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Article

Monotone Iterative and Upper–Lower Solution Techniques for Solving the Nonlinear ψ−Caputo Fractional Boundary Value Problem

by
Abdelatif Boutiara
1,
Maamar Benbachir
2,
Jehad Alzabut
3,*,† and
Mohammad Esmael Samei
4
1
Laboratory of Mathematics and Applied Sciences, University of Ghardaia, Ghardaia 47000, Algeria
2
Faculty of Sciences, Saad Dahlab University, Blida 09000, Algeria
3
Department of Industrial Engineering, OSTİM Technical University, 06374 Ankara, Turkey
4
Department of Mathematics, Faculty of Basic Science, Bu-Ali Sina University, Hamedan 6517838695, Iran
*
Author to whom correspondence should be addressed.
Current address: Department of Mathematics and General Sciences, Prince Sultan University, Riyadh 11586, Saudi Arabia.
Fractal Fract. 2021, 5(4), 194; https://doi.org/10.3390/fractalfract5040194
Submission received: 8 September 2021 / Revised: 13 October 2021 / Accepted: 27 October 2021 / Published: 3 November 2021

Abstract

:
The objective of this paper is to study the existence of extremal solutions for nonlinear boundary value problems of fractional differential equations involving the ψ Caputo derivative C D a + σ ; ψ ϱ ( t ) = V ( t , ϱ ( t ) ) under integral boundary conditions ϱ ( a ) = λ I ν ; ψ ϱ ( η ) + δ . Our main results are obtained by applying the monotone iterative technique combined with the method of upper and lower solutions. Further, we consider three cases for ψ * ( t ) as t , Caputo, 2 t , t , and Katugampola (for ρ = 0.5 ) derivatives and examine the validity of the acquired outcomes with the help of two different particular examples.

1. Introduction

The notion of fractional calculus refers to the last three centuries and it can be described as the generalization of classical calculus to orders of integration and differentiation that are not necessarily integers. Many researchers have used fractional calculus in different scientific areas [1,2,3,4].
In the literature, various definitions of the fractional-order derivative have been suggested. The oldest and the most famous ones advocate for the use of the Riemann–Liouville and Caputo settings. One of the most recent definitions of a fractional derivative was delivered by Kilbas et al., where the fractional differentiation of a function with respect to another function in the sense of Riemann–Liouville was introduced [5]. They further defined appropriate weighted spaces and studied some of their properties by using the corresponding fractional integral. In [6], Almaida defined the following new fractional derivative and integrals of a function with respect to some other function:
D a + σ , ψ * ϱ ( x ) : = 1 ψ * ( ξ ) d d x n I a + n σ , ψ * ϱ ( x ) = 1 ψ * ( ξ ) d d x n a x ψ * ( ξ ) Γ ( n σ ) ψ * ( x ) ψ * ( ξ ) n σ 1 ϱ ( ξ ) d ξ ,
where n = [ σ ] + 1 and 
I a + σ , ψ * ϱ ( x ) : = a x ψ ( ξ ) Γ ( σ ) ψ * ( x ) ψ * ( ξ ) σ 1 ϱ ( ξ ) d ξ ,
respectively. He called the fractional derivative the ψ Caputo fractional operator. In the above definitions, we get the Riemann–Liouville and Hadamard fractional operators whenever we consider ψ * ( x ) = x or ψ * ( x ) = ln x , respectively. Many researchers used this ψ Caputo fractional derivative (see [7,8,9,10,11,12,13] and the references therein). Abdo et al., in [14], investigated the BVP for a fractional differential equation (FDE) involving ψ * operator and was given as
D t 1 + n σ , ψ * ϱ ( t ) = V ( t , ϱ ( t ) ) , t ı = : [ t 1 , t 2 ] ,
ϱ ψ * [ k ] ( t 1 ) = ϱ t 1 k , ( k = 0 , 1 , 2 , , n 2 ) , ϱ ψ * [ n 1 ] ( t 2 ) = ϱ t 2 . For more details on the development of the theory of fractional differential equations, one can refer to [15,16,17,18,19,20]. In order to establish existence theory, researchers have used diverse techniques of nonlinear analysis consisting of fixed-point theory, hybrid fixed-point theory, topological degree theory, and measure of noncompactness [21,22,23,24]. However, the use of the monotone iterative technique ( MIT ) along with the method of upper and lower solutions (u-l solutions) for solving a BVP involving the operator remains rare.
In the present paper, we are interested in the MIT blended with the method of upper and lower solutions to prove the existence of extremal solutions for the following BVP of an FDE involving the operator
C D t 1 + σ ; ψ * ϱ ( t ) = V ( t , ϱ ( t ) ) , t ı , ϱ ( t 1 ) = λ I ν ; ψ * ϱ ( η ) + δ ,
where C D σ ; ψ * is the operator (1) of order 0 < σ , ν 1 , I σ ; ψ * is the operator (2), the function V : [ t 1 , t 2 ] × R R is continuous, λ and δ are real constants, and  η ( t 1 , t 2 ) . It is worth mentioning that the MIT is efficiently used in the literature to investigate the existence of extremal solutions to many applied problems of nonlinear equations [25,26,27,28,29,30,31,32,33,34,35,36,37,38].
The rest of this paper is organized as follows. In Section 2, we recall some preliminary concepts, definitions, and lemmas that will act as prerequisites to proving the main results. The main results are stated and proved in Section 3. Finally, we give numerical examples to illustrate the correctness of the outcome.

2. Preliminaries

Let σ > 0 . The left-sided ψ Riemann–Liouville fractional integral (l-s- ψ -RLfi) of order σ for an integrable function ϱ : ı R with respect to another function ψ * : ı R , which is an increasing differentiable function such that ψ * ( t ) 0 , ( t ı ) , is defined as follows:
I t 1 + σ ; ψ * ϱ ( t ) = 1 Γ ( σ ) t 1 t ψ * ( ξ ) ψ * ( t 1 ) ψ * ( ξ ) σ 1 ϱ ( ξ ) d ξ ,
where Γ is the classical Euler Gamma function [5,6]. Appendix A Algorithm A1 shows the MATLAB lines for the calculation of the l-s- ψ -RLfi. Let n N and ψ * , ϱ C n ( ı , R ) be two functions such that ψ * is increasing and ψ * ( t ) 0 , ( t ı ) . The left-sided ψ Riemann–Liouville fractional derivative (l-s- ψ -RLfd) of a function ϱ of order σ is defined by
D t 1 + σ ; ψ * ϱ ( t ) = 1 ψ * ( t ) d d t n I t 1 + n σ ; ψ * ϱ ( t ) = 1 Γ ( n σ ) 1 ψ * ( t ) d d t n t 1 t ψ * ( ξ ) ( ψ * ( t ) ψ * ( ξ ) ) n σ 1 ϱ ( ξ ) d ξ ,
where n = [ σ ] + 1 [6]. Appendix A Algorithm A2 shows the MATLAB lines for the calculation of the l-s- ψ -RLfd. In addition, the left-sided ψ Caputo fractional derivative (l-s- ψ -Cfd) of a function ϱ of order σ is defined by
C D t 1 + σ ; ψ * ϱ ( t ) = I t 1 + n σ ; ψ * 1 ψ * ( t ) d d t n ϱ ( t ) ,
where ψ * , ϱ C n ( ı , R ) are two functions such that ψ * is increasing, ψ * ( t ) 0 , ( t ı ) , and n = [ σ ] + 1 and n = σ whenever σ N and σ N , respectively [6]. To simplify the notation, we use:
ϱ ψ * [ n ] ( t ) = 1 ψ * ( t ) d d t n ϱ ( t ) .
So,
C D t 1 + σ ; ψ * ϱ ( t ) = 1 Γ ( n σ ) t t ψ * ( ξ ) ( ψ * ( t ) ψ * ( ξ ) ) n σ 1 ϱ ψ * [ n ] ( ξ ) d ξ , σ N , ϱ ψ * [ n ] ( t ) , σ N .
Appendix A Algorithm A3 shows the MATLAB lines for the calculation of C D t 1 + σ ; ψ * ϱ ( t ) . If ϱ C n ( ı , R ) , then the ψ Cfd of order σ of ϱ is determined as ([6], Theorem 3):
C D t 1 + σ ; ψ * ϱ ( t ) = D t 1 + σ ; ψ * ϱ ( t ) k = 0 n 1 ϱ ψ * [ k ] ( t 1 ) k ! ( ψ * ( t ) ψ * ( t 1 ) ) k .
Lemma 1
([8]). Let σ , ν > 0 , and ϱ L 1 ( ı , R ) . Then, I t 1 + σ ; ψ * I t 1 + σ ; ψ * ϱ ( t ) = I t 1 + σ + ν ; ψ * ϱ ( t ) , ( t ı ) . In particular, if  ϱ C ( ı , R ) , then I t 1 + σ ; ψ * I t 1 + ν ; ψ * ϱ ( t ) = I t + σ + ν ; ψ * ϱ ( t ) , ( t ı ) .
Lemma 2
([8]). Let σ > 0 . If  ϱ C ( ı , R ) , then C D t 1 + σ ; ψ * I t + σ ; ψ * ϱ ( t ) = ϱ ( t ) , ( t ı ) , and
I t 1 + σ ; ψ * C D t 1 + σ ; ψ * ϱ ( t ) = ϱ ( t ) k = 0 n 1 ϱ ψ * [ k ] ( t 1 ) k ! ψ * ( t ) ψ * ( t 1 ) k , ( t ı ) ,
whenever ϱ C n ( ı , R ) , n 1 < σ < n .
Lemma 3
([5,8]). Let t > t 1 , σ 0 , and ν > 0 . Then,
(1) 
I t 1 + σ ; ψ * ( ψ * ( t ) ψ * ( t 1 ) ) ν 1 = Γ ( ν ) Γ ( ν + σ ) ( ψ * ( t ) ψ * ( t 1 ) ) ν + σ 1 ;
(2) 
C D t 1 + σ ; ψ * ( ψ * ( t ) ψ * ( t 1 ) ) ν 1 = Γ ( ν ) Γ ( ν σ ) ( ψ * ( t ) ψ * ( t 1 ) ) ν σ 1 ;
(3) 
C D t 1 + σ ; ψ * ( ψ * ( t ) ψ * ( t 1 ) ) k = 0 , ( k { 0 , , n 1 } ) and n N .

3. Main Results

First, we start the following key fixed-point theorem.
Theorem 1
([16,17]). Consider ı O of an ordered Banach space B and a nondecreasing mapping u : ı ı . If each sequence u ϱ n u ( ı ) converges whenever ϱ n is a monotone sequence in ı, then the sequence of the u -iteration of t 1 converges to the least fixed point ϱ * of  u , and the sequence of the u -iteration of t 2 converges to the greatest fixed point ϱ * of u . Moreover, ϱ * = min { t ı : t u t } , and  ϱ * = max { t ı : t u t } .
In fact, a function ϱ C ( ı , R ) is said to be a solution of Equation (3) if  ϱ satisfies the equation C D t 1 + σ ; ψ * ϱ ( t ) = V ( t , ϱ ( t ) ) , ( t ı ) and the condition ϱ ( 0 ) = λ I t 1 σ ; ψ * ϱ ( η ) + δ . Now, we prove the the next key lemma of a solution for problem (3).
Lemma 4.
Let y C ( ı , R ) and σ ( n 1 , n ] , ( n N ) ; the linear fractional initial value problem
C D t 1 σ ; ψ * ϱ ( t ) = y ( t ) , t ı , ϱ ( t 1 ) = λ I t 1 ν ; ψ * ϱ ( η ) + δ ,
has the following unique solution:
ϱ ( t ) = I t 1 σ ; ψ * y ( t ) + 1 Λ λ I t 1 σ + ν ; ψ * y ( η ) + δ = 1 Γ ( σ ) t 1 t ψ * ( ξ ) ( ψ * ( t ) ψ * ( ξ ) ) σ 1 y ( ξ ) d ξ + 1 Λ λ Γ ( σ ) t 1 η ψ * ( ξ ) ( ψ * ( η ) ψ * ( ξ ) ) σ 1 y ( η ) d ξ + δ ,
where Λ = 1 λ Γ ( ν + 1 ) ( ψ * ( η ) ψ * ( t 1 ) ) ν .
Proof. 
Assume that ϱ satisfies (9). Then, Lemma 2 implies that
ϱ ( t ) = I σ y ( t ) + c 1 .
The condition of problem (9) implies that ϱ ( 0 ) = c 1 and
I ν ϱ ( 0 ) = I σ + ν σ ( η ) + c 1 ( ψ * ( η ) ψ * ( t 1 ) ) ν Γ ( ν + 1 ) .
Thus,
c 1 1 λ Γ ( ν + 1 ) ( ψ * ( η ) ψ * ( t 1 ) ) ν = λ I σ + ν ; ψ * y ( η ) + δ .
Consequently,
c 1 = 1 Λ λ I σ + ν ; ψ * y ( η ) + δ .
Finally, we obtain the solution (10):
ϱ ( t ) = I t 1 σ ; ψ * y ( t ) + 1 Λ λ I t 1 σ + ν ; ψ * σ ( η ) + δ ,
which completes the proof.    □
Lemma 5
(Comparison result). Let ϱ C ( ı , R ) satisfy the following inequalities:
C D t 1 σ ; ψ * ϱ ( t ) 0 , t ı , ϱ ( 0 ) λ I ν ; ψ * ϱ ( η ) .
Then, ϱ ( t ) 0 , t ı , where 0 < σ 1 is fixed.
Proof. 
Lemma 4 implies that the problem (9) has the following unique solution:
ϱ ( t ) = I t 1 + σ ; ψ * ( y ( t ) + 1 Λ λ I t 1 σ + ν ; ψ * y ( η ) + δ .
Moreover, Lemma 5 follows from (13).    □
Definition 1.
A function ϱ ̲ 0 C ( ı , R ) and ϱ ¯ 0 C ( J , R ) is said to be a lower solution (l-solution) and upper solution (u-solution) of problem (3) if it satisfies
C D t 1 + σ ; ψ * ϱ ̲ 0 ( t ) V ( t , ϱ ̲ 0 ) , ϱ ̲ 0 ( 0 ) λ I ν ; ψ * ϱ ̲ 0 ( η ) + δ , C D t 1 σ ; ψ * ϱ ¯ 0 ( t ) V ( t , ϱ ¯ 0 ) , ϱ ¯ 0 ( 0 ) λ I ν ; ψ * ϱ ¯ 0 ( η ) + δ ,
t ı , respectively.
Theorem 2.
Consider the function V C ( ı × R , R ) and the following assumptions:
(H1)
ϱ ̲ 0 , ϱ ¯ 0 C ( ı , R ) such that ϱ ̲ 0 and ϱ ¯ 0 are the l-solution and u-solution of problem (3), respectively, with  ϱ ̲ 0 ( t ) ϱ ¯ 0 ( t ) , ( t ı ) ;
(H2)
∃ a function V C ( ı , R ) such that V ( t , ϱ ¯ ) V ( t , ϱ ̲ ) 0 , for  ϱ ̲ 0 ϱ ̲ ϱ ¯ ϱ ¯ 0 ;
(H3)
λ > 0 and λ ( ψ * ( η ) ψ * ( t 1 ) ) ν < Γ ( ν + 1 ) .
Then, there exist monotone iterative sequences ( m i s ) { ϱ ̲ n } and { ϱ ¯ n } that converge uniformly on the interval ı to the extremal solutions ϱ ̲ * , ϱ ¯ * [ ϱ ̲ 0 , ϱ ¯ 0 ] , respectively, of BVP (3), where
ϱ ̲ 0 ϱ ̲ 1 ϱ ̲ n ϱ ̲ * ϱ ¯ * ϱ ¯ n ϱ ¯ 1 ϱ ¯ 0 .
Proof. 
First, for any ϱ ̲ 0 ( t ) , ϱ ¯ 0 ( t ) C ( ı , R ) , we consider the BVPs of fractional order
C D t 1 σ ; ψ * ϱ ̲ n + 1 ( t ) = V ( t , ϱ ̲ n ( t ) ) , ϱ ̲ n + 1 ( 0 ) = λ I ν ; ψ * ϱ ̲ n ( η ) + δ ,
and
C D t 1 + σ ; ψ * ϱ ¯ n + 1 ( t ) = V ( t , ϱ ¯ n ( t ) ) , ϱ ¯ n + 1 ( 0 ) = λ I ν ; ψ * ϱ ¯ n ( η ) + δ ,
t ı . Now, Lemma 4 implies that (15) and (16) have the following unique solutions:
ϱ ̲ n + 1 ( t ) = I t 1 + σ ; ψ * V ( t , ϱ ̲ n ( t ) ) + 1 Λ λ I t 1 + σ + ν ; ψ * V ( η , ϱ ̲ n ( η ) ) + δ ,
and
ϱ ¯ n + 1 ( t ) = I t 1 + σ ; ψ * V ( t , ϱ ¯ n ( t ) ) + 1 Λ λ I t 1 + σ + ν ; ψ * V ( η , ϱ ¯ n ( η ) ) + δ ,
for t ı . Then, we structure the proof as follows. For any [ ϱ ̲ 0 , ϱ ¯ 0 ] , define an operator F with F ( ) = ϱ ̲ ( ) . As a first step, we show that the operator F : [ ϱ ̲ 0 , ϱ ¯ 0 ] [ ϱ ̲ 0 , ϱ ¯ 0 ] . Let ϱ ̲ 1 = F ϱ ̲ 0 , v 1 = F v 0 . Then, ϱ ̲ 1 , ϱ ¯ 1 are well defined and satisfy
c D t 1 + σ ; ψ * ϱ ̲ 1 ( t ) = V ( t , ϱ ̲ 0 ( t ) ) , t ı , ϱ ̲ 1 ( t 1 ) = λ I ν ; ψ * ϱ ̲ 0 ( η ) + δ ,
and
c D t 1 + σ ; ψ * ϱ ¯ 1 ( t ) = V ( t , ϱ ¯ 0 ( t ) ) , t ı , ϱ ¯ 1 ( t 1 ) = λ I ν ; ψ * ϱ ¯ 0 ( η ) + δ .
We set μ ̲ ( t ) = ϱ ̲ 1 ( t ) ϱ ̲ 0 ( t ) . From (15) and Definition 1, we get
c D t 1 + σ ; ψ * μ ̲ ( t ) 0 .
Again, since μ ̲ ( t 1 ) = λ I ν ; ψ * μ ̲ ( η ) , by Lemma 5, μ ̲ ( t ) 0 , ( t ı ) . That is,
ϱ ̲ 0 ( t ) F ϱ ̲ 0 ( t ) = ϱ ̲ 1 ( t ) .
Similarly, using the definition of the upper solution, we can show that ϱ ¯ 1 = F ϱ ¯ 0 ( t ) ϱ ¯ 0 ( t ) , ( t ı ) . Now, let μ ¯ ( t ) = ϱ ¯ 1 ( t ) ϱ ̲ 1 ( t ) . From (15), (16), and ( H 2 ) , we have
c D t 1 + σ ; ψ * μ ¯ ( t ) = V ( t , ϱ ¯ 0 ( t ) ) V ( t , ϱ ̲ 0 ( t ) ) 0 .
Therefore,
μ ¯ ( t 1 ) = ϱ ¯ 1 ( t 1 ) ϱ ̲ 1 ( t 1 ) = λ I ν ; ψ * ϱ ¯ ( η ) .
Moreover, μ ¯ ( t ) 0 from Lemma 5. Thus, F ϱ ̲ 0 F ϱ ¯ 0 . This, together with ϱ ̲ 0 F ϱ ̲ 0 and F ϱ ¯ 0 ϱ ¯ 0 , implies that F is nondecreasing,
F : [ ϱ ̲ 0 , ϱ ¯ 0 ] [ ϱ ̲ 0 , ϱ ¯ 0 ] ,
and ϱ ̲ 0 F ϱ ̲ ϱ ¯ 0 for any ϱ ̲ [ ϱ ̲ 0 , ϱ ¯ 0 ] . In consequence, F [ ϱ ̲ 0 , ϱ ¯ 0 ] [ ϱ ̲ 0 , ϱ ¯ 0 ] and
F ϱ ̲ max ϱ ̲ 0 , ϱ ¯ 0 : = d .
Let { ϱ ̲ n } be an m i s in [ ϱ ̲ 0 , ϱ ¯ 0 ] . Then, ϱ ̲ 0 F ϱ ̲ n ϱ ¯ 0 and F μ ̲ n d . For any ( t , ϱ ) ı × [ d , d ] , there exists a positive constant L 0 such that | V ( t , ϱ ) | L 0 . Then, for any t 1 , t 2 ı with t 1 t 2 , we obtain
F ϱ t F ϱ t ´ = | 1 Γ ( σ ) t 1 t ψ * ( ξ ) ψ * t ψ * ( ξ ) σ 1 V ξ , ϱ ( ξ ) d ξ 1 Γ ( σ ) t 1 t ´ ψ * ( ξ ) ψ * t ´ ψ * ( ξ ) σ 1 V ξ , ϱ ( ξ ) d ξ | 1 Γ ( σ ) | t 1 t ´ ψ * ( ξ ) [ ψ * t ψ * ( ξ ) σ 1 ψ * t ´ ψ * ( ξ ) σ 1 ] V ξ , ϱ ( ξ ) d ξ | + 1 Γ ( σ ) | t ´ t 1 ψ * ( ξ ) ψ * t ψ * ( ξ ) σ 1 V ξ , ϱ ( ξ ) d ξ | L 0 Γ ( σ + 1 ) | ψ * t ψ * ( t 1 ) σ ψ * t ´ ψ * ( t 1 ) σ ψ * t ψ * t ´ σ + ψ * t ψ * t ´ σ | ,
which converges to zero as t ´ t . Let us observe that for t , t ´ ȷ ,
F ϱ t F ϱ t ´ 0 ,
when t ´ t . Thus, F ϱ n is equicontinuous on all ȷ. So, F is relatively compact on [ ϱ ̲ 0 , ϱ ¯ 0 ] . Hence, the Arzelá–Ascoli theorem implies that F is compact on [ ϱ ̲ 0 , ϱ ¯ 0 ] , and so,
F ϱ ̲ n F ϱ ̲ 0 , ϱ ¯ 0 ,
converges. On the other hand, Theorem 1 implies that the sequence of the F -iteration of ϱ ̲ 0 and ϱ ¯ 0 converges to the least and the greatest fixed points ϱ ̲ * and ϱ ¯ * of F , respectively. This, in turn, implies that problem (3) has extremal solutions ϱ ̲ * , ϱ ¯ * [ ϱ ̲ 0 , ϱ ¯ 0 ] , which can be obtained with the corresponding iterative sequences ( ϱ ̲ n ) a n d ( ϱ ¯ n ) defined in (17) and (18), respectively. Furthermore, we have
ϱ ̲ 0 ϱ ̲ 1 ϱ ̲ n ϱ ̲ * ϱ ¯ * ϱ ¯ n ϱ ¯ 1 ϱ ¯ 0 .
This completes the proof.    □

4. Some Relevant Examples

Example 1.
Consider the following problem:
C D 0 + 1 4 , ψ * ϱ ( t ) = 2 t ϱ 2 ( t ) + 1 , t ı : = [ 0 , 1 ] , ϱ ( 0 ) = 3 4 I 0 + 1 2 ϱ ( 2 3 ) + 1 2 ,
where
σ = 1 4 ı , ν = 1 2 ( 0 , 1 ] , λ = 3 4 > 0 , η = 2 3 ( 0 , 1 ) , δ = 1 2 , t 1 = 0 , t 2 = 1 ,
and V : ı × R R is given by
V ( t , ϱ ) = 2 t ϱ 2 + 1 ,
for t ı , ϱ R . We take ϱ ̲ 0 ( t ) = 0 as the lower solution and ϱ ¯ 0 ( t ) = 1 + 2 t as the upper solution of problem (21), and we take ϱ ̲ 0 ϱ ¯ 0 for t ı . So, ( H 1 ) of Theorem 2 holds. Now, we consider three cases for ψ * :
ψ 1 * ( t ) = t , ψ 2 * ( t ) = 2 t , ψ 3 * ( t ) = t .
Note that ψ 1 * ( t ) = t and ψ 3 * ( t ) = t give the Caputo and Katugampola (for ρ = 0.5 ) derivatives in this example.
With the data provided in Table 1 and  Table 2, we can see from assumption ( H 3 ) that
λ Γ ( ν + 1 ) ( ψ * ( η ) ψ * ( a ) ) ν = 3 4 Γ 1 2 + 1 ψ * 2 3 ψ * ( 0 ) 1 2 = 3 4 Γ 3 2 2 3 1 2 0.690988 < 1 , ψ * ( t ) = t . 3 4 Γ 3 2 2 2 3 1 1 2 0.648610 < 1 , ψ * ( t ) = 2 t . 3 4 Γ 3 2 2 3 1 2 0.764704 < 1 , ψ * ( t ) = t .
Table 1 and Table 2 show these results. One can see the 2D line plots of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) in Figure 1a,b. In addition, assumption ( H 2 ) is clearly satisfied.
Thus, by Theorem 2, it follows that problem (21) has extremal solutions ϱ ̲ * , ϱ ¯ * [ 0 , 1 + 2 t ] , which can be found by means of the iterative sequences { ϱ ̲ n } and { ϱ ¯ n } defined by (17) and (18), respectively, as follows:
ϱ ̲ n + 1 ( t ) = I t 1 + σ ; ψ * V ( t , ϱ ̲ n ( t ) ) + 1 Λ λ I t 1 + σ + ν ; ψ * V ( η , ϱ ̲ n ( η ) ) + δ = I 0 + 1 4 ; ψ * 2 t ( ϱ ̲ n ( t ) ) 2 + 1 + 1 Λ 3 4 I t 1 + 3 4 ; ψ * 4 3 ( ϱ ̲ n ( η ) ) 2 + 1 + 1 2
and
ϱ ¯ n + 1 ( t ) = I t 1 + σ ; ψ * V ( t , ϱ ¯ n ( t ) ) + 1 Λ λ I t 1 + σ + ν ; ψ * V ( η , ϱ ¯ n ( η ) ) + δ = I 0 + 1 4 ; ψ * 2 t ( ϱ ¯ n ( t ) ) 2 + 1 + 1 Λ 3 4 I t 1 + 3 4 ; ψ * 4 3 ( ϱ ¯ n ( η ) ) 2 + 1 + 1 2
One can see the 2D line plots of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) in Figure 2a–c. Appendix A Algorithm A4 shows how to calculate ϱ ̲ n ( t ) and ϱ ¯ n ( t ) for t ı .
Example 2.
Consider the following problem:
C D 0 + 3 5 , ψ * ϱ ( t ) = 2 t ϱ 2 ( t ) + 1 , t ı : = [ 0.1 , 1.5 ] , ϱ ( 0 ) = 5 6 I 0 + 2 3 ϱ ( 3 7 ) + 4 5 ,
where
σ = 3 5 ( 0 , 1 ] , ν = 2 3 , λ = 5 6 , η = 6 7 ( 0 , 1 ) , δ = 9 11 , t 1 = 0.1 , t 2 = 1.5 ,
and V : ı × R R is given by
V ( t , ϱ ) = 0.6 t ϱ 2 + 8.5 ,
for t ı , ϱ R . We take ϱ ̲ 0 ( t ) = 0.1 as the l-solution and ϱ ¯ 0 ( t ) = 1.1 + t as the u-solution of problem (21), and we take ϱ ̲ 0 ϱ ¯ 0 for t ȷ . So, ( H 1 ) of Theorem 2 holds. Now, we consider three cases for ψ * :
ψ 1 * ( t ) = t , ψ 2 * ( t ) = 2 t , ψ 3 * ( t ) = t .
Note that ψ 1 * ( t ) = t and ψ 3 * ( t ) = t give the Caputo and Katugampola (for ρ = 0.5 ) derivatives in this example. These results are plotted in Figure 3a,b.
With the data provided, we can see from assumption ( H 3 ) that
λ Γ ( ν + 1 ) ( ψ * ( η ) ψ * ( t 1 ) ) ν = 5 6 Γ 2 3 + 1 ψ * 6 7 ψ * ( 0.1 ) 2 3 = 5 6 Γ 5 3 6 7 0.1 1 2 0.766841 < 1 , ψ * ( t ) = t . 3 4 Γ 3 2 2 2 3 1 1 2 0.755000 < 1 , ψ * ( t ) = 2 t . 3 4 Γ 3 2 2 3 1 2 0.663661 < 1 , ψ * ( t ) = t
Table 3 and Table 4 show these results. One can see the 2D line plots of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) in Figure 3a,b. Further, assumption ( H 2 ) is clearly satisfied. Thus, by Theorem 2, it follows that problem (22) has extremal solutions ϱ * , ϱ * [ 0.1 , 1.1 + t ] , which can be found by means of the iterative sequences { ϱ ̲ n } and { ϱ ¯ n } defined by (17) and (18), respectively, as follows:
ϱ ̲ n + 1 ( t ) = I t 1 + σ ; ψ * V ( t , ϱ ̲ n ( t ) ) + 1 Λ λ I t 1 + σ + ν ; ψ * V ( η , ϱ ̲ n ( η ) ) + δ = I t 1 + σ ; ψ * 2 t ( ϱ ̲ n ( t ) ) 2 + 1 + 1 Λ λ I t 1 + σ + ν ; ψ * 2 η ( ϱ ̲ n ( η ) ) 2 + 1 + δ
and
ϱ ̲ n + 1 ( t ) = I t 1 + σ ; ψ * V ( t , ϱ ¯ n ( t ) ) + 1 Λ λ I t 1 + σ + ν ; ψ * V ( η , ϱ ¯ n ( η ) ) + δ = I t 1 + σ ; ψ * 2 t ( ϱ ¯ n ( t ) ) 2 + 1 + 1 Λ λ I t 1 + σ + ν ; ψ * 2 η + ( ϱ ¯ n ( η ) ) 2 + 1 + δ .
One can see the 2D line plots of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) for the  ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , ψ 3 * ( t ) = t , and the Katugampola derivative (for ρ = 0.5 ) in Figure 3a,b. Appendix A Algorithm A4 shows how to calculate ϱ ̲ n ( t ) and ϱ ¯ n ( t ) for t ı .

5. Conclusions

In this study, we investigated the existence of solutions for a nonlinear FDE in the frame of the ψ Caputo derivative with integral boundary conditions. To prove the main theorems, the monotone iterative and the upper–lower solution techniques in the sense of the ψ Caputo fractional operator were used. Based on certain conditions, we constructed m i s that uniformly converged to the extremal solutions of BVP. The results were tested by constructing two equations corresponding to BVP (3). Different values for ψ , such as the ψ * ( t ) = t , Caputo, ψ * ( t ) = 2 t , ψ * ( t ) = t , and Katugampola (for ρ = 0.5 ) derivatives and the upper and lower solutions, were examined and illustrated for the purpose of verification. We conclude that the results reported in this paper are of great significance for the relevant audience and can be applied to different types of fractional differential problems.

Author Contributions

Conceptualization, A.B. and M.B.; methodology, J.A.; software, M.E.S.; validation, A.B., M.B. and M.E.S.; formal analysis, M.E.S.; investigation, A.B.; resources, M.B.; data curation, M.E.S.; writing—original draft preparation, A.B.; writing—review and editing, M.E.S.; visualization, M.E.S.; supervision, J.A.; project administration, J.A.; funding acquisition, J.A. All authors have read and agreed to the published version of the manuscript.

Funding

Not applicable.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

J. Alzabut is thankful to Prince Sultan University and OSTİM Technical University for their endless support.

Conflicts of Interest

The authors declare that they have no competing interests.

Appendix A. Supporting Informations

Algorithm A1 MATLAB lines for the calculation of I t 1 + σ ; ψ * ϱ ( t ) in Equation (4).
  1:  LSfractionalintegral
Require: t 1 , σ , ψ , ϱ , t
  2:  syms v e ;
  3:  E = i n t ( s u b s ( d i f f ( ψ , v ) , v , e ) ( e v a l ( s u b s ( ψ , v , t ) ) s u b s ( ψ , v , e ) ) ( σ 1 ) s u b s ( ϱ , v , e ) , t 1 , t ) ;
  4:  mathbbI = r o u n d ( 1 / γ ( σ ) e v a l ( E ) , 8 ) ;
  5:  return mathbbI
Algorithm A2 MATLAB lines for the calculation of D t 1 α ; ψ ( t ) in Equation (5).
  1:  LSfractionalderivative
Require t 1 , σ , ψ , ϱ , t
  2:  syms v e t ;
  3:   n = f l o o r ( α ) + 1 ;
  4:   E = i n t ( s u b s ( d i f f ( ψ , v ) , v , e ) ( s u b s ( ψ , v , t ) s u b s ( ψ , v , e ) ) ( n σ 1 ) s u b s ( v a r r h o , v , e ) , e , t 1 , t ) ;
  5:   F = d i f f ( E , t , n ) ;
  6:   F = ( 1 / s u b s ( d i f f ( ψ , v ) , v , t ) ) n F ;
  7:   F = r o u n d ( 1 / γ ( n σ ) , 8 ) F ;
  8:  mathbbD = F;
  9:  return mathbbD
Algorithm A3 MATLAB lines for the calculation of C D t 1 + σ ; ψ * ϱ ( t ) in Equation (6).
  1:  LSCaputofractionalderivative
Require: t 1 , σ , ψ , ϱ , t
  2:  syms v e ;
  3:   n = f l o o r ( σ ) + 1 ;
  4:  if f i x ( α ) = = σ then
  5:    F = e v a l ( s u b s ( d i f f ( w p , v , n ) , v , t ) ) ;
  6:    E = F ;
  7:   else
  8:    F = i n t ( s u b s ( d i f f ( ψ , v ) , v , e ) ( e v a l ( s u b s ( ψ , v , t ) ) s u b s ( ψ , v , e ) ) ( n σ 1 ) e v a l ( s u b s ( d i f f ( ϱ , v , n ) , v , e ) ) , t 1 , t ) ;
  9:    E = 1 / γ ( n σ ) F ;
  10:  end if
  11:  mathbbD = E;
  12:  return mathbbD
Algorithm A4 MATLAB lines for the calculation of u n ( t ) and v n ( t ) in Example 1.
Require: t 1 , σ , ψ , ϱ , t
  1:  syms v e ;
  2:  clear;
  3:  format long;
  4:  syms v e ϑ ;
  5:   α = 1 / 4 ; β = 1 / 2 ; λ = 3 / 4 ; η = 2 / 3 ; δ = 1 / 2 ;
  6:   a = 0 ; b = 1 ;
  7:   ψ = v ; = v ;
  8:   n = f l o o r ( α ) + 1 ;
  9:   Λ = 1 λ / γ ( β + 1 ) ( e v a l ( s u b s ( ψ , v , η ) ) ( e v a l ( s u b s ( ψ , v , a ) ) ) β
  10:   u 0 = 0 ; v 0 = 1 + 2 v ;
  11:   ψ = [ s y m ( v ) s y m ( 2 v ) s y m ( v ( 1 / 2 ) ) ] ;
  12:   h = 4 ; c = 1 ;
  13:  for i = 1 to 3 do
  14:    t = a ;
  15:    r = 1 ;
  16:    M a t r i x R e s u l t s ( r , c ) = r ;
  17:    M a t r i x R e s u l t s ( r , c + 1 ) = t ;
  18:    M a t r i x R e s u l t s ( r , c + 2 ) = r o u n d ( 1 λ / γ ( β + 1 ) ( e v a l ( s u b s ( ψ ( i ) , v , η ) ) e v a l ( s u b s ( ψ ( i ) , v , a ) ) ) β , 6 ) ;
  19:    M a t r i x R e s u l t s ( r , c + 3 ) = 1 0 + 2 t ;
  20:    M a t r i x R e s u l t s ( r , c + 4 ) = 1 0 + 2 e t a ;
  21:    M a t r i x R e s u l t s ( r , c + 5 ) = r o u n d ( a b s ( L S f r a c t i o n a l i n t e g r a l ( a , α , ψ ( i ) , M a t r i x R e s u l t s ( r , c + 3 ) , t ) + 1 / M a t r i x R e s u l t s ( r , c + 2 ) ( λ ( L S f r a c t i o n a l i n t e g r a l ( a , α + β ϋ ( i ) , M a t r i x R e s u l t s ( r , c + 4 ) , η ) ) + δ ) ) , 6 ) ;
  22:    M a t r i x R e s u l t s ( r , c + 6 ) = 1 ( 1 + 2 t ) + 2 t ;
  23:    M a t r i x R e s u l t s ( r , c + 7 ) = 1 ( 1 + 2 η ) + 2 η ;
  24:    M a t r i x R e s u l t s ( r , c + 8 ) = r o u n d ( a b s ( L S f r a c t i o n a l i n t e g r a l ( a , α , ψ ( i ) , M a t r i x R e s u l t s ( r , c + 3 ) , t ) + 1 / M a t r i x R e s u l t s ( r , c + 2 ) ( λ ( L S f r a c t i o n a l i n t e g r a l ( a , α + β , ψ ( i ) , M a t r i x R e s u l t s ( r , c + 4 ) , η ) ) + δ ) ) , 6 ) ;
  25:    t = t + 1 / 2 h ;
  26:    r = r + 1 ;
  27:   while ( t b ) do
  28:     M a t r i x R e s u l t s ( r , c ) = r ;
  29:     M a t r i x R e s u l t s ( r , c + 1 ) = t ;
  30:     M a t r i x R e s u l t s ( r , c + 2 ) = r o u n d ( 1 λ / γ ( β + 1 ) ( e v a l ( s u b s ( ψ ( i ) , v , η ) ) e v a l ( s u b s ( ψ ( i ) , v , a ) ) ) β , 6 ) ;
  31:     M a t r i x R e s u l t s ( r , c + 3 ) = 1 ( M a t r i x R e s u l t s ( r 1 , c + 3 ) ) 2 + 2 t ;
  32:     M a t r i x R e s u l t s ( r , c + 4 ) = 1 ( M a t r i x R e s u l t s ( r 1 , c + 3 ) ) 2 + 2 η ;
  33:     M a t r i x R e s u l t s ( r , c + 5 ) = r o u n d ( a b s ( L S f r a c t i o n a l i n t e g r a l ( a , α , ψ ( i ) , M a t r i x R e s u l t s ( r , c + 3 ) , t ) + 1 / M a t r i x R e s u l t s ( r , c + 2 ) ( λ ( L S f r a c t i o n a l i n t e g r a l ( a , α + β , ψ ( i ) , M a t r i x R e s u l t s ( r , c + 4 ) , η ) ) + δ ) ) , 6 ) ;
  34:     M a t r i x R e s u l t s ( r , c + 6 ) = 1 ( M a t r i x R e s u l t s ( r 1 , c + 6 ) ) 2 + 2 t ;
  35:     M a t r i x R e s u l t s ( r , c + 7 ) = 1 ( M a t r i x R e s u l t s ( r 1 , c + 7 ) ) 2 + 2 η ;
  36:     M a t r i x R e s u l t s ( r , c + 8 ) = r o u n d ( a b s ( L S f r a c t i o n a l i n t e g r a l ( a , α , ψ ( i ) , M a t r i x R e s u l t s ( r , c + 6 ) , t ) + 1 / M a t r i x R e s u l t s ( r , c + 2 ) ( λ ( L S f r a c t i o n a l i n t e g r a l ( a , α + β , ψ ( i ) , M a t r i x R e s u l t s ( r , c + 7 ) , η ) ) + δ ) ) , 6 ) ;
  37:     t = t + 1 / 2 h ;
  38:     r = r + 1 ;
  39:   end while
  40:    c = c + 9 ;
  41:  end for
  42:  return M a t r i x R e s u l t s

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Figure 1. Graphical representation of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) in (a) and (b) respectively for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) in Example 1.
Figure 1. Graphical representation of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) in (a) and (b) respectively for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) in Example 1.
Fractalfract 05 00194 g001
Figure 2. Graphical representation of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) in (a), (b) and (c) respectively for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) and t ( 0 , 0.07 ) in Example 1.
Figure 2. Graphical representation of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) in (a), (b) and (c) respectively for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) and t ( 0 , 0.07 ) in Example 1.
Fractalfract 05 00194 g002
Figure 3. Graphical representation of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) in (a) and (b) respectively for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) in Example 2.
Figure 3. Graphical representation of ϱ ̲ n ( t ) and ϱ ¯ n ( t ) in (a) and (b) respectively for the ψ 1 * ( t ) = t Caputo derivative, ψ 2 * ( t ) = 2 t , and the ψ 3 * ( t ) = t Katugampola derivative (for ρ = 0.5 ) in Example 2.
Fractalfract 05 00194 g003
Table 1. Numerical results of ϱ ̲ n for ψ * ( t ) = t , 2 t , t in Example 1.
Table 1. Numerical results of ϱ ̲ n for ψ * ( t ) = t , 2 t , t in Example 1.
ϱ ̲ n
n t ψ * ( t ) = t ψ * ( t ) = 2 t ψ * ( t ) = t
1 0.00000 6.16427 1.42292 9.07593
2 0.06250 4.28485 1.48618 6.19447
3 0.12500 6.94358 2.16988 10.07951
4 0.18750 3.08762 1.32280 4.40385
5 0.25000 7.27414 2.49829 10.38117
6 0.31250 1.44744 0.99029 2.03591
7 0.37500 6.79598 2.59341 9.54727
8 0.43750 1.96779 1.26042 2.73167
9 0.50000 7.91490 3.16083 10.95387
10 0.56250 3.00121 0.16361 4.18637
11 0.62500 0.40120 0.71785 0.62015
12 0.68750 6.91232 3.19814 9.34005
13 0.75000 1.12735 0.60722 1.66134
14 0.81250 6.93050 3.44249 9.21394
15 0.87500 2.52051 0.25975 3.59983
16 0.93750 5.59257 3.21189 7.26441
17 1.00000 1.08675 1.70043 1.16584
Table 2. Numerical results of ϱ ¯ n for ψ * ( t ) = t , 2 t , t in Example 1.
Table 2. Numerical results of ϱ ¯ n for ψ * ( t ) = t , 2 t , t in Example 1.
ϱ ¯ n
n t ψ * ( t ) = t ψ * ( t ) = 2 t ψ * ( t ) = t
1 0.00000 06.1643 01.4229 09.0759
2 0.06250 06.7849 01.9923 09.9536
3 0.12500 04.4538 01.4135 07.1562
4 0.18750 11.6960 02.3487 18.5273
5 0.25000 99.2723 01.1392 01.5203 × 10 2
6 0.31250 51.8545 × 10 2 02.5625 79.2912 × 10 2
7 0.37500 13.8157 × 10 6 01.0813 21.1237 × 10 6
8 0.43750 97.9661 × 10 12 02.7994 01.4979 × 10 14
9 0.50000 49.2583 × 10 26 03.4989 × 10 12 75.3138 × 10 26
10 0.56250 12.4534 × 10 54 88.4591 × 10 38 19.0406 × 10 54
11 0.62500 79.5978 × 10 108 05.6540 × 10 94 01.2170 × 10 110
12 0.68750 32.5184 × 10 218 02.3099 × 10 204 49.7193 × 10 218
13 0.75000 N a N N a N N a N
14 0.81250 N a N N a N N a N
15 0.87500 N a N N a N N a N
16 0.93750 N a N N a N N a N
17 1.00000 N a N N a N N a N
Table 3. Numerical results of ϱ ̲ n for ψ * ( t ) = t , 2 t , t in Example 2.
Table 3. Numerical results of ϱ ̲ n for ψ * ( t ) = t , 2 t , t in Example 2.
ϱ ̲ n
n t ψ * ( t ) = t ψ * ( t ) = 2 t ψ * ( t ) = t
1 0.10000 23.0887 21.4299 12.7468
2 0.22500 01.7027 × 10 2 01.3640 × 10 2 01.0319 × 10 2
3 0.35000 01.3185 × 10 4 99.6965 × 10 2 82.2118 × 10 2
4 0.47500 68.0783 × 10 6 49.0307 × 10 6 42.9176 × 10 6
5 0.60000 17.1314 × 10 14 11.8461 × 10 14 10.8451 × 10 14
6 0.72500 01.0361 × 10 30 69.1495 × 10 28 65.6348 × 10 28
7 0.85000 36.4361 × 10 58 23.5622 × 10 58 23.0527 × 10 58
8 0.97500 04.3535 × 10 118 02.7357 × 10 118 02.7475 × 10 118
9 1.10000 06.0253 × 10 236 03.6879 × 10 236 03.7901 × 10 236
10 1.22500 N a N N a N N a N
11 1.35000 N a N N a N N a N
12 1.47500 N a N N a N N a N
Table 4. Numerical results of ϱ ¯ n for ψ * ( t ) = t , 2 t , t in Example 2.
Table 4. Numerical results of ϱ ¯ n for ψ * ( t ) = t , 2 t , t in Example 2.
ϱ ¯ n
n t ψ * ( t ) = t ψ * ( t ) = 2 t ψ * ( t ) = t
1 0.10000 23.0887 21.4299 12.7468
2 0.22500 01.1374 × 10 2 90.2639 69.2844
3 0.35000 58.6017 × 10 2 43.0855 × 10 2 37.2431 × 10 2
4 0.47500 13.6661 × 10 6 09.1617 × 10 6 08.9616 × 10 6
5 0.60000 71.6666 × 10 12 41.3606 × 10 12 49.1158 × 10 12
6 0.72500 20.3287 × 10 26 08.4297 × 10 26 15.0160 × 10 26
7 0.85000 02.0382 × 10 54 35.0156 × 10 52 01.6593 × 10 54
8 0.97500 03.2721 × 10 108 06.0417 × 10 106 02.7695 × 10 108
9 1.10000 10.7866 × 10 216 17.9871 × 10 212 08.9489 × 10 216
10 1.22500 N a N N a N N a N
11 1.35000 N a N N a N N a N
12 1.47500 N a N N a N N a N
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Boutiara, A.; Benbachir, M.; Alzabut, J.; Samei, M.E. Monotone Iterative and Upper–Lower Solution Techniques for Solving the Nonlinear ψ−Caputo Fractional Boundary Value Problem. Fractal Fract. 2021, 5, 194. https://doi.org/10.3390/fractalfract5040194

AMA Style

Boutiara A, Benbachir M, Alzabut J, Samei ME. Monotone Iterative and Upper–Lower Solution Techniques for Solving the Nonlinear ψ−Caputo Fractional Boundary Value Problem. Fractal and Fractional. 2021; 5(4):194. https://doi.org/10.3390/fractalfract5040194

Chicago/Turabian Style

Boutiara, Abdelatif, Maamar Benbachir, Jehad Alzabut, and Mohammad Esmael Samei. 2021. "Monotone Iterative and Upper–Lower Solution Techniques for Solving the Nonlinear ψ−Caputo Fractional Boundary Value Problem" Fractal and Fractional 5, no. 4: 194. https://doi.org/10.3390/fractalfract5040194

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