Research article

Further results on stability analysis of time-varying delay systems via novel integral inequalities and improved Lyapunov-Krasovskii functionals

  • This work develops some novel approaches to investigate the stability analysis issue of linear systems with time-varying delays. Compared with the existing results, we give three innovation points which can lead to less conservative stability results. Firstly, two novel integral inequalities are developed to deal with the single integral terms with delay-dependent matrix. Secondly, a novel Lyapunov-Krasovskii functional with time-varying delay dependent matrix, rather than constant matrix is constructed. Thirdly, two improved stability criteria are established by applying the newly developed Lyapunov-Krasovskii functional and integral inequalities. Finally, three numerical examples are presented to validate the superiority of the proposed method.

    Citation: Xingyue Liu, Kaibo Shi. Further results on stability analysis of time-varying delay systems via novel integral inequalities and improved Lyapunov-Krasovskii functionals[J]. AIMS Mathematics, 2022, 7(2): 1873-1895. doi: 10.3934/math.2022108

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  • This work develops some novel approaches to investigate the stability analysis issue of linear systems with time-varying delays. Compared with the existing results, we give three innovation points which can lead to less conservative stability results. Firstly, two novel integral inequalities are developed to deal with the single integral terms with delay-dependent matrix. Secondly, a novel Lyapunov-Krasovskii functional with time-varying delay dependent matrix, rather than constant matrix is constructed. Thirdly, two improved stability criteria are established by applying the newly developed Lyapunov-Krasovskii functional and integral inequalities. Finally, three numerical examples are presented to validate the superiority of the proposed method.



    As is known to all, time delays exist in the natural dynamic systems, such as transport, communication, or measurement widely. Time delay causes undesirable dynamic behaviors such as oscillation, performance deterioration, limit cycles and even instability in the model[1,2]. Thus the research about stability analysis of time-delay systems has been of great significance[3,4,5,6,7,8,9]. It has attracted enormous attention of many researchers[10,11,12,13,14,15,16,17,18].

    In general, the problem of stability analysis for time-delay systems can be divided into two categories. That are constant and time-varying delay systems. The stability criteria of time-varying delay systems are less conservatism than that of constant delay systems, owing to the full use of time delay information in stability analysis of time delay systems. The stability analysis of constant delay systems is described in literature[19].

    However, more efforts have been paid to analyze stability of time-varying delay systems. The main approach to measure conservatism is calculating the maximal admissible delay upper bounds(MADUPS). There are two major directions to reduce conservatism, namely the Lyapunov-Krasovskii functional(LKF)[20,21] structure and Linear matrix inequality(LMI) technique. There are two approaches to construct suitable LKF, namely, augmented Lyapunov-Krasovskii functional approach(ALFA) and multiple integral Lyapunov-Krasovskii functional approach(MILFA). The former introduces more state information into the vector of the positive quadratic terms. The latter adopts multiple integral terms to the LKF. Literature[22,23] proposed a new formed LKF for time-varying delay systems. Although the conservatism of the stability criteria for time-varying delay systems is reduced in the above literatures. They all introduce the constant matrix in the positive quadratic terms, such as ttτ˙xT(s)Q˙x(s)ds, which makes the conclusion conservative. Secondly, for LMI techniques, there are some useful inequalities were developed, for example, Jensen's inequality(JI)[24], Wirtinger-based integral inequality(WBII)[25], free matrix-based integral inequality(FMBLL)[26] and other LMI techniques[27,28,29,30,31,32,33,34,35].

    A new type of LKF with time-varying delay dependent matrix is constructed, which is th1th(t)˙xT(s)(Q10+(h1h(t))Q11)˙x(s)ds+th(t)th2˙xT(s)(Q20+(h2h(t))Q21)˙x(s)ds, which makes more use of the time-varying delay information in time-varying delay systems. And the influence of the time-varying rate on the stable operation of system is considered, which plays an important role in reducing the conservatism of the system.

    Two novel time delay partition inequalities are developed in this work for estimating the single integral terms with time-varying delay information. The proposed one can derive bigger MADUPS of time-varying delay systems.

    Two stability criteria of time-varying delay system are established by applying the above LKF and inequalities. Based on three numerical examples, the advantages of the stability criteria are verified through the comparison of MADUPS with different criteria.

    Notation: Let Rn denotes n-dimensional Euclidean space, Rn×n denotes the set of all n×n real matrices, Sn+ represents a set of positive definite matrices with n×n dimensions, P>0 stands for that the matrix P is real symmetric positive definite matrix, 0n×3n represents the zero element matrix with the n×3n dimensions, XT is the transpose of matrix X, He{X}=X+XT. in the matrix represents the symmetry of matrix.

    The time-varying delay system model can be obtained from following equation:

    {˙x(t)=Ax(t)+Bx(th(t))x(t)=ϕ(t)t[h2,0]. (2.1)

    where x(t)Rn is the state vector. A and B are constant matrices with appropriate dimensions. ϕ(t) is a given vector-valued initial function. The time delay, h(t), is a time-varying continuous function that satisfies:

    h1h(t)h2μ˙h(t)μ. (2.2)

    where 0h1<h2 and μ is a positive constant. Note that h1 may not be equal to 0. The initial condition, ϕ(t), is a continuous vector-valued initial function of t[h2,0].

    Before deriving the main results, the following lemmas should be introduced. When we set h10, and change the single integral terms tth(t)˙xT(s)R˙x(s)dsth(t)th2˙xT(s)R˙x(s)ds in [29] as th1th(t)˙xT(s)R˙x(s)dsth(t)th2˙xT(s)R˙x(s)ds, the following Lemma 1 and 2 can be obtained from Lemma 4 and 6 in [29].

    Lemma 1. For a block symmetric matrix ˉR=diag{R,3R} with RSn+ and any matrix SR2n×2n, the single integral terms can be estimated as:

    th1th(t)˙xT(s)R˙x(s)ds+th(t)th2˙xT(s)R˙x(s)ds1h2h1ζT1(t)[E1E2]T(M(h(t))N(h(t)))[E1E2]ζ1(t). (2.3)

    where

    ζ1(t)=col{x(t),x(th(t)),x(th1),x(th2),th1th(t)x(s)h(t)h1ds,th(t)th2x(s)h2h(t)ds,˙x(t),˙x(th(t)),˙x(th1),˙x(th2)},
    ei=[0n(i1)n,In,0n(10i)n](i=1,2,,10),
    E1=[e3e2e3+e22e5],E2=[e2e4e2+e42e6],
    M(h(t))=[α1ˉRSα2ˉR],N(h(t))=[α3SˉR1ST0α4STˉR1S],
    α1=2h2h1h(t)h2h1,α2=h(t)+h22h1h2h1,α3=h2h(t)h2h1,α4=h(t)h1h2h1.

    Lemma 2. For a block symmetric matrix ˆR=diag{R,3R,5R} with RSn+ and any matrix S1R3n×3n, the single integral terms can be estimated as:

    th1th(t)˙xT(s)R˙x(s)ds+th(t)th2˙xT(s)R˙x(s)ds1h2h1ζT2(t)[E3E4]T(R(h(t))S(h(t)))[E3E4]ζ2(t). (2.4)

    where

    ζ2(t)=col{x(t),x(th(t)),x(th1),x(th2),th1th(t)x(s)h(t)h1ds,th(t)th2x(s)h2h(t)ds,˙x(t),˙x(th(t)),˙x(th1),˙x(th2),th1th(t)th1sx(u)(h(t)h1)2duds,th(t)th2th(t)sx(u)(h2h(t))2duds},
    υi=[0n(i1)n,In,0n(12i)n](i=1,2,,12),
    E3=[υ3υ2υ3+υ2υ5υ3υ2+6υ512υ11],E4=[υ2υ4υ2+υ42υ6υ2υ4+6υ612υ12],
    R(h(t))=[α1ˆRS1α2ˆR],S(h(t))=[α3S1ˆR1ST10α4ST1ˆR1S1].

    It can be seen that, Lemma 1 and 2 can be applied to estimate the single integral terms with the same Lyapunov matrix.

    Different form the Lemma 1 and 2, we consider that the Lyapunov matrix in two single integral terms is different, such as th1th(t)˙xT(s)R1˙x(s)dsth(t)th2˙xT(s)R2˙x(s)ds, the following Lemma 3 and 4 can be obtained.

    Lemma 3. For the block symmetric matrices ˉR31=diag{R1,3R1}, ˉR32=diag{R2,3R2} with R1 and R2Sn+, and any matrix S2R2n×2n, the single integral terms can be estimated as:

    th1th(t)˙xT(s)R1˙x(s)ds+th(t)th2˙xT(s)R2˙x(s)ds1h2h1ζT1(t)[E1E2]T(M(h(t))N(h(t)))[E1E2]ζ1(t). (2.5)

    where

    M(h(t))=[α1ˉR31S2α2ˉR32],N(h(t))=[α3S2ˉR132ST20α4ST2ˉR131S2].

    Proof. We can obtain the following equations when setting γ1(s,a,b)=2sbaba.

    ba˙x(s)ds=x(b)x(a),baγ1(s,a,b)˙x(s)ds=x(b)+x(a)2babax(s)ds,baγ1(s,a,b)=0,baγ21(s,a,b)=ba3. (2.6)

    The following equations hold based on Schur complement when there exist symmetric matrices R1>0, R2>0, and any matrices Mi,i=1,2,3,4 with appropriate dimensions.

    [M1R11MT1M1R11MT2M1M2R11MT2M2R1]0,[M3R12MT3M3R12MT4M3M4R12MT4M4R2]0.

    Then the following inequalities can be obtained.

    Ξ1=th1th(t)[u1f1u1˙x(s)]T[M1R11MT1M1R11MT2M1M2R11MT2M2R1[[u1f1u1˙x(s)]ds0.Ξ2=th(t)th2[u1f2u1˙x(s)]T[M3R12MT3M3R12MT4M3M4R12MT4M4R2[[u1f2u1˙x(s)]ds0. (2.7)

    Where u1=[ET1,ET2]Tζ1(t), f1=γ1(s,th(t),th1), f2=γ1(s,th2,th(t)).

    The matrices Mi(i=1,,4) and S2 are defined as following, for any matrices Li,i=1,2,3,4 with appropriate dimensions.

    M1=1h2h1[R1,0,LT1]T,M2=1h2h1[0,3R1,LT2]T,
    M3=1h2h1[LT3,R2,0]T,M4=1h2h1[LT4,0,3R2]T,S2=[L1,L2]T=[L3,L4].

    Based on Eq (2.6), the simple algebraic calculation is as follow:

    th1th(t)[u1f1u1]T[M1R11MT1M1R11MT2M2R11MT2][u1f1u1]ds=1h2h1ζT1(t)[E1E2]T(h1h(t)h2h1)[ˉR31S2ST2ˉR131S2][E1E2]ζ1(t).
    2th1th(t)[u1f1u1]T[M1M2]˙x(s)ds=1h2h1ζT1(t)[E1E2]T[2ˉR31S20][E1E2]ζ1(t).
    th(t)th2[u1f2u1]T[M3R12MT3M3R12MT4M4R12MT4][u1f2u1]ds=1h2h1ζT1(t)[E1E2]T(h(t)h2h2h1)[S2ˉR132ST2S2ˉR32][E1E2]ζ1(t).
    2th(t)th2[u1f2u1]T[M3M4]˙x(s)ds=1h2h1ζT1(t)[E1E2]T[0S22ˉR32][E1E2]ζ1(t).

    Then we can obtain the following equation.

    Ξ1+Ξ2=th1th(t)˙x(s)R1˙x(s)dsth(t)th2˙x(s)R2˙x(s)ds+1h2h1ζT1(t)[E1E2]T(M(h(t))N(h(t)))[E1E2]ζ1(t).

    The Eq (2.7) can lead to Ξ1+Ξ20. Thus the inequality (2.5) can be derived.

    Lemma 4. For the block symmetric matrices ˉR41=diag{R1,3R1,5R1}, ˉR42=diag{R2,3R2,5R2} with R1 and R2Sn+, and any matrix S3R3n×3n, the single integral terms can be estimated as:

    th1th(t)˙xT(s)R1˙x(s)ds+th(t)th2˙xT(s)R2˙x(s)ds1h2h1ζT2(t)[E3E4]T(R(h(t))S(h(t)))[E3E4]ζ2(t). (2.8)
    R(h(t))=[α1ˉR41S3α2ˉR42]S(h(t))=[α3S3ˉR142ˉST30α4ST3ˉR141S3].

    Proof. The following equations can be obtained by setting γ1(s,a,b)=2sbaba and γ2(s,a,b)=6s26(a+b)s+b2+4ab+a2(ba)2.

    baγ2(s,a,b)˙x(s)ds=x(b)x(a)+6babax(s)ds12(ba)2babsx(u)duds,baγ22(s,a,b)ds=ba5,baγ1(s,a,b)γ2(s,a,b)ds=0,baγ2(s,a,b)ds=0. (2.9)

    The following equations also hold based on Schur complement when there exist symmetric matrices R1>0, R2>0, and any matrices Ni,i=1,2,3,4 with appropriate dimensions.

    [N1R11NT1N1R11NT2N1R11NT3N1N2R11NT2N2R11NT3N2N3R11NT3N3R1]0. (2.10)
    [N4R12NT4N4R12NT5N4R12NT6N4N5R12NT5N5R12NT6N5N6R12NT6N6R2]0. (2.11)

    Then the following inequalities can be derived.

    Ξ3=th1th(t)[u2f1u2f3u2˙x(s)]T[N1R11NT1N1R11NT2N1R11NT3N1N2R11NT2N2R11NT3N2N3R11NT3N3R1][u2f1u2f3u2˙x(s)]ds0.Ξ4=th(t)th2[u2f2u2f4u2˙x(s)]T[N4R12NT4N4R12NT5N4R12NT6N4N5R12NT5N5R12NT6N5N6R12NT6N6R2][u2f2u2f4u2˙x(s)]ds0.

    Where u2=[ET3,ET4]Tζ2(t), S3=[L5,L6,L7]T=[L8,L9,L10] and matrices Ni(i=1,,6) are defined for any matrices Li,(i=5,6,,10)

    N1=1h2h1[R1,0,0,LT5]T,N2=1h2h1[0,3R1,0,LT6]T,
    N3=1h2h1[0,0,5R1,LT7]T,N4=1h2h1[LT8,R2,0,0]T,
    N5=1h2h1[LT9,0,3R2,0]T,N6=1h2h1[LT10,0,0,5R2]T,
    f3=γ2(s,th(t),t),f4=γ2(s,th2,th(t)).

    According to the Eq (2.9) and the similar procedure of the proof for inequality (2.5), the following inequality can be derived.

    Ξ3+Ξ4=th1th(t)˙xT(s)R1˙x(s)dsth(t)th2˙xT(s)R2˙x(s)ds+1h2h1ζT2(t)[E3E4]T(R(h(t))S(h(t)))[E3E4]ζ2(t).

    The Eq (2.10) and (2.11) can lead to Ξ3+Ξ40. Thus the Lemma 4 can be proved.

    In this section, the novel LKF with time-varying delay dependent matrix is proposed. By adopting the matrix inequality Lemma 3 and 4 respectively, we can derive two new stability criteria of time-varying delay system (2.1) under the limitation (2.2), which are Theorem 1 and 2. In order to verify the superiority of introducing time-varying delay dependent matrices in reducing the conservatism, we replace the time-varying delay dependent matrices with constant delay matrices as a contrast. As a result, the same Lyapunov matrix is appeared in the single integral terms for the derivation of LKF. So the Lemma 1 and 2 is adopted to deal with the estimation of single integral terms respectively, the Corollary 1 and 2 can be derived.

    Theorem 1. Given constant h1, h2, μ, the system (2.1) is asymptotically stable if there exist positive matrices PR6n×6n, WRn×n, KRn×n, and any matrices Q10Rn×n, Q11Rn×n, Q20Rn×n, Q21Rn×n, S4R2n×2n satisfying the following LMIs:

    {W+˙h(t)Q11>0,Q10+(h1h(t))Q11>0,W+˙h(t)Q21>0,Q20+(h2h(t))Q21>0. (3.1)
    {[Ψo1Π31S4(h1h2)W2(˙h(t))]<0,[Ψo2Π31S4(h1h2)W2(˙h(t))]<0,[Ψo3Π32ST4(h1h2)W1(˙h(t))]<0,[Ψo4Π32ST4(h1h2)W1(˙h(t))]<0. (3.2)

    Where

    Ψ=[ψmn](m,n=1,2,10),W1(˙h(t))=diag{W+˙h(t)Q11,3(W+˙h(t)Q11)},W2(˙h(t))=diag{W+˙h(t)Q21,3(W+˙h(t)Q21)},Π3=[Π31,Π32],Π31=[e3e2e3+e22e5],Π32=[e2e4e2+e42e6].

    o1, o2, o3, o4 separately refers to h(t)=h1 and ˙h(t)=μ, h(t)=h1 and ˙h(t)=μ, h(t)=h2 and ˙h(t)=μ, h(t)=h2 and ˙h(t)=μ. ψoi for i=1,2,3,4 in inequalities (3.2) is the specific matrix of ψ under o1,o2,o3,o4, the four situations respectively. For simplicity, some relevant notations in Theorem 1 are defined in APPENDIX A and the more details about ψmn are listed in APPENDIX B.

    It is worth noting that the inequalities (3.1) must be satisfied under o1o4, the four situations. So the inequalities (3.1) are equal to the following linear matrix inequalities:

    {W+μQ11>0,Q10>0,W+μQ21>0,Q20+(h2h1)Q21>0,WμQ11>0,Q10>0,WμQ21>0,Q20+(h2h1)Q21>0,W+μQ11>0,Q10(h2h1)Q11>0,W+μQ21>0,Q20>0,WμQ11>0,Q10(h2h1)Q11>0,WμQ21>0,Q20>0.

    Proof. Three Lyapunov-Krasovskii functional are adopted as follows

    V(t)=3i=1Vi(t). (3.3)

    where

    V1(t)=ξT(t)Pξ(t)V2(t)=th1th(t)˙xT(s)Q1(h(t))˙x(s)ds+th(t)th2˙xT(s)Q2(h(t))˙x(s)ds+tth1˙xT(s)K˙x(s)dsV3(t)=th1th2tv˙xT(s)W˙x(s)dsdv.

    The time derivative of V(t) can be calculated as;

    ˙V(t)=ζT1(t)(He(GT1PG2)+ˆQ)ζ1(t)th1th(t)˙xT(s)[W+˙h(t)Q11]˙x(s)dsth(t)th2˙xT(s)[W+˙h(t)Q21]˙x(s)ds. (3.4)

    According to Lemma 3, the last two single integral terms of ˙V(t) can be calculated as follows:

    th1th(t)˙xT(s)[W+˙h(t)Q11]˙x(s)dsth(t)th2˙xT(s)[W+˙h(t)Q21]˙x(s)ds1h2h1ζT1(t)[E1E2]T(ω(h(t),˙h(t))ϖ(h(t),˙h(t)))[E1E2]ζ1(t). (3.5)

    From the Leibniz-Newton formulas, the following equation is true for any NRn×n.

    2[˙xT(t)+xT(t)+xT(th1)+xT(th2)+th1th(t)xT(s)ds+th(t)th2xT(s)ds]N[˙x(t)+Ax(t)+Bx(th(t))]=0. (3.6)

    The Eq (3.6) can be written as:

    ζT1(t)Φζ1(t)=0. (3.7)

    Adding the Eq (3.7) to the Eq(3.4), the time derivative of V(t) can be rewritten.

    ˙V(t)ζT1(t)Γζ1(t). (3.8)

    Therefore Γ<0 leads to ˙V(t)σx(t)2 for a sufficient small scalarσ>0, the system (2.1) is asymptotically stable with the limitation (2.2).

    when h(t)=h1

    Γ=Ψ1h1h2Π31S4W12(˙h(t))ST4ΠT31<0. (3.9)

    When h(t)=h2

    Γ=Ψ1h1h2Π32ST4W11(˙h(t))S4ΠT32<0. (3.10)

    By applying Schur complement, Formulas (3.9) and (3.10) are also equal to LMIs as Eqs (3.1) and (3.2).

    Remark 1. We divide th1th2˙xT(s)Q˙x(s)ds into th1th(t)˙xT(s)Q1(h(t))˙x(s)ds and th(t)th2˙xT(s)Q2(h(t))˙x(s)ds. And different from the constant matrices we introduce the time-varying delay dependent matrices Q1(h(t))=Q10+(h1h(t))Q11 and Q2(h(t))=Q20+(h2h(t))Q21 to V2(t). The integral terms th1th(t)˙xT(s)(W+˙h(t)Q11)˙x(s)dsth(t)th2˙xT(s)(W+˙h(t)Q21)˙x(s)ds are included in the time derivation of V(t).

    However when we divide th1th2˙xT(s)Q˙x(s)ds into th1th(t)˙xT(s)Q1˙x(s)ds and th(t)th2˙xT(s)Q2˙x(s)ds. Q1,Q2 are constant matrices, rather than the time-varying dependent matrices. There are only single integral terms th1th(t)˙xT(s)W˙x(s)ds and th(t)th2˙xT(s)W˙x(s)ds in ˙V(t), which are obtained from V3(t).

    Obviously, the time-varying dependent matrices Q1(h(t)), Q2(h(t)) bring more information about time-varying delay than the constant matrices Q1, Q2.

    In order to compare the conservative of stability criterion between time-varying delay dependent matrices and constant matrices, we replace the Q1(h(t)), Q2(h(t)) with Q1, Q2 in V2(t). The stability criteria can be derived as follows:

    Corollary 1. Given constant h1, h2, μ, the system (2.1) is asymptotically stable if there exist positive matrices P2R6n×6n, W2Rn×n, Q1Rn×n, Q2Rn×n, KRn×n, and any matrix S5R2n×2n satisfying the following LMIs:

    {[Λo1Π31S5(h1h2)W]<0,[Λo2Π31S5(h1h2)W]<0,[Λo3Π32ST5(h1h2)W]<0,[Λo4Π32ST5(h1h2)W]<0. (3.11)

    Where

    Λ=Ω1+Φ+1h1h2Π3ω2(h(t),˙h(t))ΠT3,W=diag{W2,3W2},ω2(h(t),˙h(t))=[α1WS5(h1h2)W],Ω1=He(GT1P2G2)+ˆQ2,G1=col{e1,e2,e3,e4,(h(t)h1)e5,(h2h(t))e6},G2=col{e7,(1˙h(t))e8,e9,e10,(˙h(t)1)e2+e3,(1˙h(t))e2e4},ˆQ2=diag{0n6n,Q77,Q88,Q99,Q1010},Q88=(˙h(t)1)Q1+(1˙h(t))Q2,Q99=Q1K,Q1010=Q2.

    Proof. We replace the Lyapunov matrices Q1(h(t)) and Q2(h(t)) as Q1 and Q2 separately in Lyapunov-Krasovskii functional V2(t) of the Eq (3.3). Then integral terms th1th(t)˙xT(s)W2x(s)dsth(t)th2˙xT(s)W2x(s)ds are appeared in the derivation of V(t). Owing to the same Lyapunov matrix W2, the Lemma 1 can be adopted to estimate the single integral terms. The other process is similar to the process of Theorem 1. Therefore the details can be omitted.

    It is worth noting that, the subscript of Λ in inequalities (3.11) (oii=1,2,3,4)) separately refers to h(t)=h1 and ˙h(t)=μ, h(t)=h1 and ˙h(t)=μ, h(t)=h2 and ˙h(t)=μ, h(t)=h2 and ˙h(t)=μ, the four situations. Λoi for i=1,2,3,4 in inequalities (3.11) is the specific matrix of Λ under o1,o2,o3,o4, the four situations respectively.

    Secondly, Theorem 2 for system (2.1) will be derived by Lemma 4. The notations of several parameters are defined in APPENDIX A

    Theorem 2. Given constant h1, h2, μ, the system(2.1) is asymptotically stable if there exists matrices P3R6n×6n>0, Q10Rn×n, Q11Rn×n, Q20Rn×n, Q21Rn×n, WRn×n>0, KRn×n>0, SR3n×3n such that the following LMIs hold:

    {W+˙h(t)Q11>0,Q10+(h1h(t))Q11>0W+˙h(t)Q21>0Q20+(h2h(t))Q21>0 (3.12)
    {[ˆΨo1Π1S(h1h2)V2(˙h(t))]<0,[ˆΨo2Π1S(h1h2)V2(˙h(t))]<0[ˆΨo3Π2ST(h1h2)V1(˙h(t))]<0,[ˆΨo4Π2ST(h1h2)V1(˙h(t))]<0 (3.13)

    Where

    ˆΨ=[ˆψmn](m,n=1,2,12),V1(˙h(t))=diag(W+˙h(t)Q11,3(W+˙h(t)Q11),5(W+˙h(t)Q11)),V2(˙h(t))=diag(W+˙h(t)Q21,3(W+˙h(t)Q21),5(W+˙h(t)Q21)),Π=[Π1,Π2],Π1=[υ3υ2υ3+υ22υ5υ3υ2+6υ512υ11],Π2=[υ2υ4υ2+υ42υ6υ2υ4+6υ612υ12].

    The more details about ˆψmn are listed in APPENDIX B. In addition, the process of converting stability condition (3.12) to the linear condition is same as those of the stability condition (3.1) in Theorem 1.

    Proof. We adopt the same Lyapunov-Krasovskii functional as (3.3). So the ˙V(t) can be expressed as follows:

    ˙V(t)=ζ2(t)(He(GT3P3G4+ˉQ))ζ2(t)th1th(t)˙xT(s)[W+˙h(t)Q11]˙x(s)dsth(t)th2˙xT(s)[W+˙h(t)Q21]˙x(s)ds. (3.14)

    According to Lemma 4, the last two single integral terms of ˙V(t) can be calculated as follows:

    th1th(t)˙xT(s)[W+˙h(t)Q11]˙x(s)dsth(t)th2˙xT(s)[W+˙h(t)Q21]˙x(s)ds1h1h2ζT2(t)[E3E4]T(ω3(h(t),˙h(t))ϖ3(h(t),˙h(t)))[E3E4]ζ2(t).

    The Eq (3.6) can also be rewritten as:

    ζT2(t)Φ2ζ2(t)=0. (3.15)

    Adding the (3.15) to the Eq (3.14), the time derivative of V(t) can be rewritten as follows:

    ˙V(t)ζT2(t)Γ2ζ2(t). (3.16)

    The other process is similar to those of Theorem 1. Then the follow conclusions can be derived.

    When h(t)=h1

    Γ2=ˆΨ1h1h2Π1SV12(˙h(t))STΠT1<0. (3.17)

    When h(t)=h2

    Γ2=ˆΨ1h1h2Π2STV11(˙h(t))STΠT2<0. (3.18)

    Similarity, Formulas(3.17) and (3.18) are equal to LMIs as inequalities (3.12) and (3.13) by Schur complement.

    ˆΨoi for i=1,2,3,4 in inequalities (3.13) is the specific matrix of ˆΨ under o1,o2,o3,o4, the four situations respectively.

    Remark 2. Similarity to Remark 1, when we introduce the constant matrices Q1, Q2 to V2(t), rather than Q10+(h1h(t))Q11, Q20+(h2h(t))Q21. The stability criteria can be derived by Lemma 2 as follow:

    Corollary 2. Given constant h1, h2, μ, the system (2.1) is asymptotically stable if there exist positive matrices P4R6n×6n, WRn×n, Q10Rn×n, Q20Rn×n, KRn×n, and any matrix S1R3n×3n satisfying the following LMIs:

    {[ˆΛo1Π1S1(h1h2)V]<0,[ˆΛo2Π1S1(h1h2)V]<0,[ˆΛo3Π2ST1(h1h2)V]<0,[ˆΛo4Π2ST1(h1h2)V]<0. (3.19)

    Where

    ˆΛ=Ω2+Φ2+1h1h2Πω4(h(t),˙h(t))ΠT=[ˆλmn](m,n=1,2,,12),V=diag{W,3W,5W},ω4(h(t),˙h(t))=[α1VS(h1h2)V],Ω2=He(GT3P3G4)+ˉQ2,ˉQ2=diag{0n6n,Q77,Q88,Q99,Q1010,0n2n}.

    ˆΛoi for i=1,2,3,4 in the inequalities (3.19) is the specific matrix of ˆΛ under o1,o2,o3,o4, the four situations respectively.

    In this section, Three numerical examples are used to show the validity of the proposed theorems. The conservation of criteria is checked by calculating maximal admissible delay upper bounds(MADUPS). The symbol of in Table 14 denotes that the result is not listed in the literature. The condition of μ depends on the results listed in the other literatures.

    Table 1.  MADUPS with different μ.
    μ [25] [20] [26] [29] [36] [37] Corollary 1 Theorem 1 Corollary 2 Theorem 2
    0.1 4.703 4.811 4.788 4.714 4.930 4.921 4.932 4.942 4.941 4.952
    0.2 3.834 4.101 4.060 - 4.220 4.218 4.320 4.342 4.341 3.424
    0.3 2.420 3.061 3.055 - 3.090 3.221 3.281 3.314 3.311 3.421
    0.4 2.137 2.612 2.615 - 2.660 2.792 2.812 2.922 2.911 2.987

     | Show Table
    DownLoad: CSV
    Table 2.  MADUPS with different h1 and μ.
    h1 μ method
    [38] [39] Corallary 1 Theorem 1 Corallary 2 Theorem 2
    h1=1 0.5 2.07 2.46 2.48 2.53 2.50 2.64
    0.9 1.74 2.29 2.32 2.45 2.40 2.58
    h1=2 0.5 2.43 2.79 2.92 3.05 2.95 3.2
    0.9 2.43 2.77 2.85 2.93 2.88 3.01

     | Show Table
    DownLoad: CSV
    Table 3.  MADUPS with different μ.
    μ method
    [40] [41] [26] [25] [29] Theorem 1 Theorem 2
    0.05 1.81 2.166 2.553 2.551 2.598 2.67 2.82
    0.1 1.75 2.028 2.372 2.369 2.397 2.52 2.71
    0.5 1.61 1.622 1.731 1.7 1.787 2.01 2.11

     | Show Table
    DownLoad: CSV
    Table 4.  MADUPS with different μ.
    μ [25] [26] [29] [42] [37] Theorem 1 Theorem 2
    0.1 6.590 7.148 6.610 7.230 7.308 7.408 7.821
    0.2 3.834 4.060 - 4.556 4.670 4.897 5.231
    0.5 2.420 3.055 1.687 2.509 2.664 3.124 3.423
    0.8 2.137 2.615 - 1.950 2.072 2.458 2.657

     | Show Table
    DownLoad: CSV

    Example 1. Consider the system (2.1) as follow [20,25,26,29,36,37]:

    A=[2000.9],B=[1011].

    For numerical example1, the MADUPS of h2 respecting to h1=0 and various μ calculated by our theorems and existing works are listed in Table 1. We can observe the followings:

    Table 1 presents the obtained MADUPS of system 1 for different μ. From Table 1, we can obtain the following conclusions.

    One can confirm that the results of Corollary 1 and 2 are still larger than the other methods listed in Table 1. This means the linear matrix inequality techniques (Lemma 1 and 3) can decrease the conservatism validly.

    The results of Corollary 1 and 2 are smaller than those of Theorem 1 and 2 separately. This means the Lyapunov-Krasovskii functional with time-varying delay dependent matrix plays an important role to reduce the conservatism of stability criterion.

    Theorem 2 is less conservative than Theorem 1 and Corallary 2 is less conservative than Corollary 1, which means the more augmented vectors in Lemma 3 and 4 decrease the conservatism validly.

    It also can be seen that Theorem 1 is less conservative than Corollary 2, which means the time-varying delay dependent matrix proposed in this paper is better than introducing more augmented vectors technique in reducing the conservatism of the stability criterion.

    When h10, the obtained results by applying Theorem 1, Corallary 1, Theorem 2 and Corallary 2 are listed in Table 2 and compared with the results published in previous literatures.

    From Table 2, it should be noted that when h10, the method proposed in this paper is more superior in reducing conservatism than the previous results. And all the results of Theorem 2 listed in Table 2 are better than those of Theorem 1, all the results of Corallary 2 are better than those of Corallary 1. This implies that the Theorem 2 and Corallary 2 effectively reduce the conservatism of stability criteria by introducing more details about time-varying delay in amplification vector than Theorem 1 and Corollary 1 separately. Meanwhile, the results of Corallary 1 and 2 are bigger than the results of [38,39], are smaller than those of Theorem 1 and 2 separately. We can infer that the linear matrix inequality technique of Lemma 1– 4 can reduce the conservatism and introducing time-varying delay dependent matrix can reduce conservatism effectively.

    When h1=0,μ=0.1, Theorem 2 guarantees the stability for [Example 1, h(t)=4.952]. And when h1=2,μ=0.9, Theorem 2 guarantees the stability for [Example 1, h(t)=3.01]. The state responses under h1=0,μ=0.1 and h1=2,μ=0.9 are displayed in Figure 1 and 2. It can be seen that the system is stable under given conditions.

    Figure 1.  The state trajectories of Example1 [h1=0,μ=0.1].
    Figure 2.  The state trajectories of Example 1 [h1=2,μ=0.9].

    Example 2. Considering the system (2.1) with parameters listed as follow [25,26,29,40,41]:

    A=[0111],B=[0001].

    Setting h1=0, the MADUPS of h2 respecting to various μ by utilizing the methods of literature [25,26,29,40,41] and our theorems can be derived, which are listed in Table 3.

    From the results in Table 3, one can also see that all the results obtained by Theorem 1 are larger than those obtained by other literatures listed in Table 3, and smaller than Theorem 2, which verify the above inference.

    When h1=0,μ=0.1, Theorem 2 guarantees the stability for [Example 2, h(t)=2.71]. And when h1=0,μ=0.5, Theorem 2 guarantees the stability for [Example 2, h(t)=2.11]. The state responses under h1=0,μ=0.1 and h1=0,μ=0.5 are displayed in Figure 3 and 4. It can be seen that the system is stable under given conditions.

    Figure 3.  The state trajectories of Example 2 [h1=0,μ=0.1].
    Figure 4.  The state trajectories of Example 2 [h1=0,μ=0.5].

    Example 3. Considering the system (2.1) listed as follow [25,26,29,37,42]:

    A=[0112],B=[0011].

    For numerical Example 3, setting h1=0, the comparison of our results obtained by Theorem 1 and 2 with the results in [25,26,29,37,42] is conducted in Table 4.

    The results listed in Table 4 show the Theorem 2 gives slightly larger delay bounds comparing with those of Theorem 1 and other literatures.

    When h1=0,μ=0.1, Theorem 2 guarantees the stability for [Example 3, h(t)=7.821]. And when h1=0,μ=0.8, Theorem 2 guarantees the stability for [Example 3, h(t)=2.657]. The state responses under h1=0,μ=0.1 and h1=0,μ=0.8 are displayed in Figure 5 and 6. It can be seen that the system is stable under given conditions.

    Figure 5.  The state trajectories of Example 3 [h1=0,μ=0.1].
    Figure 6.  The state trajectories of Example 3 [h1=0,μ=0.8].

    This work has investigated the stability analysis issue of linear systems with time-varying delays via some novel approaches. Firstly, two integral inequalities are put forward to deal with the single integral terms with time-varying delay dependent matrices. Secondly, the novel Lyapunov-Krasovskii functionals with the time-varying delay matrix, rather than constant matrix are proposed. Thirdly, improved stability criteria are obtained based on the proposed approaches. Finally the results of three numerical example dealt with our methods and the previous methods, are contrasted to verify the improvement of our proposed methods.

    This work was supported by the National Natural Science Foundation of China under Grant (No. 61703060, 12061088, 61802036 and 61873305), the Sichuan Science and Technology Program under Grant No. 21YYJC0469, the Project funded by China Postdoctoral Science Foundation under Grant Nos. 2020M683274 and 2021T140092, Supported by the Open Research Project of the State Key Laboratory of Industrial Control Technology, Zhejiang University, China (No. ICT2021B38), Guangdong Basic and Applied Basic Research Foundation (2021A1515011692).

    The authors declare no conflict of interest.

    The relevant notations in Theorem 1 are defined as follows:

    ξ(t)=col{x(t),x(th(t))x(th1),x(th2),th1th(t)x(s)ds,th(t)th2x(s)ds},
    Q1(h(t))=Q10+(h1h(t))Q11,Q2(h(t))=Q20+(h2h(t))Q21,
    G1=col{e1,e2,e3,e4,(h(t)h1)e5,(h2h(t))e6},
    G2=col{e7,(1˙h(t))e8,e9,e10,(˙h(t)1)e2+e3,(1˙h(t))e2e4},
    ω(h(t),˙h(t))=[α1W1(˙h(t))S4α2W2(˙h(t))],ϖ(h(t),˙h(t))=[α3S4W12(˙h(t))ST40α4ST4W11(˙h(t))S4],
    Γ=Ψ1h1h2Π3ϖ(h(t),˙h(t))ΠT3,
    Ψ=Ω+Φ+1h1h2Π3ω(h(t),˙h(t))ΠT3,
    Ω=He(GT1PG2)+ˆQ,
    ˆQ=diag{0n6n,Q77,Q88,Q99,Q1010},
    Q77=(h2h1)W+K,
    Q88=(˙h(t)1)Q10+(h(t)h1)(1˙h(t))Q11+(1˙h(t))Q20+(h2h(t))(1˙h(t))Q21,
    Q99=Q10+(h1h(t))Q11K,
    Q1010=Q20(h2h(t))Q21.

    The relevant notations in Theorem 2 are defined as follows:

    G3=col{υ1,υ2,υ3,υ4,(h(t)h1)υ5,(h2h(t))υ6},G4=col{υ7,(1˙h(t))υ8,υ9,υ10,(˙h(t)1)υ2+υ3,(1˙h(t))υ2υ4},
    ω3(h(t),˙h(t))=[α1V1(˙h(t))Sα2V2(˙h(t))],ϖ3(h(t),˙h(t))=[α3SV12(˙h(t))ST0α4STV12(˙h(t))S],
    ˆΨ=ˆΩ2+Φ2+1h1h2Πω3(h(t),˙h(t))ΠT,Γ2=ˆΨ1h1h2Πϖ3(h(t),˙h(t))ΠT,
    ˆΩ2=He(GT3P3G4)+ˉQ,ˉQ=diag{0n6n,Q77,Q88,Q99,Q1010,022n}.

    The elements in Ψ are as follows:

    ψ11=NA+ATNTψ12=(˙h(t)1)P15+(1˙h(t))P16+NBψ13=P15+ATNTψ14=P16+ATNTψ15=(h(t)h1)ATNTψ16=(h2h(t))ATNTψ17=P11+ATNTNψ18=(1˙h(t))P12ψ19=P13ψ110=P14.
    ψ22=(˙h(t)1)P25+(˙h(t)1)PT25+(1˙h(t))P26+(1˙h(t))PT26+1h1h2(4α1R1ST11ST12+ST21+ST22S11+S21S12+S22+4α2R2).
    ψ23=P25+(˙h(t)1)PT35+(1˙h(t))PT36+BTNT+1h1h2(2α1R1+ST11+ST12+ST21+ST22).
    ψ24=P26+(˙h(t)1)PT45+(1˙h(t))PT46+BTNT+1h1h2(S11S21S12+S22+2α2R2).
    ψ25=(˙h(t)1)(h(t)h1)PT55+(1˙h(t))(h(t)h1)PT56+(h(t)h1)BTNT1h1h2(2ST21+2ST22+6α1R1).
    ψ26=(˙h(t)1)(h2h(t))P56+(1˙h(t))(h2h(t))PT66+(h2h(t))BTNT+1h1h2(2S122S226α2R2).
    ψ27=PT12+BTNTψ28=(1˙h(t))P22ψ29=P23ψ210=P24.
    ψ33=P35+PT35+1h1h2(4α1R1)ψ34=P36+PT451h1h2(S11+S21S12S22).
    ψ35=(h(t)h1)PT556h1h2α1R1ψ36=(h2h(t))P561h1h2(2S12+2S22)ψ37=PT13N.
    ψ38=(1˙h(t))PT23ψ39=P33ψ310=P34.
    ψ44=P46PT46+4h1h2α2R2ψ45=(h(t)h1)PT56+2h1h2(ST21ST22).
    ψ46=(h2h(t))PT666h1h2(α2R2)ψ47=PT14Nψ48=(1˙h(t))PT24ψ49=PT34ψ410=P44ψ55=12h1h2α1R1ψ56=4h1h2S22ψ57=(h1h(t))N+(h(t)h1)PT15ψ58=(1˙h(t))(h(t)h1)PT25ψ59=(h(t)h1)PT35ψ510=(h(t)h1)PT45ψ66=12h1h2α2R2ψ67=(h2h(t))PT16+(h(t)h2)Nψ68=(1˙h(t))(h2h(t))PT26.
    ψ69=(h2h(t))PT36ψ610=(h2h(t))PT46ψ77=(h2h1)WNNT+Kψ88=(˙h(t)1)Q10+(h(t)h1)(1˙h(t))Q11+(1˙h(t))Q20+(h2h(t))(1˙h(t))Q21ψ99=Q10+(h1h(t))Q11Kψ1010=Q20(h2h(t))Q21.

    The elements in ˆΨ are as follows:

    ˆψ11=NA+ATNTˆψ12=(˙h(t)1)P15+(1˙h(t))P16+NBˆψ13=P15+ATNT.
    ˆψ14=P16+ATNTˆψ15=(h(t)h1)ATNTˆψ16=(h2h(t))ATNT.
    ˆψ17=P11+ATNTNˆψ18=(1˙h(t))P12ˆψ19=P13.
    ˆψ110=P14ˆψ111=ˆψ112=0.
    ˆψ22=(˙h(t)1)P25+(˙h(t)1)PT25+(1˙h(t))P26+(1˙h(t))PT26+1h1h2(9α1R1+9α2R2S11ST11S12ST12S13ST13+S21+ST21+S22+ST22+S23+ST23S31ST31S32ST32S33ST33).
    ˆψ23=P25+(˙h(t)1)PT35+(1˙h(t))PT36+BTNT+1h1h2(3α1R1+ST11+ST12+ST13+ST21+ST22+ST23+ST31+ST32+ST33).
    ˆψ24=P26+(˙h(t)1)PT45+(1˙h(t))PT46+BTNT+1h1h2(3α2R2+S11S21+S31S12+S22S32+S13S23+S33).
    ˆψ25=(˙h(t)1)(h(t)h1)PT55+(1˙h(t))(h(t)h1)PT56+(h(t)h1)BTNT+1h1h2(36α1R12ST212ST222ST23+6ST31+6ST32+6ST33).
    ˆψ26=(˙h(t)1)(h2h(t))P56+(1˙h(t))(h2h(t))PT66+(h2h(t))BTNT+1h1h2(36α2R2+2S122S22+2S32+6S136S23+6S33).
    ˆψ27=PT12+BTNTˆψ28=(1˙h(t))P22ˆψ29=P23ˆψ210=P24.
    ˆψ211=1h1h2(60α1R112ST3112ST32ST33)ˆψ212=1h1h2(60α2R2+12S1312S23+12S33).
    ˆψ33=P35+PT35+1h1h29α1R1.
    ˆψ34=P36+PT45+1h1h2(S11S21S31+S12+S22+S32S13S23S33).
    ˆψ35=(h(t)h1)PT55+1h1h224α1R1.
    ˆψ36=(h2h(t))P56+1h1h2(2S122S222S326S136S236S33).
    ˆψ37=PT13Nˆψ38=(1˙h(t))PT23ˆψ39=P33ˆψ310=P34.
    ˆψ311=60α1R11h1h2ˆψ312=1h1h2(12S1312S2312S33).
    ˆψ44=P46PT46+1h1h29α2R2.
    ˆψ45=(h1h(t))PT56+1h1h2(2ST212ST22+2ST236ST31+6ST326ST33).
    ˆψ46=(h(t)h2)PT66+1h1h224α2R2.
    ˆψ47=PT14Nˆψ48=(1˙h(t))PT24ˆψ49=PT34ˆψ410=P44.
    ˆψ411=1h1h2(12ST3112ST32+12ST33)ˆψ412=1h1h260α2R2.
    ˆψ55=1h1h2192α1R1ˆψ56=1h1h2(4S2212S32+12S2336S33).
    ˆψ57=(h(t)h1)PT15+(h1h(t))Nˆψ58=(1˙h(t))(h(t)h1)PT25ˆψ59=(h(t)h1)PT35.
    ˆψ510=(h(t)h1)PT45ˆψ511=1h1h2360α1R1ˆψ512=1h1h2(24S2372S33).
    ˆψ66=1h1h2192α2R2ˆψ67=(h2h(t))PT16+(h(t)h2)Nˆψ68=(1˙h(t))(h2h(t))PT26.
    ˆψ69=(h2h(t))PT36ˆψ610=(h2h(t))PT46ˆψ611=1h1h2(24ST32+72ST33).
    ˆψ612=1h1h2360α2R2ˆψ77=NNT+(h2h1)W+K.
    ˆψ88=(˙h(t)1)Q10+(h(t)h1)(1˙h(t))Q11+(1˙h(t))Q20+(h2h(t))(1˙h(t))Q21.
    ˆψ99=Q10+(h1h(t))Q11Kˆψ1010=Q20+(h2h(t))Q21.
    ˆψ1111=1h1h2720α1R1ˆψ1112=1h1h2144S33ˆψ1212=1h1h2720α2R2.


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