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Adaptive Fuzzy Control with Predefined-Time Convergence for High-Order Nonlinear Systems Facing Input Delay and Unmodeled Dynamics

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31 January 2026

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03 February 2026

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Abstract
This work addresses the design of a predefined-time adaptive fuzzy control scheme for high-order nonlinear systems with nonstrict-feedback structures, subject to unmodeled dynamics and input time delay. To mitigate the influence of unmodeled dynamics, a predefined-time auxiliary dynamic signal is incorporated into the controller design. Meanwhile, the adverse effects caused by input delay are handled by integrating a Padé approximation with the introduction of an intermediate state variable. Fuzzy logic systems are utilized to approximate the unknown nonlinear terms present in the system dynamics. Based on a recursive backstepping framework and a power-type Lyapunov function formulation, an adaptive fuzzy tracking controller with predefined-time convergence char acteristics is constructed. A detailed stability analysis demonstrates that the closed-loop system achieves practical predefined-time convergence, and appropriate selection of design parameters guarantees that the tracking errors remain confined within a small bounded region around the origin. Finally, the effectiveness and advantages of the proposed control strategy are validated through a numerical example and a practical example.
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1. Introduction

The control of high-order nonlinear systems has attracted sustained attention due to their broad applicability in complex engineering processes. Compared with strict-feedback systems, high-order nonlinear systems exhibit a more general structure, allowing them to describe intricate nonlinear dynamics more accurately. However, conventional linearization techniques often lead to uncontrollable or unobservable modes, which significantly complicates controller design [1,2,3]. To address these challenges, a constructive control framework based on the adding one power integrator technique was developed, enabling effective stabilization and tracking of high-order nonlinear systems. This approach has been widely extended to adaptive control designs for uncertain systems. Nevertheless, many existing methods rely on precise knowledge of system nonlinearities, an assumption that is difficult to satisfy in practical applications due to modeling uncertainties and external disturbances. To overcome this limitation, intelligent adaptive control schemes employing fuzzy logic systems and neural networks have been introduced. Owing to their strong learning and approximation capabilities, these methods can estimate unknown nonlinear functions online, thereby improving robustness and tracking performance for high-order nonlinear systems with unknown dynamics. Several studies have explored specific adaptive control strategies to handle these challenges in different contexts [4,5]. For example, an adaptive control strategy for high-order nonlinear multi-agent systems operating under event-triggered communication protocols has been reported to decrease communication load while maintaining coordinated tracking accuracy [6]. To overcome the well-known complexity growth associated with backstepping methods, an adaptive dynamic surface control approach incorporating parameter estimation has been proposed for high-order strict-feedback nonlinear systems [7]. Furthermore, an adaptive neural control framework with dynamic memory and event-triggered mechanisms has been introduced for high-order stochastic nonlinear systems subject to delayed output constraints, effectively addressing stochastic disturbances and constraint requirements in a unified manner [8]. Additionally, adaptive tracking control schemes for high-order nonlinear systems with time-varying delays and asymmetric output constraints have been investigated, ensuring robust tracking performance in the presence of delay effects and nonuniform constraint limits [9].
Due to modeling inaccuracies, external disturbances, measurement noise, and inevitable modeling simplifications, unmodeled dynamics frequently exist in practical control systems. These neglected dynamics, such as unknown high-order system behaviors, actuator dynamics, and unaccounted nonlinear effects, introduce additional uncertainties that are not represented in the nominal model [10,11,12]. As a consequence, the presence of unmodeled dynamics can degrade tracking accuracy, slow system responses, and in severe cases, lead to instability of the controlled plants [13,14]. Therefore, considerable research attention has been devoted to the study of nonlinear systems with unmodeled dynamics, with the objective of developing robust and adaptive control strategies that can effectively compensate for these uncertainties while guaranteeing stability and satisfactory control performance. Several studies have explored specific adaptive control strategies to address unmodeled dynamics in various contexts [15,16,17]. As an example, adaptive control scheme has been reported for nonlinear systems with input time delays, unknown dead-zone characteristics, and unmodeled dynamics, aiming to simultaneously counteract delay effects, actuator nonlinearities, and modeling inaccuracies [18]. To enhance approximation accuracy and fault-handling capability in fractional-order systems, neural network–based adaptive controller has been introduced for nonlinear dynamics affected by actuator faults and unmodeled uncertainties [19]. Moreover, event-triggered fuzzy adaptive finite-time control strategy has been proposed for stochastic nonlinear systems with unmodeled dynamics, enabling rapid convergence while alleviating communication and computational overhead [20]. Furthermore, adaptive control approach for pure-feedback nonlinear systems under full-state time-varying constraints and unmodeled dynamics has been developed to ensure closed-loop stability and continuous satisfaction of state constraints despite structural uncertainties and evolving limitations [21].
Input delay is an inevitable factor that adversely affects the control accuracy of practical systems due to limitations in actuators, communication channels, and hardware implementation [22]. The existence of input delay can significantly degrade transient response and tracking performance, and may even result in instability if not properly addressed. To mitigate the adverse effects of input delay, various compensation and approximation-based control strategies have been proposed [23,24]. Among them, the Padé approximation method has been widely adopted to transform the delayed input into an equivalent delay-free form, which greatly simplifies controller design. By incorporating Padé approximation into adaptive control frameworks, the influence of input delay in nonlinear systems can be effectively reduced, leading to improved control performance and enhanced closed-loop stability. Several studies have explored specific adaptive control strategies to address input delays in various contexts [25,26,27]. For instance, a finite-time adaptive prescribed performance control has been developed for nonlinear systems with input delay to ensure rapid convergence while compensating for delayed control actions [28]. Adaptive tracking control for nonlinear systems affected by input delay and dynamic uncertainties has been investigated by employing multi-dimensional Taylor network approximations to enhance modeling accuracy and robustness [29]. Neural network–based adaptive reinforcement learning approaches have been explored to achieve optimized backstepping tracking control for nonlinear systems with input delay, enabling online performance improvement through learning mechanisms [30]. In addition, adaptive neural control has been studied for non-strict feedback stochastic nonlinear systems with input delay to handle randomness and delayed inputs while guaranteeing stability and satisfactory tracking behavior [31].
Finite-time control has attracted considerable attention because it guarantees system convergence within a finite duration, providing faster response than asymptotic stabilization methods. It is well known that the convergence time associated with finite-time control schemes is typically a function of the system’s initial conditions, which limits their effectiveness in applications requiring a uniform convergence duration. To address this limitation, fixed-time control was proposed, where the convergence time is explicitly decoupled from the initial state of the system [32,33]. By suitably selecting the control laws, fixed-time strategies guarantee that all system trajectories reach the desired equilibrium within a prescribed bounded time interval. Nevertheless, the convergence time in fixed-time control still depends on several design parameters, and the theoretically derived upper bound is often overly conservative, resulting in a mismatch between analytical estimates and the observed convergence behavior in practical implementations [34,35,36]. In many practical applications, such as aircraft attitude control, multi-agent coordination, and cooperative robotic systems, stability must be achieved within a prescribed time interval. Neither finite-time control nor fixed-time control can guarantee convergence within an exact predefined duration. To eliminate the dependence of convergence time on initial conditions, predefined-time control was introduced, wherein the settling time is exclusively determined by a tunable control parameter rather than the system’s initial state [37,38,39]. This property enables the convergence duration to be explicitly specified a priori, rendering predefined-time control highly attractive for applications with stringent time-performance constraints. In recent years, a variety of adaptive predefined-time control frameworks have been reported for different classes of nonlinear systems [40,41,42,43]. As representative examples, predefined-time adaptive fuzzy control scheme has been developed for nonlinear systems subject to input saturation and delayed constraints, guaranteeing convergence within a designer-assigned time interval even in the presence of actuator limitations [44]. Moreover, adaptive predefined-time control approach has been proposed for stochastic switched nonlinear systems with full-state error constraints and input quantization, ensuring prescribed convergence behavior under switching dynamics and quantization effects [45]. Additionally, adaptive fuzzy predefined-time control strategy has been investigated for stochastic nonlinear systems experiencing actuator and sensor faults, thereby achieving fault-tolerant operation while preserving predefined-time stability [46]. Furthermore, adaptive fuzzy predefined-time tracking controller has been designed for nonstrict-feedback high-order nonlinear systems with input quantization, attaining accurate tracking performance within a predefined time bound despite system complexity and quantization-induced nonlinearities [47].
The motivation for this work stems from the persistent challenges encountered in controlling high-order nonlinear systems under realistic operating conditions. Despite significant advancements in adaptive control, many practical systems continue to suffer from uncertainties arising from unmodeled dynamics, input delays, actuator nonlinearities, and structural complexities. Existing control strategies, including finite-time and fixed-time approaches, often fail to guarantee precise convergence within a user-specified duration, limiting their applicability in safety-critical and time-sensitive applications such as aerospace systems, multi-agent coordination, and cooperative robotics. Moreover, while intelligent adaptive techniques using fuzzy logic systems and neural networks have improved robustness and approximation capabilities, integrating these methods with rigorous time-performance guarantees remains an open problem. These gaps inspired the present research to develop a predefined-time adaptive fuzzy control framework that simultaneously addresses high-order nonlinear dynamics, input delays, and unmodeled uncertainties, with the objective of achieving accurate, reliable, and fast tracking within a rigorously prescribed time interval. This work is further motivated by the need for a control approach that combines the flexibility of intelligent approximation with the predictability of predefined-time convergence, offering practical utility in complex, uncertain, and delayed nonlinear systems. Based on the above analysis, this study is devoted to the design of a predefined-time control framework for high-order nonlinear systems affected by dynamic uncertainties and input time delays. In contrast to the existing literature, the key contributions of this work can be outlined as follows
(i)
Relative to the control schemes presented in [31,32], this work investigates a predefined-time adaptive fuzzy control problem for high-order nonstrict-feedback nonlinear systems in the presence of unmodeled dynamics and input time delays. In contrast to finite-time and fixed-time control approaches reported in [33,34,35,36], the proposed method guarantees system stabilization within a designer-assigned time horizon. Specifically, the convergence duration is directly governed by a tunable design parameter, enabling its explicit selection prior to controller implementation to satisfy desired performance specifications. To enhance practical feasibility, a Padé approximation technique is employed to address the adverse effects of input delays. This delay-compensation mechanism ensures that the closed-loop system retains stability and satisfactory tracking performance even when control actions are subject to delays. Consequently, the developed control framework is applicable to a wide range of high-order nonlinear systems where input delay effects are unavoidable.
(ii)
A dynamic control signal based on the predefined-time control principle is designed to address the effects of unmodeled dynamics, including unknown high-order system behaviors and actuator nonlinearities. The control law ensures that the closed-loop system achieves practical predefined-time stability, meaning that system states converge to a small neighborhood around the origin within the specified time. By selecting appropriate control parameters, the tracking performance can be effectively improved, and the impact of modeling uncertainties, external disturbances, and unmodeled dynamics can be minimized. This provides both theoretical assurance and practical feasibility for high-precision control of complex nonlinear systems.
The remainder of this paper is organized as follows. Section 2 presents the problem formulation along with the required preliminary concepts. The design of the adaptive tracking controller and the associated stability analysis are detailed in Section 3. Simulation results and a representative practical application are provided in Section 4 to demonstrate the performance of the proposed method. Finally, Section 5 concludes the paper and outlines potential directions for future investigation.

2. Problem Formulation and Preliminaries

Consider a class of high-order nonlinear systems with a nonstrict-feedback structure, which can be expressed as
ξ ˙ = q ( ξ , x ) , x ˙ ι = x ι + 1 σ ι + f ι ( x ) + Δ ι ( x , ξ , t ) , ι = 1 , 2 , , h 1 , x ˙ h = u σ h ( t τ ) + f h ( x ) + Δ h ( x , ξ , t ) , y = x 1 .
where the system state vector is defined as x = x h = [ x 1 , , x h ] T R h , with the partial state vector x ι = [ x 1 , , x ι ] T R ι . The constants σ ι 1 are odd integers. The functions f ι ( x ) denote unknown smooth nonlinearities satisfying f ι ( 0 ) = 0 . The variable ξ represents unmeasured internal state dynamics, where the ξ -subsystem corresponds to unmodeled dynamics. The terms Δ ι ( · ) describe unknown nonlinear disturbances acting on the system. It is assumed that q ( · ) and Δ ι ( · ) are uncertain but locally Lipschitz continuous. The scalar variables u R and y R denote the control input and system output, respectively. τ represents an unknown input delay, which is assumed to be a positive constant.
To address the input delay appearing in the high-order nonlinear system (1), the Padé approximation technique is employed, following the approach in [22]. By virtue of the delay property of the Laplace transform, the following relationship holds:
L { u σ h ( t τ ) } = e τ υ L { u σ h ( t ) } = e x p ( τ υ / 2 ) e x p ( τ υ / 2 ) ,
where υ denotes the Laplace variable. Using the first-order Padé approximation, one has
e x p ( τ υ ) L { u σ h ( t ) } 1 τ υ 2 1 + τ υ 2 L { u σ h ( t ) } ,
where L { u ( t ) } is the Laplace transform of u ( t ) .
Remark 1.
Due to the inherent limitation of the Padé approximation, the proposed approach is applicable to systems with small input delays. When τ is sufficiently small, the approximation error e τ υ 1 τ υ 2 1 + τ υ 2 is negligible. The extension to large or time-varying delays will be investigated in future work.
To facilitate controller design, an auxiliary state x h + 1 is introduced such that
1 τ υ 2 1 + τ υ 2 L { u σ h ( t ) } = L { x h + 1 ( t ) } L { u σ h ( t ) } .
Rearranging the above equation yields
2 L { u σ h ( t ) } = L { x h + 1 ( t ) } + τ υ 2 L { x h + 1 ( t ) } .
Applying the inverse Laplace transform gives
x ˙ h + 1 = 4 τ u σ h 2 τ x h + 1 .
Define λ = 2 / τ , then the above equation can be rewritten as
x ˙ h + 1 = 2 λ u σ h λ x h + 1 .
Following the aforementioned transformations, the delayed system in (1) can be reformulated into an equivalent delay-free augmented representation given by
ξ ˙ = q ( ξ , x ) , x ˙ ι = x ι + 1 σ ι + f ι ( x ) + Δ ι ( x , ξ , t ) , ι = 1 , , h 1 , x ˙ h = x h + 1 u σ h + f h ( x ) + Δ h ( x , ξ , t ) , x ˙ h + 1 = λ x h + 1 + 2 λ u σ h , y = x 1 .
The objective of this study is to develop a predefined-time adaptive control strategy based on fuzzy logic systems for system (1), such that all closed-loop signals remain bounded within a designer-specified time interval, and the output tracking error converges to a sufficiently small neighborhood of the origin.
Assumption 1
[13]: For each ι = 1 , 2 , , h , ∃ known, smooth, and nonnegative functions Ψ ι , 1 ( · ) and Ψ ι , 2 ( · ) satisfying
Δ ι ( x , ξ , t ) Ψ ι , 1 x ι + Ψ ι , 2 ξ .
Moreover, without imposing any restriction on generality, the function Ψ ι , 2 ( · ) is assumed to satisfy Ψ ι , 2 ( 0 ) = 0 .
Assumption 2
[14]: Consider the ξ -subsystem ξ ˙ = q ( ξ , x ) associated with system (1). There exist class K functions L ̲ ( · ) , L ¯ ( · ) , and η ( · ) , together with positive constants a and ω , such that an exponentially input-to-state practically stable (Exp-ISpS) Lyapunov function V ( ξ ) can be constructed satisfying
L ̲ ( ξ ) V ( ξ ) L ¯ ( ξ ) ,
and
V ( ξ ) ξ q ( ξ , x ) a V ( ξ ) + η | x 1 | + ω .
Assumption 3
[48]: Define σ ι , for ι = 1 , 2 , , h , as positive odd integers, and let σ = max ι = 1 , 2 , , h σ ι . The odd integers σ ι satisfy the inequality
σ + 1 σ ι σ σ ι + 1 + 1 , ι = 1 , 2 , , h 1 .
Assumption 4
[36]: The reference trajectory y r ( t ) , together with its derivative of order h, is assumed to be smooth and uniformly bounded for all time.
Lemma 1
[49]: Given arbitrary real scalars P and N , and any prescribed positive constants c ˜ , d ˜ , and ε , the following result holds
| P | c ˜ | N | d ˜ c ˜ c ˜ + d ˜ ε | P | c ˜ + d ˜ + d ˜ c ˜ + d ˜ ε c ˜ d ˜ | N | c ˜ + d ˜ .
Lemma 2
[39]: Assume that conditions (10) and (11) are satisfied. Under these conditions, the function V ( ξ ) qualifies as an exponentially input-to-state practically stable (Exp-ISpS) Lyapunov function for the subsystem ξ ˙ = q ( ξ , x ) . Let g 0 and g 0 + be positive constants satisfying g 0 = 3 δ 0 ζ 2 π ζ T d , g 0 + = j 0 ζ 2 π π ζ T d and define g 0 = g 0 + g 0 + ( 0 , g ) . For any initial time t 0 0 and initial condition ξ ( t 0 ) = τ 0 , and for any continuous function η ¯ ( · ) satisfying η ¯ ( x 1 ) η ( | x 1 | ) , there exists a predefined time T 0 = T 0 g 0 , g 0 + , r 0 , τ 0 0 , a positive constant ω = ω ¯ + g 0 + ζ 2 2 2 ζ ζ 2 ζ , and a nonnegative function B ( t 0 , t ) defined for all t t 0 , such that the auxiliary signal r ( t ) satisfies
r ˙ = g 0 r 1 + ζ 2 g 0 + r 1 ζ 2 + η ¯ ( x 1 ) + ω ¯ , r ( t 0 ) = r 0 .
Moreover, the function B ( t 0 , t ) satisfies B ( t 0 , t ) = 0 , t t 0 + T 0 , and the Lyapunov function is bounded by
V ( ξ ( t ) ) r ( t ) + B ( t 0 , t ) .
The solution of the system exists for all t t 0 . Without loss of generality, the function η ¯ ( x 1 ) is chosen as η ¯ ( x 1 ) = x 1 2 λ ( x 1 2 ) under which the auxiliary dynamic signal can be rewritten as
r ˙ = g 0 r 1 + ζ 2 g 0 + r 1 ζ 2 + x 1 2 λ ( x 1 2 ) + ω ¯ , r ( t 0 ) = r 0 .
where λ ( · ) denotes a smooth nonnegative function.
Lemma 3
[39]: For arbitrary real-valued functions J 1 and J 2 , any odd integer σ > 1 , and a given constant k > 0 , one has
J 1 σ J 2 σ σ J 1 J 2 J 1 σ 1 + J 2 σ 1 ,
J 1 + J 2 k c k J 1 k + J 2 k .
where c k = 1 for k < 1 , and c k = 2 k 1 for k 1 . In this work, the exponent is selected as k = σ ι 1 . For notational convenience, both cases are unified as
J 1 + J 2 k 2 k J 1 k + J 2 k .
Lemma 4
[50]: Let ϖ > 1 and μ > 0 be constants, and define the set Ω χ = χ R | | χ | < ϱ μ , ϱ = arctanh ϖ 1 ϖ . Then, for all χ Ω χ , the inequality 1 ϖ tanh ϖ χ μ 0 is satisfied.
Lemma 5
[39]: For any χ R and any constant l > 0 , the following inequality holds 0 | χ | χ tanh χ l p 0 l , p 0 = 0.2785 .
Lemma 6
[39]: Let f ( χ ) be an unknown continuous function defined on a compact set Ω . For any prescribed constant ε > 0 , there exists a fuzzy logic system (FLS) of the form W T Φ ( χ ) such that
sup χ Ω f ( χ ) W T Φ ( χ ) ε .
where W = [ W 1 , W 2 , , W M ] T denotes the adjustable weight vector, and ε represents the minimum approximation error. Moreover, M > 1 is the number of fuzzy inference rules. The fuzzy basis function vector is defined as Φ ( χ ) = [ Φ 1 ( χ ) , Φ 2 ( χ ) , , Φ M ( χ ) ] T L = 1 M Φ L ( χ ) , where each basis function Φ L ( χ ) is selected as a Gaussian membership function given by
Φ L ( χ ) = exp ( χ μ L ) T ( χ μ L ) G L 2 , L = 1 , 2 , , M ,
with μ L and G L denoting the center and width parameters of the Gaussian function, respectively.
Lemma 7
[39]: Let Z = [ z 1 , z 2 , , z h ] T be the input vector, and let Φ ( Z ) = [ Φ 1 ( Z ) , Φ 2 ( Z ) , , Φ l ( Z ) ] T denote the corresponding fuzzy basis function vector. For any positive integer ι h , define Ξ ι = [ z 1 , z 2 , , z ι ] T . Then, the following inequality holds:
Φ ( Z ) 2 Φ ( Ξ ι ) 2 .
Consider the nonlinear dynamical system
χ ˙ = f ( χ ) ,
where χ R h denotes the state vector, the origin χ = 0 is an equilibrium point, and f : R h R h is a nonlinear mapping.
Definition 1
[39]: Let T d > 0 and X > 0 be given constants. If the state trajectory o satisfies χ ( t ) < X for all t > T d , then the equilibrium point at the origin is said to be practically predefined-time stable. The constant T d is referred to as the predefined time.
Lemma 8
[39]: Assume that there exists a Lyapunov function V ( χ ) such that
V ˙ π ζ T d V 1 + ζ 2 π ζ T d V 1 ζ 2 + B ,
where 0 < ζ < 1 , and T d and B are strictly positive constants. Under these conditions, the function V guarantees practical predefined-time stability, and the corresponding settling time is bounded above by 2 T d .

3. Controller Design and Stability Analysis

To facilitate the construction of the desired control law, the following error coordinate transformations are introduced
z 1 = x 1 y r , z ι = x ι α ι 1 , ι = 2 , 3 , , h 1 , z n = x n α h 1 + x h + 1 / λ ,
where α ι 1 denotes the virtual control signal to be designed subsequently.
Step 1: From (1) and (25), the time derivative of z 1 is obtained as
z ˙ 1 = x 2 σ 1 + f 1 ( x ) + Δ 1 ( x , ξ , t ) y ˙ r .
To analyze the stability of the first subsystem, consider the following power-type Lyapunov function
V 1 = z 1 σ σ 1 + 2 σ σ 1 + 2 + Θ ˜ 1 2 2 τ 1 + r δ 0 ,
where Θ ^ 1 is the estimate of the unknown parameter Θ 1 * and Θ ˜ 1 = Θ 1 * Θ ^ 1 denotes the corresponding estimation error. The design parameters τ 1 and δ 0 are chosen as positive constants. By invoking Assumption 1 together with (16), the time derivative of the Lyapunov function V 1 satisfies
V ˙ 1 z 1 σ σ 1 + 1 x 2 σ 1 + f 1 ( x ) y ˙ r + z 1 σ σ 1 + 1 Ψ 1 , 1 | x 1 | + z 1 σ σ 1 + 1 Ψ 1 , 2 | ξ | 1 τ 1 Θ ˜ 1 Θ ^ ˙ 1 g 0 δ 0 r 1 + ζ 2 g 0 + δ 0 r 1 ζ 2 + 1 δ 0 x 1 2 λ ( x 1 2 ) + ω ¯ δ 0 .
Applying Lemma 5, the term z 1 σ σ 1 + 1 Ψ 1 , 1 ( x 1 ) can be upper bounded as
z 1 σ σ 1 + 1 Ψ 1 , 1 | x 1 | z 1 σ σ 1 + 1 Ψ ^ 1 , 1 ( x 1 ) + l 1 , 1 * ,
where l 1 , 1 > 0 is a design constant, Ψ ^ 1 , 1 ( x 1 ) = Ψ 1 , 1 | x 1 | tanh z 1 σ σ 1 + 1 Ψ 1 , 1 ( x 1 ) l 1 , 1 , and l 1 , 1 * = 0.2785 l 1 , 1 .
By utilizing Assumption 2 together with Lemmas 2 and 5, and following estimation techniques similar to those developed in [26], the following upper bound can be derived:
z 1 σ σ 1 + 1 Ψ 1 , 2 ( | ξ | ) z 1 σ σ 1 + 1 Ψ ^ 1 , 2 ( x 1 , r ) + l 1 , 2 * + 1 4 z 1 2 ( σ σ 1 + 1 ) + m 1 ( t 0 , t ) ,
where l 1 , 2 > 0 is a design parameter, and L 1 ( · ) denotes the inverse of the L ( · ) function introduced in Assumption 2. The estimated function Ψ ^ 1 , 2 ( x 1 , r ) is defined as Ψ ^ 1 , 2 ( x 1 , r ) = Ψ 1 , 2 L 1 ( 2 r ) tanh z 1 σ σ 1 + 1 Ψ 1 , 2 L 1 ( 2 r ) l 1 , 2 , with l 1 , 2 * = 0.2785 l 1 , 2 . Moreover, the composite function Ψ 1 , 2 L 1 r ( t ) + B ( t 0 , t ) = Ψ 1 , 2 L 1 r ( t ) + B ( t 0 , t ) , and m 1 ( t 0 , t ) = Ψ 1 , 2 L 1 2 M ( t 0 , t ) 2 , where m 1 ( t 0 , t ) 0 for all t t 0 + T 0 .
Remark 2:
It is worth noting that the term x 1 2 λ ( x 1 2 ) δ 0 z 1 σ σ 1 + 1 is discontinuous at z 1 = 0 , which prevents its direct approximation using fuzzy logic systems. To overcome this difficulty, a smooth hyperbolic tangent function tanh σ σ 1 + 2 z 1 μ with a given constant μ > 0 is introduced. As a result, the expression z 1 σ σ 1 + 2 tanh σ σ 1 + 2 z 1 μ becomes well defined and continuous at z 1 = 0 .
By using (29) and (30) into (28), one has
V ˙ 1 z 1 σ σ 1 + 1 x 2 σ 1 + f ¯ 1 ( x ) y ˙ r 1 2 z 1 2 ( σ σ 1 + 1 ) 1 τ 1 Θ ˜ 1 Θ ^ ˙ 1 g 0 δ 0 r 1 + ζ 2 g 0 + δ 0 r 1 ζ 2 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 + l 1 , 1 * + l 1 , 2 * + m 1 ( t 0 , t ) + ω ¯ δ 0 ,
where f ¯ 1 ( x ) = f 1 ( x ) + Ψ ^ 1 , 1 ( x 1 ) + Ψ ^ 1 , 2 ( x 1 , r ) + ( σ σ 1 + 2 ) z 1 σ σ 1 + 1 tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 + 3 4 z 1 σ σ 1 + 1 .
Based on Lemma 6, the unknown smooth nonlinear function f 1 ( · ) is approximated using a fuzzy logic system (FLS) expressed in the form
f ¯ 1 ( Z 1 ) = W 1 * T Φ 1 ( Z 1 ) + ε 1 ( Z 1 ) ,
where Z 1 = [ x 1 , x 2 , , x h ] T is the FLS input vector, W 1 * denotes the ideal weight vector, and ε 1 ( Z 1 ) represents the fuzzy approximation error satisfying ε 1 ( Z 1 ) ε 1 * , with ε 1 * > 0 being a known constant.
By applying Young’s inequality together with Lemma 7, the following bounds can be established:
z 1 σ σ 1 + 1 f 1 | z 1 | σ σ 1 + 1 W 1 * Φ 1 ( Z 1 ) + ε 1 * | z 1 | σ σ 1 + 1 W 1 * Φ 1 ( χ 1 ) + ε 1 * 1 2 d 1 2 z 1 2 ( σ σ 1 + 1 ) Θ 1 * Φ 1 T ( χ 1 ) Φ 1 ( χ 1 ) + d 1 2 2 + 1 2 z 1 2 ( σ σ 1 + 1 ) + ε 1 * 2 2 ,
where Θ 1 * = W 1 * 2 , d 1 > 0 is a design constant, and ε 1 * > 0 denotes an unknown bound satisfying ε 1 ε 1 * .
By using (26) into (24), one has
V ˙ 1 z 1 σ σ 1 + 1 1 2 d 1 2 z 1 σ σ 1 + 1 Θ ^ 1 Φ 1 T ( χ 1 ) Φ 1 ( χ 1 ) + x 2 σ 1 α 1 σ 1 + α 1 σ 1 y ˙ r g 0 δ 0 r 1 + ζ 2 g 0 + δ 0 r 1 ζ 2 + Θ ˜ 1 τ 1 τ 1 2 d 1 2 z 1 2 ( σ σ 1 + 1 ) Φ 1 T ( χ 1 ) Φ 1 ( χ 1 ) Θ ^ ˙ 1 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 + l 1 , 1 * + l 1 , 2 * + m 1 ( t 0 , t ) + d 1 2 2 + ε 1 * 2 2 + ω ¯ δ 0 .
Furthermore, by applying Young’s inequality, for any ι = 1 , 2 , , h , one has
2 ( e + e ˜ ) Θ ˜ ι Θ ^ ι ( e + e ˜ ) Θ ˜ ι 2 + ( e + e ˜ ) Θ ι * 2 .
The virtual control law α 1 and the adaptive update law for the parameter estimate Θ ^ 1 are designed as
α 1 = 1 2 d 1 2 z 1 σ σ 1 + 1 Θ ^ 1 Φ 1 T ( χ 1 ) Φ 1 ( χ 1 ) + Γ 1 z 1 σ 1 + β 1 π ζ T d z 1 ( 1 + ζ 2 ) ( ( σ + 1 ) ( σ σ 1 + 1 ) y ˙ r 1 σ 1 ,
Θ ^ ˙ 1 = τ 1 1 2 d 1 2 z 1 2 ( σ σ 1 + 1 ) Φ 1 T ( χ 1 ) Φ 1 ( χ 1 ) 2 ( e + e ˜ ) Θ ^ 1 ,
where β 1 = ( 3 n ) ζ / 2 ( σ σ 1 + 2 ) ( 1 + ζ / 2 ) , β ¯ 1 = 1 ( σ σ 1 + 2 ) ( 1 ζ / 2 ) , Γ 1 = β ¯ 1 π ζ T d + 1 , e = ( 2 ζ ) ( 3 n ) ζ / 2 π ( 2 + ζ / 2 ) τ ζ / 2 κ ζ T d , e ˜ = ( 2 ζ ) π 2 2 ( 2 ζ / 2 ) τ κ ζ / 2 ζ T d , and the initial condition satisfies Θ ^ 1 ( 0 ) 0 .
By using (35)-(37) into (34), one has
V ˙ 1 z 1 σ σ 1 + 1 x 2 σ 1 α 1 σ 1 Γ 1 z 1 σ + 1 β 1 π ζ T d z 1 ( σ + 1 ) ( 1 + ζ / 2 ) ( e + e ˜ ) 1 τ 1 Θ ˜ 1 2 g 0 δ 0 r 1 + ζ 2 g 0 + δ 0 r 1 ζ 2 + ( e + e ˜ ) 1 τ 1 Θ 1 * 2 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 + l 1 , 1 * + l 1 , 2 * + m 1 ( t 0 , t ) + d 1 2 2 + ε 1 * 2 2 + ω ¯ δ 0 .
Using Lemmas 1 and 3, one has
z 1 σ σ 1 + 1 x 2 σ 1 α 1 σ 1 σ 1 | z 1 | σ σ 1 + 1 | x 2 α 1 | | x 2 | σ 1 1 + | α 1 | σ 1 1 | z 1 | σ + 1 + Δ 11 | z 2 | σ + 1 + Δ 12 | z 2 | ( σ + 1 ) / σ 1 ,
where Δ 11 = 2 σ 1 1 σ 1 2 σ + 1 σ + 1 σ σ 1 + 1 1 σ 1 2 σ 1 σ σ 1 + 1 σ 1 is a positive constant related to the given constants σ and σ 1 and Δ 12 = σ 1 2 ( 2 σ 1 1 + 1 ) σ + 1 σ + 1 σ σ 1 + 1 1 σ 1 ( 2 σ 1 + 2 ) σ σ 1 + 1 σ 1 α ( σ 1 1 ) ( σ + 1 ) σ 1 is a nonnegative function.
By using (39) into (38), we have
V ˙ 1 β 1 π ζ T d z 1 ( σ + 1 ) ( 1 + ζ / 2 ) β ¯ 1 π ζ T d z 1 ( σ + 1 ) ( 1 ζ / 2 ) Γ 1 z 1 σ + 1 ( e + e ˜ ) 1 τ 1 Θ ˜ 1 2 g 0 δ 0 r 1 1 + ζ / 2 g 0 + δ 0 r 1 1 ζ / 2 + Δ 11 z 2 σ + 1 + Δ 12 z 2 ( σ + 1 ) / σ 1 + ω ¯ δ 0 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 + l 1 , 1 * + l 1 , 2 * + m 1 ( t 0 , t ) + ( e + e ˜ ) 1 τ 1 Θ 1 * 2 + d 1 2 2 + ε 1 * 2 2 + β ¯ 1 π ζ T d z 1 1 ζ 2 ( σ + 1 )
Applying Lemma 1, one has
z 1 ( σ + 1 ) ( 1 ζ / 2 ) ζ T d Γ ¯ 1 β ¯ 1 π z 1 ( σ + 1 ) + ζ 2 ζ T d Γ ¯ 1 ( 1 ζ / 2 ) β ¯ 1 π 1 2 / ζ .
Next, the time derivative of V 1 can be calculated as
V ˙ 1 β 1 π ζ T d z 1 ( σ + 1 ) ( 1 + ζ / 2 ) β ¯ 1 π ζ T d z 1 ( σ + 1 ) ( 1 ζ / 2 ) ( e + e ˜ ) 1 τ 1 Θ ˜ 1 2 g 0 δ 0 r 1 1 + ζ / 2 g 0 + δ 0 r 1 1 ζ / 2 + Δ 11 z 2 σ + 1 + Δ 12 z 2 ( σ + 1 ) / σ 1 + ω ¯ δ 0 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 + l 1 , 1 * + l 1 , 2 * + m 1 ( t 0 , t ) + ( e + e ˜ ) 1 τ 1 Θ 1 * 2 + d 1 2 2 + ε 1 * 2 2 + β ¯ 1 π ζ T d ζ T d Γ ¯ 1 ( 1 ζ / 2 ) β ¯ 1 π 1 2 / ζ .
Setting P = z ι , N = j , c ˜ = D ( σ σ ι + 2 ) , d ˜ = D ( σ + 1 ) D ( σ σ ι + 2 ) , ϵ = σ + 1 σ σ ι + 2 , one obtains
z ι D ( σ + 1 ) z ι D ( σ σ ι + 2 ) j D ( σ ι 1 ) + σ ι 1 σ + 1 σ + 1 σ σ ι + 2 ( σ σ ι + 2 ) / ( σ ι 1 ) j D ( σ + 1 ) ,
where D > 0 and j > 0 are positive constants.
For (43), let us set ι = 1 , 2 , , . Defining D = 1 + ζ / 2 and j = 1 , we obtain
z ι ( σ + 1 ) ( 1 + ζ / 2 ) z ι ( σ σ ι + 2 ) ( 1 + ζ / 2 ) + σ ι 1 σ + 1 σ + 1 σ σ ι + 2 ( σ σ ι + 2 ) / ( σ ι 1 ) .
Similarly, for ι = 1 , 2 , , , if we choose D = 1 ζ / 2 and j = 1 , we have
z ι ( σ + 1 ) ( 1 ζ / 2 ) z ι ( σ σ ι + 2 ) ( 1 ζ / 2 ) + σ ι 1 σ + 1 σ + 1 σ σ ι + 2 ( σ σ ι + 2 ) / ( σ ι 1 ) .
By using (43)–(45) into (42), one has
V ˙ 1 β 1 π ζ T d z 1 ( σ σ 1 + 2 ) ( 1 + ζ / 2 ) β ¯ 1 π ζ T d z 1 ( σ σ 1 + 2 ) ( 1 ζ / 2 ) ( e + e ˜ ) 1 τ 1 Θ ˜ 1 2 g 0 δ 0 r 1 1 + ζ / 2 g 0 + δ 0 r 1 1 ζ / 2 + Δ 11 z 2 σ + 1 + Δ 12 z 2 ( σ + 1 ) / σ 1 + M 1 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 ,
where M 1 = ( β 1 + β ¯ 1 ) π ζ T d σ 1 1 σ + 1 σ + 1 σ σ 1 + 2 ( σ σ 1 + 2 ) / ( σ 1 1 ) + l 1 , 1 * + l 1 , 2 * + m 1 ( t 0 , t ) + ( e + e ˜ ) 1 τ 1 Θ 1 * 2 + d 1 2 2 + ε 1 * 2 2 + ω δ 0 + β 1 π 2 T d ζ T d Γ 1 ( 1 ζ / 2 ) β 1 π 1 2 / ζ .
Step ι ( ι = 2 , 3 , , 1 ): By using (1) and (18), the derivative of z ι is
z ˙ ι = x ι + 1 σ ι + f ι ( x ) + Δ ι α ˙ ι 1 ,
where
α ˙ ι 1 = κ = 1 ι 1 α ι 1 x κ x κ + 1 + κ = 1 ι 1 α ι 1 x κ f κ + κ = 1 ι 1 α ι 1 x κ Δ κ + κ = 1 ι 1 α ι 1 Θ ^ κ Θ ^ ˙ κ + κ = 0 ι 1 α ι 1 y ( κ ) r ( κ + 1 ) + α ι 1 r r ˙ .
Consider the following Lyapunov function as
V ι = V ι 1 + z ι σ σ ι + 2 σ σ ι + 2 + Θ ˜ ι 2 2 τ ι ,
where Θ ^ ι is the estimate of Θ ι * , Θ ˜ ι = Θ ι * Θ ^ ι , and τ ι > 0 is a designed parameter.
Let Δ ¯ ι be defined as Δ ¯ ι = Δ ι κ = 1 ι 1 α ι 1 x κ Δ κ . By invoking Assumption 2 together with Lemmas 2 and 5, and by applying arguments similar to those presented in Step 1, one has
z ι σ σ ι + 1 Δ ¯ ι z ι σ σ ι + 1 Ψ ^ ι , 1 ( x 1 , , x ι ) + z ι σ σ ι + 1 Ψ ^ ι , 2 ( x 1 , , x ι , r ) + l ι , 1 * + l ι , 2 * + 1 4 z ι 2 ( σ σ ι + 1 ) + m ι ( t 0 , t ) ,
where l ι , 1 > 0 , l ι , 2 > 0 , , Ψ ^ ι , 1 = Ψ ι , 1 + κ = 1 ι 1 α ι 1 x κ Ψ ι , 1 tanh z ι σ σ ι + 1 l ι , 1 Ψ ι , 1 + κ = 1 ι 1 α ι 1 x κ Ψ ι , 1 , l ι , 1 * = 0.2785 l ι , 1 , Ψ ι , 2 ( x 1 , x 2 , , x ι , r ) = Ψ ι , 2 L 1 ( 2 r ) + κ = 1 ι 1 α ι 1 x κ Ψ ι , 1 Ψ ι , 2 L 1 ( 2 r ) , Ψ ^ ι , 2 ( x 1 , x 2 , , x ι , r ) = Ψ ι , 2 ( x 1 , x 2 , , x ι , r ) tanh z ι σ σ ι + 1 l ι , 2 Ψ ι , 2 ( x 1 , x 2 , , x ι , r ) , m ι ( t 0 , t ) = κ = 1 ι Ψ κ , 2 L 1 ( 2 M ( t 0 , t ) ) 2 , m ι ( t 0 , t ) 0 for all t t 0 + T 0 , l ι , 2 * = 0.2785 l ι , 2 .
Using the results given in (47)–(50), the time derivative of V ι can be expressed as
V ˙ ι κ = 1 ι 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι 1 β κ β ¯ κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι 1 e + e ˜ τ κ Θ ˜ κ 2 + Δ ( ι 1 ) 1 z ι σ + 1 + Δ ( ι 1 ) 2 z ι ( σ + 1 ) / σ ι 1 τ ι Θ ˜ ι Θ ^ ˙ ι 1 2 z ι 2 ( σ σ ι + 1 ) g 0 δ 0 r 1 + ( 1 + ς ) / 2 g 0 δ 0 r 1 ( 1 ς ) / 2 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 ) δ 0 + l ι , 1 * + l ι , 2 * + m ι ( t 0 , t ) + M ι 1 + z ι σ σ ι + 1 ( x ι + 1 σ ι + f ¯ ι ( x ) κ = 1 ι 1 α ι 1 x κ x κ + 1 κ = 1 ι 1 α ι 1 x κ f κ κ = 1 ι 1 α ι 1 Θ ^ κ Θ ^ ˙ κ κ = 0 ι 1 α ι 1 y ( κ ) r ( κ + 1 ) α ι 1 r r ˙ )
where f ¯ ι ( x ) = f ι ( x ) + 3 4 z ι σ σ ι + 1 + Ψ ^ ι , 1 ( x 1 , , x ι ) + Ψ ^ ι , 2 ( x 1 , , x ι , r ) .
Now, f ¯ ι can be estimated through a fuzzy logic system (FLS) approximation of the form
f ¯ ι ( Z ι ) = W ι * T Φ ι ( Z ι ) + ε ι ( Z ι ) , ε ι ( Z ι ) ε ι * ,
where Z ι = [ x 1 , , x h , Θ ^ 1 , , Θ ^ ι 1 ] T and ε ι * > 0 is a constant.
With the help of Young’s inequality and Lemma 7, one has
z ι σ σ ι + 1 f ι | z ι | σ σ ι + 1 W ι * Φ ι ( Z ι ) + ε ι * 1 2 d ι 2 z ι 2 ( σ σ ι + 1 ) Θ ι * Φ ι T ( χ ι ) Φ ι ( χ ι ) + d ι 2 2 + 1 2 z ι 2 ( σ σ ι + 1 ) + ( ε ι * ) 2 2 ,
where Θ ι * = W ι * 2 , χ ι = [ x 1 , , x ι ] T , d ι > 0 is a design parameter, and ε ι * > 0 satisfies ε ι ε ι * .
The virtual controller α ι and the adaptive law for Θ ^ ι are designed as
α ι = 1 σ ι ( 1 2 d ι 2 z ι σ σ ι + 1 Θ ι Φ ι T ( χ ι ) Φ ι ( χ ι ) + Δ ( ι 1 ) 1 z ι σ ι + Δ ( ι 1 ) 2 z ι σ ι κ = 1 ι 1 α ι 1 x κ x κ + 1 κ = 1 ι 1 α ι 1 x κ f κ κ = 1 ι 1 α ι 1 Θ ^ κ Θ ^ ˙ κ κ = 0 ι 1 α ι 1 y ( κ ) r ( κ + 1 ) α ι 1 r r ˙ + Γ ι z ι σ ι + β ι π ς T d z ι ( 1 + ς / 2 ) ( σ + 1 ) ( σ σ ι + 1 ) ) 1 σ ι ,
Θ ^ ˙ ι = τ ι 1 2 d ι 2 z ι 2 ( σ σ ι + 1 ) Φ ι T ( χ ι ) Φ ι ( χ ι ) 2 ( e + e ˜ ) Θ ^ ι ,
where β ι = ( 3 n ) ς 2 ( σ σ ι + 2 ) ( 1 + ς / 2 ) , β ¯ ι = 1 ( σ σ ι + 2 ) ( 1 ς / 2 ) , and Γ ι = β ¯ ι π ς T d + 1 . Moreover, σ ¯ ι = σ + 1 σ ι 1 ( σ σ ι + 1 ) , Θ ^ ι ( 0 ) 0 , and σ ι is a nonnegative constant under Assumption 3. In addition, Δ ( ι 1 ) 1 = σ ι 1 2 σ ι 1 1 σ + 1 σ + 1 σ ι 1 2 σ ι 1 ( σ σ ι 1 + 1 ) σ σ ι 1 + 1 σ ι 1 ,
and Δ ( ι 1 ) 2 = σ ι 1 2 ( 2 σ ι 1 1 + 1 ) σ + 1 α ( σ ι 1 1 ) ( σ + 1 ) / σ ι 1 σ + 1 σ ι 1 ( σ σ ι 1 + 1 ) ( 2 σ ι 1 + 2 ) σ σ ι 1 + 1 σ ι 1 .
By using (53)–(55) into (51), one has
V ˙ ι κ = 1 ι 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι 1 β κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι e + e ˜ τ κ Θ ˜ κ 2 + z ι σ σ ι + 1 ( x ι + 1 σ ι α ι σ ι ) Γ ι z ι σ + 1 β ι π ς T d z ι ( 1 + ς / 2 ) ( σ + 1 ) β ι π ς T d z ι ( 1 ς / 2 ) ( σ + 1 ) + ( e + e ˜ ) 2 τ ι Θ ι * 2 g 0 δ 0 r 1 ( 1 + ς / 2 ) g ¯ 0 δ 0 r 1 ( 1 ς / 2 ) + β ι π ς T d z ι ( 1 ς / 2 ) ( σ + 1 ) + m ι ( t 0 , t ) + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 ( z 1 / μ ) x 1 2 λ ( x 1 2 ) + M ι 1 + l ι , 1 * + l ι , 2 * + d ι 2 2 + ( ε ι * ) 2 2 .
By Lemma 1 and Lemma 3, one has
z ι σ σ ι + 1 x ι + 1 σ ι α ι σ ι z ι σ + 1 + Δ ι 1 z ι + 1 σ + 1 + Δ ι 2 z ι + 1 σ ι + 1 σ ι .
where Δ ι 1 = 2 σ ι 1 σ ι 2 σ + 1 σ + 1 ( σ σ ι + 1 ) σ ι 2 σ ι σ σ ι + 1 σ ι , which is a positive constant related to the given constants σ and σ ι , and Δ ι 2 = σ ι 2 ( 2 σ ι 1 + 1 ) σ + 1 σ + 1 ( σ σ ι + 1 ) σ ι ( 2 σ ι + 1 + 2 ) σ σ ι + 1 σ ι α ( σ ι 1 ) ( σ + 1 ) σ ι , where α is a nonnegative function.
Furthermore, by Lemma 1, we have
z ι ( 1 ς / 2 ) ( σ + 1 ) ς T d Γ ¯ ι β ¯ ι π z ι σ + 1 + ς 2 ς T d Γ ¯ ι ( 1 ς / 2 ) β ¯ ι π 1 2 / ς ,
where Γ ι = Γ ι 1 .
By using (57) and (58) into (56), one has
V ˙ ι κ = 1 ι 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι 1 β ¯ κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι e + e ˜ τ κ Θ ˜ κ 2 g 0 δ 0 r 1 1 + ς / 2 g 0 δ 0 r 1 1 ς / 2 + Δ ι 1 z ι + 1 σ + 1 + Δ ι 2 z ι + 1 σ + 1 σ ι + M ι 1 + l ι , 1 * + l ι , 2 * + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 + β ¯ ι π 2 T d ς T d Γ ¯ ι ( 1 ς / 2 ) β ¯ ι π 1 2 / ς + m ι ( t 0 , t ) + ( e + e ˜ ) Θ ι * 2 2 τ ι + d ι 2 2 + ( ε ι * ) 2 2 .
Using (44) and (45) into (59), one has
V ˙ ι κ = 1 ι 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι 1 β ¯ κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 ι e + e ˜ τ κ Θ ˜ κ 2 g 0 δ 0 r 1 1 + ς / 2 g 0 δ 0 r 1 1 ς / 2 + Δ ι 1 z ι + 1 σ + 1 + Δ ι 2 z ι + 1 σ + 1 σ ι + M ι + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 2 ) δ 0 ,
where M ι = m ι ( t 0 , t ) + ( e + e ˜ ) Θ ι * 2 2 τ ι + β ¯ ι π 2 T d ς T d Γ ¯ ι ( 1 ς / 2 ) β ¯ ι π 1 2 / ς + ( β ι + β ¯ ι ) π ς T d σ ι 1 σ + 1 σ + 1 σ σ ι + 2 σ σ ι + 2 σ ι 1 + l ι , 1 * + l ι , 2 * + d ι 2 2 + ( ε ι * ) 2 2 + M ι 1 .
Step h: By using (8) and (25), one has
z ˙ h = x ˙ h α ˙ h 1 + x ˙ h + 1 λ = x h + 1 u σ h α ˙ h 1 + f h ( x ) + Δ h + 1 λ λ x h + 1 + 2 λ u σ h , = u σ h + f h ( x ) + Δ h α ˙ h 1 ,
where α ˙ h 1 is defined analogously to α ˙ ι 1 in Step ι .
Consider the following Lyapunov function as
V h = V h 1 + z h σ σ h + 2 σ σ h + 2 + Θ ˜ h 2 2 τ h ,
where Θ ^ h is the estimation of Θ h * , Θ ˜ h = Θ h * Θ ^ h , and τ h > 0 is a designed positive parameter.
Define Δ h = Δ ¯ h κ = 1 h 1 α h 1 x κ Δ κ . Similar to Step 1, one has
z h σ σ h + 1 Δ ¯ h z h σ σ h + 1 Ψ ^ h , 1 ( x 1 , , x h ) + z h σ σ h + 1 Ψ ^ h , 2 ( x 1 , , x h , r ) + l h , 1 * + l h , 2 * + 1 4 z h 2 ( σ σ h + 1 ) + m h ( t 0 , t ) ,
where l h , 1 > 0 , l h , 2 > 0 , Ψ ^ h , 1 = Ψ h , 1 + κ = 1 h 1 α h 1 x κ Ψ h , 1 tanh z h σ σ h + 1 l h , 1 Ψ h , 1 + κ = 1 h 1 α h 1 x κ Ψ h , 1 , l h , 1 * = 0.2785 l h , 1 , Ψ h , 2 ( x 1 , x 2 , , x h , r ) = Ψ h , 2 L 1 ( 2 r ) + κ = 1 h 1 α h 1 x κ Ψ h , 1 Ψ h , 2 L 1 ( 2 r ) , Ψ ^ h , 2 ( x 1 , x 2 , , x h , r ) = Ψ h , 2 ( x 1 , x 2 , , x h , r ) tanh z h σ σ h + 1 l h , 2 Ψ h , 2 ( x 1 , x 2 , , x h , r ) , m h ( t 0 , t ) = κ = 1 h Ψ κ , 2 L 1 ( 2 M ( t 0 , t ) ) 2 , m h ( t 0 , t ) 0 for all t t 0 + T 0 .
By using (63) and differentiating V h , one has
V ˙ h κ = 1 h 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 h 1 β ¯ κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 h 1 e + e ˜ τ κ Θ ˜ κ 2 1 τ h Θ ˜ h Θ ^ ˙ h g 0 δ 0 r 1 + ( 1 + ς ) / 2 g ¯ 0 δ 0 r 1 ( 1 ς ) / 2 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 1 2 λ ( x 1 ) δ 0 + l h , 1 * + l h , 2 * + m h ( t 0 , t ) + M h 1 + z h σ σ h + 1 u σ h + f ¯ h ( x )
where σ ¯ h = σ + 1 σ h 1 σ σ h + 1 denotes a nonnegative constant and
f ¯ h ( x ) = f h ( x ) + Δ ( h 1 ) 1 z h σ h + Δ ( h 1 ) 2 z h σ ¯ h + Ψ ^ h , 1 ( x ) + Ψ ^ h , 2 ( x , r ) + 3 4 z h σ σ h + 1 κ = 1 h 1 α h 1 x κ x κ + 1 κ = 1 h 1 α h 1 x κ f κ κ = 1 h 1 α h 1 Θ ^ κ Θ ^ ˙ κ κ = 0 h 1 α h 1 y ( κ ) r ( κ + 1 ) α h 1 r r ˙ .
Now, f ¯ h can be approximated by the FLS as
f ¯ h ( Z h ) = W h * T Φ h ( Z h ) + ε h ( Z h ) , ε h ( Z h ) ε h * ,
where Z h = [ x 1 , , x h , Θ ^ 1 , , Θ ^ h 1 ] T and ε h * > 0 is a constant.
With the help of Young’s inequality and Lemma 7, one has
z h σ σ h + 1 f h | z h | σ σ h + 1 W h * Φ h ( Z h ) + ε h * 1 2 d h 2 z h 2 ( σ σ h + 1 ) Θ h * Φ h T ( χ h ) Φ h ( χ h ) + d h 2 2 + 1 2 z h 2 ( σ σ h + 1 ) + ( ε h * ) 2 2 ,
By using (67) into (65), one has
V ˙ h κ = 1 h 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 h 1 β ¯ κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 h 1 e + e ˜ τ κ Θ ˜ κ 2 1 τ h Θ ˜ h Θ ^ ˙ h g 0 δ 0 r 1 + ( 1 + ς ) / 2 g ¯ 0 δ 0 r 1 ( 1 ς ) / 2 + M h 1 + l h , 1 * + l h , 2 * + m h ( t 0 , t ) + d h 2 2 + ( ϵ h * ) 2 2 + z h σ σ h + 1 u σ h ( t ) + 1 2 d h 2 z h σ σ h + 1 Θ h * Φ h T ( χ h ) Φ h ( χ h ) + 1 τ h Θ ˜ h τ h 1 2 d h 2 z h 2 ( σ σ h + 1 ) Φ h T ( χ h ) Φ h ( χ h ) Θ ^ ˙ h + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 2 2 λ ( x 2 ) δ 0 .
The real control u and the adaptive law Θ ^ h are formulated as
u = 1 2 d h 2 z h σ σ h + 1 Θ ^ h Φ h T ( χ h ) Φ h ( χ h ) + Γ h z h σ h β h π ς T d z h ( 1 + ς / 2 ) ( σ + 1 ) ( σ σ h + 1 ) 1 σ ι ,
Θ ^ ˙ h = τ h 1 2 d h 2 z h 2 ( σ σ h + 1 ) Φ h T ( χ h ) Φ h ( χ h ) 2 ( e + e ˜ ) Θ ^ h ,
where β h = ( 3 n ) ς 2 ( σ σ ι + 2 ) ( 1 + ς / 2 ) , β ¯ h = 1 ( σ σ h + 2 ) ( 1 ς / 2 ) , and Γ h = β ¯ h π ς T d + 1 , and Θ ^ h ( 0 ) 0 .
By using (69) into (70), one has
V ˙ h κ = 1 h 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 h 1 β ¯ κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 h e + e ˜ τ κ Θ ˜ κ 2 Γ h z h σ + 1 β h π ς T d z h ( 1 + ς / 2 ) ( σ + 1 ) β ¯ h π ς T d z h ( 1 ς / 2 ) ( σ + 1 ) + e + e ˜ τ h Θ h * 2 g 0 δ 0 r 1 ( 1 + ς / 2 ) g ¯ 0 δ 0 r 1 ( 1 ς / 2 ) + β h π ς T d z h ( 1 ς / 2 ) ( σ + 1 ) + m h ( t 0 , t ) + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 ( z 1 / μ ) x 1 2 λ ( x 1 2 ) δ 0 + M h 1 + l h , 1 * + l h , 2 * + d h 2 2 + ( ε h * ) 2 2 .
From Lemma 1, we have
z h ( 1 ς / 2 ) ( σ + 1 ) ς T d Γ h β ¯ h π z h σ + 1 + ς 2 ς T d Γ h ( 1 ϖ / 2 ) β ¯ h π 1 2 / ς .
By using (44), (45), and (72) into (71), one has
V ˙ h κ = 1 h 1 β κ π ς T d z κ ( 1 + ς / 2 ) ( σ σ κ + 2 ) κ = 1 h 1 β ¯ κ π ς T d z κ ( 1 ς / 2 ) ( σ σ κ + 2 ) κ = 1 h e + e ˜ τ κ Θ ˜ κ 2 g 0 δ 0 r 1 + ( 1 + ς ) / 2 g ¯ 0 δ 0 r 1 ( 1 ς ) / 2 + M h + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 2 2 λ ( x 2 ) δ 0 ,
where
M h = m h ( t 0 , t ) + ( e + e ˜ ) Θ h * 2 2 τ h + β ¯ h π 2 T d ς T d Γ ¯ h ( 1 ς / 2 ) β ¯ h π 1 2 / ς + ( β h + β ¯ h ) π ς T d σ h 1 σ + 1 σ + 1 σ σ h + 2 σ σ h + 2 σ h 1
+ l h , 1 * + l h , 2 * + d h 2 2 + ( ε h * ) 2 2 + M h 1 .
Consider the complete Lyapunov function as
V = κ = 1 h z κ σ σ κ + 2 σ σ κ + 2 + κ = 1 h 1 2 τ κ Θ ˜ κ 2 + r δ 0 .
According to [39], there exists a positive constant Υ * such that the parameter estimation error satisfies Θ ˜ ι Υ * . Invoking Lemma 1 and choosing P = Θ ˜ ι , ϵ = = 1 , c ˜ = 2 ς , and d ˜ = ς , one has
2 ς 2 Θ ˜ ι 2 ( Θ ˜ ι 2 ) 1 ς / 2 + ς 2 ,
2 ς 2 Θ ˜ ι 2 ( Θ ˜ ι 2 ) 1 + ς / 2 + ς 2 ( Υ * ) 4 .
Based on the inequalities in [39], it follows that
κ = 1 h | x κ | L ˘ κ = 1 h | x κ | L ˘ , 0 < L ˘ 1 ,
κ = 1 h | x κ | L ˘ h 1 L ˘ κ = 1 h | x κ | L ˘ , 1 < L ˘ ,
where x κ R for all κ = 1 , 2 , , h .
By employing (75)–(78) and differentiating V, one obtains
V ˙ π ς T d κ = 1 h z κ σ σ κ + 2 σ σ κ + 2 + κ = 1 h Θ ˜ κ 2 2 τ κ + r δ 0 1 + ς / 2 π ς T d κ = 1 h z κ σ σ κ + 2 σ σ κ + 2 + κ = 1 h Θ ˜ κ 2 2 τ κ + r δ 0 1 ς / 2 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 ( z 1 / μ ) x 2 2 λ ( x 2 ) δ 0 + B ¯ h π ϖ d T V 1 + ϖ / 2 π ϖ d T V 1 ϖ / 2 + 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 ( z 1 / μ ) x 2 2 λ ( x 2 ) δ 0 + B h ,
where B ¯ h = h ( 3 n ) ς / 2 π 2 2 + ς / 2 τ h 1 + ς / 2 T d Υ * 4 + h π 2 2 ς / 2 τ h 1 ς / 2 T d + B h .
Theorem 1:
For the nonlinear system described in (1), suppose that Assumptions 1–4 hold. When the control inputs are designed according to (36), (54), and (69), and the adaptive update mechanisms are selected as in (37), (55), and (69), it follows that, starting from bounded initial states, every signal of the resulting closed-loop system remains bounded. Moreover, the tracking error is driven into a sufficiently small neighborhood of the origin within a user-prescribed finite time interval.
Proof 
From the Lyapunov-based analysis, it follows that the terms π ς T d V 1 + ς / 2 and π ς T d V 1 ς / 2 are negative definite. Moreover, B ¯ h is a bounded constant. The sign of the remaining term,
1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 2 2 λ ( x 2 ) δ 0 ,
is governed by the value of z 1 . Accordingly, the analysis is divided into the following cases.
Case 1: Consider z 1 Ω z 1 = { z 1 | z 1 | < 0.8814 μ } for any μ > 0 . Since z 1 = x 1 y r , the boundedness of z 1 together with the bounded reference signal y r guarantees that x 1 remains bounded. Furthermore, due to the smooth and nonnegative nature of x 2 2 , the term
1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ x 2 2 λ ( x 2 ) δ 0
is bounded. Let Ψ 0 denote its upper bound. Consequently, the time derivative of the Lyapunov function satisfies
V ˙ π ς T d V 1 + ς / 2 π ς T d V 1 ς / 2 + B * ,
where B * = B ¯ h + Ψ 0 .
Case 2: z 1 Ω z 1 . By Lemma 4, we have 1 ( σ σ 1 + 2 ) tanh σ σ 1 + 2 z 1 μ 0 .
Thus, the Lyapunov derivative satisfies
V ˙ π ς T d V 1 + ς / 2 π ς T d V 1 ς / 2 + B ¯ h .
Combining both cases yields
V ˙ π ς T d V 1 + ς / 2 π ς T d V 1 ς / 2 + B * .
It follows from (82) that the time derivative of V satisfies the structural condition given in (24) of Lemma 8. As a consequence, the developed control scheme guarantees practical predefined-time stability of the tracking error for system (1). In particular, the Lyapunov function is ultimately bounded as V < φ T d B * π , t > 2 T d .
Figure 1 presents the block level illustration of the proposed control architecture, offering a clear overview of the overall control structure.

4. Simulation Results

This section provides two illustrative examples to verify the effectiveness of the proposed control approach and to highlight its key characteristics.
Example 1:
Consider the high-order nonlinear system as
ξ ˙ = 2 ξ + 0.25 x 1 2 , x ˙ 1 = x 2 σ 1 + x 2 cos ( x 1 2 ) + sin ( x 1 x 2 ) sin 2 ( x 1 ) + 1 + Δ 1 , x ˙ 2 = u σ 2 t τ ( t ) + x 1 2 + x 1 x 2 2 + Δ 2 , y = x 1 ,
where f 1 ( x ) = x 2 cos ( x 1 2 ) + sin ( x 1 x 2 ) sin 2 ( x 1 ) + 1 , f 2 ( x ) = x 1 2 + x 1 x 2 2 , Δ 1 = 0.5 ξ 2 x 1 x 2 , Δ 2 = ξ 2 sin ( x 1 x 2 ) , σ 1 = 1 , σ 2 = 2 and consequently σ = max { σ 1 , σ 2 } = 3 . Additionally, the input delay is modeled by τ = 0.02 . The reference trajectory is selected as y d = sin ( 0.5 t ) . The initial conditions are chosen as x ι ( 0 ) = 0.5 , Θ ^ ι ( 0 ) = 0 , and r ( 0 ) = ξ ( 0 ) = , for ι = 1 , 2 . The design constants are set to T d = 2 , ς = 4 / 99 , τ ι = 0.5 , and δ 0 = 2 . The fuzzy logic systems employ Gaussian-type basis functions given by Φ 1 = exp ( x 1 i ) 2 2 and Φ 2 = exp ( x 1 i ) 2 2 ( x 2 j ) 2 2 , where the indices satisfy i , j , k { 5 , 4 , , 4 , 5 } . Define the nonlinear functions as Ψ 1 , 1 = 1 4 x 1 2 sin 2 ( x 1 ) , Ψ 2 , 1 = 1 4 x 1 2 x 2 2 , and Ψ 1 , 2 = Ψ 2 , 2 = ξ 2 . Under these selections, Assumption 1 is satisfied. To fulfill Assumption 2, choose the Lyapunov candidate V ( ξ ) = ξ 2 together with L ̲ ( ξ ) = 1 2 ξ 2 and L ¯ ( ξ ) = 3 2 ξ 2 . In accordance with Lemma 2, select g ̲ 0 = 3 δ 0 ς / 2 π ς T d , g ¯ 0 = j 0 ς 2 π ς T d , λ ( x 1 2 ) = 5 4 x 1 2 , ω ¯ = 14 25 . Consequently, the auxiliary dynamic signal r evolves according to r ˙ = g ̲ 0 r 1 + ς / 2 g ¯ 0 r 1 ς / 2 + 5 4 x 1 4 + 1 25 .
The first-step virtual controller α 1 is synthesized following the design in (36), while the real control signal u is generated in accordance with (69). The parameter estimation dynamics Θ ^ ˙ 1 and Θ ^ ˙ 2 are specified by the update laws given in (55).
The performance of the proposed adaptive control scheme is evaluated through the simulation results shown in Figure 2, Figure 3, Figure 4, Figure 5, Figure 6 and Figure 7. Figure 2 compares the system output y with the desired reference signal y r , from which it can be observed that the output accurately follows the reference trajectory, demonstrating satisfactory tracking behavior. The corresponding tracking error z 1 is shown in Figure 3, where it is seen to gradually decrease and remain confined within a small region near the origin, indicating successful achievement of the tracking objective. Figure 4 illustrates the time response of the state variable x 2 . The results indicate that x 2 stays within acceptable bounds throughout the simulation interval, which supports the stability of the closed loop system. The evolution of the estimated parameters Θ ^ 1 and Θ ^ 2 is presented in Figure 5. Their bounded and well behaved trajectories confirm the capability of the adaptive laws to compensate for parametric uncertainties. The control input u together with the delayed signal u ( t τ ) is shown in Figure 6. Both signals vary smoothly over time, demonstrating that the input delay does not induce oscillations or destabilizing effects. Finally, Figure 7 depicts the unmodeled dynamics ξ and r, which remain bounded during the entire simulation. Overall, these simulation outcomes verify that the proposed control framework ensures boundedness of all system signals while maintaining reliable and accurate tracking performance.
Example 2:
Consider a practical application involving a one-link robotic manipulator with motor dynamics, as investigated in [51]. The dynamic equations of the system are given by
D q ¨ + B q ˙ + N sin ( q ) = I + I d , M I ˙ + H I = K m q ˙ + V ,
where q, q ˙ , and q ¨ denote the link position, velocity, and acceleration, respectively. The variable I represents the generated motor torque, I d = sin ( q ˙ ) cos ( I ) denotes the disturbance torque, and V is the electromechanical control input. The system parameters are chosen as D = 1 kg · m 2 , B = 1 N · m · s / rad , N = 10 N · m , M = 0.3 H , H = 1.0 Ω , and K m = 2 N · m / A . It is assumed that the system is subject to input delay and unmodeled dynamics. Define the state variables as x 1 = q , x 2 = q ˙ , x 3 = I / D , and the delayed control input as u t τ = V t τ ( t ) / ( D M ) .
Then, the system (84) can be transformed as
ξ ˙ = 2 ξ + 0.25 x 1 2 , x ˙ 1 = x 2 σ 1 + Δ 1 , x ˙ 2 = x 3 σ 2 N D sin ( x 1 ) B D x 2 + 1 D sin ( x 2 ) cos ( D x 3 ) + Δ 2 , x ˙ 3 = K m M D x 2 H M D x 3 + u σ 2 t τ ( t ) + Δ 3 , y = x 1 ,
where f 1 ( x ) = 0 , f 2 ( x ) = N D sin ( x 1 ) B D x 2 + 1 D sin ( x 2 ) cos ( D x 3 ) , f 3 ( x ) = K m M D x 2 H M D x 3 , Δ 1 = ξ x 1 x 2 x 3 , Δ 2 = ξ x 2 cos ( x 1 x 2 ) , Δ 3 = ξ x 3 sin ( x 1 x 2 ) , σ 1 = 1 , σ 2 = 1 , σ 3 = 3 , and consequently σ = max { σ 1 , σ 2 , σ 3 } = 3 . Additionally, the input delay is modeled by τ = 0.02 .
The reference trajectory is selected as y r = 0.5 ( sin ( t ) ) . The initial states and parameter estimates are chosen as x ι ( 0 ) = 0.5 , Θ ^ ι ( 0 ) = 0 , and r ( 0 ) = ξ ( 0 ) = 0 , for ι = 1 , 2 , 3 . The design constants are set to T d = 2 , ς = 4 / 99 , τ ι = 0.5 , and δ 0 = 2 .
The fuzzy logic systems employ Gaussian-type basis functions given by Φ 1 = exp ( x 1 i ) 2 2 , Φ 2 = exp ( x 1 i ) 2 2 ( x 2 j ) 2 2 , Φ 3 = exp ( x 1 i ) 2 2 ( x 2 j ) 2 2 ( x 3 k ) 2 2 , where the indices satisfy i , j , k { 5 , 4 , , 4 , 5 } .
Define the nonlinear functions as Ψ 1 , 1 = 1 4 x 1 2 sin 2 ( x 1 ) , Ψ 2 , 1 = 1 4 x 1 2 x 2 2 , Ψ 3 , 1 = 1 4 x 3 2 cos 2 ( x 1 x 2 ) , and Ψ 1 , 2 = Ψ 2 , 2 = Ψ 3 , 2 = ξ 2 . Under these selections, Assumption 1 is satisfied. To fulfill Assumption 2, choose the Lyapunov candidate V ( ξ ) = ξ 2 together with L ̲ ( ξ ) = 1 2 ξ 2 and L ¯ ( ξ ) = 3 2 ξ 2 . In accordance with Lemma 2, select g ̲ 0 = 3 δ 0 ς / 2 π ς T d , g ¯ 0 = j 0 ς 2 π ς T d , λ ( x 1 2 ) = 5 4 x 1 2 , ω ¯ = 14 25 . Consequently, the auxiliary dynamic signal r evolves according to r ˙ = g ̲ 0 r 1 + ς / 2 g ¯ 0 r 1 ς / 2 + 5 4 x 1 4 + 1 25 .
The first-step virtual controllers α 1 and α 2 are synthesized following the design in (54), while the real control signal u is generated in accordance with (69). The parameter estimation dynamics Θ ^ ˙ 1 , Θ ^ ˙ 2 and Θ ^ ˙ 3 are specified by the update laws given in (55). The performance of the proposed adaptive control method is evaluated through the simulation results depicted in Figure 8, Figure 9, Figure 10, Figure 11, Figure 12 and Figure 13. Figure 8 presents the time responses of the system output y along with the desired reference signal y r , showing close agreement and indicating that the controller achieves precise output tracking. The associated tracking error z 1 is shown in Figure 9, where it gradually decreases and remains within a small neighborhood of the origin, confirming the successful achievement of the tracking objective. The temporal behaviors of the state variables x 2 and x 3 are illustrated in Figure 10, demonstrating that both states remain bounded over the entire simulation period, which validates the stability of the closed-loop system under the proposed controller. Figure 11 depicts the evolution of the estimated adaptive parameters Θ ^ 1 , Θ ^ 2 , and Θ ^ 3 , whose bounded and smooth trajectories confirm the effectiveness of the adaptive laws in handling parametric uncertainties. Figure 12 compares the control input u with the delayed input u ( t τ ) , and the smooth variations of these signals indicate that input delays do not introduce instability or undesirable oscillations. Finally, Figure 13 shows the unmodeled dynamics ξ and r, which remain bounded throughout the simulation, further illustrating the robustness of the proposed approach. Collectively, these simulation results demonstrate that the developed control strategy ensures boundedness of all system signals while achieving accurate and reliable tracking performance.

5. Conclusions

This study has investigated the design of a predefined-time adaptive fuzzy control scheme for high-order nonlinear systems with nonstrict-feedback structures, considering the presence of unmodeled dynamics and input delays. To compensate for the effects of unmodeled dynamics, a predefined-time auxiliary dynamic signal was incorporated, while the impact of input delays was alleviated using a Padé approximation in conjunction with an intermediate variable. Fuzzy logic systems were utilized to approximate the unknown nonlinear functions, thereby reducing reliance on an accurate mathematical model of the system. By integrating the recursive backstepping technique with a power-type Lyapunov function framework, an adaptive fuzzy predefined-time tracking controller was developed. A comprehensive analytical study establishes that the designed feedback dynamics ensure practical predefined-time convergence of the closed-loop system, while suitable adjustment of the controller gains confines the tracking deviations within a small vicinity of the equilibrium point. The effectiveness and advantages of the proposed control strategy were further validated through simulation examples. Future research will focus on extending the proposed predefined-time adaptive fuzzy control framework to more complex system classes, such as switched stochastic nonlinear systems. In such systems, random disturbances, stochastic uncertainties, and switching behaviors coexist, posing significant challenges to stability analysis and controller design. Incorporating predefined-time performance guarantees under stochastic effects and switching signals, while accounting for unmodeled dynamics and input delays, remains an open and meaningful research direction. Additionally, event-triggered mechanisms and network-induced constraints will be considered to improve communication efficiency and practical implementability in large-scale and distributed control systems.

Author Contributions

Mohamed Kharrat : Writing – original draft, Supervision, Paolo Mercorelli: Writing – review & editing. All authors have read and agreed to the published version of the manuscript.

Data Availability Statement

No data were used for the research described in the article.

Conflicts of Interest

The authors declare no conflicts of interest.

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Figure 1. Block diagram depicting the structure of the developed control architecture.
Figure 1. Block diagram depicting the structure of the developed control architecture.
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Figure 2. Trajectories of y and y r .
Figure 2. Trajectories of y and y r .
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Figure 3. The trajectory of the tracking error z 1 .
Figure 3. The trajectory of the tracking error z 1 .
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Figure 4. State variables x 2 .
Figure 4. State variables x 2 .
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Figure 5. Adaptive laws Θ ^ 1 and Θ ^ 2 .
Figure 5. Adaptive laws Θ ^ 1 and Θ ^ 2 .
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Figure 6. System input u ( t τ ) and control input u.
Figure 6. System input u ( t τ ) and control input u.
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Figure 7. Trajectories of ξ and r.
Figure 7. Trajectories of ξ and r.
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Figure 8. Trajectories of y and y r .
Figure 8. Trajectories of y and y r .
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Figure 9. The trajectory of the tracking error z 1 .
Figure 9. The trajectory of the tracking error z 1 .
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Figure 10. State variables x 2 and x 3 .
Figure 10. State variables x 2 and x 3 .
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Figure 11. Adaptive laws Θ ^ 1 , Θ ^ 2 , and Θ ^ 3 .
Figure 11. Adaptive laws Θ ^ 1 , Θ ^ 2 , and Θ ^ 3 .
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Figure 12. Control input u and system input u ( t τ ) .
Figure 12. Control input u and system input u ( t τ ) .
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Figure 13. Trajectories of ξ and r.
Figure 13. Trajectories of ξ and r.
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