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R E S E A R C H

Open Access

Landweber iterative method for

identifying a space-dependent source for the

time-fractional diffusion equation

Fan Yang

*

, Yu-Peng Ren, Xiao-Xiao Li and Dun-Gang Li

*Correspondence: [email protected] School of Science, Lanzhou University of Technology, Lanzhou, Gansu 730050, P.R. China

Abstract

This paper is devoted to identifying an unknown source for a time-fractional diffusion equation with variable coefficients in a general bounded domain. This is an ill-posed problem. Firstly, we obtain a regularization solution by the Landweber iterative regularization method. The convergence estimates between regularization solution and exact solution are given undera priorianda posterioriregularization parameter choice rules, respectively. The convergence estimates we obtain are optimal order for anypin two parameter choice rules,i.e., it does not appear to be a saturating phenomenon. Finally, the numerical examples in the one-dimensional and two-dimensional cases show our method is feasible and effective.

MSC: 35R25; 47A52; 35R30

Keywords: time-fractional diffusion equation; ill-posed problem; unknown source; Landweber iterative method

1 Introduction

Nowadays, the study of time-fractional diffusion equations has drawn attention from var-ious disciplines of science and engineering, such as mechanical engineering [, ], vis-coelasticity [], Lévy motion [], electron transport [], dissipation [], heat conduction [–] and high-frequency financial data []. A number of experiments have shown that, in the process of modeling real physical phenomena such as Brownian motion [], frac-tional calculus and derivatives provide more accurate simulations than tradifrac-tional calculus with integer order derivatives. Fractional derivatives have also proved to be more flexible in describing viscoelastic behavior. In particular, fractional models are believed to be more realistic in describing anomalous diffusion in heterogeneous porous media.

In recent years, people gradually find that the fractional derivative in describing the memory and genetic of material has a natural advantage. The slow diffusion can be char-acterized by the long-tailed profile in the spatial distribution of densities as time passes and continuous-time random walk has been applied to the underground environmental problem. Thus fractional derivatives are applied to many science fields, especially in the analytical [–] and numerical [–]. However, in practical problems, we need to re-trieve the part boundary data or source term of the equation by measuring the data. This leads to the inverse problem of the fractional diffusion equation. In this respect, some work

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has been published. In [], the authors studied the inverse problem for restoration of the initial data of a solution, classical in time and with values in a space of periodic spatial dis-tributions for a time-fractional diffusion equation and diffusion-wave equation. In [], the authors considered the problem of identifying an unknown coefficient in a nonlin-ear diffusion equation. In [], the authors considered the backward inverse problem for a time-fractional diffusion equation. In [], Liu and Yamamoto used the quasi-reversibility method to solve a backward problem for a time-fractional diffusion equation in the one-dimensional case. In [], Murio used the mollification technique to solve source terms identification for a time-fractional diffusion equation. In [], Wang solved a backward problem for a time-fractional diffusion equation with variable coefficients in a general bounded domain by the Tikhonov regularization method. In [], Zhang considered an inverse source problem for a fractional diffusion equation.

In this paper, we consider the following problem:

⎧ ⎪ ⎪ ⎪ ⎪ ⎪ ⎨ ⎪ ⎪ ⎪ ⎪ ⎪ ⎩

tu(x,t) – (Lu)(x,t) =f(x), x,t∈(,T),  <α< , u(x,t) = , x,t∈(,T), u(x, ) = , x,

u(x,T) =g(x), x,

(.)

whereis a bounded domain inRdwith sufficient smooth boundaryand t is the Caputo fractional derivative of orderαdefined by

tu(x,t) = ⎧ ⎨ ⎩

(–α)

t

(x,τ)

(tτ)α ,  <α< ,

ut(x,t), α= . (.)

–Lis a symmetric uniformly elliptic operator and its expression is

Lu(x) = d

i=

∂xi

d

j=

aij(x)

∂xju(x) +c(x)u(x), x, (.) where the coefficient

aij=ajiC() (≤i,jd) and, for any given constantc> , we have

c d

i=

ξi≤

d

i,j=

aij(x)ξiξj, x,ξ∈Rd,

c(x)≤, c(x)c().

Denote the eigenvalues of –Lbyλn. We supposeλn(see []) satisfy

 <λ≤λ≤ · · · ≤λn≤ · · ·, lim

n→+∞λn= +∞ (.) and the corresponding eigenfunctionϕn(x)H()H

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The source functionf(x) is unknown in problem (.). We use the additional condition u(x,T) =g(x) to identify the unknown sourcef(x). In practice, measurable datag(x) are never known exactly. We assume that the exact data g(x) and the measured datagδ(x) satisfy

gδ, (.)

where · is theL() norm andδ>  is a noise level.

Ifα= , the equation of problem (.) is a standard heat conduction equation. There have been published a lot of research results (see [–], etc.). In this paper, we only consider  <α<  for identifying the unknown source of the time-fractional diffusion equation. In [], Zhang used a truncation method to identify the unknown source for the time-fractional diffusion equation, and in [], Wang simplified the Tikhonov regularization method to solve it, but they consider an inverse source problem for the time-fractional diffusion equation in a regular domain. In [], the author used the quasi-reversibility method to solved problem (.). However, the error estimates from [, ] are not optimal order, which will lead to a saturating phenomenon.

In this article, the Landweber iterative method is used to deal with the ill-posedness problem (.) in a general region and convergence estimates are all obtained undera priori anda posteriorichoice regularization parameter rules. Moreover, convergence estimates are all optimal order according to our method. The Landweber iteration method [], proposed by Landweber, Friedman and Bialy, is a kind of iterative algorithm for solving the operator equationKx=y.

The structure of this paper is as follows. In Section , some basic lemmas and results are given. In Section , the Landweber iterative regularization method and regularization so-lution are given. In Section , the convergence estimates under thea priorianda posteriori regularization parameter choice rules are given. In Section , numerical implementation and numerical examples are given. In Section , some conclusions as regards this paper are given.

2 Lemma and results

Definition .([]) The Mittag-Leffler function is defined by

,β(z) =

k= zk

(αk+β), z∈C, (.)

whereα>  andβ∈Rare arbitrary constants.

Lemma .([]) For the Mittag-Leffler function,we have

,β(z) =zEα,α+β(z) +

(β). (.)

Lemma .([]) Letλ> ,that is,

epttγk+β–E(k) γ,β

±atγdt= k!p γβ

(pγa)k+, Re(p) >|a| 

γ, (.)

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Lemma . implies that the Laplace transform oftγk+β–E(k)

γ,βatγ) is k!β (a)k+.

Lemma .([]) For <α< ,η> ,we have≤,(–η)≤and Eα,(–η)is a com-pletely monotonic function,i.e.,

(–)n d n

dηnEα,(–η)≥, η≥. (.) Lemma . Supposeλnare the eigenvalues of operator–L.Ifλn≥ · · ·λ≥,then there exists a positive constant Cwhich depends onα,T,λsuch that

C

λnTα,+α

λnTα≤ 

λnTα, (.)

where C(α,T,λ) =  –,(–λ).

Proof From Lemma . and Lemma ., we easily get

,+α

λnTα=,(–λnT α) – 

λnTα =

 –,(–λnTα)

λnTα

λnTα. (.)

From Lemma ., we know,(–λnTα)≤,(–λ) whenλnλ, so

,+α

λnTα= –,(–λnT α)

λnTα

 –,(–λ)

λnTα =

C

λnTα, (.)

whereC(α,T,λ) =  –,(–λ).

3 Regularization method As in [, ], define

D(–L)γ=

ψL() :

n=

λnγ(ψ,ϕn)<∞

, (.)

where (·,·) is the inner product inL() andD((–L)γ) is a Hilbert space with the norm

ψD((–L)γ)=

n=

λnγ(ψ,ϕn)  

. (.)

Now using separation of variables and Lemma ., we get the solution of problem (.) as follows:

u(x,t) =

n=

f(x),ϕn(x)

,+α

λntα

ϕn(x).

Denotefn= (f(x),ϕn(x)),gn= (g(x),ϕn(x)) and lett=T. Then

g(x) =u(x,T) =

n=

fnTαEα,+α

λnTα

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and

gn=fnTαEα,+α

λnTα. (.)

Hence we obtain

fn= gn

,+α(–λnTα)

(.)

and

f(x) =

n= fnϕn=

n=

,+α(–λnTα)

gnϕn(x). (.)

Using Lemma ., we have

TαEα,+α

λnTα=,(–λnT α) – 

λn ≤ 

λn

. (.)

Consequently,

Tα  ,+α(–λnTα)

λn. (.)

Small errors in the high-frequency components for (x) will be amplified by

E

α,+α(–λnTα), so problem (.) is ill-posed. We must use the regularization method to solve it. We first impose thea prioribound for the exact solutionf(x) as follows:

f(x) D((–L)

p

)≤E, p> , (.)

whereEis the positive constant.

A conditional stability estimate of the inverse source problem (.) is given below.

Theorem .([]) Iff(x) D((–L)

p

)≤E,then f(x)≤CE

p+g(x)

p

p+, (.)

where C:=Cp+p

is a constant.

To findf(x), we need to solve the following integral equation:

(Kf)(x) :=

k(x,ξ)f(ξ)=g(x). (.)

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Forϕn(x) being an orthonormal basis inL(),

σn=TαEα,+α

λnTα, n= , , . . . (.)

are singular values ofKandϕnis the corresponding eigenvector.

Now, we use the Landweber iterative method to obtain the regularization solution for (.). We rewrite the equationKf =gin the formf = (I–aKK)f +aKgfor somea>  and give the following iterative form:

f(x) := , fm(x) =IaKKfm–(x) +aKg(x), m= , , , . . . , (.)

wheremis the iterative step number, which is also the selected regularization parameter. ais called the relaxation factor and satisfies  <a<K. ForKis a self-adjoint operator, we obtain

fm,δ(x) =a m–

k=

IaKkKgδ(x). (.)

Using (.), we get

fm,δ(x) =Rmgδ(x) =

n=

 – ( –aTαE

α,+α(–λnTα))m

,+α(–λnTα)

gnδϕn(x), (.)

where

n= (gδ(x),ϕn(x)).

Becauseσn=TαEα,+α(–λnTα) are singular values ofKand  <a<K, we can easily see  <aTαE

α,+α(–λnTα) < .

4 Error estimate under two parameter choice rules

In this section, we will give error estimates under thea priorichoice rule and thea poste-riorichoice rule.

An a priori choice rule

Theorem . Let f(x),given by(.),be the exact solution of problem(.).Let fm,δ(x)be the regularization solution.Let conditions(.)and(.)hold.If we choose regularization parameter m= [b],where

b=

E

δ

p+

, (.)

then we have the following error estimate:

fm,δ(·) –f(·)CE

p+δ

p

p+, (.)

where[b]denotes the largest integer less than or equal to b and C=

a+( p aC)

p

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Proof Using the triangle inequality, we have

fm,δ(·) –f(·)=

n=

 – ( –aTαE

α,+α(–λnTα))m

,+α(–λnTα)

gnδϕn(x)

n=

,+α(–λnTα) gnϕn(x)

n=

 – ( –aTαE

α,+α(–λnTα))m

,+α(–λnTα)

gnδϕn(x)

n=

 – ( –aTαE

α,+α(–λnTα))m

,+α(–λnTα)

gnϕn(x)

+

n=

 – ( –aTαE

α,+α(–λnTα))m

,+α(–λnTα)

gnϕn(x)

n=

,+α(–λnTα) gnϕn(x)

=fm,δ(·) –fm(·)+fm(·) –f(·). Using conditions (.), we get

fm,δ(·) –fm(·)=

n=

( – ( –aTαE

α,+α(–λnTα))m) TαE

α,+α(–λnTα)

gnδgn

≤sup n≥

A(n)δ,

whereA(n) :=–(–aTαE

α,+α(–λnTα))m E

α,+α(–λnTα) . Because  <x< , we have

x≤√x (.)

and

( –x)h≥ –hx (h> ). (.)

Using (.) and (.), we obtain

 – –aTαEα,+α

λnTαm≤√amTαEα,+α

λnTα, (.)

i.e.,

A(n)≤√am, (.)

so

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On the other hand, using (.), we get

fm(·) –f(·)= ∞ n=

[ – ( –aTαE

α,+α(–λnTα))m] – 

,+α(–λnTα)

gnϕn(x)  = ∞ n=

( –aTαE

α,+α(–λnTα))m TαE

α,+α(–λnTα) gn

=

n=

 –aTαEα,+α

λnTαm(λn)pfn(λn)p

≤sup n≥

B(n)E,

whereB(n) := ( –aTαE

α,+α(–λnTα))m(λn)– p .

Using Lemma ., we have

B(n)

 –aC  

λn

m

(λn)p. (.)

Let

F(s) :=

 –aC   s

m

sp, s:=λn. (.)

LetssatisfyF(s) = . Then we easily get

s=

aC

(m+p) p

 

, (.)

so

F(s) =

 – p m+p

m aC

(m+p) p

p

p (m+ )aC

p  , (.) i.e., F(s)p aC  p

(m+ )–p. (.)

Thus we obtain

B(n)

p aC

p

(m+ )–p. (.)

Hence

fm(·) –f(·)≤ p aC  p

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Combining (.) and (.), we choosem= [b] and we get

fm,δ(·) –f(·)CE

p+δ

p

p+, (.)

whereC:=

a+ (aCp )

p

. The theorem is proved.

An a posteriori selection rule

We construct regularization solution sequences fm,δ(x) by the Landweber iterative method. Let r>  be a fixed constant. Stop the algorithm at the first occurrence of m=m(δ)∈Nwith

Kfm,δ(·) –gδ(·)rδ, (.)

whererδ.

Lemma . Letρ(m) =Kfm,δ(·) –gδ(·).Then we have the following conclusions: (a) ρ(m)is a continuous function;

(b) limm→ρ(m) =; (c) limm→+∞ρ(m) = ;

(d) ρ(m)is a strictly decreasing function,for anym∈(, +∞).

Lemma . shows that there exists a unique solution for inequality (.).

Lemma . Let(.)hold,so the regularization parameter m satisfies

m

p+  aC 

E (r– )δ

p+

. (.)

Proof From (.), we show the representation

Rmg=

n=

 – ( –aTαE

α,+α(–λnTα))m

,+α(–λnTα)

gnϕn(x) (.)

for everygH(), so

KRmgg=

n=

 –aTαEα,+α

λnTαm(g,ϕn). (.)

Because| –aTαE

α,+α(–λnTα)|< , we obtainKRm––I ≤. Using (.), we obtain

KRm–ggKRm––(KRm––I)

g

KRm––

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On the other hand, using (.), we obtain

KRm–gg= ∞ n=

 – –aTαEα,+α

λnTαm–gnϕn

n= gnϕn

= ∞ n=

 –aTαEα,+α

λnTα

m– (g,ϕn)

=

n=

 –aTαEα,+α

λnTαm–

·TαEα,+α

λnTα(f,ϕn)λ

p

p n ≤ ∞ n=

 –aTαEα,+α

λnTα

m–

,+α

λnTα λpn E. Let

C(n) := –aTαEα,+α

λnTα

m–

,+α

λnTα

(λn)– p

, (.)

so

(r– )δC(n)E. (.)

Using Lemma ., we have

C(n)

 –aC   λn m– λp –

n . (.)

Let

G(s) =

 –aC   s

m–

sp–, s:=λn. (.)

Supposes∗satisfiesG(s∗) = . Then we get

s∗=

aC

(m+p– ) p+ 

 

, (.)

so

G(s∗) =

 – p+  m+p– 

m–

aC(m+p– ) p+ 

p+

p+  maC

p+

. (.)

Using (.) and (.), we get

(r– )δ

p+  aC 

p+

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Thus

m

p+  aC 

E (r– )δ

p+

.

Theorem . Let f(x),given by(.),be the exact solution of problem(.).Let fm,δ(x) be the regularization solution.The conditions(.)and(.)hold and the regularization parameter is given by(.).Then we have the following error estimate:

fm,δ(·) –f(·)≤C(r+ ) p p++C

Ep+δ p

p+, (.)

where C= (pC+ )

 (

r–)  p+.

Proof Using the triangle inequality, we obtain

fm,δ(·) –f(·)fm,δ(·) –fm(·)+fm(·) –f(·). (.)

Using (.) and Lemma ., we get

fm,δ(·) –fm(·)≤√amδCEp+δ

p

p+, (.)

whereC:= (pC+ )

 (

r–)  p+.

For the second part of the right side of (.), we know

Kfm(·) –f(·)=

n=

– –aTαEα,+α

λnTα

m gnϕn(x)

=

n=

– –aTαEα,+α

λnTαmgnnϕn(x)

+

n=

– –aTαEα,+α

λnTαmgnδϕn(x).

Using (.) and (.), we have

K

fm(·) –f(·)≤(r+ )δ. (.) We also have

fm(·) –f(·) D((–L)

p ) =

n=

– –aTαEα,+α

λnTαm

·

gn

,+α(–λnTα) 

(λn)p  

n= (λn)p

gn

,+α(–λnTα)  

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Using Theorem ., we have fm(·) –f(·)≤C(r+ )

p p+Ep+δ

p

p+. (.)

Therefore

fm,δ(·) –f(·)C (r+ )

p p++C

Ep+δ p

p+. (.)

5 Numerical implementation and numerical examples

In this section, we will use several numerical examples to show effectiveness of the Landweber iterative method.

5.1 One-dimensional case

Since the exact solution of problem (.) is difficult to give, we get the data functiong(x) by solving the following direct problem:

⎧ ⎪ ⎪ ⎪ ⎪ ⎪ ⎨ ⎪ ⎪ ⎪ ⎪ ⎪ ⎩

tu(x,t) – (Lu)(x,t) =f(x),  <t<T,  <x< , u(x, ) = , ≤x≤,

u(,t) = , ≤tT, u(,t) = , ≤tT.

(.)

When the source functionf(x) is given, we use the finite difference method to obtain data functiong(x).

The time and space step size of the grid aret=TN andx=M, respectively.tn=nt, n= , , , . . . ,N, indicates grid points on time interval [,T] andxi=ix,i= , , , . . . ,M, is the grid point of space interval [, ]. The value of each grid point is denoted byun

i = u(xi,tn).

The following time-fractional differential is given in [, ]:

tu(xi,tn)≈ (t)α

( –α) n–

j=

bjunijunij–, (.)

wherei= , . . . ,M– ,n= , . . . ,Nandbj= (j+ )–αj–α.

The spatial derivative difference scheme is given as follows []:

Lu(xi,tn)≈  (x)

ai+

u n

i+– (ai++ai–)u n i +ai–u

n i–

+c(xi)uni, (.)

whereai+

 =a(xi+),xi+ = xi+xi+

 .

For the inverse problem, we need to obtain a matrixKsuch thatKf =uNi . In order to obtain it, we use the same method as in [], that is,

K=A,

Kn=Ah n–

j=

(bj+–bj)Knj+, n= , . . . ,N,

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whereh:=(t(–)–αα),

A(M+)×(M+)= ⎛ ⎜ ⎝ 

A–

(M–)×(M–) 

⎞ ⎟ ⎠

and

A(M–)×(M–)= ⎛ ⎜ ⎜ ⎜ ⎜ ⎜ ⎝

d –(x)a  –(x)a

d –  (x)a

 . .. . .. . ..

(x)aM– dM– ⎞ ⎟ ⎟ ⎟ ⎟ ⎟ ⎠ ,

wheredi=(x)(ai++ai) –c(xi) +h,i= , . . . ,M– . Then we obtain the regularization solution by

f =a m–

k=

IaKTKkKTgδ. (.)

Noise data are generated by adding random perturbation,i.e.,

=g+εrandsize(g).

The relative error level and absolute error level are computed by

er=

(f –,δ)

(f) and ea=

 (M+ )

f,δ. (.)

5.2 Two-dimensional case

Let= (,l)×(,l) be a rectangle domain. Consider the following time-fractional dif-fusion equation:

⎧ ⎪ ⎪ ⎨ ⎪ ⎪ ⎩

tαu=uxx+uyy+f(x,y), (x,y),t∈(,T),

u(x,y, ) = , (x,y),

u(,y,t) =u(l,y,t) =u(x, ,t) =u(x,l,t) = , t∈[,T].

(.)

Letxi=ix,i= , , . . . ,M;yj=jy,j= , , . . . ,M;tn=nt,n= , , . . . ,N, wherex= l

M,y= l

M andt= T

N are space and time steps, respectively. The approximate values of each grid pointuare denoted byuni,ju(xi,yj,tn). Thus, we use initial and boundary conditions of equation (.) to getui,j= ,un,j=uMn ,j= ,uni,=uni,M= .

Let the integer order derivative difference scheme be given as follows:

u(xi,yj,tn+)

∂x ≈

uni+,+j– uin,+j +uni–,+j (x) ,

u(xi,yj,tn+)

∂y ≈

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It is easy to obtain the numerical solution ofu(x,y,T) =g(x,y) by the scheme

h n–

k= bk

uin,jkuink–=px

uni+,j– uni,j+uni–,j+py

uni,j+– uni,j+uni,j–+fi,j, (.)

wherepx= 

(x),py=(y) andhandbkare defined in the one-dimensional case. DenoteUn= (un,, . . . ,uMn –,,un,, . . . ,unM–,, . . . ,un,M–, . . . ,uMn –,M–) andf = (f,, . . . , fM–,,f,, . . . ,fM–,, . . . ,f,M–, . . . ,fM–,M–). Then we obtain the following iterative scheme:

AU=f,

AUn=f +Un–+ωUn–+· · ·+ωn–U

(n= , , . . . ,N),

(.)

whereωi=bi––biand

A∗= ⎛ ⎜ ⎜ ⎜ ⎜ ⎝

A, –pyI –pyI A, –pyI

–pyI . .. –pyI –pyI AM–,M–

⎞ ⎟ ⎟ ⎟ ⎟ ⎠∈R

(M–)(M–)×(M–)(M–),

Ai,i= ⎛ ⎜ ⎜ ⎜ ⎜ ⎝

h+ px+ py –px

–px h+ px+ py –px

–px . .. –px –px h+ px+ py

⎞ ⎟ ⎟ ⎟ ⎟ ⎠∈R

(M–) ,

whereIis the unit matrix with order (M– )×(M– ).

For the inverse problem, we can obtain a matrixKsuch thatKf =uNi,jby

K=A∗–

,

Kn=K+hK

n–

i=

ωiKni, n= , . . . ,N,

K=KN.

We take as noise data by adding a random perturbation,i.e.,

(·,·) =g(·,·) +ε·randsize(g).

Then we obtain the regularization solution in the two-dimensional case by

f =a m–

k=

IaKTKkKTg(·,·)δ. (.)

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Figure 1 The comparison of numerical effects between the exact solution and its regularized solution for Example 1.

In the one-dimensional computational procedure, we chooseT= . Let= (, ),a(x) = x+  andc(x) = –(x+ ). We use the algorithm in [] to compute the Mittag-Leffler function. In discrete format, we compute the direct problem withM= ,N=  and we chooseM= ,N=  for solving the inverse problem.

Example  Take the smooth functionf(x) =( –x)αsin(πx).

Example  We take the piecewise smooth function

f(x) = ⎧ ⎪ ⎪ ⎪ ⎪ ⎪ ⎨ ⎪ ⎪ ⎪ ⎪ ⎪ ⎩

, ≤x, (x–), <x≤, –(x–), <x≤,

, 

<x≤.

(.)

Figure  shows the comparisons between the exact solution and its regularized so-lution for various noise levels ε= ., ., . in the case of α = ., ., .. The iterative step m = ,, ,, ,, for α = ., in the case of α = ., m= ,, ,, , andm= ,, ,, ,, forα= ..

Example  Consider the following discontinuous function:

f(x) = ⎧ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎨ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎩

, ≤x≤., , . <x≤., , . <x≤., –, . <x≤., , . <x≤.

(.)

Figure  shows the comparison between the exact solution and its regularized so-lution for various noise levels ε= ., ., . in the case of α = ., ., .. The iterative step m= ,, ,, , for α = ., in the case of α = ., m= ,, ,, ,, andm= ,, ,, ,, forα= ..

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it-Figure 2 The comparison of numerical effects between the exact solution and its regularized solution for Example 2.

Figure 3 The comparison of numerical effects between the exact solution and its regularized solution for Example 3.

erative step m= ,, ,,, ,, forα = ., in the case ofα= ., m= ,, ,,, ,, andm= ,, ,,, ,, forα= ..

In Figures -, we see that the smallerεandα, the better the regularized solution is. Moreover, we see that thea posterioriparameter choice also works well.

Example  Take source functionf(x,y) =xy.

In Example , we takeT = .,M=M= ,N=  andl=l= . Figure  shows the comparison between the exact solution and its regularized solution for various noise levelsε= ., . in the case ofα= .. The iterative stepm= , forε= ., m= ,, when the error levelε= ..

Example  Take source functionf(x,y) =sin(x)sin(y) +sin(x)sin(y).

In Example , we takeT= ,M=M= ,N=  andl=l=π. Figure  shows the comparison between the exact solution and its regularized solution for various noise levels

ε= ., . in the case ofα= .. The iterative stepm=  forε= .,m=  when

error levelε= ..

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Figure 4 The comparison of numerical effects between the exact solution and its regularized solution for Example 4.

Figure 5 The comparison of numerical effects between the exact solution and its regularized solution for Example 5.

6 Conclusion

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two regularization methods to identify the spatial variable source for the time-fraction diffusion equation. In [], the authors used quasi-reversibility regularization methods to identify the spatial variable source for the time-fraction diffusion equation. From [], under thea prioriregularization parameter choice rule, the authors found the orders of error estimate convergence areO(δ

p

p+) ( <p) andO(δ) (p> ) and under thea posterioriregularization parameter choice rule, the authors found the orders of error es-timate convergence areO(δ

p

p+) ( <p) andO(δ) (p> ). In [], under thea priori anda posterioriregularization parameter choice rules, the authors found the orders of error estimate convergence areO(δ

p

p+) ( <p) andO(δ) (p> ), but in our paper, under thea priorianda posterioriregularization parameter choice rules, we found the order of error estimate convergence isO(δp+p ). Comparing references [, ], under the a posterioriregularization parameter choice, asp> , the authors found the error esti-mate convergence isO(δ) (p> ), which is a saturating phenomenon,i.e., if we add the smoothness of the solution, the error estimate order does not improve. In our method, the error estimate convergence isO(δ

p

p+), which does not appear to be a saturating

phe-nomenon. Finally, three numerical results show that the Landweber iterative method is very effective for this kind of ill-posed problems.

Acknowledgements

The authors would like to thanks the editor and the referees for their valuable comments and suggestions, that improved the quality of our paper.

Funding

The work is supported by the National Natural Science Foundation of China (11561045, 11501272) and the Doctor Fund of Lan Zhou University of Technology.

Abbreviations Not applicable.

Availability of data and materials Not applicable.

Competing interests

The authors declare that they have no competing interests.

Authors’ contributions

The main idea of this paper was proposed by FY. Y-PR prepared the manuscript initially and performed all the steps of the proofs in this research. All authors read and approved the final manuscript.

Publisher’s Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Received: 21 June 2017 Accepted: 1 November 2017

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Figure

Figure 1 The comparison of numerical effects between the exact solution and its regularized solutionfor Example 1.
Figure 2 The comparison of numerical effects between the exact solution and its regularized solutionfor Example 2.
Figure 4 The comparison of numerical effects between the exact solution and its regularized solutionfor Example 4.

References

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