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Articles

Landweber iteration regularization method for identifying unknown source on a columnar symmetric domain

, &
Pages 1109-1129 | Received 13 Oct 2016, Accepted 18 Sep 2017, Published online: 08 Oct 2017

Abstract

In this paper, an inverse source problem for the Helium Production–Diffusion Equation on a columnar symmetric domain is investigated. Based on an a priori assumption, the optimal error bound analysis and a conditional stability result are given. This problem is ill-posed and Landweber iteration regularization method is used to deal with this problem. Convergence estimates are presented under the priori and the posteriori regularization choice rules. For the a priori and the a posteriori regularization parameters choice rules, the convergence error estimates are all order optimal. Numerical examples are given to show that the regularization method is effective and stable for dealing with this ill-posed problem.

AMS Subject Classifications:

1. Introduction

Source identification problem is the most commonly encountered inverse problems in heat conduction. These problems have been studied over several decades due to their significance in a variety of scientific and engineering applications such as in groundwater migration, pollution source identification and control, environmental protection [Citation1].

In this paper, we study the following source identification problem for the Helium production–diffusion equation [Citation2] which considers the local helium concentration gradients resulting from ejection of high energy alpha particles from grain surfaces. It is assumed that the grain is of a columnar diffusion geometry as illustrated in Figures and , which is actually consistent with laboratory measurements of helium diffusion

Figure 1. The 3-D model for the columnar symmetric domain.

Figure 1. The 3-D model for the columnar symmetric domain.

Figure 2. The 2-D model for the columnar symmetric domain.

Figure 2. The 2-D model for the columnar symmetric domain.

from apatite. As a consequence of radiogenic production and diffusive loss u(rt) which only depends on the columnar symmetric domain radius r denotes the concentration of helium. We consider the following problem:(1.1) ut-1rur-urr=f(r),0<t<T,0<r<r0,u(r,0)=0,0rr0,u(r0,t)=0,0tT,limr0u(r,t)is bounded0<t<T,0<r<r0.(1.1)

The data are given as the final observation of the helium concentration:(1.2) u(r,T)=g(r),0rr0.(1.2)

Given the data function g(r), the inverse radiogenic source problem is to reconstruct the source term f(r), which accounts for the ejection of high energy alpha particles. This problem is closely connected to the (U-Th)/He isotopes dating, one method of low temperature thermochronometry. Since the (U-Th)/He isotopes dating achieves a relative low temperature condition that cannot be reached by other isotopes systems, as well as the fact that high-precision, high-sensitivity Helium analysis are comparatively easy, it has been widely used in the study of mountain uplift and the geomorphic evolution, and the dating of terrestrial and extraterrestrial materials. For more physical context and applications, we refer to the papers [Citation2Citation4] and the references cited therein. Since the data g(r) are based on (physical) observation, there must be measurement error, and we assume the measured data function gδ(r) satisfies(1.3) gδ(·)-g(·)δ.(1.3)

Besides the motivation of the radiogenic source identification for the helium diffusion, heat source identification problem is an important branch in inverse problem research. About source identification problem, due to their significance in a variety of scientific and engineering application, it has been studied over several decades. Now about various types of heat sources in one dimensional, there are much research results, such as [Citation5Citation32]. Compared with one-dimensional diffusion equation, about the high-dimensional case, there is relative little research result. In [Citation33], the authors took the Landweber iteration as a numerical method to identify unknown source in columnar domain. In [Citation34], the authors also took the Landweber iteration as a numerical method to identify spatial source in a bound domain. But in [Citation33,Citation34], the authors cannot give the error estimate between the exact solution and the regularization solution. In [Citation35], the authors used the spectral method to identify the heat source in a spherically symmetric parabolic equation. In [Citation36], the authors used the spectral method to identify the heat source in columnar symmetric domain and proved the uniqueness of a solution. But in [Citation35,Citation36], the regularization parameters are selected by the a priori rule. There is a defect for any a priori method, i.e. the a priori choice of the regularization parameter depends seriously on the a priori bound E of the unknown solution. However, the a priori bound E cannot be known exactly in practice, and working with a wrong constant E may lead to the bad regularized solution. Moreover the error estimates in [Citation35,Citation36] are only logarithm type.

In this study, one of our purposes is that Landweber iteration as a regularization method is firstly used to deal with this problem. Secondly, we prove an optimal error bound of this problem is Hölder type under a special ‘source condition’. The third purpose is that we give the a priori and a posteriori choice of the regularization parameters for Landweber iteration regularization method. For a priori and a posteriori choices of the regularization parameter, we all obtain the Hölder type stability estimates which are all order optimal. Finally, we give some different examples to show the comparison of numerical effect between a priori and a posteriori regularization choice rules.

Throughout this paper, L2[0,r0;r] denotes the Hilbert space of Lebesgue measurable functions f with weight r on [0,r0]. (·,·) and · denote the inner and norm on L2[0,r0;r], respectively, with the norm(1.4) f(·)=0r0r|f(r)|2dr12.(1.4)

Using the method of separation of variable, we get the solution of problem (Equation1.1)(see [Citation36]):(1.5) u(r,t)=n=1f(·),Xn(·)kn(t)Xn(r),(1.5)

where(1.6) kn(t)=r0un21-e-unr02t,Xn(r)=2r0J1(un)J0unrr0,n=1,2,3,,(1.6)

and {Xn(r)} is an orthonormal basis of L2[0,r0;r], J0(.) and J1(.) is Zero-order Bessel function and First-order Bessel function, respectively. un is the infinite number real roots of the equation(1.7) J0(r)=0,(1.7)

and satisfies(1.8) 0<u1<u2<u3<···<un<···,limnun=.(1.8)

Denote(1.9) fn=(f(·),Xn(·))=0r0rf(r)Xn(r)dr,gn=(g(·),Xn(·))=0r0rg(r)Xn(r)dr.(1.9)

Throughout this paper, all scalar product is computed by (Equation1.9). Using u(r,T)=g(r), we obtain(1.10) g(r)=n=1fnknXn(r)(1.10)

and(1.11) f(r)=n=1gnknXn(r),(1.11)

where(1.12) kn=Te-unr02(T-tn).(1.12)

From Equation (Equation1.11), we can see that kn-1 as n. So the exact data function g(r) must satisfy the property that (g,Xn(·)) decays rapidly. But in applications, the input data g(r) can only be measured and never be exact. As for the measured data function gδ(r) only belongs to L2[0,r0;r], we cannot expect it has the same decay rate in L2[0,r0;r]. Thus the problem (Equation1.1) is ill-posed. So we must use regularization method to deal with problem (Equation1.1). Before this, we still give an a priori bound on the unknown heat source.

DenoteQp=ψL2[0,r0;r];n=1unr0p|(ψ(·),Xn(·))|2<,

where (·,·) is product of L2[0,r0;r], p>0 is a constant, then Qp is a Hilbert space which norm is denoted by(1.13) ψQp:=n=1unr0p|(ψ,Xn(·))|212.(1.13)

So we suppose(1.14) f(·)QpE,(1.14)

where E>0 is a constant.

This paper is organized as follows. Section 2 gives the optimal error bound for problem (Equation1.1). Section 3 gives the conditional stability estimate for problem (Equation1.1). Section 4 obtains the order-optimal error estimates under the a priori and the a posteriori parameter choice rules. Section 5 gives some numerical examples to show the effectiveness of this method. Section 6 puts an end to this paper with a brief conclusion.

2. Preliminary result and optimal error bound for problem (Equation1.1)

2.1. Preliminary result

To find f(r), we define a linear operator K:L2[0,r0;r]L2[0,r0;r], and only need to solve the following integral equation:(2.1) Kf(r)=0r0k(r,ξ)f(ξ)dξ=g(r),(2.1)

where(2.2) k(r,ξ)=n=1knXn(r)Xn(ξ).(2.2)

From (Equation2.2), we know k(r,ξ)=k(ξ,r), so K is a self-adjoint and compact operator. Now we give a important Lemma as follows:

Lemma 2.1:

[see in [Citation37,Citation38]] Let {kn}n=1 mention (Equation1.12). Let un be the infinite number real roots of the equation J0(r)=0, so there exist two positive constants C1 and C2 such that(2.3) C1unknC2un.(2.3)

Consider an arbitrary ill-posed operator equation [Citation40Citation44]:(2.4) Ax=y,(2.4)

where A:L2[0,r0;r]L2[0,r0;r] is a linear bounded between infinite dimensional Hilbert spaces X and Y with non-closed range R(A) of A. Assume that yδY are available noisy data with y-yδδ. Any operator R:YX can be considered as a special method for approximately solving (Equation2.4), and the approximate solution of (Equation2.4) is given by Ryδ.

Let MX be a bounded set. Let us introduce the worst case error (δ,R) for identifying x from yδ as [Citation39Citation43]:(2.5) (δ,R):=supRyδ-x|xM,yδY,Ax-yδδ.(2.5)

The best possible error bound (or optimal error bound) is defined as the infimum over all mappings R:YX:(2.6) ω(δ):=infR(δ,R).(2.6)

Now let us review some optimality results if the set M=Mφ,E is given by(2.7) Mφ,E=xX|x=[φ(AA)]-12v,vE,(2.7)

where the operator function φ(AA) is well defined via spectral representation [Citation30,Citation42,Citation45](2.8) φ(AA)=0aφ(λ)dEλ,(2.8)

where AA=0aλdEλ is the spectral decomposition of AA, Eλ denotes the spectral family of the operator AA. a is a constant which satisfies AAa. In the case when A is a multiplication operator, Ax(s)=γ(s)x(s), the operator function φ(AA) has the form(2.9) φAA)x(s)=φ(|γ(s)|2x(s).(2.9)

Then a method R0 is called [Citation43]

(i)

optimal on the set Mφ,E if (δ,R0)=ω(δ,E) holds;

(ii)

order optimal on the set Mφ,E if (δ,R0)Cω(δ,E) with C1 holds.

In order to derive an explicit (best possible) optimal error bound for the worst case error (δ,R) defined in (Equation2.5), we assume that the function φ in (Equation2.8Equation2.9) satisfies the following assumption:

Assumption 2.1.1:

[Citation42,Citation43,Citation45]] The function φ(λ):(0,a](0,) in (Equation2.8), where a is a constant such that AAa, is continuous and has the following properties:

(i)

limλ0φ(λ)=0;

(ii)

φ is strictly monotonically increasing on (0, a];

(iii)

ρ(λ)=λφ-1(λ):(0,φ(a)](0,aφ(a)] is convex.

Now we will formulate our main result of this section concerning the best possible worst case error ω(δ,E) defined in (Equation2.6) for identifying the solution f of problem (Equation1.1) from noisy data gδ under condition (Equation1.3) and fMφ,E, where the set Mφ,E is given by (Equation2.7). We introduce the optimal error bound by(2.10) ω(δ,E):=infRsup{Rgδ-f|fMφ,E,gδL2[0,r0;r],g-gδδ},(2.10)

where R is an arbitrary method for approximation solving problem (Equation1.1), sup{Rgδ-f} means the maximum error(the worst case error) between the Rgδ and f as fMφ,E,gδL2[0,r0;r],g-gδδ, infRsup{Rgδ-f} means the smallest case error between the Rgδ and f for all mapping R:YMφ,E, which is called the optimal error bound.

Under Assumption 2.1.1, the next theorem gives us a general formula for the optimal error bound.

Theorem 2.1:

[Citation42,Citation43,Citation45]] Let Mφ,E be given by (Equation2.7), let Assumption 2.1.1 be satisfied, and let δ2E2σ(AAφ(AA)), where σ(AA) denotes the spectrum of operator AA, then(2.11) ω(δ,E)=Eρ-1δ2E2.(2.11)

2.2. Optimal error bound for problem (Equation1.1)

In this section, we consider the best possible worst case error (Equation2.6) for identifying f(r) from noisy data gδ(r) provided (Equation1.3) and fMp,E hold, where Mp,E is given by(2.12) fMp,E=fL2[0,r0;r]|fQpE,p>0,(2.12)

where ·Qp denotes the norm in Sobolev space Qp with(2.13) f(·)Qp:=n=1unr0p|(f(·),Xn(·))|212.(2.13)

Let us formulate problem (Equation1.1) as an operator equation(2.14) Af=g(2.14)

with linear operator AL(L2[0,r0;r],L2[0,r0;r]). From (Equation1.10), we obtain(2.15) n=1r0un21-e-unr02T(f(·),Xn(·))Xn(r)=g(r).(2.15)

So the singular values of operator A are(2.16) σn=r0un21-e-unr02T.(2.16)

Proposition 2.2.1:

Consider the operator Equation (Equation2.14), the set Mp,E is given in (Equation2.12). So φ=φ(λ) is given (in parameter representation) by(2.17) λ(l)=1-e-l2Tl22,φ(l)=l-p,0l<.(2.17)

Proof Comparing (Equation2.13) with (Equation2.7), we obtain(2.18) φ(AA)=un2r02-p.(2.18)

Due to (Equation1.11), we obtain that φ is given (in parameter representation) by λ(un)=r021-e-unr02Tun22, φ(un)=un2r02-p. We substitute un2r02=l and obtain (Equation2.17)).

We will discuss properties of the function φ=φ(λ)(λ(0,)) which is given (in parameter representation) by (Equation2.17) in the following.

Proposition 2.2.2:

The function φ(λ) defined by (Equation2.17) is continuous and has the following properties:

(i)

limλ0φ(λ)=0.

(ii)

φ is strictly monotonically increasing.

(iii)

ρ(λ)=λφ-1(λ) is strictly monotonically increasing and possesses the following parameter representation: (2.19) λ(l)=l-p,ρ(l)=l-p1-e-l2Tl22,0l<.(2.19)

(iv)

ρ-1(λ) is strictly monotonically increasing and possesses the following parameter representation: (2.20) λ(l)=l-p1-e-l2Tl22,ρ-1(l)=l-p,0l<.(2.20)

(v)

For the inverse function ρ-1(λ), there holds (2.21) ρ-1(λ)=λpp+2(1+o(1)),forλ0.(2.21)

Proof The proof of (i)–(iv) are obvious. We only give the proof of (v). Let F(λ)=ρ-1(λ)λ-pp+2, we obtainlimλ0F(λ)=limll-plp2p+21l21-e-l2T-pp+2=limll0=1.

The proof of (Equation2.21) is completed.

Proposition 2.2.3:

The function ρ(λ) defined by (Equation2.18Equation2.19) is strictly convex.

Proof The proof is similar to [Citation42,Citation43,Citation45], and we omit it.

Now we will formulate our main result of this section concerning the best possible worst case error ω(δ,E) defined in (Equation2.6) for identifying the solution f(r) of problem (Equation1.1) from noisy data gδ(r).

Theorem 2.2:

Let conditions (Equation1.3) and (Equation2.12) hold. Then the optimal error bound for solving problem (Equation1.1) is(2.22) ω(δ,E)=δpp+2E2p+2(1+o(1)),forδ0.(2.22)

Proof Combining (Equation2.11) with (Equation2.21), we obtainω(δ,E)=Eρ-1δ2E2=Eδ2E2pp+2(1+o(1))=δpp+2E2p+2(1+o(1)),forδ0.

3. Some auxiliary results and a conditional stability result

In this section, we first give some important Lemmas, which are very useful for main conclusions of this paper.

Lemma 3.1:

As constants a>0,p>0,m>0,su1>0, and 0<aC12s2<1, we have(3.1) F(s)=1-aC12s2ms-p2C3(m+1)-p4,(3.1)

where C3:=paC12p4.

Proof It is easily known that F(s)>0 and lims0F(s)=0. Equation F(s)=0 exists unique solution s0, then(3.2) F(s)sups[u1,+)F(s)F(s0),(3.2)

where s0=aC12(4m+p)p12>0, thusF(s)1-p4m+pmaC12(4m+p)p-p4C3(m+1)-p4.

Lemma 3.2:

As constants a>0,p>0,m>0,su1>0, and 0<aC12s2<1, there has(3.3) G(s)=1-aC12s2m-1s-p2-1C4m-p+24,(3.3)

where C4:=p+22aC12p+24.

Proof The proof is similar to proof of Lemma 3.1, we omit it.

Theorem 3.1:

Let f(r) be the solution of problem (Equation1.1) with the exact data g(r). For f(·)QpE, we have(3.4) f(·)C5E2p+2g(·)pp+2,(3.4)

where C5:=r0C1pp+2.

Proof Due to (Equation2.3) and (Equation1.14), use Hölder inequality, we obtainf(·)2=n=1kn-1(g(·),Xn(·))Xn(·)2=n=1kn-2|gn|2=n=1kn-2|gn|4p+2|gn|2pp+2=n=1kn-(p+2)|gn|22p+2(|gn|2)pp+2n=1kn-(p+2)|gn|22p+2n=1|gn|2pp+2n=1C1-pr0punpr0pkn-2|gn|22p+2n=1|gn|2pp+2r0C12pp+2E4p+2g(·)2pp+2.

So(3.5) f(·)C5E2p+2g(·)pp+2,(3.5)

where C5:=r0C1pp+2. This completes the proof of Theorem 3.1.

4. Regularization method and convergence estimate

In this section, we apply the Landweber iterative method to obtain the regularization solution for problem (Equation1.1). Let fm,δ(r) satisfy:f0(r):=0,fm,δ(r)=(I-aKK)fm-1,δ(r)+aKgδ(r),m=1,2,3,,

where m is not only iterative step number, but also is regularization parameter. a is the relaxation factor which satisfies 0<a<1K2. Due to K is self adjoint operator, we use singular value σn of compact operator K to obtain the expression of regularization solution of problem (Equation1.1) as follows:(4.1) fm,δ(r)=Rmgδ(r)=n=11-(1-akn2)mkngnδXn(r),(4.1)

where the operator Rm:=L2[0,r0;r]L2[0,r0;r] is defined by(4.2) Rm:=ak=0m-1(I-aK2)kK.(4.2)

4.1. A priori parameter choice rules

In this subsection, we will give an error estimate for under the a priori choice rule.

Theorem 4.1:

Let f(r) given by (Equation1.11) be the exact solution of problem (Equation1.1). Let fm,δ(r) given by (Equation4.1) be the regularization solution. The conditions (Equation1.3) and (Equation1.14) hold. If we choose regularization parameter m=[b], where(4.3) b=Eδ4p+2,(4.3)

then we have the following error estimate:(4.4) fm,δ(·)-f(·)C6E2p+2δpp+2,(4.4)

where [b] denotes the largest integer less than or equal to b, and C6(a,p):=a+r0p2paC12p4.

Proof Using triangle inequality, we get(4.5) fm,δ(·)-f(·)fm,δ(·)-fm(·)+fm(·)-f(·).(4.5)

Using (Equation1.3) and (Equation4.1), we get(4.6) fm,δ(·)-fm(·)2=n=11-1-akn2mkngnδ-gnXn(·)2(4.6) (4.7) supn1(An2)n=1gnδ-gnXn(·)2supn1(An2)δ2,(4.7)

where An:=1-(1-akn2)mkn.

Due to 0<akn2<1, use Bernoulli’s inequality, we obtain(4.8) 1-1-akn2mamkn2amkn.(4.8)

So(4.9) Anam.(4.9)

Thus(4.10) fm,δ(·)-fm(·)amδ.(4.10)

In addition, using (Equation1.14), we getfm(·)-f(·)2=n=11-(1-akn2)mkngnXn(·)-n=11kngnXn(·)2=n=1(1-akn2)mkngnXn(·)2=n=1r0p21-akn2mun-p2unr0p2fnXn(·)2r0psupn11-akn22mun-pn=1unr0p2fnXn(·)2r0psupn1Bn2E2, where Bn:=1-akn2mun-p2. Using Lemmas 2.1 and 3.1, we have(4.11) Bn1-aC12un2mun-p2C3(m+1)-p4.(4.11)

Thus(4.12) fm(·)-f(·)r0p2C3(m+1)-p4E.(4.12)

For iterative step m is a integer, if we choose m=[b]<m+1, we obtainfm,δ(·)-f(·)fm,δ(·)-fm(·)+fm(·)-f(·)amδ+r0p2C3(m+1)-p4E<amδ+r0p2C3(m)-p4EaE2p+2δpp+2+r0p2C3E2p+2δpp+2=a+r0p2paC12p4E2p+2δpp+2=C6E2p+2δpp+2,

where C6=a+r0p2paC12ep4. The proof of theorem is completed.

4.2. An a-posteriori selection rule

In this subsection, we give the a posteriori regularization choice rule. Assume τ>1, and which is a fixed constant. Stop the algorithm at the first occurrence of m=m(δ)N0 with(4.13) Kfm,δ(·)-gδ(·)τδKfm-1,δ(·)-gδ(·),(4.13)

where gδτδ.

Lemma 4.1:

Let ϱ(m)=Kfm,δ(·)-gδ(·), then we have the following conclusions:

(a)

ϱ(m) is a continuous function;

(b)

limm0ϱ(m)=gδ;

(c)

limm+ϱ(m)=0;

(d)

ϱ(m) is a strictly decreasing function for any m(0,+).

The proof of Lemma 4.1 is omitted.

Remark 4.1:

Lemma 4.1 shows that there exists an unique solution to inequality (Equation4.13).

Lemma 4.2:

Suppose τ>1, let m=m(δ,gδ)N0 choose from (Equation4.13), then we obtain the regularization parameter m satisfies:(4.14) mr02pp+2p+22aC12C2τ-14p+2Eδ4p+2.(4.14)

Proof From operator expression (Equation4.2) and (Equation1.10), we obtain(4.15) Rmg=n=11-1-akn2mkngnXn(r)(4.15)

and thus(4.16) KRmg-g2=n=11-akn22m|(g(·),Xn(·))|2.(4.16)

So KRm-1-I1. From (Equation4.13), we knowKRm-1g-gKRm-1gδ-gδ-(KRm-1-I)g-gδτδ-KRm-1-Iδ(τ-1)δ.

On the other hand, using (Equation1.14) and Lemma 2.1, we haveKfm-1(·)-g(·)=n=11-1-akn2m-1gnXn(·)-n=1gnXn(·)=n=1(1-akn2)m-1(g,Xn)Xn(·)n=1r0p2C21-akn2m-1fnunr0p2un-1-p2Xn(·)r0p2C2supn11-akn2m-1un-1-p2n=1fnunr0p2Xn(·)r0p2C2supn1C(n)E,

where C(n):=(1-akn2)m-1un-1-p2.

Using Lemmas 2.1 and 3.2, we obtain(4.17) C(n)C4m-p+24.(4.17)

So(4.18) (τ-1)δr0p2C2C4m-p+24E.(4.18)

Thusmr02pp+2C2C4τ-14p+2Eδ4p+2=r02pp+2p+22aC12C2τ-14p+2Eδ4p+2.

Now we give the important result of this section.

Theorem 4.2:

Let f(r) given by (Equation1.11) be the exact solution of problem (Equation1.1). Let fm,δ(r) be the regularization solution. The conditions (Equation1.3) and (Equation1.14) hold, and the regularization parameter is given by (Equation4.13), then we have the following error estimate:(4.19) fm,δ(·)-f(·)(C5(τ+1)pp+2+C7)E2p+2δpp+2,(4.19)

where C7:=r0pp+2p+22C1212C2r-12p+2 is a constant.

Proof Using triangle inequality, we obtain(4.20) fm,δ(·)-f(·)fm,δ(·)-fm(·)+fm(·)-f(·).(4.20)

Combining Lemma 4.2 and (Equation4.10), we get(4.21) fm,δ(·)-fm(·)amδr0pp+2p+22C1212C2τ-12p+2E2p+2δpp+2=:C7E2p+2δpp+2.(4.21)

For the second part of the right side of (Equation4.20), using (Equation1.3) and (Equation4.13), we haveK(fm(·)-f(·))=n=11-akn2mgnXn(·)=n=11-akn2mgn-gnδXn(·)+n=11-akn2mgnδXn(·)(τ+1)δ.

Due tofm(·)-f(·)Qp=n=1unr0p1-akn22mkn2gn212=n=11-akn22mfn2unr0p12E.

Using Theorem 3.1, we have(4.22) fm(·)-f(·)C5(τ+1)pp+2E2p+2δpp+2.(4.22)

Therefore(4.23) fm,δ(·)-f(·)C5(τ+1)pp+2+C7E2p+2δpp+2.(4.23)

5. Numerical implementation and numerical examples

In this section, we use three examples to illustrate the effectiveness of Landweber iteration method under two regularization parameter choice rules. Moreover, the comparisons of numerical effectiveness between the a posteriori parameter choice and the a priori parameter choice rule are shown. For noisy data gδ(r), we give as follows:(5.1) gδ(r)=g+ε·randn(size(g)),(5.1)

where(5.2) g=(g(r1),,g(rn))T,ri=(i-1)Δr,Δr=r0n-1,i=1,2,,n.(5.2)

The total noise level δ can be measured in the sense of Root-Mean-Square Error(RMSE) according to(5.3) δ=gδ-gl2=1ni=1ngi-giδ212.(5.3)

The relative error between exact solution and regularization solution is computed by(5.4) er=1ni=1nfi-fim,δ212.(5.4)

Choose τ=1.1, in order to obtain the posteriori regularization parameter, we use the bisection method to solve the Equation (Equation4.13).

First we give that (u(rt), f(r)) is the analytical solution of problem (Equation1.1).

Figure 3. Example 1. p=1,E=1.1 (a) ε=0.05; (b) ε=0.01; (c) ε=0.001.

Figure 3. Example 1. p=1,E=1.1 (a) ε=0.05; (b) ε=0.01; (c) ε=0.001.

Figure 4. Example 2. p=1,E=1.1 (a) ε=0.05; (b) ε=0.01; (c) ε=0.001.

Figure 4. Example 2. p=1,E=1.1 (a) ε=0.05; (b) ε=0.01; (c) ε=0.001.

Figure 5. Example 3. p=1,E=1.1 (a) ε=0.05; (b) ε=0.01; (c) ε=0.001.

Figure 5. Example 3. p=1,E=1.1 (a) ε=0.05; (b) ε=0.01; (c) ε=0.001.

Example 1:

It is easy to verify that the function u(r,t)=J0(r)(1-e-t),(r,t)[0,2.4]×[0,1] is the exact solution of problem (Equation1.1) with source f(r)=-J0(r)r-J(r). The exact data function g(r)=J0(r)(1-e-1).

Now we use Example 1 to compute the relative errors for different priori bound E with p=2, and different p with priori bound E=1.1, respectively. We also use Example 1 to compare with the numerical results between the Tikhonov regularization and the landweber iteration method under two different regularization parameter choice rules. The Tikhonov regularization solution is given as follows [Citation46]:(5.5) fαδ(r)=n=1kn-11+α2kn-2gnXn(r).(5.5)

About more details about the Tikhonov regularization solution, one can see the Lemma 3.1 of reference [Citation46]. In our numerical experiments, we use finite term to compute (Equation4.1) and (Equation5.3Equation5.5), i.e. fm,δ(r)=Rmgδ(r)=n=11001-(1-akn2)mkngnδXn(r),fαδ(r)=n=1100kn-11+α2kn-2gnXn(r).

Table gives the relative error of Example 1 for different priori bound E with p=2. From Table we can see that different priori bound E leads to different numerical results. Table shows the relative errors of Example 1 for different p with E=1.1. From Table  we find as p increases, the relative error decreases. But as p increases some value, the relative error also increases. This means we cannot reduce the relative error through improving the smoothness of the solution.

Tables and show the relative errors for different ε under two choice rule for two regularization methods about Example 1 with p=2. We can see that effectiveness of Landweber iterative method is better than Tikhonov method.

Table 1. Relative errors of Example 1 for different priori bound E with p=2.

Table 2. Relative errors of Example 1 for different p with priori bound E=1.1.

Table 3. Relative errors for different ε under the a priori choice rule for two regularization methods about Example 1 (p=2).

Table 4. Relative errors for different ε under the a posteriori choice rule for two regularization methods about Example 1 (p=2).

Example 2:

Consider a piecewise smooth source:(5.6) f(r)=0,0rπ4,4π(r-π4),π4<rπ2,-4π(r-3π4),π2<r3π4,0,3π4<rπ.(5.6)

Example 3:

Consider the following discontinuous function:(5.7) f(r)=0,0rπ3,1,π3<r2π3,0,2π3<rπ.(5.7)

From Figures , we can see that the smaller ε, the better the computed approximation is. Moreover, we can see that the a posteriori parameter choice also works well. In Examples 2–3, since the direct problem with the source f(r) does not have an explicit solution, the data g(r) are obtained by solving the direct problem. Figure shows the comparisons between the exact solution and its computed approximation with different noise levels for Example 2. Figure indicates the comparisons between the exact solution and its computed approximation with different noise levels for Example 3. From Figures , it can be seen that the numerical solution is less ideal than that of Example 1. Because in examples 2, 3, the exact solutions are non-smooth and discontinuities functions, the recover data near the non-smooth and discontinuities points are not accurate. This is the well-known Gibbs phenomenon. But considered the ill-posed problem, the results presented in Figures and are reasonable.

6. Conclusion

In this paper, we propose an efficient regularization method for identifying a space-dependent source. Under the a priori condition, we give the optimal error bound for this problem. Moreover, we obtain the stability estimate using the conditional stability. Thirdly, under a priori and a posteriori parameter choice rules, we all obtain the order-optimal error estimates. Finally, the numerical experiments show this proposed method works effectively.

Additional information

Funding

The project is supported by the National Natural Science Foundation of China [grant number 11561045], [grant number 11501272]; the Doctor Fund of Lan Zhou University of Technology.

Notes

No potential conflict of interest was reported by the authors.

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