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Research article

Finite-time fuzzy output-feedback control for p-norm stochastic nonlinear systems with output constraints

  • Received: 06 September 2020 Accepted: 19 November 2020 Published: 11 December 2020
  • MSC : 37F15, 34D09

  • This paper investigates the finite-time control problem of p-norm stochastic nonlinear systems subject to output constraint. Combining a tan-type barrier Lyapunov function (BLF) with the adding a power integrator technique, a fuzzy state-feedback controller is constructed. Then, an output-feedback controller design scheme is developed by the constructed state-feedback controller and a reduce-order observer. Finally, both the rigorous analysis and the simulation results demonstrate that the designed output-feedback controller not only guarantees that the output constraint is not violated, but also ensures that the system is semi-global finite-time stable in probability (SGFSP).

    Citation: Liandi Fang, Li Ma, Shihong Ding. Finite-time fuzzy output-feedback control for p-norm stochastic nonlinear systems with output constraints[J]. AIMS Mathematics, 2021, 6(3): 2244-2267. doi: 10.3934/math.2021136

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  • This paper investigates the finite-time control problem of p-norm stochastic nonlinear systems subject to output constraint. Combining a tan-type barrier Lyapunov function (BLF) with the adding a power integrator technique, a fuzzy state-feedback controller is constructed. Then, an output-feedback controller design scheme is developed by the constructed state-feedback controller and a reduce-order observer. Finally, both the rigorous analysis and the simulation results demonstrate that the designed output-feedback controller not only guarantees that the output constraint is not violated, but also ensures that the system is semi-global finite-time stable in probability (SGFSP).



    Over the past decades, a variety of control design strategies have been proposed for different nonlinear systems [1,2,3,4,5,6,7]. Especially, many approximated-based control schemes have been developed for uncertain nonlinear systems by using neural networks (NNs) or the fuzzy logic systems (FLSs) [8,9,10,11,12,13,14,15,16,17,18,19]. Among these studies, the research of stochastic systems is much more attracted (see, e.g. [16,17,18,19] and the references therein), due to their wide application. It is worth noting that the aforementioned NNs-based or FLSs-based control strategies haven't taken output constraint into account. In fact, many practical systems are usually required to satisfy an output constraint in the operation for considering the performance specifications or safety [20,21]. It is well known that, the BLF-based approaches are useful tools to settle controller design problems of output-constrained nonlinear systems, see references [22,23,24,25,26,27] for instances. In the latest research progress of constrained control, many kinds of adaptive neural or fuzzy control design methods have been presented by combining the different BLFs with NNs or FLSs approximators for various stochastic nonlinear systems subject to output constraint and unknown nonlinearities in [28,29,30,31,32]. Nevertheless, the above-mentioned works have mainly considered strict-feedback stochastic systems whose fractional powers are all equal to one, rather than p-norm stochastic nonlinear systems in which the fractional powers are the positive odd rational numbers and at least one of the fractional powers is greater than one.

    As an important class of nonlinear systems, the p-norm stochastic nonlinear systems which are more general and complex, have received increased attention in recent years. For such a kind of systems, many control design problems have been well solved by utilizing the adding a power integrator technique under some strong or weaker growth conditions [33,34,35,36,37]. Subsequently, references [38,39,40] have taken these growth conditions away and considered the adaptive NNs control for switched and large-scale stochastic high-order nonlinear systems. Meanwhile, the control problems have been investigated for p-norm nonlinear systems with output/states constraints under some nonlinear growth conditions in a few literatures, such as [41,42,43,44]. In these works, different state-feedback controllers have been mainly constructed and finite-time stability has been obtained. Worth noting that an output-feedback controller has been designed for high-order planar deterministic nonlinear systems in [44]. On these basics, references [45,46,47,48] have further taken both unknown nonlinearities and constraints into accounts, and designed some fuzzy controllers for p-norm stochastic nonlinear systems with output/states constraints. However, it should be pointed out that the above-mentioned results of p-norm stochastic nonlinear systems have mainly focused on addressing the asymptotical convergence rather than the finite-time convergence in the case of unknown nonlinearities. As a matter of fact, the finite-time convergence has only been investigated for p-norm stochastic nonlinear systems with known nonlinearities satisfying some nonlinear growth conditions. On the other hand, it can be observed that the existing constrained controllers of p-norm stochastic nonlinear systems are mainly based on the assumption that full-state measurements are available. In other words, when only the system output can be accurately measured, the problem of finite-time output-feedback control for p-norm stochastic nonlinear systems with unknown nonlinearities and output constraints, to our best knowledge, has never been considered in the literature.

    Motivated by above discussions, this paper will investigate how to design the finite-time output-feedback controller for a kind of p-norm stochastic nonlinear systems subject to output constraint. The main contributions can be summarized as follows: 1) It is first time to consider p-norm stochastic nonlinear systems with output constraints and unmeasurable states. Note that the existing studies have mainly addressed the constrained control problems under the the assumption that all the states are measurable (e.g., [33,34,35,36,37,41,43]), while this paper investigates the constrained control design in the case of that the states are all unmeasurable except the system output. What's more, the system nonlinearities are completely unknown. Thus, this work will extend and develop the existing control design theory for p-norm stochastic nonlinear systems; 2) A finite-time controller is designed. The developed scheme not only ensures the system output is constrained in a given compact set, but also enables the closed-loop system is semi-global finite-time stable in probability (SGFSP).

    In this paper, we consider the following class of p-norm stochastic nonlinear systems

    dxi=xpi+1dt+ϕi(ˉxi)dt+gTi(ˉxi)dω,i=1,,n1,dxn=updt+ϕn(x)dt+gTn(x)dω,y=x1, (2.1)

    where ω is a r-dimension standard Wiener process; x=(x1,,xn)TRn is system state vector; uRandyR are respectively control input and output; the fractional power pR1odd:={m/k|mk,mandkarepositiveoddintegers}; for i=1,,n, ˉxi=(x1,,xi)TRi; ϕi:RiR and gi:RiRr are unknown continuous functions satisfying ϕi(0)=0,gi(0)=0. The system output y=x1 is measurable and constrained in Π1={y(t)R,|y(t)|<ε} with a constant ε>0, while the other states x2,,xn are all unmeasurable.

    The objective of this paper is to design a finite-time fuzzy output-feedback controller for system (2.1) such that: 1) the output don't violate the given constrained boundary; 2) all the signals of the closed-loop system converge to a small compact of the original point in finite-time in probability in presence of unknown nonlinearities and unmeasured states xi(i=2,,n).

    Firstly, some concepts and lemmas are presented for preliminaries. Consider the following stochastic system

    dx=ϕ(x)dt+g(x)dω, (2.2)

    where ϕ(x) and g(x) are continuous functions with satisfying ϕ(0)=g(0)=0.

    Definition 1. [1] For any given V(x)C2(Rn), associated with system (2.2), the second-order differential operator is defined as follows:

    V=Vxϕ(x)+12tr{gT(x)2Vx2g(x)}. (2.3)

    Definition 2. [17] The equilibrium x=0 of stochastic nonlinear system (2.2) is semi-global finite-time stable in probability (SGFSP) if for all x(t0,ω)=x(0), there exist a constant c>0 and a settling time T(c,x0,ω)< to make E[x(t,ω)]<c, for all tt0+T.

    Lemma 1. [17] Consider the stochastic system (2.2) and assume that f(0), h(0) are bounded uniformly in t. If there exist a C2 Lyapunov function V:RnR+, functions ϱ1,ϱ2K, and constants ˉμ0>0, 0<ˉς0<1 and ˉν0>0 such that

    {ϱ1(|x|)V(x)ϱ2(|x|)V(x)ˉμ0V(x)ˉς0+ˉν0,xRn, (2.4)

    Then, the stochastic nonlinear system (2.2) is SGFSP.

    Remark 1. As stated in [17], the Eq (2.4) implies that there exists the stochastic setting time function T(x,ω)=1l0ˉμ0(1ˉς0)[E[V1ˉς0(x(0))](ˉν0(1l0)ˉμ0)ˉς01ˉς0], such that E[Vˉς0(x)]ˉν0(1l0)ˉμ0 for all tt0+T(x,ω), where 0<l01 is an arbitrary constant.

    Lemma 2. [7] Let a,bR+witha1. For any ζ,ηR, the following inequalities hold:

    (i) |ζaηa|a(2a2+2)|ζη|(|ζη|a1+ηa1),

    (ii) ζbaηba∣≤211aζbηb1a,

    (iii) (|ζ|+|η|)1a|ζ|1a+|η|1a211a(|ζ|+|η|)1a.

    Lemma 3. [42] For any constants k1,k2,ϑ,ςR+ and any variables ζ1,ζ2R, we have the following inequality

    ϑ|ζ1|k1|ζ2|k2ςk1k1+k2|ζ1|k1+k2+k1k1+k2ϑk1+k2k2ςk1k2|ζ2|k1+k2.

    Lemma 4. [8] Let p(0,), for any ζiR,i=1,,n, one has

    (|ζ1|++|ζn|)pb(|ζ1|p++|ζn|p),

    where b=max{np1,1}.

    Lemma 5. [36] If ζ,ηR and p>1 is an odd number, then

    (ζη)(ζpηp)12p1(ζη)p+1.

    Lemma 6. [12] With any a0>0,c0>0, and ζ(t)>0, for ˙η(t)=a0ζ(t)c0η(t), if η(0)0 can be satisfied, then one has η(t)0 for t0.

    In this paper, the nonlinear functions ϕi() and gi() are all unknown. The unknown functions will be approximated by the FLSs based on the following presented lemma.

    Lemma 7. [49] Let F(X) be a continuous function defined on a compact set Π0. Then, for a given desired level of accuracy δ>0, there exists a fuzzy logic system ΥTΨ(X) such that

    supXΠ0|F(X)ΥTΨ(X)|δ,

    Υ=(υ1,,υN)T is the ideal constant weight vector, and Ψ(X)=(ψ1(X),,ψN(X))TNj=1ψj(X) is the basis function vector, with N>1 being the number of the fuzzy rules and ψj(X) being chosen as Gaussian functions, i.e., for j=1,,N

    ψj(X)=exp[(Xλj)T(Xλj)ϑ2j]

    where λj=(λj1,,λjn)T and ϑj respectively denote the center vector and the width of the Gaussian function.

    Remark 2. In view of Lemma 7, any function F(X) which is defined and continuous on a compact set Π0, can be approximated by

    F(X)=ΥTΨ(X)+ϵ(X),

    where ϵ(X) is the FLS approximation error satisfying |ϵ(X)|<δ.

    In this section, a fuzzy state-feedback controller will be explicitly designed for system (2.1) by combining a tan-type BLF and the FLSs into the adding a power integrator technique.

    First of all, we introduce a coordinate transformation as follow

    χ1=x1,χi=xiHqi,i=2,,n,ν=uHqn+1, (3.1)

    where q1=0, qj=qj1+1p(j=2,,n+1), and H>1 is a constant to be determined later. Based on (3.1), system (2.1) turns into

    dχi=Hχpi+1dt+fi(ˉχi)dt+hTi(ˉχi)dω,i=1,,n1,dχn=Hνpdt+fn(χ)dt+hTn(χ)dω,y=χ1. (3.2)

    where ˉχi=(χ1,,χi), f1=ϕ1, h1=g1, fj=ϕjHqj, and hj=gjHqj,(j=2,,n).

    In what follows, a fuzzy state-feedback controller will be designed through n steps based on the equivalent system (3.2).

    Define

    ξ1=χ1,ξi=χiβi1,i=2,,n, (3.3)

    where βi's are the virtual signals being constructed later.

    Step 1. From (3.1), we can get

    dξ1=dχ1=(Hχp2+f1)dt+hT1dω. (3.4)

    Choose the first Lyapunov function

    V1=ε42πtan(πξ412ε4)+12b1˜α21VB(ξ1)+12b1˜α21,

    where b1>0 is an adjustment parameter, ˜α1=α1ˆα1 is the estimate error and ˆα1 is the estimator of the parameter α1.

    Remark 3. Clearly, VB(ξ1)=ε42πtan(πξ412ε4) is a tan-type BLF adopted to deal with the system output constraint. Compared to the log-type BLF, VB(ξ1) possesses the following characteristic:

    limεVB(ξ1)=ε42πtan(πξ412ε4)=ξ414,

    which implies that the proposed method is also applicable to the system without output constraints.

    Then, one can easily get from the definition of VB(ξ1) that

    VBξ1=S1(ξ1)ξ31, (3.5)
    2VBξ21=3S1(ξ1)ξ21+4πε4tan(πξ412ε4)S1(ξ1)ξ61. (3.6)

    where S1(ξ1)=sec2(πξ412ε4).

    In view of (2.3), (3.5) and (3.6), it is not hard to gain

    V1=VBξ1(Hχp2+f1)+122VBξ21hT1h11b1˜α1˙ˆα1=S1(ξ1)ξ31(Hχp2+f1)1b1˜α1˙ˆα1+32S1(ξ1)h12ξ21+2πε4tan(πξ412ε4)S1(ξ1)h12ξ61.

    From Lemma 3, one obtains

    32S1(ξ1)h12ξ2134S1(ξ1)2h14ξ41+34.

    Then, we have

    V1HS1(ξ1)ξ31χp2+HS1(ξ1)ξ31F1(Z1)ϱ1ε42πtan(πξ412ε4)1b1˜α1˙ˆα1+34, (3.7)

    where Z1=χ1,

    F1(Z1)=1H[f1+34S1(ξ1)2h14ξ1]+1H2πε4tan(πξ412ε4)S1(ξ1)h12ξ31+ϱ1ε4sin(πξ412ε4)2Hπξ31cos(πξ412ε4).

    and ϱ1>0 is an adjustment parameter.

    Thus, by Lemma 7, one can approximate F1(Z1) by

    F1(Z1)=ΥT1Ψ1(Z1)+ϵ1(Z1), (3.8)

    where |ϵ1(Z1)|δ1 and δ1>0 is a given constant.

    Since ΨT1()Ψ1()1, it is easily obtained from Lemma 3 that

    S1(ξ1)ξ31F1(Z1)S1(ξ1)|ξ1|3(Υ1Ψ1+δ1)3σ11α1p+3(S1(ξ1))p+33ξp+31+3p+3(S1(ξ1))p+33ξp+31+pp+3σ3p11+pp+3δp+3p1, (3.9)

    where α1=Υ1p+33 and σ11>0 is an adjustment parameter.

    Substituting (3.9) into (3.7) gets

    V1HS1(ξ1)ξ31(xp2βp1)+HS1(ξ1)ξ31βp1ϱ1ε42πtan(πξ412ε4)+3Hp+3S1(ξ1)p+33[σ11ˆα1+1]ξp+31+pHp+3σ3p11+H˜α1[3σ11p+3(S1(ξ1))p+33ξp+311b1H˙ˆα1]+34+pHp+3δp+3p1. (3.10)

    Then, one could design

    β1=M1p1ξ1φ1ξ1 (3.11)

    and

    ˙ˆα1=3Hb1σ11p+3(S1(ξ1))p+33ξp+31d1ˆα1, (3.12)

    where M13p+3(S1(ξ1))p3[σ11ˆα1+1]+ρ1S1(ξ1)+ϱ1>0; ϱ1,d1>0 are adjustment parameters; and the value of ρ1>0 will be given in the next step.

    Substituting (3.11) and (3.12) into (3.10), gets

    V1ϱ1ε42πtan(πξ412ε4)H(ρ1+ϱ1)ξp+31+HS1(ξ1)ξ31(χp2βp1)+d1b1˜α1ˆα1+34+pHp+3σ3p11+pHp+3δp+3p1.

    In addition, it is easily obtained that

    d1b1˜α1ˆα1=d1b1(α1˜α1)˜α1d1˜α212b1+d1α212b1.

    Therefore, we can get

    V1ϱ1ε42πtan(πξ412ε4)d1˜α212b1H(ρ1+ϱ1)ξp+31+Q1+HS1(ξ1)ξ31(xp2βp1), (3.13)

    where Q1=34+pHp+3σ3p11+pHp+3δp+3p1+d1α212b1.

    Remark 4. Notice that

    limξ10ε4sin(πξ412ε4)cos(πξ412ε4)2πξ31=limξ10ε4πξ412ε4cos(πξ412ε4)2πξ31=0,

    which means that the continuity of F1(Z1) is ensured.

    Remark 5. According to Lemma 6, one gets ˆα10, for t0. In each design step, this characteristic will be always applied.

    Step 2. From (3.3) and Itˆo's formula, we have

    dξ2=(Hχp3+f2β1)dt+(h2β1χ1h1)Tdω, (3.14)

    where β1=β1χ1(Hχp2+f1)+β1ˆα1˙ˆα1+122β1χ21hT1h1. Combining the definition of β1 with the properties of f1(χ1) and h1(χ1), implies that β1 is valid and continuous.

    Choose the second Lyapunov function as

    V2=V1+Λ2 (3.15)

    with

    Λ2=14ξ42+12b2˜α22, (3.16)

    where b2>0 is an adjustment parameter, ˜α2=α2ˆα2 is the estimate error and ˆα2 is the estimator of the parameter α2.

    Applying (2.3), (3.14) and (3.16), it can be gotten that

    Λ2=ξ32(Hχp3+f2β1)1b2˜α2˙ˆα2+32h2β1χ1h12ξ22. (3.17)

    Besides, applying Lemma 3 renders

    32h2β1χ1h12ξ2234h2β1χ1h14ξ42+34.

    On the other hand, we gets

    S1(ξ1)ξ31(χp2βp1)S1(ξ1)|ξ1|3|χp2βp1|DS1(ξ1)|ξ1|3(|ξ2|p+φp1|ξ1|p1|ξ2|)ρ1ξp+31+τ2ξp+32+pσ12p+3ξp+32, (3.18)

    where D=(2p2+2)p; ρ1=1p+3[3(DS1(ξ1))p+33σp312+(p+2)S1(ξ1)], τ2=S1(ξ1)φp(p+3)1p+3, and σ12>0 is an adjustment parameter.

    Thus, from (3.13), (3.17) and (3.18), we have

    V2=V1+Λ2ϱ1ε42πtan(πξ412ε4)d12b1˜α21Hϱ1ξp+311b2˜α2˙ˆα2+Hξ32(χp3βp2)+Hξ32βp2+Hξ32F2(Z2)+Hpσ12p+3ξp+32+Q1+34, (3.19)

    where Z2=(ˉx2,ˆα1)T,

    F2(Z2)=1H[f2β1]+τ2ξp2+34Hh2β1χ1h14ξ2.

    Obviously, the continuity of F2(Z2) can be directly proved by the fact that the functions f2(ˉχ2), h2(ˉχ2) and β1 are all continuous. Thus, F2(Z2) can be approximated as

    F2(Z2)=ΥT2Ψ2(Z2)+ϵ2(Z2), (3.20)

    where |ϵ2(Z2)|δ2 and δ2>0 is a given constant.

    In view of the fact ΨT2()Ψ2()1 and Lemma 3, we obtain

    ξ32F2(Z2)|ξ2|3(Υ2Ψ2+δ2)3σ21α2p+3ξp+32+pp+3σ3p21+3p+3ξp+32+pp+3δp+3p2, (3.21)

    where α2=Υ2p+33 and σ21>0 is an adjustment parameter.

    Substituting (3.21) into (3.19) yields

    V2ϱ1ε42πtan(πξ412ε4)d12b1˜α21Hϱ1ξp+31+Hξ32(χp3βp2)+Hξ32βp2+3Hp+3[σ21ˆα2+1]ξp+32+Hpσ12p+3ξp+32+H˜α2[3σ21p+3ξp+321b2H˙ˆα2]+Q1+34+pHp+3σ3p21+pHp+3δp+3p2. (3.22)

    Then, one can design

    β2=M1p2ξ2φ2ξ2 (3.23)

    and

    ˙ˆα2=3Hb2σ21p+3ξp+32d2ˆα2, (3.24)

    where M23p+3[σ21ˆα2+1]+pσ12p+3+ρ2+ϱ2>0; ϱ2>0,d2>0 are adjustment parameters. The value of ρ2>0 will be given in the next step.

    In addition, it is evident that

    d2b2ˆα2˜α2d2˜α222b2+d22b2ˆα22. (3.25)

    Substituting (3.25) into (3.22), one gets

    V2ϱ1ε42πtan(πξ412ε4)2j=1dj2bj˜α21H2j=1ϱjξp+3j+Hξ32(χp3βp2)+2j=1Qj, (3.26)

    where Q2=34+pHp+3σ3p12+pHp+3δp+3p2+d2α222b2.

    Inductive Step (3kn). In view of above two steps, we can deduce the following similar property whose proof can be found in the Appendix.

    Proposition 1. For the kth Lyapunov function Vk:ΠkR+ as

    Vk=Vk1+Λk (3.27)

    with

    Λk=14ξ4k+12bk˜α2k, (3.28)

    there exists a virtual controller βk and the adaptive law of ˆαk of the following forms

    βk=M1pkξkφkξk, (3.29)
    ˙ˆαk=3Hbkσk1p+3ξp+3kdkˆαk, (3.30)

    such that

    Vkϱ1ε42πtan(πξ412ε4)kj=1dj˜α2j2bjHρkξp+3kHkj=1ϱjξp+3j+kj=1Qj+Hξ3k(χpk+1βpk), (3.31)

    where Mk3p+3[σk1ˆαk+1]+pσk12p+3+ρk+ϱk>0; bk,ϱk,dk>0 are adjustment parameters; and the value of ρk>0 will be given in the next step.

    Step n According to above steps, there exist a series of virtual controllers and adaptive parameter laws (βk,ˆαk)(k=1,,n) make that Eq (3.31) holds when k=n with χn+1=ν. Therefore, the fuzzy adaptive control law can be designed as

    βn=M1pnξnφnξn, (3.32)
    ˙ˆαn=3Hbnσn1p+3ξp+3ndnˆαn. (3.33)

    Apparently, one can further get

    Vnϱ1ε42πtan(πξ412ε4)nj=1dj˜α2j2bjHnj=1ϱjξp+3j+nj=1Qj+Hξ3n(νpβpn). (3.34)

    By the definitions of ξk(k=1,,n), one gets the fuzzy state-feedback controller

    βn=(ˉφ1χ1++ˉφnχn), (3.35)

    where ˉφk=nj=kφj for k=1,,n.

    In this subsection, a fuzzy output-feedback controller will be designed by combining the above-constructed state-feedback controller with the state-observer constructed later. Since χ2,,χn are unmeasurable, a reduced-order observer is required. Firstly, define a series of new variables as follows:

    zi=χiγiγ2χ1,i=2,,n.

    Then, it directly gets

    dzi=H(χpi+1γiγ2χp2)dt+(fiγiγ2f1)dt+[hiγiγ2h1]Tdω,i=2,,n1,dzn=H(νpγnγ2χp2)dt+(fnγnγ2f1)dt+[hnγnγ2h]Tdω,

    where γi1(i=2,,n) are gain parameters to be determined. Hence, the (n1)-dimensional observer can be constructed as [36]

    ˙ˆzi=H(ˆzi+γiγ2χ1)pHγiγ2(ˆz2+γ2χ1)p,i=2,,n1,˙ˆzn=HνpHγnγ2(ˆz2+γ2χ1)p. (3.36)

    According to (3.36), the estimate ˆχi of χi can be gotten by

    ˆχi=ˆzi+γiγ2χ1,i=2,,n. (3.37)

    Thus, one constructs the implementable controller of system (2.4) by using Eq (3.35) and the certainty equivalence principle as below:

    ν=(ˉφ1ˆχ1++ˉφnˆχn). (3.38)

    Therefore, the output-feedback controller of origin system (2.1) is

    u=Hqn+1ν=Hqn+1(ˉφ1ˆχ1++ˉφnˆχn). (3.39)

    In this section, we will analyze the appropriate values of the gains γi(i=2,,n) and some constant parameters in output-feedback controller.

    To determine the observer gains γ2,,γn, we first define the error dynamics

    eiχiˆχi,i=2,,n. (3.40)

    Further, the following coordinate transformation is introduced

    ˜e2=e2,˜e3=e3γ3e2,,˜en=enγnen1. (3.41)

    It can easily infer from (3.40) and (3.41) that

    d˜ei=H[(χpi+1ˆχpi+1)γi(χpiˆχpi)]dt+[fiγifi1]dt+[hiγihi1]Tdω,i=2,,n1d˜en=Hγn(χpnˆχpn)dt+[fnγnfn1]dt+[hnγnhn1]Tdω. (3.42)

    Now, a proposition is provided for helping to determine gain constants, whose proof will be given in Appendix.

    Proposition 2. For the Lyapunov function

    Un=14γni=2˜e4i,

    by utilizing Lemmas 2-5, Eqs (2.3) and (3.42), it is not difficult to obtain

    UnH[ni=2γγi2p1˜ep+3i+ni=2ˉci˜ep+3i+ni=26γp+33(p+3)Hp+33˜ep+3i]+(p1)Hp+3+˜F1(χ), (3.43)

    where γ>0 is an adjustment constant; ˉci=ˉci(γi+1,,γn)>0,(i=2,,n1) are constants independent of H; and ˉcn is a constant independent of H and γi(i=2,,n); and ˜F1(χ)=Hni=2[14(fiγifi1)4+3γ234H23hiγihi14+2p1p+3χp+3i] is an unknown continuous function.

    Besides, we can obtain from Lemmas 2-4 that

    |ξ3n(νpβpn)|D|ξn|3|νβn|[|νβn|p+|βn|p]D(n1)p|ξn|3ni=2ˉφpi|ei|p+D|ξn|3(ni=2ˉφi|ei|)φp1n|ξn|p1p+1p+3ni=2ep+3i+τnξp+3n˜ιini=2˜ep+3i+˜F2(ξn), (3.44)

    where ˜F2(ξn)=τnξp+3n; τn=3p+3ni=2[D(n1)pˉφpi]p+33+p+2p+3ni=23[D(n1)pφp1nˉφi]p+3p+2; ˜ιn=np+2p+1p+3 and ˜ιi=˜ιi(γi+1,,γn)(i=2,,n1) are positive constants.

    Then, substituting (3.44) into (3.34) yields

    Vnϱ1ε42πtan(πξ412ε4)nj=1dj˜α2j2bjHnj=1ϱjξp+3j+nj=1Qj+Hni=2˜ιi˜ep+3i+˜F2(ξn). (3.45)

    Then, define the entire Lyapunov function V=Vn+Un. Apparently, it directly infers from Proposition 2 and Eq (3.45) that

    V=Vn+Unϱ1ε42πtan(πξ412ε4)nj=1dj˜α2j2bjHnj=1ϱjξp+3j+˜F()+nj=1QjHni=2[γγi2p1ˉci˜ιi]˜ep+3i+Hni=26γp+33(p+3)Hp+33˜ep+3i+(p1)Hp+3, (3.46)

    where ˜F()=˜F1()+˜F2().

    Using FLS to deal with the unknown function ˜F(), one deduces from Lemma 7 that ˜F()=ΥT0Ψ0+ϵ0()Υ0Ψ0+δ03p+3α0+pp+3+δ0 where α0=Υ0p+33.

    Therefore, the observer gains γ2,,γn and constant H can be chosen in the following recursive manner

    γnmax{2p1γ(ˉcn+˜ιn+1+θn),1},γn1max{2p1γ(ˉcn1(γn)+˜ιn1(γn)+1+θn1),1},γ2max{2p1γ(ˉc2(γn,,γ3)+˜ι2(γn,,γ3)+1+θ2),1},Hmax{1,(6p+3)3p+3γ}. (3.47)

    Then, Eq (3.46) turns into

    Vϱ1ε42πtan(πξ412ε4)nj=1dj˜α2j2bjHni=1ϱiξp+3iHni=2θi˜ep+3i+Q, (3.48)

    where θi(i=2,,n) are positive constants, and Q=ni=1Qj+(p1)Hp+3+3p+3α0+pp+3+δ0.

    On the other hand, it can be verified from Lemma 3 that

    ˜e4i4p+3˜ep+3i+p1p+3,ξ4i4p+3ξp+3i+p1p+3, (3.49)

    which renders

    Hni=2θi˜ep+3ini=2ˉθi4˜e4i+p14Hni=2θi,Hni=2ϱiξp+3ini=2ˉϱi4ξ4i+p14Hni=2ϱi, (3.50)

    where i=2,,n, ˉθi=(p+3)Hθi and ˉϱi=(p+3)Hϱi. Further, we get

    Vϱ1ε42πtan(πξ412ε4)nj=1dj˜α2j2bjni=2ˉϱi4ξ4ini=2ˉθi4˜e4i+ˉQ, (3.51)

    where ˉQ=Q+p14Hni=2θi+p14Hni=2ϱi.

    To state the main result, the following theorem is presented.

    Theorem 1. For the p-norm stochastic nonlinear system (2.1) and a given constant, there exists a finite-time fuzzy output-feedback controller (3.39) together with the parameter adaptive laws (3.12), (3.24), (3.30), and (3.33) such that

    i) the system output isn't violated in the sense of probability, i.e., P{|y(t)|<ε}=1.

    ii) all the signals in the closed-loop stochastic nonlinear system (2.1) are SGFSP.

    Proof. ⅰ) Let μ0=min{ϱ1,d1,,dn,ˉϱ2,ˉϱn,ˉθ2γ,ˉθnγ} and π0=ˉQ. Then, Eq (3.51) can be expressed as

    Vμ0V+π0. (3.52)

    We can easily get from Eq (3.52) that

    EV(t)V(t0)eμ0t+π0μ0. (3.53)

    For x(0)=(x1(t0),,xn(t0))T satisfying x1(t0)Π1, it easily obtains that the mean of V(t) is bounded, which implies that V is bounded in probability. It can be directly deduced from the definition of V that

    P{VB(ξ1)<}=1. (3.54)

    Consequently, it is clear that P{|y(t)|<ε}=P{|ξ1(t)|<ε}=1, which demonstrates that the output constraint of system (2.1) is not violated in the sense of probability.

    ⅱ) For 0<ˉς0<1, it is easy to get from Lemma 3 that

    Vˉς0ˉς0V+(1ˉς0).

    Further, one has

    μ0Vμ0ˉς0Vˉς0+(1ˉς0)μ0ˉς0. (3.55)

    Then, substituting (3.55) into (3.52) drives

    Vˉμ0Vˉς0+ˉπ0, (3.56)

    where ˉμ0=μ0ˉς0 and ˉπ0=(1ˉς0)μ0ˉς0+π0.

    Let T=1l0ˉμ0(1ˉς0)[E(V1ˉς0(χ(0),˜e(0),ˆα(0)))(ˉπ0ˉμ0(1ˉς0))1ˉς0ˉς0] where χ(0)=(χ1(t0),,χn(t0))T, ˜e(0)=(˜e2(t0),,˜en(t0))T, ˆα(0)=(ˆα1(t0),,ˆαn(t0)), 0<l0<1 is a constant. Then it follows from Lemma 1 that for tt0+T, E(V1ς(χ,˜e,ˆα))ˉπ0ˉμ0(1ˉς0), which means that all the signals in the closed-loop systems are semi-global finite-time stable in probability.

    Remark 6. In this paper, we construct an output-feedback controller rather than the designed state-feedback controllers in existing results about output constraints. On the other hand, it should be pointed out the considered constraint is symmetric rather than asymmetric, which leads that the proposed scheme can not be directly employed or further extended to the case of asymmetric constraints. However, a control scheme based on a new BLF can be developed for asymmetric output constraints in a similar way to this paper. In addition, another limitation is that all of the fractional powers are equal to p. If pi's are taken different values, the proposed strategy seems not applicable. In the future, we will address the two issues.

    The validation of the proposed strategy will be testified by the following system.

    {dx1=x1352dt+2ln(1+x21)dt+4x21dω,dx2=u135dt+x1x22dt+x22dω,y=χ1, (4.1)

    where the output y=x1 is measurable and constrained by Π1={y(t)R,|y(t)|<1}, and the state x2 is unmeasurable.

    According to the controller design procedure, we can respectively design the finite-time output-feedback controller, the adaptive laws and the observer as follows:

    u=H90169(M5131x1+M5132ˆχ2),˙ˆα1=15Hb1σ1128(S1(x1))2815x2851d1ˆα1,˙ˆα2=15Hb2σ2128ξ2852d2ˆα2,˙ˆz2=Hν135Hγ2(ˆz2+γ2x1)135,ˆχ2=ˆz2+γ2x1, (4.2)

    where M1=1528(S1(x1))1315[σ11ˆα1+1]+ρ1S1(x1)+ϱ1 and M2=1528[σ21ˆα2+1]+13σ1228+ρ2+ϱ2.

    Now, we choose the related parameters as γ=1.5,σ11=22,σ21=20,σ12=1, θ2=3, b1=b2=40, d1=d2=2, ϱ1=ϱ2=1 and infer H=1.6,γ2=8.1. Next, the initial states and adaptive parameters are selected as [x1(0),x2(0),ˆx2(0),ˆα1,ˆα2]T=[0.4,8,8,10,10]T the simulation results are displayed in Figures 14.

    Figure 1.  Trajectory of x1(t) with ε=1.
    Figure 2.  Trajectory of x2(t) with ε=1.
    Figure 3.  Trajectory of u.
    Figure 4.  Trajectory of ˆα.

    Figure 1 provides the trajectory of x1(t), which indicates that the system output constraint is not violated under controller (4.2). Meanwhile, the trajectories of x2(t) and ˆx2(t) are given in Figure 2, which shows that x2(t) is well estimated by ˆx2(t). Moreover, the trajectory of the controller u is displayed in Figure 3. Finally, Figure 4 expresses the curves of the adaptive parameter vector under the developed strategy. Also, one could evidently observe from these figures that all the signals of system (4.1) are semi-global finite-time stable in probability under controller (4.2).

    In this paper, the output-feedback controller design problem is investigated for a class of p-norm stochastic nonlinear systems with output constraints. Through using a tan-type BLF, an adaptive fuzzy state-feedback controller is proposed by the adding a power integrator technique. Then, a finite-time fuzzy output-feedback controller is constructed by combining the proposed state-feedback controller and a reduced-order observer. Both rigorous proof and the simulation example verify that the designed controller can ensure the achievement of the system output constraint and semi-global finite-time stability of all the signals in probability. In the future, we will consider the situations of asymmetric constraints, different fractional powers, or multi-input multi-output stochastic nonlinear systems.

    This work was supported by supported by the National Science Foundation of China under Grant 61973142, the Jiangsu Natural Science Foundation for Distinguished Young Scholars under Grant BK20180045, the Priority Academic Program Development of Jiangsu Higher Education Institutions, and the Project of Anhui Province Outstanding Young Talent Support Program under Grant gxyq2018089.

    The authors declare that there are no conflicts of interest.

    Proof of Proposition 1. Firstly, suppose there exist βk1(3kn) such that

    Vk1ϱ1ε42πtan(πξ412ε4)k1j=1dj˜α2j2bjHρk1ξp+3k1Hk1j=1ϱjξp+3j+k1j=1Qj+Hξ3k1(χpkβpk1). (A.1)

    At the same time, from Itˆo's formula and (3.1), one gets

    dξk=(Hχpk1+fkβk1)dt+(hkk1j=1βk1χjhj)Tdω, (A.2)

    where βk1=k1j=1βk1χj(Hχpj+1+fj)+Σk1j=1βk1ˆαj˙ˆαj+12k1j,l=12βk1χjχlhTjhl. Clearly, βk1 is valid and continuous, which can be illustrated in a similar way by following the lines to obtain β1.

    We choose the Lyapunov function as

    Vk=Vk1+Λk (A.3)

    with

    Λk=14ξ4k+12bk˜α2k, (A.4)

    where bk>0 is an adjustment parameter, ˜αk=αkˆαk is the parameter error, and ˆαk is the estimation of the unknown parameter αk.

    Applying (2.3), (A.2) and (A.4), one can obtain

    Λk=ξ3k(Hχpk+1+fkβk1)1bk˜αk˙ˆαk+32hkk1j=1βk1χjhj2ξ2k. (A.5)

    It is not difficult to get from Lemma 3 that

    32hkk1j=1βk1χjhj2ξ2k34hkk1j=1βk1χjhj4ξ4k+34. (A.6)

    On the other hand, from Lemmas 2 and 3, one can verify

    ξ3k1(χpkβpk1)D|ξk1|3[|ξk|p+φp1k1|ξk1|p1|ξk|]ρk1ξp+3k1+τkξp+3k+pσk12p+3ξp+3k, (A.7)

    where ρk1=1p+3[3Dp+33σp312+p+2], τk=φ(p1)(p+3)1p+3, and σk12>0 is an adjustment parameter.

    From (A.1)-(A.7), it can be deduced that

    Vk=Vk1+Λkϱ1ε42πtan(πξ412ε4)k1j=1dj˜α2j2bjHk1j=1ϱjξp+3j+k1j=1Qj+34+Hpσk12p+3ξp+3k+Hξ3kFk(Zk)+Hξ3k(χpk+1βpk)+Hξ3kβpk (A.8)

    where Zk=(ˉχTk,ˉˆαTk1)T, ˉˆαk1=(ˆα1,,ˆαk1)T and

    Fk(Zk)=1H(fkβk1)+τkξpk+34hkk1j=1βk1χjhj4ξk.

    Similar to the first two steps, Fk(Zk) can also be approximated as

    Fk(Zk)=ΥTkΨk(Zk)+ϵk(Zk), (A.9)

    where |ϵk(Zk)|δk and δk>0 is a given constant.

    One directly obtains from Eq (A.9) and Lemma 3 that

    ξ3kFk(Zk)|ξk|3(ΥkΨk+δk)3σk1αkp+3ξp+3k+pp+3σ3pk1+3p+3ξp+3k+pp+3δp+3pk, (A.10)

    where αk=Υkp+33 and σk1>0 is an adjustment parameter.

    Substituting (A.10) into (A.8) renders

    Vkϱ1ε42πtan(πξ412ε4)k1j=1dj˜α2j2bjHk1j=1ϱjξp+3j+Hξ3k(χpk+1βpk)+3Hp+3[σk1ˆαk+1]ξp+3k+Hpσk12p+3ξp+3k+Hξ3kβpk+k1j=1Qj+H˜αk[3σk1p+3ξp+3k1bkH˙ˆαk]+34+pHp+3σ3pk1+pHp+3δp+3pk. (A.11)

    Then, we can design

    βk=M1pkξkφkξk,˙ˆαk=3Hbkσk1p+3ξp+3kdkˆαk, (A.12)

    where Mk3p+3[σk1ˆαk+1]+pσk12p+3+ρk+ϱk; ϱk,dk>0 are adjustment parameters; and the value of ρk>0 will be given in (k+1)th step.

    Moreover, one has

    dkbkˆαk˜αkdk2bk˜α2k+dk2bkˆα2k. (A.13)

    From (A.1)-(A.13), it can be deduced that

    Vkϱ1ε42πtan(πξ412ε4)kj=1dj˜α2j2bjHkj=1ϱjξp+3jHτkξp+3k+kj=1Qj+Hξ3k(χpk+1βpk), (A.14)

    where Qk=34+pHp+3σ3pk1+pHp+3δp+3pk+dkα2k2bk. The proof of Proposition 1 is completed.

    Proof of Proposition 2. By the definition of Un, one has

    Un=Hγn1i=2˜e3i(χpi+1ˆχpi+1)Hγni=2˜e3iγi(χpiˆχpi)+γni=2˜e3i(fiγifi1)+32γni=2˜e2ihiγihi12=Hni=2γγi˜e3i[(ˆχi+˜ei)pˆχpi]Hni=2γγi˜e3i[χpi(ˆχi+˜ei)p]+Hni=3γ˜e3i1(χpiˆχpi)+Hni=2γH˜e3i(fiγifi1)+Hni=23γ2H˜e2ihiγihi12. (A.15)

    By Lemma 5, one can infer

    γγi˜e3i[(ˆχi+˜ei)pˆχpi]=γγi˜e2i(ˆχi+˜eiˆχi)[(ˆχi+˜ei)pˆχpi]γγi2p1˜ep+3i. (A.16)

    Since χiˆχi˜ei=i1j=2γiγj+1˜ej, we can get that through applying Lemmas 2-5

    |γγi˜e3i[χpi(ˆχi+˜ei)p]|γγi|˜ei|3|χiˆχi˜ei||(χiˆχi˜ei)p1+χp1i|γi|˜ei|3(i1j=2γiγj+1|˜ej|)p+γi|˜ei|3[1p(i1j=2γiγj+2|˜ej|)p+p1p|χi|p]3γγip+3˜ep+3i+pγγip+3(i1j=2γiγj+1|˜ej|)p+3+3γγip(p+3)˜ep+3i+γγip+3(i1j=2γiγj+2|˜ej|)p+3+3(p1)(γγi)p+33p(p+3)˜ep+3i+p1p+3χp+3iij=2˜aij˜ep+3j+p1p+3χp+3i, (A.17)

    where ˜aij=˜aij(γi,,γj+1) is a constant independent of H.

    Noting that ei=i1j=2γiγj+1˜ej+˜ei, one has

    |γ˜e3i1(χpiˆχpi)|=γ|˜ei1|3|χpi(χiei)p|2pγ|˜ei1|3(|χi|p+|ei|p)3(2pγ)p+33p+3˜ep+3i1+pp+3χp+3i+3(2pγ)p+33p+3˜ep+3i1+pp+3ep+3i6(2pγ)p+33p+3˜ep+3i1+p2p+2p+3[ξp+3i+φp+3i1ξp+3i1]+pip+2p+3[˜ep+3i+i1j=2(γiγj+1)p+3˜ep+3j]ij=2˜cij(γi,,γj+1)˜ep+3j+pp+3χp+3i, (A.18)

    where ˜cij=˜cij(γi,,γj+1) is a constant independent of H.

    In addition, we have

    γH˜e3i(fiγifi1)+32γH˜e2ihiγihi123γ432H43˜e4i+14(fiγifi1)4+γ234H23hiγihi146γp+33(p+3)Hp+33˜ep+3i+p1p+3+14(fiγifi1)4+3γ234H23hiγihi14. (A.19)

    Substituting (A.16)-(A.19) into (A.15) yields

    UnH[ni=2γγi2p1˜ep+3ini=2ˉci˜ep+3i6γp+33(p+3)Hp+33˜ep+3i]+(p1)Hp+3+ni=2(2p1)Hp+3χp+3i+ni=2H[14(fiγifi1)4+3γ234H23hiγihi14],

    where ˉci=ij=2(˜aji+˜cji). The proof of Proposition 2 is completed.



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