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Research article

Practical stability for nonlinear systems with generalized conformable derivative

  • Received: 04 March 2023 Revised: 18 April 2023 Accepted: 20 April 2023 Published: 27 April 2023
  • MSC : 34A34, 34A08

  • In this study, we give the stability analysis of a class of nonlinear systems with a generalized conformable derivative, which guarantees that their solutions converge to a ball centered at the origin. The theoretical foundations of the practical stability are investigated in this work. Furthermore, the concept is elucidated with an application. Finally, the theoretical findings offered are illustrated with two numerical examples.

    Citation: Mohammed Aldandani, Omar Naifar, Abdellatif Ben Makhlouf. Practical stability for nonlinear systems with generalized conformable derivative[J]. AIMS Mathematics, 2023, 8(7): 15618-15632. doi: 10.3934/math.2023797

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  • In this study, we give the stability analysis of a class of nonlinear systems with a generalized conformable derivative, which guarantees that their solutions converge to a ball centered at the origin. The theoretical foundations of the practical stability are investigated in this work. Furthermore, the concept is elucidated with an application. Finally, the theoretical findings offered are illustrated with two numerical examples.



    As the effectiveness of data systems continues to improve, more and more mathematical approaches are being applied to real-world applications to yield exceptional outcomes. Fractional approaches, such as fractional calculus, fractional Fourier analysis, and the linear canonical transform, are gaining importance in the field of mathematics and among applied mathematicians. The theory and method of fractional domain analysis may further define the dynamic process of signal translation from the time domain to the frequency domain, thereby creating a new avenue for non-stationary signal analysis and treatment studies. In technical domains, such as radar, communications, and sonar, fractional approaches are preferred over traditional integral methods because they bring novel concepts, procedures, and ideas [1,2,3,28,29,30,31,33]. Due to the unpredictability of signals in actual engineering systems and the effects of different disturbances and noises on the transmission process, despite the numerous benefits of these new fractional approaches, there are still critical issues that need to be resolved. Additionally, fractional theory is confronted with several practical limitations in engineering, such as sampling and filtering in the sphere of multidimensional signals.

    Lyapunov stability is a fundamental concept in control theory and plays a significant role in the analysis of fractional order systems. Lyapunov stability analysis of fractional order systems aims to establish the stability of a system by determining whether its trajectory remains within a certain region of the state space. Unlike integer-order systems, fractional order systems exhibit complex behaviors, such as memory effects, non-locality, and infinite-dimensional dynamics, which make their stability analysis more challenging. In the past few decades, several Lyapunov stability criteria have been proposed for fractional order systems, including algebraic, geometric, and analytical methods. These criteria have been used to establish practical stability, asymptotic stability, uniform stability, and robust stability for fractional order systems. Despite the progress made in the field, the Lyapunov stability analysis of fractional order systems remains an active area of research with significant potential for future advancements [38,39]. However, Khalil et al. [4,20] presented a new derivative called the conformable Fractional Derivative (FD), which goes beyond the conventional limit definitions of derivatives. Some theorems of classical calculus require alternate expansions for fractional differential models, and this idea makes that possible. Academics find the conformable derivative intriguing since it appears to possess all the features of the conventional derivative [5], and it makes computations easier with FD formulas. There are now several applications of this novel idea. In fact, a new exact solution was presented for Burgers-type equations with conformable derivatives in [6], and [7] investigates the time scales method of dealing with conformable derivatives. Additionally, parameter variation was investigated in this work [8]. The Fractional Fourier series is also addressed in the publication [9], and new conformable derivative properties are described in study [10]. Conversely, [11] looks at a generalization of the classical conformable fractional derivative and establishes the Generalized Fractional Derivative (GCD) as a new class of fractional derivatives. Several examples in research show that the solution to the diffusion equation is unique (see [12]). Multi-agent systems with impulsive control protocols [13], numerical methods [14], the time power-based grey model [15], the multivariate grey system model [16], controllability and observability [17], the Barbalat Lemma [18], H infinite observers [19], exponential quasi-synchronization [21], partial practical stability [22], stability analysis depending on a parameter [23] are just a few examples of recent research that have expanded on the GCD. Numerous recent research articles highlight the significance of the conformable derivative in tackling a wide range of issues in science and engineering, demonstrating its widespread applicability [32,34,35]. However, the conformable derivative has not yet been fully investigated, and there are still unanswered questions about it.

    On the other hand, the definition of practical stability for nonlinear systems is widely utilized to demonstrate the stability of such systems, where the state converges towards an arbitrarily small neighborhood of the origin. Various authors have developed the concept of practical stability, as shown in references [36,37]. This notion is especially significant in engineering applications when there are unpredictable, time-varying, or unbounded external inputs or disturbances that might create instability and oscillations. If the system's trajectories wobble around an unstable route in this case, the best course of action is to guarantee that the system's performance is still acceptable in a practical sense. This means that if the starting values of the external disturbances are constrained, the deviations of the system's motion from equilibrium should remain within specified boundaries given by the physical circumstances, resulting in the system being stable. The concept of practical stability has been extended to fractional order systems, and has been shown to be an effective tool for analyzing the stability of such systems, particularly when traditional methods may be insufficient, see for example [24,25]. In fact, work [25] explores the notion of practical stability for a class of general conformable nonlinear systems. For a certain class of fractional-order nonlinear systems, Makhlouf in [22] has developed a stability analysis that guarantees convergence of certain solutions towards a ball.

    In this study, we have conducted a theoretical investigation of the practical stability analysis for a class of nonlinear systems with a generalized conformable derivative, a topic that has not been previously addressed in the literature. Our main contribution is providing detailed descriptions of practical uniform stability and practical global uniform asymptotic stability results for the proposed system. To demonstrate the validity of our theoretical findings, we have applied the approach to a specific nonlinear system with generalized conformable derivative. Additionally, we have provided a numerical simulation to show the effectiveness of the proposed approach in practice. Overall, our study offers a novel and comprehensive approach to practical stability analysis for nonlinear systems with generalized conformable derivative.

    Driven by the foregoing interpretations, our study is summarized by the following key points:

    ● To the best of our knowledge, there are no published papers that address the fundamental and theoretical analysis of practical stability of nonlinear systems with a generalized conformable derivative.

    ● We provide a detailed description of practical uniform stability and practical global uniform asymptotic stability results.

    ● An application of the practically globally uniformly asymptotically stable result is presented to illustrate the validity of the theoretical findings.

    ● We also provide two numerical examples with simulation results to demonstrate the effectiveness of the proposed results.

    We begin by giving some definitions and preliminary results (see [4,7,11,12]).

    Definition 2.1. Let h be a function defined on [z1,z2) so, the GCD of h is defined by

    Tβ,ϕz1z1h(s)=limτ0h(s+τϕz1(s,β))h(s)τ, (2.1)

    for all s>z1, where β(0,1] and ϕz1(s,β) is a positive function and satisfies

    ϕz1(.,β1)ϕz1(.,β2),

    where β1β2 and β1, β2(0,1], ϕz1(s,1)=1.

    If Tβ,ϕz1z1h(s) exists, for every s(z1,z), for some z>z1 and limsz1+Tβ,ϕz1z1h(s) exists, then, by definition

    Tβ,ϕz1z1h(z1):=limsz1+Tβ,ϕz1z1h(s).

    Remark 2.1. As a further analysis of GCD's properties, we assume that ϕz1(s,β)>0, for all s>z1, 1ϕz1(.,β) is locally integrable and

    sz11ϕz1(u,β)dug(sz1),

    where g is a positive function with

    limtg(t)=.

    Definition 2.2. For 0<β<1, the general Conformable Integral (CI) of a continuous function h is given by

    Iβ,ϕz1z1h(s)=sz1h(l)ϕz1(l,β)dl. (2.2)

    Lemma 2.1. Let h be a continuous function on [z1,z2]. Therefore

    Tβ,ϕz1z1Iβ,ϕz1z1h(s)=h(s),

    for every sz1.

    Definition 2.3. It is said that a function ϖC(R+,R+) belongs to class K if ϖ(0)=0 and it is strictly increasing. It will belong to class K if it in addition limz+ϖ(z)=+.

    Lemma 2.2. [27] If ϖK, then for every d1,d2R+, we have

    ϖ(d1+d2)ϖ(2d1)+ϖ(2d2).

    Lemma 2.3. [26] For every d1,d20 and q1, we have

    (d1+d2)q2q1(dq1+dq2)

    and

    (d1+d2)1q(d1q1+d1q2).

    In this section, the following parameterized differential equations with GCD derivatives are considered:

    Tβ,ϕr0r0x(t)=f(t,x,ι), tr0, x(r0)=x0, (3.1)

    where r0R+, ιR+ and f(.,.,ι)C(R+×Rn,Rn). We denote by xι(t;r0,x0) the solution of the system (3.1). For m>0, we write x=(y,z), zRp, yRm.

    Definition 3.1. The system (3.1) is called ι-y-practically uniformly stable (ι-y-PUS), if for each l2>0 there is l1>0 and ˆι(0,ι] such that for every r0R+, for every x0Rn with x0<l1 and for every ι(0,ˆι], yι(t;r0,x0)<l2 for every tr0.

    Definition 3.2. The system (3.1) is called ι-y-practically uniformly bounded (ι-y-PUB), if for each l1>0, there is l2>0 and ˆι(0,ι] such that for every r0R+, for every x0Rn with x0<l1 and for each ι(0,ˆι], yι(t;r0,x0)<l2 for every tr0.

    Definition 3.3. The system (3.1) is called ι-y-globally uniformly practically attractive (ι-y-GUPA), if for each l1>0, l2>0 there is T>0 and ˆι(0,ι] such that for every r0R+, for every x0Rn with x0<l1 and for every ι(0,ˆι], yι(t;r0,x0)<l2 for every tr0+T.

    Definition 3.4. The system (3.1) is called ι-y-practically globally uniformly asymptotically stable (ι-y-PGUAS), if it is ι-y-PUS, ι-y-PUB and ι-y-GUPA.

    Definition 3.5. The system (3.1) is called ι-y-practically uniformly exponentially stable (ι-y-PUES), if for every 0<ιι there is positive scalars C(ι), δ(ι) and ϱ(ι) such that:

    yι(t;r0,x0)C(ι)x0Eϕr0β(δ(ι),t,r0)+ϱ(ι), tr00, (3.2)

    where

    Eϕr0β(δ,t,r0)=eδtr01ϕr0(s,β)ds

    with ϱ(ι)0 as ι0+ and there is C, δ1, δ2>0, such that δ1δ(ι)δ2 and 0<C(ι)C for every ι(0,ι].

    Theorem 3.1. Let ι>0. Suppose that for every 0<ιι, there is a C1 function Vι: R+×RnR, class K functions ϖj, (j=1,2), θC(R+,R+) and constants ς1(ι)>0, ς2(ι)>0, r1(ι)>0 and r2(ι)>0 such that

    (1)

    ς1(ι)ϖ1(y)Vι(t,x)ς2(ι)ϖ2(γ)+r1(ι), xRn, t0. (3.3)

    (2)

    Tβ,ϕr0r0Vι(t,xι(t;r0,x0))θ(t)r2(ι), tr00, (3.4)

    where γ=(x1,x2,...,xk), mkn, with

    ι(0,ι], 0<ς2(ι)ς1(ι)K, where K>0.

    ● There is M>0, such that

    tr01ϕr0(s,β)θ(s)dsM, tr00.

    d(ι)0 as ι0+, where

    d(ι)=(r1(ι)+Mr2(ι))ς1(ι).

    Then, the system (3.1) is ι-y-PUS. Moreover, if ϖjK,(j=1,2), therefore, the system (3.1) is ι-y-PUB.

    Proof. Let l2>0. We consider l1>0 and ˆι(0,ι], such that

    ϖ2(l1)<ϖ1(l2)2K

    and

    r1(ι)+r2(ι)Mς1(ι)<ϖ1(l2)2, ι(0,ˆι].

    It follows from (3.3) and (3.4) that

    Vι(t,xι(t;r0,x0))Vι(r0,x0)+r2(ι)tr01ϕr0(s,β)θ(s)dsς2(ι)ϖ2(x0)+r1(ι)+r2(ι)M. (3.5)

    For x0Rn, with x0<l1, we get Then,

    ϖ1(yι(t;r0,x0))ς2(ι)ς1(ι)ϖ2(x0)+r1(ι)+r2(ι)Mς1(ι)Kϖ2(l1)+r1(ι)+r2(ι)Mς1(ι)<ϖ1(l2), tr0. (3.6)

    Thus,

    yι(t;r0,x0)<l2, tr0.

    Therefore, the system (3.1) is ι-y-PUS. We now consider the case where ϖjK,(j=1,2).

    Let l1>0. Take ˆι1(0,ι] such that

    r1(ι)+r2(ι)Mς1(ι)<1, ι(0,ˆι1].

    In this case (3.6) becames:

    ϖ1((yι(t;r0,x0))<Kϖ2(l1)+1.

    Then,

    yι(t;r0,x0)<ϖ11(Kϖ2(l1)+1), tr0.

    Hence, the system (3.1) is ι-y-PUB.

    Remark 3.1. In Theorem 3.1, if γ=y=x, we get the practical uniform stability and the practical uniform boundedness of the solutions of the system (3.1).

    Theorem 3.2. Let ι>0. Suppose that for every 0<ιι, there is a C1 function Vι: R+×RnR, class K functions ϖj, (j=1,2), θC(R+,R+) and constants ς1(ι)>0, ς2(ι)>0, ς3(ι)>0, r1(ι)>0 and r2(ι)>0 such that

    (1)

    ς1(ι)ϖ1(y)Vι(t,x)ς2(ι)ϖ2(γ)+r1(ι), xRn, t0. (3.7)

    (2)

    Tβ,ϕr0r0Vι(t,xι(t;r0,x0))ς3(ι)ϖ2(γι(t;r0,x0)))+θ(t)r2(ι), tr00, (3.8)

    where γ=(x1,x2,...,xk), mkn, with

    ι(0,ι], ς3(ι)ς2(ι)c and 0<ς2(ι)ς1(ι)Ψ, with c, Ψ>0.

    ● There is M1>0, such that

    tr01ϕr0(s,β)Eϕr0β(c,t,r0)Eϕr0β(c,s,r0)θ(s)dsM1, tr00.

    d(ι)0 as ι0+, where

    d(ι)=r1(ι)(ς2(ι)+Mς3(ι))ς1(ι)ς2(ι)+r2(ι)Mς1(ι),

    with M=M1+1c.

    Therefore, the system (3.1) is ι-y-PGUAS.

    Proof. From Eqs (3.7) and (3.8) we give:

    Tβ,ϕr0r0Vι(t,xι(t;r0,x0))cVι(t,xι(t;t0,x0))+ς3(ι)ς2(ι)r1(ι)+θ(t)r2(ι)cVι(t,xι(t;r0,x0))+ϱ(t)l(ι), tr0, (3.9)

    where

    ϱ(t)=(1+θ(t))

    and

    l(ι)=r1(ι)ς3(ι)ς2(ι)+r2(ι).

    Using Lemma 1 in [25], we get

    Vι(t,xι(t;r0,x0))Eϕr0β(c,t,r0)Vι(r0,x0)+Ml(ι),  tr0.

    By (3.7), we get

    ϖ1(yι(t;r0,x0))1ς1(ι)Eϕr0β(c,t,r0)(ς2(ι)ϖ2(x0)+r1(ι))+Ml(ι)ς1(ι). (3.10)

    Then,

    ϖ1(yι(t;r0,x0))ς2(ι)ς1(ι)Eϕr0β(c,t,r0)ϖ2(x0)+d(ι). (3.11)

    Using Lemma 2.2, we get

    yι(t;r0,x0)ϖ11(2ΨEϕr0β(c,t,r0)ϖ2(x0))+ϖ11(2d(ι)). (3.12)

    Let l2>0. From (3.12), we get

    yι(t;r0,x0)ϖ11(2Ψϖ2(x0))+ϖ11(2d(ι)). (3.13)

    We have

    limr0ϖ11(2Ψϖ2(r))=0

    and

    limι0ϖ11(2d(ι))=0,

    then, there is l1>0 and ˆι(0,ι], such that

    yι(t;r0,x0)<l2,  tr0,  x0<l1,  ι(0,ˆι).

    Therefore, the system (3.1) is ι-y-PUS.

    Let d1>0, we have

    limι0ϖ11(2d(ι))=0,

    then, there exists ˆι1>0, such that

    yι(t;r0,x0)<ϖ11(2Ψϖ2(d1))+1,   x0<d1,  ι(0,ˆι1).

    Therefore, the system (3.1) is ι-y-PUB.

    Let δ1>0, δ2>0. Let x0Rn such that x0<δ1. It follows from (3.12) that

    yι(t;r0,x0)ϖ11(2ΨEϕr0β(c,t,r0)ϖ2(δ1))+ϖ11(2d(ι)).

    We have

    limt+g(t)=0,

    then there exist T>0 and ˆι2>0 such that

    yι(t;r0,x0)<δ2,   tr0T, ι(0,ˆι2).

    Therefore, the system (3.1) is ι-y-GUPA. Thus, the system (3.1) is ι-y-PGUAS.

    Remark 3.2. In Theorem 3.2, if γ=y=x, we get the practical global uniform asymptotic stability of the system (3.1).

    Remark 3.3. In Theorem 3.2, if we have

    ϖ1(z)=p1zq

    and

    ϖ2(z)=p2zq

    with p1,p2>0 and q1, then the system (3.1) is ι-y-PUES.

    In this section, we examine a class of system that can be modelled by the following system:

    Tβ,ϕr0r0x(t)=Ax(t)+ξ(t,x), tr0, y=Cx, (4.1)

    where ARn×n,CRp×n and ξ: R+×RnRn.

    We now focus on the most important assumptions made in the observer stability proof, with respect to the system described by (4.1).

    (H1) Suppose that (A,C) is observable, Consequently, there exists a matrix L of dimension n×p for which the eigenvalues of the matrix A0=ALC are in the open-left-half plane.

    (H2) There exists a p×1 function w(t,x) that verify:

    Pξ(t,x)=CTw(t,x), (4.2)

    where PRn×Rn and PT=P, such that

    AT0P+PA0=2Q, (4.3)

    with QT=Q>0.

    (H3) There exist a positive scalar function α(t,y) such that

    w(t,x)α(t,y). (4.4)

    (H4) There is M1>0 such that

    tr01ϕr0(s,β)Eϕr0β(λmin(Q)2λmax(P),t,r0)Eϕr0β(λmin(Q)2λmax(P),s,r0)θ(s)dsM1, tr00. (4.5)

    To recap, our goal is to create an observer that can make estimates of the states x(t;r0,x0) described in (4.1). Our proposed observer for this purpose is as follows:

    Tβ,ϕr0r0ˆx(t)=A0ˆx+Ly+u, (4.6)

    where ˆxRn is the estimated vector of x and the control uRn is defined as

    u=P1CTCeα2(t,y)Ceα(t,y)+ιθ(t), (4.7)

    with ι>0, θ(t) is a positive continuous function and e=xˆx denote the vector error.

    Before establishing the stability result for the suggested observer, we initially develop the dynamics of the observation error. We get:

    Tβ,ϕr0r0e(t)=A0e+ξ(t,x)u. (4.8)

    The following stability theorem is now stated.

    Theorem 4.1. Under assumptions (H1)(H4) the observation error (4.8) is ι-e-PGUAS.

    Proof. Let the Lyapunov function V be

    V=12eTPe. (4.9)

    We obtain by considering the time derivative of V along the trajectory of the specified observation error system:

    Tβ,ϕr0r0V(t,eι(t;r0,e0))=eι(t;r0,e0)TQeι(t;r0,e0)+eι(t;r0,e0)TP(ξ(t,x(t;r0,x0))u). (4.10)

    Substituting (4.2) and (4.7) into (4.10) yields

    Tβ,ϕr0r0V(t,eι(t;r0,e0))=eι(t;r0,e0)TQeι(t;r0,e0)+eι(t;r0,e0)TP(P1CTw(t,x(t;r0,x0)P1CTCeι(t;r0,e0)α2(t,y)Ceι(t;r0,e0)α(t,y)+ιθ(t)). (4.11)

    Then, the following upper bound on Tβ,ϕr0r0V(t) is obtained:

    Tβ,ϕr0r0V(t,eι(t;r0,e0))ceι(t;r0,e0)2+Ceι(t;r0,e0)α(t,y)Ceι(t;r0,e0)2α2(t,y)Ceι(t;r0,e0)α(t,y)+ιθ(t), (4.12)

    where c=λmin(Q).

    By getting a common denominator for the final two components in Eq (4.12), the upper bound on Tβ,ϕr0r0V is reduced to be as follows:

    Tβ,ϕr0r0V(t,eι(t;r0,e0))ceι(t;r0,e0)2+ιCeι(t;r0,e0)α(t,y)θ(t)Ceι(t;r0,e0)α(t,y)+ιθ(t). (4.13)

    Therefore,

    Tβ,ϕr0r0V(t,eι(t;r0,e0))ceι(t;r0,e0)2+ιθ(t). (4.14)

    It follows from Theorem 3.2 that the system (4.8) is ι-e-PGUAS.

    Remark 4.1. The above theorem discusses the application of an observer design for a class of generalized conformable fractional-order nonlinear systems with a practical stability result.

    Example 5.1. Let us consider the following system

    Tβ,ϕr0r0x1(t)=x1+sin(x2)2x1+ι2et21+x21,Tβ,ϕr0r0x2(t)=x2+cos(x3)2x2+ι2et21+x22,Tβ,ϕr0r0x3(t)=5x3, (5.1)

    where x=(x1,x2,x3)R3.

    Let

    V(t,x)=x21+x222.

    We get

    Tβ,ϕr0r0V(t,x(t;r0,x0))x1(t;r0,x0)Tβ,ϕr0r0x1(t;r0,x0)+x2(t;r0,x0)Tβ,ϕr0r0x2(t;r0,x0)x21+x222+ι2et2. (5.2)

    According to Theorem 3.2 the system (5.1) is ι-(x1,x2)-PGUAS.

    In Figure 1, there is a representation of the computed numerical solutions for the state x1 and x2 of a particular system described by Eq (5.1). The graph in Figure 1 illustrates how the state x1 and x2 of the system changes over time, providing the result of Theorem 3.2.

    Figure 1.  The evolution of (x1,x2) for r0=0, β=0.7, ϕr0(s,β)=(sr0)1β and ι=0.1.

    Example 5.2. Let us consider the system (4.1) for

    A=(1122),  C=(10)

    and

    ξ(t,x)=(cos(x2)x1,0).

    One choose

    Q=(1112)

    and by solving the Lyapunov equation, one gets

    P=(1001)

    and

    L=(01).

    Thus, (H2) is verified with w(t,x)=cos(x2)x1. Also, (H3) is verified with α(t,y)=|x1|.

    Our proposed observer for this purpose is as follows:

    Tβ,ϕr0r0ˆx(t)=A0ˆx+Ly+u,

    where

    A0=(1112)

    and u is defined as

    u=(e1x21|e1||x1|+ιθ(t)0),

    where e1=x1ˆx1 and θ(t)=1.

    According to Theorem 4.1 the error system is ι-e-PGUAS. The numerical solutions of the error system are illustrated in Figures 2 and 3. In this case, according to Figures 2 and 3, we can see the convergence of the solution towards a small ball centered at the origin.

    Figure 2.  The evolution of the error e1 for r0=0, β=0.5, ϕr0(s,β)=(sr0)1β and ι=0.01.
    Figure 3.  The evolution of the error e2 for r0=0, β=0.5, ϕr0(s,β)=(sr0)1β and ι=0.01.

    In this paper, we analyze the stability of a class of nonlinear systems with a generalized conformable derivative, which ensures that their solutions converge to a ball centered at the origin. In this paper, the theoretical underpinnings of practical stability are addressed. In addition, the notion is illustrated by an application. Finally, the presented theoretical insights are demonstrated by a numerical example that corresponds to the selected application.

    The authors declare that there are no conflicts of interest.



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