Abstract

This paper investigates the stability properties of a class of dynamic linear systems possessing several linear time-invariant parameterizations (or configurations) which conform a linear time-varying polytopic dynamic system with a finite number of time-varying time-differentiable point delays. The parameterizations may be timevarying and with bounded discontinuities and they can be subject to mixed regular plus impulsive controls within a sequence of time instants of zero measure. The polytopic parameterization for the dynamics associated with each delay is specific, so that (𝑞+1) polytopic parameterizations are considered for a system with 𝑞 delays being also subject to delay-free dynamics. The considered general dynamic system includes, as particular cases, a wide class of switched linear systems whose individual parameterizations are timeinvariant which are governed by a switching rule. However, the dynamic system under consideration is viewed as much more general since it is time-varying with timevarying delays and the bounded discontinuous changes of active parameterizations are generated by impulsive controls in the dynamics and, at the same time, there is not a prescribed set of candidate potential parameterizations.

1. Introduction

The stabilization of dynamic systems is a very important question since it is the first requirement for most of applications. Powerful techniques for studying the stability of dynamic systems are Lyapunov stability theory and fixed point theory which can be easily extended from the linear time-invariant case to the time-varying one as well as to functional differential equations, as those arising, for instance, from the presence of internal delays, and to certain classes of nonlinear systems, [1, 2]. Dynamic systems which are of increasing interest are the so-called switched systems which consist of a set of individual parameterizations and a switching law which selects along time, which parameterization is active. Switched systems are essentially timevarying by nature even if all the individual parameterizations are timeinvariant. The interest of such systems arises from the fact that some existing systems in the real world modify their parameterizations to better adapt to their environments. Another important interest of some of such systems relies on the fact that changes of parameterizations through time can lead to benefits in certain applications, [313]. The natural way of modelling these situations lies in the definition of appropriate switched dynamic systems. For instance, the asymptotic stability of Liénard-type equations with Markovian switching is investigated in [4, 5]. Also, time-delay dynamic systems are very important in the real life for appropriate modelling of certain biological and ecology systems and they are present in physical processes implying diffusion, transmission, tele-operation, population dynamics, war and peace models, and so forth. (see, e.g., [1, 2, 1218]). Linear switched dynamic systems are a very particular case of the dynamic system proposed in this paper. Switched systems are very important in practical applications since their parameterizations are not constant. A switched system can result, for instance, from the use of a multimodel scheme, a multicontroller scheme, a buffer system or a multiestimation scheme. For instance, a (nonexhaustive) list of papers deal with some of these questions related to switched systems follow(1)In [15], the problem of delay-dependent stabilization for singular systems with multiple internal and external incommensurate delays is focused on. Multiple memoryless state-feedback controls are designed so that the resulting closed-loop system is regular, independent of delays, impulsefree and asymptotically stable. A relevant related problem for obtaining sufficiency-type conditions of asymptotic stability of a time-delay system is the asymptotic comparison of its solution trajectory with its delayfree counterpart provided that this last one is asymptotically stable, [19].(2)In [20], the problem of the 𝑁-buffer switched flow networks is discussed based on a theorem on positive topological entropy.(3)In [21], a multi-model scheme is used for the regulation of the transient regime occurring between stable operation points of a tunnel diode-based triggering circuit.(4)In [22, 23], a parallel multi-estimation scheme is derived to achieve close-loop stabilization in robotic manipulators whose parameters are not perfectly known. The multi-estimation scheme allows the improvement of the transient regime compared to the use of a single estimation scheme while achieving at the same time closed-loop stability.(5)In [24], a parallel multi-estimation scheme allows the achievement of an order reduction of the system prior to the controller synthesis so that this one is of reducedorder (then less complex) while maintaining closed-loop stability. (6)In [25], the stabilization of switched dynamic systems is discussed through topologic considerations via graph theory.(7)The stability of different kinds of switched systems subject to delays has been investigated in [1113, 17, 2628].(8)The stability switch and Hopf bifurcation for a diffusive prey-predator system is discussed in [6] in the presence of delay. (9)A general theory with discussed examples concerning dynamic switched systems is provided in [3].(10)Some concerns of time-delay impulsive models are of increasing interest in the areas of stabilization, neural networks, and Biological models with particular interest in positive dynamic systems. See, for instance, [2940] and references therein.

The dynamic system under investigation is a linear polytopic system subject to internal point delays and feedback state-dependent impulsive controls. Both parameters and delays are assumed to be timevarying in the most general case. The control impulses can occur as separate events from possible continuous-time or bounded-jump type parametrical variations. Furthermore, each delayed dynamics is potentially parameterized in its own polytope. Those are the main novelties of this paper since it combines a time-varying parametrical polytopic nature with individual polytopes for the delay-free dynamics with time-varying parameters which are unnecessarily smooth for all time with a potential presence of delayed dynamics with point time-varying delays. The case of switching between parameterizations at certain time instants, what is commonly known as a switched system, [3, 17, 2028], is also included in the developed formalism as a particular case as being equivalent to define the whole systems as a particular parameterization of the polytopic system at one of its vertices. The delays are assumed to be time differentiable of bounded time-derivative for some of the presented stability results but just bounded for the rest of results. An important key point is that if the system is stabilizable, then it can be stabilized via impulsive controls without requiring the delay-free dynamics of the system as it is then shown in some of the given examples. Usually, for a given interimpulse time interval, the impulsive amplitudes are larger as the instability degree becomes larger, and the signs of the control components also should be appropriate, in order to compensate it by the stabilization procedure. Such a property also will hold for nonpolytopic parameterizations. The design philosophy adopted in the paper is that stabilization might be achieved through appropriate impulsive controls at certain impulsive time instants without requiring the design of a standard regular controller. The paper is organized as follows. Section 2 discusses the various evolution operators valid to build the state-trajectory solutions in the presence of impulsive feedback state-dependent controls. Analytic expressions are given to define such operators. In particular, an important operator defined and discussed in this paper is the so-called impulsive evolution operator. Such an evolution operator is sufficiently smooth within open time intervals between each two consecutive impulsive times, but it also depends on impulses at time instants with hose ones happen. Section 3 discusses new global stability and global asymptotic stability issues based on Krasovsky-Lyapunov functionals taking account of the feedback state-dependent control impulses. The relevance of the impulsive controls towards stabilization is investigated in the sense that the most general results do not require stability properties of the impulse-free system (i.e., that resulting as a particular case of the general one in the absence of impulsive controls). Some included very conservative stability results follow directly from the structures of the state-trajectory solution and the evolution operators of Section 2 without invoking Lyapunov stability theory. It is proven that stabilization is achievable if impulses occur at certain intervals and with the appropriate amplitudes. Finally, two application examples are given in Section 4.

Notation 1.1. Z, R, and C are the sets of integer, real, and complex numbers, respectively.
𝐙+ and 𝐑+ denote the positive subsets of 𝐙, respectively, and 𝐂+ denotes the subset of C of complex numbers with positive real part, and 𝑛={1,2,,𝑛}𝐙+, forall𝑛𝐙+.
𝐙 and 𝐑 denote the negative subsets of 𝐙, respectively, and 𝐂 denotes the subset of C of complex numbers with negative real part.𝐙0+=𝐙+{0},𝐑0+=𝐑+{0},𝐂0+=𝐂+𝐙{0}0=𝐙{0},𝐑0=𝐑{0},𝐂0=𝐂{0}(1.1)
Given some linear space 𝑋 (usually R or C), then C(𝑖)(𝐑0+,𝑋) denotes the set of functions of class 𝐶(𝑖). Also, BPC(𝑖)(𝐑0+,𝑋)and PC(𝑖)(𝐑0+,𝑋) denote the set of functions in 𝐶(𝑖1)(𝐑0+,𝑋) which, furthermore, possess bounded piecewise continuous or, respectively, piecewise continuous 𝑖th derivative on 𝑋.
𝐿(𝑋) denotes the set of linear operators from 𝑋 to 𝑋. In particular, the linear space denoted by 𝑋 denotes the state space of the dynamic system with controls in the linear space 𝑈.
𝐼𝑛 denotes the 𝑛th identity matrix.
The symbols 𝑀0,𝑀0,𝑀0,and𝑀0 stand for positive definite, negative definite, positive semidefinite, and negative semidefinite square real matrices 𝑀, respectively. The notations 𝑀𝐷,𝑀𝐷,𝑀𝐷,and𝑀𝐷 stand correspondingly for (𝑀𝐷)0,(𝑀𝐷)0,(𝑀𝐷)0,and(𝑀𝐷)0, and Superscript “𝑇” stands for transposition of matrices and vectors.
𝜆max(𝑀) and 𝜆min(𝑀)stand for the maximum and minimum eigenvalues of a definite square real matrix 𝑀=(𝑚𝑖𝑗).
A finite or infinite strictly ordered sequence of impulsive time instants is defined by Imp={𝑡𝑖𝐑0+𝑡𝑖+1>𝑡𝑖}, where an impulsive control 𝑢(𝑡𝑖)𝛿(𝑡𝑡𝑖) occurs with 𝛿() being the Dirac delta of the Dirac distribution.

2. The Dynamic System Subject to Time Delays and Impulsive Controls

Consider the following polytopic linear time-differential system of state vector and control of respective dimensions 𝑛 and 𝑚 and being subject to 𝑞 time-varying point delays:̇𝑥(𝑡)=𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗𝐴(𝑡)𝑖𝑗(𝑡)𝑥𝑡𝑖(𝑡)+𝐵𝑖𝑗(𝑡)𝑢𝑖𝑗(𝑡)=𝜆𝑇(𝑡)𝑥(𝑡)+,𝑢(𝑡)(2.1) where the incommensurate time-varying delays are 0(𝑡)=0forall𝑡𝐑0+, 𝑖PC(1)(𝐑0+,𝐑0+), forall𝑖𝑞={1,2,,𝑞} (i.e., the delays are continuous time differentiable of bounded time derivative), and𝜆𝑇𝜆(𝑡)=01(𝑡)𝜆02(𝑡)𝜆0𝑁(𝑡)𝜆𝑞1(𝑡)𝜆𝑞2(𝑡)𝜆𝑞𝑁,(𝑡)𝑥𝑇𝑥(𝑡)=𝑇𝐴(𝑡)𝑇01(𝑡)𝐴𝑇0𝑁(𝑡)𝑥𝑇𝑡𝑞𝐴(𝑡)𝑇𝑞1(𝑡)𝐴𝑇𝑞𝑁,(𝑡)𝑢𝑇𝑢(𝑡)=𝑇01(𝑡)𝐵𝑇01(𝑡)𝑢𝑇0𝑁(𝑡)𝐵𝑇0𝑁(𝑡)𝑢𝑇𝑞1(𝑡)𝐵𝑇𝑞1(𝑡)𝑢𝑇𝑞𝑁(𝑡)𝐵𝑇𝑞𝑁(𝑡)(2.2) are vector functions from 𝐑0+ to 𝐑(𝑞+1)𝑁, 𝐑(𝑞+1)𝑁𝑛 and 𝐑(𝑞+1)𝑁𝑚, respectively, and

(i) 𝑥𝐑0+[,0)𝑋𝐑𝑛 is the state vector, which is almost everywhere time differentiable on 𝐑0+ satisfying (2.1), subject to bounded piecewise continuous initial conditions on [,0),that is, 𝑥=𝜑BPC(0)([,0],𝐑𝑛), where =(0)=max𝑖𝑞sup(𝑖(0))=max𝑖𝑞sup𝑡𝐑0+((𝑡)), and 𝑢𝑖𝑗𝐑0+𝑈𝐑𝑚 are the control vectors forall𝑖𝑞{0}forall𝑗𝑁 and 𝐴𝑖𝑗BPC(0)(𝐑0+,𝐑𝑛×𝑛) and 𝐵𝑖𝑗BPC(0)(𝐑0+,𝐑𝑛×𝑚) parameterize the dynamic system.

(ii) 𝜆𝑖𝑗BPC(0)(𝐑0+,𝐑0+), subject to the constraint 𝑞𝑖=0𝑁𝑗=0𝜆𝑖𝑗(𝑡)[𝑐1,𝑐2]𝐑+,forall𝑡𝐑0+ with >𝜀2𝑐2𝑐1𝜀10 are the weighting scalar functions defining the polytopic system in the various delayed dynamics and parameterizations which are not all simultaneously zero at any time for some given lower-bound and upper-bound scalars 𝜀1 and 𝜀2. Note that there exist two summations in (2.1) related to these scalar functions, one them referring to the contribution of delayed dynamics for the various delays and the second one related to the system parameterization within the polytopic structure. It will be not assumed through the paper that the delay-free auxiliary system is stable. Note that the dynamic system can be seen as a convex polytopic dynamic systeṁ𝑥(𝑡)=𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗(𝑡)̇𝑥𝑖𝑗(𝑡)(2.3) formed with subsystems of the form ̇𝑥𝑖𝑗(𝑡)=𝐴𝑖𝑗(𝑡)𝑥(𝑡𝑖(𝑡))+𝐵𝑖𝑗(𝑡)𝑢𝑖𝑗(𝑡). The controls 𝑢𝑖𝑗𝐑0+𝑈𝐑𝑚 are generated from the state-feedback impulsive controller as follow: 𝑢𝑖𝑗(𝑡)=𝐾𝑖𝑗(𝑡)𝑥𝑡𝑖(𝑡)𝑖𝑞={1,2,,𝑞};𝑡𝐑0+𝑢,for𝑖=0,𝑡Imp,0𝑗𝑡+=𝐾0𝑗𝑡++𝐾0𝑗𝑥𝑡(𝑡)+for𝑖=0,𝑡Imp,(2.4) where the strictly ordered Imp:={𝑡𝑖𝐑0+𝑡𝑖+1>𝑡𝑖,𝑖𝐙+} is the so-called sequence of impulsive time instants where the control impulses occur whose elements form a monotonically increasing sequence; that is, for any well posed test function 𝑓𝐑𝐑, 𝑓(𝑡)=𝑓(𝜏)𝛿(𝑡𝜏)𝑑𝜏=𝑡+𝑡𝑓(𝜏)𝛿(𝑡𝜏)𝑑𝜏=lim𝜀0+𝑡+𝜀𝑡𝜀𝑓(𝜏)𝛿(𝑡𝜏)𝑑𝜏,(2.5) where 𝛿(𝑡) is the Dirac distribution at time 𝑡=0 with the following notational convention being used:𝑔(𝑡+)=lim𝜀0+𝑔(𝑡+𝜀)𝑔(𝑡)=lim𝜀0+𝑔(𝑡𝜀) either if 𝑡Imp or if 𝑔 is bounded having left and right limits at a discontinuity point 𝑡𝐑0+, and 𝑔(𝑡+)=𝑔(𝑡)if 𝐑0+𝑡Imp since the functions used are all left-continuous functions. Partial sequences of impulsive time instants are denoted by specifying the time intervals they refer to, as for instance, Imp[𝑇1,𝑇2]={𝑡Imp𝑡[𝑇1,𝑇2]} and Imp[𝑇1,𝑇2)={𝑡Imp𝑡[𝑇1,𝑇2)}. Note that Imp=Imp[0,). The regular and impulsive controller gain matrices are, respectively, 𝐾𝑖𝑗BPC(0)(𝐑0+,𝐑𝑚×𝑛) and 𝐾𝑖𝑗Imp𝐑𝑚×𝑛 being a discrete sequence of bounded matrices. Note that, if 𝐾0𝑗(𝑡) is discontinuous at the time instant 𝑡, then 𝐾0𝑗(𝑡+)𝐾0𝑗(𝑡) even if 𝑡Imp. The extensions to vector and matrix test functions are obvious by using respective appropriate zero components or entries if impulses do not occur at time 𝑡, a particular component or matrix entry. The substitution of the control law (2.4) into the open-loop system equation (2.1) leads to the closed-loop functional dynamic system as follows:̇𝑥(𝑡)=𝑁𝑗=1𝜆0𝑗𝐴(𝑡)0𝑗(𝑡)+𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝛿(0)𝑥(𝑡)+𝑞𝑖=1𝑁𝑗=1𝜆𝑖𝑗(𝑡)𝐴𝑖𝑗(𝑡)𝑥𝑡𝑖,𝑥𝑡(𝑡)+=𝐼𝑛+𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗𝑥(𝑡)(𝑡);(2.6)

forall𝑡𝐑0+ with 𝐾0𝑗(𝑡)=0; forall𝑡Imp, where𝐴𝑖𝑗(𝑡)=𝐴𝑖𝑗(𝑡)+𝐵𝑖𝑗(𝑡)𝐾𝑖𝑗(𝑡),𝑖𝑞{0}𝑗𝑁,(2.7)

Equation (2.6) becomeṡ𝑥(𝑡)=𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗(𝑡)𝐴𝑖𝑗(𝑡)𝑥𝑡𝑖(𝑡),(2.8) for all 𝑡Imp and also at the left limits for all 𝑡Imp, and 𝑥(𝑡+)𝑥(𝑡)=𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝑥(𝑡), which is zero if 𝑡Imp, with 𝑡̇𝑥+=𝑁𝑗=1𝜆0𝑗(𝑡)𝐴0𝑗𝑡+𝑥𝑡++𝑞𝑁𝑖=1𝑗=1𝜆𝑖𝑗(𝑡)𝐴𝑖𝑗𝑡+𝑥𝑡+𝑖(𝑡)(2.9) for the right limits of all 𝑡Imp. Define 𝐷=Imp𝐷𝑝, where𝐷𝑝=𝑖𝑞{0},𝑗𝑁𝐷𝐴𝑖𝑗𝑖𝑞{0},𝑗𝑁𝐷𝐵𝑖𝑗𝑖𝑞{0},𝑗𝑁𝐷𝜆𝑖𝑗𝑖𝑞{0},𝑗𝑁𝐷𝐾𝑖𝑗(2.10) is the total set of discontinuities on 𝐑0+ of 𝐴𝑖𝑗BPC(0)(𝐑0+,𝐑𝑛×𝑛), 𝐵𝑖𝑗BPC(0)(𝐑0+,𝐑𝑛×𝑚), 𝜆𝑖𝑗BPC(0)(𝐑0+,𝐑0+), and 𝐾𝑖𝑗BPC(0)(𝐑0+,𝐑𝑚×𝑛)forall𝑖𝑞{0}, forall𝑗𝑁 which are in the respective sets 𝐷𝐴𝑖𝑗, 𝐷𝐵𝑖𝑗, 𝐷𝜆𝑖𝑗, and 𝐷𝐾𝑖𝑗. The following technical assumptions are made.

Assumption. thereexist𝜐𝐑+ such that 𝑡𝑘+1𝑡𝑘𝜐,forall𝑡𝑘,𝑡𝑘+1(>𝑡𝑘)Imp.

Assumption. ((𝑗𝑁𝐷𝐵0𝑗)(𝑗𝑁𝐷𝜆𝑖𝑗))Imp=.
Assumption 2.1 implies that the sequence of impulsive time instants is a real sequence with no accumulation points. It is a technical assumption to guarantee the existence and uniqueness of an almost everywhere time-differentiable state-trajectory solution. Assumption 2.2 is needed for all the functions 𝜆0𝑗(𝐵0𝑗)𝑘BPC(0)(𝐑0+,𝐑0+)forall𝑗𝑁, forall𝑘𝑛 and forall𝑚, build with the entries 𝐵0𝑗BPC(0)(𝐑0+,𝐑𝑛×𝑚). This follows since they are piecewise continuous on 𝐑0+ and, furthermore, continuous at any small neighborhood around any point of the sequence of impulsive time instants where control impulses occur. From Picard-Lindeloff theorem, there is a unique solution for any vector function of initial conditions 𝜑BPC(0)([,0],𝐑𝑛) and 𝑥BPC(1)(𝐑+,𝐑𝑛). The state-trajectory solution of the closed-loop system (2.8)-(2.9) for initial conditions  𝜑BPC(0)([,0],𝐑𝑛) is given byΨ𝑥(𝑡)=Ψ(𝑡)1(0)𝑥(0)+𝑞𝑁𝑖=1𝑗=1𝑡0Ψ1(𝜏)𝜆𝑖𝑗(𝜏)𝐴𝑖𝑗(𝜏)𝑥𝜏𝑖+(𝜏)𝑑𝜏𝑡𝑘Imp[𝑁0,𝑡)𝑗=1𝜆0𝑗𝑡𝑘Ψ1𝑡𝑘𝐵0𝑗𝑡𝑘𝐾0𝑗𝑡𝑘𝑥𝑡𝑘=Ψ𝑠𝑡,𝑡0𝑥𝑡0+𝑞𝑁𝑖=1𝑗=1𝑡0𝜆𝑖𝑗(𝜏)Ψ𝑠(𝑡,𝜏)𝐴𝑖𝑗(𝜏)𝑥𝜏𝑖+(𝜏)𝑑𝜏𝑡𝑘Imp𝑡0𝑁,𝑡𝑗=1𝜆0𝑗𝑡𝑘Ψ𝑠𝑡,𝑡𝑘𝐵0𝑗𝑡𝑘𝐾0𝑗𝑡𝑘𝑥𝑡𝑘,(2.11) subject to 𝑥(𝑡)=𝜑(𝑡),forall𝑡[,0], where(1)Ψ(𝑡)𝐶(0)(𝐑0+,𝐑𝑛×𝑛) is an almost everywhere differentiable matrix function on 𝐑+ (being time differentiable on the non connected real set 𝑡𝑖Imp(𝑡𝑖+1𝑡𝑖)) with unnecessarily continuous time derivatives which satisfies ̇Ψ(𝑡)=𝑁𝑗=1𝜆0𝑗(𝑡)𝐴0𝑗(𝑡)Ψ(𝑡) on 𝐑+ with Ψ(0)=𝐼𝑛. If 𝐴𝑖𝑗, 𝐵𝑖𝑗, 𝜆𝑖𝑗,and 𝐾𝑖𝑗forall𝑖𝑞{0}, forall𝑗𝑁 are everywhere continuous on 𝐑+,then Ψ(𝑡)𝐶(1)(𝐑0+,𝐑𝑛×𝑛), Ψ𝑠(,)𝐑20+𝐑𝑛×𝑛as Ψ𝑠(𝑡,𝜏)=Ψ(𝑡)Ψ1(𝜏)forall𝑡𝜏, and (2)Imp[𝑡0,𝑡):={𝑡𝑘𝐑0+𝑡0𝑡𝑘(Imp)<𝑡}Imp is the strictly ordered sequence of impulsive time instants with input impulses occurred on [𝑡0,𝑡) for any 𝑡0𝐑+. Also, Imp(𝑡0,𝑡):={𝑡𝑘Imp𝑡0<𝑡𝑘<𝑡}Imp;Imp(𝑡0,𝑡]:={𝑡𝑘Imp𝑡0<𝑡𝑘𝑡}Imp are defined in a closed way.The solution (2.11) is identically defined by 𝑍𝑥(𝑡)=𝑍(𝑡)1(0)𝑥(0)+0𝑍1+(𝜏)𝜑(𝜏)𝑑𝜏𝑡𝑘Imp𝑁(0,𝑡)𝑗=1𝜆0𝑗𝑡𝑘𝑍1𝑡𝑘𝐵0𝑗𝑡𝑘𝐾0𝑗𝑡𝑘𝑥𝑡𝑘,(2.12) where 𝑍(𝑡)𝐶(0)(𝐑0+,𝐑𝑛×𝑛) is an almost everywhere differentiable matrix function on 𝐑+, with unnecessarily continuous time derivatives, which satisfies (2.8) on 𝐑+ with Z (0)=𝐼𝑛, 𝑍(𝑡)=0forall𝑡𝐑. Defining the matrix function 𝑍𝑠(,)𝐑20+𝐑𝑛×𝑛 as 𝑍𝑠(𝑡,𝜏)=𝑍(𝑡)𝑍1(𝜏)forall𝑡𝜏, one has from (2.12) for 𝑡[𝑡𝑘,𝑡𝑘+1] for any two consecutive given𝑡𝑘,𝑡𝑘+1Imp as follow: 𝑥(𝑡)=𝑍𝑠𝑡,𝑡𝑘𝑥𝑡+𝑘+𝑞𝑖=10𝑖𝑍𝑠𝑡,𝑡𝑘𝜑𝑡+𝜏𝑘++𝜏𝑑𝜏𝑁𝑗=1𝑍𝑠𝑡,𝑡𝑘𝜆0𝑗𝑡𝑘𝐵0𝑗𝑡𝑘+1𝑥𝑡+𝑘+1𝐾0𝑗𝑡𝑘+1,(2.13) which becomes for 𝑡=𝑡+𝑘+1 as follow: 𝑥𝑡+𝑘+1=𝐼𝑛+𝑁𝑗=1𝑍𝑠𝑡𝑘+1,𝑡𝑘𝐵0𝑗𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝑥𝑡𝑘+1=𝑍𝑠𝑡𝑘+1,𝑡𝑘𝑥𝑡+𝑘+𝑞𝑖=10𝑖𝑍𝑠𝑡,𝑡𝑘𝜑𝑡+𝜏𝑘++𝜏𝑑𝜏𝑁𝑗=1𝑍𝑠𝑡𝑘+1,𝑡𝑘𝜆0𝑗𝑡𝑘𝐵0𝑗𝑡𝑘+1𝑥𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝛿𝑡,𝑡𝑘+1,(2.14) where 𝛿(𝑡,𝑡𝑘+1)=1 if 𝑡=𝑡𝑘+1 and zero otherwise is the Kronecker delta. In view of (2.12), the state-trajectory solution can be defined by the impulsive evolution operator {𝑇(𝑡,𝑡𝑘)𝑡[𝑡𝑘,𝑡𝑘+1],forall𝑡𝑘Imp}, associated with {𝑍(𝑡)𝑡𝐑0+} where 𝑇(,){([𝑡𝑘,𝑡𝑘+1]𝑡𝑘Imp{0})}𝐿(𝑋), which is represented by 𝑥(𝑡)=𝑇(𝑡,𝑡𝑘)𝑥𝑡+𝑘; forall𝑡[𝑡𝑘,𝑡𝑘+1],forall𝑡𝑘Impso that: 𝑥(𝑡)=𝑇𝑡,𝑡𝑘𝑥𝑡+𝑘,𝑥𝑡+𝑘+1𝑡=𝑇+𝑘+1,𝑡𝑘𝑥𝑡+𝑘=𝐼𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝑘+1𝐵0𝑗𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝑇𝑡𝑘+1,𝑡𝑘𝑥𝑡+𝑘,(2.15)forall𝑡[𝑡𝑘,𝑡𝑘+1],forall𝑡𝑘Imp, where 𝑥𝑡 and 𝑥𝑡+ denote the strings of state solution trajectory and {𝑥(𝜏)𝜏[𝑡,𝑡)} and {𝑥(𝜏)𝜏[𝑡,𝑡]}, respectively. The subsequent result follows directly for the state-trajectory solution from (2.11) for any initial conditions 𝜑BPC(0)([,0],𝐑𝑛).

Theorem 2.3. The following properties hold.
(i) The state-trajectory solution satisfies the following equations on any interval [𝜁,𝑡)𝐑0+for any 𝜑BPC(0)([,0],𝐑𝑛): 𝑥𝑡+𝑘+1=𝐼𝑛+𝑁𝑗=1Ψ𝑠𝑡𝑘+1,𝑡𝑘+1𝜆0𝑗𝑡𝑘+1𝐵0𝑗𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝑥𝑡𝑘+1(2.16)=Ψ𝑠𝑡𝑘+1𝑥𝜁,𝜁++𝑡𝑘+1𝜁+Ψ𝑠𝑡𝑘+1,𝜏𝑞𝑁𝑖=1𝑗=1𝜆𝑖𝑗(𝜏)𝐴𝑖𝑗(𝜏)𝑥𝜏𝑖+(𝜏)𝑑𝜏𝑡𝑖Imp𝜁,𝑡𝑘+1𝑁𝑗=1𝜆0𝑗𝑡𝑖Ψ𝑠𝑡𝑘+1,𝑡𝑖𝐵0𝑗𝑡𝑖𝐾0𝑗𝑡𝑖𝑥𝑡𝑖=𝐼(2.17)𝑛+𝑁𝑗=1Ζ𝑠𝑡𝑘+1,𝑡𝑘+1𝐵0𝑗𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝑥𝑡𝑘+1(2.18)=Ζ𝑠𝑡𝑘+1𝑥𝜁,𝜁++𝑞𝑖=10𝑖𝑍𝑠𝑡𝑘+1𝑥+,𝜁+𝜏(𝜁+𝜏)𝑑𝜏𝑡𝑖Imp𝜁,𝑡𝑘+1𝑁𝑗=1𝜆0𝑗𝑡𝑖𝑍𝑠𝑡𝑘+1,𝑡𝑖𝐵0𝑗𝑡𝑖𝑥𝑡𝑖𝐾0𝑗𝑡𝑖𝑡(2.19)=𝑇+𝑘+1𝑥,𝜁𝜁+=(2.20)𝑡𝑖,𝑡𝑖+1Imp𝜁,𝑡𝑘+1𝐼𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝑖+1𝐵0𝑗𝑡𝑖+1𝐾0𝑗𝑡𝑖+1𝑇𝑡𝑖+1,𝑡𝑖𝑥𝜁+,(2.21)forall𝑡𝑘+1(>𝜁)Imp,forall𝜁𝐑0+ with 𝑇(𝑡𝑘+1,𝑡𝑘+1)=𝑍𝑠(𝑡𝑘+1,𝑡𝑘+1)=Ψ𝑠(𝑡𝑘+1,𝑡𝑘+1)=𝐼𝑛. Equations (2.17) and (2.19) are also valid by replacing 𝑡𝑘+1𝑡, forall𝑡(𝑡𝑘+1,𝑡𝑘+2) if 𝑡𝑘+2Impand forall𝑡(𝑡𝑘+1,) if (𝑡𝑘+1,)Imp=, that is, if the sequence of impulsive time instants is finite with the last impulsive time instant being 𝑡𝑘+1. Equation (2.21) has to be modified by replacing𝑡𝑘+1𝑡and then by premultiplying it by 𝑇(𝑡,𝑡𝑘+1).
(ii) Assume that 𝑡𝑖,𝑡𝑖+1Imp𝜁,𝑡𝑘+1𝐼𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝑖+1𝐵0𝑗𝑡𝑖+1𝐾0𝑗𝑡𝑖+1𝑇𝑡𝑖+1,𝑡𝑖𝑀𝑇𝐼1(2.22)𝑛+𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗𝑇(𝑡)𝑡,𝑡𝑐imp𝑀𝑇1,(2.23)forall𝑡𝑘+1(>𝜁)Imp, forall𝜁𝐑0+, and forall𝑡𝑡𝑐imp provided that 𝑐imp=cardImp[0,)<, then Γ𝑥Lp(𝐑+,𝑋)𝐶Γ, where ΓDom(Γ)𝑋L𝑝(𝐑+,𝑋) is defined by (Γ𝑥)(𝑡)=𝑇(𝑡,𝜃)𝑥. for all 𝑥𝑋.

Proof. (i) It follows directly for the state-trajectory solution from (2.11), (2.14), and (2.15) for any time interval [𝜁,𝜁) of initial conditions 𝜑BPC(0)([,0],𝐑𝑛).
(ii) The first part follows from the definition of the impulsive evolution operator. If, in addition, 𝑀𝑇<1, then it follows from the following given constraints: lim𝑡𝑇(𝑡,𝜃)𝜉=0,𝑡(>𝜃)𝐑+,𝜃𝐑0+,𝜉𝑋𝑇(𝑡,𝜃)𝜉(2.24) is bounded, forall𝜉𝑋, forall𝑡(>𝜃)𝐑+,𝜃𝐑0+𝑇(𝑡,𝜃)𝐶𝑇,some𝐑𝐶𝑇1,𝑡(>𝜃)𝐑+,𝜃𝐑0+(2.25) (from the uniform boundedness principle). Now, note that the operator ΓDom(Γ)𝑋𝐿𝑝(𝐑+,𝑋) is closed and then bounded from the closed graph theorem, so that the proof of Property (ii) is complete.

Remark 2.4. Stabilization by impulsive controls may be combined with the design of regular stabilization controllers or used as the sole stabilization tool. Some advantages related to the use of impulsive control for stabilization of stabilizable systems arise in the cases when the classical regular controller are of high design and maintenance costs.

3. Stability

The global asymptotic stability of the controlled system is now investigated. Firstly, a conservative stability result follows from Theorem 2.3 (2.16)–(2.21), which does not take into account possible compensations of the impulsive controls for stabilization purposes.

Theorem 3.1. Assume that the sequence Imp is infinite, Ψ𝑠(𝑡,𝜏)𝑘Ψ𝑒𝜌𝜓(𝑡𝜏), forall𝑡𝜏+𝑡0, some finite 𝑡0>0,some 𝐑+𝑘Ψ>0, and some 𝜌𝜓𝐑+ as follow: 𝑘Ψ1+sup𝑡𝑘+𝑖𝑝𝜏𝑡𝑘+(𝑖+1)𝑝𝑞𝑖=1𝑁𝑗=1𝜆𝑖𝑗(𝜏)𝐴𝑖𝑗(𝜏)2𝜌Ψ+𝑡𝑗Imp𝑡𝑘+𝑖𝑝,𝑡𝑘+(𝑖+1)𝑝𝑁𝑗=1𝜆0𝑗𝑡𝑗𝐵0𝑗𝑡𝑗𝐾0𝑗𝑡𝑗𝑒𝜌Ψ(𝑡𝑘+(𝑗+1)𝑝𝑡𝑗)21,(3.1) for some 𝑝𝐙+, some finite 𝑘𝐙0+, some subsequence {𝑡𝑘+𝑖𝑝}Imp, forall𝑖𝐙0+. Thus, the closed-loop system (2.8)-(2.9) is globally stable. If the above inequality is strict, then the system is globally asymptotically stable. Also, if the sequence Imp is finite, then the results are valid 𝑘Ψ(1+sup𝑡𝑘𝜏<𝑞𝑖=1𝑁𝑗=1𝜆𝑖𝑗(𝜏)𝐴𝑖𝑗(𝜏)2/𝜌Ψ)1(<1)with 𝑡𝑘 being the last element of the finite sequence Imp

Now, a general stability result follows, which proves that (in general, nonasymptotic) global stability is achievable by some sequence of impulsive controls generated from appropriate impulsive controller gains.

Theorem 3.2. There is a sequence of impulsive time instants Imp={𝑡𝑖𝐑0+} such that the closed-loop system (2.6)–(2.7) is globally stable for any function of initial conditions 𝜑BPC(0)([,0],𝐑𝑛) for some sequence of impulsive controller gains 𝐾0𝑗𝐑0+𝐑𝑛×𝑚, forall𝑗𝑁,forall𝑖𝑞{0}.

Proof. The basic equation to build the stability proof is 𝑥(𝑡+)𝑥(𝑡)=𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝑥(𝑡), forall𝑡Imp and any sequence of impulsive time instants Imp. Consider prefixed real constants 𝐾𝑖𝐑+(𝑖4) fulfilling 𝐾1𝐾3𝜀1 and 𝐾4𝐾2𝜀2 with 𝜀1(0,𝐾3)𝐑0+ and 𝜀2(0,𝐾2)𝐑0+such that 𝑥𝑘(0)[𝐾3,𝐾4][𝐾1+𝜀1,𝐾2𝜀2][𝐾1,𝐾2], for all 𝑘𝑛. The proof of global stability is now made by complete induction. Assume that some finite or infinite 𝑡𝐑+ exists such that 𝑥𝑘(𝜏)[𝐾1,𝐾2]; forall𝜏[0,𝑡), but 𝑥𝑘(𝑡)((,𝐾3)(𝐾4,))[𝐾1,𝐾2]for some 𝑘𝑛, some 𝐾3𝐑 with an existing (perhaps empty) partial sequence of impulsive time instants Imp[0,𝑡) until time 𝑡. Such a time 𝑡 always exists from the boundedness and almost everywhere continuity of the state-trajectory solution. Then, 𝑡Imp so that Imp[0,𝑡]=Imp[0,𝑡){𝑡} is fixed as the first impulsive time instant and <𝐾3𝑥𝑘𝑡+=𝛿(𝑘,)+𝑁𝑚𝑗=1𝑛𝑖=1=1𝜆0𝑗(𝑡)𝐵0𝑗𝑘𝑖(𝑡)𝐾0𝑗𝑖𝑥(𝑡)(𝑡)𝐾4<,(3.2) where the entry notation 𝑀=(𝑀𝑖𝑗)for a matrix 𝑀 is used, provided that the impulsive controller gain 𝐾0𝑗𝑖𝑘(𝑡) is chosen so that the following constraint holds: 𝐾3𝑁𝑗=1𝑚𝑖(𝑘)=1𝑛(𝑘)=1𝜆0𝑗(𝑡)𝐵0𝑗𝑘𝑖(𝑡)𝐾0𝑗𝑖𝑥(𝑡)(𝑡)𝑥𝑘(𝑡)1+𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗𝑘𝑖(𝑡)𝐾0𝑗𝑖𝑘𝑥(𝑡)𝑘(𝑡)𝐾0𝑗𝑘𝑘𝐾(𝑡)4𝑁𝑗=1𝑚𝑖(𝑘)=1𝑛(𝑘)=1𝜆0𝑗(𝑡)𝐵0𝑗𝑘𝑖(𝑡)𝐾0𝑗𝑖𝑥(𝑡)(𝑡)𝑥𝑘(𝑡)1+𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗𝑘𝑖(𝑡)𝐾0𝑗𝑘𝑘𝑥(𝑡)𝑘.(𝑡)(3.3)
Note by direct inspection of (3.3) that such a controller gain always exists. As a result, 𝑥𝑘(𝑡+)[𝐾3,𝐾4][𝐾1,𝐾2], forall𝑘𝑛. By continuity of the state-trajectory solution, there exists a finite 𝑇(𝑡,𝐾)𝐑+ such that 𝑥𝑘(𝜏)[𝐾3𝐾,𝐾4+𝐾][𝐾1,𝐾2] for any prefixed 𝐾𝐑+, forall𝜏[𝑡,𝑡+𝑇(𝑡,𝐾)), forall𝑘𝑛 provided that𝐾3𝐾1𝐾𝐾2𝐾4. Since 𝑥𝑘(𝑡+𝑇(𝑡,𝐾))((,𝐾3)(𝐾4,))[𝐾1,𝐾2]then 𝑥𝑘(𝜏)[𝐾1,𝐾2],forall𝜏[0,𝑡+𝑇(𝑡)), forall𝑘𝑛. Also, 𝑥𝑘(𝜏)[𝐾1,𝐾2] for all𝜏[0,𝑡+𝑇(𝑡)], forall𝑘𝑛 if an impulsive controller gain is chosen at time 𝑡+𝑇(𝑡) by replacing 𝑡𝑡+𝑇(𝑡) in (3.3) and Imp[0,𝑡+𝑇(𝑡)]=Imp[0,𝑡+𝑇(𝑡)){𝑡+𝑇(𝑡)} with Imp[0,𝑡+𝑇(𝑡))=Imp[0,𝑡]. It has been proven that 𝑥𝑘(𝜏)[𝐾1,𝐾2], forall𝜏[0,𝑡) for any given 𝑡𝐑0+, forall𝑘𝑛 then 𝑥𝑘(𝜏)[𝐾1,𝐾2], forall𝜏[0,𝑡+𝑇(𝑡)], for some 𝑇(𝑡)𝐑+,and for all 𝑘𝑛 so that the result holds by complete induction for forall𝑡𝐑0+ with a bounded sequence of impulsive controller gains at some appropriate sequence of impulsive time instants Imp:={𝑡𝑖𝐑0+}.

Remark 3.3. Note that Theorem 3.2 holds irrespective of the values of the regular controller gain functions 𝐾𝑖𝑗𝐑0+𝐑𝑚×𝑛 for some appropriate sequence of impulsive controller gains 𝐾0𝑗𝐑0+𝐑𝑛×𝑚, forall𝑗𝑁,forall𝑖𝑞{0}. The reason is that the stabilization mechanism consists of decreasing the absolute values of the state components as much as necessary at its right limits at the impulsive time instants for any values of their respective left-hand-side limits and values at previous values at the intervals between consecutive impulsive time instants.

The subsequent result establishes that the stabilization is achievable with the stabilizing impulsive controller gains being chosen arbitrarily except at some subsequence of the impulsive time instants.

Theorem 3.4. The closed-loop system (2.6)–(2.7) is globally stable for any 𝜑BPC(0)([,0],𝐑𝑛) and any given set of regular controller gain functions 𝐾𝑖𝑗𝐑0+𝐑𝑛×𝑚 if the sequence of impulsive time instants Imp={𝑡𝑖𝐑0+} is chosen so that (1)the sequence of impulsive controller gains 𝐾0𝑗𝐑0+𝐑𝑛×𝑚, forall𝑗𝑁;forall𝑖𝑞{0} is chosen appropriately for some subsequence of impulsive time instants Imp={𝑡𝑘}Impsatisfying 𝑡𝑘+1𝑡𝑘𝑇(𝑡𝑘)<, for each two consecutive 𝑡𝑘,𝑡𝑘+1Imp(2)such a sequence of impulsive controller gains is chosen arbitrarily for the sequence ImpImp.

Proof. Consider the following Lyapunov functional candidate 𝑉𝐑0+×𝐑𝑛𝐑0+, [17]: 𝑉𝑡,𝑥𝑡=𝑥𝑇(𝑡)𝑃𝑥(𝑡)+𝑞𝑖=1𝑡𝑡𝑖(𝑡)𝑥𝑇(𝜏)𝑆𝑖(𝜏)𝑥(𝜏)𝑑𝜏,(3.4) where 𝐑𝑛×𝑛𝑃=𝑃𝑇0 and 𝑆𝑖BPC(0)(𝐑0+,𝐑𝑛×𝑛) fulfils 𝑆𝑖(𝑡)0, forall𝑡𝐑0+, forall𝑖𝑞. One gets by taking time-derivatives in (3.4) using (2.6) as follow: ̇𝑉𝑡,𝑥𝑡=2𝑥𝑇(𝑡)𝑃𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝛿(0)+𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗(𝑡)𝐴𝑖𝑗(𝑡)𝑥𝑡𝑖+(𝑡)𝑥(𝑡)𝑞𝑖=1𝑥𝑇(𝑡)𝑆𝑖̇(𝑡)𝑥(𝑡)1𝑖𝑥(𝑡)𝑇𝑡𝑖𝑆(𝑡)𝑖𝑡𝑖𝑥(𝑡)𝑇𝑡𝑖(𝑡)(3.5)=̂𝑥𝑇(𝑡)𝑄(𝑡)̂𝑥(𝑡)=̂𝑥𝑇𝑄(𝑡)𝑑(𝑡)+𝑄𝑜𝑑(𝑡)̂𝑥(𝑡),(3.6) where 𝑥̂𝑥(𝑡)=𝑇(𝑡)𝑥𝑇𝑡1(𝑡)𝑥𝑇𝑡𝑞(𝑡)𝑇,𝑄𝑄(𝑡)=Blockmatrix𝑖𝑗(𝑡)𝑖,𝑗,𝑞+1(3.7) with 𝑄11(𝑡)=𝑁𝑗=1𝜆0𝑗𝐴(𝑡)0𝑗(𝑡)+𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝛿(0)𝑇𝑃+𝑃𝑁𝑗=1𝜆0𝑗𝐴(𝑡)0𝑗(𝑡)+𝐵0𝑗(𝑡)𝐾0𝑗+(𝑡)𝛿(0)𝑞𝑖=1𝑆𝑖𝑄(𝑡)1,𝑖+1(𝑡)=𝑄𝑇𝑖+1,1(𝑡)=𝑁𝑗=1𝜆𝑖𝑗(𝑡)𝑃𝐴𝑖𝑗(𝑡),𝑖𝑄𝑞,𝑖𝑖̇(𝑡)=1𝑖𝑆(𝑡)𝑖𝑡𝑖(𝑡),𝑄𝑖𝑗(𝑡)=0,𝑖,𝑗(𝑖)𝑄𝑞+1{1},𝑑(𝑡)=Blockdiag𝑄11(𝑡)𝑄22(𝑡)𝑄𝑞+1,𝑞+1,𝑄(𝑡)𝑜𝑑𝑄(𝑡)=(𝑡)+𝑄𝑑=(𝑡)0𝑄12(𝑡)𝑄1,𝑞+1(𝑡)𝑄𝑇12(𝑡)0𝑄23(𝑡)𝑄2,𝑞+1(𝑡)𝑄𝑇𝑞+1,1(𝑡)𝑄𝑇𝑞+1,2(𝑡)(𝑡)𝑄𝑇𝑞+1,𝑞,(𝑡)(𝑡)0(3.8) so that the following cases arise:
(1) if 𝑡𝐷,then 𝑄11(𝑡)=𝑁𝑗=1𝜆0𝑗(𝑡)𝐴𝑇0𝑗(𝑡)𝑃+𝑃𝑁𝑗=1𝜆0𝑗(𝑡)𝐴0𝑗+(𝑡)𝑞𝑖=1𝑆𝑖𝑄(𝑡),1,𝑖+1(𝑡)=𝑄𝑇𝑖+1,1(𝑡)=𝑁𝑗=1𝜆𝑖𝑗(𝑡)𝑃𝐴𝑖𝑗(𝑡),𝑖𝑄𝑞,𝑖𝑖(̇𝑡)=1𝑖(𝑆𝑡)𝑖𝑡𝑖(𝑡),𝑄𝑖𝑗(𝑡)=0,𝑖,𝑗(𝑖)𝑞+1{1},(3.9)
(2) if 𝑡𝐷Imp, then (3.8) still holds to the left of any 𝑡𝐑0+. Similar equations as (3.9) stand for 𝑡+ by replacing 𝑡𝑡+ in all the matrix functions entries which become modified only if the time instant 𝑡 is a discontinuity point of the corresponding matrix function entry,
(3) if 𝑡Imp, then the left-hand-side limit of 𝑄(𝑡) is defined with block matrices as follow: 𝑄11(𝑡)=𝑁𝑗=1𝜆0𝑗𝐴(𝑡)0𝑗(𝑡)+𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝛿(0)𝑇𝑃+𝑃𝑁𝑗=1𝜆0𝑗𝐴(𝑡)0𝑗(𝑡)+𝐵0𝑗(𝑡)𝐾0𝑗+(𝑡)𝛿(0)𝑞𝑖=1𝑆𝑖𝑄(𝑡),1,𝑖+1(𝑡)=𝑄𝑇𝑖+1,1(𝑡)=𝑁𝑗=1𝜆𝑖𝑗(𝑡)𝑃𝐴𝑖𝑗(𝑡),𝑖𝑄𝑞,𝑖𝑖̇(𝑡)=1𝑖𝑆(𝑡)𝑖𝑡𝑖(𝑡),𝑄𝑖𝑗(𝑡)=0,𝑖,𝑗(𝑖)𝑞+1{1},(3.10) and the right-hand-side limits are defined with block matrices as follow: 𝑄11𝑡+=𝑁𝑗=1𝜆0𝑗𝐴(𝑡)0𝑗𝑡++𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝑇𝑃+𝑃𝑁𝑗=1𝜆0𝑗𝐴(𝑡)0𝑗𝑡++𝑁𝑗=1𝐵0𝑗(𝑡)𝐾0𝑗+(𝑡)𝑞𝑖=1𝑆𝑖𝑡+𝑄1,𝑖+1𝑡+=𝑄𝑇𝑖+1,1𝑡+=𝑁𝑗=1𝜆𝑖𝑗(𝑡)𝑃𝐴𝑖𝑗𝑡+,𝑖𝑄𝑞,𝑖𝑖𝑡+̇=1𝑖𝑆(𝑡)𝑖𝑡𝑖(𝑡)+,𝑄𝑖𝑗(𝑡)=0,𝑖,𝑗(𝑖)𝑞+1{1},(3.11) since from Assumption 2.1, the scalar functions 𝜆𝑖𝑗(𝑡) and the matrix functions 𝐵0𝑗(𝑡), forall𝑖𝑞{0},forall𝑗𝑁 cannot be discontinuous at the sequence Imp. As in (3.11), a matrix function entry at 𝑡+ is more distinct than its left-hand-side limit at 𝑡 only if it has a discontinuity at the time instant 𝑡. Thus, ̇𝑉𝑡+,𝑥𝑡+̇𝑉𝑡,𝑥𝑡=̂𝑥𝑇𝑄𝑡(𝑡)+𝑡𝑄(𝑡)̂𝑥(𝑡),𝑉+,𝑥𝑡𝑉𝑡,𝑥𝑡̇𝑉𝑡=0,𝑡Imp,+,𝑥𝑡+̇𝑉𝑡,𝑥𝑡𝑡=0,𝑡𝐷since𝑄+=𝑄(𝑡).(3.12) Furthermore, in view of (3.5), ̇𝑉𝑡+,𝑥𝑡+̇𝑉𝑡,𝑥𝑡=̂𝑥𝑇𝑡+𝑄𝑡+𝑡̂𝑥+̂𝑥𝑇(𝑡)𝑄(𝑡)̂𝑥(𝑡),𝑡Imp.(3.13) If, in addition, 𝑡𝐷𝑝, that is, if 𝑡Imp𝐷𝑝, and since 𝑄(𝑡+)=𝑄(𝑡), (3.13) becomes ̇𝑉𝑡+,𝑥𝑡+̇𝑉𝑡,𝑥𝑡=̂𝑥𝑇𝑡+𝑡𝑄(𝑡)̂𝑥+̂𝑥𝑇(𝑡)𝑄(𝑡)̂𝑥(𝑡),(3.14) Furthermore, 𝑉𝑡+,𝑥𝑡+𝑉𝑡,𝑥𝑡=𝑡+𝑡̇𝑉𝜏,𝑥𝜏𝑑𝜏×𝑥𝑇(𝑡)𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝑇𝑃𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)+2𝑃𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝑥(𝑡),𝑡Imp.(3.15) since 𝑥(𝑡+)𝑥(𝑡)=𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝑥(𝑡) from (2.4) (which results to be zero for 𝑡Imp). Now, for any 𝑘𝐙0+and some 𝑝𝑘𝐙+, consider a sequence of consecutive impulsive time instants Imp(𝑡𝑘,𝑡𝑘+𝑝𝑘)={𝑡𝑘,𝑡𝑘+1,,𝑡𝑘+𝑝𝑘}Imp, so that, 𝑉𝑡+𝑘+𝑝𝑘,𝑥𝑡+𝑘𝑘+𝑝𝑡𝑉+𝑘,𝑥𝑡+𝑘=𝑡+𝑘𝑘+𝑝𝑡+𝑘̇𝑉𝜏,𝑥𝜏=𝑑𝜏𝑝𝑘𝑖=1𝑡𝑘+𝑖𝑡+𝑘+𝑖1̇𝑉𝜏,𝑥𝜏𝑑𝜏+2𝑥𝑇𝑡𝑘+𝑖𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖+𝑥𝑇𝑡𝑘+𝑖𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐾𝑇0𝑗𝑡𝑘+𝑖𝐵𝑇0𝑗𝑡𝑘+𝑖×𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖(3.16)𝑝𝑘𝑖=1𝑡𝑘+𝑖𝑡+𝑘+𝑖1||𝛼(𝜏)𝑥𝑇(𝜏)𝑄𝑑(𝜏)||𝑥(𝜏)𝑑𝜏+𝑡𝑘+1𝑡+𝑘+𝑖1||𝛽(𝜏)𝑥𝑇(𝜏)𝑄𝑜𝑑(𝜏)||𝑥(𝜏)𝑑𝜏+𝑥𝑇𝑡𝑘+𝑖𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐾𝑇0𝑗𝑡𝑘+𝑖𝐵𝑇0𝑗𝑡𝑘+𝑖×𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖𝑡2𝜇𝑘+𝑖|||||𝑥𝑇𝑡𝑘+𝑖𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖|||||(3.17) by using the binary indicator functions as follow:(a)𝛼𝐑0+{1,1} defined by 𝛼(𝑡)=1 if 𝑥𝑇(𝑡)𝑄𝑑(𝑡)𝑥(𝑡)>0 and 𝛼(𝑡)=1 otherwise, forall𝑡𝐑0+,(b)𝛽𝐑0+{1,1} defined by 𝛽(𝑡)=1 if 𝑥𝑇(𝑡)𝑄𝑜𝑑(𝑡)𝑥(𝑡)>0 and 𝛽(𝑡)=1 otherwise, forall𝑡𝐑0+,(c)𝜇Imp{1,1} defined by,𝜇(𝑡𝑘)=1 if 𝑥𝑇(𝑡+𝑗)𝑃(𝑁𝑗=1𝜆0𝑗(𝑡𝑗)𝐵0𝑗(𝑡𝑗)𝐾0𝑗(𝑡𝑗))𝑥(𝑡+𝑗)>0 and 𝜇(𝑡𝑘)=1 otherwise; forall𝑡𝑘Imp. Equation (3.17) is less than or equal to zero, which implies that 𝑉(𝑡+𝑘+𝑝𝑘,𝑥𝑡+𝑘𝑘+𝑝)𝑉(𝑡+𝑘,𝑥𝑡+𝑘) if 𝑝𝑘𝑖=1𝑡𝑘+𝑖𝑡+𝑘+𝑖1||𝛼(𝜏)𝑥𝑇(𝜏)𝑄𝑑(𝜏)||𝑥(𝜏)𝑑𝜏+𝑡𝑘+𝑖𝑡+𝑘+𝑖1||𝛽(𝜏)𝑥𝑇(𝜏)𝑄𝑜𝑑(𝜏)||𝑥(𝜏)𝑑𝜏+𝑥𝑇𝑡𝑘+𝑖𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐾𝑇0𝑗𝑡𝑘+𝑖𝐵𝑇0𝑗𝑡𝑘+𝑖×𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖𝑡2𝜇𝑘+𝑖|||||𝑥𝑇𝑡𝑘+1𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖|||||0,(3.18) which holds with an existing Imp𝑡𝑘=𝑡𝑘+𝑝𝑘[𝑡𝑘,𝑡𝑘+𝑝𝑘] for each𝑡𝑘+𝑖Imp(forall𝑖𝑝𝑘{0}) with impulsive control gains 𝐾0𝑗(𝑡𝑘)=Λ0𝑗(𝑡𝑘)𝐵𝑇0𝑗(𝑡𝑘)𝑃 of the jth parameterization of the polytopic system, where 𝐑𝑛×𝑛Λ0𝑗(𝑡𝑘)=Λ𝑇0𝑗(𝑡𝑘), forall𝑗𝑁 if 𝑁𝑗=1𝜆0𝑗𝑡𝑘𝜆maxΛ0𝑗𝑡𝑘𝑃𝐵0𝑗𝑡𝑘2×1𝜆0𝑗𝑡𝑘𝜆2minΛ0𝑗𝑡𝑘𝜆min𝐵𝑇0𝑗𝑡𝑘𝑃2𝐵0𝑗𝑡𝑘𝜆maxΛ0𝑗𝑡𝑘1𝑥𝑡𝑘22𝑘𝑖=1𝑡𝑘+𝑖𝑡+𝑘+𝑖1||𝛼(𝜏)𝑥𝑇(𝜏)𝑄𝑑(𝜏)||𝑥(𝜏)𝑑𝜏+𝑡𝑘+𝑖𝑡+𝑘+𝑖1||𝛽(𝜏)𝑥𝑇(𝜏)𝑄𝑜𝑑(𝜏)||+𝑥(𝜏)𝑑𝜏𝑘1𝑖=1𝑥𝑇𝑡𝑘+𝑖𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐾𝑇0𝑗𝑡𝑘+𝑖𝐵𝑇0𝑗𝑡𝑘+𝑖×𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖|||||𝑥2𝑇𝑡𝑘+𝑖𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝑃𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖|||||,(3.19) where 𝑡𝑘=max𝑖𝑝𝑘(𝑡𝑘+𝑖Imp𝑥𝑇(𝑡𝑘+𝑖)(𝑁𝑗=1𝜆0𝑗(𝑡𝑘+𝑖)𝑃𝐵0𝑗(𝑡𝑘+𝑖)𝐾0𝑗(𝑡𝑘+𝑖))𝑥(𝑡𝑘+𝑖)0)
The existence of 𝑡𝑘[𝑡𝑘,𝑡𝑘+𝑝𝑘] has been proven for time instants 𝑡𝑘+𝑖Imp(forall𝑖𝑝𝑘{0}), and some 𝑝𝑘𝐙0+ such that 𝑥𝑇(𝑡𝑘)(𝑁𝑗=1𝜆0𝑗(𝑡𝑘)𝑃𝐵0𝑗(𝑡𝑘)𝐾0𝑗(𝑡𝑘))𝑥(𝑡𝑘)0 if𝑥(𝑡𝑘)0 for appropriate impulsive controller gains 𝐾0𝑗(𝑡𝑘),forall𝑗𝑁. In particular, if Λ0𝑗(𝑡𝑘)=𝜈(𝑡𝑘)𝐼𝑚0 with 𝜈(𝑡𝑘)𝐑{0} being a scalar common for the impulses injected at all the parameterizations of the polytopic system, then the condition in (3.19) becomes in particular,𝜈𝑡𝑘1𝜌𝑡𝑘𝑥𝑡𝑘22×𝑘𝑖=1𝑡𝑘+𝑖𝑡+𝑘+𝑖1||𝛼(𝜏)𝑥𝑇(𝜏)𝑄𝑑(𝜏)||𝑥(𝜏)𝑑𝜏+𝑡𝑘+𝑖𝑡+𝑘+𝑖1||𝛽(𝜏)𝑥𝑇(𝜏)𝑄𝑜𝑑(𝜏)||+𝑥(𝜏)𝑑𝜏𝑘1𝑖=1𝑥𝑇𝑡𝑘+𝑖𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐾𝑇0𝑗𝑡𝑘+𝑖𝐵𝑇0𝑗𝑡𝑘+𝑖×𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖|||||𝑥2𝑇𝑡𝑘+𝑖𝑁𝑗=1𝜆0𝑗𝑡𝑘+𝑖𝑃𝐵0𝑗𝑡𝑘+𝑖𝐾0𝑗𝑡𝑘+𝑖𝑥𝑡𝑘+𝑖|||||,𝜌𝑡𝑘:=𝑁𝑗=1𝜆0𝑗𝑡𝑘𝜆maxΛ0𝑗𝑡𝑘𝑃𝐵0𝑗𝑡𝑘2×1𝜆0𝑗𝑡𝑘𝜆2minΛ0𝑗𝑡𝑘𝜆min𝐵𝑇0𝑗𝑡𝑘𝑃2𝐵0𝑗𝑡𝑘𝜆maxΛ0𝑗𝑡𝑘.(3.21) It follows by simple inspection that 𝜈(𝑡𝑘) may be chosen to satisfy (3.21) and, furthermore, 𝜈(𝑡𝑘) for some 𝑡𝑘Imp[𝑡𝑘,𝑡𝑘+𝑝𝑘]. It is now proven by contradiction that the sequences {𝑥(𝑡𝑘)𝑡𝑘Imp}and {𝑥(𝑡+𝑘)𝑡𝑘Imp} are both bounded. Assume that 𝑆𝜈={𝜈(𝑡𝑘)}𝑡𝑘Imp[𝑡𝑘,𝑡𝑘𝑘+𝑝] is an unbounded sequence. Then, there is an infinite subsequence 𝑆𝜈𝑆𝜈 such that 𝑆𝜈𝜈(𝑡𝑘)± as 𝑡𝑘, forall𝑡𝑘Imp. From the definition of the Lyapunov function candidate (3.4) and the guaranteed property 𝑉(𝑡+𝑘,𝑥𝑡+𝑘)𝑉(𝑡+𝑘,𝑥𝑡+𝑘)𝑉(𝑡+1,𝑥𝑡+1)<, (from (3.17), if (3.21) holds), it follows that 𝑥(𝑡+𝑘)𝑀+𝜑𝑘< for any positive finite constant 𝑀𝜑 depending on the bounded function of initial conditions of the system (3.4). Also, 𝑥(𝑡𝑘)𝑀𝜑𝑘< since the discontinuities at the state trajectory solution caused by impulses are second-class finite jump-type discontinuities. Then, the sequences {𝑥(𝑡𝑘)}𝑡𝑘Impand {𝑥(𝑡𝑘+)}𝑡𝑘Imp are bounded by positive real constants, 𝑀𝜑=max𝑡𝑘Imp(max𝑡𝑘[𝑡𝑘,𝑡𝑘𝑘+𝑝]𝑀𝜑𝑘) and 𝑀+𝜑=max𝑡𝑘Imp(max𝑡𝑘[𝑡𝑘,𝑡𝑘𝑘+𝑝]𝑀+𝜑𝑘), respectively. This implies that (3.21) may be fulfiled with <𝜈(𝑡𝑘)<, also, since (1)the state-trajectory solution of the closed-loop system is continuous and almost everywhere time differentiable except at second-class discontinuity points on a set of zero measure, and(2)the state-trajectory solution of the closed-loop system is bounded on the subsequence Imp. Thus, it cannot beunbounded on ImpImp since, otherwise, it could not be an almost everywhere smooth state-trajectory solution.As a result, it exist 𝐶=𝐶(𝑇,Imp)𝐑+ and 𝐶+=𝐶+(𝑇,Imp)𝐑+ such that 𝑥(𝑡𝑘)𝐶𝑀𝜑 and 𝑥(𝑡+𝑘)𝐶+𝑀+𝜑, forall𝑡𝑘Imp and the candidate (3.4) is a Lyapunov functional. The result has been proven.

The proof of the global asymptotic stability of the system requires to extend Theorem 3.4 by guaranteeing that the state-trajectory solution converges asymptotically to zero as time tends to infinity. This requires also stabilizability-type conditions on the nonimpulsive part of the closed-loop solution. The following result holds.

Theorem 3.5. The closed-loop system (2.6)–(2.7) is globally asymptotically stable for any 𝜑BPC(0)([,0],𝐑𝑛) and a given sequence of impulsive time instants if the regular controller gain functions 𝐾𝑖𝑗𝐑0+𝐑𝑛×𝑚 and the sequence of impulsive controller gains 𝐾0𝑗𝐑0+𝐑𝑛×𝑚, forall𝑗𝑁,forall𝑖𝑞{0} are chosen so that the following matrix inequalities hold for some 𝐑𝑛×𝑛𝑃=𝑃𝑇0 and 𝑆𝑖BPC(0)(𝐑0+,𝐑𝑛×𝑛) which fulfils 𝑆𝑖(𝑡)0, forall𝑡𝐑0+, forall𝑖𝑞 as follow: 𝑄11(𝑡)0,𝑄22(𝑡)𝑄𝑇12(𝑡)𝑄111(𝑡)𝑄𝑇12(𝑡)0,𝑡𝐑0+𝑄D,(3.22)11𝑡+0,𝑄22𝑡+𝑄𝑇12𝑡+𝑄111𝑡+𝑄𝑇12𝑡+𝑄0,𝑡𝐷Imp,11𝑡+0,𝑄22𝑡+𝑄𝑇12𝑡+𝑄111(𝑡+)𝑄𝑇12𝑡+𝑄𝑡0,𝑡𝐷Imp,(3.23)+𝑄(𝑡)0,𝑡Imp,(3.24) where 𝑄12(𝑡)=𝑄𝑇21(𝑡)=𝑁𝑗=1𝜆1𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆2𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆𝑞𝑗(𝑡)𝑃𝐴1𝑗,(𝑡)(3.25)𝑄22̇(𝑡):=Blockdiag11𝑆(𝑡)11𝑡1̇(𝑡)12(𝑡)×𝑆22𝑡2̇(𝑡)1𝑞𝑆(𝑡)𝑞𝑞𝑡𝑞.(𝑡)(3.26)

Proof. From (3.6) and (3.12), the system is globally asymptotically stable if the Lyapunov functional candidate (3.4) is in fact a Lyapunov functional which is guaranteed if(a)̇𝑉(𝑡,𝑥𝑡)<0, forall𝑡𝐑0+ such that 𝑥𝑡0 what holds if and only if 𝑄(𝑡)0, forall𝑡𝐑0+(b)𝑉(𝑡+,𝑥𝑡+)𝑉(𝑡,𝑥𝑡), forall𝑡Imp what holds if and only if 𝑄(𝑡+)𝑄(𝑡), forall𝑡𝐑0+.The first condition holds from (3.9) via Schur’s complement if (3.22)-(3.23) hold. The second condition holds if (3.24) holds.

Remark 3.6. Theorem 3.5 can be tested directly from (3.9)–(3.11) with direct algebraic tests. However, it is very restrictive since it does not provide with conditions guaranteeing a cooperative achievement of global asymptotic stability among the non-impulsive and impulsive parts. Note that necessary conditions for the fulfilment of Theorem 3.5 are from (3.9)–(3.11): 𝑄11(𝑡)0, 𝑄11(𝑡+)0 (i.e., the Lyapunov matrix inequality holds for forall𝑡𝐑0+𝐷, and for the left and right limits of all 𝑡𝐷), and 𝑄11(𝑡+)𝑄11(𝑡)0, forall𝑡Imp.

Remark 3.7. Note that (3.22)-(3.23) imply that 𝑄22(𝑡)𝑄𝑇12(𝑡)𝑄111(𝑡)𝑄𝑇12(𝑡)0,𝑡𝐑0+𝐷,(3.27)𝑄22(𝑡)𝑄𝑇12(𝑡)𝑄111(𝑡)𝑄𝑇12(𝑡)0,𝑄22𝑡+𝑄𝑇12𝑡+𝑄111𝑡+𝑄𝑇12𝑡+0,(3.28)forall𝑡𝐷Imp since 𝑄𝑇12(𝑡)𝑄111(𝑡)𝑄𝑇12(𝑡) is symmetric and𝑄111(𝑡)0and 𝑄22(𝑡)𝑄𝑇12(𝑡)𝑄111(𝑡)𝑄𝑇12(𝑡)0,𝑄22𝑡+𝑄𝑇12𝑡+𝑄111𝑡+𝑄𝑇12𝑡+0,𝑡𝐷Imp,(3.29) As a result, sup𝑡𝐑+0[max𝑖𝑞̇(max(𝑖̇(𝑡),𝑖(𝑡+)))]<1is a necessary condition for Theorem 3.5 to hold.

Concerning Theorem 3.5, (3.22)-(3.23), note that isolated bounded discontinuities in ̇𝑉(𝑡,𝑥𝑡) do not affect to maintain 𝑉(𝑡,𝑥𝑡) as a positive strictly monotonically decreasing functional on 𝐑0+. Therefore, Theorem 3.5 can be relaxed by removing a set of zero measure of 𝐑0+𝐷(and then of 𝐑0+) to evaluate (3.22)-(3.23) and also bounded discontinuities at the sequence Imp from (3.24). The resulting modified stability result follows.

Corollary 3.8. The closed-loop system (2.6)–(2.7) is globally asymptotically stable for any 𝜑BPC(0)([,0],𝐑𝑛) and a given sequence of impulsive time instants if the regular controller gain functions 𝐾𝑖𝑗𝐑0+𝐑𝑛×𝑚 and the sequence of impulsive controller gains 𝐾0𝑗𝐑0+𝐑𝑛×𝑚, forall𝑗𝑁,forall𝑖𝑞{0} are chosen so that the following matrix inequalities hold for some 𝐑𝑛×𝑛𝑃=𝑃𝑇0 and 𝑆𝑖BPC(0)(𝐑0+,𝐑𝑛×𝑛) which fulfils 𝑆𝑖(𝑡)0, forall𝑡𝐑0+, forall𝑖𝑞 as follow: 𝑁𝑗=1𝜆0𝑗(𝑡)𝐴𝑇0𝑗(𝑡)𝑃+𝑃𝑁𝑗=1𝜆0𝑗(𝑡)𝐴0𝑗+(𝑡)𝑞𝑖=1𝑆𝑖(𝑡)0,(3.30) almost everywhere in 𝐑0+, ̇Blockdiag11𝑆(𝑡)11𝑡1̇(𝑡)12(𝑡)×𝑆22𝑡2(̇𝑡)1𝑞(𝑆𝑡)𝑞𝑞𝑡𝑞(𝑡)𝑁𝑗=1𝜆1𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆2𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆𝑞𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑇×𝑁𝐽=1𝜆0𝑗(𝑡)𝐴𝑇0𝑗(𝑡)𝑃𝑃𝑁𝐽=1𝜆0𝑗(𝑡)𝐴0𝑗(𝑡)𝑞𝑖=1𝑆𝑖(𝑡)1×𝑁𝑗=1𝜆1𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆2𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆𝑞𝑗(𝑡)𝑃𝐴1𝑗,(𝑡)(3.31) almost everywhere in𝐑0+, and 𝑄𝑡+=𝑄(𝑡)𝑁𝑗=1𝜆0𝑗(𝑡)𝐾𝑇0𝑗(𝑡)𝐵𝑇0𝑗(𝑡)𝑃+𝑃𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗0(𝑡)000,𝑡Imp,(3.32) where 𝑄𝑖𝑗(𝑡+)=𝑄𝑖𝑗(𝑡) if 𝑄𝑖𝑗(𝑡) is not impulsive and 𝑄𝑖𝑗(𝑡+)=𝑄𝑖𝑗(𝑡+), otherwise.

Proof. Equations (3.30)-(3.31) follow from Theorem 3.5 by expanding 𝑄11(𝑡)0,𝑄22(𝑡)𝑄𝑇12(𝑡)𝑄111(𝑡)𝑄𝑇12(𝑡)0 from (3.8)-(3.9) and (3.25)-(3.26) on 𝐑0+excepting time instants of bounded isolated discontinuities. Equation (3.32) follow from (3.24), forall𝑡Imp also excluding bounded discontinuities at the time-derivative of the Lyapunov functional since they are irrelevant for analysis since they do not generate bounded jumps at the Lyapunov functional.

Corollary 3.8 holds in terms of more restrictive but it is easier to test conditions given in the subsequent result.

Corollary 3.9. Corollary 3.8 holds if 𝑁𝑗=1𝜆0𝑗(𝑡)𝐴𝑇0𝑗(𝑡)𝑃+𝑃𝑁𝑗=1𝜆0𝑗(𝑡)𝐴0𝑗+(𝑡)𝑞𝑖=1𝑆𝑖(𝑡)𝑞(𝑡)𝐼𝑛,(3.33) almost everywhere in 𝐑0+ for some 𝑞BPC(0)(𝐑0+,𝐑+) which satisfies 𝑞𝑞(𝑡)>min0,𝑁𝑗=1𝜆1𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆2𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆𝑞𝑗(𝑡)𝑃𝐴1𝑗(𝑡)22min𝑖𝑞𝜆min𝑆𝑖𝑖𝑡𝑖,(𝑡)(3.34) provided that max𝑖𝑞̇𝑖(𝑡)<min𝛾,1𝑁𝑗=1𝜆1𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆2𝑗(𝑡)𝑃𝐴1𝑗(𝑡)𝑁𝑗=1𝜆𝑞𝑗(𝑡)𝑃𝐴1𝑗(𝑡)22𝑞(𝑡)min𝑖𝑞𝜆min𝑆𝑖𝑖𝑡𝑖,(𝑡)(3.35) almost everywhere in 𝐑0+, and (3.32) holds forall𝑡Imp.

The following result states that stabilization is achievable under impulsive control impulses which respect a maximum separation time interval and exceed an upper bound of the maximum delay provided that it is bounded.

Corollary 3.10. Assume that (1)all the delays are uniformly bounded for all time,(2)¬𝑡𝐑0+𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)0forall𝑗𝑁 and fix a real constant >𝑇𝑇(sup𝑡𝐑0+(𝑡)). Fix a real constant >𝑇𝑇(sup𝑡𝐑0+(𝑡)). Thus, there is always a globally stabilizing impulsive control law by appropriate design of one of the impulsive controller gains and choice of the interval sequences of impulsive instants as follow:𝐾0𝐑0+𝐑𝑚×𝑛,]𝑁,Imp(𝑗𝑇,(𝑗+1)𝑇(3.36) for each time interval (𝑗𝑇,(𝑗+1)𝑇], forallj(j0)𝐙0+ and some given arbitrary finite 𝑗0𝐙0+.

Proof. One has from (3.4) that Δ𝑉𝑡,𝑥𝑡𝑡=𝑉+,𝑥𝑡+𝑉𝑡,𝑥𝑡=𝑥𝑇𝑡+𝑡𝑃𝑥+𝑥𝑇(𝑡)𝑃𝑥(𝑡),𝑡𝐑0+,(3.37) which equalizes zero at 𝑡Imp, since 𝑞𝑖=1𝑡+𝑡𝑖(𝑡)+𝑥𝑇(𝜏)𝑆𝑖(𝜏)𝑥(𝜏)𝑑𝜏=𝑞𝑖=1𝑡𝑡𝑖(𝑡)𝑥𝑇(𝜏)𝑆𝑖(𝜏)𝑥(𝜏)𝑑𝜏,𝑡𝐑0+,(3.38) since the discontinuities of the state vector at 𝑡Imp are bounded. Thus, one has for any arbitrary 𝑇𝐑+that 𝑉𝑡+𝑡+𝑇𝑉+𝑡𝑡+𝑇̂𝑥𝑇+(𝜏)𝑄(𝜏)̂𝑥(𝜏)𝑑𝜏𝑡𝑖Imp](𝑡,𝑡+𝑇𝑥𝑇𝑡+𝑖𝑡𝑃𝑥+𝑖𝑥𝑇𝑡𝑖𝑡𝑃𝑥𝑖𝑡𝑡+𝑇̂𝑥𝑇+(𝜏)𝑄(𝜏)̂𝑥(𝜏)𝑑𝜏𝑡𝑖Imp](𝑡,𝑡+𝑇𝑥𝑇𝑡𝑖𝐼𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐾𝑇0𝑗𝑡𝑖𝐵0𝑗𝑡𝑖𝐼×𝑃𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵0𝑗𝑡𝑖𝐾0𝑗𝑡𝑖𝑥𝑡𝑃𝑖,𝑡𝐑𝟎+.(3.39) Define 𝑡=𝑡𝑡(𝑡,𝑇)=𝑖]𝑡Imp(𝑡,𝑡+𝑇𝑥𝑡0Imp𝑡,𝑡+𝑇𝑥𝑖=0,𝑡𝑖𝑡Imp],𝑡+𝑇(𝑡,𝑡+𝑇𝐑0+(3.40) as the last impulsive sampling instant in (𝑡,𝑡+𝑇], where the state vector is nonzero. Thus, 𝑉(𝑡++𝑇)𝑉(𝑡+) if 𝑥𝑇𝑡𝐼𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝐾𝑇0𝑗𝑡𝐵𝑇0𝑗𝑡𝐼×𝑃𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝐵0𝑗𝑡𝐾0𝑗𝑡𝑥𝑡𝑃𝑡𝑖+𝑇̂𝑥𝑇(𝜏)𝑄(𝜏)̂𝑥(𝜏)𝑑𝜏𝑡𝑖Imp(𝑡,𝑡](𝑡,𝑇)𝑥𝑇𝑡𝑖𝐼𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵𝑇0𝑗𝑡𝑖𝐼×𝑃𝑛+𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵0𝑗𝑡𝑖𝐾0𝑗𝑡𝑖𝑥𝑡𝑃𝑖(3.41) from (3.6). Since the interval (𝑡,𝑡+𝑇) is finite, it follows that the Lyapunov functional candidate is bounded on the interval, provided that it is bounded at a single point. The result follows by applying the above upper-bounding constraint recursively for 𝑡=𝑗𝑇,forall𝑗𝑗0and appropriate choice of the impulsive sequence Imp(𝑗𝑇,(𝑗+1)𝑇]since the state vector cannot be identically zero on (𝑗𝑇,(𝑗+1)𝑇] for >𝑇𝑇(sup𝑡𝐑0+(𝑡))except for the trivial state-trajectory solution.

Remark 3.11. Corollary 3.10 may be directly reformulated under weaker (but easier to deal with) conditions by using ̇𝑉𝑡,𝑥𝑡̂𝑥𝑇(𝑡)𝑄(𝑡)̂𝑥(𝑡)=̂𝑥𝑇𝑄(𝑡)𝑑(𝑡)+𝑄𝑜𝑑𝜆(𝑡)̂𝑥(𝑡)min𝑄𝑑(𝑡)𝜆max𝑄𝑇0𝑑(𝑡)𝑄0𝑑(𝑡)̂𝑥(𝑡)22,(3.42)Δ𝑉𝑡,𝑥𝑡𝑡:=𝑉+,𝑥𝑡+𝑉𝑡,𝑥𝑡=𝑥𝑇(𝑡)𝑁𝑗=1𝜆0𝑗(𝑡)𝐾𝑇0𝑗(𝑡)𝐵𝑇0𝑗𝑃(𝑡)𝑁𝑗=1𝜆0𝑗(𝑡)𝐵0𝑗(𝑡)𝐾0𝑗(𝑡)+2𝑁𝑗=1𝜆0𝑗(𝑡)𝐾𝑇0𝑗(𝑡)𝐵𝑇0𝑗𝑃(𝑡)𝑥(𝑡).(3.43)

4. Examples

4.1. Example for Scalar Systems

̇𝑥(𝑡)=𝑎𝑥(𝑡)+𝑎0(𝑡)𝑥(𝑡)+𝑡𝑘Imp(0,𝑡)𝐾(𝑡𝑘)𝑥(𝑡𝑘)𝛿(𝑡𝑡𝑘)for some constant delay 0. Its solution satisfies for 𝑇𝑘=𝑡𝑘+1𝑡𝑘, forall𝜃[0,𝑇𝑘] with 𝑈(𝑡) being the unit step (Heaviside) function,𝑥𝑡+𝑘+𝜃=𝑒𝑎𝜃𝑥𝑡+𝑘+𝜃0𝑒𝑎𝜏𝑎0𝑡𝑘𝑥𝑡+𝜏𝑘𝑡+𝜏𝑑𝜏+𝐾𝑘+1𝑈𝜃𝑇𝑘𝑥𝑡𝑘+1×sup𝑡𝜏𝑘𝑡,max𝑘+1,𝑡𝑘||||||𝑡𝑥(𝜏)1+𝐾𝑘+1𝑈𝜃𝑇𝑘||||||𝑒𝑎𝜃𝑥𝑡+𝑘+𝜃0𝑒𝑎𝜏𝑎0𝑡𝑘𝑥𝑡+𝜏𝑘||||,+𝜏𝑑𝜏𝜃0,𝑇𝑘sup𝑡𝜃𝑘,𝑡𝑘+1||||𝑥(𝜏)max𝜃0,𝑇𝑘||𝑡1+𝐾𝑘+1𝑈𝜃𝑇𝑘||max𝜃0,𝑇𝑘|||||𝑒𝑎𝜃||𝑥𝑡+𝑘||+||||𝑒𝑎𝜃1𝑎||||×max𝜏0,𝑇𝑘||𝑎0𝑡𝑘||+𝜏sup𝑡𝜏𝑘𝑡,max𝑘+1,𝑡𝑘|||||||||𝑥(𝜏),𝜃0,𝑇𝑘sup𝑡𝜏𝑘,𝑡𝑘+1||||𝑥(𝜏)max1,max𝜃0,𝑇𝑘||𝑡1+𝐾𝑘+1𝑈𝜃𝑇𝑘||×max𝜃0,𝑇𝑘𝑒𝑎𝜃||𝑥𝑡+𝑘||+||||𝑒𝑎𝜃1𝑎||||max𝜏0,𝑇𝑘||𝑎0𝑡𝑘||+𝜏×maxsup𝑡𝜏𝑘,𝑡𝑘+1||||𝑥(𝜏),sup𝑡𝜏𝑘+1,𝑡𝑘||||𝑈𝑡𝑥(𝜏)𝑘𝑡𝑘+1.(4.1)

Note that ||𝑥𝑡𝑘+1||𝑡𝐶𝑘+1𝑡sup𝜏𝑘𝑡,max𝑘+1,𝑡𝑘||||,||𝑥𝑡𝑥(𝜏)+𝑘+1||𝑡𝐶+𝑘+1𝑡sup𝜏𝑘𝑡,max𝑘+1,𝑡𝑘||||,𝑥(𝜏)(4.2) with𝐶𝑡+𝑘+1=||𝑡1+𝐾𝑘+1||𝐶𝑡𝑘+1𝑡,𝐶𝑘+1=𝑒𝑎𝑇𝑘+||||𝑒𝑎𝑇𝑘1𝑎||||max𝜏0,𝑇𝑘||𝑎0𝑡𝑘||+𝜏,(4.3) and also||𝑥𝑡𝑘+1||+𝜃𝐶𝜃𝑡𝑘+1sup𝑡𝜏𝑘𝑡,max𝑘+1,𝑡𝑘||||,||𝑥𝑡𝑥(𝜏)+𝑘+1||+𝜃𝐶𝜃𝑡+𝑘+1sup𝑡𝜏𝑘𝑡,max𝑘+1,𝑡𝑘||||,𝑥(𝜏)(4.4) for all θ [0,𝑇𝑘+1], so that ||𝑥𝑡𝑘+1||+𝜃max𝑖𝑝𝐶𝜃𝑡𝑘+𝑖sup𝑡𝜏𝑘𝑡,max𝑘+𝑝𝑖=1𝑇𝑘+𝑖,𝑡𝑘||||||𝑥𝑡𝑥(𝜏)+𝑘+1||+𝜃max𝑖𝑝𝐶𝜃𝑡+𝑘+𝑖sup𝑡𝜏𝑘𝑡,max𝑘+𝑝𝑖=1𝑇𝑘+𝑖,𝑡𝑘||||𝑥(𝜏)(4.5)forall𝜃[0,𝑝𝑖=1𝑇𝑘+𝑖] and any finite 𝑝𝐙+. Thus, thereexistΩ𝜃(𝑡𝑘+1,𝑡𝑘)[1,)𝐑+, which might be computed with direct simple calculations via (4.3), which equalizes max𝑖𝑝𝑘+1(𝐶𝜃(𝑡+𝑘+𝑖)) with 𝑝𝑘+1being a positive integer accounting for a subsequence of consecutive impulsive time instants{𝑡𝑘+𝑖𝑖𝑝𝑘+1}. Thus, it follows from (4.5) that maxsup𝑡𝜏𝑘,𝑡𝑘+1||||𝑥(𝜏),sup𝑡𝜏𝑘+1,𝑡𝑘||||𝑈𝑡𝑥(𝜏)𝑘𝑡𝑘+1Ω𝜃𝑡𝑘+1,𝑡𝑘sup𝑡𝜏𝑘,𝑡𝑘+1||||.𝑥(𝜏)(4.6) It follows directly from (4.6) into (4.1) and complete induction that if max𝜃0,𝑡𝑘+1𝑡𝑘||𝑡1+𝐾𝑘+1𝑈𝜃𝑇𝑘||max𝜃0,𝑡𝑘+1𝑡𝑘𝑒𝑎𝜃+||||𝑒𝑎𝜃1𝑎||||max𝜏0,𝑡𝑘+1𝑡𝑘||𝑎0𝑡𝑘||Ω+𝜏𝜃𝑡𝑘+1,𝑡𝑘1,(4.7)forall𝑡𝑘Imp(𝑡0,) for some finite 𝑡0𝐑0+then the system is globally uniformly stable for any admissible function of initial conditions 𝜑BPC(0)([,0],𝐑) withsup𝑡𝐑0+||||𝑥(𝑡)sup𝑡,𝑡0,||||𝑥(𝑡)𝐾𝑥<,(4.8) with 𝑥(𝑡)=𝜑(𝑡),forall𝑡[,0]. If the inequality in (4.7) is strict, then the system is globally asymptotically stable for any 𝜑BPC(0)([,0],𝐑).

Note that if, furthermore, 𝑡𝑘+1>𝑡𝑘+, forall𝑡𝑘,𝑡𝑘+1Imp, then Ω𝜃(𝑡𝑘+1,𝑡𝑘)=1,forall𝑡𝑘,𝑡𝑘+1Imp so that (4.7) holds if the subsequent constraints hold for some real constant 𝛾(0,1]𝐑0+ as follow:max𝜃0,𝑡𝑘+1𝑡𝑘𝑒𝑎𝜃+||||𝑒𝑎𝜃1𝑎||||max𝜏0,𝑡𝑘+1𝑡𝑘||𝑎0𝑡𝑘||+𝜏𝛾,max𝜃0,𝑡𝑘+1𝑡𝑘||𝑡1+𝐾𝑘+1𝑈𝜃𝑇𝑘||𝛾1,(4.9) which may be fulfiled without requiring neither 𝑎0 (global stability of the auxiliary system with no delayed dynamics) nor 𝑎+|𝑎0(𝑡)|0(global stability independent of the delay size) by using appropriate impulses of appropriate signs so that the above inequalities hold. A similar consideration applies for global asymptotic stability one of the inequalities in (4.9) being well posed and strict without requiring neither 𝑎<0(global asymptotic stability of the auxiliary system with no delayed dynamics) nor 𝑎+|𝑎0(𝑡)|<0 (global asymptotic stability independent of the delay size). Note also that these above results are particular results of Theorem 3.1 for a scalar system (2.1)-(2.4) with a single parameterization with the non-impulsive controller being identically zero and the control parameter b being unity. If the scalar dynamic system is of polytopic type 3d bẏ𝑥(𝑡)=𝑁𝑗=1𝜆0𝑗𝑎(𝑡)0𝑗(𝑡)𝑥(𝑡)+𝑡𝑘Imp(0,𝑡)𝐾0𝑗𝑡𝑘𝑥𝑡𝑘𝛿𝑡𝑡𝑘+𝑞𝑁𝑖=1𝑗=1𝜆𝑖𝑗(𝑡)𝑎𝑖𝑗(𝑡)𝑥𝑡𝑖(𝑡)=𝑎𝑥(𝑡)+𝑁𝑗=1𝑡𝑘Imp(0,𝑡)𝜆0𝑗𝑡𝑘𝐾0𝑗𝑡𝑘𝑥𝑡𝑘𝛿𝑡𝑡𝑘+𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗(𝑡)𝑎𝑖𝑗(𝑡)𝑥𝑡𝑖,(𝑡)(4.10) provided that 𝑁𝑗=1𝜆0𝑗(𝑡)=1, 𝜆0𝑗(𝑡)𝐑0+, 𝑎0𝑗(𝑡)=𝑎0𝑗(𝑡)𝑎, 𝑎𝑖𝑗(𝑡)=𝑎𝑖𝑗(𝑡), forall𝑖𝑞,forall𝑗𝑁,forall𝑡𝐑0+ and any arbitrary constant 𝑎𝐑 so that,𝑥𝑡+𝑘+𝜃=𝑒𝑎𝜃𝑥𝑡+𝑘+𝜃0𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗𝑡𝑘𝑒+𝜏𝑎𝜏𝑎𝑖𝑗𝑡𝑘𝑥𝑡+𝜏𝑘+𝜏𝑖+(𝜏)𝑑𝜏𝑁𝑗=1𝜆0𝑗𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝑈𝜃𝑇𝑘𝑥𝑡𝑘+1,𝜃0,𝑇𝑘,(4.11)

Thus, the first inequality of (4.1) becomes,sup𝑡𝜃𝑘,𝑡𝑘+1||||𝑥(𝜏)max𝜃0,𝑇𝑘|||||1+𝑁𝑗=1𝜆0𝑗𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝑈𝜃𝑇𝑘|||||×max𝜃0,𝑇𝑘|||||𝑒𝑎𝜃||𝑥𝑡+𝑘||+||||𝑒𝑎𝜃1𝑎||||max𝜏0,𝑇𝑘|||||𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗𝑡𝑘+𝜏𝑎𝑖𝑗𝑡𝑘|||||×+𝜏sup𝑡𝜏𝑘𝑡(𝑡),max𝑘+1(𝑡),𝑡𝑘||||||||||,𝑥(𝜏)(4.12)forall𝜃[0,𝑇𝑘], where (𝑡)=max𝑖𝑞sup(𝑖(𝑡)). Thus, (4.7) is modified as follows.max𝜃0,𝑡𝑘+1𝑡𝑘|||||1+𝑁𝑗=1𝜆0𝑗𝑡𝑘+1𝐾0𝑗𝑡𝑘+1𝑈𝜃𝑇𝑘|||||×max𝜃0,𝑡𝑘+1𝑡𝑘𝑒𝑎𝜃+||||𝑒𝑎𝜃1𝑎||||max𝜏0,𝑡𝑘+1𝑡𝑘|||||𝑞𝑁𝑖=0𝑗=1𝜆𝑖𝑗𝑡𝑘+𝜏𝑎𝑖𝑗𝑡𝑘|||||+𝜏×Ω𝜃𝑡𝑘+1,𝑡𝑘1,(4.13) which guarantees global stability from Theorem 3.1 and if the above inequality is strict, then global asymptotic stability is guaranteed.

Example 4.1. This example refers to the stability of the impulsive closed-loop system (2.8), subject to (2.7) and (2.9), by application of Corollary 3.10 to Theorems 3.4-3.5 and Remark 3.11. Assume that the non impulsive controller gains𝐾𝑖𝑗(𝑡)are identically zero for all time so that𝐴𝑖𝑗(𝑡)=𝐴𝑖𝑗(𝑡), forall𝑖𝑞{0},forall𝑗𝑁and (3.7)–(3.12) are stated for this particular case. Then, the system is controlled by the impulsive controller gains which are nonzero only at set of zero measure defined by all the sequence of impulsive time instants. Note from Remark 3.11 that Δ𝑉(𝑡,𝑥𝑡)=0if 𝑡Imp. Note also that if there only one Imp𝑡𝑖(𝑡,𝑡+𝑇] at which 𝑥(𝑡𝑖)0 so that for the controller gain choice 𝐾0𝑗(𝑡𝑖)=𝜈0(𝑡𝑖)𝐼𝑛 then 𝑉𝑡++𝑇,𝑥𝑡+𝑉𝑡,𝑥𝑡𝑡𝑡+𝑇+𝜆min𝑄𝑑(𝜏)𝜆max𝑄𝑇0𝑑(𝜏)𝑄0𝑑(𝜏)̂𝑥(𝜏)22+𝜆𝑑𝜏min𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐾𝑇0𝑗𝑡𝑖𝐵𝑇0𝑗𝑡𝑖𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵0𝑗𝑡𝑖𝐾0𝑗𝑡𝑖2𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐾𝑇0𝑗𝑡𝑖𝐵𝑇0𝑗𝑡𝑖𝑃2𝑥𝑡𝑖22𝑡𝑡+𝑇+𝜆max𝑄𝑇0𝑑(𝜏)𝑄0𝑑𝜆(𝜏)min𝑄𝑑(𝜏)̂𝑥(𝜏)22+𝜆𝑑𝜏min𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵𝑇0𝑗𝑡𝑖𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵0𝑗𝑡𝑖𝜈0𝑡𝑖2𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵𝑇0𝑗𝑡𝑖𝑃2𝜈0𝑡𝑖𝑥𝑡𝑖220(4.14) if 𝜈0𝑡𝑖𝑏𝑡0,𝑖+𝑏2𝑡𝑖𝑡+4𝑎𝑖𝑐𝑡𝑖𝑡2𝑎𝑖,𝜆min𝑄𝑑(𝑡)𝜆max𝑄𝑇0𝑑(𝑡)𝑄0𝑑(𝑡),𝑡𝐑0+,(4.15) where 𝑎𝑡𝑖=𝜆min𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵𝑇0𝑗𝑡𝑖𝑃𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵0𝑗𝑡𝑖𝑥𝑡𝑖22,𝑏𝑡𝑖=2𝑁𝑗=1𝜆0𝑗𝑡𝑖𝐵𝑇0𝑗𝑡𝑖𝑃2𝑥𝑡𝑖22,𝑐𝑡𝑖=𝑡𝑡+𝑇+𝜆min𝑄𝑑(𝜏)𝜆max𝑄𝑇0𝑑(𝜏)𝑄0𝑑(𝜏)̂𝑥(𝜏)22𝑑𝜏,(4.16) which can always be fulfilled with 𝜈0𝑖(𝑡𝑖)=0(i.e., zero impulsive controller of the given class of impulsive controllers) since the right-hand equation (4.16) holds, which is a condition of global stability of the impulse-free system. If (4.16) is replaced with 𝜈0𝑡𝑖𝑏𝑡0,𝑖+𝑏2𝑡𝑖𝑡4𝑎𝑖𝑐𝑡𝑖𝑡2𝑎𝑖,𝜆min𝑄𝑑>(𝑡)𝜆max𝑄𝑇0𝑑(𝑡)𝑄0𝑑,(𝑡)𝑡𝐑0+,(4.17) then global asymptotic stability is guaranteed. However, assume that 𝜆min(𝑄𝑑(𝑡))<𝜆max(𝑄𝑇0𝑑(𝑡)𝑄0𝑑(𝑡))𝑐(𝑡𝑖)0 (except possibly on a set of zero measure) implying 𝑐(𝑡𝑖)0. Then, global stability is not guaranteed without impulsive controls since the candidate is not a Lyapunov functional. However, the choice 𝜈0(𝑡𝑖)[0,(𝑏(𝑡𝑖)+(𝑏2(𝑡𝑖)4𝑎(𝑡𝑖)|𝑐(𝑡𝑖)|)/2𝑎(𝑡𝑖)] and a sufficiently small 𝑇(𝑡)𝐑+ containing each impulsive time instant ensuring that ||𝑐𝑡𝑖||𝑇(𝑡)max[]𝜏𝑡,𝑡+𝑇(𝑡)||||𝜆min𝑄𝑑(𝜏)𝜆max𝑄𝑇0𝑑(𝜏)𝑄0𝑑(𝜏)̂𝑥(𝜏)22||||𝑏2𝑡𝑖𝑡4𝑎𝑖(4.18) also guarantees global stability even although the impulsive-free system is not stable. If𝜈0(𝑡𝑖)(0,(𝑏(𝑡𝑖)+(𝑏2(𝑡𝑖)4𝑎(𝑡𝑖)|𝑐(𝑡𝑖)|)/2𝑎(𝑡𝑖))then global asymptotic stability is guaranteed provided that 𝜆min(𝑄𝑑(𝑡))>𝜆max(𝑄𝑇0𝑑(𝑡)𝑄0𝑑(𝑡))(𝑐(𝑡𝑖)>0) on a connected subset of 𝐑0+of infinite measure in order to guarantee the global asymptotic convergence to zero of the state-trajectory solution. That means that asymptotic stability is guaranteed under the last conditions for finite time intervals but, after some finite time, the conditions (4.17) are fulfilled. Note that it has not been assumed that the polytope of vertices 𝐴𝑖𝑗(𝑡)=𝐴𝑖𝑗(𝑡),forall𝑖𝑞{0},forall𝑗𝑁 is a stability matrix at any time. The example is very easily extendable to the case of simultaneous control under a standard control and an impulsive one so that 𝐴𝑖𝑗(𝑡)=𝐴𝑖𝑗(𝑡)+𝐵𝑖𝑗𝐾𝑖𝑗, forall𝑖𝑞{0},forall𝑗𝑁.

Example 4.2. An automatic steering device was designed by Minorsky for the battleship New Mexico in 1962, [32]. There is a direction indicating instrument tracking the current direction of motion and there is also an instrument defining the suitable reference motion. Another problem solved by Minorsky for ships is that of the stabilization of the rolling by the activated tanks method in which ballast water is pumped from a position to another one by means of a propeller pump controlled by electronic instrumentation. The second-order delayed resulting dynamics for rolling control of the ship has the following standard form: ̈𝑦(𝑡)+𝛼̇𝑦(𝑡)+𝛽̇𝑦(𝑡)+𝜔20𝑦(𝑡)=𝑢0(𝑡),(4.19) where the various parameters are positive, where the last left-hand side term is related to stiffness, 𝛼 is the standard dumping coefficient excluding delay effects, and 𝛽 is the dumping coefficient produced by pumping which has a delay when the dump becomes overworked (in not overworked normal operation points, the delay =0 and the dumping coefficient is 𝛼+𝛽). If the open-loop control action is modified using feedback to improve the original dynamics as follows: 𝑢0(𝑡)𝑢(𝑡)=𝑢0(𝑡)+𝑘𝛼̇𝑦(𝑡)+𝑘𝛽̇𝑦(𝑡)+𝑘𝜔𝑦(𝑡)(4.20) then, the resulting closed-loop differential equation becomes, ̈𝑦(𝑡)+𝛼𝑘𝛼̇𝑦(𝑡)+𝛽𝑘𝛽𝜔̇𝑦(𝑡)+20𝑘𝜔𝑦(𝑡)=𝑢0(𝑡),(4.21) which can be also described in the state-space form (1) through two first-order differential equations by the state variables 𝑥1(𝑡)=𝑦(𝑡), 𝑥2(𝑡)=̇𝑦(𝑡) as ̇𝑥1(𝑡)̇𝑥2=𝑘(𝑡)01𝜔𝜔20𝑘𝛼𝑥𝛼1(𝑥𝑡)2+(𝑡)000𝑘𝛽𝑥𝛽1(𝑥𝑡)2+01𝑢(𝑡)0(𝑡).(4.22) The above system is positive if and only if 𝑘𝜔𝜔20 and 𝑘𝛽𝛽 irrespective of the value of (𝑘𝛼𝛼) since 𝐴0=[𝑘01𝜔𝜔20𝑘𝛼𝛼] (the system delay-free matrix) is a Metzler matrix, the control vector 𝑏>0and the delayed matrix of dynamics 𝐴1=[000𝑘𝛽𝛽]>0. A complete discussion about positivity is found in [32]. The fundamental matrix of the above system is Ψ(𝑡,0)=𝑒𝐴0𝑡𝐼+0𝑡𝑒𝐴0𝜏𝐴1Ψ(𝜏,0)𝑈(𝑡)𝑑𝜏,(4.23) where 𝑈(𝑡)=1(𝑡)is the unit step (Heaviside) function. In Minorsky’s problem 𝑢0(𝑡)𝑎sin𝜔𝑡 which is not a positive control for all time. Now, consider the stability problem rather than the positivity one under a polytopic parameterization numbered by “1” and “2” one being stable while the other being unstable. Consider the case where switches occur between both vertices of the polytope. The polytope model is adopted to deal wit the uncertainty in the parameter (𝑘𝜔𝜔20) which is known to be close zero, but its sign is unknown if, for instance, it is slightly time varying around zero.
(1) Assume that the uncontrolled parameterization 1 is stable independent of the delay under the following constraints: 𝑘𝜔1<𝜔201,𝑘𝛼1<𝛼1,𝐴112<12||𝜆max𝐴01+𝐴𝑇01||,(4.24) where 𝐴01=[𝑘01𝜔1𝜔201𝑘𝛼1𝛼1],𝐴11=[000𝑘𝛽1𝛽1]. The two first constraints ensure that 𝐴01 is a stability matrix while the third one ensures stability independent of the delay of the uncontrolled system or under any control guaranteeing that the modified closed-loop matrices 𝐴𝑖1 (𝑖=1,2) satisfiy similar stability constraints.
(2) Assume that the uncontrolled parameterization 2 is unstable under the following constraints: 𝑘𝜔2>𝜔202,𝑘𝛼2<𝛼2,𝐴122<12||𝜆max𝐴02+𝐴𝑇02||,(4.25) where𝐴02=[𝑘01𝜔2𝜔202𝑘𝛼2𝛼2], 𝐴12=[000𝑘𝛽2𝛽2]. The two first constraints ensure that 𝐴01 is a stability matrix while the third one ensures stability independent of the delay of the uncontrolled system or under any control guaranteeing that the modified closed-loop matrices 𝐴𝑖1 (𝑖=1,2) satisfy similar stability constraints. There are several possibilities to stabilize the system by choosing to generate impulsive controls at certain switching time instants in between parameterizations. Two of them are the following.
(1) Stabilizing Law 1 via Impulse-Free Switching between Parameterizations with Minimum Residence Time at the Stable Parameterization 1
Choose 𝑢00. Let ImpΞ={𝑡𝑖𝐑0+}𝑖𝐙0+be the sequence of switching time instants in-between the parameterizations 1 and 2 and vice-versa. Prefix a designer’s choice of indexing index integer ̂𝑖𝐙0+which might be sufficiently large but finite. Thus, for any 𝐙0+̂𝑖𝑖(even) the active 2-parameterization is unstable on [𝑡𝑖,𝑡𝑖+1) with switching to parameterization 1 at t =𝑡𝑖+1. Proceed as follows. Choose 𝑡𝑖+2>𝑡𝑖+1 with sufficiently large residence time interval 𝑇𝑖+1=𝑡𝑖+2𝑡𝑖 at the active stable parameterization 1 so that the subsequent stability constraint holds Ψ𝑡𝑖+2,𝑡𝑖+12Ψ𝑡𝑖+1,𝑡𝑖2𝑡𝜎𝑖+2,𝑡𝑖+11,(4.26) with the prefixed real sequence Θ={𝜎(𝑡𝑖+2,𝑡𝑖+1)1}𝑖(̂𝑖)𝐙0+ for any 𝑡𝑖+1>𝑡𝑖. The above switching law between parameterizations generates a stable polytopic system with switches at the polytope vertices. This simple law has to direct immediate extensions. (a) The use of an impulsive-free stabilizing control law which makes the parameterization 1 stable with a greater stability degree that its associate open-loop counterpart. (b) To guarantee the stability constraint by considering strips including some finite number of consecutive switches in-between parameterizations 1-2 by guaranteeing a sufficiently large residence time at the current stable active parameterization 1. Note that if the sequence Θ has infinitely many members strictly less than one, the global exponential stability of the polytopic system with switches in between vertices is guaranteed.
(2) Stability Might Be Achieved with Impulsive Controls at Switching Time Instants for a Switching Sequence Ξ Indexed for 𝐙0+̂ii(Even) as Above
Proceed as follows. (1) Choose 𝑡𝑖+2Ξ at time instants such that 𝑥1(𝑡𝑖+2)0for each triple of switching time instants which does not respect the stability constraint (i.e., if Ψ(𝑡𝑖+2,𝑡𝑖+1)2Ψ(𝑡𝑖+1,𝑡𝑖)2>1). (2) Define a sequence of real numbers {𝜀(𝑡𝑖+2)}𝑖(̂𝑖)𝐙0+ defined by 𝜀(𝑡𝑖+2)=|𝜀(𝑡𝑖+2)|sgn𝑥1(𝑡𝑖+2) if 𝑥2(𝑡𝑖+2)0 and 𝜀(𝑡𝑖+2)=0 if 𝑥2(𝑡𝑖+2)=0 such that 𝜀(𝑡𝑖) is zero if and only if 𝑥2(𝑡𝑖+2)=0. (3) Generate an impulsive control𝑢0(𝑡𝑖+2)=𝐾(𝑡𝑖+2)𝛿(𝑡𝑡𝑖+2) with controller sequence{𝐾(𝑡𝑖+2)}𝑖(̂𝑖)𝐙0+defined as 𝐾𝑡𝑖+2=𝜀𝑡𝑖+2sgn𝑥1𝑡𝑖+2𝑥2𝑡𝑖+2𝑥2𝑡𝑖+2,if𝑥2𝑡𝑖+20,1if𝑥2𝑡𝑖+2𝑥=0,1𝑡+𝑖+2=𝑥1𝑡𝑖+2,𝑥2𝑡+𝑖+2=𝑡1+𝐾𝑖+2𝑥2𝑡𝑖+2𝑡=𝜀𝑖+2.(4.27) Now, note by taking into account from the companion form of the state-space realization that 𝑥2(𝑡)=̇𝑥1(𝑡), 𝑘𝜔2>𝜔202, and 𝑘𝛼2<𝛼2, it follows for 𝛿>0 from the mean value theorem for integrals of continuous integrands that, ̇𝑥1𝑡+𝑖+2=𝑥2𝑡+𝑖+2=𝑡1+𝐾𝑖+2𝑥2𝑡𝑖+2𝑡=𝜀𝑖+2||𝜀𝑡=𝑖+2||sgn𝑥1𝑡𝑖+2if𝑥2𝑡𝑖+2𝑥0,2𝑡+𝑖+2=0if𝑥2𝑡𝑖+2=0(4.28) Since 𝑥2(𝑡) is Lipschitz-continuous, then for any given 𝜀0𝐑+, it exists 𝛿=𝛿(𝑡𝑖+2,𝜀0)𝐑+ being a monotone increasing function of the argument 𝜎 such that using the mean value theorem for integrals of continuous bounded integrands, one has forall𝜎[0,𝜎); forall𝜎𝐑+ as follow:̇𝑥1𝑡𝑖+2+𝜎=𝑥2𝑡+𝑖+2𝜀𝑡+𝜎𝑖+2𝜀0𝑡,𝜀𝑖+2+𝜀0||𝑥2𝑡𝑖+2||||𝜀𝑡+𝜎𝑖+2||+𝜀0,𝑥1𝑡𝑖+2+𝜎=𝑥1𝑡𝑖+2+𝑡𝑖+2𝑡+𝜎𝑖+2̇𝑥1(𝜏)𝑑𝜏=𝑥1𝑡𝑖+2+𝜎𝑥2||𝑥(𝜁)1𝑡𝑖+2||||𝜀𝑡+𝜎(1𝜎)𝑖+2||+𝜀0,(4.29) for some 𝐑+𝜁(𝑡𝑖+2,𝑡𝑖+2+𝛿). Thus, for sufficiently small |𝜀(𝑡𝑖+2)| and𝜀0, one has 𝑥𝑡𝑖+2+𝜎21+(1𝜎)2||𝜀𝑡𝑖+2||+𝜀0,(4.30) so that there is a close time instant 𝑡=𝑡𝑖+2+𝜎 to 𝑡𝑖+2(for a sufficiently small 𝜎𝐑+) such that 𝑥(𝑡𝑖+2+𝜎)2 is arbitrarily small by choosing a sufficiently small |𝜀(𝑡𝑖+2)| in the sequence and a sufficiently small 𝜀0. Thus stabilization is achievable via impulsive controls proceeding in this way at the unstable parameterization when necessary through the above technique.

Acknowledgments

The author thanks to the Spanish Ministry of Education by its support of this work through Grant DPI2009-07197 and to the Basque Government by its support through Grants IT378-10 and SAIOTEK SPE07UN04. He is also grateful to the reviewers by their useful comments.