External stability and H∞\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$H_{\infty }$\end{document} control of switching systems with delay and impulse

In this paper, we investigate the external stability and H∞\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$H_{\infty }$\end{document} control of switching systems with time-varying delay and impulse. First of all, a modified two-direction inequality (relation) between the switching numbers and the maximum, minimum dwell time is proposed. This new inequality is applied to proving the external stability of switching systems with delay and impulse consisting of subsystems with Hurwitz stable matrices of internal dynamics. By using this new inequality, a normal L2\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$L_{2}$\end{document} norm constraint is derived rather than weighted L2\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$L_{2}$\end{document} norm constraint. In addition, by a realizable switching law, the obtained result is extended to the switching systems comprised of subsystems with both Hurwitz stable and unstable matrices of internal dynamics. The results are finally applied to H∞\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$H_{\infty }$\end{document} control and illustrated by a numerical example.


Introduction
External stability (ES) is defined as a property of control systems: every L 2 input generates an L 2 zero-state output [1][2][3][4], which plays an essential role in system analysis. As one type of systems, switching systems(SSs), consisting of a family of subsystems, and a switching rule that orchestrates the switching between them [5][6][7][8], have been an important framework in the area of input-output analysis. In practice, effects of time delay [9,10] and impulse [11,12] are usually inevitable. Therefore, there are lots of results on system and input-output analysis of delayed SSs [11][12][13][14][15][16][17][18][19][20][21]. For example of a discrete-time framework, the problem of robust exponential H ∞ filtering for switched fuzzy delayed systems was investigated in [15]; for example of a continuous-time framework, in [11], fault-tolerant synchronization for SSs with delay and impulse was considered.
In the field of ES, H ∞ control, H ∞ model reduction, L 2 -gain analysis and disturbance attenuation for the SSs, how to obtain the L 2 norm bound constraint is a critical part of our study. Owing to the essence of SSs and average dwell time(DT) scheme, the concept of weighted L 2 norm bound constraint, instead of the normal L 2 norm bound constraint, has been proposed [16,17,22]. However, this weighted concept changes the original physical meaning of L 2 . Recently, some researchers tried to remove this label "weighted", see [18] in 2012, [23] in 2016 and [19] in 2017. However, there are still some doubtful problems. Specifically, Liu and Yuan adopted a normal L 2 relation between input and output in [18] but where the average DT could not be substituted into the integral in (36); In [23], Eq. (21) could not be directly derived because (s) could not be guaranteed greater than zero; Syed Ali et al. employed the square of L 2 norm, see (6) in [19], but it is questionable for the cancelation of e α(T-s) on both sides of the inequality right below (57). Very recently, a two-direction inequality ( t-τ T max ≤ N σ (t, τ ) ≤ t-τ T min ) between the switching numbers and the maximum, minimum DT was proposed in [11] such that the label "weighted" can be removed properly. Furthermore, an improved two-direction inequality ( t-τ T max -1 ≤ N σ (t, τ ) ≤ t-τ T min +1) was provided in [24,25]. But this improved inequality is still not precise enough. A more accurate two-direction inequality (max{ t-τ T max -1, 0} ≤ N σ (t, τ ) ≤ t-τ T min + 1) was given in [21]. To the best of our knowledge, this more accurate two-direction inequality has not been used to study the ES and H ∞ control of SSs with delay and impulse.
In order to study the ES of SSs comprised of subsystems with both Hurwitz stable and unstable matrices, a suitable switching law is necessary. There are a few results that have been reported in [22,[25][26][27][28][29]. Some state-dependent switching laws were proposed in [27,28], while some time-dependent switching laws were presented [22,25,26,29]. The authors of [29] applied fast switching and slow switching, respectively, to unstable and stable subsystems. In [26], the precondition inf t≥t 0 [ T -1 (t) T + (t) ] ≥ -β α was given to guarantee that -γ t = T -1 (t)α + T + (t)β < 0 holds. But this precondition cannot make sure that -γ t = T -1 (t)α + T + (t)β holds or that T -1 (t)α + T + (t)β is a linear function as desired. Only T -1 (t)α + T + (t)β < 0 can be deduced there. Another resolution was proposed in [22], a new separation of switching instants was arranged in advance. By a given parameter c * > 0 without a specified sequence of time instants, the switching law in [25] is easier and clearer to implement than the one in [22]. This makes it worth to study how to adopt the switching law in [25] to investigate the ES and H ∞ control of SSs with delay and impulse.
Motivated by the above discussion, the problem of ES and H ∞ control of SSs with delay and impulse is investigated in this paper. The main contribution of the paper is as follows. First, a two-direction inequality (relation) between the switching numbers and the maximum, minimum DT is used such that the label "weighted" can be removed properly and the normal L 2 norm constraint is derived. Second, a suitable switching law is adopted to deal with the SSs with both Hurwitz stable and unstable subsystems. Third, we take the overlooked case 0 < μ < 1 into consideration (in almost all mentioned results above the range of μ is only larger or equal to 1), i.e. the range of switching parameters μ is extended to the set of all positive real numbers. Fourth, the non-weighted H ∞ control [30][31][32] of switching control systems with delay and impulse is established, in which the matrices of internal dynamics of the controlled system are not necessarily all Hurwitz as usual. Finally, the effectiveness of the results is illustrated by a numerical example.

Problem statement and preliminaries
Let R n denote the n-dimensional real Euclidean space. For x ∈ R n , x denotes the Euclidean norm of x. We use the notation L 2 ([0, ∞), R n ) to denote the class of square integrable functions from [0, ∞) to R n , i.e. for each x ∈ L 2 ([0, ∞), R n ), the L 2 norm of x is x(t + s) . The notation P > 0 indicates that matrix P is positive definite. λ max (P) (λ min (P)) denotes the maximum (minimum) eigenvalue of matrix P. αmeans such a positive number that the inequality A T i P i + P i A i + α -P i < 0 holds where A i is Hurwitz stable, while α + means such a positive number that A T i P i + P i A iα + P i < 0 holds where A i is not Hurwitz stable.
Consider the following switching control system with delay and impulse: where x(t) ∈ R n , u(t) ∈ R m and y(t) ∈ R p represent the state vector, external input vector and output vector, respectively.
, E σ (t) and I σ (t) are constant matrices with appropriate dimensions, where σ (t) is the switching signal, which takes values from P = {1, 2, . . .} and σ (t) = i ∈ P means the subsystem i is active at t. The switching time instants Remark 2.1 Hereẋ is considered as the right derivative of x based on two considerations. On the one hand, the derivative at t 0 is taken to be a right derivative, since φ(θ ) may not admit a left derivative at t 0 or this left derivative even exists but may not equal the right hand function. To be consistent with the derivative at t 0 ,ẋ(t k ) needs to be the notation of the right derivative at t k . On the other hand, at t k , the subsystem σ (t k ) = σ (t + k ) is already active, i.e.ẋ(t) It follows thatẋ(t k ) also denotes the right derivative at t k .

Remark 2.2
The solution x(t) is right continuous at t k , i.e. x(t + k ) = x(t k ), sinceẋ(t k ) represents the right derivative at t k and the right derivative is defined based on right continuity. (Here θ indicates the zero function.) The L 2 gain is the maximum ratio of y L 2 / u L 2 .

Main results
At the beginning of this section, the ES of SSs with delay and impulse consisting of subsystems with Hurwitz A i s is proved. Then the obtained result is extended to the ES of SSs, in which not all subsystems are Hurwitz stable, by employing a switching law. In obtained results, the normal L 2 norm constraint, rather than a weighted L 2 norm constraint, is derived by using the new proposed relation (2). Finally, the derived results of ES is applied to H ∞ control.

External stability
In this subsection, by using Eq. (2), the ES of SSs with delay and impulse consisting of subsystems that are all Hurwitz stable, and subsystems that are not all Hurwitz stable, is proved, respectively.
3.1.1 All subsystems are Hurwitz stable Theorem 3.1 Given scalars α > 0, μ > 0 and the numbers of any two consecutive subsystems i, j ∈ P (σ switches from j to i), the system (1) is externally stable with a L 2 gain γ , if there exist n × n positive definite matrices P i , Q i , P j , Q j such that and Proof Consider the following Lyapunov functional candidate: andV respectively. (3), by using the Schur complement [33], we obtain Therefore, we can deduce thaṫ Thus, integrating the inequality (9) from t k-1 to t, t ∈ [t k-1 , t k ), produces Using the Schur complement again, it follows from the first inequality in (4) that (I + The second inequality in (4) and the calculation above together imply that Using the technique in (2.7) of [22], it follows from (10) and (11) that Under the zero initial condition, we acquire That is, To obtain the ES, we discuss (14) in three cases, that is, μ > 1, μ = 1 and 0 < μ < 1. For the case of μ > 1 (ln μ > 0). It follows from (2) (14) can be rearranged as follows: where α -ln μ T max > 0 and α -ln μ T min > 0 due to (5) and α > 0. Integrating both sides of (15) from t = t 0 to ∞ and interchanging the order of integrals lead to By The remaining arguments for the other two cases, μ = 1 and 0 < μ < 1, are analogous to the above analysis and will not be reproduced here. Consider u(s) = 0, for s ∈ [0, t 0 ], then which implies that the system (1) is externally stable with a L 2 gain γ .
Remark 3.1 The switching parameter 0 < μ < 1 was usually overlooked, as mentioned also in [11]. Only μ ≥ 1 was considered in [16][17][18]22] and in [19] that was η ≥ 1. If the sets of those matrices (such as P i , Q i in this work) were finite, as assumed in [16][17][18][19]22], it would be not easy to consider this overlooked case. However, in [11,25] and this work, the switching index set, see P below (1), is not restricted to be finite such that the just mentioned sets of matrices can be infinite. Moreover, in conditions like Q i ≤ μQ j , i and j are only any two consecutive (j is just after i) rather than two arbitrary indices as in [16][17][18][19]22]. These together make the case 0 < μ < 1 feasible, i.e. the range of μ can be all positive real numbers.
Remark 3.2 It follows from (12) and Theorem 3.1, the zero-input state

Not all subsystems are Hurwitz stable
In the following, we consider to investigate the ES of SSs consisting of subsystems that are not all Hurwitz stable.
For a subsystem A i (Hurwitz stable), similar to (6)-(10), A di , B i , C i , D i on [t k-1 , t k ), replacing α with αunder the condition (3), then, for t ∈ [t k-1 , t k ), we can derive that For a subsystem A i (not Hurwitz), there always exist P i > 0 and α + > 0 (as long as α + is large enough), such that holds, we can deduce thaṫ Therefore, the following inequality holds: Under the inequality in (4), using the same arguments as in (12), (13) and (14), from t 0 to t, t ∈ [t k-1 , t k ), we can get And then where T + (t, τ ), T -(t, τ ) denote the total active time of those subsystems with Hurwitz A i s, not Hurwitz A i s over (τ , t), respectively.
Taking the case μ > 1 as an example, the exponential index on the left side of (26): while the same index on the right side of (26) may not be immediately increased to be in the form: -λ(ts), λ > 0. Now, we choose a scalar α * ∈ (0, α -) arbitrarily and propose the following switching law.
Corollary 3.1 Given scalars α > 0, 0 < α -< α, α + > 0, 0 < μ < 1 and the numbers of any two consecutive subsystems i, j ∈ P (σ switches from j to i), the system (1) is externally stable with a L 2 gain γ , if there exist real n × n positive definite matrices P i , Q i , P j , Q j such that, for each subsystem (A i is Hurwitz), for each subsystem (A i is not Hurwitz), and where μ = γ μ -α + +| ln μ|/T max Proof Taking a similar process to (20) to (26), we have Suppose α + < | ln μ| T max and choose μ = γ μ -α + +| ln μ|/T max α -+| ln μ|/T min . Then following a similar process to (16) to (19), we can prove that the control system (1), consisting of both subsystems with Hurwitz A i s and subsystems with A i s that are not Hurwitz, is externally stable with a L 2 gain γ .

Application to H ∞ control
In this section, we apply the derived results of ES to H ∞ control. The so-called H ∞ control is named from the H ∞ functions defined on the H ∞ (Hardy) space (see page 1 in [30]): H ∞ := {F : C → C|F is analytic, sup Re(s)>0 |F(s)| < ∞} equipped with the norm F ∞ := sup Re(s)>0 |F(s)|, for F ∈ H ∞ . As is well known (also see page 4 in [31]), transfer functions for finite dimensional linear control systems are rational functions with real coefficients. Thus, we may consider the subset of H ∞ consisting of real-rational functions: RH ∞ ⊂ H ∞ . In fact [31], a transfer function F(s) ∈ RH ∞ if and only if F is proper (lim s→∞ F(s) < ∞) and stable (F has no poles in the closed right half complex plane). In this case, F ∞ = sup ω∈R |F(jω)| = sup u∈L 2 ,u =θ y L 2 / u L 2 , where u, y denote the input, output of the considered control system [1]. Therefore, the transfer function of a linear control system F(s) is a real-rational H ∞ function implies that the control system is externally stable, i.e. every L 2 input only excites an L 2 zero-state output. If the input is considered to be a disturbance, then ES measures the robustness of the zero-state output on the disturbance, i.e. it ensures that the zero-state output excited by the energy-bounded (because the square of the L 2 norm of a signal can be considered as the energy content of the signal) disturbance will not blow up.
For linear control systems, H ∞ control is to find a control (consisting of measured variables) such that the norm of the transfer function from the disturbance (input) u d to the output y (something we want to minimize) F d→y ∞ is minimized, i.e. the zero-state output excited by disturbance y d is minimized [32]. For nonlinear control systems including the system considered in this paper, they do not have transfer functions as the linear ones do. However, the same name H ∞ control is employed for the following control objective: to find a control such that the controlled system is asymptotically stable when no disturbances are present, and moreover, has finite L 2 gain from u d to y, under the zero initial condition (is externally stable from u d to y), see page 6 in [31]. As we see above, for either linear or nonlinear control systems, H ∞ control has the same physical meaning: the H ∞ controller starts to stabilize the system after the energy-bounded disturbance has already decayed to zero, then maintains the stabilized system to be externally stable from the disturbance to the output such that effect of the disturbance on the output is attenuated during the steady period. This specializes the practical importance of H ∞ control in industry roared with noises. However, by the existing average dwell time approach, those results obtained for switched system are only on weak noise attenuation index of weighted form than cannot truly reflect the practical meaning of H ∞ problems [17].
In this section, by adopting maximum, minimum dwell time and the new proposed twodirection inequality (2), we state the details for the non-weighted H ∞ control of switching control systems with delay and impulse. Consider (1) with both control input u c and disturbance input u d as follows: As just discussed, the control (input) u c is comprised of measured variables. A special (and common) form is u c = K σ (t) x (state feedback), where K σ (t) is the control gain to be designed and x is the state variable that is pre-assumed to be measurable (available). Generally, u c may be also designed as a function of x t (delayed state feedback), x(tk ) (impulsive state feedback) and y (output feedback) as needed, if they can be measured.
Controlled by u c = K σ (t) x, the system above can be rewritten aṡ The H ∞ control problem is to find K σ (t) such that (41) is asymptotically stable when u d = 0, and is externally stable from u d to y, i.e. y(t) L 2 ≤ γ * u d (t) L 2 for some prescribed constant γ * , when φ(θ ) = 0.
Comparing (41) with (1), it can be concluded that the objectives of H ∞ control are all achieved (since exponential stability implies asymptotic stability and the ES is already proven) in different cases if A σ (t) , C σ (t) are replaced byĀ σ (t) ,C σ (t) , respectively, in the corresponding theorems. To avoid tediousness, we only state a theorem for the H ∞ control corresponding to Theorem 3.2. The result corresponding to Theorem 3.1 is left to the reader.
Remark 3.8 After substitutingĀ i ,C i , nonlinear terms like P i B i K i and K T i B T i P i appear in (42) and (43). We can first left and right multiply (42), (43) by diag(P -1 i , I, I, I). Then we apply the Schur complement and use -Q -1 i ≤ -2 i I + 2 i Q i , i > 0 to derive the following linear matrix inequalities of P -1 i , Q i and Y i : (42), (43), respectively. It follows that K i = Y i P i . As for the first inequality in (44), we can first left and right multiply it by diag(P -1 j , I). Then left and right multiply it by diag(I, P -1 i ) to derive an equivalent linear matrix inequal-ity as Thus, all matrix inequalities in Theorem 3.3 are already transformed to linear matrix inequalities of P -1 i , Q i and Y i that can be solved by Matlab.
Remark 3.9 It is arbitrary to pre-assume that a certainĀ i is Hurwitz or not surely Hurwitz, as long as feasible solutions for the inequalities can be found; see Example 4.1, whereĀ 1 is pre-assumed to be Hurwitz.

Illustrative example
In this section, we provide an example of H ∞ control with numerical simulations to illustrate previous results.
As introduced before, the H ∞ controller u c = K σ (t) x starts to stabilize the system (the state x 1 with the initial condition φ(θ ) completely equaling x 2 in each case is almost stabilized between t = 7 s and t = 14 s, and after t = 21 s, see Fig. 5) after the energy-bounded disturbance u d has already decayed to zero (between t = 7 s and t = 14 s, and after t = 21 s; see Fig. 2), then maintains the stabilized system to be externally stable from the disturbance to the output such that the effect of the disturbance on the output is attenuated during the steady period, see γ 2 (t) of each case in Fig. 4, defined as ( under the initial condition φ(θ ), which is less than γ * = 1 and is of almost the same form as γ 0 (t). However, before the system is stabilized for the first time, i.e. during the transient period, the ES cannot be ensured, see γ 1 (t) of each case in Fig. 4, defined as ( t 0 y 2 (s) ds/ t 0 u 2 d (s) ds) 1 2 under the initial condition φ(θ ), which is larger than γ around t = 0 s.

Conclusion
The ES and H ∞ control problem of SSs with delay and impulse has been investigated in this paper. After introducing the definitions of the maximum, minimum DT, we have applied the relation between the number of switchings and the maximum, minimum DT to prove the ES of SSs consisting of subsystems that are all Hurwitz stable. For those SSs comprised of subsystems that are not all Hurwitz stable, a realizable switching law has been employed to study their ES. And then the normal L 2 norm constraint has been derived. The label "weighted" has been removed properly in this paper. Finally, these results have been applied to H ∞ control and illustrated by a numerical example. In the future, we will first study the ES of nonlinear switching control systems without impulse or with impulse, then investigate the stability of SSs with switching signals driven by stochastic processes.