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Research article

Neuro-adaptive finite-time control of fractional-order nonlinear systems with multiple objective constraints

  • Received: 17 May 2023 Revised: 19 June 2023 Accepted: 17 July 2023 Published: 19 December 2023
  • This paper presents a neuro-adaptive finite-time control strategy for uncertain nonstrict-feedback fractional-order nonlinear systems with multiple-objective constraints. To stabilize the uncertain nonlinear fractional-order systems, neural networks (NNs) are employed to identify the unknown nonlinear functions, and dynamic surface control is used to avoid the computational complexity of the backstepping design procedure. The effect caused by the algebraic loop problem can be solved via establishing fractional-order adaptive laws. Introducing a new barrier function, the system output is always limited to the predefined time-varying acceptable range while effectively solving the multi-objective constraint problem. Utilizing fractional-order finite-time stability theory, a finite-time control scheme is constructed to drive the system output to the reference signal in finite time, which ensures better tracking performance. Two examples are given to illustrate the availability and superiority of the presented control scheme.

    Citation: Lusong Ding, Weiwei Sun. Neuro-adaptive finite-time control of fractional-order nonlinear systems with multiple objective constraints[J]. Mathematical Modelling and Control, 2023, 3(4): 355-369. doi: 10.3934/mmc.2023029

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  • This paper presents a neuro-adaptive finite-time control strategy for uncertain nonstrict-feedback fractional-order nonlinear systems with multiple-objective constraints. To stabilize the uncertain nonlinear fractional-order systems, neural networks (NNs) are employed to identify the unknown nonlinear functions, and dynamic surface control is used to avoid the computational complexity of the backstepping design procedure. The effect caused by the algebraic loop problem can be solved via establishing fractional-order adaptive laws. Introducing a new barrier function, the system output is always limited to the predefined time-varying acceptable range while effectively solving the multi-objective constraint problem. Utilizing fractional-order finite-time stability theory, a finite-time control scheme is constructed to drive the system output to the reference signal in finite time, which ensures better tracking performance. Two examples are given to illustrate the availability and superiority of the presented control scheme.



    In recent years, fractional-order calculus has received increasing attention since it describes actual systems more effectively than integral order calculus. Fractional-order calculus is a generalized calculation of traditional integer-order calculus. Notably, fractional-order systems have potential benefits and design flexibility, which can accurately characterize many physical phenomena, such as electromagnetic waves, viscoelastic materials models and chaotic systems [1,2]. Recently, some research outcomes were reported on fractional-order nonlinear system control [3,4]. Due to the presence of fractional-order derivatives and uncertain nonlinearities, almost all control methods currently in effective use for integer-order nonlinear systems cannot be readily extended to fractional-order nonlinear systems.

    The backstepping control methodology is one of the most commonly used approaches for nonlinear systems. Specifically, NNs and fuzzy logic systems (FLSs) have become popular tools for modeling and controlling nonlinear systems due to their superior approximation properties [5,6]. Motivated by these results, some advanced adaptive intelligent control approaches are applied to the control of fractional-order nonlinear systems [7,8]. In [7], an adaptive fuzzy controller was constructed using the backstepping recursive technique to deal with unknown external disturbances of strict-feedback fractional-order nonlinear systems. Motivated by [7], a fractional-order filter-based dynamic surface control scheme was presented in [8] to solve the "complexity explosion". Many efforts are being made to investigate intelligent adaptive control for fractional-order nonlinear systems, including output-feedback control [9], optimal control [10] and input nonlinearities (for example, input saturation, dead zone and hysteresis [11,12]). However, the aforementioned results can only guarantee the convergent time tends to infinity.

    Generally speaking, for many practical engineering applications, the study of finite-time stability is of greater significance compared to infinite-time stability since finite-time control has better fast transient performance and better robustness to uncertainties [13,14]. Note that the studies of finite-time stability for fractional-order nonlinear systems has produced some achievements. In [15], a finite time adaptive fuzzy controller was constructed using a sliding mode technique to cope with the finite-time stabilization problem for fractional-order nonlinear systems. Then, [16] introduced a fractional command filter to reduce the influence of filtering errors on control performance based on [15]. A class of adaptive event triggered finite time control problems was investigated in [17], and a new fractional-order finite time stability criterion was established. It is noteworthy that the above research ignores the impact of constraints.

    There always exist some constraints in engineering applications because of physical limitations or safety considerations. If these constraints are not handled appropriately, it might lead to the decline of control performance and even system stability. Some researchers have recently addressed the nonlinear constraint control problem using the barrier Lyapunov function (BLF) [18,19] or a nonlinear state-dependent transformation [20]. Note that [18,19,20] only applies to integer-order systems due to the complexity of fractional calculus. As a backdrop, the constraint problem of fractional-order nonlinear systems is a fascinating and challenging task. By incorporating a BLF to avoid full-state constraint violations, an event-triggered controller was devised in [21] to simultaneously reduce the communication burden on the controlled system. On this basis, the research in [22] was extended to uncertain fractional-order nonlinear nonstrict-feedback systems with input saturation and full-state constraints.

    Furthermore, focusing on fractional-order systems with immeasurable states and full-state constraints, an adaptive fuzzy output feedback control was established in [23]. It should be noted that the process of constraint control would inevitably involve multi-objective constraints, such as reducing logistics cost and improving commodity transportation quality [24] or lowering production cost and increasing production rate [25], which cannot be solved by conventional constraint methods. Correspondingly, the adaptive control schemes in [26,27,28] were presented for such controlled systems under multiple objective constraints. In spite of these attempts, to the authors' best knowledge, no results has been reported on fractional-order nonlinear systems control with multi-objective constraints, which is one of the our research motivations.

    Inspired by the above observation and analysis, this paper focuses on the neuro-adaptive finite-time control of fractional-order nonlinear systems in nonstrict-feedback form subject to multiple objective constraints which contain unknown nonlinear dynamics and external disturbances. The primary characteristics and innovations of this paper are listed below:

    1) This study introduces the neuro-adaptive finite time control method of the multi-objective constraints for fractional-order nonlinear systems by introducing a novel barrier function. Different objective functions are constrained to the predefined acceptable range by selecting the appropriate weight coefficients. Note that the results on the multi-objective constrained nonlinear systems in [26,27,28] only apply to integer-order systems without relating to fractional-order systems. Besides, the control method for the constrained nonlinear system is studied in [26], while the finite time convergence is not considered. Unlike the constant value constraint in [27,28], this paper adopts a time-varying constraint, which is more in line with engineering applications.

    2) The system plants considered in this work is more general than those in [7,8,15,16,17,21]. A new parameter adaptive law is designed to control the nonlinear fractional-order system in nonstrict-feedback form, which eliminates the effect of unknown external disturbance and the algebraic loop problem. The devised control scheme ensures that the system output tracks the desired signal in finite time. Compared with [7,8,21,22], the control algorithm proposed in this paper accelerates the tracking rate and improves convergence.

    The rest of this article can be summarized as follows: Section 2 gives the formulation and preliminary preparation of the problem. Section 3 presents the main results and a finite-time neuro-adaptive control method based on the backstepping algorithm. Section 4 provides simulation example to elaborate on the feasibility of the developed control algorithms. Section 5 summarizes this paper.

    Two definitions of fractional calculus are introduced as follows.

    Definition 2.1. ([29]) The Riemann-Liouville (RL) fractional integral of order α>0 for the function f(t)Cn([t0,+],R) is defined as

    RLIαtf(t)=1Γ(α)t0f(τ)(tτ)1αdτ,

    where

    Γ()=+0τα1eτdτ

    represents the Gamma function, which satisfies

    Γ(1)=1.

    Cn is the collection of all continuous functions whose derivatives of the integer orders i=1,2,,n are all continuous. Then, the αth Caputo fractional-order derivative is expressed by

    c0Dαtf(t)=1Γ(nα)t0f(n)(τ)(tτ)α+1ndτ,

    where c0Dαt represents the αth order Caputo differential operator whose time starts from zero. n1α<n, nN+. Here, the superscript "RL" denotes the Riemann-Liouville derivative and "c" denotes the Caputo derivative. In this paper, only the case α(0,1) is considered.

    Consider a class of nonstrict-feedback systems with external disturbances described as follows:

    c0Dαtxi=gi(x)xi+1+fi(x)+di(t), i=1,,n1,c0Dαtxn=gn(x)u+fn(x)+dn(t),y=x1, (2.1)

    where

    x=[x1,x2,...,xn]TRn

    and yR are the state vector and the system output, respectively. uR is the input of the controlled system. fi(x)R and gi(x)R denote the unknown but smooth nonlinear functions. di(t)R represents an unknown continuous external disturbance in the subsystem. Additionally, consider the system (2.1) subject to multiple objective constraints

    kj1(t)<Jj(x1)<kj2(t), j=1,,m (2.2)

    and

    Jj(x1)=r1x1+r2x21++rjxj1, (2.3)

    where Jj(x1) is the jth objective function and the rj denote the weighting coefficients. By selecting appropriate weighting coefficients, we ensure that all objective functions can be unified within the common boundary

    K1(t)<{J1(x1),J2(x1),,Jm(x1)}<K2(t) (2.4)

    with

    K1(t)=max{k11(t),k21(t),,km1(t)}

    and

    K2(t)=min{k12(t),k22(t),,km2(t)}.

    Remark 2.1. It is worth indicating that system (2.1) is more general than those considered in results mentioned in the introduction. If gi(x)=1 and

    x=ˉxi(ˉxi=[x1,x2,,xi]TRi,  i=1,,n),

    system (2.1) will degenerate into the systems investigated in [8,15]. When di(t)=0, system (2.1) becomes the system considered in [7,16,17,21,22].

    To facilitate the controller design, we make common assumptions in the following points.

    Assumption 2.1. For i=1,2,,n, the functions gi(x) are continuous, and there exist unknown constants gm>0 and gM>0 satisfying

    0<gm≤∣gi()∣≤gM.

    For notation conciseness, we denote gi(x) as gi.

    Assumption 2.2. For i=1,2,,n, the external disturbances are bounded such that |di(t)|ˉdi with ˉdi being unknown positive constants.

    Assumption 2.3. The desired signal yd and its fractional-order derivative are continuous and limited with Y0,1,2, which satisfy that

    |yd|Y0,  c0DαtydY1andc0Dαt[c0Dαtyd]Y2,

    where Y0, Y1 and Y2 are positive constants.

    The following definition of finite-time stability for fractional-order nonlinear systems is introduced.

    Definition 2.2. ([13]) Let ξ=0 be the equilibrium point of a fractional-order system c0Dαtξ=f(ξ,u). It is called to be practical finite-time stable if for all initial conditions ξ(t0)=ξ0, there exists a constant ϵ>0 and a settling time T(ϵ,ξ0)< which satisfy ξ<ϵ, tt0+T.

    Control objective: The aims of this paper are to construct a finite-time adaptive controller for system (2.1) to ensure that the system output y is capable of tracking the desired signal yd in finite time, and that multiple different objective function constraints are not transgressed. Simultaneously, all closed-loop signals are guaranteed to be bounded.

    Then, the following lemmas will be used in the stability analysis of fractional-order nonlinear system.

    Lemma 2.1. ([30]) Suppose that f(t): [t0,]R, the following inequality holds for all tt0,

    RLIαt0,t(c0Dαtf(t))=f(t)n1j=0f(j)(t0)j!(tt0)j.

    Lemma 2.2. (Gronwall-Bellman integral inequality [31]) Let f(t) satisfy

    f(t)tt0p(τ)f(τ)dτ+q(t)

    with a real function p(t) and a differentiable real function q(t). There is

    f(t)tt0q(τ)exp(tτp(r)dr)dτ+q(t0)exp(tτp(τ)dτ),

    where tt0. In particular, if q(t)=q is a constant, we have

    f(t)qexp(tτp(τ)dτ).

    Lemma 2.3. ([32]) Suppose 0<α<1, ϱ>1 and f(t)C1([0,+),R). It holds that

    c0Dαtfϱ(t)Γ(1+ϱ)Γ(1+ϱα)fϱα(t)c0Dαtf(t).

    Lemma 2.4. ([33]) Assume that x(t)Rn is a smooth and differentiable function vector. Then,

    c0Dαt(xT(t)x(t))2xT(t)c0Dαtx(t), tt0.

    Lemma 2.5. ([34]) Let y(x(t)): ΩR and x(t): [t0,+)Ω be two continuously differentiable functions, where ΩR is a set. If y(x(t)) is convex over Ω (i.e., 2y(x)/x20), then

    c0Dαty(x)(y(x)/x)c0Dαtx

    holds for any tt0 and constant 0<α<1.

    Lemma 2.6. ([14]) For ι1>0, ι2>0, ι3>0, μ10, μ20, and μ30, the following inequality holds

    μι11μι22μ3ι3μι1+ι21+ι2ι1ι2×[ι1ι3(ι1+ι2)]ι1ι2μι1+ι22μι1+ι2ι23.

    Note that the radial basis NN function is used as a promising tool to approximate unknown nonlinear functions [5]. For an unknown continuous nonlinear function F(Z): RnR, we can approximate it using the NN function y(Z)=θTφ(Z), where θ is a weight vector, which can be represented as

    F(Z)=θTφ(Z)+δ(Z),

    where δ(Z) is the approximation error.

    θ=[θ1,θ2,...,θl]TRl, (l>1)

    is the ideal weight vector defined as

    θ=argminθRn{supZΩZ|F(Z)θTφ(Z)|},

    where

    φ(Z)=[φ1(Z),φ2(Z),  ,φn(Z)]T

    is the basis function vector and n is the number of neurons. φi(Z) is a Gaussian function formed as

    φi(Z)=exp[(Zpi)T(Zpi)q2i],  i=1,2,,n,

    where qi and pi are the center of the receptive field and width of the ith hidden layer.

    To achieve the multi-objective constraints, different objective functions are guaranteed to be confined within a certain acceptable range. Inspired by [26], a barrier function is introduced as

    =Jl(x1)Jl(x1)K1(t)+Jl(x1)K2(t)Jl(x1), (3.1)

    where lΛ={1,,m} and Jl(x1) is the abstract function with respect to x1 satisfying Jl(x1)/x10 in the open compact set ΩJ. K1(t) and K2(t) represent the upper and lower bounds of Jl(x1) such that K1(t)<K+1 and K2(t)>K2, respectively. For any initial value Jl(0)ΩJ, if JlK+1 or JlK2, then . In general, if Jl is to comply with the constraint, then it is sufficient to ensure that is bounded. So, the issue of satisfying the objective function constraint can be turned into ensuring that is bounded.

    Remark 3.1. It is remarkable that multi-objective constraints are widespread in various practice systems. Nevertheless, in practical engineering applications, the multiple optimization objectives we consider may be contradictory, such as reducing logistics cost and improving commodity transportation quality, reducing production cost and increasing production rate or other physical scenarios. It is unrealistic that all objective functions are reaching their optimum simultaneously. Therefore, we take K1(t) and K2(t) as the maximum of the common lower bound and the minimum of the common upper bound of all objective functions, respectively. Note that K1(t) and K2(t) can be asymmetric and possibly time-varying functions, which is different from [26,27,28]. By this compromise scheme, all objective functions can be unified simultaneously in the same boundary.

    Then, from Lemma 2.5, by taking αth order derivative of , it yields

    c0Dαt(x)xc0Dαtx=ϖ1(c0DαtJj(x1))+ϖ2 (3.2)

    with

    ϖ1=K1(t)/(Jj(x1)K1(t))2+K2(t)/(K2(t)Jj(x1))2

    and

    ϖ2=Jj(c0DαtK1(t))/(Jj(x1)K1(t))2Jj(c0DαtK2(t))/(K2(t)Jj(x1))2.

    Then, c0Dαt is rewritten as

    c0Dαtϖ11c0Dαtx1+ϖ2, (3.3)

    where ϖ11=ϖ10sign(ϖ10). Since

    ϖ10=ϖ1Jj(x1)/x1andJj(x1)/x10,

    it is deduced that ϖ110.

    Let us define the errors as

    z1=ˆyd,zn=xiˉαi,i=2,,n, (3.4)

    where

    ˆyd=J(yd)/(J(yd)K1(t))+J(yd)/(K2(t)J(yd))

    and ˉαi are the output of the fractional-order filters with virtual control signal αi1 as the corresponding input signals, which is defined as

    τic0Dαtˉαi+ˉαi=αi1,ˉαi(0)=αi1(0), (3.5)

    where τi is a positive time constant. χi=ˉαiαi1 denotes the filter error cased by the fractional-order filter.

    Step 1: Thus, according to (3.1) and (3.4), the αth fractional-order derivative of z21/2 is derived as

    12c0Dαt(z21)ϖ11z1(g1z2+g1α1+F1(X1)+d1)+gm2χ22z1c0Dαtˆyd, (3.6)

    where

    F1(X1)=f1+g1ϖ211z1/2+ϖ2/ϖ11

    and

    X1=(x1,...,xn,yd,c0Dαtyd)T.

    Since the continuous function F1(X1) contains the unknown functions f1 and g1, the NN function θT1φ1(X1) is employed to approximate it. According to Lemma 2.6, for given ε1>0, it is known that

    F1(X1)=θT1φ1(X1)+δ1,

    where θT1 and φ1(X1) are the optimal weight vector and the NN Gaussian function vector, respectively. δ1 is the minimum approximation error satisfying δ1ε1.

    Using Young's inequality and the property

    0<φT1()φ1()1,

    we have

    z1c0Dαtz1=ϖ11z1(g1z2+g1α1+θT1φ1(X1)+δ1+d1)+gm2χ22z1c0Dαtˆydϖ11z1(g1z2+g1α1)+gm2χ22+|ϖ11z1|gmρ1+θT12ϖ211z214κ1φT1(x1)φ1(x1)+κ1φT1(x1)φ1(x1)z1c0Dαtˆydϖ11z1(g1z2+g1α1)+gm2χ22+|ϖ11z1|gmρ1+gmω1ΘT1ϖ211z21+κ1z1c0Dαtˆyd, (3.7)

    where

    Θ1=max{θ12/gm}

    and

    ρ1=(ˉd1(t)+ε1)/gm,

    κ1 is a positive constant and

    ω1=1/(4κ1φT1(x1)φ1(x1)).

    Remark 3.2. Note that F1(X1) contains all the state variables, which implies that system (2.1) is a nonstrict-feedback system. If the traditional backstepping design method is adopted, the algebraic loop problem arises. In order to avoid such problem, this paper uses the adaptive parameter Θ1 to participate in the construction of the controller. In addition, the adaptive parameter ρ1 and the compensation function ()/tanh(/ς) with ς>0, are introduced to handle the affect brought by uncertainties, approximation errors and external disturbances.

    Consider the following Lyapunov function

    V1=12z21+gm2γ1˜Θ21+gm2Γ1˜ρ21, (3.8)

    where γ1>0 and Γ1>0 are the design constants, ˜Θ1=Θ1ˆΘ1 stands for the estimation error when ˆΘ1 is estimating Θ1. Define ˜ρ1=ρ1ˆρ1 when ˆρ1 is used to estimate of ρ1.

    According to Lemma 2.4, we estimate the αth Caputo fractional derivative of V1 as

    c0DαtV1ϖ11z1(g1z2+g1α1)+gmω1ΘT1ϖ211z21+κ1+|ϖ11z1|gmρ1+gm2χ22z1c0Dαtydgmγ1˜Θ1c0Dαt(ˆΘ1)gmΓ1˜ρ1c0Dαt(ˆρ1). (3.9)

    The virtual controller α1, the adaptive laws ˆΘ1 and ˆρ1 are

    α1=1ϖ11(c1z1k1z2β11+c0Dαtˆyd)ω1ϖ11z1ˆΘ1ˆρ1tanh(ϖ11z1ς), (3.10)
    c0DαtˆΘ1=γ1ω1ϖ211z21μ1ˆΘ1, (3.11)
    c0Dαtˆρ1=Γ1ϖ11z1tanh(ϖ11z1ς)π1ˆρ1, (3.12)

    where c1,k1,μ1,π1 are positive constants with 12<β<1.

    Substituting (3.10)–(3.12) into (3.9) produces

    c0DαtV1ϖ11g1z1z2c1gmz21k1gmz2β1+gm2χ22+gmμ1γ1˜Θ1ˆΘ1+gmπ1Γ1˜ρ1ˆρ1+gm|ϖ11z1|ρ1gmϖ11z1ρ1tanh(ϖ11z1ς)+κ1. (3.13)

    Applying the property of the inequality ||()tanh(/ς)0.2785ς, where ς>0, then (3.13) can be rewritten as

    c0DαtV1ϖ11g1z1z2c1gmz21k1gmz2β1+gm2χ22+gmμ1γ1˜Θ1ˆΘ1+gmπ1Γ1˜ρ1ˆρ1+Δ1, (3.14)

    where Δ1=0.2785ςgmρ1+κ1.

    From (3.5), we have

    c0Dαtχi=c0Dαtˉαic0Dαtαi1=χiτi+Hi, (3.15)

    where i=2,,n, Hi() is the continuous function related to variables z1,,zi, ˆΘ1,,ˆΘi, ˆρ1,,ˆρi, χ2,,χi, yd,c0Dαtyd and c0Dαt[c0Dαtyd]. Meanwhile, there may exist positive constants Υi satisfying |Hi|<Υi in the compact set Ξ. Then, it yields

    χic0Dαtχi=χ2iτi+χiHi(141τi)χ2i+Υ2i. (3.16)

    Step i (i=2,,n1): Similar to previous steps, then, it follows from (2.1) and (3.4) that

    c0Dαtzi=gi(zi+1+χi+αi)+fi+dic0Dαtˉαi. (3.17)

    Now, consider the following Lyapunov function

    Vi=Vi1+12z2i+12χ2i+gm2γi˜Θ2i+gm2Γi˜ρ2i, (3.18)

    where γi>0 and Γi>0 are the design parameters. ˆΘi is the estimate of Θi with

    ˜Θi=ΘiˆΘiandΘi=max{θi2/gm}.

    Define

    ρi=(ˉdi(t)+εi)/gmand˜ρi=ρiˆρi

    with ˆρi being the estimation of ρi.

    Then, the αth derivative of (3.18) gives

    c0DαtVic0DαtVi1+zi[gi(zi+1+αi)+Fi(Xi)+dic0Dαtˉαi]+gm2χ2igmγ2˜Θic0Dαt(ˆΘi)gmΓi˜ρic0Dαt(ˆρi)+Υ2i, (3.19)

    where

    Fi(Xi)=fi+gizi1+gizi/2,

    and

    Xi=(x1,,xn,ˆΘ1,,ˆΘi,ˆρ1,,ˆρi,
    yd,c0Dαtyd,c0Dαt[c0Dαtyd])T. 

    Based on the NN function approximation, some transformations are exploited

    zi(Fi(Xi)+di)ziθTiφi(Xi)+zi(δi+di)|zi|gmρi+θTi2z2i4κiφTi(xi)φi(xi)+κiφTi(xi)φi(xi)|zi|gmρi+gmωiΘTiz2i+κi, (3.20)

    where

    ωi=1/(4κiφTi(xi)φi(xi))

    and κi>0 is a design parameter.

    Construct the ith intermediate control function αi, and the adaptation laws of ˆΘi and ˆρi as follows:

    αi=cizikiz2β1iωiziˆΘi+c0Dαtˉαiˆρitanh(ziς), (3.21)
    c0DαtˆΘi=γiωiz2iμiˆΘi, (3.22)
    c0Dαtˆρi=Γizitanh(ziς)πiˆρi, (3.23)

    where ci,ki,μi and πi are positive constants.

    Substituting (3.20)–(3.23) into (3.19) yields

    c0DαtViij=1cjgmz2jij=1kjgmz2βj+gm2χ2i+1+ij=2(141τj+gm2)χ2j+ij=1gmμjγj˜ΘjˆΘj+ij=1gmπjΓj˜ρjˆρj+zigizi+1+ij=1Δj, (3.24)

    where

    Δi=Δi1+0.2785ςgmρi+κi+Υ2i.

    Step n: Along with step i, the derivative of zn is

    c0Dαtzn=gnu+fn+dnc0Dαtˉαn. (3.25)

    Similar to the previous steps, consider the Lyapunov function candidate as

    Vn=Vn1+12z2n+12χ2n+gm2γn˜Θ2n+gm2Γn˜ρ2n, (3.26)

    where γn and Γn are the positive design constants.

    Then, the αth derivative of (3.26) is calculated as

    c0DαtVnc0DαtVn1+zn[gnu+Fn(Xn)+dnc0Dαtˉαn]+gm2χ2ngmγ2˜Θnc0Dαt(ˆΘn)gmΓn˜ρnc0Dαt(ˆρn)+Υ2n, (3.27)

    where

    Fn(Xn)=fn+gnzn1+gnzn/2,  
    Xn=(x1,,xn,ˆΘ1,,ˆΘn,ˆρ1,,ˆρn,
    yd,c0Dαtyd,c0Dαt[c0Dαtyd])T. 

    Based on the NN approximation, it follows that

    zn(Fn+dn)znθTnφn(Xn)+zn(δn+dn)|zn|gmρn+θTn2z2n4κnφTnφn+κnφTnφn|zn|gmρn+gmωnΘTnz2n+κn, (3.28)

    where

    ωn=1/(4κnφTi(xn)φi(xn))

    and κn is a positive constant.

    It follows from (3.27) and (3.28) that

    c0DαtVnc0DαtVn1+zngnu+gmωnΘTnz2n+|zn|gmρnznc0Dαtˉαn+gm2χ2n+κngmγn˜Θnc0Dαt(ˆΘn)gmΓn˜ρnc0Dαt(ˆρn)+Υ2n. (3.29)

    Then, take the actual input u and adaptive laws as

    u=cnznknz2β1nωnznˆΘn+c0Dαtˉαnˆρntanh(znς), (3.30)
    c0DαtˆΘn=γnωnz2nμnˆΘn, (3.31)
    c0Dαtˆρn=Γnzntanh(znς)πnˆρn, (3.32)

    where cn,kn,μ2,πn are design positive constants.

    Invoking (3.29)–(3.32), we have

    c0DαtVnnj=1cjgmz2jnj=1kjgmz2βj+nj=2(141τj+gm2)χ2j+nj=1gmμjγj˜ΘjˆΘj+nj=1gmπjΓj˜ρjˆρj+nj=1Δj, (3.33)

    where

    Δn=Δn1+0.2785ςgmρn+κn+Υ2n.

    The above control method can be outlined in the following theorem.

    Theorem 3.1. Suppose that Assumptions 2.1–2.3 hold for the nonstrict feedback fractional-order nonlinear systems (2.1) subject to multiple objective constraints (3.1), the actual control law constructed in (3.30) is based on the virtual control laws (3.10) and (3.21), the parameter adaptive laws ((3.11), (3.22), (3.31)) and ((3.12), (3.23), (3.32)). Then, it ensures that the system output driven to track the desire signal in finite time, the different objective functions do not transgress their constrained sets and all signals in the closed-loop systems are guaranteed to be bounded.

    Proof. Based on Young's inequality, it is derived that

    nj=1gmμjγj˜ΘjˆΘjnj=1gmμjγj˜Θ2j+nj=1gmμjγjΘ2j,nj=1gmπjΓj˜ρjˆρjnj=1gmπjΓj˜ρ2j+nj=1gmπjΓjρ2j. (3.34)

    Therefore, c0DαtVn is expressed as

    c0DαtVnnj=1cjgmz2jnj=1kjgmz2βjnj=1gmμjγj˜Θ2j+nj=2(141τj+gm2)χ2j+nj=1gmπjΓj˜ρ2j+nj=1gmμjγjΘ2j+nj=1gmπjΓjρ2j+nj=1Δj. (3.35)

    Using Lemma 2.6, for

    ι1=1ι2, ι2=β, ι3=ι1ι32, μ1=1, μ2=nj=1˜ρ2j/Γj

    and μ3=1, we obtain

    nj=1(1γj˜Θ2j)βι3+nj=11γj˜Θ2j. (3.36)

    Similarly, we have

    nj=1(1Γj˜ρ2j)βι3+nj=11Γj˜ρ2j

    and

    nj=2(14χ2j)βι3+nj=214χ2j.

    Through above analysis, it follows that

    c0DαtVnnj=1cjgmz2jnj=1kjgmz2βjnj=1(gmμj1)1γj˜Θ2jnj=2(1τj12gm2)χ2jnj=1(gmπj1)1Γj˜ρ2jnj=1(1γj˜Θ2j)βnj=1(1Γj˜ρ2j)βnj=2(14χ2j)β+Ψ, (3.37)

    where

    Ψ=nj=1(gmμj/γj)ˆΘ2j+nj=1(gmπj/Γj)ˆρ2j+nj=1Δj+3ι3.

    Choose the design parameters such that gmμj1>0, gmπj1>0 (j=1,,n) and 1/τj1/2gm/2>0 (j=2,,n). If we let

    a=min{2cjgm,2/τj+11gm,2(gmμj1)/γj,2(gmπj1)/Γj}

    and

    b=min{kjgm2β,1/2β,2β/γj,2β/Γj},  j=1,,n1,

    then the inequality (3.37) is stated as

    c0DαtVnaVnbVβn+Ψ. (3.38)

    For (3.38), two parts are discussed as follows.

    Part 1: Defining V(t)=Vn(t)Ψ/a, according to Lemma 2.2 and c0DαtVnaVn+Ψ, then V(t) is transformed into

    c0DαtV(t)a(V(t)+Ψa)+Ψ=aV(t). (3.39)

    Thus, there exists (t)R+ such that

    c0DαtV(t)=aV(t)(t). (3.40)

    Based on Lemma 2.1, taking the fractional integration RLIαt of (3.40) from t0 to t, we obtain

    c0DαtV(t)=V(t0)tt0(tτ)α1Γ(α)(aV(τ)+(t))dτV(t0)aΓ(α)tt0(tτ)α1V(τ)dτ. (3.41)

    On the other hand, from Lemma 2.2, we know that

    V(t)V(t0)exp(a(tt0)αΓ(α+1)). (3.42)

    Substituting V(t)=Vn(t)Ψ/a into (3.42), the inequality (3.42) is computed as

    Vn(t)(Vn(t0)Ψa)exp(a(tt0)αΓ(α+1))+ΨaΨa. (3.43)

    According to the definition of Vn and (3.43), the error variables satisfies

    limt|z1|=2Ψ/a.

    Therefore, from the above-mentioned inequality, we can conclude the boundedness of Vn, which indicates that zi, ˜Θi, ˜ρi for i=1,,n and χj for i=2,,n are bounded.

    Consider z1=ˆyd. Based on the boundedness of ˆyd, the boundedness of is ensured, and from (3.1), the Jl is bounded in the constraints. Considering the definition of Jl, we can get that x1 is bounded by |x1|X0 with X0>0. Moreover, according to Assumption 2.3, there exist the bounds of yd, i.e., Y0 such that J(Y0)K1>0, and K2J(Y0)>0. Then, combining it with the definition of the tracking error, we obtain

    |e1||x1yd||X0Y0|.

    From th Eqs (3.10)–(3.12), variables α1, ˙ˆΘ1 and ˙ˆρ1 are bounded. In the following, we are summarizing that xi,ˉαi,˙ˆΘi,˙ˆρi (i=2,,n), αj (j=2,,n1) and the actual input u are bounded. Hence, all the variables of the closed-loop system are bounded.

    Part 2: We show that zi,˜θ and ˜ρ have finite-time convergence. From (3.38), it is clear to obtain that

    c0DαtVnbVβn+Ψ. (3.44)

    Note that there exists a constant 0<ϑ<1 such that the inequality (3.44) can be rewritten as

    c0DαtVnbϑVβnb(1ϑ)Vβn+Ψ. (3.45)

    If Vn>(Ψ/b(1ϑ))1/β, we have c0DαtVnbϑVβn. Choosing β=2p1, ˉς=1+α, applying Lemma 2.3, we show that

    Vnc0DαtVn=Γ(2)Γ(2+α)c0DαtVα+1nbϑV2pn. (3.46)

    Defining ˉV=Vα+1n, we deduce that

    ˉV[(2p)/(α+1)]=V2pn.

    Therefore, the above inequality leads to

    c0DαtˉVα2pα+1bϑΓ(2+α)Γ(2)Γ(1+α2pα+1)Γ(12pα+1). (3.47)

    Taking the integration of the inequality (3.47) from 0 to t, we get

    ˉVα2pα+1ˉV(0)α2pα+1bϑΓ(2+α)Γ(2)Γ(1+α2pα+1)Γ(12pα+1)tαΓ(1+α). (3.48)

    Then, the reaching time Tr is evaluated as

    Tr=[V(α(1+α)2p)n(0)Γ(2)Γ(12p1+α)Γ(1+α)bϑΓ(2+α)Γ(1+α2p1+α)]1α.

    If Vn(Ψ/b(1ϑ))1/β, based on previous analysis, the trajectory of of all variables in Vn will not be greater than (Ψ/b(1ϑ))1/β.

    Therefore, it can be indicated that the controlled system is finite-time stable and the tracking error e1 can be converged into a sufficiently small neighborhood around the origin in the setting time Tr. The proof is completed.

    A block diagram of our control design structure is given in Figure 1.

    Figure 1.  Block diagram of the provided scheme structure.

    Remark 3.3. The design parameters ci, ki, ωi, γi, Γi, μi and πi are only a sufficient condition to ensure the finite time stability of the control system and they should be a trade-off between tracking performance and controlling costs. From the proof of Theorem 3.1, the selection of some key design parameters are provided as below:

    1) Increasing ci, γi, Γi, κi and ς helps to increase a in (3.38), subsequently reducing the error bound;

    2) Increasing ki, ωi helps to increase b in (3.38), subsequently accelerating the convergence rate;

    3) Increasing or decreasing μi, πi will affect the approximation performance of FLS and the estimation effect of disturbances and approximation errors.

    Remark 3.4. It should be emphasized that the form of (3.38) is discussed in two parts. First, the fractional-order finite-time stability criterion is introduced to ensure that the tracking error converges to a compact set within a finite-time. Then, fractional-order Lyapunov theory is employed to ensure the stability of the closed-loop system. Note that the finite-time control scheme proposed in this paper has a faster convergence rate than [15] when the initial state is far away from the origin point.

    Remark 3.5. It is worth noting that the establishment of time Tr is not an explicit relationship, that is, Tr is not easy to calculate in practical applications. Compared with finite time control, predefined time control [35] has some superior advantages, such as that the upper bound of the settling time can be preset and independent of the initial conditions and the convergence accuracy can be ensured. However, this usually means that the control input needs to be large enough to achieve its outstanding convergence performance. Therefore, how to make a tradeoff between the convergence accuracy/time and the excessive control input is a problem that researchers continue to consider. It is undoubtedly a good choice to consider the optimal control of a certain performance index.

    In the following, we illustrate the validity of the proposed method through numerical example. The dynamic model of 2-order fractional-order nonlinear systems is as follows

    {c0Dαtx1=(1+x21)x2+x2e0.5x1+d1(t),c0Dαtx2=x1x22+(3+cos(x1x2))u+d2(t),y=x1, (4.1)

    where the fractional order α is chosen as 0.95, and the external disturbances are given as d1=d2=0.1sin(t).

    The controller parameters are chosen as

    c1=8,c2=20,k1=0.5,k2=1,β=97/101,τ=0.05
    ς=1,κ1=2,κ2=2,γ1=10,γ2=10,μ1=0.8,
    μ2=0.8,Γ1=10,Γ2=10,π1=0.8,π2=0.8,
    x(0)=[0.3,0.5]T,ˆρ(0)=[0.5,0.5]T,ˆΘ(0)=[0.4,0.4]T.

    The reference signal is yd=0.5sin(t) and it follows that

    Jd=m1yd+m2y2d+m3y3d.

    We employ 11 nodes for each dimension of the NN with the center spaced in [-10, 10] and with the width 2.

    The objective function Jl is bounded

    JlΩJ:={JlR:K1(t)<Jl(x1)<K2(t)},

    and three cases of objective functions are executed as

    {Case 1:J1(x1)=x1,Case 2:J2(x1)=0.1x1+0.08x21,Case 3:J3(x1)=0.02x1+0.12x21+0.4x31,

    where the constraining boundaries are set as K1=0.850.15sin(t) and K2=1.2+0.5sin(t). m1=1,m2=m3=0 means that J1=x1, which is the case with output constraints.

    The simulation results of system (4.1) are depicted in Figures 29 under the three cases. Figures 2, 4 and 6 show that the system output y=x1, and the trajectories of desired signal yd, and the values of the error signals converge to zero in finite time, which means that the system output is confined in the prescribed constraints and the trajectory of the state x2 is bounded. Figures 3, 5 and 7 show the curve of adaptive laws and the control inputs. It can be seen from these figures that the trajectories of adaptive laws are bounded in all the three cases. The multiple objective functions, in view of Figure 8, have no violated constraints and approximate the desired objective trajectories Jd.

    Figure 2.  Case 1: tracking performance.
    Figure 3.  Case 1: trajectories of variables x2, z2, and control input u.
    Figure 4.  Case 2: tracking performance.
    Figure 5.  Case 2: trajectories of variables x2, z2, and control input u.
    Figure 6.  Case 3: tracking performance.
    Figure 7.  Case 3: trajectories of variables x2, z2, and control input u.
    Figure 8.  Trajectories of J following Jd under the three cases.
    Figure 9.  Trajectories of system output y and the reference signal yd under difference methods.

    To show the superiority of the proposed method, we use the control approach without finite time control technique in [7] to control the nonlinear system (4.1). For fair comparison, the initial conditions and control parameters are the same as in Example 1. The contrasting simulation result is plotted in Figure 9. It can be seen from Figure 9 that the proposed finite time controller in this paper has more satisfactory convergence speed and tracking performance. The comparative results in Figure 9 indicate that the settling time of the proposed finite time control method is less than 0.5 s, whereas the settling time of without finite time control becomes larger.

    This article has explicitly focused on the finite-time adaptive tracking control problem for nonstrict-feedback fractional-order nonlinear systems under multiple objective constraints and unknown disturbances. The NNs are utilized to identify the unknown dynamics. Meanwhile, a novel barrier function is constructed to ensure that all objective functions are constrained within the preset range, while keeping the system output in the prescribed boundaries. The stability analysis and simulation results illustrated that all the signals in the fractional-order nonlinear system are bounded, and the tracking error is guaranteed to converge to a small neighborhood of the origin in finite time. Future research will extend the finite time method to fractional-order nonlinear systems with immeasurable states and input nonlinearities.

    The authors declare they have not used Artificial Intelligence (AI) tools in the creation of this paper.

    This work was supported in part by the National Natural Science Foundation of China under Grant 62073189 and Grant 62173207, and in part by the Taishan Scholar Project of Shandong Province under Grant tsqn202211129.

    All authors declare no conflicts of interest in this paper.



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