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Article

A Novel Event-Dependent Intermittent Control for Synchronization of Fractional-Order Coupled Neural Networks with Mixed Delays and Higher-Order Interactions

1
College of Computer Science, Inner Mongolia University, Hohhot 010021, China
2
School of Mathematical Sciences, Inner Mongolia University, Hohhot 010021, China
3
School of Mathematics and Statistics, Beijing Jiaotong University, Beijing 100044, China
4
School of Mathematical Sciences, Hebei Normal University, Shijiazhuang 050024, China
5
Department of Computer, Control and Management Engineering, Sapienza University of Rome, 00185 Roma, Italy
*
Authors to whom correspondence should be addressed.
Fractal Fract. 2025, 9(12), 824; https://doi.org/10.3390/fractalfract9120824
Submission received: 4 November 2025 / Revised: 12 December 2025 / Accepted: 15 December 2025 / Published: 17 December 2025
(This article belongs to the Special Issue Fractional Stochastic Process: Theory and Applications)

Abstract

This paper investigates the synchronization problem of fractional-order coupled neural networks (FOCNNs) featuring higher-order interactions and mixed delays under an event-dependent intermittent control framework. The proposed model incorporates higher-order interactions to more accurately capture the complex cooperative behaviors observed in real neural systems. To facilitate analysis, several novel theoretical tools are developed, which extend the existing framework of fractional-order control and provide upper bounds for the solutions of delayed fractional-order systems. Furthermore, a new event-dependent intermittent controller is designed, and sufficient synchronization criteria are rigorously derived. Finally, numerical simulations are presented to verify the effectiveness and robustness of the proposed control strategy.

1. Introduction

Coupled neural networks (CNNs), as a representative class of complex dynamical networks, have attracted considerable research attention over the past few decades. A CNN consists of numerous interconnected nodes, each describing an individual dynamic neural subsystem. Unlike conventional neural networks, CNNs not only exhibit the intrinsic dynamic properties of neural systems but also demonstrate richer and more complex behaviors arising from their topological structures and inter-node interactions. Owing to these characteristics, CNNs have been extensively applied in diverse fields such as signal processing, pattern recognition, and speech analysis [1,2,3]. Among the various dynamic behaviors of CNNs, synchronization stands out as a fundamental cooperative phenomenon in both natural and artificial systems, with significant practical implications for areas including power transmission, robotic coordination, and multi-agent collaboration [4,5,6].
Recent advances in the study of CNNs have motivated researchers to employ fractional calculus as a powerful mathematical tool for modeling their complex dynamical behavior [7,8,9]. Compared with traditional integer-order calculus, fractional calculus provides a more effective framework for characterizing the intricate features of complex systems, particularly those exhibiting memory effects and multi-time-scale dynamics [10,11,12]. Consequently, increasing attention has been devoted to the study of fractional-order coupled neural networks (FOCNNs). By introducing fractional-order operators into conventional CNNs, these networks inherit the memory-dependent properties of fractional calculus and exhibit a wider range of dynamic behaviors, such as bifurcation, chaos, and multistability [13,14]. Therefore, this work focuses on the synchronization analysis of fractional-order coupled neural networks.
In neuroscience, increasing evidence indicates that interactions among brain regions often arise from collective activity involving multiple nodes rather than simple pairwise connections. This motivates the study of higher-order interaction networks [15,16]. To capture such complex cooperative behaviors, researchers have developed models based on hypergraphs and simplicial complexes, which describe group-wise interactions and offer a richer representation of structural and functional relationships in neural systems [17,18]. Recent studies have further illustrated their significance: for instance, Mehrabbeik et al. [19] analyzed how higher-order coupling parameters affect the dynamics of memristive Rulkov neurons, while Farrera-Megchun et al. [20] investigated the impact of higher-order interactions in networks of Huber–Braun neurons. These advances show that higher-order interaction networks provide powerful tools for understanding complex neural dynamics, underscoring their theoretical and practical importance.
With the increasing demand for stability, efficiency, and energy optimization in modern engineering systems, intermittent control has attracted considerable attention as an effective control strategy [21,22,23]. By activating control inputs only during selected time intervals, intermittent control avoids continuous actuation, alleviates abrupt state variations, and significantly reduces energy consumption and operational costs. Over the past decade, its effectiveness has been widely demonstrated in various control systems. For instance, Sang [24] proposed an intermittent control scheme for the exponential synchronization of chaotic neural networks with actuator saturation, while Ding et al. [25] developed an event-dependent intermittent strategy for delayed discrete-time neural networks, with stability conditions derived via linear matrix inequalities.
Event-triggered or event-dependent control has become a major research trend in fractional-order systems. Xue et al. [26] proposed intermittent event-triggered control for complex networks and established new stability criteria. Hu et al. [27] further developed a fixed time event-dependent intermittent strategy for reaction-diffusion systems. More recently, event-dependent intermittent control has been extensively studied for large-scale networked systems due to its ability to further reduce communication burden and computational overhead [28,29]. unlike standard event-triggered methods, the proposed event-dependent intermittent control mechanism integrates event-triggering with intermittent actuation, ensuring that control updates occur only when necessary within active intervals. However, the presence of time delays, which are inevitable in neural signal transmission, may induce oscillations or even instability [30,31]. Compared with integer-order systems, fractional-order systems exhibit inherent memory effects, making delay-dependent control more challenging. To date, intermittent control for fractional-order systems with mixed delays remains insufficiently explored, which motivates the present study.
Existing synchronization studies on fractional-order neural networks have mainly focused on pairwise interactions or single-delay structures, leaving the combined effects of higher-order interactions and mixed delays largely unexplored. Moreover, most intermittent control strategies rely on pre-designed periodic schemes, which may lead to unnecessary control updates. To address these gaps, this work develops an event-dependent intermittent framework tailored to fractional-order systems with complex coupling structures.
1.
Higher-order interactions are incorporated into the FOCNN model, allowing a more accurate description of multi-neuronal coordination and overcoming the limitations of traditional pairwise interaction frameworks [24,25].
2.
A fractional Halanay inequality with an explicit solution upper bound is established, which extends existing results for single-delay systems and provides an effective tool for stability analysis of delayed fractional-order networks [30,32].
3.
An event-dependent intermittent control strategy is adopted, which relaxes the strict time constraints on control action and effectively handles the memory effect and mixed delays in fractional-order systems. Based on this scheme, synchronization criteria for FOCNNs are further derived [25,30,33].
Structure: The essential preliminaries and model descriptions are presented in Section 2. The synchronization criteria for FOCNNs are derived in Section 3. Two numerical simulations are conducted in Section 4 to validate the theoretical results. Finally, conclusions are summarized in Section 5.
Notations: The notations used in this paper are described as follows. N denotes the set of natural numbers; R represents the set of real numbers; R + stands for the set of positive real numbers; R q × p denotes the q × p -dimensional real space; I N is the N-dimensional identity matrix; diag { · } represents a diagonal matrix; L { f ( t ) } ( s ) denotes the Laplace transform of f ( t ) ; λ max ( A ) indicates the maximum eigenvalue of matrix A; C 1 ( [ t 0 , + ) ; R ) denotes the set of continuously differentiable functions defined on [ t 0 , + ) ; The symbol ⊗ denotes the Kronecker product.

2. Preliminaries and Model Description

2.1. Preliminaries

Definition 1
([34]). For a continuously differentiable function f ( t ) , the Caputo fractional derivative of order β ( 0 , 1 ) is defined as
D t β t 0 C f ( t ) = 1 Γ ( 1 β ) t 0 t f ˙ τ ( t τ ) β d τ ,
where t 0 0 denotes the initial time, f ˙ ( t ) represents the time derivative of f ( t ) , Γ ( · ) denotes the Gamma function.
Definition 2
([34]). With two parameters α > 0 , β > 0 , the Mittag-Leffler function is defined as
E α , β ( z ) = k = 0 + z k Γ ( α k + β ) ,
where z C . Denoting β = 1 , its one-parameter form is described as
E α ( z ) = E α , 1 ( z ) = k = 0 + z k Γ ( α k + 1 ) .
Especially, E 1 , 1 ( z ) = e z .
Lemma 1
([34]). Consider the fractional-order differential equation
D t β t 0 C h ( t ) = ξ h ( t ) , t t 0 ,
where h ( t ) is continuously differentiable, ξ R and β ( 0 , 1 ) . Then we have
h ( t ) = h ( t 0 ) E β ξ ( t t 0 ) β , t t 0 .
Lemma 2
([35]). Let m ( t ) C 1 ( [ t 0 , + ) , R ) and β ( 0 , 1 ) . If there exists t 1 > t 0 such that m t 1 = 0 and m ( t ) < 0 for t 0 t < t 1 , then D t β t 0 C m t 1 > 0 .
Lemma 3
([36]). Assume that Q ( s ) = L { q ( t ) } ( s ) . If all poles of Q ( s ) are in the open left-half complex plane, then lim t + q ( t ) = lim s 0 s Q ( s ) .
Lemma 4
([37]). Given any real matrices X, Y, positive definite matrix P with appropriate dimensions and a constant c > 0 , such that X T Y + Y T X c X T P X + c 1 Y T P 1 Y .
Lemma 5.
For the Mittag-Leffler function E β ρ ( t t 0 ) β with β ( 0 , 1 ) and ρ , τ 0 , then
lim t + 0 τ E β ρ t t 0 s β d s E β ρ t t 0 β = τ .
Proof. 
By the integral mean value theorem, for any t t 0 + τ , there exists ξ t [ 0 , τ ] such that
0 τ E β σ t t 0 s β d s = τ E β σ t t 0 ξ t β .
Subsequently, we can obtain
E β ρ ( t t 0 ξ t ) β E β σ t t 0 β E β ρ ( t t 0 τ ) β E β σ t t 0 β .
By applying the mean value theorem, there exists ξ ¯ t [ t τ , t ] satisfying
E β ρ ( t t 0 τ ) β E β σ t t 0 β = τ d E β ρ ( t t 0 ) β d t t = ξ ¯ t = τ ρ ( ξ ¯ t t 0 ) β 1 E β , β ρ ( ξ ¯ t t 0 ) β ,
where t t 0 + τ .
According to [34] and Lemma 3
lim t + ( t t 0 ) β 1 E β , β ρ ( t t 0 ) β = s lim s 0 L { ( t t 0 ) β 1 E β , β ρ ( t t 0 ) β } ( s ) = lim s 0 s s β + ρ = 0 .
Therefore, for any ε ( 0 , 1 ) , there exists t ˜ > t 0 such that
E β ρ ( t t 0 ) β E β ρ t t 0 τ β < ε
for t > t ˜ . Then, we obtain
lim t + E β ρ ( t t 0 ξ t ) β E β σ t t 0 β = 0 ,
which implies
lim t + 0 τ E β σ t t 0 s β d s E β ρ ( t t 0 ) β = lim t + τ E β ρ ( t t 0 ξ t ) β E β ρ ( t t 0 ) β = τ .
Lemma 6.
Assume that h ( t ) C 1 [ t 0 , + ) , R , h ( t ) < 0 for t [ t 0 τ , t 0 ] and
D t β t 0 C h ( t ) ξ h ( t ) + η 1 max 0 , h ( t τ ) + η 2 max 0 , t τ t h ( s ) d s ,
where t t 0 , τ 0 , 0 < β < 1 , ξ R , η 1 , η 2 0 . Then h ( t ) < 0 for t t 0 .
Proof. 
We claim that h ( t ) < 0 for t t 0 . If the claim is false, there must exist a time t ˜ > t 0 such that h ( s ) < 0 for s t 0 τ , t ˜ and h ( t ˜ ) = 0 . It follows from Lemma 2 that D t β t 0 C h ( t ˜ ) > 0 . However, from the condition (1), we obtain
D t β t 0 C h ( t ˜ ) ξ h ( t ˜ ) + η 1 max 0 , h ( t ˜ τ ) + η 2 max 0 , t ˜ τ t ˜ h ( s ) d s = 0 ,
which is a contradiction. Therefore, h ( t ) < 0 for t t 0 . □
Lemma 7.
Let h ( t ) C 1 [ t 0 , + ) , R be bounded on ( t 0 τ , t 0 ] , 0 < β < 1 and τ 0 . If ξ > η 1 + η 2 τ such that
D t β t 0 C h ( t ) ξ h ( t ) + η 1 h ( t τ ) + η 2 t τ t h ( s ) d s , t t 0 ,
where ξ, η 1 and η 2 are positive constants, then
h ( t ) κ E β σ t t 0 β ,
for t t 0 , where
κ = sup s [ τ , 0 ] h ( t 0 + s ) E β ( σ τ β ) ,
and σ > 0 is determined by
ξ = σ + η 1 sup t t 0 + τ E β σ ( t t 0 τ ) β E β σ ( t t 0 ) β + η 2 sup t t 0 + τ 0 τ E β σ ( t t 0 s ) β d s E β σ ( t t 0 ) β .
Proof. 
Define the continuous auxiliary function g ( σ ) as
g ( σ ) = σ + η 1 sup t t 0 + τ E β σ ( t t 0 τ ) β E β σ ( t t 0 ) β + η 2 sup t t 0 + τ 0 τ E β σ ( t t 0 s ) β d s E β σ ( t t 0 ) β .
By the monotonicity of the Mittag–Leffler function and Lemma 5, there exist positive constants M 1 and M 2 such that
E β σ ( t t 0 τ ) β E β σ ( t t 0 ) β ( 1 , M 1 ] ,
and
0 τ E β σ ( t t 0 s ) β d s E β σ ( t t 0 ) β ( τ , M 2 ] .
Consequently, it follows that
lim σ 0 + g ( σ ) < ξ , g ( ξ η 1 η 2 τ ) > ξ .
Therefore, there exists a constant
σ ( 0 , ξ η 1 η 2 τ )
such that g ( σ ) = ξ .
Then, define
H ( t ) = κ E β σ ( t t 0 ) β .
for t t 0 and H ( t ) = κ for t [ t 0 τ , t 0 ] . By the properties of the Mittag-Leffler function [34], we have
D t β t 0 C H ( t ) = D t β t 0 C κ E β σ t t 0 β = σ κ E β σ t t 0 β .
When t t 0 , t 0 + τ , derived from (4) and (6),
D t β t 0 C H ( t ) ξ η 1 η 2 τ κ E β σ t t 0 β ξ κ E β σ t t 0 β + η 1 κ E β σ τ β + η 2 κ τ ξ H ( t ) + η 1 h ( t τ ) + η 2 0 τ H ( t s ) d s ,
where κ = sup s τ , 0 h ( t 0 + s ) E β σ τ β and H ( t s ) κ .
For t t 0 + τ , we obtain the following by combining (4) and (6)
D t β t 0 C H ( t ) = ξ + η 1 sup t t 0 + τ E β σ t t 0 τ β E β σ t t 0 β + η 2 × sup t t 0 + τ 0 τ E β σ t t 0 s β d s E β σ t t 0 β κ E β σ t t 0 β ξ κ E β σ t t 0 β + η 1 κ E β σ t t 0 τ β + η 2 κ 0 τ E β σ t t 0 s β d s ξ H ( t ) + η 1 H ( t τ ) + η 2 0 τ H ( t s ) d s .
Thus, for t t 0 , it follows from (2), (7) and (8) that
D t β t 0 C H ( t ) λ H ( t ) + η 1 max 0 , H ( t τ ) + η 2 0 τ H ( t s ) d s ,
where H ( t ) = h ( t ) H ( t ) and H ( t ) < 0 for t [ t 0 τ , t 0 ] . By Lemma 6, we have H ( t ) 0 , which implies that h ( t ) H ( t ) for t t 0 . Consequently, inequation (3) holds. □
Remark 1.
The inequality ξ > η 1 + η 2 τ can be written explicitly as a constraint on the delay: 0 τ < ξ η 1 η 2 , provided that ξ > η 1 . If ξ η 1 , then no admissible delay τ exists. Hence, for fixed ξ, η 1 , and η 2 , the delay τ is bounded from above; if ξ is a tunable (design) parameter, increasing ξ allows larger admissible delays.
Remark 2.
Traditional fractional Halanay-type inequalities (e.g., [32,38]) usually provide only an asymptotic result such as lim t V ( t ) = 0 , which is adequate for studying global synchronization but insufficient for systems whose dynamics evolve in a piecewise manner. In the present work, the event-dependent control induces a sequence of switching intervals, and thus explicit upper bounds of the state norm on each interval are required. When applied to systems with mixed discrete and distributed delays, classical inequalities either fail to capture the interaction of the delay types or lead to overly conservative estimates. Lemma 7 overcomes these limitations by producing interval-wise upper bounds expressed via the Mittag–Leffler function, thereby enabling a refined analysis suited to the mixed-delay, piecewise dynamics considered in this paper.
Lemma 8.
Let h ( t ) C 1 [ t 0 , + ) , R be bounded on ( t 0 τ , t 0 ] If
D t β t 0 C h ( t ) ξ h ( t ) + η 1 h ( t τ ) + η 2 t τ t h ( s ) d s , t t 0 ,
where η 1 , η 2 > 0 and ξ η 1 + η 2 τ , then
h ( t ) < p t 0 E β ξ + η 1 + η 2 τ t t 0 β
for p t 0 > h t 0 and t t 0 , + .
Proof. 
Let p ( t ) be an auxiliary comparison function defined by
D t β t 0 C p ( t ) = ξ + η 1 + η 2 τ p ( t ) , t t 0 ,
with the initial condition
p ( s ) > h ( s ) , s t 0 τ , t 0 .
From Lemma 1 and Equation (10) that
p ( t ) = p t 0 E β ξ + η 1 + η 2 τ t t 0 β ,
which implies sup τ s 0 p t ˜ + s = p t ˜ for t t 0 + τ .
For t t 0 , we obtain the following by combining (9) and (10)
D t β t 0 C m ( t ) ξ m ( t ) + η 1 h ( t τ ) p ( t ) + η 2 t τ t h ( s ) p ( t ) d s ,
where m ( t ) = h ( t ) p ( t ) , and m ( s ) < 0 for s [ t 0 τ , t 0 ] .
Then, we claim that h ( t ) < p ( t ) for t t 0 . If the claim is false, there must exist a time t ˜ > t 0 such that h ( s ) p ( s ) < 0 for s t 0 τ , t ˜ and h ( t ˜ ) p ( t ˜ ) = 0 . It follows from Lemma 2 that D t β t 0 C m ( t ˜ ) > 0 . From (11), we have h ( t ˜ τ ) < p ( t ˜ τ ) p ( t ˜ ) and h ( s ) < p ( s ) p ( t ˜ ) for s [ t ˜ τ , t ˜ ] . Hence, we obtain
D t β t 0 C m ( t ˜ ) ξ m ( t ˜ ) + η 1 h ( t ˜ τ ) p ( t ˜ ) + η 2 t ˜ τ t ˜ h ( s ) p ( t ˜ ) d s < 0 ,
which leads to a contradiction. Therefore,
h ( t ) < p ( t ) = p ( t 0 ) E β ξ + η 1 + η 2 τ ( t t 0 ) β , t t 0 .
Remark 3.
The convergence of the system for ξ > η 1 + η 2 τ is established in Lemma 7, while an explicit upper bound of the solution for ξ η 1 + η 2 τ is derived in Lemma 8. These two lemmas together provide a complete analytical characterization of the system over the entire parameter range. Moreover, the proposed upper-bound estimation method is computationally feasible and offers a solid theoretical basis for subsequent controller design.

2.2. Model Description

The mathematical model for the controlled FOCNN with n nodes and s-dimensional interactions takes the following form
D t β t p C x i ( t ) = C x i ( t ) + D f x i ( t ) + B f x i ( t τ ) + A t τ t f x i ( s ) d s + m 1 j 1 = 1 n d i j 1 W 1 h 1 ( x i ( t ) , x j 1 ( t ) ) + m 2 j 1 = 1 n j 2 = 1 n d i j 1 j 2 W 2 h 2 ( x i ( t ) , x j 1 ( t ) , x j 2 ( t ) ) + + m s j 1 = 1 n j s = 1 n d i j 1 j s W s h s ( x i ( t ) , x j 1 ( t ) , , x j s ( t ) ) + I ( t ) + u i ( t ) ,
where t t p , t p + 1 , β ( 0 , 1 ) , x i ( t ) = ( x i 1 ( t ) , x i 2 ( t ) , …, x i N ( t ) ) T R N denotes the state vector of the node i and i { 1 , 2 , , n } , f · presents the activation function, C = diag ( c 1 , c 2 , , c N ) > 0 is the self-regulation matrix, D = d i j N × N , B = b i j N × N , A = a i j N × N are connection weight matrices, I ( t ) = ( I 1 ( t ) , I 2 ( t ) , …, I N ( t ) ) T denotes time-varying external input, u i ( t ) is control input, τ 0 represents the time delay with initial condition x i ( m ) = ψ i ( m ) for m t 0 , we suppose that sup l N t l + 1 t l = T ^ < + and inf l N t l + 1 t l   > T ˇ > 2 τ . For r { 1 , . . . , s } , the positive definite matrix W r R N × N denotes the internal coupling matrix. The coupling strengths h r : R N × ( r + 1 ) R N for r 1 , 2 , , s are nonlinear coupling functions of rth-dimension, satisfying h 1 ( x ) = h 2 ( x , x ) = = h s ( x , x , , x ) . If the r-dimensional simplex [ i , j 1 , , j r ] is connected in the simplicial complex, then d i j 1 j r = 1 holds for any permutation of the indices { i , j 1 , , j r } . Otherwise, d i j 1 j r = 0 . From [39], the r-th coupling function is governed by
h r ( x i ( t ) , x j 1 ( t ) , , x j r ( t ) ) = 1 r ( x j 1 ( t ) + x j 2 ( t ) + + x j r ( t ) r x i ( t ) ) .
The concept of the classical Laplacian matrix is extended in [40]. The Laplacian matrix L r = { l r , i j } n × n for r-order interactions can be defined as
l r , i j = l ¯ r , i j for i j , l ¯ r , i for i = j ,
where l ¯ r , i j = j 1 = 1 n j 2 = 1 n j r 1 = 1 n d i j j 1 j r 1 , l ¯ r , i = j 1 = 1 n j 2 = 1 n j s = 1 n d i j 1 j r .
Therefore, model (13) can be expressed as
D t β t p C x i ( t ) = C x i ( t ) + D f x i ( t ) + B f x i ( t τ ) + A t τ t f x i ( s ) d s + I ( t ) r = 1 s j = 1 n m r l r , i j W r x j ( t ) + u i ( t ) .
The isolated nodes of network (13) follow
D t β t p C y ( t ) = C y ( t ) + D f y ( t ) + B f y ( t τ ) + A t τ t f y ( s ) d s + I ( t ) ,
where t t p , t p + 1 , and y ( m ) = ψ ¯ ( m ) for m t 0 .
Define synchronization error as the e i ( t ) = x i ( t ) y ( t ) . Then, one yields
D t β t p C e i ( t ) = C e i ( t ) + D f x i ( t ) f y ( t ) + B f x i ( t τ ) f y ( t τ ) + A t τ t f x i ( s ) f y ( s ) d s r = 1 s j = 1 n m r l r , i j W r e j ( t ) + u i ( t ) .
Assumption 1.
There exists constant ξ > 0 such that
f ( x ) f ( y ) T f ( x ) f ( y ) ξ x y T x y ,
for x , y R N .

3. Main Result

The control objective is to ensure that all trajectories of system (13) asymptotically synchronize with the target dynamics (15), such that the system error satisfy lim t + e i ( t ) = 0 . To reduce energy consumption, we propose an energy-efficient intermittent control framework with the following
u i ( t ) = ρ ( t k ) Θ i e i ( t ) , t t k , t k + 1 ,
where Θ i > 0 is control gain. ρ ( t k ) = 1 if the control input is active and affects the system dynamics for t t k , t k + 1 , and ρ ( t k ) = 0 if there is no control input for t t k , t k + 1 . To establish the triggering sequence t p , p N , we define a decaying threshold function G : R R + with the asymptotic property lim t G ( t ) = 0 . The event times are then determined iteratively by
ρ ( t k ) = 1 if e ( t k ) 2 G ( t k ) , 0 if e ( t k ) 2 < G ( t k ) .
Remark 4.
Event-dependent intermittent control regulates the controller’s active and rest states through dynamic triggering mechanisms (e.g., state thresholds). In contrast to traditional periodic intermittent controllers [21,33], our proposed control scheme (17) incorporates an event-triggered mechanism that flexibly adjusts the controller’s working and resting states based on actual demands. This approach enables the control strategy to better align with the system’s real-time operational requirements, significantly enhancing control adaptability and precision.
Theorem 1.
Under Assumption 1, the system (13) can achieve synchronization under the controller (17) if
2 Θ i > ω ,
where ν i > 0 , and
ω = λ max ν 1 DD T + ν 2 BB T + ν 3 τ AA T 2 C r = 1 s m r λ min L r W r + ν 1 1 + ν 2 1 + ν 3 1 τ ξ .
Proof. 
Construct the Lyapunov function candidate V ( t ) = e ( t ) 2 . Further, it can be computed that
D t β t k C V ( t ) i = 1 n 2 e i T ( t ) A t τ t f x i ( s ) f y ( s ) d s C e i ( t ) + D f x i ( t ) f y ( t ) + B f x i ( t τ ) f y ( t τ ) r = 1 s j = 1 n m r l r , i j W r e j ( t ) ρ ( t k ) Θ i e i ( t ) ,
where t t k , t k + 1 . By Lemma 4 and Assumption 1, the following inequalities hold:
2 i = 1 n e i T ( t ) D f x i ( t ) f y ( t ) ν 1 i = 1 n e i T ( t ) DD T e i ( t ) + ν 1 1 ξ i = 1 n e i T ( t ) e i ( t ) , 2 i = 1 n e i T ( t ) B f x i ( t τ ) f y ( t τ ) ν 2 i = 1 n e i T ( t ) BB T e i ( t ) + ν 2 1 ξ i = 1 n e i T ( t τ ) e i ( t τ ) , 2 i = 1 n e i T ( t ) A t τ t f x i ( s ) f y ( s ) d s ν 3 τ i = 1 n e i T ( t ) AA T e i ( t ) + ν 3 1 ξ i = 1 n t τ t e i T ( s ) e i ( s ) d s .
It can be deduced that
i = 1 n j = 1 n e i T ( t ) m r l r , i j W r e j ( t ) = m r e T ( t ) L r W r e ( t ) ,
where e T ( t ) = ( e 1 T ( t ) , e 2 T ( t ) , …, e n T ( t ) ) T . Hence, we can derive
D t β t k C V ( t ) i = 1 n e i T ( t ) 2 C + ν 1 DD T + ν 2 BB T + ν 3 τ AA T + ν 1 1 ξ I N 2 ρ ( t k ) Θ i I N × e i ( t ) r = 1 s m r e T ( t ) L r W r e ( t ) + ν 2 1 ξ i = 1 n e i T ( t τ ) e i ( t τ ) + ν 3 1 ξ i = 1 n t τ t e i T ( s ) e i ( s ) ds ,
where t t k , t k + 1 . Next, the system behavior is analyzed under varying threshold function configurations.
If ρ ( t k ) = 1 for t t k , t k + 1 , from (18), we have
D t β t k C V ( t ) η V ( t ) + ν 2 1 ξ V ( t τ ) + ν 3 1 ξ t τ t V ( s ) d s ,
where η = 2 Θ i λ max ν 1 DD T + ν 2 BB T + ν 3 τ AA T 2 C r = 1 s m r λ min L r W r + ν 1 1 ξ . Applying the fractional-order Halanay-type inequality given in Lemma 7, we derive that
V ( t ) sup s τ , 0 V ( t k + s ) E β σ τ β E β σ t t k β ,
where σ 0 , η ν 2 1 ξ ν 3 1 ξ .
If ρ ( t k ) = 0 for t t k , t k + 1 . From (18) we can obtain V ( t k ) < G ( t k ) and
D t β t k C V ( t ) 2 Θ i η V ( t ) + ν 2 1 ξ V ( t τ ) + ν 3 1 ξ t τ t V ( s ) d s .
Further, by Lemma 8 and Equation (20), one can get
V ( t ) G ( t k ) E β η ¯ t t k β ,
where t t k , t k + 1 , η ¯ = 2 Θ i η + ν 2 1 ξ + ν 3 1 ξ τ . Note that we require η ¯ > 0 , as control is unnecessary for systems with naturally asymptotic decay.
Hence, combining (19) and (21) we can conclude that
V ( t ) max sup s τ , 0 V ( t k + s ) E β σ τ β E β σ t t k β , G ( t k ) E β η ¯ t t k β ,
for t t k , t k + 1 .
For any t t 0 , t 1 , we have
V ( t ) max V ¯ ( t 0 ) E β σ t t 0 β , G ( t 0 ) E β η ¯ t t 0 β ,
where V ¯ ( t 0 ) = sup s τ , 0 V ( t 0 + s ) E β σ τ β . Hence,
sup s τ , 0 V ( t 1 + s ) max V ¯ ( t 0 ) E β σ t 1 τ t 0 β , G ( t 0 ) E β η ¯ t 1 t 0 β .
For any t t 1 , t 2 , we get
V ( t ) max sup s τ , 0 V ( t 1 + s ) E β σ τ β E β σ t t 1 β , G ( t 1 ) E β η ¯ t t 1 β max V ¯ ( t 0 ) E β σ t 1 τ t 0 β E β σ τ β E β σ t t 1 β , G ( t 0 ) E β η ¯ t 1 t 0 β × E β σ t t 1 β E β σ τ β , G ( t 1 ) E β η ¯ t t 1 β max V ¯ ( t 0 ) ς E β σ t t 1 β , G ( t 0 ) E β η ¯ t 1 t 0 β E β σ t t 1 β E β σ τ β , G ( t 1 ) E β η ¯ t t 1 β ,
where ς = max k N + E β σ t k τ t k 1 β E β σ τ β < 1 . Therefore
sup s τ , 0 V ( t 2 + s ) max V ¯ ( t 0 ) ς E β σ t 2 τ t 1 β , G ( t 0 ) E β η ¯ t 1 t 0 β ς ¯ , G ( t 1 ) E β η ¯ t 2 t 1 β ,
where ς ¯ = max k N + E β σ t k t k 1 β E β σ τ β < 1 .
For any t t 2 , t 3 , we get
V ( t ) max sup s τ , 0 V ( t 2 + s ) E β σ τ β E β σ t t 2 β , G ( t 2 ) E β η ¯ t t 2 β max V ¯ ( t 0 ) ς 2 E β σ t t 2 β , G ( t 0 ) E β η ¯ t 1 t 0 β ς ¯ E β σ t t 2 β E β σ τ β , G ( t 1 ) E β η ¯ t 2 t 1 β E β σ t t 2 β E β σ τ β , G ( t 2 ) E β η ¯ t t 2 β .
Further,
sup s τ , 0 V ( t 3 + s ) max V ¯ ( t 0 ) ς 2 E β σ t 3 τ t 2 β , G ( t 0 ) E β η ¯ t 1 t 0 β ς ¯ 2 , G ( t 1 ) E β η ¯ t 2 t 1 β ς ¯ , G ( t 2 ) E β η ¯ t 3 t 2 β .
Thus, one concludes that, for any l N + and t t l , t l + 1 , there exists
sup s τ , 0 V ( t l + s ) max m = 1 , 2 , , l V ¯ ( t 0 ) ς l 1 E β σ t l τ t l 1 β , G ( t m ) E β η ¯ t m t m 1 β ς ¯ l m ,
and from (22) and (23), we get
V ( t ) max sup s τ , 0 V ( t l + s ) E β σ τ β E β σ t t l β , G ( t l ) E β η ¯ t t l β max m = 1 , 2 , , l V ¯ ( t 0 ) ς l , G ( t m ) E β η ¯ T ^ β ς ¯ l m + 1 .
Note that lim t + G ( t ) = 0 , for any 0 < ε < 1 , there must exist a l 1 , l 2 , l 3 > 0 such that
G ( t ) < ε E β η ¯ T ^ β , t t l 1 , ς l < ε V ¯ ( t 0 ) , l l 2 , ς ¯ l 1 l 3 + 1 < ε sup t t 0 G ( t ) E β η ¯ T ^ β , t t l 3 .
Hence, we have
max m = 1 , 2 , , l 1 l 3 + 1 G ( t m ) E β η ¯ T ^ β ς ¯ l m + 1 < max m = 1 , 2 , , l 1 l 3 + 1 sup t t 0 G ( t ) E β η ¯ T ^ β ς ¯ l 1 l 3 + 1 < ε , max m = l 1 l 3 + 1 , , l 1 G ( t m ) E β η ¯ T ^ β ς ¯ l m + 1 < max m = l 1 l 3 + 1 , , l 1 G ( t m ) E β η ¯ T ^ β < ε ,
for t t max l 1 , l 2 , l 3 , which implies V ( t ) < ε , t t max l 1 , l 2 , l 3 . □
Remark 5.
Theorem 1 first presents a criterion for achieving synchronization in fractional-order systems with complex delays using intermittent control. In previous studies [41,42], it has been challenging to obtain upper bounds for the states of fractional-order delay systems. By utilizing Lemmas 7 and 8, we derived the upper bounds for both the controlled and uncontrolled systems. Based on these results, we established a synchronization criterion, providing new insights and approaches for further research on intelligent control of fractional-order delay systems.
Remark 6.
When t 1 + , controller (17) degenerates into a continuous controller. Remarkably, the synchronization of the system can still be guaranteed under controller (17) with the conditions specified in Theorem 1. This special case not only demonstrates the flexibility of our control strategy but also verifies the generality of the proposed theoretical results.
The switching mechanism Θ ( t k ) , being governed by the threshold function G ( t ) , exhibits degenerate behavior when specific forms of G ( t ) are adopted. In particular, the controller (17) reduces to classical intermittent control for certain G ( t ) selections.
u i ( t ) = Θ ¯ i e i ( t ) , t T k , T ˜ k , 0 , t T ˜ k , T k + 1 ,
where T k = t 2 k and T ˜ k = t 2 k + 1 for k N + . Combining system (13) and controller (24), the error system can be rewritten as
D t β t k C e i ( t ) = C e i ( t ) + D f x i ( t ) f y ( t ) + B f x i ( t τ ) f y ( t τ ) + A t τ t f x i ( s ) f y ( s ) d s r = 1 s j = 1 n m r l r , i j W r e j ( t ) Θ ¯ i e i ( t ) , t T k , T ˜ k , D t β T ˜ k C e i ( t ) = C e i ( t ) + D f x i ( t ) f y ( t ) + B f x i ( t τ ) f y ( t τ ) + A t τ t f x i ( s ) f y ( s ) d s r = 1 s j = 1 n m r l r , i j W r e j ( t ) , t T ˜ k , T k + 1 .
Theorem 2.
Under Assumption 1, then the network (25) can achieve synchronization under the control protocol (24) if
E β σ T ˇ β E β η ¯ T ^ β < 1 ,
where η ¯ = λ max ν ¯ 1 DD T + ν ¯ 2 BB T + ν ¯ 3 τ AA T 2 C + ν ¯ 1 1 ξ + ν ¯ 2 1 ξ + ν ¯ 3 1 ξ τ r = 1 s m r λ min L r W r , η ˜ = 2 Θ ¯ i η ¯ + ν ¯ 2 1 ξ + ν ¯ 3 1 ξ τ , ν ¯ i > 0 and σ > 0 is given by
η ˜ = σ + ν ¯ 2 1 ξ sup t t 0 + τ E β σ t t 0 τ β E β σ t t 0 β + ν ¯ 3 1 ξ sup t t 0 + τ 0 τ E β σ t t 0 s β d s E β σ t t 0 β .
Proof. 
Construct the Lyapunov function candidate
V ( t ) = i = 1 n e i T ( t ) e i ( t ) .
From the analytical framework established in Theorem 1, we can derive
D t β t k C V ( t ) η ˜ V ( t ) + ν ¯ 2 1 ξ V ( t τ ) + ν ¯ 3 1 ξ t τ t V ( s ) d s , t T k , T ˜ k , D t β T ˜ k C V ( t ) η 2 Θ ¯ i V ( t ) + ν ¯ 2 1 ξ V ( t τ ) + ν ¯ 3 1 ξ t τ t V ( s ) d s , t T ˜ k , T k + 1 .
Moreover, resulting from Lemma 7 and Theorem 1, we have
V ( t ) V ( T k ) E β σ t t k β , t T k , T ˜ k , V ( t ) V T ˜ k E β η ¯ t T ˜ k β , t T ˜ k , T k + 1 .
Then, for any t T 0 , T ˜ 0 , we have
V ( t ) V T 0 E β σ t T 0 β .
For any t T ˜ 0 , T 1 , one gets
V ( t ) V T 0 E β σ T ˜ 0 T 0 β E β η ¯ t T ˜ k β .
Thus, one concludes that, for any t T l , T ˜ l , there exists
V ( t ) V t 0 j = 1 l E β σ T ˜ j T j β E β η ¯ T j + 1 T ˜ j β E β σ t T l β V t 0 j = 0 l E β σ T ˜ j T j β E β η ¯ T j + 1 T ˜ j β .
For any t T ˜ l , T l + 1 , there have
V ( t ) V t 0 j = 0 l E β σ T ˜ j T j β E β η ¯ T j + 1 T ˜ j β E β η ¯ t T ˜ l β V t 0 j = 0 l E β σ T ˜ j T j β E β η ¯ T j + 1 T ˜ j β .
Note that 0 < E β σ T ˇ β E β η ¯ T ^ β < 1 . Hence, for any ε > 0 , there must exists a l ¯ such that
V ( t ) V t 0 E β σ T ˇ β E β η ¯ T ^ β l ¯ < ε
for t l ¯ . Consequently, it is straightforward to derive that lim t + V ( t ) = 0 . □
Remark 7.
Intermittent controller (24) is the classic form currently used to address fractional-order systems. Due to the special memory properties of fractional-order systems and the lack of relevant tools, there has been no research on intermittent control for delay fractional-order systems in the existing literature. Theorem 2, based on the results obtained in this paper, successfully overcomes the challenges posed by the memory effects of fractional-order systems and the impact of system delays on synchronization.

4. Numerical Examples

Two numerical examples validate the efficacy of our theoretical findings, showcasing network synchronization under the proposed intermittent control scheme.
Example 1.
Consider the following FOCNN with higher-order interactions, in which network is described as
D t 0.96 t p C x i ( t ) = C x i ( t ) + D f x i ( t ) + B f x i ( t τ ) + A t τ t f x i ( s ) d s + 0.5 j 1 = 1 n d i j 1 W 1 h 1 ( x i ( t ) , x j 1 ( t ) ) + 0.5 j 1 = 1 n j 2 = 1 n d i j 1 j 2 × W 2 h 2 ( x i ( t ) , x j 1 ( t ) , x j 2 ( t ) ) + I ( t ) + u i ( t ) , t t p , t p + 1 ,
where t t p , t p + 1 , x i ( t ) = x i 1 ( t ) , x i 2 ( t ) T R 2 , f 1 z = tanh z , f 2 z = z + 1 z 1 / 2 , h 1 ( x i ( t ) , x j 1 ( t ) ) = x j 1 ( t ) x i ( t ) and h 2 ( x i ( t ) , x j 1 ( t ) , x j 2 ( t ) ) = 1 2 x j 1 ( t ) + x j 2 ( t ) 2 x i ( t ) , I ( t ) = 0.2 cos ( t ) , 0.1 sin ( t ) T . It is clear that Assumption 1 holds. Assume that W 1 = W 2 = 0.3 0 0 0.4 , C = 2.5 0 0 2.5 , D = 1 2 1.5 1 , B = 1.5 1 3 0.5 , A = 0.5 1 0.5 1 , t 2 k + 1 t 2 k = 0.2 , t 2 ( k + 1 ) t 2 k + 1 = 0.1 . The topology structure of model (27) is shown in Figure 1. Meanwhile, the corresponding Laplacian matrices are
L 1 = 2 0 1 1 0 0 1 2 0 0 1 0 1 0 3 0 0 1 0 0 0 2 1 1 0 1 0 1 3 1 0 0 1 1 1 3 , L 2 = 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2 1 1 0 0 0 1 2 1 0 0 0 1 1 2 .
The initial values of networks (27) are randomly chosen as follows: x 1 ( 0 ) = 1 , 2 T , x 2 ( 0 ) = 2 , 1.8 T , x 3 ( 0 ) = 3 , 2.5 T , x 4 ( 0 ) = 2 , 1.5 T , x 5 ( 0 ) = 3 , 3 T , x 6 ( 0 ) = 1 , 1 T . Let the prescribed threshold function G ( t ) = 6 E 0.96 3 t 0.96 , and the control gain Θ i = 5 is established by Theorem 1.
The behavior of the state variables x i ( t ) of the network described by Equation (27) without control is shown in Figure 2. From the plot, it is evident that synchronization cannot be achieved by the network’s intrinsic structure alone, indicating that additional intervention is needed to drive the system towards synchronization.
Figure 3 presents the time evolution of the state variables x i ( t ) when the system is governed by the controller described in Equation (17). The controlled system shows a significant improvement in the behavior of the state variables, with the trajectories of x i ( t ) now moving toward synchronization. This indicates that the applied control mechanism effectively guides the network towards a synchronized state, as compared to the uncontrolled system.
To further analyze the effectiveness of the control, Figure 4 illustrates the trajectories of the error term e ( t ) 2 and the function G ( t ) under the influence of the controller. The error term e ( t ) 2 represents the deviation between the states of the individual nodes, and it can be seen from the figure that this error decreases over time, which suggests that the network’s synchronization is improving. Meanwhile, the function G ( t ) demonstrates the overall system’s performance, further confirming the success of the controller in reducing the error.
Finally, the time response of the intermittent control, as described by Equation (17), is shown in Figure 5. This figure highlights the dynamic nature of the control process, where the control is applied intermittently to adjust the system’s trajectory. The intermittent application of control provides a more efficient method for synchronization by reducing the overall energy expenditure while still maintaining the necessary adjustments to guide the network towards synchronization.
Example 2.
For the second example, we selected C = 3 0 0 3 , D = 2 1 1 2 , B = 2.5 2 1 1.5 , A = 1.5 2 1.5 3 , W 1 = W 2 = 0.2 0 0 0.2 , while keeping the other system parameters consistent with those in Example 1. The control gain Θ i = 10 is established by Theorem 2.
The state variable trajectories x i ( t ) of the network in Equation (27) without control are shown in Figure 6. It is clear that synchronization cannot be achieved through the network’s intrinsic structure alone, requiring external intervention.
Figure 7 illustrates the time evolution of x i ( t ) when the system is controlled by the mechanism in Equation (26). The controlled system shows a notable improvement, with the state variables’ trajectories moving toward synchronization, demonstrating the effectiveness of the control.
Figure 8 shows the error term e ( t ) under the controller (24), which decreases over time, indicating improving synchronization in the network. Finally, Figure 9 presents the time response of the intermittent control from Equation (24), emphasizing its dynamic application. The intermittent control method offers a more efficient approach for synchronization, minimizing energy consumption while maintaining necessary adjustments to guide the system toward synchronization.

5. Conclusions

This work demonstrates that incorporating higher-order interactions and mixed delays significantly influences the synchronization behavior of fractional-order coupled neural networks. By developing new analytical tools for fractional systems and an event-dependent intermittent controller, we establish synchronization criteria that reduce control frequency while maintaining stability. The numerical results confirm the effectiveness of these findings. Future research may extend the proposed approach to networks with stochastic disturbances, adaptive event thresholds, or hardware implementation constraints.

Author Contributions

Conceptualization, Z.W., D.Y. and H.L.; methodology, Z.W. and D.Y.; software, Z.W. and X.L.; validation, Y.Y. and P.C.; formal analysis, Z.W., D.Y. and H.L.; investigation, Z.W. and X.L.; resources, Y.Y. and P.C.; writing—original draft preparation, Z.W.; writing—review and editing, D.Y., H.L. and Y.Y.; visualization, Z.W. and X.L. All authors have read and agreed to the published version of the manuscript.

Funding

This work was supported in part by the National Natural Science Foundation of China (Grant Nos 12161063, 62173027, 12201175); in part by the Key Project of Inner Mongolia Natural Science Foundation (Grant No. 2025ZD036); in part by the Inner Mongolia Autonomous Region Science and Technology Plan Project (Grant No. 2025KYPT0098); in part by the Youth Top Talent Project of of Hebei Education Department (No. BJK2024125).

Data Availability Statement

The raw data supporting the conclusions of this article will be made available by the authors on request.

Conflicts of Interest

We declare that we have no conflict of interest.

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Figure 1. 2-simplicial complex formed by 6 nodes, where 1 , 2 , 1 , 3 , 2 , 5 , 3 , 6 represent 1-simplex and 4 , 5 , 6 denotes 2-simplex.
Figure 1. 2-simplicial complex formed by 6 nodes, where 1 , 2 , 1 , 3 , 2 , 5 , 3 , 6 represent 1-simplex and 4 , 5 , 6 denotes 2-simplex.
Fractalfract 09 00824 g001
Figure 2. Trajectories of the state variables x i ( t ) of system (27) without control, with fractional order β = 0.96 , and initial conditions x 1 ( 0 ) = ( 1 , 2 ) T , x 2 ( 0 ) = ( 2 , 1.8 ) T , x 3 ( 0 ) = ( 3 , 2.5 ) T , x 4 ( 0 ) = ( 2 , 1.5 ) T , x 5 ( 0 ) = ( 3 , 3 ) T , x 6 ( 0 ) = ( 1 , 1 ) T .
Figure 2. Trajectories of the state variables x i ( t ) of system (27) without control, with fractional order β = 0.96 , and initial conditions x 1 ( 0 ) = ( 1 , 2 ) T , x 2 ( 0 ) = ( 2 , 1.8 ) T , x 3 ( 0 ) = ( 3 , 2.5 ) T , x 4 ( 0 ) = ( 2 , 1.5 ) T , x 5 ( 0 ) = ( 3 , 3 ) T , x 6 ( 0 ) = ( 1 , 1 ) T .
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Figure 3. Trajectories of the state variables x i ( t ) of system (27) under the intermittent controller (17), with control gain Θ i = 5 and threshold function G ( t ) = 6 E 0.96 ( 3 t 0.96 ) .
Figure 3. Trajectories of the state variables x i ( t ) of system (27) under the intermittent controller (17), with control gain Θ i = 5 and threshold function G ( t ) = 6 E 0.96 ( 3 t 0.96 ) .
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Figure 4. Time responses of the synchronization error e ( t ) 2 and the threshold function G ( t ) under the proposed intermittent controller for system (27).
Figure 4. Time responses of the synchronization error e ( t ) 2 and the threshold function G ( t ) under the proposed intermittent controller for system (27).
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Figure 5. Time response of the intermittent control input u i ( t ) governed by the controller (17) for system (27).
Figure 5. Time response of the intermittent control input u i ( t ) governed by the controller (17) for system (27).
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Figure 6. Trajectories of system (27) for β = 0.96 without control in Example 2.
Figure 6. Trajectories of system (27) for β = 0.96 without control in Example 2.
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Figure 7. Trajectories of the state variables x i ( t ) of system (27) under the intermittent controller (17), with control gain Θ i = 10 in Example 2.
Figure 7. Trajectories of the state variables x i ( t ) of system (27) under the intermittent controller (17), with control gain Θ i = 10 in Example 2.
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Figure 8. Time responses of the synchronization error e ( t ) 2 under the proposed intermittent controller for system (27). in Example 2.
Figure 8. Time responses of the synchronization error e ( t ) 2 under the proposed intermittent controller for system (27). in Example 2.
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Figure 9. Time evolution of intermittent control input u i ( t ) for system (27) in Example 2.
Figure 9. Time evolution of intermittent control input u i ( t ) for system (27) in Example 2.
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Wu, Z.; Yang, D.; Li, H.; Yu, Y.; Liu, X.; Cattani, P. A Novel Event-Dependent Intermittent Control for Synchronization of Fractional-Order Coupled Neural Networks with Mixed Delays and Higher-Order Interactions. Fractal Fract. 2025, 9, 824. https://doi.org/10.3390/fractalfract9120824

AMA Style

Wu Z, Yang D, Li H, Yu Y, Liu X, Cattani P. A Novel Event-Dependent Intermittent Control for Synchronization of Fractional-Order Coupled Neural Networks with Mixed Delays and Higher-Order Interactions. Fractal and Fractional. 2025; 9(12):824. https://doi.org/10.3390/fractalfract9120824

Chicago/Turabian Style

Wu, Zhilin, Dongsheng Yang, Hong Li, Yongguang Yu, Xiang Liu, and Piercarlo Cattani. 2025. "A Novel Event-Dependent Intermittent Control for Synchronization of Fractional-Order Coupled Neural Networks with Mixed Delays and Higher-Order Interactions" Fractal and Fractional 9, no. 12: 824. https://doi.org/10.3390/fractalfract9120824

APA Style

Wu, Z., Yang, D., Li, H., Yu, Y., Liu, X., & Cattani, P. (2025). A Novel Event-Dependent Intermittent Control for Synchronization of Fractional-Order Coupled Neural Networks with Mixed Delays and Higher-Order Interactions. Fractal and Fractional, 9(12), 824. https://doi.org/10.3390/fractalfract9120824

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