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Article

Inverse Problem for a Time Fractional Parabolic Equation with Nonlocal Boundary Conditions

1
Department of Mathematics & Statistics, American University of the Middle East, Egaila 54200, Kuwait
2
Faculty of Engineering and Architecture, Fenerbahçe University, Istanbul 34758, Turkey
3
Department of Computer Engineering, Faculty of Engineering, Cyprus International University, North Cyprus, Mersin 10, Nicosia 99258, Turkey
*
Author to whom correspondence should be addressed.
Mathematics 2022, 10(9), 1479; https://doi.org/10.3390/math10091479
Submission received: 13 March 2022 / Revised: 13 April 2022 / Accepted: 22 April 2022 / Published: 28 April 2022
(This article belongs to the Topic Engineering Mathematics)

Abstract

:
This article considers an inverse problem of time fractional parabolic partial differential equations with the nonlocal boundary condition. Dirichlet-measured output data are used to distinguish the unknown coefficient. A finite difference scheme is constructed and a numerical approximation is made. Examples and numerical experiments, such as man-made noise, are provided to show the stability and efficiency of this numerical method.

1. Introduction

Numerous authors from the scientific, engineering, and mathematics fields have, in recent years, dealt with the dynamical systems described by fractional partial differential equations. This area has markedly grown worldwide.
Fractional-order partial-differential equations are the generalization of known classical-order partial-differential equations. Various methods have been formulated to solve fractional differential equations, such as the Laplace transform method, the Fourier transform method, the iteration method and the operational method. Generally speaking, nonlinear fractional differential equations do not have precise analytical solutions, which is why approximate and numerical techniques have been used. An equation in a specific region with a specific piece of data is known as a “direct problem”. In contrast, determining an unknown coefficient, an unknown source function or unknown boundary condition using measured output data is termed an “inverse problem”. According to unknown input, an inverse problem can be termed an inverse problem of coefficient identification, an inverse problem of source identification or an inverse problem of boundary value identification. Generally, inverse problems are ill-posed problems, since they are very sensitive to errors in measured input.
Nonlocal boundary conditions have recently received more attention in the mathematical formulation and numerical solution to inverse coefficient problems. There are physical applications in which nonlocal boundary conditions are encountered, such as chemical diffusion and heat-conduction biological processes. Inverse problems for time-fractional parabolic equations with nonlocal boundary conditions in their initial stages require exploration, as not many articles have been written on this. Furthermore, the numerical solution to these problems has still not been studied. An inverse coefficient, time-fractional parabolic partial-differential equation is studied in this paper, in the case of nonlocal boundary conditions. An analytical solution is obtained using eigenfunction expansions. An analysis of the time-dependent inverse coefficient problem is provided, with an additional measurement of the output data of Dirichlet type at the boundary point for the fractional diffusion equation, and the distinguishability of the mapping is investigated. The measured output data, the explicit form of input–output mapping, are additionally constructed. The fact that the distinguishability of input–output mapping implies the injectivity of the mapping is proved. The Fourier method is used to find a unique solution to the problem. Noisy Dirichlet measured output data are used to introduce the input–output mapping, consequently procuring an analytical representation of the mapping. Finally, a numerical approximation of the problem is constructed using the finite difference method. This paper is related to the modeling of diffusion problems, known as diffusion equation as given in (1):
D t α u ( x , t ) = u x x ( x , t ) p ( t ) u ( x , t ) + F ( x , t ) 0 < α 1 , ( x , t ) Ω T
u ( x , 0 ) = g ( x )
u x ( 0 , t ) = u x ( 1 , t ) , u ( 0 , t ) = Ψ 1 ( t )
where Ω T = ( x , t ) R 2 : 0 < x < 1 , 0 < t T and the fractional derivative D t α u ( x , t ) is defined in Caputo sense D t α u ( x , t ) = ( I 1 α u ) ( t ) , 0 < α 1 , I α being the Riemann–Liouville fractional integral,
( I α f ) ( t ) = 1 Γ ( α ) 0 t ( t τ ) α 1 · f ( τ ) d τ 0 < α 1 f ( t ) α = 0
Equations (1)–(3) indicate an inverse problem with respect to the unknown function p ( t ) . F ( x , t ) is a source function.
The left boundary value function Ψ 1 ( t ) belongs to C [ 0 , T ] . This function g ( x ) satisfies the following consistency conditions:
( C 1 ) g ( 0 ) = Ψ 1 ( 0 ) ( C 2 ) g ( 1 ) = u x ( 0 , 0 )
Under (C1) and (C2), the initial boundary value problem (1)–(3) has the unique solution u ( x , t ) , which is defined in the domain Ω ¯ T = { ( x , t ) R 2 : 0 x 1 , 0 t T } and belongs to the space
C ( Ω ¯ T ) W t 1 ( 0 , T ) C x 2 ( 0 , 1 )
where the solution u is continuous with respect to x and t and t, u t is in L 1 , u x and u x x is continuous.

2. An Analysis of the Inverse Coefficient Problem with Measured Data H ( T ) = U ( 1 , T )

Consider the inverse problem with measured output data h ( t ) at x = 1 . To formulate the solution for the parabolic problem (1)–(3) by using the Fourier method of separation of variables, we first introduce an auxiliary function v ( x , t ) as follows:
v ( x , t ) = u ( x , t ) Ψ 1 ( t ) ( 1 x ) , x [ 0 , 1 ]
by which we transform problem (1)–(3) into a problem with homogeneous boundary conditions. Therefore, the initial boundary value problem (1)–(3) can be rewritten in terms of v ( x , t ) in the given form:
D t α v ( x , t ) v x x ( x , t ) = D t α Ψ 1 ( t ) ( 1 x ) p ( t ) v ( x , t ) p ( t ) Ψ 1 ( t ) ( 1 x ) + F ( x , t )
v ( x , 0 ) = g ( x ) Ψ 1 ( 0 ) ( 1 x )
v x ( 0 , t ) v x ( 1 , t ) = 0
v ( 0 , t ) = 0
The unique solution to the initial-boundary value problem can be represented in the following form [1]:
v ( x , t ) = k = 1 < ζ ( θ ) , X k ( θ ) > E α , 1 ( λ k , t α ) Y k ( x ) + k = 1 0 t s α 1 · E α , α ( λ k s α ) < ξ ( θ , t s ; p j ( t ) ) , X k ( θ ) > d s Y k ( x )
where
ζ ( x ) = g ( x ) Ψ 1 ( 0 ) ( 1 x )
ξ ( x , t ) = D t α Ψ 1 ( t ) ( 1 x ) p ( t ) v ( x , t ) p ( t ) Ψ 1 ( t ) ( 1 x ) + F ( x , t )
Moreover, < ζ ( θ ) , Φ n ( θ ) > = 0 1 Φ n ( θ ) ζ ( θ ) d θ ; E α , β is the generalized Mittag–Leffler function, defined by [2]
E α , β ( z ) = n = 0 z n Γ ( β n + α )
Assume that X k ( x ) is the solution to the following Sturm–Liouville problem [3].
Φ x x ( x ) = λ Φ ( x ) 0 < x < 1 Φ ( 1 ) = Φ ( 0 ) Φ ( 0 ) = 0
Y 0 ( x ) = x , Y 2 k 1 ( x ) = x · cos ( 2 π k x ) , Y 2 k ( x ) = sin ( 2 π k x ) , k = 1 , 2 , , X 0 ( x ) = 2 , X 2 k 1 ( x ) = 4 cos ( 2 π k x ) , X 2 k ( x ) = 4 ( 1 x ) sin ( 2 π k x ) , k = 1 , 2 , . The system of functions Y n ’s are biorthonormal bases, that is, < < Y i , X j > > = 0 otherwise < < Y i , X j > > = 1 if i = j . These are also Riesz bases in L 2 .
The Dirichlet type of the measured output data at the boundary x = 1 in terms of v ( x , t ) can be written in the following form [4,5,6,7,8,9,10,11,12,13,14,15]:
h ( t ) = u ( 1 , t ) = v ( 1 , t )
To simplify (12), define the following:
z k ( t ) = k = 1 < ζ ( θ ) , X k ( θ ) > E α , 1 ( λ k t α )
w k ( t ) = k = 1 0 t s α 1 E α , α ( λ k s α ) < ξ ( θ , t s ; p j ( t ) ) , X k ( θ ) > d s
By using z k ( t ) and w k ( t ) , we can write the solution as follows:
v ( x , t ) = k = 1 z k ( t ) Y k ( x ) + k = 1 w k ( t ) Y k ( x )
The analytical solution to the problem [16,17,18,19,20,21,22,23,24,25,26,27,28,29,30] in series form is given in (20). Therefore, by substituting x = 1 ,
h ( t ) = v ( 1 , t ) = k = 1 z k ( t ) Y k ( 1 ) + k = 1 w k ( t ) Y k ( 1 )
is obtained.
As a result, h ( t ) is analytically determined as a series representation. The right-hand side of (21) defines the input–output mapping Ψ [ p ] :
Ψ [ p ] : = k = 1 z k ( t ) Y k ( 1 ) + k = 1 w k ( t ) Y k ( 1 )
The relationship between the functions p 1 ( t ) , p 2 ( t ) K at x = 1 and the corresponding outputs h j ( t ) = u ( 1 , t ; p j ) , j = 1 , 2 are given in the following lemma.
Lemma 1.
Let v 1 ( x , t ) = v ( x , t ; p 1 ) and v 2 ( x , t ) = v ( x , t ; p 2 ) be the solutions to the direct problem (8)–(11) corresponding to the admissible coefficients p 1 ( t ) , p 2 ( t ) K . If h j ( t ) = u ( 1 , t ; p j ) j = 1 , 2 are the corresponding outputs [31,32] h j ( t ) j = 1 , 2 satisfy the following series identity.
Δ h ( t ) = k = 1 Δ w k ( t ) Y k ( 1 )
for each t ( 0 , T ] where Δ h ( t ) = h 1 ( t ) h 2 ( t ) , Δ w k ( t ) = w k 1 ( t ) w k 2 ( t ) .
Proof. 
By using identity (21), the measured output data h j ( t ) = v ( 1 , t ) j = 1 , 2 can be written as:
h 1 ( t ) = k = 1 z k 1 ( t ) Y k ( 1 ) + k = 1 w k 1 ( t ) Y k ( 1 )
h 2 ( t ) = k = 1 z k 2 ( t ) Y k ( 1 ) + k = 1 z k 2 ( t ) Y k ( 1 )
Respectively, since, z k 1 = z k 2 ( t ) from the definition of z k ( t ) . The difference of these formulas implies the desired result. □
The lemma and the definitions enable us to reach the following conclusion.
Corollary 1.
Let the conditions of Lemma 1 hold. If, in addition, < ξ ( x , t ; p 1 ( t ) ) ξ ( x , t ; p 2 ( t ) ) , X k ( x ) > = 0 t ( 0 , T ] hold, then h 1 ( t ) = h 2 ( t ) t ( 0 , T ] .
Since Y k ( x ) k = 0 , 1 , 2 , forms a basis for the space and Y k ( 1 ) 0 k = 0 , 1 , 2 , , then < ξ 1 ( x , t ; p 1 ( t ) ) ξ 2 ( x , t ; p 2 ( t ) ) , X k ( x ) > 0 , at least for some k N . Hence, through the lemma, we can conclude that h 1 ( t ) h 2 ( t ) , which leads us to the following consequence: Ψ [ p 1 ] Ψ [ p 2 ] implies that p 1 ( t ) p 2 ( t ) .
Theorem 1.
Let conditions (C1) and (C2) hold. Assume that Ψ [ · ] : K C [ 0 , T ] is the input–output mapping defined by (22) and corresponding to the measured output h ( t ) = u ( 1 , t ) . In this case, the mapping Ψ [ p ] has the distinguishability property in the class of admissible parameter K, i.e., Ψ [ p 1 ] Ψ [ p 2 ] p 1 , p 2 K implies p 1 ( t ) p 2 ( t ) .
Proof. 
From the above explanation, the proof is clear. □

3. Numerical Method

This section considers the inverse problem given by (1)–(3) and (17). We use the finite difference method to discretize this problem. The domain 0 , 1 × 0 , T is divided into an M × N mesh with the spatial step size k = 1 / M in x direction and the time step size τ = T / N , respectively.
The grid points x i , t n are defined by
x i = i k ; i = 0 ; 1 ; 2 ; ; M ;
t j = j τ ; j = 0 ; 1 ; 2 ; ; N ;
in which M and N, are integers. The notations u i j , F i j , p j , g i , ψ 1 j and h j finite difference approximations of u ( x i , t j ) , F ( x i , t j ) , p ( t j ) , g ( x i ) , ψ 1 ( t j ) and h ( t j ) , respectively.
The finite-difference approximation for discretizing problem (1)–(3) and (17) is:
1 Γ ( 1 α ) m = 1 j + 1 Γ ( j m α + 1 ) ( j m ) ! u i m u i m 1 τ α = 1 h 2 u i + 1 j + 1 2 u i j + 1 + u i 1 j + 1 p j u i j + 1 + F i j
u i 0 = g i
u 0 j = ψ 1 j
u M + 1 j = u M j + u 1 j ψ 1 j ,
where 1 i M and 0 j N .
Now, let us construct the predicting-correcting mechanism. Firstly, if we use the measured output data- u ( 1 , t ) = h ( t ) , we obtain
p ( t ) = D t α h ( t ) u x x ( 1 , t ) F ( 1 , t ) h ( t ) .
The finite difference approximation of p ( t ) is
p j = H j 1 k 2 u M + 1 j + 1 2 u M j + 1 + u M 1 j + 1 F M j h j ,
where H j = D t α h ( t j ) , j = 0 , 1 , , N .
In numerical computation, since the time step is very small, we can take p j ( 0 ) = p j 1 , u i j ( 0 ) = u i j 1 , j = 0 , 1 , 2 , , N , i = 1 , 2 , , M . At each s-th iteration step, we first determine p j ( s ) from the formula.
p j ( s ) = H j 1 k 2 u M + 1 j + 1 ( s ) 2 u M j + 1 ( s ) + u M 1 j + 1 ( s ) F M j h j .
Then, from (26)–(29), we obtain:
1 Γ ( 1 α ) m = 1 j + 1 Γ ( j m α + 1 ) ( j m ) ! u i m ( s + 1 ) u i m 1 ( s ) τ α = 1 h 2 u i + 1 j + 1 ( s + 1 ) 2 u i j + 1 ( s + 1 ) + u i 1 j + 1 ( s + 1 ) p j ( s ) u i j + 1 ( s + 1 ) + F i j
u 0 j ( s ) = ψ 1 j
u M + 1 j ( s ) = u M j ( s ) + u 1 j ( s ) ψ 1 j ,
The system of Equations (27) and (33)–(35) can be solved by the Gauss elimination method and u i j + 1 ( s + 1 ) is determined. If the difference in values between the two iterations reaches the prescribed tolerance, the iteration is stopped and we accept the corresponding values p j ( s ) , u i j + 1 ( s + 1 ) ( i = 1 , 2 , , N x ) as p j , u i j + 1 ( i = 1 , 2 , , N x ) , on the (j)-th time step, respectively. By virtue of this iteration, we can move from level j to level j + 1 .
Example 1.
Consider the following problem for α = 1 / 2 :
F ( x , t ) = 16 t 2 5 π t + t 5 t 3 ( 2 π ) 2 sin ( 2 π x ) + cos 2 ( 2 π x ) exp ( sin ( 2 π x ) ) , φ ( x ) = 0 , Ψ 1 ( t ) = t 3 , and the measured output data is h ( t ) = t 3 ,
It is easy to check that the exact solution is:
p ( t ) , u ( x , t ) = t 2 , t 3 exp ( sin ( 2 π x ) ) .
Let us apply the scheme above for the step sizes k = 0.05 , τ = 0.05 . Figure 1 and Figure 2 show the exact and the numerical solutions of p ( t ) , u ( x , t ) when T = 1 .
We can see from these figures that the agreement between the numerical and exact solutions for p ( t ) and u ( x , T ) is excellent.

4. Conclusions

The distinguishability property of the input–output mapping Ψ [ · ] : K C [ 0 , T ] was investigated using measured output data x = 1 . The measured output data h ( t ) were obtained analytically as a series representation. This also leads to the input–output mapping Ψ [ · ] in an explicit form. In future studies, the authors plan to consider various fractional inverse coefficients or inverse source problems.

Author Contributions

Data curation, F.K.; Formal analysis, E.O.; Methodology, E.Ö. All authors have read and agreed to the published version of the manuscript.

Funding

The research received no external funding.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. The exact and numerical solutions of p ( t ) . The exact solution is shown with dashes line.
Figure 1. The exact and numerical solutions of p ( t ) . The exact solution is shown with dashes line.
Mathematics 10 01479 g001
Figure 2. The exact and numerical solutions of u ( x , 1 ) . The exact solution is shown with dashes line.
Figure 2. The exact and numerical solutions of u ( x , 1 ) . The exact solution is shown with dashes line.
Mathematics 10 01479 g002
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Ozbilge, E.; Kanca, F.; Özbilge, E. Inverse Problem for a Time Fractional Parabolic Equation with Nonlocal Boundary Conditions. Mathematics 2022, 10, 1479. https://doi.org/10.3390/math10091479

AMA Style

Ozbilge E, Kanca F, Özbilge E. Inverse Problem for a Time Fractional Parabolic Equation with Nonlocal Boundary Conditions. Mathematics. 2022; 10(9):1479. https://doi.org/10.3390/math10091479

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Ozbilge, Ebru, Fatma Kanca, and Emre Özbilge. 2022. "Inverse Problem for a Time Fractional Parabolic Equation with Nonlocal Boundary Conditions" Mathematics 10, no. 9: 1479. https://doi.org/10.3390/math10091479

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