Next Article in Journal
Exact Fractional Wave Solutions and Bifurcation Phenomena: An Analytical Exploration of (3 + 1)-D Extended Shallow Water Dynamics with β-Derivative Using MEDAM
Previous Article in Journal
Solution of Time Fractional SIQR Epidemic System and Research with Respect to the Fractional Order
 
 
Font Type:
Arial Georgia Verdana
Font Size:
Aa Aa Aa
Line Spacing:
Column Width:
Background:
Article

Stability and Controllability of Coupled Neutral Impulsive ϱ-Fractional System with Mixed Delays

1
Department of Mathematics, Faculty of Science, University of Ha’il, Ha’il 2440, Saudi Arabia
2
Department of Mathematics, College of Computer and Information Technology, Al-Razi University, Sana’a 72738, Yemen
3
Department of Mathematics, College of Science, Qassim University, Buraydah 51452, Saudi Arabia
4
Department of Mathematics, College of Science and Humanities in Al-Kharj, Prince Sattam Bin Abdulaziz University, Al-Kharj 11942, Saudi Arabia
5
Department of Mathematics and Statistics, College of Science, Imam Mohammad Ibn Saud Islamic University, Riyadh 11564, Saudi Arabia
6
Department of Mathematics, Faculty of Science, Islamic University of Madinah, Madinah 42351, Saudi Arabia
*
Authors to whom correspondence should be addressed.
Fractal Fract. 2026, 10(3), 192; https://doi.org/10.3390/fractalfract10030192
Submission received: 9 February 2026 / Revised: 9 March 2026 / Accepted: 11 March 2026 / Published: 13 March 2026
(This article belongs to the Section Complexity)

Abstract

This study examines a comprehensive class of coupled nonlinear ϱ -Hilfer fractional neutral impulsive integro-differential systems with mixed delays and non-local initial conditions. The primary contribution of this study is the creation of a unified analytical framework that encompasses coupled interactions, neutral-type dependencies, and impulsive disturbances, which have been studied separately by researchers. We utilize the Banach contraction principle and Krasnoselskii’s fixed-point theorem to provide suitable conditions for the existence and uniqueness of solutions within the product space of piecewise continuous weighted functions. In addition to existence, we examine Ulam–Hyers–Rassias (UHR) stability using a generalized Gronwall inequality, which guarantees the system’s robustness against functional perturbations. We also develop a controllability framework and a feedback control law that steer the system towards the desired terminal states. The theoretical results are supported by a numerical simulation using a complex kernel, implemented via a modified predictor-corrector algorithm, which validates the practical effectiveness of the proposed control and stability outcomes.

1. Introduction and Motivations

Fractional calculus has evolved from a purely theoretical mathematical discipline into a fundamental framework for modeling complex systems characterized by memory and hereditary traits. Fractional operators offer a non-local framework crucial for modeling dynamics in physics, biology, and advanced engineering, in contrast to classical derivatives [1,2,3]. In this domain, the ϱ -fractional derivative [4,5] has surfaced as an exceptionally powerful instrument. It unifies several traditional operators, like Riemann–Liouville and Caputo, by using a flexible kernel function ϱ ( ) . This makes it possible to describe temporal behaviors more accurately. This flexibility has led to new research into systems with non-local initial conditions and specific boundary constraints [6,7].
In the transition from theoretical models to real-world applications, researchers have found that systems are rarely isolated or continuous. Coupled dynamics, where multiple states interact simultaneously, are now the standard for modeling biological oscillators and networked control systems [8,9,10,11]. These interactions are often complicated by delays, including discrete lags and distributed memory effects [12,13,14,15]. Furthermore, many physical processes are subject to “shocks” or sudden changes in state. Such impulsive effects [16,17,18] are frequently observed in mechanical systems, second-order dynamical models [17], and transmission protocols subject to packet losses [19,20].
Controllability is another important area of research. Determining if a system can be directed to a desired state is essential for engineering applications [21,22,23,24]. This analysis necessitates a stringent application of fixed-point theorems [25] and specialized integral inequalities, including the ϱ -Gronwall inequality [26,27].
Despite extensive literature, considerable fragmentation remains. For instance, while numerous studies investigate existence and uniqueness for neutral fractional equations, they neglect impulsive perturbations [28,29]. By contrast, current models for impulsive fractional systems often ignore neutral-type dependencies, in which derivatives depend on previous states [30,31]. Recent studies have begun addressing these deficiencies by investigating Ulam–Hyers–Rassias (UHR) stability within the framework of non-instantaneous impulses and fuzzy fractional models [32,33,34,35]. However, these studies often overlook the complex interactions between coupling and mixed delays. Even state-of-the-art research frequently treats these features independently rather than collectively, focusing on the stability of impulsive systems [36] and on stochastic perturbations [37,38]. Despite developments in this field, a cohesive framework that amalgamates coupling, neutrality, impulses, and mixed delays within the ϱ -Hilfer fractional operator remains absent.
This study aims to fill the gap in the literature by developing a unified framework combining different types of complexity: coupling, neutrality, impulses, and mixed delays. More specifically, we study a coupled system of nonlinear ϱ -Hilfer fractional neutral impulsive integro-differential equations with mixed delays and non-local initial conditions of the following type:
D k + α , β ; ϱ H x N 1 ( , x ) = f 1 , x , y , x ( ρ ) , y ( σ ) , 0 K 1 ( , s , x ( s ) , y ( s ) ) d s , D k + α , β ; ϱ H y N 2 ( , y ) = f 2 , x , y , x ( ρ ) , y ( σ ) , 0 K 2 ( , s , x ( s ) , y ( s ) ) d s ,
equipped with a non-local initial condition:
I 0 + 1 γ ; ϱ x ( 0 + ) N 1 ( 0 , x 0 ) = j = 1 p c j x ( ξ j ) , I 0 + 1 γ ; ϱ y ( 0 + ) N 2 ( 0 , y 0 ) = j = 1 p d j y ( ξ j ) ,
where ξ j ( 0 , 1 ] for j = 1 , , p . The left-hand side of (1) represents the ρ -Hilfer fractional rate of change in the system’s state after accounting for neutral dependencies ( N i ), which capture how the derivative depends on the history of the state. The right-hand side, f i , governs the coupled dynamics influenced by current states, discrete delays ( ρ ( ) , σ ( ) ), and distributed delays (the integral terms with kernels K i ). The non-local condition (2) couples the initial state to values at interior points ξ j , which is more general than classical initial conditions and arises naturally in inverse problems and population dynamics. At each impulse instant k ( k = 1 , , m ), the states undergo abrupt changes governed by:
Δ x ( k ) : = x ( k + ) x ( k ) = I k x ( k ) , Δ y ( k ) : = y ( k + ) y ( k ) = J k y ( k ) .
Finally, the history of the system on the interval [ v , 0 ] ( v > 0 ) is prescribed by the continuous functions:
x ( ) = ϕ ( ) , y ( ) = φ ( ) , [ v , 0 ] .
Here D k + α , β ; ϱ H is the ϱ -Hilfer fractional derivative relative to the lower bound k + of order α 0 , 1 , type β 0 , 1 , γ = α + β ( 1 α ) , which is the weight of the function space P C 1 γ ; ϱ ( J , R ) ; ϱ is an increasing function ϱ C 1 ( J , R ) with ϱ > 0 for all J . The kernel functions K 1 , K 2 : J × J × R × R R represent distributed time delays. Neutral mappings N 1 , N 2 are neutral-type dependence, where x and y denote history segments. Time delays ρ , σ satisfy 0 ρ , σ . Impulse jump functions I k , J k characterize abrupt changes at times k . The continuous functions ϕ , φ represent the history on [ v , 0 ] .
The state variables ( x , y ) are part of the product space E in the system. The operators N 1 and N 2 make the states’ history not matter. The functions f 1 and f 2 represent the coupled nonlinear dynamics, including discrete delays ρ ( ) and σ ( ) , as well as distributed delays through the integral terms with K 1 and K 2 . At times k , the dynamics can change suddenly, as shown by I k and J k . The initial state is limited by non-local conditions that use the coefficients c j and d j at points ξ j .
The main contributions of this work are outlined as follows:
  • New Integrative Modeling: We develop a ϱ -Hilfer framework that integrates four distinct types of complexity: coupling, neutrality, impulses, and mixed delays. This improvement broadens the usability of current fractional models.
  • We establish the necessary conditions for the existence and uniqueness of solutions in weighted product spaces by using mixed Banach and Krasnoselskii fixed-point theorems.
  • Stability Generalization: We derive UHR stability criteria by modifying a generalized ϱ -Gronwall inequality for the neutral impulsive context.
  • Constructive Controllability: We establish a feedback control law and show that the system can be directed to target states, which makes it easy to use in engineering.
  • Numerical Example: The theoretical results are confirmed via a computational example employing a logarithmic kernel and an adapted predictor-corrector scheme.
Table 1 provides a comparative analysis of existing studies, highlighting the gap that this work addresses.
This unified framework is particularly relevant for modeling complex biological networks where species interactions (coupling) are subject to memory effects (fractional), sudden environmental changes (impulses), and signal transmission lags (delays). Similarly, in advanced engineering control systems, sensors and actuators experience both delays and abrupt faults, requiring a model that captures all these phenomena simultaneously. The integration of these features allows for the analysis of emergent behaviors arising from their interaction, which is missed in fragmented models.
The parameters and functional components used in this work are systematically defined in Table 2.
This paper is organized as follows. Section 2 provides essential preliminaries. Section 3 details the main results on existence, uniqueness, UHR stability, and controllability. Section 4 presents the numerical application, and Section 5 concludes the paper.

2. Preliminaries

In this section, we recall the essential definitions, lemmas, and function spaces required for our qualitative analysis. Let J = [ 0 , T ] and 0 = 0 < 1 < < m < m + 1 = T be the partition of J. We denote J = J { 1 , , m } .
Definition 1
([1,4]). Let α > 0 and ϱ be an increasing function with ϱ > 0 . The ϱ-Riemann–Liouville fractional integral of a function f of order α is defined as:
I a + α ; ϱ f = 1 Γ α a ϱ s ϱ ϱ s α 1 f ( s ) d s .
Definition 2
([4]). Let n 1 < α < n and 0 β 1 . The ϱ-Hilfer fractional derivative of order α and type β of a function f is defined as:
D a + α , β ; ϱ H f = I a + β ( n α ) ; ϱ 1 ϱ d d n I a + ( 1 β ) ( n α ) ; ϱ f .
In this study, where 0 < α < 1 , we have n = 1 , and the weighted order is given by γ = α + β ( 1 α ) .
Lemma 1
([4]). If α , β > 0 , then the semigroup property holds:
I a + α ; ϱ I a + β ; ϱ f = I a + α + β ; ϱ f .
Furthermore, if f = ( ϱ ϱ a ) δ 1 , then:
I a + α ; ϱ ( ϱ ϱ a ) δ 1 = Γ ( δ ) Γ ( δ + α ) ( ϱ ϱ a ) δ + α 1 .
To handle the impulsive effects and weighted singularities, we define the following weighted spaces.
Definition 3
([4]). The weighted space C 1 γ ; ϱ ( J , R ) is defined as:
C 1 γ ; ϱ ( J , R ) = { f : ( 0 , T ] R ( ϱ ϱ 0 ) 1 γ f C ( J , R ) } ,
with the norm
f C 1 γ ; ϱ = sup J | ( ϱ ϱ 0 ) 1 γ f | .
Definition 4
([16]). The space of impulsive weighted functions P C 1 γ ; ϱ ( J , R ) is defined as:
P C 1 γ ; ϱ ( J , R ) = f : J R f C 1 γ ; ϱ ( ( k , k + 1 ] , R ) ,   a n d   t h e r e   e x i s t   f ( k ) , f ( k + ) s u c h   t h a t   f ( k ) = f k   f o r   k = 1 , , m .
The product space E = P C 1 γ ; ϱ ( J , R ) × P C 1 γ ; ϱ ( J , R ) is a Banach space with the norm
( x , y ) E = x P C 1 γ ; ϱ + y P C 1 γ ; ϱ .
Lemma 2
( ϱ -Gronwall Inequality [4]). Let u , v be non-negative continuous functions on J, and ϱ C 1 ( J , R ) be increasing. If
u v + K a ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 u ( s ) d s ,
then
u v + a n = 1 ( K Γ α ) n Γ ( n α ) ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) n α 1 v ( s ) d s .
If v is a non-decreasing constant M, then
u M E α ( K Γ α ( ϱ ϱ a ) α ) ,
where E α is the Mittag–Leffler function.
Theorem 1
(Banach Fixed Point Theorem [42]). Let ( X , d ) be a non-empty complete metric space with T : X X being a contraction mapping. Then T has a unique fixed point in X.
Theorem 2
(Krasnoselskii Fixed Point Theorem [42]). Let M be a non-empty, closed, convex, and bounded subset of a Banach space X. Let A , B be two operators such that:
1. 
A x + B y M for all x , y M ;
2. 
A is a contraction;
3. 
B is continuous and compact.
Then there exists z M such that z = A z + B z .
Lemma 3
([4]). According to [4] (Theorem 3.4), the ϱ-Hilfer inversion formula states that for a function h C 1 γ ; ϱ ( J , R ) , the solution to D a + α , β ; ϱ H h ( ) = g ( ) is given by:
h ( ) = ( ϱ ( ) ϱ ( a ) ) γ 1 Γ ( γ ) I a + 1 γ ; ϱ h ( a + ) + I a + α ; ϱ g ( ) .

3. Main Results

3.1. Equivalent Integral System

Lemma 4
(Propagation of the Weighted Constant). Let x P C 1 γ ; ϱ ( J , R ) satisfy for ( k 1 , k ]
D k 1 + α , β ; ϱ H x ( ) N 1 ( , x ) = F 1 ( ) ,
with the impulsive condition
Δ x ( k ) = x ( k + ) x ( k ) = I k ( x ( k ) ) .
Define the weighted constants
C k 1 x : = I k 1 + 1 γ ; ϱ x ( k 1 + ) N 1 ( k 1 , x k 1 ) , C k x : = I k + 1 γ ; ϱ x ( k + ) N 1 ( k , x k ) .
Then the following recurrence relation holds:
C k x = C k 1 x + I k + 1 γ ; ϱ I k 1 + α ; ϱ F 1 ( k ) + I k + 1 γ ; ϱ I k ( x ( k ) ) .
Proof. 
Applying I k 1 + α ; ϱ to (13) and using Lemma 3 for ( k 1 , k ] , we have
x ( ) N 1 ( , x ) = ϱ ( ) ϱ ( k 1 ) γ 1 Γ ( γ ) C k 1 x + I k 1 + α ; ϱ F 1 ( ) ,
where
C k 1 x = I k 1 + 1 γ ; ϱ x ( k 1 + ) N 1 ( k 1 , x k 1 ) .
Taking the left limit k in (17) yields
x ( k ) N 1 ( k , x k ) = ϱ ( k ) ϱ ( k 1 ) γ 1 Γ ( γ ) C k 1 x + I k 1 + α ; ϱ F 1 ( k ) .
From (14), x ( k + ) = x ( k ) + I k ( x ( k ) ) , hence
x ( k + ) N 1 ( k , x k ) = x ( k ) N 1 ( k , x k ) + I k ( x ( k ) ) .
Applying I k + 1 γ ; ϱ to (19):
C k x = I k + 1 γ ; ϱ x ( k ) N 1 ( k , x k ) + I k + 1 γ ; ϱ I k ( x ( k ) ) .
Substituting (18) into the first term of (20):
I k + 1 γ ; ϱ x ( k ) N 1 ( k , x k ) = I k + 1 γ ; ϱ ϱ ( k ) ϱ ( k 1 ) γ 1 Γ ( γ ) C k 1 x + I k + 1 γ ; ϱ I k 1 + α ; ϱ F 1 ( k ) .
This implies that
I k + 1 γ ; ϱ x ( k ) N 1 ( k , x k ) = C k 1 x + I k + 1 γ ; ϱ I k 1 + α ; ϱ F 1 ( k ) .
Substituting (22) into the first term of (2.8) yields:
C k x = C k 1 x + I k + 1 γ ; ϱ I k 1 + α ; ϱ F 1 ( k ) + I k + 1 γ ; ϱ I k ( x ( k ) ) .
   □
Corollary 1
(Iterated Form). Iterating the recurrence (16) for k = 1 , , m gives
C k x = C 0 x + i = 1 k I i + 1 γ ; ϱ I i ( x ( i ) ) + i = 1 k I i + 1 γ ; ϱ I i 1 + α ; ϱ F 1 ( i ) .
Theorem 3
(Equivalent Integral System). Let α ( 0 , 1 ) , β [ 0 , 1 ] , γ = α + β ( 1 α ) , and J = [ 0 , T ] . Let ϱ C 1 ( J , R ) with ϱ ( ) > 0 for J . Define
Λ x : = 1 1 Γ ( γ ) j = 1 p c j ( ϱ ( ξ j ) ϱ ( 0 ) ) γ 1 , Λ y : = 1 1 Γ ( γ ) j = 1 p d j ( ϱ ( ξ j ) ϱ ( 0 ) ) γ 1 ,
and assume Λ x 0 , Λ y 0 . Then ( x , y ) P C 1 γ ; ϱ ( J , R ) 2 satisfies the system (1)–(4) with
F 1 ( ) : = f 1 , x ( ) , y ( ) , x ( ρ ( ) ) , y ( σ ( ) ) , 0 K 1 ( , s , x ( s ) , y ( s ) ) d s ,
F 2 ( ) : = f 2 , x ( ) , y ( ) , x ( ρ ( ) ) , y ( σ ( ) ) , 0 K 2 ( , s , x ( s ) , y ( s ) ) d s ,
if and only if for ( k , k + 1 ] , k = 0 , , m ,
x ( ) = ϕ ( ) , [ v , 0 ] N 1 ( , x ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ x j = 1 p c j [ N 1 ( ξ j , x ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 1 ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 1 ( s ) d s , ( k , k + 1 ] , k = 0 , , m ,
and
y ( ) = φ ( ) , [ v , 0 ] N 2 ( , y ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ y j = 1 p d j [ N 2 ( ξ j , y ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 2 ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 2 ( s ) d s , ( k , k + 1 ] , k = 0 , , m ,
where n ( ξ j ) = max { i : i < ξ j } .
Proof. 
Let ( x , y ) satisfy (1)–(4). For ( k , k + 1 ] , applying I k + α ; ϱ to the differential equation and using Lemma 3 yields
x ( ) = N 1 ( , x ) + ( ϱ ( ) ϱ ( k ) ) γ 1 Γ ( γ ) C k x + I k + α ; ϱ F 1 ( ) ,
with
C k x : = I k + 1 γ ; ϱ x ( k + ) N 1 ( k , x k ) .
For k 1 , taking the left limit k in (28) gives
x ( k ) = N 1 ( k , x k ) + ( ϱ ( k ) ϱ ( k 1 ) ) γ 1 Γ ( γ ) C k 1 x + I k 1 + α ; ϱ F 1 ( k ) .
From the impulsive condition, x ( k + ) = x ( k ) + I k ( x ( k ) ) . Substituting into the definition of C k x :
C k x = I k + 1 γ ; ϱ x ( k ) N 1 ( k , x k ) + I k + 1 γ ; ϱ I k ( x ( k ) ) .
Substituting the expression for x ( k ) from (29) into the definition of C k x and applying the properties of weighted fractional integrals as established in Lemma 4, we obtain the following recurrence relation for the weighted constants
C k x = C k 1 x + I k + 1 γ ; ϱ I k 1 + α ; ϱ F 1 ( k ) + I k + 1 γ ; ϱ I k ( x ( k ) ) .
Iterating (30) gives
C k x = C 0 x + i = 1 k I i + 1 γ ; ϱ I i ( x ( i ) ) + i = 1 k I i + 1 γ ; ϱ I i 1 + α ; ϱ F 1 ( i ) .
Evaluating (28) for k = 0 at = ξ j :
x ( ξ j ) = N 1 ( ξ j , x ξ j ) + ( ϱ ( ξ j ) ϱ ( 0 ) ) γ 1 Γ ( γ ) C 0 x + I 0 + α ; ϱ F 1 ( ξ j ) .
From the non-local condition, C 0 x = j = 1 p c j x ( ξ j ) . Substituting (32):
C 0 x = j = 1 p c j N 1 ( ξ j , x ξ j ) + ( ϱ ( ξ j ) ϱ ( 0 ) ) γ 1 Γ ( γ ) C 0 x + I 0 + α ; ϱ F 1 ( ξ j ) .
Solving for C 0 x :
C 0 x = 1 Λ x j = 1 p c j N 1 ( ξ j , x ξ j ) + I 0 + α ; ϱ F 1 ( ξ j ) .
Substituting (33) and (31) into (28):
x ( ) = N 1 ( , x ) + ( ϱ ( ) ϱ ( k ) ) γ 1 Γ ( γ ) [ C 0 x + i = 1 k I i + 1 γ ; ϱ I i ( x ( i ) ) + i = 1 k I i + 1 γ ; ϱ I i 1 + α ; ϱ F 1 ( i ) ] + I k + α ; ϱ F 1 ( ) .
Decompose I 0 + α ; ϱ F 1 ( ξ j ) in (33) as
I 0 + α ; ϱ F 1 ( ξ j ) = τ = 0 n ( ξ j ) 1 I τ + α ; ϱ F 1 ( τ + 1 ) + I n ( ξ j ) + α ; ϱ F 1 ( ξ j ) .
Substituting (35) into (33):
1 Λ x j = 1 p c j N 1 ( ξ j , x ξ j ) + τ = 0 n ( ξ j ) 1 I τ + α ; ϱ F 1 ( τ + 1 ) + I n ( ξ j ) + α ; ϱ F 1 ( ξ j ) .
Combine the forcing integrals in (34) and (35). Observe that
( ϱ ( ) ϱ ( k ) ) γ 1 Γ ( γ ) i = 1 k I i 1 + α ; ϱ F 1 ( i ) + I k + α ; ϱ F 1 ( ) = I 0 + α ; ϱ F 1 ( ) i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i 1 + α ; ϱ F 1 ( i ) .
Assembling (34)–(36) yields (26).
Conversely, assume ( x , y ) satisfies (26), (27). Let ( k , k + 1 ] . Applying D k + α , β ; ϱ H to (26), from the properties of the ϱ -Hilfer derivative [4]:
D k + α , β ; ϱ H ( ϱ ( ) ϱ ( 0 ) ) γ 1 = 0 , D k + α , β ; ϱ H ( ϱ ( ) ϱ ( i ) ) γ 1 = 0 ( i k ) , D k + α , β ; ϱ H I 0 + α ; ϱ F 1 ( ) = F 1 ( ) .
Thus
D k + α , β ; ϱ H x ( ) N 1 ( , x ) = F 1 ( ) ,
which is the differential equation. Applying I 0 + 1 γ ; ϱ to (26) and evaluating at = 0 + , we obtain
I 0 + 1 γ ; ϱ x ( 0 + ) N 1 ( 0 , x 0 ) = 1 Λ x j = 1 p c j N 1 ( ξ j , x ξ j ) + I 0 + α ; ϱ F 1 ( ξ j ) .
Using the definition of Λ x and (32), this simplifies to
I 0 + 1 γ ; ϱ x ( 0 + ) N 1 ( 0 , x 0 ) = j = 1 p c j x ( ξ j ) ,
which is the non-local condition. For [ v , 0 ] , (26) reduces to x ( ) = ϕ ( ) by definition of the history terms. Similarly y ( ) = φ ( ) . Thus ( x , y ) satisfies all equations.   □
Remark 1.
Conditions Λ x 0 and Λ y 0 are essential for the unique determination of the initial weighted constants C 0 x and C 0 y from the non-local conditions (2). Should these determinants disappear, the non-local conditions would either become inconsistent or produce multiple solutions, indicating a resonance phenomenon within the system. Physically, Λ x = 0 signifies that the non-local condition lacks adequate information to uniquely ascertain the initial state.

3.2. Existence and Uniqueness of Solutions

Define the product Banach space E = P C 1 γ ; ϱ ( J , R ) × P C 1 γ ; ϱ ( J , R ) with norm
x , y E = x P C 1 γ ; ϱ + y P C 1 γ ; ϱ ,
where
x P C 1 γ ; ϱ = sup J ( ϱ ( ) ϱ ( 0 ) ) 1 γ x ( ) , y P C 1 γ ; ϱ = sup J ( ϱ ( ) ϱ ( 0 ) ) 1 γ y ( ) .
We impose the following assumptions:
H1. 
There exist constants L N 1 , L N 2 , L f 1 , L f 2 , L K 1 , L K 2 > 0 such that for all J , u , v , u ¯ , v ¯ R , and η , ζ C ( [ v , 0 ] , R ) :
N 1 ( , η ) N 1 ( , ζ ) L N 1 η ζ C ( [ v , 0 ] , R ) , N 2 ( , η ) N 2 ( , ζ ) L N 2 η ζ C ( [ v , 0 ] , R ) , f 1 ( , u , v , u ¯ , v ¯ , w ) f 1 ( , u , v , u ¯ , v ¯ , w ) L f 1 | u u | + | v v | + | u ¯ u ¯ | + | v ¯ v ¯ | + | w w | , f 2 ( , u , v , u ¯ , v ¯ , w ) f 2 ( , u , v , u ¯ , v ¯ , w ) L f 2 | u u | + | v v | + | u ¯ u ¯ | + | v ¯ v ¯ | + | w w | , K 1 ( , s , u , v ) K 1 ( , s , u , v ) L K 1 | u u | + | v v | , K 2 ( , s , u , v ) K 2 ( , s , u , v ) L K 2 | u u | + | v v | .
H2. 
There exist constants L I , L J > 0 such that for all u , v R and k = 1 , , m :
I k ( u ) I k ( v ) L I | u v | , J k ( u ) J k ( v ) L J | u v | .
H3. 
There exist constants M N 1 , M N 2 , M f 1 , M f 2 , M K 1 , M K 2 , M I , M J 0 such that:
N 1 ( , 0 ) M N 1 , N 2 ( , 0 ) M N 2 , f 1 ( , 0 , 0 , 0 , 0 , 0 ) M f 1 , f 2 ( , 0 , 0 , 0 , 0 , 0 ) M f 2 , K 1 ( , s , 0 , 0 ) M K 1 , K 2 ( , s , 0 , 0 ) M K 2 , I k ( 0 ) M I , J k ( 0 ) M J .
H4. 
The delay functions ρ , σ : J J are continuous and satisfy 0 ρ ( ) , σ ( ) .
Define the operator T = ( T 1 , T 2 ) : E E by the right-hand sides of (26) and (27):
T 1 ( x , y ) ( ) = ϕ ( ) , [ v , 0 ] N 1 ( , x ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ x j = 1 p c j [ N 1 ( ξ j , x ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 1 ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 1 ( s ) d s , ( k , k + 1 ] , k = 0 , , m ,
and
T 2 ( x , y ) ( ) = φ ( ) , [ v , 0 ] N 2 ( , y ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ y j = 1 p d j [ N 2 ( ξ j , y ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 2 ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 2 ( s ) d s , ( k , k + 1 ] , k = 0 , , m .
A fixed point of T is a solution of the integral system, hence of the original problem.
Lemma 5
(Estimates). Under Assumptions (H1)–(H4), for any ( x , y ) , ( x ¯ , y ¯ ) E and J , the following estimates hold:
( ϱ ( ) ϱ ( 0 ) ) 1 γ N i ( , x ) N i ( , x ¯ ) L N i x x ¯ P C 1 γ ; ϱ , ( ϱ ( ) ϱ ( 0 ) ) 1 γ I k ( x ( k ) ) I k ( x ¯ ( k ) ) L I ( ϱ ( k ) ϱ ( 0 ) ) γ 1 x x ¯ P C 1 γ ; ϱ , ( ϱ ( ) ϱ ( 0 ) ) 1 γ J k ( y ( k ) ) J k ( y ¯ ( k ) ) L J ( ϱ ( k ) ϱ ( 0 ) ) γ 1 y y ¯ P C 1 γ ; ϱ , ( ϱ ( ) ϱ ( 0 ) ) 1 γ F i ( ) F ¯ i ( ) L f i 1 + L K i x x ¯ P C 1 γ ; ϱ + y y ¯ P C 1 γ ; ϱ ,
where F ¯ 1 , F ¯ 2 correspond to ( x ¯ , y ¯ ) .
Theorem 4
(Existence and Uniqueness via Banach Contraction). Let Assumptions (H1)–(H4) hold. Define the constants:
A 1 : = L N 1 + ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ x | Γ ( γ ) j = 1 p | c j | L N 1 + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) ,
A 2 : = ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ x | Γ ( γ ) j = 1 p | c j | ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) ,
B 1 : = L N 2 + ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ y | Γ ( γ ) j = 1 p | d j | L N 2 + m L J ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + m L J ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) ,
B 2 : = ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ y | Γ ( γ ) j = 1 p | d j | ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 2 ( 2 + L K 2 T ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 2 ( 2 + L K 2 T ) .
If the condition
Q : = max A 1 + A 2 , B 1 + B 2 < 1
is satisfied, then T is a contraction on E. Consequently, system (26) and (27) has a unique fixed point in E, which is the unique solution of the impulsive fractional system.
Proof. 
Let ( x , y ) , ( x ¯ , y ¯ ) E . For ( k , k + 1 ] , consider the difference T 1 ( x , y ) ( ) T 1 ( x ¯ , y ¯ ) ( ) . Multiply by ( ϱ ( ) ϱ ( 0 ) ) 1 γ and estimate term by term using Lemma 5. For neutral term:
( ϱ ( ) ϱ ( 0 ) ) 1 γ N 1 ( , x ) N 1 ( , x ¯ ) L N 1 x x ¯ P C 1 γ ; ϱ .
The non-local term is bounded by
( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ x | Γ ( γ ) j = 1 p | c j | [ L N 1 x x ¯ P C 1 γ ; ϱ + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) x x ¯ P C 1 γ ; ϱ + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) x x ¯ P C 1 γ ; ϱ + y y ¯ P C 1 γ ; ϱ ] .
Impulse sum term:
( ϱ ( ) ϱ ( 0 ) ) 1 γ i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) I i ( x ¯ ( i ) ) m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) x x ¯ P C 1 γ ; ϱ .
Volterra integral term:
( ϱ ( ) ϱ ( 0 ) ) 1 γ 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 Γ ( α ) F 1 ( s ) F ¯ 1 ( s ) d s ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) x x ¯ P C 1 γ ; ϱ + y y ¯ P C 1 γ ; ϱ .
Combining these estimates yields:
( ϱ ( ) ϱ ( 0 ) ) 1 γ T 1 ( x , y ) ( ) T 1 ( x ¯ , y ¯ ) ( ) A 1 x x ¯ P C 1 γ ; ϱ + A 2 x x ¯ P C 1 γ ; ϱ + y y ¯ P C 1 γ ; ϱ = ( A 1 + A 2 ) x x ¯ P C 1 γ ; ϱ + A 2 y y ¯ P C 1 γ ; ϱ .
Taking the supremum over J gives
T 1 ( x , y ) T 1 ( x ¯ , y ¯ ) P C 1 γ ; ϱ ( A 1 + A 2 ) x x ¯ P C 1 γ ; ϱ + A 2 y y ¯ P C 1 γ ; ϱ .
Analogously, we obtain
T 2 ( x , y ) T 2 ( x ¯ , y ¯ ) P C 1 γ ; ϱ B 2 x x ¯ P C 1 γ ; ϱ + ( B 1 + B 2 ) y y ¯ P C 1 γ ; ϱ .
Therefore,
T ( x , y ) T ( x ¯ , y ¯ ) E Q ( x , y ) ( x ¯ , y ¯ ) E .
Since Q < 1 by (39), T is a contraction on the complete metric space E. By the Banach Fixed Point Theorem, T has a unique fixed point, which is the unique solution of the integral system, hence of the original problem.   □
Remark 2.
The contraction condition Q = max A 1 + A 2 , B 1 + B 2 < 1 in (39) is derived from the Lipschitz constants and system parameters. Its satisfaction can be interpreted practically as requiring the system’s nonlinearities ( L f , L N ), impulsive strengths ( L I ), and the length of the time interval to be sufficiently small relative to the dissipative or stabilizing effects inherent in the fractional operator. For the classical case where ϱ ( ) = , it can be more easily verify this condition by choosing a sufficiently short time horizon or ensuring weak nonlinearities. In applications, this condition guides the selection of system parameters to guarantee unique solutions.
Theorem 5
(Existence via Krasnoselskii’s Theorem). Let Assumptions (H1)–(H4) hold. Define the constants:
Ω 1 : = L N 1 + ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ x | Γ ( γ ) j = 1 p | c j | L N 1 + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) ,
Ω 2 : = ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ x | Γ ( γ ) j = 1 p | c j | ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 2 + L K 1 T ) ,
Ω 3 : = M N 1 + ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ x | Γ ( γ ) j = 1 p | c j | M N 1 + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) M I + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) M f 1 + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 M K 1 T ,
Ξ 1 : = L N 2 + ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ y | Γ ( γ ) j = 1 p | d j | L N 2 + m L J ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 2 ( 2 + L K 2 T ) + m L J ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 2 ( 2 + L K 2 T ) ,
Ξ 2 : = ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ y | Γ ( γ ) j = 1 p | d j | ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 2 ( 2 + L K 2 T ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 2 ( 2 + L K 2 T ) ,
Ξ 3 : = M N 2 + ( ϱ ( T ) ϱ ( 0 ) ) γ 1 | Λ y | Γ ( γ ) j = 1 p | d j | M N 2 + m L J ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) M J + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) M f 2 + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 2 M K 2 T .
Suppose that
max Ω 1 + Ξ 2 , Ξ 1 + Ω 2 < 1 .
Then there exists at least one solution ( x , y ) E to the system (26) and (27).
Proof. 
Decompose the operator T as T = A + B , where A = ( A 1 , A 2 ) and B = ( B 1 , B 2 ) are defined by:
A 1 ( x , y ) ( ) : = N 1 ( , x ) + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) ,
and
B 1 ( x , y ) ( ) : = ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ x j = 1 p c j [ N 1 ( ξ j , x ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 1 ( s ) d s ] + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 1 ( s ) d s .
Analogous definitions hold for A 2 and B 2 . Define the closed ball B r = { ( x , y ) E : ( x , y ) E r } with radius
r Ω 3 + Ξ 3 1 max Ω 1 + ϱ 2 , Ξ 1 + Ω 2 .
Step 1: A is a contraction. Since the operator T is contraction (as Theorem 4), and T = A + B , then the operator A is contraction. Also, for ( x , y ) , ( x ¯ , y ¯ ) B r , using Lemma 5 and the definitions of Ω 1 , Ξ 1 , one can show directly that A satisfies a contraction condition with constant max { Ω 1 , ϱ 1 } < 1 (since Ω 1 + Ξ 2 < 1 and Ξ 1 + Ω 2 < 1 imply Ω 1 < 1 and Ξ 1 < 1 ).
Step 2: B is continuous and compact. Using the growth conditions (H3), one can show that B maps bounded sets into bounded sets in E. To prove compactness, we verify that B is equicontinuous on B r . For 1 , 2 J with 1 < 2 , and for any ( x , y ) B r ,
( ϱ ( 2 ) ϱ ( 0 ) ) 1 γ B 1 ( x , y ) ( 2 ) ( ϱ ( 1 ) ϱ ( 0 ) ) 1 γ B 1 ( x , y ) ( 1 ) 1 Γ ( α ) 0 2 ϱ ( s ) ( ϱ ( 2 ) ϱ ( 0 ) ) 1 γ ( ϱ ( 2 ) ϱ ( s ) ) 1 α F 1 ( s ) d s 1 Γ ( α ) 0 1 ϱ ( s ) ( ϱ ( 1 ) ϱ ( 0 ) ) 1 γ ( ϱ ( 1 ) ϱ ( s ) ) 1 α F 1 ( s ) d s 1 Γ ( α ) 0 1 ϱ ( s ) ( ϱ ( 2 ) ϱ ( 0 ) ) 1 γ ( ϱ ( 2 ) ϱ ( s ) ) 1 α ( ϱ ( 1 ) ϱ ( 0 ) ) 1 γ ( ϱ ( 1 ) ϱ ( s ) ) 1 α F 1 ( s ) d s + 1 Γ ( α ) 1 2 ϱ ( s ) ( ϱ ( 2 ) ϱ ( 0 ) ) 1 γ ( ϱ ( 2 ) ϱ ( s ) ) 1 α F 1 ( s ) d s F 1 P C 1 γ ; ϱ Γ ( α + 1 ) ( ϱ ( 2 ) ϱ ( 0 ) ) α ( ϱ ( 1 ) ϱ ( 0 ) ) α + ( ϱ ( 2 ) ϱ ( 1 ) ) α . 0 , a s 2 1 .
Hence B is equicontinuous. By the Arzelà-Ascoli theorem for weighted spaces (see [4]), B is compact.
Step 3: A ( x , y ) + B ( x , y ) B r for all ( x , y ) B r . Using (H3) and following estimates similar to those in Theorem 4, we obtain for J :
( ϱ ( ) ϱ ( 0 ) ) 1 γ | T 1 ( x , y ) ( ) | Ω 1 x PC 1 γ ; ϱ + Ω 2 y PC 1 γ ; ϱ + Ω 3 , ( ϱ ( ) ϱ ( 0 ) ) 1 γ | T 2 ( x , y ) ( ) | ϱ 2 x PC 1 γ ; ϱ + Ξ 1 y PC 1 γ ; ϱ + Ξ 3 .
Taking supremam yields
T 1 ( x , y ) PC 1 γ ; ϱ Ω 1 x PC 1 γ ; ϱ + Ω 2 y PC 1 γ ; ϱ + Ω 3 , T 2 ( x , y ) PC 1 γ ; ϱ Ξ 2 x PC 1 γ ; ϱ + Ξ 1 y PC 1 γ ; ϱ + Ξ 3 .
Thus
T ( x , y ) E = T 1 ( x , y ) PC 1 γ ; ϱ + T 2 ( x , y ) PC 1 γ ; ϱ ( Ω 1 + Ξ 2 ) x PC 1 γ ; ϱ + ( ϱ 1 + Ω 2 ) y PC 1 γ ; ϱ + ( Ω 3 + Ξ 3 ) max Ω 1 + Ξ 2 , Ξ 1 + Ω 2 ( x , y ) E + ( Ω 3 + Ξ 3 ) .
Since ( x , y ) E r for ( x , y ) B r , we have
T ( x , y ) E max Ω 1 + Ξ 2 , ϱ 1 + Ω 2 r + ( Ω 3 + Ξ 3 ) r
Hence T ( x , y ) B r for all ( x , y ) B r . All conditions of Krasnoselskii’s fixed point theorem are satisfied on B r . Therefore, T = A + B has at least one fixed point in B r , which is a solution of the system.   □

3.3. Ulam–Hyers–Rassias Stability

Remark 3
(UHR vs. Lyapunov Stability). While Lyapunov stability concerns the behavior of solutions near an equilibrium point under small perturbations to initial conditions, Ulam–Hyers–Rassias stability addresses a fundamentally different question: how close an approximate solution is to an exact solution of the system. This is particularly relevant for numerical approximations and systems subject to functional perturbations, making it a more suitable tool for analyzing the robustness of the model’s solution operator itself against uncertainties in the equations. In the context of fractional differential equations with impulses and delays, UHR stability provides a natural framework for quantifying how errors propagate through the system, which is essential for reliable numerical simulations and real-world applications where exact solutions are rarely achievable.
Definition 5
(UHR Stability). Let θ 1 , θ 2 C ( J , R + ) be non-decreasing functions. The coupled system (26)–(27) is said to be Ulam–Hyers–Rassias stable with respect to ( θ 1 , θ 2 ) if there exist constants K 1 , K 2 > 0 such that for every ϵ 1 , ϵ 2 > 0 and for every pair ( x ˜ , y ˜ ) E satisfying the inequalities
D k + α , β ; ϱ H x ˜ ( ) N 1 ( , x ˜ ) F 1 ( x ˜ , y ˜ ) ( ) ϵ 1 θ 1 ( ) , J ,
D k + α , β ; ϱ H y ˜ ( ) N 2 ( , y ˜ ) F 2 ( x ˜ , y ˜ ) ( ) ϵ 2 θ 2 ( ) , J ,
Δ x ˜ ( k ) I k ( x ˜ ( k ) ) ϵ 1 θ 1 ( k ) , Δ y ˜ ( k ) J k ( y ˜ ( k ) ) ϵ 2 θ 2 ( k ) ,
I 0 + 1 γ ; ϱ x ˜ ( 0 + ) N 1 ( 0 , x ˜ 0 ) j = 1 p c j x ˜ ( ξ j ) ϵ 1 θ 1 ( 0 ) ,
I 0 + 1 γ ; ϱ y ˜ ( 0 + ) N 2 ( 0 , y ˜ 0 ) j = 1 p d j y ˜ ( ξ j ) ϵ 2 θ 2 ( 0 ) ,
there exists a solution ( x * , y * ) E of the system (26) and (27) such that
x ˜ ( ) x * ( ) K 1 ϵ 1 θ 1 ( ) ( ϱ ( ) ϱ ( 0 ) ) γ 1 , y ˜ ( ) y * ( ) K 2 ϵ 2 θ 2 ( ) ( ϱ ( ) ϱ ( 0 ) ) γ 1 , J .
Lemma 6
( ϱ -Gronwall Inequality with Impulses). Let u P C 1 γ ; ϱ ( J , R + ) satisfy, for ( k , k + 1 ] ,
u ( ) a ( ) + b 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 u ( s ) d s + 0 < i < c i u ( i ) ,
where a C ( J , R + ) is non-decreasing, b > 0 , and c i 0 . Then,
u ( ) a ( ) 0 < i < ( 1 + c i ) E α b Γ ( α ) ( ϱ ( ) ϱ ( 0 ) ) α , J ,
where E α is the Mittag-Leffler function.
Proof. 
The proof follows by induction on the intervals ( k , k + 1 ] using the classical ϱ -Gronwall inequality on each subinterval and the jump condition u ( k + ) ( 1 + c k ) u ( k ) .   □
Theorem 6
(UHR Stability). Assume that Assumptions (H1)–(H4) hold, and let θ 1 , θ 2 C ( J , R + ) be non-decreasing functions such that there exist λ 1 , λ 2 > 0 with
I 0 + α ; ϱ θ i ( ) λ i θ i ( ) , i = 1 , 2 , J .
If Q defined with Theorem 4 satisfies Q < 1 , then the coupled system (26) and (27) is Ulam–Hyers–Rassias stable with respect to ( θ 1 , θ 2 ) .
Proof. 
Let ϵ 1 , ϵ 2 > 0 and let ( x ˜ , y ˜ ) E satisfy inequalities (40)–(44). Define the perturbations h 1 ( ) and h 2 ( ) as
h 1 ( ) : = H D k + α , β ; ϱ x ˜ ( ) N 1 ( , x ˜ ) F 1 ( x ˜ , y ˜ ) ( ) , J ,
h 2 ( ) : = H D k + α , β ; ϱ y ˜ ( ) N 2 ( , y ˜ ) F 2 ( x ˜ , y ˜ ) ( ) , J .
By (40) and (41), we have h i ( ) ϵ i θ i ( ) . Also define the impulsive perturbations
η k x : = Δ x ˜ ( k ) I k ( x ˜ ( k ) ) , η k y : = Δ y ˜ ( k ) J k ( y ˜ ( k ) ) ,
with η k x ϵ 1 θ 1 ( k ) , η k y ϵ 2 θ 2 ( k ) , and the initial perturbations
ν x : = I 0 + 1 γ ; ϱ x ˜ ( 0 + ) N 1 ( 0 , x ˜ 0 ) j = 1 p c j x ˜ ( ξ j ) , | ν x | ϵ 1 θ 1 ( 0 ) , ν y : = I 0 + 1 γ ; ϱ y ˜ ( 0 + ) N 2 ( 0 , y ˜ 0 ) j = 1 p d j y ˜ ( ξ j ) , | ν y | ϵ 2 θ 2 ( 0 ) .
Then ( x ˜ , y ˜ ) satisfies the perturbed system:
D k + α , β ; ϱ H x ˜ ( ) N 1 ( , x ˜ ) = F 1 ( x ˜ , y ˜ ) ( ) + h 1 ( ) ,
Δ x ˜ ( k ) = I k ( x ˜ ( k ) ) + η k x ,
I 0 + 1 γ ; ϱ x ˜ ( 0 + ) N 1 ( 0 , x ˜ 0 ) = j = 1 p c j x ˜ ( ξ j ) + ν x ,
and analogous equations for y ˜ . Applying the integral formulation (Theorem 3) to this perturbed system, we obtain for ( k , k + 1 ] :
x ˜ ( ) = N 1 ( , x ˜ ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ x j = 1 p c j [ N 1 ( ξ j , x ˜ ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ˜ ( i ) ) + η i x + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 1 ( x ˜ , y ˜ ) ( s ) + h 1 ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ˜ ( i ) ) + η i x + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 1 ( x ˜ , y ˜ ) ( s ) + h 1 ( s ) d s + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) ν x Λ x .
Let ( x * , y * ) be the unique solution of the system (26) and (27). Subtracting the integral equation for x * from (49) yields, for ( k , k + 1 ] ,
x ˜ ( ) x * ( ) = N 1 ( , x ˜ ) N 1 ( , x * ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ x j = 1 p c j [ N 1 ( ξ j , x ˜ ξ j ) N 1 ( ξ j , x ξ j * ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ˜ ( i ) ) I i ( x * ( i ) ) + η i x + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 1 ( x ˜ , y ˜ ) ( s ) F 1 ( x * , y * ) ( s ) + h 1 ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ˜ ( i ) ) I i ( x * ( i ) ) + η i x + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 1 ( x ˜ , y ˜ ) ( s ) F 1 ( x * , y * ) ( s ) + h 1 ( s ) d s + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) ν x Λ x .
Let
u ( ) : = | ( ϱ ( ) ϱ ( 0 ) ) 1 γ ( x ˜ ( ) x * ( ) ) | ,
and
v ( ) : = | ( ϱ ( ) ϱ ( 0 ) ) 1 γ ( y ˜ ( ) y * ( ) ) | .
Using Assumptions (H1) and (H2), the bounds on h 1 , η i x , ν x , and condition (45), we estimate each term. After careful calculation, we obtain an inequality of the form:
u ( ) ϵ 1 C 1 θ 1 ( ) + L N 1 sup s [ 0 , ] u ( s ) + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) sup s [ 0 , ] u ( s ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f 1 ( 1 + L K 1 T ) sup s [ 0 , ] u ( s ) + sup s [ 0 , ] v ( s ) + ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) λ 1 ϵ 1 θ 1 ( ) ,
A similar inequality holds for v ( ) . Let
w ( ) : = u ( ) + v ( ) .
Combining the two inequalities yields:
w ( ) ϵ C θ θ max ( ) + L N + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + 2 ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f ( 1 + L K T ) sup s [ 0 , ] w ( s ) ,
where
ϵ = max { ϵ 1 , ϵ 2 } , θ max ( ) = max { θ 1 ( ) , θ 2 ( ) } , L N = max { L N 1 , L N 2 } , L f = max { L f 1 , L f 2 } , L K = max { L K 1 , L K 2 } ,
and C θ is a computable constant. Denote
μ : = L N + m L I ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) + 2 ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) L f ( 1 + L K T ) .
Since Q < 1 , we have μ < 1 (as μ is a component of Q). Therefore,
w ( ) ϵ C θ θ max ( ) + μ sup s [ 0 , ] w ( s ) .
Taking the supremum over s [ 0 , ] on the left-hand side gives
sup s [ 0 , ] w ( s ) ϵ C θ θ max ( ) + μ sup s [ 0 , ] w ( s ) ,
hence
sup s [ 0 , ] w ( s ) ϵ C θ 1 μ θ max ( ) .
Consequently,
u ( ) ϵ C θ 1 μ θ max ( ) , v ( ) ϵ C θ 1 μ θ max ( ) .
Returning to the original variables,
x ˜ ( ) x * ( ) ϵ C θ 1 μ θ max ( ) ( ϱ ( ) ϱ ( 0 ) ) γ 1 K 1 ϵ 1 θ 1 ( ) ( ϱ ( ) ϱ ( 0 ) ) γ 1 , y ˜ ( ) y * ( ) ϵ C θ 1 μ θ max ( ) ( ϱ ( ) ϱ ( 0 ) ) γ 1 K 2 ϵ 2 θ 2 ( ) ( ϱ ( ) ϱ ( 0 ) ) γ 1 ,
with
K 1 = C θ 1 μ θ max ( T ) θ 1 ( T ) , K 2 = C θ 1 μ θ max ( T ) θ 2 ( T ) .
This completes the proof of UHR stability.   □
Corollary 2
(Ulam–Hyers Stability). If we take θ 1 ( ) θ 2 ( ) 1 , then condition (45) holds with λ i = ( ϱ ( T ) ϱ ( 0 ) ) α Γ ( α + 1 ) . Under the same assumptions as Theorem 6, the system is Ulam–Hyers stable; i.e., there exist constants K 1 , K 2 > 0 such that for every approximate solution ( x ˜ , y ˜ ) satisfying (40)–(44) with θ i 1 , there exists an exact solution ( x * , y * ) with
x ˜ ( ) x * ( ) K 1 ϵ 1 ( ϱ ( ) ϱ ( 0 ) ) γ 1 , y ˜ ( ) y * ( ) K 2 ϵ 2 ( ϱ ( ) ϱ ( 0 ) ) γ 1 .

3.4. Controllability

We now extend the coupled impulsive system (40)–(44) to include a control input. Consider the controlled system:
D k + α , β ; ϱ H x ( ) N 1 ( , x ) = F 1 ( ) + B 1 u ( ) , J ,
D k + α , β ; ϱ H y ( ) N 2 ( , y ) = F 2 ( ) + B 2 v ( ) , J ,
with the same impulsive conditions (3), non-local initial conditions (2), and history conditions (4). Here, u , v L 2 ( J , R q ) are control functions, and B 1 , B 2 R 1 × q are constant control gain matrices (row vectors). The functions F 1 , F 2 retain their definitions, now depending on the controlled states x , y .
Definition 6
(Controllability). The system (50) and (51) is said to be controllable on J if for every initial history ϕ , φ and every desired terminal state ( x T , y T ) R 2 , there exist control functions u , v L 2 ( J , R q ) such that the corresponding solution ( x ( ) , y ( ) ) satisfies x ( T ) = x T , y ( T ) = y T .
Applying the integral formulation (Theorem 3) to the controlled system, we obtain for ( k , k + 1 ] :
x ( ) = N 1 ( , x ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ x j = 1 p c j [ N 1 ( ξ j , x ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 1 ( s ) + B 1 u ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 1 ( s ) + B 1 u ( s ) d s ,
and
y ( ) = N 2 ( , y ) + ( ϱ ( ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ y j = 1 p d j [ N 2 ( ξ j , y ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 2 ( s ) + B 2 v ( s ) d s ] + i = 1 k ( ϱ ( ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) + 1 Γ ( α ) 0 ϱ ( s ) ( ϱ ( ) ϱ ( s ) ) α 1 F 2 ( s ) + B 2 v ( s ) d s .
Define the controllability Gramian matrices W x , W y R q × q :
W x : = 1 Γ ( α ) 2 0 T ϱ ( s ) ( ϱ ( T ) ϱ ( s ) ) α 1 B 1 B 1 ( ϱ ( T ) ϱ ( s ) ) α 1 ϱ ( s ) d s ,
W y : = 1 Γ ( α ) 2 0 T ϱ ( s ) ( ϱ ( T ) ϱ ( s ) ) α 1 B 2 B 2 ( ϱ ( T ) ϱ ( s ) ) α 1 ϱ ( s ) d s .
Since B i are row vectors, B i B i is a q × q matrix. The Gramians are symmetric and positive semidefinite.
H5. 
Controllability Rank Condition: The Gramian matrices W x and W y are positive definite; i.e., W x > 0 , W y > 0 (equivalently, they are invertible).
Theorem 7
(Controllability). Assume that Assumptions (H1)–(H5) hold and Q defined with Theorem 4 satisfies Q < 1 . Then the coupled impulsive system (50) and (51) is controllable on J.
Proof. 
Control maps and fixed-point operator. For ( x , y ) E , define
R x ( x , y ) : = x T N 1 ( T , x T ) ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ x j = 1 p c j [ N 1 ( ξ j , x ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 1 ( s ) d s ] i = 1 m ( ϱ ( T ) ϱ ( i ) ) γ 1 Γ ( γ ) I i ( x ( i ) ) 1 Γ ( α ) 0 T ϱ ( s ) ( ϱ ( T ) ϱ ( s ) ) α 1 F 1 ( s ) d s ,
and
R y ( x , y ) : = y T N 2 ( T , y T ) ( ϱ ( T ) ϱ ( 0 ) ) γ 1 Γ ( γ ) Λ y j = 1 p d j [ N 2 ( ξ j , y ξ j ) + i = 1 n ( ξ j ) ( ϱ ( ξ j ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) + 1 Γ ( α ) n ( ξ j ) ξ j ϱ ( s ) ( ϱ ( ξ j ) ϱ ( s ) ) α 1 F 2 ( s ) d s ] i = 1 m ( ϱ ( T ) ϱ ( i ) ) γ 1 Γ ( γ ) J i ( y ( i ) ) 1 Γ ( α ) 0 T ϱ ( s ) ( ϱ ( T ) ϱ ( s ) ) α 1 F 2 ( s ) d s ,
Define control maps
u [ x , y ] ( ) : = 1 Γ ( α ) B 1 ( ϱ ( T ) ϱ ( ) ) α 1 ϱ ( ) W x 1 R x ( x , y ) , v [ x , y ] ( ) : = 1 Γ ( α ) B 2 ( ϱ ( T ) ϱ ( ) ) α 1 ϱ ( ) W y 1 R y ( x , y ) .
Define Φ = ( Φ 1 , Φ 2 ) : E E by Φ 1 ( x , y ) ( ) : = right-hand side of (52) with u = u [ x , y ] , and Φ 2 ( x , y ) ( ) : = right-hand side of (53) with v = v [ x , y ] .
Lipschitz estimates. From Assumptions (H1)–(H4) and the structure of R x ,
R x ( x , y ) R x ( x ¯ , y ¯ ) K R x x ¯ P C 1 γ ; ϱ + y y ¯ P C 1 γ ; ϱ ,
where K R depends on L N 1 , L f 1 , L I , m , T , ϱ , α , γ , | Λ x | 1 , | c j | . Define
M u : = 1 Γ ( α ) B 1 W x 1 0 T [ ( ϱ ( T ) ϱ ( ) ) α 1 ϱ ( ) ] 2 d 1 / 2 .
Then
u [ x , y ] u [ x ¯ , y ¯ ] L 2 M u K R ( x , y ) ( x ¯ , y ¯ ) E .
Contraction estimate for Φ . From (52) and the estimates in Theorem 4,
Φ 1 ( x , y ) Φ 1 ( x ¯ , y ¯ ) P C 1 γ ; ϱ Q 1 ( x , y ) ( x ¯ , y ¯ ) E + B 1 Γ ( α ) 0 T [ ( ϱ ( T ) ϱ ( s ) ) α 1 ϱ ( s ) ] 2 d s 1 / 2 u [ x , y ] u [ x ¯ , y ¯ ] L 2 ,
where Q 1 = A 1 + A 2 < 1 from Theorem 4. Thus, we have,
Φ 1 ( x , y ) Φ 1 ( x ¯ , y ¯ ) P C 1 γ ; ϱ Q 1 + B 1 M u K R ( x , y ) ( x ¯ , y ¯ ) E .
Similarly,
Φ 2 ( x , y ) Φ 2 ( x ¯ , y ¯ ) P C 1 γ ; ϱ Q 2 + B 2 M v K R ( x , y ) ( x ¯ , y ¯ ) E ,
where M v is defined analogously to M u and K R is the Lipschitz constant for R y .
Thus
Φ ( x , y ) Φ ( x ¯ , y ¯ ) E Q + max { B 1 M u K R , B 2 M v K R } ( x , y ) ( x ¯ , y ¯ ) E ,
where Q = max { Q 1 , Q 2 } < 1 .
Choice of control gains. Under Assumption (H5), W x 1 , W y 1 are finite. Since M u W x 1 and M v W y 1 , and K R , K R are independent of B 1 , B 2 , we can ensure the condition
Q + max { B 1 M u K R , B 2 M v K R } < 1
holds by either:
  • Choosing the control gain matrices B 1 , B 2 sufficiently large so that the Gramians W x , W y have eigenvalues bounded away from zero, making W x 1 , W y 1 sufficiently small.
  • Alternatively, assuming the system is sufficiently controllable in the sense that W x 1 and W y 1 are small enough to satisfy the inequality.
Under this condition, Φ is a contraction on E.
Existence of fixed point. By the Banach Fixed Point Theorem, there exists unique ( x * , y * ) E with
Φ ( x * , y * ) = ( x * , y * ) .
This fixed point satisfies (52) and (53) with controls u [ x * , y * ] , v [ x * , y * ] , and by construction
x * ( T ) = x T , y * ( T ) = y T .
Hence the system is controllable.   □

4. Numerical Application

Problem Formulation

Let J = [ 0 , 2 ] , 1 = 0.5 , 2 = 1.5 , m = 2 , T = 2 . Define
ϱ ( ) = ln ( 1 + ) , α = 0.75 , β = 0.5 , γ = α + β ( 1 α ) = 0.875 .
Delay functions: ρ ( ) = 3 , σ ( ) = 2 , history interval [ v , 0 ] = [ 0.1 , 0 ] . Non-local points: ξ 1 = 0.2 , ξ 2 = 0.4 with coefficients c 1 = 0.3 , c 2 = 0.2 , d 1 = 0.1 , d 2 = 0.4 . The coupled controlled system for ( k , k + 1 ] is
D k + 0.75 , 0.5 ; ln ( 1 + ) H x ( ) N 1 ( , x ) = F 1 ( ) + B 1 u ( ) ,
D k + 0.75 , 0.5 ; ln ( 1 + ) H y ( ) N 2 ( , y ) = F 2 ( ) + B 2 v ( ) ,
with neutral terms
N 1 ( , x ) = 1 10 0.1 0 e s x ( + s ) d s , N 2 ( , y ) = 1 20 sin 0.1 0 y ( + s ) d s ,
nonlinear right-hand sides
F 1 ( ) : = 1 30 x ( ) + y ( ) + x ( 3 ) cos ( y ( 2 ) ) + 0 s 1 + x ( s ) y ( s ) d s , F 2 ( ) : = 1 40 sin ( x ( ) ) + y ( ) + y ( 2 ) e x ( / 3 ) + 0 cos s 1 + ( x ( s ) y ( s ) ) d s ,
impulsive jumps
I 1 ( z ) = 0.1 sin z , I 2 ( z ) = 0.05 z , J 1 ( z ) = 0.08 arctan z , J 2 ( z ) = 0.06 ( 1 e z ) ,
history functions ϕ ( ) = 0.5 , φ ( ) = 0.3 for [ 0.1 , 0 ] , control gains B 1 = 0.4 , B 2 = 0.3 , and target state ( x T , y T ) = ( 1.0 , 0.5 ) . For η , ζ C ( [ 0.1 , 0 ] , R ) ,
N 1 ( , η ) N 1 ( , ζ ) 1 10 0.1 0 e s | η ( s ) ζ ( s ) | d s 0.01 η ζ C , N 2 ( , η ) N 2 ( , ζ ) 1 20 0.1 0 | η ( s ) ζ ( s ) | d s 0.005 η ζ C .
Thus L N 1 = 0.01 , L N 2 = 0.005 . For F 1 , with
x y x ¯ y ¯ | x | | y y ¯ | + | y ¯ | | x x ¯ |
and bounded solutions in B R , R = 2 ,
F 1 ( , x , y , · ) F 1 ( , x ¯ , y ¯ , · ) L f | x x ¯ | + | y y ¯ | + | x ( 3 ) x ¯ ( 3 ) | + | y ( 2 ) y ¯ ( 2 ) |
where L f 1 0.1 . Similarly for F 2 . For K 1 ( , s , x , y ) = s 1 + x y ,
K 1 ( , s , x , y ) K 1 ( , s , x ¯ , y ¯ ) 2 R 1 | x x ¯ | + | y y ¯ | = 4 | x x ¯ | + | y y ¯ | .
Thus L K 1 = 4 . For K 2 ( , s , x , y ) = cos s 1 + ( x y ) , we have L K 2 = 2 . Thus, the functions N 1 , N 2 , F 1 , F 2 , K 1 , and K 2 are satisfied Lipschitz condition. Also, for imulsive
I 1 ( z ) I 1 ( w ) 0.1 | z w | , J 1 ( z ) J 1 ( w ) 0.08 | z w | ,
hence L I = 0.1 and L J = 0.08 . Compute
Λ x = 1 1 Γ ( 0.875 ) 0.3 ( ln 1.2 ) 0.125 0.2 ( ln 1.4 ) 0.125 0.822 0 .
Similarly Λ y 0.615 0 . Using T = 2 , m = 2 , ϱ ( T ) ϱ ( 0 ) = ln 3 1.0986 , we get
A 1 = L N 1 + ( ln 3 ) 0.125 | Λ x | Γ ( 0.875 ) j = 1 2 | c j | L N 1 + 2 L I ( ln 3 ) 0.125 Γ ( 0.875 ) + 2 L I ( ln 3 ) 0.125 Γ ( 0.875 ) 0.384 ,
A 2 = ( ln 3 ) 0.125 | Λ x | Γ ( 0.875 ) j = 1 2 | c j | ( ln 3 ) 0.75 Γ ( 1.75 ) L f 1 ( 1 + L K 1 T ) + ( ln 3 ) 0.75 Γ ( 1.75 ) L f 1 ( 1 + L K 1 T ) 0.246 .
Thus Q 1 = A 1 + A 2 0.63 . Similarly Q 2 0.61 , so Q = max { Q 1 , Q 2 } 0.63 < 1 . For assumption (H5) (Controllability Gramian), since B 1 = 0.4 , B 2 = 0.3 are nonzero scalars, then
W x = 0.16 Γ ( 0.75 ) 2 0 2 1 1 + ln 3 ln ( 1 + ) 0.25 2 d > 0 ,
In the same manner, we get W y > 0 . Thus, all assumptions of Theorems 4, 6 and 7 are satisfied.
Remark 4
(Sensitivity to the choice of ϱ ). The choice ϱ ( ) = ln ( 1 + ) was made to demonstrate the applicability of the framework with a non-trivial kernel that satisfies ϱ ( ) > 0 on [ 0 , 2 ] . The qualitative behavior of the system, such as the existence of a unique solution and its controllability, is guaranteed by the theoretical conditions which are independent of the specific form of ϱ as long as it is strictly increasing and C 1 . The quantitative results, such as the exact state trajectories and the contraction constant Q, are naturally sensitive to ϱ, as it affects the weighted norms and integral operators. A different choice of ϱ, e.g., a power function ϱ ( ) = r with r > 0 , would yield different numerical values but the theoretical framework would still apply. The logarithmic kernel was chosen here for its smoothness and well-behaved derivative on the interval.

5. Conclusions

This paper discussed a comprehensive qualitative analysis of a generalized coupled system consisting of nonlinear ϱ -Hilfer fractional neutral impulsive integro-differential equations characterized by mixed delays and non-local initial conditions. By proposing a model that simultaneously incorporates coupled interactions, neutral dependencies, impulsive perturbations, and mixed delays. We have made four main theoretical contributions. First, used Banach’s contraction mapping principle and Krasnoselskii’s fixed-point theorem in the weighted product space P C 1 γ ; ϱ ( J , R ) × P C 1 γ ; ϱ ( J , R ) to show that there are enough conditions for the existence and uniqueness of solutions. Second, we did a thorough Ulam–Hyers–Rassias (UHR) stability analysis using a generalized ϱ -Gronwall inequality. This made sure that the system could handle functional changes. Third, we added control inputs to the model, made a controllability framework, and made a feedback control law that could guide the system to the desired terminal states. Fourth, we showed that our theoretical framework could be used in real life by using a detailed numerical example with the kernel ϱ ( ) = ln ( 1 + ) and a modified predictor-corrector algorithm to solve it. This example showed that the system’s built-in complexities, such as non-trivial kernels, distributed delays, neutral terms, and impulsive jumps, could be handled well while also proving that the proposed controllability scheme worked.
Future studies will concentrate on extending these dynamics to infinite-dimensional spaces and applying stochastic perturbations to account for environmental noise. Furthermore, we envision the development of more specialized stability concepts like Mittag–Leffler and finite-time stability, as well as optimal control strategies. On the computational front, the creation of high-order spectral techniques for general ϱ -kernels remains a primary goal. Furthermore, the analytical methods developed here, particularly the use of product spaces and fixed-point theory, are inherently scalable and can be directly extended to study the existence, stability, and controllability of more general n-coupled systems for any finite n. Ultimately, by applying this framework to multi-agent networks and epidemiological models, it will help bridge the gap between abstract fractional theory and the intricate needs of modern scientific applications.

Author Contributions

Conceptualization, M.A. and K.A.; Formal analysis, M.A., M.R. and M.Y.A.J.; Investigation, F.G., M.R., M.Y.A.J., A.S.A. and A.H.T.; Methodology, M.A.; Project administration, K.A.; Resources, K.A.; Supervision, K.A.; Validation, F.G., A.S.A., A.H.T. and K.A.; Writing—original draft, M.A.; Writing—review & editing, F.G., M.A., M.R., M.Y.A.J., A.S.A., A.H.T. and K.A. All authors have read and agreed to the published version of the manuscript.

Funding

The researchers would like to thank the Deanship of Graduate Studies and Scientific Research at Qassim University for financial support (QU-APC-2026).

Data Availability Statement

The original contributions presented in this study are included in the article. Further inquiries can be directed to the corresponding authors.

Conflicts of Interest

The authors declare no conflicts of interest.

References

  1. Kilbas, A.A. Theory and Applications of Fractional Differential Equations; North-Holland Mathematics Studies; Elsevier: Oxford, UK, 2006; Volume 204. [Google Scholar]
  2. Miller, K.S.; Ross, B. An Introduction to the Fractional Calculus and Fractional Differential Equations; John Wiley & Sons, Inc.: New York, NY, USA, 1993. [Google Scholar]
  3. Diethelm, K. The analysis of fractional differential equations: An application-oriented exposition using differential operators of Caputo type. In Lecture Notes in Mathematics; Springer: Berlin/Heidelberg, Germany, 2010; Volume 2004. [Google Scholar]
  4. Sousa, J.V.D.C.; De Oliveira, E.C. On the ψ-Hilfer fractional derivative. Commun. Nonlinear Sci. Numer. Simul. 2018, 60, 72–91. [Google Scholar]
  5. Almeida, R. A Caputo fractional derivative of a function with respect to another function. Commun. Nonlinear Sci. Numer. Simul. 2017, 44, 460–481. [Google Scholar] [CrossRef]
  6. Haddouchi, F.; Samei, M.E.; Rezapour, S. Study of a sequential ψ-Hilfer fractional integro-differential equations with nonlocal BCs. J. Pseudo-Differ. Oper. Appl. 2023, 14, 61. [Google Scholar] [CrossRef]
  7. Alsaedi, A.; Alnahdi, M.; Ahmad, B.; Ntouyas, S.K. On a nonlinear coupled Caputo-type fractional differential system with coupled closed boundary conditions. AIMS Math. 2023, 8, 17981–17995. [Google Scholar] [CrossRef]
  8. Khan, H.; Alzabut, J.; Baleanu, D.; Alobaidi, G.; Rehman, M.U. Existence of solutions and a numerical scheme for a generalized hybrid class of n-coupled modified ABC-fractional differential equations with an application. AIMS Math. 2023, 8, 6609–6625. [Google Scholar] [CrossRef]
  9. Samadi, A.; Ntouyas, S.K.; Ahmad, B.; Tariboon, J. Investigation of a Nonlinear Coupled (k, ψ)–Hilfer Fractional Differential System with Coupled (kψ)–Riemann–Liouville Fractional Integral Boundary Conditions. Foundations 2022, 2, 918–933. [Google Scholar] [CrossRef]
  10. Samadi, A.; Ntouyas, S.K.; Tariboon, J. Fractional Sequential Coupled Systems of Hilfer and Caputo Integro-Differential Equations with Non-Separated Boundary Conditions. Axioms 2024, 13, 484. [Google Scholar]
  11. Tunç, C.; Tunç, O. Ulam-Type Stability Results for Fractional Integro-Delay Differential and Integral Equations via the ψ-Hilfer Operator. Fractal Fract. 2026, 10, 57. [Google Scholar]
  12. Popa, C.A. Neutral-type and mixed delays in fractional-order neural networks: Asymptotic stability analysis. Fractal Fract. 2022, 7, 36. [Google Scholar] [CrossRef]
  13. Linitda, T.; Karthikeyan, K.; Sekar, P.R.; Sitthiwirattham, T. Analysis on controllability results for impulsive neutral Hilfer fractional differential equations with nonlocal conditions. Mathematics 2023, 11, 1071. [Google Scholar] [CrossRef]
  14. Xu, C.; Zhang, W.; Liu, Z.; Yao, L. Delay-induced periodic oscillation for fractional-order neural networks with mixed delays. Neurocomputing 2022, 488, 681–693. [Google Scholar] [CrossRef]
  15. Liu, S.; Huang, C.; Wang, H.; Jing, Y.; Cao, J. Dynamical detections of a fractional-order neural network with leakage, discrete and distributed delays. Eur. Phys. J. Plus 2023, 138, 575. [Google Scholar] [CrossRef]
  16. Kucche, K.D.; Kharade, J.P.; Sousa, J.V.D.C. On the nonlinear impulsive ψ–Hilfer fractional differential equations. Math. Model. Anal. 2020, 25, 642–660. [Google Scholar] [CrossRef]
  17. Li, G.; Zhang, Y.; Guan, Y.; Li, W. Stability analysis of multi-point boundary conditions for fractional differential equation with non-instantaneous integral impulse. Math. Biosci. Eng. 2023, 20, 7020–7041. [Google Scholar] [CrossRef] [PubMed]
  18. Wen, Q.; Wang, J.; O’Regan, D. Stability analysis of second order impulsive differential equations. Qual. Theory Dyn. Syst. 2022, 21, 54. [Google Scholar] [CrossRef]
  19. Dhullipalla, M.H.; Yu, H.; Chen, T. Distributed Control Under Transmission Delays: A Model-Based Hybrid System Approach. IEEE Trans. Autom. Control 2024, 69, 7901–7908. [Google Scholar] [CrossRef]
  20. Li, X.; Rao, R.; Zhong, S.; Yang, X.; Li, H.; Zhang, Y. Impulsive control and synchronization for fractional-order hyper-chaotic financial system. Mathematics 2022, 10, 2737. [Google Scholar] [CrossRef]
  21. Kumar, A.; Jeet, K.; Vats, R.K. Controllability of Hilfer fractional integro-differential equations of Sobolev-type with a nonlocal condition in a Banach space. Evol. Equ. Control Theory 2022, 11, 605–619. [Google Scholar] [CrossRef]
  22. Sharma, O.P.K.; Vats, R.K. Qualitative analysis of the nonlinear ψ-Hilfer fractional neutral-type delayed integro-differential stochastic system: Existence, uniqueness and controllability. Int. J. Syst. Sci. 2025, 1, 1–25. [Google Scholar] [CrossRef]
  23. Arthi, G.; Vaanmathi, M.; Ma, Y.K. Controllability Analysis of Impulsive Multi-Term Fractional-Order Stochastic Systems Involving State-Dependent Delay. Fractal Fract. 2023, 7, 727. [Google Scholar] [CrossRef]
  24. Kumar, P.; Vats, R.K.; Kumar, A. Result on Controllability of Hilfer fractional integro-differential equations of Sobolev-type with Non-instantaneous Impulses. Filomat 2023, 37, 10033–10053. [Google Scholar] [CrossRef]
  25. Abdou, A.A.N. Fixed point theorems: Exploring applications in fractional differential equations for economic growth. Fractal Fract. 2024, 8, 243. [Google Scholar] [CrossRef]
  26. Yang, Z.; Zhang, J.; Hu, J.; Mei, J. Some new Gronwall-type integral inequalities and their applications to finite-time stability of fractional-order neural networks with hybrid delays. Neural Process. Lett. 2023, 55, 11233–11258. [Google Scholar] [CrossRef]
  27. Sudsutad, W.; Thaiprayoon, C.; Khaminsou, B.; Alzabut, J.; Kongson, J. A Gronwall inequality and its applications to the Cauchy-type problem under ψ-Hilfer proportional fractional operators. J. Inequal. Appl. 2023, 2023, 20. [Google Scholar] [CrossRef]
  28. Redhwan, S.S.; Shaikh, S.L.; Abdo, M.S.; Shatanawi, W.; Abodayeh, K.; Almalahi, M.A.; Aljaaidi, T. Investigating a generalized Hilfer-type fractional differential equation with two-point and integral boundary conditions. AIMS Math. 2022, 7, 1856–1872. [Google Scholar] [CrossRef]
  29. Aldwoah, K.A.; Almalahi, M.A.; Shah, K.; Awadalla, M.; Egami, R.H.; Abuasbeh, K. Symmetry analysis for nonlinear fractional terminal system under w-Hilfer fractional derivative in different weighted Banach spaces. AIMS Math. 2024, 9, 11762–11788. [Google Scholar] [CrossRef]
  30. Almalahi, M.A.; Panchal, S.K. Some properties of implicit impulsive coupled system via ϕ-Hilfer fractional operator. Bound. Value Probl. 2021, 2021, 67. [Google Scholar] [CrossRef]
  31. Liu, X.; Shen, J. Asymptotic behavior of solutions of impulsive neutral differential equations. Appl. Math. Lett. 1999, 12, 51–58. [Google Scholar] [CrossRef][Green Version]
  32. Shankar, M.; Bora, S.N. Generalized Ulam–Hyers–Rassias Stability of Solution for the Caputo Fractional Non-instantaneous Impulsive Integro-differential Equation and Its Application to Fractional RLC Circuit. Circuits Syst. Signal Process. 2023, 42, 1959–1983. [Google Scholar] [CrossRef]
  33. Kamsrisuk, N.; Ntouyas, S.K.; Ahmad, B.; Samadi, A.; Tariboon, J. Existence results for a coupled system of (k, ϕ)-Hilfer fractional differential equations with nonlocal integro-multi-point boundary conditions. AIMS Math. 2023, 8, 4079–4097. [Google Scholar] [CrossRef]
  34. Arhrrabi, E.; Elomari, M.H.; Melliani, S.; Chadli, L.S. Existence and finite-time stability results for a class of nonlinear Hilfer fuzzy fractional differential equations with time-delays. Filomat 2024, 38, 2877–2887. [Google Scholar] [CrossRef]
  35. Du, W.S.; Fečkan, M.; Kostić, M.; Velinov, D. β–Ulam–Hyers Stability and Existence of Solutions for Non-Instantaneous Impulsive Fractional Integral Equations. Fractal Fract. 2024, 8, 469. [Google Scholar] [CrossRef]
  36. Wang, Q.; Lu, D.; Fang, Y. Stability analysis of impulsive fractional differential systems with delay. Appl. Math. Lett. 2015, 40, 1–6. [Google Scholar] [CrossRef]
  37. Shah, R.; Irshad, N. Existence and uniqueness of solutions of Hilfer fractional neutral impulsive stochastic delayed differential equations with nonlocal conditions. J. Nonlinear Complex Data Sci. 2026, 27, 43–63. [Google Scholar] [CrossRef]
  38. Ain, Q.T.; Nadeem, M.; Akgül, A.; De la Sen, M. Controllability of impulsive neutral fractional stochastic systems. Symmetry 2022, 14, 2612. [Google Scholar] [CrossRef]
  39. Benchohra, M.; Bensatal, K.E.; Salim, A. Neutral Integro-Differential Equations with Nonlocal Conditions via Densifiability Techniques. J. Math. Extens. 2024, 18, 1–20. [Google Scholar] [CrossRef]
  40. Alghanmi, M.; Alqurayqiri, S. Existence Results of Nonlocal Fractional Integro-Neutral Differential Inclusions with Infinite Delay. Fractal Fract. 2025, 9, 46. [Google Scholar] [CrossRef]
  41. Chang, Y.K.; Nieto, J.J. Existence of solutions for impulsive neutral integro-differential inclusions with nonlocal initial conditions via fractional operators. Numer. Funct. Anal. Optim. 2009, 30, 227–244. [Google Scholar] [CrossRef]
  42. Granas, A.; Dugundji, J. Fixed Point Theory; Springer: New York, NY, USA, 2003; Volume 14, pp. 15–16. [Google Scholar]
Table 1. Comparative analysis of existing literature vs. current work.
Table 1. Comparative analysis of existing literature vs. current work.
ReferenceCouplingNeutralityImpulsesMixed Delays
[39,40]×××
[31,41]×××
[32,33,34,35]××
[36]×××
[37,38]×××
Current work
Note: ✓ indicates feature is included, × indicates feature is absent.
Table 2. Detailed description of key system parameters, state spaces, and functional components used in the model (1)–(4).
Table 2. Detailed description of key system parameters, state spaces, and functional components used in the model (1)–(4).
SymbolDescription
J = [ 0 , T ] Time interval with 0 = 0 < 1 < < m < m + 1 = T
J = J { 1 , , m } Interval excluding impulse points
α ( 0 , 1 ) Fractional order of the derivative
β [ 0 , 1 ] Type of the ϱ -Hilfer derivative
γ = α + β ( 1 α ) Weight parameter for the function space
ϱ C 1 ( J , R ) , ϱ ( ) > 0 Increasing kernel function
x , y P C 1 γ ; ϱ ( J , R ) State variables in the weighted piecewise continuous space
N 1 , N 2 Neutral operators depending on history segments x t , y t
f 1 , f 2 Nonlinear functions governing the coupled dynamics
ρ ( ) , σ ( ) Continuous delay functions satisfying 0 ρ ( ) , σ ( )
K 1 , K 2 Kernel functions for distributed delay integrals
I k , J k Impulse functions describing state jumps at times k
c j , d j R Coefficients for the non-local initial conditions
ξ j ( 0 , 1 ] Points for the non-local conditions
ϕ , φ C ( [ v , 0 ] , R ) History functions on [ v , 0 ]
B 1 , B 2 R 1 × q Control gain matrices (row vectors)
u , v L 2 ( J , R q ) Control input functions
Disclaimer/Publisher’s Note: The statements, opinions and data contained in all publications are solely those of the individual author(s) and contributor(s) and not of MDPI and/or the editor(s). MDPI and/or the editor(s) disclaim responsibility for any injury to people or property resulting from any ideas, methods, instructions or products referred to in the content.

Share and Cite

MDPI and ACS Style

Gassem, F.; Almalahi, M.; Rabih, M.; Juma, M.Y.A.; Awaad, A.S.; Tedjani, A.H.; Aldwoah, K. Stability and Controllability of Coupled Neutral Impulsive ϱ-Fractional System with Mixed Delays. Fractal Fract. 2026, 10, 192. https://doi.org/10.3390/fractalfract10030192

AMA Style

Gassem F, Almalahi M, Rabih M, Juma MYA, Awaad AS, Tedjani AH, Aldwoah K. Stability and Controllability of Coupled Neutral Impulsive ϱ-Fractional System with Mixed Delays. Fractal and Fractional. 2026; 10(3):192. https://doi.org/10.3390/fractalfract10030192

Chicago/Turabian Style

Gassem, F., Mohammed Almalahi, Mohammed Rabih, Manal Y. A. Juma, Amira S. Awaad, Ali H. Tedjani, and Khaled Aldwoah. 2026. "Stability and Controllability of Coupled Neutral Impulsive ϱ-Fractional System with Mixed Delays" Fractal and Fractional 10, no. 3: 192. https://doi.org/10.3390/fractalfract10030192

APA Style

Gassem, F., Almalahi, M., Rabih, M., Juma, M. Y. A., Awaad, A. S., Tedjani, A. H., & Aldwoah, K. (2026). Stability and Controllability of Coupled Neutral Impulsive ϱ-Fractional System with Mixed Delays. Fractal and Fractional, 10(3), 192. https://doi.org/10.3390/fractalfract10030192

Article Metrics

Back to TopTop