Joule's heat is described as (see[5,6])

    Q(x,t)=EJ=ρ|×H|2,(x,t)QT,

    where J is the complex conjugate of J.

    When the metal material is heated, it will melt. Therefore, solid and liquid coexist in the heated object during induction heating. This process can be modeled as system of phase field equations. A solid-liquid coexistence region which is usually described by using the interface with finite thickness ξ (See[2]). Let function u be the temperature and phase function ϕ describe the degree of melting. Then, in the process of induction heating, the phase change phenomena can be modeled by a strong coupling system as follows (a similar model can refer to the literature [2]):

    {ut+12lϕt(k(x)u)=ρ|×H|2,(x,t)QT,τϕtξ2ϕ12(ϕϕ3)=2u,(x,t)QT,

    where l, τ and k(x) are the latent heat (per unit mass), relaxation time and the thermal conductivity, respectively.

    Since magnetic field is more difficult to measure and control than electric field in engineering practice, we consider the boundary control problem of electric field. In addition, some parts of the boundary are insulated for ease of operation in the specific induction heating and melting process. Therefore, a part of the boundary is adiabatic, the other part is used to control magnetic field by electric field. After imposing the initial boundary value and normalizing certain physical parameters, we present the following system of phase field arising from inductive heating:

    {Ht+××H=0,(x,t)QT,(1.1)ut(k(x)u)=|×H|212lϕt,(x,t)QT,(1.2)ϕtϕ12(ϕϕ3)=2u,(x,t)QT,(1.3)n×H=0,(x,t)SΓ1=Γ1×(0,T],(1.4)n×[×H(x,t)]=n×G(x,t),(x,t)SΓ2=Γ2×(0,T],(1.5)H(x,0)=H0(x),xΩ,(1.6)(un,ϕn)=(0,0),(x,t)SΓ=Ω×(0,T],(1.7)(u(x,0),ϕ(x,0))=(u0(x),ϕ0(x)),xΩ,(1.8)

    where the boundary Ω=Γ1Γ2 is split into two disjoint measurable subsets Γ1 and Γ2, both of which are nonempty, n is the outward unit normal on Ω,un=un is the normal derivative on Ω and G is the electric field generated by external optoelectronic devices which will be considered as a control variable.

    In order to obtain optimal strategy for the electric field action such that the temperature profile at the final stage has a relative uniform distribution and minimum energy consumption, we state our optimal control problem as follows.

    Optimal control problem (P): Assume that the temperature uT() and degree of melting ϕT() are given in L2(Ω), we would like to find an optimal control GUad such that the cost functional

    J(G;H,ϕ,u)=12Ω|u(x,T)uT(x)|2dx+12Ω|ϕ(x,T)ϕT(x)|2dx+λ2T0Γ2|G(x,t)|2dsdt (1.9)

    achieves its minimum at (H,ϕ,u) under the state equations by coupled systems (1.1)(1.8), where λ>0 is a typical regularization parameter, G(,) belongs to the following admissible control set:

    Uad={GL2(0,T;L2(Γ2)):GL2(0,T;L2(Γ2))A0<+},

    where A0 is a known constant.

    For optimal control problems of the system coupled by Maxwell's equations with nonlinear heat equation in microwave heating, there are several papers dealing with in recent years. Wei and Yin [7] discussed the existence and necessary conditions of the optimal control on the boundary electric field control. Further, they proved the regularity of weak solutions of coupled nonlinear systems and gave necessary conditions for uniform microwave heating when microwave acts in three directions in the paper [8]. The problem of realizing uniform microwave heating through frequency control was considered (see, for examples, Yin [9] and Liao [10]). The Bang-Bang properties for time optimal controls on microwave heating was also discussed in [11]. But the controlled system in researches above does not contain the phase field process.

    Without Maxwell's equations, the research on the qualitative theory and optimal control of phase field equations is a very active topic from the 1980s. On phase field model, one can refer to Temam's related references [12] and Caginalp [2]. In order to more accurately express the subtle physical characteristics, some authors studied the phase field equations with corresponding parameters [13,14,15,16]. However, it is worth mentioning that, based on Caginalp's phase field model [2], Hoffman and Jiang [15] generalized the model and obtained the well-posedness of the solution for controlled system and necessary conditions for related optimal problem. In addition, the solidification or melting models of some metal alloys with multiple crystals were described. For the two kinds of crystallization [16], the well-posedness of the phase field equation was studied, and the maximum principle is deduced by using Dubovitskii-Milyutin method [17]. Limited by mathematical techniques, the well-posedness of the phase field equations of three crystals was studied only in one dimension [18]. Later, Colli studied the distributed optimal control problem of this kind of system to supplement this analysis [19]. There are abundant articles on several numerical simulation aspects of phase field model, such as [20,21,22,23,24,25]. However, the previous work did not involve the phase field coupling system (1.1)(1.8) in the induction heating process. There exist some difficulties in this study. Firstly, the boundary conditions (1.4) and (1.5) are mixed. Secondly, the heat source |×H|2 is required in L2(QT). Finally, the Fréchet differentiability of state variables H,u and ϕ on control variable G is also a complicated problem.

    The rest of this article is organized as follows. In Section 2, some symbols and assumptions used in this paper are given, and we showed that there is unique solution for the controlled system. In Section 3, we prove several important properties of the control-to-state operator. Section 4 is devoted to the existence and necessary condition for optimal control problem. Some concluding remarks are given in Section 5.

    For the sake of convenience, we recall some function spaces associated with Maxwell's equations. Let

    V(curl,Ω)={ML2(Ω):×ML2(Ω)},X={ML2(Ω):×ML2(Ω),n×M=0 on Γ1}.

    Then, V(curl,Ω) and X are Hilbert spaces equipped with inner product

    (M,N)=Ω[(×M)(×N)+MN],

    where N represents the complex conjugate of N. Obviously, X is a linear subspace of V(curl,Ω). A norm on V(curl,Ω) and X is given by V(curl,Ω)=(,).

    To take account of the boundary conditions, we introduce two trace mappings Υt:V(curl,Ω)Y(Ω) and ΥT:V(curl,Ω)Y(Ω) (the dual space of Y(Ω)) defined by Υt(M)=n×M|Ω and ΥT(M)=n×(n×M|Ω), respectively, where n is the above description and Y(Ω) is a Hilbert space (see [26]) as follow

    Y(Ω)={fH12(Ω):there exists MV(curl,Ω) with Υt(M)=f},

    with norm

    fY(Ω)=infMV(curl,Ω),Υt(M)=fMV(curl,Ω).

    We begin with some basic assumptions.

    A(2.1) The vector function H0()L2(Ω) is given and nonnegative.

    A(2.2) For almost every t(0,T), the function G(,t) is defined on Γ2 with an extension such that G(,t)V(curl,Ω) with extended function ˉG(,t) satisfies

    ˉG(,t)V(curl,Ω)C0G(,t)L2(Γ2),

    where C0 is a constant that depends only on Ω.

    For convenience, we shall denote the extended function ˉG(,t) by G(,t) with G(,t)V(curl,Ω).

    Lemma 1. Under the assumptions A(2.1) and A(2.2), there is a unique weak solution HL2(0,T;X) for the parabolic problem (1.1) and (1.4)(1.6). The weak solution HL2(0,T;X) is defined by

    T0ΩHΦtdxdt+T0Ω(×H)(×Φ)dxdt=ΩH0Φ(x,0)dxT0n×G,ΥT(Φ)Γ2dt,

    for any function ΦH1(0,T;X) with Φ(x,T)=0a.e.xΩ. Moreover, there are constants C10 and C20, which depend only on known data, such that

    supt[0,T]H(,t)L2(Ω)+HL2(0,T;V(curl,Ω))C1(GL2(0,T;L2(Γ2))+H0L2(Ω)), (2.1)
    ×H(,t)6L6(Ω)C2G(,t)2L2(Ω),a.e.t[0,T]. (2.2)

    Proof. Since (1.1) is a linear equations with conditions (1.4)(1.6), the existence and uniqueness of the solution can be proved by Galerkin's method (see [27]). Meanwhile, estimates (2.1) are also derived (see [27], Chapter III, Theorem 2.2). According to E=×H in Section 1 and Lemma 3 in [7], we find that ×H=EH1(Ω) and ×HH1(Ω)C2G2L2(Ω). Finally, by virtue of Sobolev's embedding theorem with N=3, we can derive the desired estimate (2.2).

    Remark 1. Note that the boundary condition (1.4) gives no information about n×[×H] on SΓ1. We eliminate this portion of the integral by taking test function Φ such that ΥT(Φ)=0 on SΓ1. Hence, the variational problem of Lemma 1 leaves only the integral term on SΓ2.

    Next, a stability result is established which will be useful for deriving the first-order necessary optimality conditions for Problem (P) in Section 1.

    Lemma 2. In addition to the assumptions A(2.1) and A(2.2), assume that H1 and H2 are two weak solutions of the system (1.1) and (1.4)(1.6) corresponding to G1 and G2, respectively. Then the following stability estimate holds:

    H1H2L2(0,T;V(curl,Ω))CG1G2L2(0,T;L2(Γ2)),

    where the constant C depends only on known data in A(2.2).

    Proof. Define G=G1G2 and H=H1H2. Then, in the sense of weak solution, HL2(0,T;X) solves the system

    {Ht+××H=0,(x,t)QT,n×H=0,(x,t)SΓ1,n×[×H(x,t)]=n×G(x,t),(x,t)SΓ2,H(x,0)=0,xΩ.

    By means of similar estimates in (2.1), it can then be shown that the required estimate holds.

    With the weak solution HL2(0,T;X) of problem (1.1) and (1.4)(1.6), we now turn to study the problem (1.2), (1.3) and (1.6)(1.8) (i.e., the phase field problem). Let us list some Banach spaces:

    W(0,T)={uL2(0,T;H1(Ω)):utL2(0,T;H1(Ω))},W2,12(QT)={uL2(QT):uxi,uxixj,utL2(QT),i=1,2,3},W24(Ω)={uL4(Ω):uxi,uxixjL4(Ω),i=1,2,3}.

    We impose some basic assumptions which ensure the well-posedness of controlled system:

    A(2.3) (a) Let u0(),uT()L2(Ω) be nonnegative.

    (b) The function k:ΩR is given with 0<k1k(x)k2 for constants k1 and k2.

    A(2.4) Function ϕ0()W24(Ω) satisfying ϕ0n|Ω=0 and ϕT()L2(Ω) is nonnegative.

    In order to study the phase field model, we state some lemmas.

    Lemma 3. (Lions-Peetre's embedding theorem [28])The embedding W2,12(QT)L10(QT) is continuous. Moreover, whenever 2˜p<10, the embedding W2,12(QT)L˜p(QT) is compact.

    Lemma 4. Assume that vL2(QT) and ψ0W24(Ω) with ψ0n|Ω=0. Then the following problem

    {ψtψ12(ψψ3)=v(x,t),(x,t)QT,ψn(x,t)=0,(x,t)SΓ,ψ(x,0)=ψ0(x),xΩ, (2.3)

    has a unique strong solution ψW2,12(QT) satisfying

    ψW2,12(QT)C(ψ0W24(Ω)+vL2(Ω)+C0), (2.4)

    where C0=maxyR(32y214y4) and C is a constant only depends on Ω and T.

    Proof. The proof is given by applying Leray-Schauder's fixed point theorem (see [29]). To this end, let B=L6(QT) and consider the mapping Tσ:BB, which is given by

    Tσ(η)=ψ,

    where σ[0,1] and ψ is the unique solution of the following linear system:

    {ψtψ=σ[12(ηη3)+2v(x,t)],(x,t)QT,ψn(x,t)=0,(x,t)SΓ,ψ(x,0)=ψ0(x),xΩ. (2.5)

    It is not hard to know that σ[12(ηη3)+2v]L2(QT). By using the Lp-theory of parabolic equation, the system (2.5) has a unique solution ψW2,12(QT). From Lemma 3, mapping Tσ is compact on B.

    Next, let ψB be a fixed point of Tσ for some σ[0,1]. Thus, ψ solves the following problem

    {ψtψ=σ[12(ψψ3)+2v(x,t)],(x,t)QT,ψn(x,t)=0,(x,t)SΓ,ψ(x,0)=ψ0(x),xΩ. (2.6)

    Multiplying Eq (2.6) by ψ, integrating on (0,t)×Ω with t[0,T], integrating by parts and applying Young's inequality, it follows that

    Ωψ2(t)dx+t0Ω|ψ|2dxdt+t0Ω|ψ|4dxdtC1[T0Ωv2dxdt+Ωψ20(x)dx+maxyR(32y214y4)], (2.7)

    where C1 only depends on Ω and T.

    Multiplying Eq (2.6) by ψt and making the similar operation as before, it is not hard to get that

    Ωψ4(t)dx+Ω|ψ|2dxdt+t0Ωψ2tdxdtC2(Ω|ψ0|2dxdt+t0Ωv2dxdt+Ωψ40dxdt+Ωψ2(t)dx), (2.8)

    where C2 only depends on T.

    Multiplying Eq (2.6) by ψ and performing the similar calculation, it yields that

    Ω|ψ(t)|2dx+t0Ω|ψ|2dxdt+t0Ωψ2|ψ|2dxdtC3(Ω|ψ0|2dxdt+t0Ωv2dxdt+t0Ω|ψ|2dxdt), (2.9)

    where C3 only depends on T.

    According to (2.7)–(2.9), we take C=max(C1,C2,C2)0 which depends on Ω and T, such that

    ψW2,12(QT)C(ψ0W24(Ω)+vL2(Ω)+C0), (2.10)

    where C0=maxyR(32y214y4).

    By the compact embedding W2,12(QT)L6(QT), we get

    ψBCψW2,12(QT)C.

    where the positive constant C does not depend on σ.

    By Leray-Schauder's fixed point theorem, there exists a fixed point ψL6(QT)W2,12(QT) for the operator T1, i.e., ψ=T1ψ.

    The rest of the work is to prove the uniqueness of the solution. Let vL2(QT) and ψ1,ψ2(i=1,2) be two solutions of problem (2.3). Then Ψ:=ψ1ψ2 satisfies the following problem

    {ΨtΨ=D(ψ1,ψ2)Ψ,(x,t)QT,Ψn(x,t)=0,(x,t)SΓ,Ψ(x,0)=0,xΩ, (2.11)

    where D(ψ1,ψ2)=12[1(ψ21+ψ1ψ2+ψ22)]L5(QT) by applying Lemma 3 and D(ψ1,ψ2)12.

    Testing the equation in (2.11) by etΨ(x,t), integrating by parts, it holds that

    ΩΨ2(t)etdx+t0Ω|Ψ|2etdxdt=t0Ω(12+D)Ψ2etdxdt0.

    Therefore, one can obtain that

    ΩΨ2(t)etdx=t0Ω|Ψ|2etdxdt=0,

    which implies that Ψ=0 a.e. xΩ for every t[0,T].

    Lemma 5. [30,p175–177] Under assumption A(2.3), for any given function fL2(QT), the following problem:

    {ut(k(x)u)=f(x,t),(x,t)QT,un(x,t)=0,(x,t)SΓ,u(x,0)=u0(x),xΩ

    has a unique weak solution uW(0,T). Moreover, there exists a positive constant C which depends on known data, such that

    uW(0,T)C(u0L2(Ω)+fL2(QT)). (2.12)

    It follows from Lemmas 4 and 5 that there is a unique solution for the problem (1.2)(1.3) and (1.7)(1.8).

    Lemma 6. Under the assumptions A(2.1)A(2.4), the coupled system (1.2)(1.3) with the initial boundary condition (1.7)(1.8) has at least one solution (u,ϕ)W(0,T)×W2,12(QT) for any given HL2(0,T;X). Moreover, the following estimates hold:

    uW(0,T)+ϕW2,12(QT)C(ϕ0W24(Ω)+u0L2(Ω)+G2L2(0,T;L2(Γ2))+C0), (2.13)

    where the positive constants C and C0 depend on known data.

    Proof. Let B=L2(QT). Define a mapping Tσ:BB by

    Tσv=u,

    where σ[0,1] and u is the unique solution of the following problem:

    {ut(k(x)u)=|×H|212lϕt,(x,t)QT,ϕtϕ12(ϕϕ3)=2σv,(x,t)QT,(un(x,t),ϕn(x,t))=(0,0),(x,t)SΓ,(u(x,0),ϕ(x,0))=(u0(x),ϕ0(x)),xΩ. (2.14)

    The first equation of (2.14) has a unique solution by Lemma 4. Combining Lemma 1, we can get |×H(x,t)|212lϕt(x,t)L2(QT). It follows from Lemma 5 that the second equation of (2.14) has a unique solution uW(0,T). Note that W(0,T)L2(QT) are compact by Aubin's Lemma ([30], p148). Therefore, the mapping Tσ is well defined and compact from B into B.

    It remains to estimate all fixed points of Tσ. Assume that uB is a fixed point, i.e., Tσu=u. Then,

    {ut(k(x)u)=|×H|212lϕt,(x,t)QT,ϕtϕ12(ϕϕ3)=2σu,(x,t)QT,(un(x,t),ϕn(x,t))=(0,0),(x,t)SΓ,(u(x,0),ϕ(x,0))=(u0(x),ϕ0(x)),xΩ. (2.15)

    Multiplying the first equation of (2.15) by u+12lσϕ, integrating over Ω×(0,t) with 0tT, integrating by parts, using Young's inequality, we know that

    12(1σlε)Ωu2(t)dx+12(l2σ24σlC(ε))Ωϕ2(t)dx+k1(1lσ2ε)t0Ω|u|2dxdtlk1σ2C(ε)t0Ω|ϕ|2dxdtC(t0Ωu2dxdt+t0Ωϕ2dxdt+u02L2(Ω)+ϕ02L2(Ω)+G4L2(0,T;L2(Γ2))), (2.16)

    where ε and ε are two sufficiently small parameters, C(ε) and C(ε) are sufficiently large constants corresponding to ε and ε, respectively.

    Multiplying the first equation of (2.15) by ϕ and acting the similar process as before, it yields that

    12Ωϕ2(t)dx+t0Ω|ϕ|2dxdt+14t0Ωϕ4dxdtC[maxyR(x,t)QT(12y214y4)+ϕ02L2(Ω)+t0Ωu2dxdt+t0Ωϕ2dxdt]. (2.17)

    Multiplying (2.17) by A>0 and adding it to (2.16). It can be easily deduced that

    12(1σlε)Ωu2(t)dx+12(A+l2σ24σlC(ε))Ωϕ2(t)dx+k1(1lσ2ε)t0Ω|u|2dxdt+(Alk1σ2C(ε))t0Ω|ϕ|2dxdt+A4t0Ωϕ4dxdtC[t0Ω(u2+ϕ2)dxdt+u02L2(Ω)+ϕ02L2(Ω)+G4L2(0,T;L2(Γ2))+C0], (2.18)

    where C0=maxyR(12y214y4) and AR is an arbitrary parameter. Choosing the appropriate A,ε and ε, it can be ensured that all the integrals on the left side of (2.18) are positive. This means that there exists a constant C>0 such that

    Ω[u2(t)+ϕ2(t)]dxΩ[u2(t)+ϕ2(t)]dx+t0Ω(|u|2+|ϕ|2+ϕ4)dxdtC[t0Ω(u2+ϕ2)dxdt+u02L2(Ω)+ϕ02L2(Ω)+G4L2(0,T;L2(Γ2))+C0]. (2.19)

    By Gronwall's inequality, it implies that

    Ω[u2(t)+ϕ2(t)]dxC(u02L2(Ω)+ϕ02L2(Ω)+G4L2(0,T;L2(Γ2))+C0),

    Substituting the previous inequlity into (2.19), it produces that

    Ω[u2(t)+ϕ2(t)]dx+t0Ω(|u|2+|ϕ|2+ϕ4)dxdt2C(u02L2(Ω)+ϕ02L2(Ω)+G4L2(0,T;L2(Γ2))+C0) (2.20)

    for all t[0,T].

    Multiplying the second equation of (2.14) respectively by ϕt and ϕ and performing the similar calculation, one can get

    Ω[ϕ4(t)+|ϕ(t)|2]dx+t0Ωϕ2tdxdtC(ϕ02L2(Ω)+ϕ2L2(Ω)+ϕ04L4(Ω)+u2L2(QT)) (2.21)

    and

    Ω|ϕ(t)|2dx+t0Ω(|ϕ|2+ϕ2|ϕ|2)dxdtC(ϕ02L2(Ω)+ϕ2L2(QT)+u2L2(QT)). (2.22)

    Combining (2.20)–(2.22), one can obtain

    ϕW2,12(QT)C(ϕ0W24(Ω)+u0L2(Ω)+G2L2(0,T;L2(Γ2))+C0). (2.23)

    Invoking (2.12) in Lemma 5, one have the following estimate

    t0utH1(Ω)dtC(u0L2(Ω)+ϕtL2(QT)+G2L2(0,T;L2(Γ2))). (2.24)

    Estimates (2.20) and (2.24) yield to

    uW(0,T)C(u0L2(Ω)+ϕ0L2(QT)+G2L2(0,T;L2(Γ2))+C0). (2.25)

    It follows from (2.25) and the embedding W(0,T)L2(QT) that all fixed points of Tσ are uniformly bounded in B. By Leray–Schauder's fixed point theorem, there exists a fixed point uL2(QT)W(0,T) of the operator T1, i.e., u=T1u.

    Next, we will establish a stability result.

    Lemma 7. Suppose that Hi(i=1,2) are two weak solutions of the system (1.1) and (1.4)(1.6) corresponding to Gi(i=1,2) and (ui,ϕi)(i=1,2) are two solutions of the phase equations (1.2), (1.3), (1.7) and (1.8). Then the following stability estimate holds.

    u1u2W(0,T)+ϕ1ϕ2W2,12(QT)CG1G2L2(0,T;L2(Γ2)), (2.26)

    where the constant C depends only on known data in A(2.2).

    Proof. Define H=H1H2,u=u1u2 and ϕ=ϕ1ϕ2. Then (u,ϕ)W(0,T)×W2,12(QT) is a solution of the following problem.

    {ut[k(x)u]=×(H1+H2)×H12lϕt,(x,t)QT,ϕtϕ=D(ϕ1,ϕ2)ϕ+2u,(x,t)QT,(un(x,t),ϕn(x,t))=(0,0),(x,t)SΓ,(u(x,0),ϕ(x,0))=(0,0),xΩ, (2.27)

    where D(ϕ1,ϕ2)=12[1(ϕ21+ϕ1ϕ2+ϕ22)]12 and D(ϕ1,ϕ2)L5(QT).

    Multiplying the second equation of (2.27) by etϕ, integrating on Ω×(0,t), one can obtain that

    Ωϕ2(t)dx+t0Ω|ϕ|2dxdtC(t0Ωu2dxdt+t0Ωϕ2dxdt). (2.28)

    Gronwall's inequality implies that

    Ωϕ2(t)dx+t0Ω|ϕ|2dxdtCT0Ωu2dxdt. (2.29)

    Testing the first equation of (2.27) by u+l2ϕ, integrating by parts and using Young's, Hölder's and Cauchy's inequalities, we get

    1lε2Ωu2(t)dx+(l8lC(ε)2)Ωϕ2(t)dx+(k1l2k2ε)t0Ω|u|2dxdtlk2C(ε)2t0Ω|ϕ|2dxdt12(t0Ω|×(H1+H2)|4dxdt)14[(t0Ω|×H|4dxdt)12+t0Ω|u|2dxdt]. (2.30)

    Mltiplying (2.28) by a parameter A>0 and adding it to (2.30), next, choosing suitable parameters A,ε,ε such that the coefficients of Ωu2dx,Ωϕ2dx,t0Ω|u|2dxdt and t0Ω|ϕ|2dxdt are all nonnegative, then there exists a constant C such that

    Ω[u2(t)+ϕ2(t)]dx+t0Ω(|u|2+|ϕ|2)dxdtC[(t0Ω|×H|4dxdt)12+t0Ω(|u|2+|ϕ|2)dxdt].

    Using the Gronwall's inequality, one obtains

    Ω[u2(t)+ϕ2(t)]dx+T0Ω(|u|2+|ϕ|2)dxdtC(T0Ω|×H|4dxdt)12. (2.31)

    Similarly, testing the second equation of (2.27) by ϕt, integrating by parts and using Young's, Hölder's and Cauchy's inequalities, we get

    t0Ωϕ2tdxdt+Ω|ϕ(t)|2dxC[t0Ωu2dxdt+(t0Ωϕ103dxdt)35], (2.32)

    where C depends on DL5(QT).

    Finally, testing the second equation of (2.27) by ϕ, integrating by parts and using Young's, Hölder's and Cauchy's inequality, we get

    t0Ω|ϕ|2dxdt+Ω|ϕ(t)|2dxC[t0Ω|u|2dxdt+(t0Ωϕ103dxdt)35], (2.33)

    where C depends on DL5(QT).

    Combining (2.31)–(2.33), we find that

    ϕW2,12(QT)C(ϕL103(QT)+×HL4(QT)). (2.34)

    Since W2,12(QT)L103(QT), the following interpolation inequality holds

    ϕL103(QT)εϕW2,12(QT)+C(ε)ϕL2(QT). (2.35)

    Substituting (2.35) in (2.34), choosing the appropriate ε and invoking (2.33), it follows that

    ϕW2,12(QT)C×HL4(QT)CG1G2L2(0,T;L2(Γ2)). (2.36)

    By Lemma 5, we also have

    utL2(0,T;H1(Ω))CG1G2L2(0,T;L2(Γ2)). (2.37)

    Finally, estimates (2.31) and (2.37) yield

    uW(0,T)CG1G2L2(0,T;L2(Γ2)).

    Corollary 1. Under the assumptions A(2.1)A(2.4), the solution (u,ϕ)W(0,T)×W2,12(QT) in Lemma 6 is unique.

    With Lemmas 1, 6 and 7, we can obtain the following theorems.

    Theorem 1. Under the assumptions A(2.1)A(2.4), the coupled system (1.1)(1.8) has a unique solution (H,u,ϕ)L2(0,T;X)×W(0,T)×W2,12(QT). Meanwhile, there exists a constant K1 such that

    supt[0,T]H(,t)L2(Ω)+HL2(0,T;V(curl,Ω))+uW(0,T)+ϕW2,12(QT)K1. (2.38)

    Definition 1. The mapping

    P:L2(0,T;L2(Γ2))L2(0,T;X)×W(0,T)×W2,12(QT),GP(G)=(H,u,ϕ),

    defined by Theorem 1 is called the control-to-state operator.

    In this section, we give and show several important properties of P, which will be very useful in proving the existence of optimal control and deriving optimality conditions.

    Theorem 2. Under the assumptions A(2.1)A(2.4), the operator P is weakly sequentially continuous.

    Proof. Taking {Gm}m=1L2(0,T;L2(Γ2)) such that

    GmG weakly in L2(0,T;L2(Γ2)), whenever m+. (3.1)

    Assuming that (Hm,um,ϕm) is the solution of (1.1)(1.8) associated with Gm for m=1,2,, i.e.,

    P(Gm)=(Hm,um,ϕm).

    We will show that there exists (H,u,ϕ)L2(0,T;X)×W(0,T)×W2,12(QT) such that

    P(Gm)P(G)=(H,u,ϕ)

    weakly in L2(0,T;X)×W(0,T)×W2,12(QT), as m.

    According to the definition of P, it follows that

    T0ΩHmΦtdxdt+T0Ω×Hm×Φdxdt=ΩH0(x)Φ(x,0)dxT0n×Gm,ΥT(Φ)Γ2dt, (3.2)
    T0Ωumvtdxdt+T0Ωkumvdxdt=Ωu0(x)v(0,x)dx+T0Ω|×Hm|2vdxdtl2T0Ω(ϕm)tvdxdt, (3.3)
    T0Ωϕmηtdxdt+T0Ωϕmηdxdt+12T0Ω(ϕmϕ3m)ηdxdt=Ωϕ0(x)η(x,0)dx2T0Ωumηdxdt, (3.4)

    for any vH1(QT) with v(T,x)=0, ΦH1(0,T;X) with Φ(x,T)=0 and ηW2,12(QT) with η(x,T)=0. By Theorem 1, the sequence {(Hm,um,ϕm)} is bounded in reflexive space L2(0,T;V(curl,Ω))×W(0,T)×W2,12(QT). Thus, there is a subsequence of {(Hm,um,ϕm)}, again denoted by {(Hm,um,ϕm)}, such that

    HmH weakly in L2(0,T;V(curl,Ω)), (3.5)
    umu weakly in L2(QT), (3.6)
    umu weakly in L2(0,T;L2(Ω)), (3.7)
    ×Hm×H weakly in L2(0,T;L2(Ω)), (3.8)
    ϕmϕ weakly in W2,12(QT). (3.9)

    It follows from Eq (3.2) and (3.5), (3.8) that

    T0n×Gm,ΥT(Φ)Γ2dtΩH0(x)Φ(x,0)dxT0ΩHΦtdxdtT0Ω×H×Φdxdt

    as m. It can be verified from (3.1) that

    T0ΩHΦtdxdt+T0Ω×H×Φdxdt=ΩH0(x)Φ(x,0)dxT0n×G,ΥT(Φ)Γ2dt (3.10)

    From the compact embedding W2,12(QT)L6(Ω), we obtain

    ϕmϕstrongly in L6(QT). (3.11)

    It follows from Eqs (3.4) and (3.6), (3.9), (3.11) that

    T0Ωϕηtdxdt+T0Ωϕηdxdt+12T0Ω(ϕ(ϕ)3)ηdxdt=Ωϕ0(x)η(x,0)dx2T0Ωuηdxdt. (3.12)

    Since ×Hm(,t)L6(Ω) and ×H6L6(Ω)G2L2(Γ2), we have

    ×Hm(,t)×H(,t) weakly in L6(Ω). (3.13)

    It follows from Eqs (3.4) and (3.6), (3.7), (3.13) that

    T0Ωuvtdx+T0Ωk(x)uvdx=Ωu0(x)v(0,x)dx+T0Ω|×H|2vdxl2T0Ωϕtvdxdt, (3.14)

    Equations (3.10), (3.12) and (3.14) imply that (H,u,ϕ) is a weakly solution of problem (2.1) corresponding to G. That is P(G)=(H,u,ϕ). The above statement shows that every subsequence has a subsequence converging to the same (H,u,ϕ). Hence, the entire sequence (Hm,um,ϕm) converges weakly to (H,u,ϕ).

    With Lemmas 2 and 7, one can easily see that P is Lipschitz continuous.

    Theorem 3. Under the assumptions A(2.1)A(2.4), the operator P is Lipschitz continuous, that is, there exists a constant L>0 such that

    H1H2L2(0,T;V(curl,Ω))+u1u2W(0,T)+ϕ1ϕ2W2,12(QT)LG1G2L2(0,T;L2(Γ2)),

    whenever GiL2(0,T;L2(Γ2)) and (Hi,ui,ϕi)=P(Gi),i=1,2.

    Theorem 4. Under the assumptions A(2.1)A(2.4), the operator P is Fréchet differentiable. Its directional derivative at GUad in the direction ˉG is given by

    P(G)ˉG=(ˉH,ˉu,ˉϕ),

    where the triple of functions (ˉH,ˉu,ˉϕ) denotes the weakly solution of the following linear system at (H,u,ϕ)=P(G) :

    {ˉHt+××ˉH=0,(x,t)QT,ˉut[k(x)ˉu]=2×H×ˉH12lˉϕt,(x,t)QT,ˉϕtˉϕ12ˉϕ(13ϕ2)=2ˉu,(x,t)QT,n×ˉH=0,(x,t)SΓ1,n×(×ˉH)=n×ˉG,(x,t)SΓ2,ˉH(x,0)=0,xΩ.(ˉun(x,t),ˉϕn(x,t))=(0,0),(x,t)SΓ,(ˉu(x,0),ˉϕ(x,0))=(0,0),xΩ. (3.15)

    Proof. We present the proof in the following steps.

    Step 1: We show that the operator P is Gâteaux differentiable for each GUad.

    Set Gε=G+εˉG with a sufficiently small parameter ε>0 such that G+εˉGUad. Moreover, assume that (Hε,uε,ϕε) is the solution of (1.1)(1.8) corresponding to Gε. Define

    ˉHε=HεHε,ˉuε=uεuε,ˉϕε=ϕεϕε.

    It is easily shown that (ˉHε,ˉuε,ˉϕε) satisfies

    {(ˉHε)t+××ˉHε=0,(x,t)QT,(ˉuε)t[k(x)ˉuε]=[×(Hε+H)]×ˉHε12l(ˉϕε)t,(x,t)QT,(ˉϕε)tˉϕε12ˉϕε[1(ϕ2ε+ϕεϕ+ϕ2)]=2ˉuε,(x,t)QT,n×ˉHε=0,(x,t)SΓ1,n×(×ˉHε)=n×ˉG,(x,t)SΓ2,ˉHε(x,0)=0,xΩ.((ˉuε)n(x,t),(ˉϕε)n(x,t))=(0,0),(x,t)SΓ,(ˉuε(x,0),ˉϕε(x,0))=(0,0),xΩ. (3.16)

    Under assumptions A(2.2) and A(2.3), by using similar estimates as Theorem 3, we can derive the following estimates:

    ˉHεL2(0,T;V(curl,Ω))+ˉuεW(0,T)+ˉϕεW2,12(QT)CˉGL2(0,T;L2(Γ2)), (3.17)
    HεHL2(0,T;V(curl,Ω))+uεuW(0,T)+ϕεϕW2,12(QT)CεˉGL2(0,T;L2(Γ2)), (3.18)

    where C and C depend only on known data. It follows from (3.17) that there exists a subsequence of (ˉHε,ˉuε,ˉϕε) (still denoted by (ˉHε,ˉuε,ˉϕε)) and (ˉH,ˉu,ˉϕ)L2(0,T;V(curl,Ω))×W(0,T)×W2,12(QT) such that

    ˉHεˉH weakly in L2(0,T;V(curl,Ω)), (3.19)
    ˉuεˉu weakly in L2(QT), (3.20)
    ˉuεˉu weakly in L2(0,T;L2(Ω)), (3.21)
    ×ˉHε×ˉH weakly in L2(0,T;L2(Ω)), (3.22)
    ˉϕεˉϕ weakly in W2,12(QT), (3.23)

    as ε0.

    It is easy to show that ×ˉHε(,t)L6(Ω) and ×ˉHε6L6(Ω)ˉG2L2(Γ2). Therefore,

    ×ˉHε(,t)×ˉH(,t) weakly in L6(Ω). (3.24)

    By the compact embedding W2,12(QT)Li(QT)(i=2,3,,9) and (3.18)–(3.24), taking the limits of (3.16) as ε0, we obtain that (ˉH,ˉu,ˉϕ) satisfies the problem (3.15).

    The uniqueness of solution for the system (3.15) is easy to prove because it is linear. The calculations above means that the control-to-state operator P is Gâteaux differentiable at G, that is,

    DP(G;ˉG)=(ˉH,ˉu,ˉϕ)(G;ˉG).

    Step 2: We show that DP(G;ˉG) is a linear bounded operator with respect to ˉG.

    Obviously, DP(G;ˉG) is linear. Similar to Lemmas 2 and 7, it can be concluded from (3.15) that

    ˉHL2(0,T;V(curl,Ω))+ˉuW(0,T)+ˉϕW2,12(QT)CKL2(0,T;L2(Γ2)),

    which means that DP(G;ˉG) is bounded with respect to ˉG. Hence, one has

    DP(G;ˉG)=(ˉH,ˉu,ˉϕ)(G;ˉG)=P(G)ˉG,

    where P(G) is a bounded and linear operator.

    Step 3: We verify that P(G) is continuous with G.

    Choosing G1,G2Uad, for any KUad with KL2(0,T;L2(Γ2))=1, define

    (˜H,˜u,˜ϕ):=(ˉH,ˉu,ˉϕ)(G1;K)(ˉH,ˉu,ˉϕ)(G2;K).

    It is easy to verify that (˜H,˜u,˜ϕ)L2(0,T;X)×W(0,T)×W2,12(QT) satisfies the following system in weakly sense.

    {˜Ht+×טH=0, in QT,˜ut[k(x)˜u]=f112l˜ϕt, in QT,˜ϕt˜ϕ=(1213ϕ2(G2))˜ϕ+f2+2˜u, in QT,nטH=0, in SΓ1,n×(טH)=0, in SΓ2,˜H(x,0)=0, in Ω,(˜un(x,t),˜ϕn(x,t))=(0,0), in SΓ,(˜u(x,0),˜ϕ(x,0))=(0,0), in Ω, (3.25)

    where

    f1=2[×H(G1)×ˉH(G1;K)×H(G2)×ˉH(G2;K)],f2=13ˉϕ(G1;K)(ϕ(G1)+ϕ(G2))(ϕ(G1)ϕ(G2)).

    Obviously, (3.25) implies ˜H=0 which directly means ˉH(G1;K)=ˉH(G2;K). Therefore, (3.25) can be simplified as the following system

    {˜ut[k(x)˜u]=2×H(G1,K)×(H(G1)H(G2))12l˜ϕt, in QT,˜ϕt˜ϕ=(1213ϕ2(G2))˜ϕ+f2+2˜u, in QT,(˜un(x,t),˜ϕn(x,t))=(0,0), in SΓ,(˜u(x,0),˜ϕ(x,0))=(0,0), in Ω.

    Similar to Lemma 7, the following estimates can be derived

    ˜uW(0,T)+˜ϕW2,12(QT)C(f2L2(QT)+×(H(G1)H(G2))L4(QT))CG1G2L2(0,T;L2(Γ2))KL2(0,T;L2(Γ2)).

    In addition, we also have estimates:

    ˜HL2(0,T;V(curl,Ω))+˜uW(0,T)+˜ϕW2,12(QT)CG1G2L2(0,T;L2(Γ2))KL2(0,T;L2(Γ2)).

    This completes the proof.

    In this section, we will show the existence of an optimal control for problem (P).

    Theorem 5. Under the assumptions A(2.1)A(2.4), there exists an optimal control for the problem (P).

    Proof. Owing to P(G)=(H,u,ϕ), we can eliminate H,u and ϕ from J to obtain the reduced cost functional

    J(G;H,u,ϕ)=J(G;P(G))=:f(G).

    Since f(G)0, there exists the infimum

    j:=infGUadf(G)R,

    and there is a minimizing sequence {Gm}m=1Uad such that limmf(Gm)=j.

    It follows from {Gm}m=1Uad and GmL2(0,T;L2(Γ2))< that there exists a subsequence of {Gm}m=1Uad, again denoted by {Gm}m=1Uad, such that

    GmG weakly in L2(0,T;L2(Γ2)).

    Moreover, the closeness of set Uad implies that GUad.

    Observe that f is weakly sequentially lower semi-continuous and the control-to-state operator P is weakly sequentially continuous by Theorem 2. Consequently,

    j=limmf(Gm)f(G)j.

    Therefore, G is an optimal control.

    Using the Lagrange technique, we can deduce the adjoint system of (1.1)(1.8) as follows:

    {Nt××N=×[2p×H0],(x,t)QT,pt+[k(x)p]=2ψ,(x,t)QT,ψt+ψ+12ψ[13(ϕ0)2]=12lpt,(x,t)QT,n×N=0,(x,t)SΓ1,n×(×N)=n×[2p×H0],(x,t)SΓ2,N(x,T)=0,xΩ,(pn(x,t),ψn(x,t))=(0,0),(x,t)SΓ,(p(x,T),ψ(x,T))=(u0(T)uT,ϕ0(x,T)ϕT(x)12lp(x,T)),xΩ, (4.1)

    where (H0,u0,ϕ0) is a solution of (1.1)(1.8) corresponding to G0Uad.

    The equations for the adjoint states N,p and ψ run backwards in time.

    Theorem 6. In addition to the assumptions A(2.1)A(2.4), assume that (H0,u0,ϕ0) is the optimal solution of the system (1.1)(1.8) corresponding to the optimal control G0Uad. Then the adjoint system (4.1) has a unique solution (N,p,ψ)L2(0,T;X)×W(0,T)×W2,12(QT).

    Proof. By taking t=Tτ with τ[0,T], the functions N,p,ψ,H0,u0 and ϕ0 are transformed into ˜N,˜p,˜ψ,˜H0,˜u0 and ˜ϕ0, respectively. Consequently, the solution of (4.1) is equivalent to the solution to the (forward) parabolic initial-boundary value problem:

    {˜Nτ+×טN=×[2˜pטH0],(x,τ)QT,˜pτ+[k(x)˜p]=2˜ψ,(x,τ)QT,˜ψτ+˜ψ+12˜ψ[13(˜ϕ0)2]=12l˜pτ,(x,τ)QT,nטN=0,(x,τ)SΓ1,n×(טN)=n×(2˜pטH0),(x,τ)SΓ2,˜N(x,0)=0,xΩ,(˜pn(x,τ),˜ψn(x,τ))=(0,0),(x,τ)SΓ,(˜p(x,0),˜ψ(x,0))=(˜u0(0)uT,˜ϕ0(0)ϕT(x)12l˜p(x,0)),xΩ. (4.2)

    Note that this is a linear parabolic system, the existence and uniqueness of solution are easily proved.

    Theorem 7. In addition to the assumptions A(2.1)A(2.4), suppose that (H0,u0,ϕ0) is the optimal solution of the system (1.1)(1.8) corresponding to the optimal control G0Uad. Then there exists (N,p,ψ), which satisfies the adjoint system (4.1). Moreover, the following inequality is satisfied:

    T0Γ2[n×(GG0)ΥT(N)+λG0(GG0)]dsdt0,GUad.

    Proof. Substituting P(G0)=(H0,u0,ϕ0) into (1.9), one can obtain the reduced cost functional f,

    J(G0;H0,u0,ϕ0)=J(G0;P(G0))=:f(G0).

    By Theorem 5, the Fréchet derivative of f(G) is given by

    f(G0)(GG0)=Ω[u0(T)uT]ˉu(T)dx+Ω[ϕ0(T)ϕT]ˉψ(T)dx+λT0Γ2G0(GG0)dsdt, (4.3)

    where (ˉH,ˉu,ˉψ) is the solution of the problem (3.15) with ˉG=GG0

    Multiplying the second equation of problem (3.15) by the adjoint state p, integrating over Ω×[0,T] and integrating by parts, one can find that

    Ω[u0(T)uT]ˉu(T)dxT0Ω[pt+[k(x)p]]ˉudxdt=T0Ω2×ˉH×H0pdxdtl2Ωˉϕ(T)p(T)dxdt+l2T0Ωˉϕptdxdt. (4.4)

    Substituting the second equation in (4.1) into (4.4), it can be seen that

    Ω[u0(x,T)uT]ˉu(T)dx=T0Ω(2×ˉH×H0p+l2ˉϕpt2ψˉu)dxdtl2Ωˉϕ(T)[u0(T))uT]dxdt. (4.5)

    Multiplying the first equation in (4.1) and the first equation of (3.15) by ˉH and N, respectively, integrating over Ω×[0,T] and integrating by parts, we obtain

    T0ΩNˉHtdxdt+T0Ω×N×ˉHdxdt=T0Ω2p×H0×ˉHdxdt (4.6)

    and

    T0ΩNˉHtdxdt+T0Ω×N×ˉHdxdt=T0Γ2n×(GG0)ΥT(N)dsdt. (4.7)

    From (4.5)–(4.7), one has

    Ω[u0(x,T)uT]ˉu(T)dx=T0Ω[l2ˉϕpt2ψˉu]dxdtl2Ωˉϕ(T)[u0(T))uT]dxdtT0Γ2n×(GG0)ΥT(N)dsdt.

    Now we turn to the integral Ω(ϕ0(T))ϕT)ˉψ(T)dx. Analogously, multiplying the third of (3.15) by ψ and then integrating by parts, it yields that

    Ω[ϕ0(T))ϕT]ˉψ(T)dx=T0Ω[ˉϕψt+ˉϕΔψ+12ˉϕ(13(ϕ0)2)ψ+2ˉuψ]dxdt+l2ΩP(T)ˉϕ(T)dx. (4.8)

    Multiplying the third equation in (4.1) by ˉϕ and integrating over Ω×[0,T], we have

    T0Ω[ˉϕψt+ˉϕΔψ+12ˉϕ(13(ϕ0)2)ψ]dxdt=l2T0ωptˉϕdxdt. (4.9)

    Substituting (4.9) into (4.8), we see that

    Ω[ϕ0(T))ϕT]ˉψ(T)dx=T0Ω(2ˉuψl2ptˉϕ)dxdt+l2ΩP(T)ˉϕ(T)dx.

    Recall that p(T)=u0(T)uT in (4.1). Therefore,

    Ω[u0(T))uT]ˉu(T)dx+Ω[ϕ0(T))ϕT]ˉψ(T)dx=T0Γ2n×(GG0)ΥT(N)dsdt. (4.10)

    Note that (H0,u0,ϕ0) is the optimal solution of the system (1.1)(1.8) corresponding to the optimal control G0Uad. Therefore, it can be concluded from (4.3) and (4.10) that

    0f(G0)(GG0)=T0Γ2[n×(GG0)ΥT(N)+λG0(GG0)]dsdt,GUad.

    The proof is completed.

    In this paper, we study an optimal control problem arising from a metal melting process by using a induction heating method. The controlled system is a nonlinear coupled system given by Maxwell's equations, heat equation and phase field equation. The goal of optimal control is to find the electric field action on a part of the boundary such that the temperature profile at the final stage has a relative uniform distribution and minimum energy consumption. The new existence and uniqueness theorem on the solution of controlled system is established in the case that the resistivity ρ(x,t)=1 or ρ does not depend on x. By defined a control-to-state operator P and studied its properties, we showed that there is at least one optimal control and derived the first order optimality condition.

    When the resistivity ρ(x,t) depends on position x, the heat source generated by the electromagnetic field is ρ|×H|2L1(QT), which cannot be guaranteed the requirement L2(QT) in proof of the existence of solutions for heat equation. This is a challenging problem. We intend to further work on this, as well as make a numerical simulation for the problem, in the near future.

    The authors would like to thank anonymous referees for helpful comments and suggestions which improved the original version of the paper. This work is supported by the National Natural Science Foundation of China (Nos. 11761021, 12001131), the Natural Science Foundation of Guizhou Province (No. [2018]1118) and the Foundation of Research Project for Graduate of Guizhou Province (No. YJSCXJH [2020]083).

    The authors declare that they have no competing interests.



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