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Research Article

A modified quasi-boundary value method for a backward problem for the inhomogeneous time conformable fractional heat equation in a cylinder

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Pages 1323-1342 | Received 14 Apr 2019, Accepted 28 Oct 2020, Published online: 18 Nov 2020

ABSTRACT

The time conformable heat equation is a generalization of classical heat equation involved local and limit-based derivative, which is called conformable fractional derivative. In this paper, we study a backward problem for the time conformable fractional heat equation defined in cylindrical coordinates for the axis-symmetric case which is a severely ill-posed problem. By using a modified quasi-boundary value method, the problem is regularized and some new error estimates are obtained. The numerical experiment shows that the method is feasible and effective.

AMS Subject Classifications:

1. Introduction

Fractional calculus appears in many fields of science and engineering, such as signal processing, finance and plasma physics, aerodynamics and control systems, viscoelasticity, bioengineering and biomedical [Citation1–3]. Many researchers tried to give a definition of fractional derivative. Most of them used an integral form of fractional derivative. One of the well-known fractional derivatives is the Riemann–Liouville fractional order derivative, for α[n1,n), the derivative of f is RLDaα(f)(t)=1Γ(nα)dndtnatf(x)(tx)αn+1dx. The second one is the so-called Caputo derivative, for α[n1,n), the derivative of f is CDaα(f)(t)=1Γ(nα)atf(n)(x)(tx)αn+1dx. Obviously, the RL and Caputo fractional derivatives are non-local operators represented by convolutional integrals with weakly singular kernels. The inverse problem for the heat equation where the time-derivative is in the sense of Caputo fractional order is of great interest to many researchers as these operators are effective for modelling of sub/super-anomalous behaviours of physical processes [Citation4–12].

Although non-local fractional derivatives give natural memory and genetic effects in the physical system, the fractional derivatives obtained in this kind of calculus seem very complicated and lose some basic properties of general derivatives, such as product rule and chain rule. Accordingly, the authors in [Citation13] define a new well-behaved simple fractional derivative called ‘the conformable derivative’ depending just on the basic limit defnition of the derivative and this concept seems to satisfy all the requirements of the standard derivative. Namely,

Definition 1.1

[Citation13] (CFD)

Given a function f:[0,)R. Then the conformable fractional derivative of order α(0,1) of f is defined by Dtαf(t)=limh0f(t+ht1α)f(t)h, for all t>0.

If f is αdifferentiable in some (0,a) and limt0+Dtαf(t) exists, then define Dtαf(0)=limt0+Dtαf(t). Note that if f is differentiable, then Dtαf(t)=t1αf(t), where f(t)=limh0f(t+h)f(t)h. They then proved the product rule, the fractional mean value theorem solved some (conformable) fractional differential equations where the fractional exponential function etαα played an important rule. While in case of well-known fractional calculus Mittag-Leffler functions generalized exponential functions.

This new theory is studied by Abdeljawad [Citation14] and Atangana [Citation15]. In addition, Anderson and Ulness in [Citation16] gave a potential application of the conformable derivative in quantum mechanics. In [Citation17], Dazhi Zhao et al. generalized the definition of conformable fractional derivative of order α(0,1) by means of Linear Extended Gteaux derivative (LEGD) to general conformable fractional derivative (GCFD). They also gave physical and geometrical interpretations of this new derivative which thus indicate potential applications in physics and engineering. The definition of the GCFD of arbitrary order given by them is as follows:

Definition 1.2

[Citation17] (GCFD of arbitrary order)

Let α(n,n+1], for some nN and f be n-differentiable at t>0. Then the α-fractional derivative of f is defined as Dψαf(t)=DψαnDnf(t)=limϵ0f(n)(t+ϵψ(t,αn))f(n)(t)ϵ, if the limit exists. When ψ(t,α)=t1α, Dψαf(t) coincides with Khalil's definition [Citation13]. In other words, CFD is a special case of GCFD. Then geometrical interpretations of the GCFD is that the gradient of a function f projects onto a function ψ(t,αn) or a special function ψ(t,αn) projects onto the gradient of a function f from a different viewpoint. And physical interpretation of GCFD can be regarded as a special velocity, its direction and strength rely on ψ(t,αn). Although the conformable derivative has no nonlocality [Citation18,Citation19], there exists some advantages for this kind of derivative such as the formula of integral by parts.

On partial differential equations with the conformable derivative, there are several studies. Çenesiz, Kurt and Nane in [Citation20] gave stochastic solutions of conformable fractional Cauchy problems by running the processes corresponding to Cauchy problems with a nonlinear deterministic clock. In [Citation21], Çenesiz et al. studied the solutions of time and space fractional heat differential equations and Fourier sine and Fourier cosine transform definitions were given. Hammad and Khalil in [Citation22] applied conformable Fourier series to interpret the solution for the conformable heat equation. In [Citation23], Avci et al. aimed to find the fundamental solution of a conformable heat equation acting on a radial symmetric plate. In [Citation24], Yavuz et al. aimed the numerical inverse Laplace homotopy technique for solving some interesting 1-D time-fractional heat equations based on the Laplace homotopy perturbation method. In [Citation25], Vu et al. studied an inverse time problem for the nonhomogeneous heat equation under the conformable derivative and obtained a Hölder-type estimation error for the whole time interval. In [Citation26], the authors introduced the conformable double Laplace transform which could be used to solve fractional partial differential equations that represented many physical and engineering models. In [Citation27], R. I. Nuruddeen et al. considered the fractional heat diffusion models featuring fractional order derivatives in both the Caputo's and the new conformable derivatives to further investigate the development by analysing two solutions. For more literature on solutions, refer to [Citation28–33].

Based on the above research, the inverse problem of heat equation under conformal derivatives is naturally considered. But there are few mathematical results about the time conformable heat equation in an axis-symmetric cylinder. In this study, we are concerned with a backward problem for the inhomogeneous time conformable fractional heat equation in a cylinder. Let us consider the following time conformable heat equation in an axis-symmetric cylinder (1) αtαu(r,z,t)=a2ur2+1rur+2uz2+f(r,z,t),(1) subjected to the following initial and boundary conditions given respectively as (2) u(r,z,0)=h(r,z),0<rR,(2) and (3) u(R,z,t)=u(0,z,t)=0,t>0, 0<zL,u(r,0,t)=u(r,L,t)=0,t>0, 0<rR,u is finite,t>0, 0<rR, 0<zL,(3) where αtα represents the conformable fractional derivative of order α(0<α1). a is thermal diffusivity constant and f(r,z,t) denotes a heat source.

Solving this equation with the given information f(r,z,t) and h(r,z) is called the direct problem. From the information given at final time (4) u(r,z,T)=g(r,z),(4) the goal of the inverse problem is to recover the information {u(r,z,t),h(r,z) initial condition} for 0t<T. This inverse backward problem is an ill-posed problem. We propose a modified quasi-boundary value method to solve it (refer to [Citation34]). In our method, the convergence speed will gradually increase corresponding to different levels of smoothness of the exact solution. Under some suitable conditions for exact solution u, we will introduce an error estimate of order δαpTα+αp(p>0).

The remainder of this paper is organized as follows. In Section 2, formulation for the problem (Equation1)–(Equation4) and the ill-posedness of the backward heat problem are presented. We construct the regularized solution by a modified quasi-boundary value method and study the well-posedness of problem (Equation22)–(Equation24) in Section 3. Section 4 provides the detailed convergence analysis under different levels of the smoothness of the exact solution. Finally, in Section 5, we give some numerical examples to verify the theory.

2. Formulation for the problem and the ill-posed backward heat problem

We introduce the Lebesgue space associated with the measure rdr, i.e. Lr2(Ω)=v:ΩR measurable;Ωv2(r,z)rdrdz<+, which is a Hilbert space with the scalar product u,vr=Ωu(r,z)v(r,z)rdrdz, and the corresponding norm is given by vLr2(Ω)=Ωv2(r,z)rdrdz12. The weighted Sobolev spaces defined on Ω are introduced as follows Hrm(Ω)=vLr2(Ω);p+qvrpzqLr2(Ω),p,qN,p+qm. Throughout this paper, for the convenience of writing, we denote ,r and by the inner product and the norm in Lr2(Ω), where Ω=(0,R)×(0,L). Let's first consider what the weak solution of the problem (Equation1)–(Equation3) is. We call a function uL2([0,T];Hr,01(Ω))C1((0,T);Hr2(Ω)) to be a weak solution for problem (Equation1)–(Equation3) if (5) dαdtαu(,,t),WLr2(Ω)u(,,t),WLr2(Ω)=f(,,t),WLr2(Ω),(5) for all functions WHr,01(Ω)Hr2(Ω). Here, W=a(2Wr2+1rWr+2Wz2). In fact, it is enough to choose W in the orthogonal basis of Lr2(Ω). So, next, we derive an analytical solution for the problem (Equation1)–(Equation3) based on the eigenfunction expansion and the eigenfunction system are complete and orthogonal with weight r in Lr2(Ω).

Let u(r,z,t)=X(r)Y(z)T(t), substitute it into the corresponding homogeneous equation for (1.1), then we get d2Xdr2+1rdXdrX(r)+d2Ydz2Y(z)1adαTdtαT(t)=0. This equation is true, meaning that the items in the formula should be constants, so we get d2Xdr2+1rdXdrX(r)=ρ,d2Ydz2Y(z)=l,1adαTdtαT(t)=λ, where ρ,l,λ are the undetermined constants introduced when separating variables, ρ+l=λ. Further, by separating the boundary conditions (Equation3), we get the following results (6) d2Xdr2+1rdXdr+ρX=0,r(0,R),X(0)=X(R)=0.(6) (7) d2Ydz2+lY=0,z(0,L),Y(0)=Y(L)=0.(7)

The eigenvalues of problem (Equation6) are (8) ρn=μnR2,n=1,2,,(8) and the corresponding eigenfunctions are Xn(r)=J0μnrR,n=1,2,, where μn denotes the zeros of Bessel function J0.

The eigenvalues of problem (Equation7) are (9) lm=mπL2,m=1,2,,(9) and the corresponding eigenfunctions are Ym(z)=sinmπLz,m=1,2,. {J0(μnrR)sin(mπLz)}n,m1 are complete and orthogonal in Lr2(Ω) and the follow orthogonality properties 0RJ0μnrRJ0μirRrdr=0,ni,R2J12(μn)2,n=i,0LsinmπLzsinkπLzdz=0,mk,L2,m=k. Thus the solution u(r,z,t) and nonhomogeneous term f(r,z,t) of problem (Equation1)–(Equation3) can be represented as follows (10) u(r,z,t)=m,n=1umn(t)J0μnrRsinmπLz,(10) (11) f(r,z,t)=m,n=1fmn(t)J0μnrRsinmπLz,(11) where umn(t), fmn(t) are the generalized Fourier coefficients.

By substituting (Equation10), (Equation11) into (Equation1) and (Equation2), in this case, the conformable fractional differential equation reduces to (12) dαumn(t)dtα+aμnR2+mπL2umn(t)=fmn(t),(12) (13) umn(0)=hmn,(13) where (14) fmn(t)=4LR2J12(μn)0R0LJ0μnrRsinmπLzf(r,z,t)rdrdz,(14) (15) hmn=4LR2J12(μn)0R0LJ0μnrRsinmπLzh(r,z)rdrdz.(15) By applying fractional Laplace transform (detailed solution process can be found in [Citation35]), we can get the solution of the initial problem (Equation12)–(Equation13) as follows (16) umn(t)=hmneaμnR2+mπL2tαα+0teaμnR2+mπL2tαsααsα1fmn(s)ds.(16) Denote by λmn=μnR2+mπL2, by substituting (Equation16) into (Equation10), we get (17) u(r,z,t)=m,n=1hmneaλmntαα+0teaλmntαsααsα1fmn(s)dsJ0μnrRsinmπLz.(17) Applying (Equation4) and (Equation17), we obtain (18) gmn=hmneaλmnTαα+0TeaλmnTαsααsα1fmn(s)ds,(18) where gmn=4LR2J12(μn)0R0LJ0μnrRsinmπLzg(r,z)rdrdz. Using (Equation18), (Equation17) becomes (19) u(r,z,t)=m,n=1eaλmnTαtααgmntTeaλmntαsααsα1fmn(s)dsJ0μnrRsinmπLz=m,n=1eaλmnTαtααgmntTeaλmnsαTααsα1fmn(s)dsJ0μnrRsinmπLz.(19) If we denote ωn(r)=2RJ1(μn)J0(μnrR), φm(z)=2Lsin(mπLz) and ψm,n(r,z)=ωn(r)φm(z), then it is easy to check that the eigenfunctions {ψm,n(r,z)}n,m1 form an orthonormal basis in Lr2(Ω). Using the eigenfunctions as the basises, we can expand (20) u(r,z,t)=m,n=1u(r,z,t),ψm,n(r,z)rψm,n(r,z).(20) Let gδ be the measured data satisfying (21) gδgδ.(21) Since t<T, from (Equation19) we know that, when λmn become larger, eaλmnTαtαα increases very quickly. Therefore, the term eaλmnTαtαα is the cause of instability and the problem (Equation1)–(Equation4) is ill-posed and a regularization is necessary. In the next Section, we shall construct the regularized solution and establish the approximation for the problem.

Remark 2.1

When α=1, (Equation17) is the solution of the classical first-order time-derivative initial value problem of partial differential equation with inhomogeneous term. When α0, eaλmnTαtαα(Tt)aλmn, the ill-posedness becomes weak. This is a very interesting phenomenon for inverse problems involved fractional derivative.

3. Well-posedness of the regularized problem

In this section, we will apply a modified quasi-boundary value method to regularize (Equation1)–(Equation4). We will consider problem (Equation1)–(Equation4) with adjusted information so that the adjusted problem can be well-posed and approximate to the original problem. Starting from the ideas mentioned in the paper of [Citation34], we consider the following approximate problem (22) αtαw(r,z,t)=a2wr2+1rwr+2wz2+fν(r,z,t),(r,z,t)Ω×(0,T),w(0,z,t)=w(R,z,t)=w(r,0,t)=w(r,L,t)=0,(r,z,t)Ω×[0,T],w(r,z,T)=gν(r,z),(r,z)Ω,(22) where (23) fν(r,z,t)=m,n=1fmn(t)1+νeabλmnTααJ0μnrRsinmπLz,(23) (24) gν(r,z)=m,n=1gmn1+νeabλmnTααJ0μnrRsinmπLz.(24) In formulas (Equation22)–(Equation24), fmn(t), gmn are defined by (Equation14) and (Equation15), ν is a regularization parameter depending on δ. The real number b1 is a constant.

From (Equation17), we note that the exact solution u is smooth if the exact data g is smooth also. However, real data from actual measurements is often discrete and non-smooth. We shall therefore always assume that fL((0,T);Lr2(Ω)) and gLr2(Ω) and the error of the data is given in Lr2(Ω) only. In the following theorem, we give the well-posedness of problem (Equation22)–(Equation24). But before we do that, let's give a useful lemma.

Lemma 3.1

For λmn,a,ν>0, we have eaλmnTαtαα1+νeabλmnTαανtαTαbTα.

Proof.

For 0cd, we have (25) eaλmnc1+νeaλmnd=eaλmnc(1+νeaλmnd)cd(1+νeaλmnd)1cdeaλmnc(1+νeaλmnd)cdeaλmnc(νeaλmnd)cd=νcd.(25) Since 0tT, b1, we have 0TαtααbTαα. If we let c=Tαtαα, d=bTαα in (3.4), then eaλmnTαtαα1+νeabλmnTαανtαTαbTα. This ends the proof.

Remark 3.1

Similar to (Equation25), we can also prove that (26) eaλmnc1+νeaλmndνcd.(26) In fact, for 0cd, we still have eaλmnc1+νeaλmnd=eaλmnc(1+νeaλmnd)cd(1+νeaλmnd)1cdeaλmnc(1+νeaλmnd)cdeaλmnc(νeaλmnd)cd=νcd.

Theorem 3.1

Let fL((0,T);Lr2(Ω)) and gLr2(Ω). Then, (Equation22)–(Equation24) has uniquely a weak solution w(r,z,t)C([0,T];Lr2(Ω)) defined as follows: w(r,z,t)=m,n=1eaλmnTαtαα1+νeabλmnTααgmntTeaλmnsαTααsα1fmn(s)ds×J0μnrRsinmπLz. The solution depends continuously on gLr2(Ω) in C([0,T];Lr2(Ω)).

Proof.

Denote by w(r,z,0)=ϕ(r,z). Compare (Equation23) and (Equation11), similar to getting (Equation17), we obtain (27) w(r,z,t)=m,n=1ϕmneaλmntαα+0teaλmntαsααsα1fmn(s)1+νeabλmnTααds×J0μnrRsinmπLz.(27) From (Equation24) and (Equation27), we have (28) gmn1+νeabλmnTαα=ϕmneaλmnTαα+0TeaλmnTαsααsα1fmn(s)1+νeabλmnTααds.(28) Applying (Equation27) and (Equation28), we obtain (29) w(r,z,t)=m,n=1eaλmnTαtαα1+νeabλmnTααgmntTeaλmnsαTααsα1fmn(s)ds×J0μnrRsinmπLz.(29) Hence, (Equation29) is the solution of the regularized problem (Equation22)–(Equation24).

Now we show that w(r,z,t)C([0,T];Lr2(Ω)).

For t[0,T], applying the inequality (xy)22x2+2y2, x,yR, a direct calculation gives w(,,t)2=m,n=1eaλmnTαtαα1+νeabλmnTααgmntTeaλmnsαTααsα1fmn(s)ds2ν2tαTαbTαm,n=12gmn2+m,n=12tTeaλmnsαTααsα1fmn(s)ds2ν2tαTαbTα2m,n=1gmn2+2m,n=1sup0sT|fmn(s)|2tTeaλmnsαTααsα1ds2ν2tαTαbTα2m,n=1gmn2+2m,n=1sup0sT|fmn(s)|21eaλmnTαtααaλmn2ν2tαTαbTα2m,n=1gmn2+2fL((0,T);Lr2(Ω))2m,n=11eaλmnTαtααaλmn22ν2tαTαbTαgLr2(Ω)2+MfL((0,T);Lr2(Ω))2, where M=m,n=11eaλmnTαtααaλmn2m,n=11a2μnR2+mπL22<+. Since fL((0,T);Lr2(Ω)) and gLr2(Ω), so m,n=1eaλmnTαtαα1+νeabλmnTααgmntTeaλmnsαTααsα1fmn(s)dsJ0μnrRsinmπLz is convergent in Lr2(Ω) uniformly in t[0,T], we see that w(r,z,t)C([0,T];Lr2(Ω)).

Now, we prove the uniqueness of the solution. Let vν1(r,z,t) and vν2(r,z,t) be two solutions of (Equation22)–(Equation24). We denote v(r,z,t)=vν1(r,z,t)vν2(r,z,t). It is clear that v(r,z,T)=0. We expand v(r,z,t) as (30) v(r,z,t)=m,n=1vmn(t)J0μnrRsinmπLz(30) with the coefficient vmn(t)=4LR2J12(μn)0R0LJ0μnrRsinmπLzv(r,z,t)rdrdz. Problem (Equation22)–(Equation24) is linear and v(r,z,t) is the solution of the problem (Equation22)–(Equation24), thus we get (31) dαvmn(t)dtα+aλmnvmn(t)=fmnν(t),(31) where fmnν(t)=4LR2J12(μn)0R0LJ0μnrRsinmπLzfν(r,z,t)rdrdz. The condition v(r,z,T)=0 yields vmn(T)=0. Then, the well-posedness for the fractional differential equation (Equation31) with the boundary condition vmn(T)=0 yields vmn(t)=0 in t[0,T]. This infers that v(r,z,t)0. Then vν1(r,z,t)=vν2(r,z,t).

Next, we prove the stability of the solution.

Let vν1(r,z,t) and vν2(r,z,t) be two solutions of (Equation22)–(Equation24) corresponding to the final data gδ1(r,z) and gδ2(r,z). From (Equation27), we have (32) vν1(r,z,t)=m,n=1eaλmnTαtαα1+νeabλmnTααgmnδ1tTeaλmnsαTααsα1fmn(s)ds×J0μnrRsinmπLz,(32) (33) vν2(r,z,t)=m,n=1eaλmnTαtαα1+νeabλmnTααgmnδ2tTeaλmnsαTααsα1fmn(s)ds×J0μnrRsinmπLz,(33) where gmnδ1=4LR2J12(μn)0R0LJ0μnrRsinmπLzgδ1(r,z)rdrdz,gmnδ2=4LR2J12(μn)0R0LJ0μnrRsinmπLzgδ2(r,z)rdrdz. Hence (34) vν1(r,z,t)vν2(r,z,t)=m,n=1eaλmnTαtαα1+νeabλmnTααgmnδ1gmnδ2J0μnrRsinmπLz.(34) Using the eigenfunctions ψm,n(r,z) as a basis, formula (Equation34) can be rewritten as (35) vν1(r,z,t)vν2(r,z,t)=m,n=1eaλmnTαtαα1+νeabλmnTααgδ1gδ2,ψm,nrψm,n(r,z).(35) By Lemma 3.1 and (Equation35), we have (36) vν1(r,z,t)vν2(r,z,t)2=m,n=1eaλmnTαtαα1+νeabλmnTααgδ1gδ2,ψm,nr2ν2tαTαbTαm,n=1gδ1gδ2,ψm,nr2=ν2tαTαbTαgδ1gδ22.(36) This ends the proof.

4. Estimators and convergence results

Theorem 4.1

The real numbers b1,a>0 are constants. Assume that there exists a positive number E1 such that (37) m,n=1e2aλmntααu(r,z,t),ψm,nr2<E12,0tT.(37) Let gδLr2(Ω) be a measured data satisfying (Equation21). Let wδ(r,z,t) be the solution of problem (Equation22)–(Equation24) corresponding to the final data gδ. If the regularization parameter is chosen by ν=(δE1)b, then we have the following convergence estimate u(,,t)wδ(,,t)2E11tαTαδtαTα,for 0tT.

Proof.

Using the triangle inequality, we have (38) u(,,t)wδ(,,t)u(,,t)w(,,t)+w(,,t)wδ(,,t)=I1+I2.(38) We firstly give an estimate for the second term I2. A proof similar to (Equation36), we have I22=w(,,t)wδ(,,t)2ν2tαTαbTαggδ2ν2tαTαbTαδ2. Thus (39) I2νtαTαbTαδ.(39) Now we give the bound for the first term I1. From (Equation20) and (Equation29), we obtain u(r,z,t)w(r,z,t)=m,n=1νeabλmnTαα1+νeabλmnTααeaλmnTαtααgmntTeaλmnsαTααsα1fmn(s)ds×J0μnrRsinmπLz=m,n=1νeabλmnTαα1+νeabλmnTααeaλmntααeaλmntααu(r,z,t),ψm,nrψm,n(r,z)=m,n=1eaλmntαα1+ν1eabλmnTααeaλmntααu(r,z,t),ψm,nrψm,n(r,z). So using (Equation26), we get I12=u(r,z,t)w(r,z,t)2=m,n=1eaλmntαα1+ν1eabλmnTαα2e2aλmntααu(r,z,t),ψm,nr2ν2tαbTαE12. Thus (40) I1νtαbTαE1.(40) From (Equation38), (Equation39) and (Equation40), we have (41) u(,,t)wδ(,,t)νtαbTαE1+νtαTαbTαδ.(41) Choose the regularization parameter ν by νtαbTαE1=νtαTαbTαδ. Thus we get (42) ν=δE1b.(42) Then, we have a convergence estimate u(,,t)wδ(,,t)2E11tαTαδtαTα. This ends the proof.

Theorem 4.2

The real numbers b1,a>0 are constants. Assume that there exist positive numbers p, E2 such that m,n=1e2apλmnu(r,z,t),ψm,nr2<E22. Let gδLr2(Ω) be a measured data satisfying (Equation21). Let wδ(r,z,t) be the solution of problem (Equation22)–(Equation24) corresponding to the final data gδ. The regularization parameter is chose by ν=δbTαTα+αp, then one has u(,,t)wδ(,,t)E2δαpTα+αp+δtα+αpTα+αp,for 0tT.

Proof.

Using the triangle inequality, we have (43) u(,,t)wδ(,,t)u(,,t)w(,,t)+w(,,t)wδ(,,t)=I3+I4.(43) A proof similar to (Equation39), we have (44) I4νtαTαbTαδ.(44) Now we give the bound for the term I3. From (Equation20) and (Equation29), we obtain u(r,z,t)w(r,z,t)=m,n=1νeabλmnTαα1+νeabλmnTααeaλmnTαtααgmntTeaλmnsαTααsα1fmn(s)ds×J0μnrRsinmπLz=m,n=1νeabλmnTαα1+νeabλmnTααeapλmneapλmnu(r,z,t),ψm,nrψm,n(r,z)=m,n=1eapλmn1+ν1eabλmnTααeapλmnu(r,z,t),ψm,nrψm,n(r,z). So using (Equation26), we get I32=u(r,z,t)w(r,z,t)2=m,n=1eapλmn1+ν1eabλmnTαα2e2apλmnu(r,z,t),ψm,nr2ν2αpbTαE22. Thus (45) I3ναpbTαE2.(45) From (Equation43), (Equation44), (Equation45), we have (46) u(,,t)wδ(,,t)ναpbTαE2+νtαTαbTαδ.(46) Choose the regularization parameter ν by (47) ν=δbTαTα+αp.(47) Then, we have a convergence estimate u(,,t)wδ(,,t)E2δαpTα+αp+δtα+αpTα+αp. This ends the proof.

Remark 4.1

In (Equation37), if f = 0, (Equation37) becomes u(,,0)r2<E12, which is the usual source condition.

Remark 4.2

In Theorem 4.1, the error estimate is not good at t = 0 because the condition for the exact solution u is weak. In Theorem 4.2, we assume that the exact solution is smoother, in these cases, for t = 0, we get u(,,0)wδ(,,0)(E2+1)δαpTα+αp. At t = 0, the convergence rate is δαpTα+αp. If we take p=(b1)Tαα, the fastest convergence is δb1b. Therefore, for a large constant b, it can approach the convergence rate of δ. This is because a-prior condition of the exact solution is very strong, i.e. it requires that the exact solution is analytic.

Remark 4.3

When p=tαα, (Equation40) and (Equation45) are the same. At this point, Theorem 4.1 and Theorem 4.2 are identical.

5. Numerical experiments

In this section, we conduct some numerical experiments with an example because Theorem 4.1 and Theorem 4.2 are identical in some sense. For the sake of simplicity, we fix a = 1. We consider the problem (48) αtαu(r,z,t)=2ur2+1rur+2uz2+f(r,z,t),u(R,z,t)=u(0,z,t)=0,t>0, 0<zL,u(r,0,t)=u(r,L,t)=0,t>0, 0<rR,u(r,z,T)=g(r,z),(48) where (49) f(r,z,t)=1+μ1R2+πL2etααJ0μ1rRsinπLz,g(r,z)=eTααJ0μ1rRsinπLz,λ11=μ1R2+πL2.(49) Under the above assumptions, the exact solution of the problem (Equation48) is (50) u(r,z,t)=eλ11TαtααetααJ0μ1rRsinπLz.(50) Now, due to errors in the measurement process, the measured data is perturbed by a ‘noise’ with level δ i.e (51) gδ(r,z)=g(r,z)+δJ0μ1rRsinπLz.(51) In our numerical experiments, we always fix T = 1, R = 1, L=π. So at the final time, the data error is (52) g(,)gδ(,)=δ.(52) The solution of (Equation48) for the final value gδ is given by (53) uδ(r,z,t)=etαα+δeλ11TαtααJ0μ1rsinz.(53) The regularized solution is (54) wδ(r,z,t)=eλ11Tαtαα1+νebλ11Tααetαα+δJ0μ1rsinz.(54) From (Equation52) and (Equation42), the regularization parameter is ν=(δE1)b with E1=u(,,0)r.

Let (55) e(δ)=wδu(55) be the error between the regularized solution wδ and the exact solution u.

Relative error between the exact solution and the regularized solution which is defined by (56) er(δ)=wδuu.(56) Consider the following cases:

Case 1. In this case, we fix α=0.4, b = 3.1, t = 0.2. We take different values of δ. We have Figure  and Table . It can be seen from Figure and Table  that as the measurement error δ becomes smaller, the regularized solutions are getting closer to the exact solution.

Figure 1. The exact solution and the regularized solutions in Table . (a) α=0.4, t = 0.2, δ=0.5000. (b) α=0.4, t = 0.2, δ=0.3000. (c) α=0.4, t = 0.2, δ=0.1000. (d) α=0.4, t = 0.2, δ=0.0100.

Figure 1. The exact solution and the regularized solutions in Table 1. (a) α=0.4, t = 0.2, δ=0.5000. (b) α=0.4, t = 0.2, δ=0.3000. (c) α=0.4, t = 0.2, δ=0.1000. (d) α=0.4, t = 0.2, δ=0.0100.

Table 1. The relative error in Figure .

Case 2. Now, we fix α=0.6, b = 3.1, δ=0.1. We take different values of t. We have Figure  and Table . Comparing Figure with Figure , we find that when t becomes closer to zero, the rate at which the regularization converges to the exact solution slows down. This is consistent with our theoretical analysis.

Figure 2. The exact solution and the regularized solutions in Table . (a) α=0.6, δ=0.1000, t = 0.01. (b) α=0.6, δ=0.1000 , t = 0.05. (c) α=0.6, δ=0.1000, t = 0.5. (d) α=0.6, δ=0.1000, t = 0.8.

Figure 2. The exact solution and the regularized solutions in Table 2. (a) α=0.6, δ=0.1000, t = 0.01. (b) α=0.6, δ=0.1000 , t = 0.05. (c) α=0.6, δ=0.1000, t = 0.5. (d) α=0.6, δ=0.1000, t = 0.8.

Table 2. The relative error in Figure .

Case 3. Let b = 3.1, t = 0.6, δ=0.05. We take different values of α. We have Figure  and Table . Figure and Table  show that as the α is smaller, the error between the regularized solution and the exact solution decreases. Through numerical experiments, we find that the smaller α is, the better reconstruction result is. Finally, it should be noted that the value of b is determined after many numerical experiments. Although theoretically, when b is greater than or equal to 1, our method is convergent. But for the appropriate choice b, we will get faster convergence speed.

Figure 3. The exact solution and the regularized solutions in Table . (a) α=0.1, t = 0.6, δ=0.05. (b) α=0.3, t = 0.6, δ=0.05. (c) α=0.6, t = 0.6, δ=0.05. (d) α=1, t = 0.6, δ=0.05.

Figure 3. The exact solution and the regularized solutions in Table 3. (a) α=0.1, t = 0.6, δ=0.05. (b) α=0.3, t = 0.6, δ=0.05. (c) α=0.6, t = 0.6, δ=0.05. (d) α=1, t = 0.6, δ=0.05.

Table 3. The relative error in Figure .

6. Conclusion

In this paper, we study a backward problem for the inhomogeneous conformable fractional heat equation in a cylinder. We solve it by a modified quasi-boundary value method. we have established an error estimate between exact and regularized solutions. Corresponding to different levels of the smoothness of the exact solution, the convergence rates are improved gradually. Numerical examples show that our proposed regularization method is effective and stable.

Acknowledgements

We would like to thank the anonymous referees and the editor for valuable comments and helpful suggestions, which substantially improved the earlier version of the paper. This work is partially supported by the Natural Science Foundation of China (No 11661072), the Natural Science Foundation of Northwest Normal University, China (No NWNU-LKQN-17-5).

Disclosure statement

No potential conflict of interest was reported by the author(s).

Additional information

Funding

This work is partially supported by the the Natural Science Foundation of China [grant number No 11661072], the Natural Science Foundation of Northwest Normal University (NWNU), China [grant number NWNULKQN- 17-5].

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