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Article

Application of the Averaging Method to the Optimal Control of Parabolic Differential Inclusions on the Semi-Axis

1
Faculty of Mechanics and Mathematics, Taras Shevchenko National University of Kyiv, 4E Academician Glushkov Avenue, 03127 Kyiv, Ukraine
2
School of Mathematics and Statistics, Victoria University of Wellington, P.O. Box 600, Wellington 6140, New Zealand
*
Author to whom correspondence should be addressed.
These authors contributed equally to this work.
Axioms 2025, 14(1), 74; https://doi.org/10.3390/axioms14010074
Submission received: 30 October 2024 / Revised: 10 January 2025 / Accepted: 17 January 2025 / Published: 20 January 2025

Abstract

:
In this paper, we use the averaging method to find an approximate solution for the optimal control of parabolic differential inclusion with fast-oscillating coefficients on a semi-axis.

1. Introduction

The intensive development of science and technology consistently drives the search for effective control methods for various natural, economic, social, and technical processes. Mathematical models of such processes are represented by optimal control problems for different classes of evolutionary systems [1,2,3,4,5].
There are many approaches used in the investigation of control problems for differential equations and inclusions, with asymptotic methods being used fairly extensively [6]. One of the most successful among these is the averaging method, which was originally developed and rigorously justified by Krylov and Bogolyubov for the approximate analysis of oscillating processes in non-linear mechanics, and then further refined for control-related problems (see, e.g., the monograph by Plotnikov [7]). Motivated by modern engineering control applications, the averaging method has been recently applied to the solution of optimal control problems for linear control systems with rapidly oscillating coefficients within a finite interval [8] and on the semi-axis [9]. The approximate solutions of the optimal control problems for non-linear systems of differential inclusions with fast-oscillating parameters were investigated in [10,11] for the cases of a finite interval and on the semi-axis, respectively. The optimal control problem on the semi-axis for the Poisson equation with nonlocal boundary conditions was studied in [12]. The averaging method can also be applied to the study of singularly perturbed systems [13,14] and optimal control problems for differential equations with rapidly oscillating coefficients, both on a finite time interval and on the half-line [15,16]. Further applications of the averaging method for parabolic systems with fast-oscillating coefficients were considered in [17,18,19,20].
In the present paper, we use the averaging method for the investigation of the optimal control problem for nonlinear parabolic differential inclusion with fast-oscillating coefficients (with respect to the time variable) on a semi-axis. In contrast to the generic non-linear case of [11], we specifically make use of parabolicity in our setup. With this, we prove that the optimal control for the averaged problem can be considered as an “approximately” optimal one for the original problem. It is noteworthy to say that the results of [17,18,19] differ significantly from those of the current paper since only optimal control problems for parabolic equations were considered in [17,18], and while the optimal control for parabolic inclusions was considered in [19], it was only considered on finite intervals. The current paper, however, addresses the optimal control for parabolic inclusions on infinite intervals, which poses substantial challenges and requires an essentially different method of investigation. In particular, differential inclusions require the proper treatment of multi-valued functions, and the infinite interval for the corresponding optimal control problem raises an additional challenge in estimating the “tale” in the cost functional.

2. Problem Statement

Let Ω R n , n N be a bounded domain. In a cylinder Q = ( 0 , + ) × Ω , let us consider an initial boundary-value problem for a parabolic inclusion
y t A y + f t ε , y ( t , x ) + g ( y ) u , ( t , x ) Q , y | Ω = 0 , y | t = 0 = y 0 ( x ) .
Here, ε > 0 is a small parameter, f : R + × R + c o n v ( R ) (the space of nonempty, compact, convex subsets of R ) is a given multi-valued mapping, g : R R , q : Ω × R R are given real-valued mappings, A is a Laplacian operator, y is an unknown state function, and u is an unknown control function, which satisfies the following constraints:
u U L 2 ( Q ) ,
J ( y , u ) = Q e γ t q ( x , y ( t , x ) ) d t d x + α Q u 2 ( t , x ) d t d x inf ,
where γ , α are positive constants. Later, in Section 3, under natural and mild conditions on f , g , u , q , we will show that the problem of optimal control (1)–(3) has a solution { y ¯ ε , u ¯ ε } , i.e., for every u U and for any solution y ε of (1) with control u, it holds that
J ( y ¯ ε , u ¯ ε ) J ( y ε , u ) .
Despite proving the existence of a solution to (1)–(3), its construction is a challenging problem due to the presence of fast-varying coefficients. To address this issue, we consider the problem of finding an approximate solution of (1)–(3) by transitioning to the averaged coefficients. For this purpose, we assume there exists f ¯ : R R such that uniformly with regard to y R
d i s t H f ¯ ( y ) , 1 T 0 T f ( s , y ) d s 0 , T ,
where d i s t H ( A , B ) is a Hausdorff metric between sets A and B and the integral of the multivalued map is considered in the sense of Aumann [21]. Having the averaged version f ¯ of multi-valued mapping f at hand, we pose the following optimal control problem:
y t A y + f ¯ ( y ) + g ( y ) u , ( t , x ) Q , y | Ω = 0 , y | t = 0 = y 0 ( x ) ,
u U L 2 ( Q ) ,
J ( y , u ) = Q e γ t q ( x , y ( t , x ) ) d t d x + α Q u 2 ( t , x ) d t d x inf .
The primary objective of the paper is thus to prove the convergence
J ( y ¯ ε , u ¯ ε ) J ( y ¯ , u ¯ ) , ε 0 ,
where { y ¯ ε , u ¯ ε } is the solution of (1)–(3), and { y ¯ , u ¯ } is the solution of (5)–(7).

3. Preliminaries and Notation

Subsequently, we assume the following assumptions for the parameters of problem (1)–(3) are fulfilled:
( f 1 ) Multi-valued function f : R + × R + c o n v ( R ) is continuous and there exist C , C 1 > 0 such that
t 0 y R f ( t , y ) + : = sup ξ f ( t , y ) ξ R C + C 1 y R ,
where ξ R denotes the Euclidean norm of ξ R n ;
( g 1 ) function g : R R is a continuous function and there exists C 2 > 0 such that
y R g ( y ) R C 2 ;
( q 1 ) function q : Ω × R R is a Caratheodori function and there exists C 3 > 0 and functions K 1 L 2 ( Ω ) , K 2 L 1 ( Ω ) such that
q ( x , ξ ) R C 3 ξ R 2 + K 1 ( x ) , q ( x , ξ ) K 2 ( x ) ;
( U 1 ) U L 2 ( Q ) is closed and convex, 0 U ;
( γ 1 ) γ > 2 C 1 2 + 1 + C 2 ;
( A 1 ) uniformly with regard to y R , there exists the limit (4).
For u U and y 0 L 2 ( Ω ) , we understand the solution of (1) as a mild solution on every finite time interval; i.e., y is a solution of (1). If y L l o c 2 ( 0 , + ; H 0 1 ( Ω ) ) L l o c ( 0 , + ; L 2 ( Ω ) ) such that T > 0 , φ H 0 1 ( Ω ) , η C 0 ( 0 , T ) the following equality holds:
0 T ( y , φ ) H · η d t + 0 T ( y , φ ) H · η d t = 0 T ( l ( t ) , φ ) H · η d t + + 0 T ( g ( y ) u , φ ) H · η d t , l ( t ) f t ε , y
and l L l o c 2 ( 0 , + ; L 2 ( Ω ) ) .
Hereafter, we denote by · H and ( · , · ) H the classical norm and scalar product in H = L 2 ( Ω ) , by · V the classical norm in V : = H 0 1 ( Ω ) , and by V the dual space to V.
Note that due to assumptions ( f 1 ) and ( g 1 ) and the properties of operator A for y, from the definition of the mild solution we have
y t L l o c 2 ( 0 , + ; V ) .
Following this, we denote by F ε (or F ¯ ) a set of all pairs { y , u } , where y is a solution of (1) (or (5)) with control u.
The following lemma gives us result about the solvability of the optimal control problem (1)–(3).
Lemma 1. 
Let the conditions ( f 1 ), ( g 1 ), ( q 1 ), ( U 1 ), and ( γ 1 ) hold true. Then, for every ε > 0 , the problem (1)(3) has a solution { y ¯ ε , u ¯ ε } , that is,
J ( y ¯ ε , u ¯ ε ) J ( y , u ) { y , u } F ε .
Proof. 
We fix arbitrary ε > 0 and drop index ε throughout the proof for readability. First of all, note that by Theorem 3.1 from [22], the set of admissible pairs F ε is not empty. For further investigations, let us consider some a priori estimates for solutions. Taking into account the definition of the mild solution for parabolic inclusion, suppose that φ H 0 1 ( Ω )
d d t ( y , φ ) + ( y , φ ) = ( f 1 ( t ) , φ ) + ( g ( y ) u , φ ) for   almost   all   ( a . a . ) t > 0 f 1 ( t ) f ( t , y ( t ) )
Thus, we can consider the following equality:
0 s y ( t ) , y ( t ) H d t + 0 s y , y H d t = 0 s f 1 ( t ) , y ( t ) H d t + 0 s g ( y ) u , y ( t ) d t .
Integrating by parts, and taking into account Young’s inequality and the assumption ( g 1 ), we obtain
y ( s ) H 2 + 2 C ^ 0 s y ( t ) V 2 d t y 0 H 2 + 0 s f 1 ( t ) H 2 + y ( t ) H 2 d t + + C 2 0 s u ( t ) H 2 d t + 0 s y ( t ) 2 d t ,
where C ^ is the constant from the inequality y H 2 C ^ y V 2 for an arbitrary y H 0 1 ( Ω ) . Using (9), we have
f 1 ( t ) H 2 2 C 2 | Ω | + C 1 2 y ( t ) H 2 .
Then, from (16) we obtain
y ( s ) H 2 + 2 C ^ 0 s y ( t ) V 2 d t y 0 H 2 + 0 s 2 C 2 | Ω | d t + 0 s 2 C 1 2 y ( t ) H 2 d t + + 0 s y ( t ) H 2 d t + C 2 0 s u ( t ) H 2 d t + C 2 0 s y ( t ) H 2 d t = = y 0 H 2 + 2 C 2 | Ω | s + C 2 0 s u ( t ) H 2 d t + ( 2 C 1 2 + 1 + C 2 ) 0 s y ( t ) H 2 d t
and using Gronwall’s inequality, we arrive at
y ( t ) H 2 y 0 H 2 + 2 C 2 | Ω | t + C 2 u L 2 ( 0 , + ; H ) e ( 2 C 1 2 + 1 + C 2 ) t .
Note that from (16) and (17), we can conclude that M > 0 :
y L 2 ( 0 , T ; V ) 2 M T > 0 .
Due to the inclusion from (1), (9), and (17), we obtain
f 1 ( t ) H 2 ( C 2 | Ω | + C 1 2 M 1 ) 1 / 2 for a . a . t > 0
y ( t ) V C ^ ^ y ( t ) V + C | Ω | + C 1 M 1 + C 2 u ( t ) H for a . a . t > 0 ,
where M 1 = y 0 H 2 + 2 C 2 | Ω | T + C 2 u L 2 ( 0 , + ; H ) 2 e ( 2 C 1 2 + 1 + C 2 ) T , and as a consequence, there exist M 2 : = 2 ( C 2 | Ω | + C 1 2 M 1 ) T 1 / 2 and M 3 > 0 such that
f 1 L 2 ( 0 , T ; H ) M 2 , y L 2 ( 0 , T ; V ) M 3 T > 0 .
Taking into account ( q 1 ), we obtain
J ( y , u ) Q e γ t C 3 y R + K 1 ( x ) d t d x + α Q u 2 ( t , x ) d t d x .
In view of (17), we have
Q C 3 e γ t y R 2 d t d x C 3 0 + e γ t y 0 H 2 + 2 C 2 | Ω | t + C 2 u L 2 ( 0 , + ; H ) 2 e ( 2 C 1 2 + 1 + C 2 ) t d t = : I 1 + I 2 + I 3 .
Due to ( γ 1 ) and ( q 1 ), we obtain
I 1 : = C 3 0 + e ( γ + 2 C 1 2 + 1 + C 2 ) t y 0 H 2 d t = = C 3 y 0 H 2 γ + 2 C 1 2 + 1 + C 2 e ( γ + 2 C 1 2 + 1 + C 2 ) t | 0 + = = C 3 y 0 H 2 γ + 2 C 1 2 + 1 + C 2 = C 3 y 0 H 2 γ ( 2 C 1 2 + 1 + C 2 ) ,
I 2 = C 3 0 + 2 C 2 | Ω | t e ( γ + 2 C 1 2 + 1 + C 2 ) t d t = = C 3 2 C 2 | Ω | t e ( γ + 2 C 1 2 + 1 + C 2 ) t γ + 2 C 1 2 + 1 + C 2 | 0 + C 3 2 C 2 | Ω | 0 + e ( γ + 2 C 1 2 + 1 + C 2 ) t γ + 2 C 1 2 + 1 + C 2 d t = = C 3 2 C 2 | Ω | e ( γ + 2 C 1 2 + 1 + C 2 ) t ( γ + 2 C 1 2 + 1 + C 2 ) 2 | 0 + = C 3 2 C 2 | Ω | ( γ + 2 C 1 2 + 1 + C 2 ) 2 ,
I 3 = C 3 C 2 0 + u L 2 ( 0 , + ; H ) 2 e ( γ + 2 C 1 2 + 1 + C 2 ) t d t = = C 3 C 2 u L 2 ( 0 , + ; H ) 2 γ + 2 C 1 2 + 1 + C 2 e ( γ + 2 C 1 2 + 1 + C 2 ) t | 0 + = C 3 C 2 u L 2 ( 0 , + ; H ) 2 γ ( 2 C 1 2 + 1 + C 2 ) .
Further we have that
Q e γ t K 1 ( x ) d t d x = 0 + e γ t d t · Ω K 1 ( x ) d x = = e γ t γ | 0 + · Ω K 1 ( x ) d x = 1 γ Ω K 1 ( x ) d x = 1 γ Ω d x 1 / 2 · Ω K 1 2 ( x ) d x 1 / 2 = | Ω | 1 / 2 γ · K 1 L 2 ( Ω ) .
Taking into account (23)–(26), we have
J ( y , u ) C 3 y 0 H 2 γ ( 2 C 1 2 + 1 + C 2 ) + C 3 2 C 2 | Ω | ( γ + 2 C 1 2 + 1 + C 2 ) 2 + C 3 C 2 u L 2 ( 0 , + ; H ) 2 γ ( 2 C 1 2 + 1 + C 2 ) + + | Ω | 1 / 2 γ · K 1 L 2 ( Ω ) + α u L 2 ( 0 , + ; H ) 2 L y 0 H 2 + u L 2 ( 0 , + ; H ) 2 + K 1 L 2 ( Ω ) + 1 < ,
where L = max { C 3 γ ( 2 C 1 2 + 1 + C 2 ) ; C 3 C 2 γ ( 2 C 1 2 + 1 + C 2 ) + α ; | Ω | 1 / 2 γ ; C 3 2 C 2 ( γ + 2 C 1 2 + 1 + C 2 | Ω | ) 2 } .
Now, let { y n , u n } be a minimizing sequence, that is,
lim n J ( y n , u n ) = inf { y , u } F ε J ( y , u ) = : J ¯ ε .
Note that in view of ( q 1 ) { y , u } F ε , it holds that
J ( y , u ) K 2 L 1 ( Ω ) γ J ¯ ε K 2 L 1 ( Ω ) γ > .
From (28), for rather large n
J ( y n , u n ) J ¯ ε + 1 .
On the other hand,
J ( y n , u n ) K 2 L 1 ( Ω ) γ + α u n L 2 ( 0 , + ; H ) 2 .
Inequalities (29), (30) imply that { u n } is bounded in L 2 ( 0 , + ; H ) and thus for subsequence
u n u weakly in L 2 ( 0 , + ; H )
In view of the convexity of U, we have that u U . From (17), (18) we obtain that T > 0 { y n } is bounded in L 2 ( 0 , T ; V ) L ( 0 , T ; H ) , from (21) we have that y n t is bounded in L 2 ( 0 , T ; V ) . Due to the Compactness Lemma from [23], we conclude that up to subsequence T > 0
y n y weakly in L 2 ( 0 , T ; V ) , y n y i n L 2 ( 0 , T ; H ) , t 0 y n ( t ) y ( t ) weakly in H , y n ( t , x ) y ( t , x ) a . e . i n Q .
Let us consider y n to be a mild solution of the problem
y n t = A y n + f 1 n ( t ) + g ( y n ) u n y n | Ω = 0 y n | t = 0 = y 0 ( x )
with f 1 n ( t ) f ( t , y n ( t ) ) .
From (21), (32), and Lemma 3.2 from [24], we have that f 1 n f 1 weakly in L 2 ( 0 , T ; H ) , y n y in C ( 0 , T ; H ) T > 0 , where y is the solution of (1) and f 1 ( t ) f ( t , y ( t ) ) . Thus, from (32) and Lebesgue’s Dominated Convergence Theorem, we can pass to the limit in the equality (12), which we can apply to { y n , u n } and receive that { y , u } F ε . In view of to the pointwise convergence,
e γ t · q ( x , y n ( t , x ) ) e γ t q ( x , y ( t , x ) ) a . e . i n Q ,
Given Fatou’s lemma and the weak convergence in (31), we obtain
J ¯ ε = lim n J ( y n , u n ) lim ̲ n Q e γ t q ( x , y n ( t , x ) ) d t d x + + lim ̲ n α Q u 2 ( t , x ) d t d x J ( y , u ) .
Therefore, { y , u } is a solution of (1)–(3). □
Remark 1. 
In view of the properties of the Hausdorff metric, we have that Condition ( f 1 ) is satisfied for the averaged function f ¯ ( y ) with the same constants as for f ( t , y ) . Indeed,
ξ f ( t , y ) : ξ R C + C 1 y R .
Due to the condition d i s t H f ¯ , 1 T 0 T f ( s , y ) d s 0 , T , we obtain that ε > 0 T 0 : T T 0 we have f ¯ ( y ) O ε 1 T 0 T f ( s , y ) d s . Furthermore, we obtain
f ¯ ( y ) R 1 T 0 T f ( s , y ) d s + + ε 1 T 0 T f ( s , y ) + d s + ε C + C 1 y R + ε .
The existence of a solution { y ¯ , u ¯ } to (5)(7) can be proved following similar arguments to the proof of the existence of { y ¯ ε , u ¯ ε } for problem (1)(3). Note, however, that the construction of { y ¯ , u ¯ } is much simpler than that of { y ¯ ε , u ¯ ε } due to the averaged nature of the coefficients involved.

4. Main Result

Theorem 1. 
Suppose that the assumptions ( f 1 ), ( g 1 ), ( q 1 ), ( u 1 ), ( γ 1 ), and ( A 1 ) are fulfilled and, moreover, that for every u U there exists a unique solution of the problem (5). We additionally assume that η > 0 δ > 0 t 0 y , z R
y z R < δ d i s t ( f ( t , y ) , f ( t , z ) ) < η .
Let { y ¯ ε , u ¯ ε } be a solution of (1)(3). Then,
J ( y ¯ ε , u ¯ ε ) J ( y ¯ , u ¯ ) , ε 0
and up to subsequence
y ¯ ε y ¯ i n L 2 ( 0 , + ; H ) ,
u ¯ ε u ¯ w e a k l y i n L 2 ( 0 , + ; H ) .
Here, { y ¯ , u ¯ } is a solution of (5)(7).
Proof. 
Let ε n 0 and { y ¯ n , u ¯ n } be a solution of (1)–(3) for ε = ε n . Since { y ¯ n , u ¯ n } is an optimal pair, we obtain
J ( y ¯ n , u ¯ n ) J ( y n , 0 ) ,
where y n is a solution of (1) with ε = ε n and u 0 . Therefore, from (27) and (30), we obtain
K 2 L 1 ( Ω ) γ + α u ¯ n L 2 ( 0 , + ; H ) L ( y 0 H 2 + K 1 L 2 ( Ω ) + 1 ) .
Applying similar reasoning as in the proof of Lemma 1, we conclude that on subsequence for some y ^ , u ^ :
u ¯ n u ^   weakly   in   L 2 ( 0 , + ; H ) , n ,
y ¯ n y ^ in   the   sense   of   ( 32 ) , n .
Let us show that { y ^ , u ^ } F ¯ , i.e., y ^ is a solution of the corresponding averaged problem (5) with control u ^ . In order to achieve this goal, we have to make a limit transition in the equality
y ¯ n ( T ) , φ H y 0 , φ H + 0 T y ¯ n , φ H d t = = 0 T f 1 ε n ( t ) , φ H d t + 0 T g ( y ¯ n ) u ¯ n , φ H d t
for arbitrary φ V and T > 0 , where f 1 ε n ( t ) f t ε n , y ¯ n .
As for the left-hand side of the equality (41), the limit transition is a direct consequence of (40). From the Dominated Convergence Theorem, we have that
g ( y ¯ n ) g ( y ^ ) i n L 2 ( 0 , T ; H ) , n Ω 0 T f 1 ε n ( t ) φ d t d x Ω 0 T f ¯ ( y ^ ) φ d t d x = d i s t H Ω 0 T f 1 ε n ( t ) φ d t d x , Ω 0 T f ¯ ( y ^ ) φ d t d x d i s t H Ω 0 T f t ε n , y ¯ n ( t , x ) φ d t d x , Ω 0 T f ¯ ( y ^ ) φ d t d x .
We still have to prove that
d i s t H Ω 0 T f t ε n , y ¯ n ( t , x ) φ d t d x , Ω 0 T f ¯ ( y ^ ) φ d t d x 0 , n .
First of all, let us note that due to ( A 1 ) and [25] 0 < a < b φ H , it holds that
d i s t H Ω a b f t ε n , ψ ( x ) φ d t d x , Ω a b f ¯ ( ψ ( x ) ) φ d t d x 0 , n
In view of Egorov’s theorem [26] δ > 0 Q 1 δ Q T such that μ ( Q 1 δ ) < δ and
y ¯ n y ^   uniformly   on   Q T \ Q 1 δ , a s n .
Here, μ is Lebesgue’s measure on R 2 .
On the other hand, there exists a sequence of step functions
y m ( t , x ) = k = 1 m y k m ( x ) χ A k m ( t ) , { y k m } H
with { A k m = ( a k m , b k m ) } being a covering of ( 0 , T ) such that
y m y ^   in   L 2 ( 0 , T ; H )   and   almost   everywhere   in   Q T .
Moreover, δ > 0 Q 2 δ Q T such that μ ( Q 2 δ ) < δ and
y m y ^   uniformly   on   Q T \ Q 2 δ a s m .
Furthermore, we have that
d i s t H Q T f t ε n , y ¯ n ( t , x ) φ d t d x , Q T f ¯ ( y ^ ( t , x ) ) φ d t d x d i s t H Q T f t ε n , y ¯ n ( t , x ) φ d t d x , Q T f t ε n , y ^ ( t , x ) φ d t d x + + d i s t H Q T f t ε n , y ^ ( t , x ) φ d t d x , Q T f ¯ ( y ^ ( t , x ) ) φ d t d x = : I 1 ( n ) + I 2 ( n ) .
Due to (44), Hölder’s inequality, (9), and (17), we have
I 1 ( n ) Q T d i s t H f t ε n , y ¯ n ( t , x ) , f t ε n , y ^ ( t , x ) φ d t d x Q T \ Q 1 δ d i s t H f t ε n , y ¯ n ( t , x ) , f t ε n , y ^ ( t , x ) φ d t d x + + Q 1 δ d i s t H f t ε n , y ¯ n ( t , x ) , f t ε n , y ^ ( t , x ) φ d t d x Q T \ Q 1 δ d i s t H f t ε n , y ¯ n ( t , x ) , f t ε n , y ^ ( t , x ) φ R d t d x + + 2 C Q 1 δ φ d t d x + 2 C 1 Q 1 δ y R φ d t d x Q T \ Q 1 δ d i s t f t ε n , y ¯ n ( t , x ) , f t ε n , y ^ ( t , x ) φ R d t d x + + 2 C φ H · δ 1 / 2 T 1 / 2 + 2 C 1 M 1 φ H · δ 1 / 2 · T .
Due to (34), for a given δ > 0 λ n 1 t 0
y z R < λ d i s t f t ε n , y , f t ε n , z δ 1 / 2 .
Therefore, choosing n 1 such that n n 1
sup ( t , x ) Q T \ Q 1 δ y ¯ n ( t , x ) y ^ ( t , x ) < λ ,
we have from (46) that n n 1
I 1 ( n ) δ 1 / 2 μ 1 / 2 ( Q T ) φ H T + 2 C φ H δ 1 / 2 T + + 2 C 1 M 1 φ H δ 1 / 2 T C ˜ ( T ) δ 1 / 2 .
On the other hand, for every step function y m ( t , x ) , we have, using (43), that m 1
d i s t H Q T f t ε n , y m ( t , x ) φ d t d x , Q T f ¯ ( y m ( t , x ) ) φ d t d x = = d i s t H k = 1 m Ω A k m f t ε n , y k m ( t , x ) φ d t d x , k = 1 m Ω A k m f ¯ ( y k m ( x ) ) φ d t d x k = 1 m d i s t H Ω A k m f t ε n , y k m ( t , x ) φ d t d x , Ω A k m f ¯ ( y k m ( x ) ) φ d t d x 0 , n .
Thus, m 1 n 2 = n 2 ( m ) n n 2
d i s t H Q T f t ε n , y m ( t , x ) φ d t d x , Q T f ¯ ( y m ( t , x ) ) φ d t d x < δ .
Furthermore, m 0 m m 0 n 1
d i s t H Q T \ Q 2 δ f t ε n , y ^ ( t , x ) φ d t d x , Q T \ Q 2 δ f t ε n , y m ( t , x ) φ d t d x Q T \ Q 2 δ d i s t H f t ε n , y ^ ( t , x ) , f t ε n , y m ( t , x ) φ R d t d x δ 1 / 2 μ 1 / 2 ( Q T ) φ H T ,
d i s t H Q T \ Q 2 δ f ¯ ( y ^ ( t , x ) ) φ d t d x , Q T \ Q 2 δ f ¯ ( y m ( t , x ) ) φ d t d x Q T \ Q 2 δ d i s t H f ¯ ( y ^ ( t , x ) ) φ , f ¯ ( y m ( t , x ) ) φ R d t d x δ 1 / 2 μ 1 / 2 ( Q T ) φ H T .
Combining (48)–(51), we obtain m m 0 n n 2 ( m )
I 2 ( n ) 2 δ 1 / 2 μ 1 / 2 ( Q T ) φ H T + δ C ˜ ˜ ( T ) δ 1 / 2 .
Inequalities (47), (52) imply (42). Thus, we can pass to the limit in (41) and obtain that ( y ^ , u ^ ) F ¯ .
Let us now show that { y ^ , u ^ } is an optimal process in (5)–(7).
Due to Fatou’s lemma, we have
lim ̲ n J ( y ¯ n , u ¯ n ) J ( y ^ , u ^ ) .
On the other hand, for every u U and any y n —a solution of (1) with control u and ε = ε n —we obtain
J ( y ¯ n , u ¯ n ) J ( y n , u ) .
Applying similar reasoning as in proof of the Lemma 1 for { y n } , we obtain that y n y in the sense of (32), where y is a unique solution of (5) with control u.
Let us show that
Q e γ t q ( x , y n ( t , x ) ) d t d x Q e γ t q ( x , y ( t , x ) ) d t d x .
Indeed, due to ( q 1 ), we have
e γ t q ( x , y n ( t , x ) ) C 3 e γ t y n ( t , x ) R 2 + e γ t K 1 ( x ) .
Since y n y in L 2 ( 0 , T ; H ) and a.e. in Q, in view of ( γ 1 ), (17), (23)–(26), we deduce from Lebesgue’s Dominated Convergence Theorem:
T > 0 Q T e γ t q ( x , y n ( t , x ) ) d t d x Q T e γ t q ( x , y ( t , x ) ) d t d x , n .
On the other hand, from (17) and (55),
T + Ω e γ t q ( x , y n ( t , x ) ) d t d x T + e γ t C 3 y n ( t ) H 2 + | Ω | 1 / 2 K 1 L 2 ( Ω ) d t T + e γ t ( ( C 3 y 0 H 2 + 2 C 2 C 3 | Ω | t + C 3 C 2 u L 2 ( 0 , + ; H ) 2 ) e ( 2 C 1 2 + 1 + C 2 ) t + + | Ω | 1 / 2 K 1 L 2 ( Ω ) ) d t = : J 1 + J 2 + J 3 + J 4 .
Let us consider each term of the right hand side of (57) separately:
J 1 : = T + C 3 y 0 H 2 e ( γ + 2 C 1 2 + 1 + C 2 ) t d t = = C 3 y 0 H 2 γ + 2 C 1 2 + 1 + C 2 e ( γ + 2 C 1 2 + 1 + C 2 ) t | T + = = C 3 y 0 H 2 γ ( 2 C 1 2 + 1 + C 2 ) e ( γ + 2 C 1 2 + 1 + C 2 ) T ;
J 2 : = T + 2 C 2 C 3 | Ω | t e ( γ + 2 C 1 2 + 1 + C 2 ) t d t = 2 C 2 C 3 | Ω | t e ( γ + 2 C 1 2 + 1 + C 2 ) t γ + 2 C 1 2 + 1 + C 2 | T + 2 C 2 C 3 | Ω | T + e ( γ + 2 C 1 2 + 1 + C 2 ) t γ + 2 C 1 2 + 1 + C 2 d t = = 2 C 2 C 3 T | Ω | e ( γ + 2 C 1 2 + 1 + C 2 ) T γ ( 2 C 1 2 + 1 + C 2 ) 2 C 2 C 3 | Ω | e ( γ + 2 C 1 2 + 1 + C 2 ) t ( γ + 2 C 1 2 + 1 + C 2 ) 2 | T + = = 2 C 2 C 3 T | Ω | e ( γ + 2 C 1 2 + 1 + C 2 ) T γ ( 2 C 1 2 + 1 + C 2 ) + 2 C 2 C 3 | Ω | e ( γ + 2 C 1 2 + 1 + C 2 ) T ( γ + 2 C 1 2 + 1 + C 2 ) 2 ;
J 3 : = T + C 3 C 2 u L 2 ( 0 , + ; H ) 2 e ( γ + 2 C 1 2 + 1 + C 2 ) t d t = = C 3 C 2 u L 2 ( 0 , + ; H ) 2 γ + 2 C 1 2 + 1 + C 2 e ( γ + 2 C 1 2 + 1 + C 2 ) t | T + = = C 3 C 2 u L 2 ( 0 , + ; H ) 2 γ ( 2 C 1 2 + 1 + C 2 ) e ( γ + 2 C 1 2 + 1 + C 2 ) T ;
J 4 : = T + e γ t | Ω | 1 / 2 K 1 L 2 ( Ω ) d t = | Ω | 1 / 2 K 1 L 2 ( Ω ) e γ t γ | T + = = | Ω | 1 / 2 K 1 L 2 ( Ω ) e γ T γ .
Combining (58)–(61), we obtain (54).
From (54) we obtain the following inequality: { y , u } F ¯
J ( y ^ , u ^ ) lim ̲ n J ( y ¯ n , u ¯ n ) lim ̲ n J ( y n , u ) = J ( y , u ) .
This means that { y ^ , u ^ } is a solution of (5)–(7).
Let us substitute u = u ^ in previous arguments. Then, y = y ^ in view of uniqueness. Thus, from (62), we obtain
J ( y ^ , u ^ ) lim ̲ n J ( y ¯ n , u ¯ n ) J ( y ^ , u ^ ) .
These inequalities imply that up to subsequence
J ( y ¯ n , u ¯ n ) J ( y ^ , u ^ ) , n .
Since J ( y ^ , u ^ ) = inf { y , u } F ¯ J ( y , u ) , then the convergence in (64) holds for the whole sequence. Therefore, (35) is proved. □
Let us consider an example of an investigated problem. Let Ω = ( 0 , l ) , A y = 2 y x 2 and consider the following problem:
y t A y e y 2 · sin 2 2 t ε , e y 2 · sin 2 t ε + u , ( t , x ) Q , y | x = 0 = y | x = l = 0 , y | t = 0 = y 0 ( x ) , J ( y , u ) = Q e γ t y 2 ( t , x ) d t d x + α Q u 2 ( t , x ) d t d x inf .
The corresponding averaged problem is
y t A y = 1 2 + u , ( t , x ) Q , y | x = 0 = y | x = l = 0 , y | t = 0 = y 0 ( x ) , J ( y , u ) = Q e γ t y 2 ( t , x ) d t d x + α Q u 2 ( t , x ) d t d x inf .
We consider a control u L 2 ( Q ) such that u ( t , x ) R 1 a.e. We can see that Lemma 1 (Remark 1) and Theorem 1 can be applied to problems (65) and (66).

5. Discussion

Our aim was to establish a theoretical result illustrating the effectiveness of the averaging method in finding approximate solutions for the optimal control problem of a nonlinear parabolic differential inclusion with rapidly oscillating parameters. Specifically, we demonstrated that the optimal control of the averaged problem can be regarded as “approximately” optimal for the original perturbed system. Importantly, this was achieved under fairly mild and natural assumptions regarding the system’s parameters. To further highlight the significance and utility of the averaging method in such contexts, we intend to extend our research to its application in control problems involving hyperbolic differential inclusions.

Author Contributions

Conceptualization, N.K. and P.F.; methodology, N.K. and P.F.; formal analysis, N.K. and P.F.; investigation, N.K. and P.F.; writing—original draft preparation, N.K. and P.F.; writing—review and editing, N.K. and P.F. All authors have read and agreed to the published version of the manuscript.

Funding

This research received no external funding.

Data Availability Statement

Data are contained within the article.

Conflicts of Interest

The authors declare no conflicts of interest.

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Kasimova, N.; Feketa, P. Application of the Averaging Method to the Optimal Control of Parabolic Differential Inclusions on the Semi-Axis. Axioms 2025, 14, 74. https://doi.org/10.3390/axioms14010074

AMA Style

Kasimova N, Feketa P. Application of the Averaging Method to the Optimal Control of Parabolic Differential Inclusions on the Semi-Axis. Axioms. 2025; 14(1):74. https://doi.org/10.3390/axioms14010074

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Kasimova, Nina, and Petro Feketa. 2025. "Application of the Averaging Method to the Optimal Control of Parabolic Differential Inclusions on the Semi-Axis" Axioms 14, no. 1: 74. https://doi.org/10.3390/axioms14010074

APA Style

Kasimova, N., & Feketa, P. (2025). Application of the Averaging Method to the Optimal Control of Parabolic Differential Inclusions on the Semi-Axis. Axioms, 14(1), 74. https://doi.org/10.3390/axioms14010074

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