Abstract

A new lemma is proposed to determine the negative imaginary (NI) properties of time-delay systems of retarded and neutral types. The lemma is employed for stability analysis in the context of positive feedback interconnection of infinite-mode NI systems and time-delay systems. A cantilever beam with a collocated piezoelectric sensor and actuator pair is studied as an infinite-mode NI system. A novel time-delay controller is proposed to be used within positive position feedback (PPF) and parametrized based on H-norm optimization targeting the vibration suppression of the flexible beam. The proposed lemma demonstrates that the designed controller is NI. We also present a corollary to ensure the stability of the closed-loop beam system with the proposed controller using Lyapunov and dissipation based stability approaches. The theoretical results are further verified by simulations. Moreover, the efficacy of the controller is evaluated against a state-of-the-art controller for vibration suppression. Simulation results show that the proposed controller achieves better performance in suppressing vibrations without significant change in robustness.

1 Introduction

Passivity as a fundamental concept of circuit theory has become significant for systems and control theory after its generalization to dissipativity by Willems [1]. Both the passivity and dissipativity properties of linear and nonlinear systems have been extensively studied; see, e.g., Refs. [2] and [3]. Its implications are important in a wide range of control concepts with applications in many different fields. For instance, it is used in the robust control design of chemical processes [4] and applied to the adaptive control of robot manipulators [5]. The standout property of the dissipativity theorem is preserving the dissipative property in parallel or feedback connections of two dissipative systems. This fact provides applicability to the control of complex systems such as multi-agent system control, e.g., see Refs. [6] and [7]. Passivity and dissipativity theories involve the energy-based analysis of the input–output characteristics of systems. Passive systems basically cannot store more energy than they receive from the environment. The stored energy and the energy supplied to the system are generalized for dissipative systems as the storage function and the supply rate function, respectively [2,8]. In the context of time-delay systems (TDS), which is the main concern of this paper, the general approach to investigate the passivity of TDS is to utilize an appropriate Lyapunov–Krasovskii functional (LKF) as a storage function. In Ref. [9], sufficient conditions in terms of linear matrix inequalities (LMIs) are given for the passivity of linear TDS of retarded and neutral types. Passivity analysis based on LKF construction and the passivity-based stabilization of linear TDS are addressed in Ref. [10]. Dissipativity-based state feedback and dynamic output feedback control of TDS is studied in Ref. [11]. One can see Ref. [12] reducing conservativeness on passivity conditions. Furthermore, dissipativity conditions for the class of singular TDS are determined over LMIs in Ref. [13].

The energy-based approach of dissipativity provides a unified framework for the design and stability analysis of a wide class of complex systems. However, there are classes of systems which cannot be comprehensively analyzed within the conventional dissipation-based framework, despite exhibiting energy dissipation and finite energy storage. One of these class of systems is referred to negative imaginary (NI) systems since their dissipation property cannot be analyzed via static supply rate functions. NI systems theory is inspired by vibration suppression control of flexible systems with positive position feedback (PPF) where position sensors and force actuators are used [14]. First studies on NI systems were conducted on the frequency domain properties of transfer function models [15,16] where the stability condition of positive feedback interconnection of NI systems is defined simply over the open loop system DC gain. NI system theory has been preferably used in various fields because of this simple stability rule, e.g., see Ref. [17]. A recent study [18] proposed an algorithm to design static output feedback control which makes the closed-loop system NI with a predetermined H-norm. Moreover, NI theory is utilized to unify the vibration suppression techniques using PPF [19], and applied, for instance, to nanopositioning [20,21], to highly resonant structures [22], and to multi-agent system control [2325].

Negative imaginary system properties are also related to the energy storage and the dissipation properties of systems. Reference [26] has shown the correspondence between NI and passive systems based on their dissipation characteristics. Passive systems are dissipative with respect to the supply rate defined by the input to output signal relation (u,y), whereas the NI systems are dissipative with respect to the dynamic supply rate defined for the pair (u,y˙). Consequently, NI, namely, dynamic passive systems, can be considered complementary to passive systems, i.e., to positive real systems. Contrary to passive systems, the dissipativity analysis of NI systems has not been thoroughly explored in Ref. [17]. References [2730] primarily focus on the dissipative properties of linear NI systems, while nonlinear systems are considered in Refs. [26] and [31]. The frequency domain properties of NI-TDS are studied in Refs. [32] and [33]. To the best of our knowledge, the dissipation-based analysis of the NI characteristics of TDS has not been studied yet.

In this paper, we examine the NI (dynamic passivity) property of linear TDS of neutral and retarded type based on dissipativity framework and propose novel sufficient conditions. As an application of the studied problem, we consider the vibration suppression of a flexible cantilever beam which is known to be an NI system [19]. We present a new time-delay controller of retarded type used within positive feedback, which is applied to the collocated piezoelectric sensor (PES) and piezoelectric actuator (PEA) pair to control the beam. The vibration suppression performance of the proposed controller is shown to be better via simulations as compared to a state-of-the-art work [34]. The proposed controller is parametrized with the formulated norm-based optimization problem solved by the standard genetic algorithms and the recent tds-control toolbox [35]. The parametrized controller is shown to be NI by the derived NI condition for linear TDS. Then, a complete stability analysis of the system with the proposed controller is performed by applying a dissipativity-based stability theorem for interconnected NI systems.

The delayed feedback control is used in different concepts to reduce the vibration of flexible cantilever beams with PES–PEA pairs. The cantilever beam is a flexible system with distributed parameters and therefore naturally modeled by a partial differential equation (PDE) [36,37], which results in infinite modes. It is often to model such a system by a transfer function with a finite number of modes utilizing an appropriate truncation method [38]. The stability analysis and control design are then performed on this approximate transfer function model with a small number of modes [39,40]. In Ref. [41], the authors apply an inverse shaper based controller to suppress the vibratory modes of the beam using collocated PES–PEA pairs. This controller design and performance analysis are conducted through the finite mode system model simulation results, where the closed-loop stability is not guaranteed theoretically but shown via simulation results. In Ref. [42], the delayed feedback combined with a modal filter is applied to suppress the vibratory multimodes where the stability analysis is fulfilled via Nyquist technique based on a nonminimum phase beam model with a small number of modes. An important concept using delays for control is the delayed resonator, which has been used for both vibration suppression and energy harvesting for flexible beams with PES–PEA pairs [43,44]. Therein, the resonator is designed over a truncated finite mode system model which is also used for stability analysis applying the D-subdivision method to the transcendental characteristic polynomial. A nonlinear flexible beam model is considered in Refs. [45] and [46], and the delayed feedback using a multiscale method is applied for control where the closed-loop system stability is ensured through the eigenvalues of the linearized finite-mode model. As compared to the mentioned literature, we address the stability problem of the considered TDS differently over the flexible system model with infinite modes. The stability conditions are derived for the infinite-mode system model and depend mainly on the dissipative properties of the time-delayed controller. The analysis over the finite mode system model is avoided for the accuracy.

The paper is organized as follows. In Sec. 2, the existing definitions related to linear time-invariant (LTI) dissipative and dynamic passive systems are provided along with the stability theorem for dynamic passive systems. Section 3 presents the problem description, including the system model and controller structure. In Sec. 4, we introduce a new dissipativity approach for TDS of neutral and retarded type and a new time-delay controller for vibration suppression. In Sec. 5, we present a simple motivational example to show advantages of the proposed time-delay controller and provide a case study that presents the usage of the proposed stability conditions on NI-TDS to the active vibration control of a flexible beam via simulations. The paper concludes in Sec. 6.

Notation: Rn denotes the n dimensional Euclidean space, and the set of non-negative real numbers is represented as R+. Rm×n denotes the set of real matrices of dimension m×n. P>0 is referred to as symmetric and positive definite matrix for PRn×n. C1 stands for all differentiable class of functions whose derivative is continuous. The scalar valued storage function and the supply rate function are denoted by S(·) and s(·), respectively.

2 Preliminaries on Negative Imaginary Systems

In this section, we present the definitions and theorems related to dissipative, passive, and NI-LTI systems represented by
(1)

where x(t)Rn is the system state, u(t)Rm is the system input, and y(t)Rm is the system output. The definitions of dissipativity and dynamic passivity are given below.

Definition 1. [2] The system given byEq.(1)is dissipative with respect to the supply rates(u(t),y(t)), if there exists a storage functionS(x(t)):RnR+of class ofC1which satisfies
(2)

for all input signalsu(t), wherex(t)exists for allt[0,T].

The dissipation inequality (2) can be alternatively formulated in its differential form given by
(3)

which is called as differential dissipation inequality [2]. The choice of supply rate holds significant importance in characterization of the dissipation properties of systems. There are different options for selecting the supply rate. In particular, the system given by Eq. (1) is passive if it is dissipative for supply rate s(u(t),y(t))=u(t)Ty(t).

Definition 2. [26,31] The system(1)forD=0is said to be dynamic passive or NI, if there exists a storage functionS(x(t)):RnR+ofclass ofC1which satisfies the differential dissipation inequality
(4)

for all input signalsu(t), wheres(u(t),y˙(t))=u(t)Ty˙(t)is the dynamical supply rate function andx(t)exists for allt[0,T].

Remark 1. Note that the NI systems are the dual of the positive real (passive) systems [26]. Also instead of the term dynamic passive, the term NI is used throughout the paper.

An LMI-based condition for NI-LTI systems is given in the following lemma.

Lemma 1. [47] The system(1)is NI if and only ifdet(A)0and there exist matricesP=PT>0, WRm×m, andLRm×nsatisfying the LMI
(5)

A more strict dissipation-based characterization of NI systems is presented in the following definition.

Definition 3. [26] Assume that the system(1)forD=0is asymptotically stable. Then, the system(1)is said to be strictly dynamic passive or strictly negative imaginary (SNI), if there exists a storage functionS(x(t)):RnR+of class ofC1which satisfies the dissipation inequality
(6)
for all input signalsu(t), wheres(u(t),y˙(t))=u(t)Ty˙(t)is the dynamical supply rate function andx(t)exists for allt[0,T]. In addition, if
(7)

is satisfied for allt>0, thenlimtu(t)=0.

A dissipation-based analysis of the dynamic passivity of nonlinear systems along with a corresponding stability theorem is proposed in Ref. [26]. Since we are concerned only with linear systems in this paper, an equivalent version of this stability theorem for linear systems is represented in the following.

Theorem 1. [26] Consider two linear dynamical systems G and C each represented byEq.(1)and interconnected as in Fig. 1. Assume that G and C are NI and SNI, respectively. If the DC gain of C is positive and the open-loop DC gain of the system in Fig. 1 lies within the interval[1,1], then the positive feedback interconnection of G and C is asymptotically stable.

Fig. 1
Block diagram with positive feedback connection
Fig. 1
Block diagram with positive feedback connection
Close modal

Proof. The proof of the theorem is given in Ref. [26] based on the Lyapunov stability theorem and LaSalle's invariance principle.▪

The stability of the positive feedback interconnection of the NI and SNI systems is defined in terms of simple and trivial gain conditions above. This paper considers the problem of analyzing the NI characteristics of linear TDS. Moreover, we provide conditions similar to Theorem 1 for the stability of positive feedback interconnection of infinite-dimensional SNI systems, in particular, flexible Euler–Bernoulli beams, with an NI-TDS which is the proposed delayed controller in this paper.

3 A Negative Imaginary Lemma for Time-Delay Systems

In this section, we investigate the NI property of the TDS of neutral and retarded types governed by
(8)

where x(t)Rn, u(t)Rm, z(t)Rm, A0,A1Rn×n, B1Rn×m, CRm×n, and g,hR+ are constant delays. As for passive systems, the NI property holds for dynamical systems only with the same number of inputs and outputs [2]. Here, we aim to establish a criterion for the system (8) to be NI independent of the neutral-type delay g, i.e., being NI for all g values. To achieve this, the system first needs to be robustly stable against small variations in g, which implies that the absolute values of all the eigenvalues of F are strictly less than one, i.e., F is a Schur–Cohn stable matrix; see Refs. [9] and [48]. Thus, the following assumption holds for the rest of the paper.

Assumption 1. All the eigenvalues of F are inside the unit circle.

Remark 2. Despite the fact that Definitions 2 and 3 are given for a nondelayed LTI system (1), they are valid for the system (8) to be NI. This is because the dissipative properties of systems are defined based on the relationship between the energy transferred to the system input and the energy stored in the system. Therefore, the definitions with the given dissipation inequality conditions in Eqs. (2)(4) are preserved for TDS. For instance, the passivity condition for the system (8) is given in Ref. [9] as
(9)
which corresponds to Eq. (2) for s(u(t),y(t))=uT(t)y(t) and for some storage function S(x(t))>0 since

for all x(0)=x0. Following this approach, we conclude that Definitions 2 and 3 are valid also for the delay system (8) to be NI or SNI. On the other hand, dissipative properties change regarding the delay type or the occurrence of delay meaning which signal is delayed in the system. For instance, it is shown in Refs. [49] and [50] that the systems with input and/or output delays cannot be passive or dynamically passive. The delays in Eq. (8) occur at the state vector and its derivative, which is one of our motivations to investigate the NI properties of the system.

Based on Definition 2 for NI systems and Remark 2, the following NI lemma is proposed for the systems represented by Eq. (8) utilizing an appropriate LKF as the storage function.

Lemma 2. If there exist the matricesP>0,R>0,U>0,S>0,P2, andP3which satisfy the following LMI:
(10)

then the system(8)under Assumption 1 is NI for allg0.

Proof. Defining a new state variable y(t), an equivalent descriptor form [51] of the system (8) is given as
(11)
This way, the system state variables of the equivalent descriptor form are considered as x and y. Note that the NI characteristics of the system (11) are same as of the system (8). Regarding this, the aim is to find an appropriate storage function which satisfies the dissipation inequality (4) in Definition 2 as explained in Remark 2 to prove that the system (11), i.e., the system (8), is NI. For this purpose, we consider the storage function depending on variables x and y in the form of the LKF
(12)
which is commonly used in the stability analysis of TDS [52]. For readability, let us express Eq. (12) separately for each term as
(13)
Due to the descriptor model transformation, the novelty is not in the selected LKF, but in the calculation of its derivative with respect to time [52]. Considering the descriptor model (11) for differentiation of V1, we get
(14)
where P2,P3Rn×n are the slack variables. The derivatives of other terms are derived as
(15)
(16)
(17)
Subsequently, by applying Jensen's inequality [53] for the integral term of Eq. (17), one gets
(18)
Jensen's inequality is used to calculate the upper bound of the derivative term in Eq. (17). Then, we substitute the supply rate s(u(t),z˙(t))=u(t)Tz˙(t) and the derivative of the storage function S˙(x(t),y(t))=V˙(x(t),y(t)) derived in Eqs. (14)(17) into the dissipation inequality (4). Finally, defining
and using Eq. (18), we arrive at
(19)

Φconst in Eq. (19) is the matrix on the left-hand side of Eq. (10), which completes the proof.▪

Note that LMI (10) is affine in h2. Thus, the upper bound of the delay h where the system (8) is NI can be computed using an iterative line search on h keeping Eq. (10) feasible [54]. The computational complexity of LMIs is commonly given in terms of the number of decision variables and order. The order and the number of decision variables of LMI (10) is 5n and 3n2+3n, respectively, which is one of the least among other studies on TDS; see, e.g., Table 1 in Ref. [55] for the LMI analyses of key TDS studies. Indeed, the computational complexity rises as the system dimension n increases. We demonstrate the number of decision variables and the consumed CPU time to solve LMI (10) in Sec. 6 for the proposed time-delay controller with increasing dimensions.

Table 1

System parameters of the motivational example

k1k2ω1ω2ζ1ζ2
11503140.0010.001
k1k2ω1ω2ζ1ζ2
11503140.0010.001

The other objective of this study is to demonstrate the usage and verification of the proposed approach above for LTI–TDS through a suitable case study. For this purpose, we first present a flexible beam system in Sec. 4 and then propose a time-delay controller to suppress the vibrations on the beam.

4 Flexible Beam as a Negative Imaginary System and Vibration Control

In this section, we present the flexible beam system fixed at one end and released at the other so that it can move freely at one end as shown in Fig. 2. A collocated PES–PEA pair is attached to the beam for vibration suppression. The Euler–Bernoulli beam model is used to characterize the beam. The amplitude of oscillation, denoted as y(r,t) along the yaxis direction at any point r on the beam, is measured by the induced voltage V0(t) of the PES. The applied voltage Vi(t) by the PEA generates a bending moment M(r,t) to counteract and mitigate the vibration.

Fig. 2
Scheme of a cantilever beam with a collocated piezoelectric sensor–actuator pair
Fig. 2
Scheme of a cantilever beam with a collocated piezoelectric sensor–actuator pair
Close modal
The general motion equation of the Euler–Bernoulli beam is a fourth-order PDE
(20)
where E is the Young's modulus of elasticity, I is the second moment of area, ρ is the density, and A is the cross-sectional area of the beam. When the controllers with standard transfer functions are used together with the PDE model, it may be difficult or even impossible to perform the analysis and synthesis problem. Assumed mode technique presented in Ref. [56] models the system with the transfer function G(s) expressed as the sum of infinite second-order systems defined from Vi(t) to Vo(t)
(21)

where ϕi(r) is the ith mode shape, ωsi is the ith natural frequency, ζsi is the ith damping ratio, L is the length of the beam, Ca and Cs are the gain values calculated with the beam parameters, and r1 and r2 are the starting and ending positions of the piezoelectric material on the beam, respectively. An important feature of the infinite dimensional beam model, which is utilized in this study, is given in the following property.

Property 1. Second-order single-input single-output systems characterized by positive parameters and their infinite sums are shown to be SNI inRef. [19]. Consequently, the beam model G(s) given byEq.(21)is SNI since the parameterCais negative whereas all the other parameters are positive; seeRef. [56].

The system model (21), which contains an infinite number of resonant modes, is not practical to be used for controller design. Therefore, it is preferred to use a system model with a finite number of modes that accurately represents the system dynamics. These modes are chosen within the desired frequency bandwidth where the vibration damping is targeted. Thus, the model (21) is truncated to M modes of interest as
(22)

where usually the high frequency modes are neglected. The constant feed-through term D in Eq. (22) is to correct the undesired fact of the truncation, namely, the alteration of the actual zeros of Eq. (21) with neglecting the high frequency modes. The term D is determined via various approaches such as in Refs. [37] and [38] to improve the accuracy of the truncated model.

4.1 Positive Position Feedback Control.

Various control methods have been developed for vibration suppression of smart flexible systems. PPF control is a pioneering method designed specifically for flexible systems with collocated PES–PEA pairs. The block diagram of PPF is given in Fig. 1, where G(s) and C(s) represent the flexible system model and the PPF controller, respectively. Moreover, w(t) and y(t) represent the disturbance signal and the transverse vibration (displacement) of the flexible system, respectively.

Positive position feedback control proposed in Ref. [57] aims to suppress the vibrations via adding an extra damping to the system through the incorporation of a second-order filter. The filter is designed such that an additional damping is supplied to the targeted resonant mode of the flexible system (21). In Ref. [14], this approach was extended to a multimodal design where the several system resonant modes are targeted by the parallel interconnection of second-order filters utilized in PPF. A more recent study [34] improved the multimodal filter design by connecting first-order low-pass filters additional to the second-order filters for each targeted system modes, which results in the PPF controller transfer function
(23)

and named as the multimode modified positive position feedback (MMPPF). This extension provides a performance enhancement especially for the steady-state disturbances acting on the system, see Refs. [34] and [58]. Note that N in Eq. (23) is the number of targeted system modes that is commonly chosen NM to reduce the computational load in design. Nevertheless, the increment in the number of resonant modes to be damped corresponds to an increase in the number of both the second-order and the first-order filters in Eq. (23), which means an increase in the order of MMPPF controller.

To avoid the mentioned rise in the controller order and to achieve better vibration suppression for the considered flexible structure, we take advantage of the time delays as control parameters. Namely, we propose a time-delay controller in Sec. 5 where also an optimization-based parametrization is presented. Furthermore, the stability of the time-delayed closed-loop system is analyzed via the proposed NI lemma in Sec. 3.

5 Active Vibration Suppression Via Time-Delay Controller

Time-delay based control techniques are utilized in vibration control since they enhance damping performance with ease of implementation, see, e.g., Refs. [5963]. Inspired from such studies, we propose the time-delay controller of retarded type in the form of
(24)

used within positive position feedback for vibration suppression on flexible systems like the considered beam in Sec. 4. We refer to Eq. (24) as the PPFR controller, where R stands for retarded, and apply it to the flexible system as shown in Fig. 1 to suppress vibrations. Compared to the MMPPF in Eq. (23), we replace the multiple first-order low-pass filters interconnected in parallel with a single time-delayed low-pass filter in Eq. (24). Note that, to suppress N modes of the system, the MMPPF requires N low-pass filters in parallel increasing the controller order, whereas the PPFR uses a single filter regardless of the number of targeted modes to be suppressed. Thus, PPFR has an advantage of having lower order in implementation for practical applications when N>1.

In the following motivational example, we explain and demonstrate the advantages of the proposed PPFR controller compared to the MMPPF controller for vibration suppression problem over a simple vibratory system model.

5.1 Motivational Example.

Let us consider a two-mode vibratory system model given as
(25)

where k1k2,ζ1ζ2, and ω1ω2 are the gains, damping ratios, and natural frequencies for the first and second vibration modes, respectively, which are given in Table 1.

In order to suppress the vibration of the first resonant mode of the system above, we use PPFR (24) and MMPPF (23) controllers for N=1 in a positive feedback interconnection, as shown in Fig. 1. The damping and frequency parameters of both controllers are chosen as ζc1=ζ1, ζc2=ζ2, ωc1=ω1, and ωc2=ω2 as explained in Ref. [34]4A. The rest of the both controllers' parameters are determined as in Table 2 using an H-norm based optimization method, which is detailed in Sec. 5.3. Note that for a fair comparison of the controller performances, the same optimization procedure with the same cost functions is applied to parametrize the both controllers. The frequency responses of the two-mode system model and closed-loop system with the PPFR and MMPPF controllers are illustrated in Fig. 3, and the followings are observed:

Fig. 3
Frequency responses of open-loop system and the closed-loop systems controlled with PPFR and MMPPF
Fig. 3
Frequency responses of open-loop system and the closed-loop systems controlled with PPFR and MMPPF
Close modal
Table 2

Controller parameters for the motivational example

PPFRkc1αca0a1h
0.03226.42168.5997.4990.19
PPFRkc1αca0a1h
0.03226.42168.5997.4990.19
MMPPFkc1γc1
0.0160.383
MMPPFkc1γc1
0.0160.383
  • PPFR controller provides lower magnitude at the targeted first mode frequency which means better vibration suppression compared to MMPPF.

  • PPFR controller provides also better vibration suppression for the second mode which is not considered as a design objective, compared to MMPPF.

The reason of observed advantages of PPFR above can be explained by the frequency responses of the controllers in Fig. 4. PPFR controller has periodic peaks in frequency response due to the periodic characteristic of the delay term ehs, which results in magnitudes higher than MMPPF. Consequently, better performance in suppressing vibrations for both the targeted and nontargeted modes in design is achieved. Another fact seen from the closed-loop frequency responses in Fig. 3 is that the PPFR controlled system has lower magnitudes for low frequencies which is a desired behavior to avoid spillover effect of the frequencies away from the targeted resonance frequency [34,58].

Fig. 4
Frequency responses of PPFR and MMPPF controllers
Fig. 4
Frequency responses of PPFR and MMPPF controllers
Close modal

The closed-loop system with PPFR has a retarded distribution in poles which depart from imaginary axis with increasing moduli. Rightmost pole within a spectral distribution is often the dominant pole of TDS which characterizes stability and dynamic response. Regarding that, the rightmost pole's damping ratio is defined as the equivalent damping factor where a higher equivalent damping factor corresponds to a better-damped system. As suggested in Ref. [64], we calculate the equivalent damping factors of the dominant poles of the closed-loop systems as given in Table 3 where the PPFR controlled system has a higher equivalent damping. Thus, PPFR damps the flexible system better than MMPPF.

Table 3

Damping factors of the closed-loop systems

ControllerRightmost poleEquivalent damping
PPFR0.08042±50.04i0.0016
MMPPF0.0704±50i0.0014
ControllerRightmost poleEquivalent damping
PPFR0.08042±50.04i0.0016
MMPPF0.0704±50i0.0014

5.2 Stability Analysis of the Flexible System With Positive Position Feedback Retarded Control.

Stability analysis of the infinite-mode model for cantilever beam (21) controlled with a time-delay controller as in Fig. 1 constitutes a challenging problem. In Refs. [4346] where delays are utilized as control parameters, stability is analyzed considering the truncated system model (22) in closed-loop architecture which may cause inaccuracy. It is because of the approximation of high-frequency modes by the constant term D in Eq. (22). To overcome this fact, dissipation-based stability analysis stands out as a particularly suitable approach due to SNI property of the infinite-mode beam model (21). In Ref. [65], the passivity definitions for nonlinear systems without delay and linear time-delay systems are naturally extended to retarded types of nonlinear time-delay systems. The stability analysis of the negative feedback interconnection of passive nonlinear time-delay systems is performed through an inherent generalization of the dissipation-based stability theorem for nonlinear systems. For linear NI systems with rational transfer functions, the positive feedback interconnection is guaranteed under a straightforward open-loop gain condition. A Lyapunov-based stability condition equivalent to the open-loop DC gain criterion is proposed, and the stability condition for the positive feedback interconnection of NI and SNI systems is provided [66]. In Ref. [26], the definitions of linear NI systems are generalized to nonlinear dynamic passive systems. Using Lyapunov stability theory and certain gain conditions which can be equivalently formulated as the DC gain criterion for linear systems, stability conditions for nonlinear dynamic passive systems are derived. Following a similar approach, we demonstrate that an infinite-dimensional linear system interconnected with a time-delay system via positive feedback is stable under specific conditions (cf. Corollary 1).

The state space representation of the PPFR controller (24) is
(26)
where
(27)

Note that Eq. (26) is in the form of the system (8) with F=0. Therefore, Lemma 2 formulated in terms of the LMI (10) can be employed to analyze that the PPFR controller is NI or not. Then, we provide the following corollary for the stability of the considered system with the proposed delayed control.

Corollary 1. Consider the closed-loop system given by Fig. 1 where G(s) is the flexible beam model(21)andC(s)is the PPFR controller(24)which satisfies
(28)

whereKR+is the upper limit of the DC gain of the flexible beam(21). Then, the system is asymptotically stable if the LMI(10)with the matrices(27)is satisfied for anyP>0,R>0,U>0,S>0,P2,P3, andF=0.

Proof. Recall that the state-space representation of PPFR controller (26) is in the form of the system (8) with F=0. Then, if there exist matrices P>0,R>0,U>0,S>0,P2, and P3 satisfying the LMI (10) with A0,A1,B1,C in Eq. (27) and F=0, we conclude that the PPFR controller (24) is NI by Lemma 2. Moreover, the storage function (12) is determined for PPFR, which is denoted as Vc(xc) where xc=(x,y) from this point onward.

Now let us represent the flexible beam model (21) in state-space as
(29)
where
(30)

In Eq. (30), L¯ represents arbitrarily large number of system modes. Since beam model is SNI according to Property 1, there exists a positive definite storage function Vb(xb)=xbTPbxb with PbT=Pb>0 for the system (29) with the matrices (30), which satisfies dissipation inequality (6), used also for the proof of Lemma 1, see Ref. [47].

For the closed-loop stability analysis, the disturbance signal w(t) given in Fig. 1 is considered as zero without loss of generality. The beam model G(s) and the PPFR controller C(s) are connected such that the input signals to each are ub(t)=z(t) and u(t)=yb(t), respectively. A Lyapunov-based approach is used for the stability analysis of the closed-loop system. The candidate Lyapunov function is proposed as
(31)

If the open-loop system DC gain lies within the range [1,1] and the DC gain of SNI system is positive as stated in Theorem 1, then W(xc,xb) is always positive, refer to Lemma 8 in Ref. [26]. Since DC gain of each mode of the beam model is positive due to the collocated structure of the PES–PEA pair, i.e., kbi>0i, the DC gain of SNI system is always positive. Moreover, determining the upper limit of the DC gain of the infinite model (21) as K which is always greater than the DC gain of the system (29) with the matrices (30) with any finite L¯, and considering the condition (28) is satisfied for the controller, then it is assured that the open-loop system DC gain remains within the range [1,1] which guaranties W(xc,xb)>0 for all xc0 and xb0.

Now, we need to show that the derivative of the candidate Lyapunov function (31)
(32)
is negative for all xc0 and xb0. Since the flexible beam system (29) with the matrices (30) is SNI, an auxiliary system can be defined as
(33)
with L and P satisfying Lemma 1 [26,47]. Using the output of the auxiliary system, V˙b can be expressed as
(34)
Then, using the relation (34) in Eq. (32), we obtain
(35)

since we have V˙cu(t)z˙(t)0 from PPFR being NI and V˙bub(t)y˙b(t)0 from beam model being SNI. W˙(xc,xb) can only remain zero if y˜b=0. Considering SNI property of the beam, the equality V˙b=uby˙b holds, then limtub0 as stated in Definition 3. Since ub0 results in yb0, which in turn ensures xb0. Moreover, since ub=z with positive feedback in Fig. 1, this directly leads to z0. Furthermore, PPFR controller is observable due to the structure of A0 and C in Eq. (27) which follows x0. Therefore, W˙ is zero only when the system trajectory approaches to the origin [0, 0], which is the stable equilibrium point of the linear closed-loop system.▪

5.3 Controller Parametrization and Robustness Analysis.

In this subsection, we present an optimization-based approach to parametrize the proposed controller PPFR for efficient suppression of the resonant modes. Also, a sensitivity function is presented to evaluate the controller robustness against the deviation of the natural frequency of flexible beam.

The PPFR controller applied in positive feedback has two structural parameters ωci and ζci which is equal to the ith natural frequency and ith damping ratio of the flexible beam modes. Thus, it remains to parametrize the other terms of PPFR which are kci,αc,a0,a1,h. For this purpose, we present a parametrization approach via H-norm based optimization for the closed-loop transfer function T(s) for the positive feedback of G(s) in Eq. (22) and C(s) in Eq. (24). We describe the optimization problem as
(36)

where bi is the predefined weighting constant for ith resonant mode, and Hi(s) is the predefined weighting bandpass filter around ith system resonant frequency ωsi. The term b0T(0), representing the weighted DC gain, is also considered to mitigate deterioration around the DC frequency and enhance the controller's performance at lower frequencies. The closed-loop system transfer function T(s) in Eq. (36) includes internal time delays. Due to the nonconvex nature of the optimization problem, matlabgeneticalgorithm (ga) is used to search parameters, and the weighted infinite norm of the cost function (36) is calculated via tds-control toolbox [35].

The flowchart in Fig. 5 shows the integrated use of the ga and tds-control toolboxes. The initial value of the cost function is calculated for the initial parameters determined by ga. Standard genetic operations are then used to generate new parameters for optimization problem based on the best parameters determined in the previous iteration. These iterations are continued until the maximum number of iteration is reached, then the search is terminated. The parameters that minimize the cost function over all iterations are the solution to the optimization problem.

Fig. 5
Methodology for solving the optimization problem to parametrize controller
Fig. 5
Methodology for solving the optimization problem to parametrize controller
Close modal
In order to evaluate the performance of the PPFR controller parametrized with Eq. (36), a sinusoidal disturbance signal w(t) (cf. Fig. 1) with the same frequency as the resonant mode of the system is applied. However, the uncertainties in the resonant frequency of the system may cause dramatic degradation in the vibration suppression performance of the controller. The sensitivity function S(s) is defined as
(37)
where G(s) and C(s) are the finite-mode flexible beam and the controller transfer functions, respectively. Then, the characteristic slope is defined as
(38)

where Δω is the uncertainty of ith system resonant frequency utilized to analyze the controller robustness to uncertainties in the system's resonant frequency [67,68]. The smaller the slope of κi means the lower sensitivity of the controlled system to deviations in the resonance frequency to be suppressed.

In Sec. 6, the proposed H-norm based design is performed for PPFR and MMPPF controllers, where MMPPF controller as a state-of-the-art work is chosen for comparison of the performance with the PPFR controller.

6 Numerical Simulations

In this section, we address the vibration control problem of the real cantilever beam with the parameters given in Table 4 studied in Refs. [56] and [69]. Regarding these parameters, we use two models in the form of Eq. (22) with different number of modes, where
Table 4

Flexible beam parameters [56,69]

Beam length (L0.77m 
Beam width (W0.05m 
Beam thickness (h0.006m 
Beam density (ρ2.770×103 
Piezomaterial position (r10.05m 
Piezomaterial position (r20.12m 
Piezomaterial Young's modulus (Ep6.7×1010N/m2 
Charge constant (d312.1×1010m/V 
Voltage constant (g311.15×102 
Capacitance (C) 1.05×107F 
Piezomaterial width (Wp0.025 m 
Piezomaterial thickness (hp2.5×104m 
Coupling coefficient (k310.34 
Beam length (L0.77m 
Beam width (W0.05m 
Beam thickness (h0.006m 
Beam density (ρ2.770×103 
Piezomaterial position (r10.05m 
Piezomaterial position (r20.12m 
Piezomaterial Young's modulus (Ep6.7×1010N/m2 
Charge constant (d312.1×1010m/V 
Voltage constant (g311.15×102 
Capacitance (C) 1.05×107F 
Piezomaterial width (Wp0.025 m 
Piezomaterial thickness (hp2.5×104m 
Coupling coefficient (k310.34 

The first model is with low number of modes where M=4, which is used for the controller parametrization to reduce the computational burden. The second one is with higher number of modes where M=20 used for simulations to verify the stability ensured by Corollary 1 and the controller performance. The model with higher number of modes is to represent the infinite system model more accurately.

We first consider the beam model (22) derived from the parameters given in Table 4 with M=4 resonant modes. The natural frequencies and damping ratios for each mode are provided in Table 5. We target two of these modes, i.e., choose N=2 in the controllers PPFR (24) and MMPPF (23), and parametrize them by solving optimization problem (36) following the procedure in Fig. 5. Note that the parameters to be optimized for MMPPF in Eq. (36) are kci and γci. The obtained controller parameters are given in Table 6. Then, the parametrized controller is shown to be NI via using the proposed Lemma 2.

Table 5

System modes for the model (22) with M=4

ωsi (rad/s)ζsi
Mode 10.0502×1030.0006
Mode 20.3145×1030.0019
Mode 30.8801×1030.0053
Mode 41.7254×1030.0103
ωsi (rad/s)ζsi
Mode 10.0502×1030.0006
Mode 20.3145×1030.0019
Mode 30.8801×1030.0053
Mode 41.7254×1030.0103
Table 6

Controller parameters found by the optimization procedure proposed in Sec. 5.3

PPFRkc1kc2αca0a1h
0.1860.12349.62291.8958.6920.116
PPFRkc1kc2αca0a1h
0.1860.12349.62291.8958.6920.116
MMPPFkc1kc2γc1γc2
0.1040.1080.2650.233
MMPPFkc1kc2γc1γc2
0.1040.1080.2650.233

Remark 3. LMI (10) for the controller in Table 6 is solved with 75 decision variables in 0.0721 s of CPU time on a standard laptop with 2.6 GHz CPU (i7) and 16 GB RAM. We also solved LMI (10) for the controllers parametrized when the number of targeted modes are N=3, N=4, and N=5 in 0.1204, 0.2219, and 0.5598 s of CPU time, with 140, 225, and 330 decision variables, respectively. The LMIs were solved simply via “feasp” command in matlab.

We calculate the DC gain of the infinite-mode beam model (21) with parameters listed in Table 4 regarding the change in the number of system modes M as shown in Fig. 6 from which we conclude that the system DC gain converges approximately to 0.55. Consequently, we choose the upper limit of the DC gain as K=0.7 in condition (28) to hold a safety margin for stability analysis. Also, the DC gain of the parametrized PPFR controller is found to be 0.8 resulting that the condition (28) is satisfied. Therefore, the closed-loop stability of the infinite-mode system with obtained PPFR controller is guaranteed by Corollary 1. In order to verify the theoretical stability results, the simulation of the system in Fig. 1 with the parametrized PPFR controller and the beam model with 20 modes is performed.

Fig. 6
DC gain values calculated with respect to the number of modes considered in the beam model
Fig. 6
DC gain values calculated with respect to the number of modes considered in the beam model
Close modal

Figure 7 illustrates the frequency responses of the beam model and of the closed-loop systems with PPFR and MMPPF controllers. Both controllers designed via the given optimization approach are able to suppress the targeted two resonant modes. However, the PPFR controller provides better vibration suppression at the targeted resonant frequencies as compared to MMPPF. We also show the closed-loop frequency responses with the 4-mode and 20-mode system models controlled with PPFR in Fig. 8. As it is supposed to be, the frequency responses of the 4-mode and 20-mode system models are consistent for the targeted frequency range. Besides, it is seen that the system modes with higher frequencies are not amplified with the designed PPFR controller.

Fig. 7
Frequency responses of the open-loop system and closed-loop system controlled with PPFR and MMPPF for the 4-mode beam model
Fig. 7
Frequency responses of the open-loop system and closed-loop system controlled with PPFR and MMPPF for the 4-mode beam model
Close modal
Fig. 8
Frequency responses of the open-loop system and closed-loop system controlled with PPFR for the 4-mode and 20-mode beam models
Fig. 8
Frequency responses of the open-loop system and closed-loop system controlled with PPFR for the 4-mode and 20-mode beam models
Close modal

We also simulate the time-domain performance of the designed controllers when a periodic disturbance and an impulsive disturbance are applied to the cantilever beam system. The response of the system is the PES voltage that corresponds to the displacement of the beam at the point where the sensor is attached. The primary objective is to demonstrate the stability of the infinite-mode system according to Corollary 1 through simulations and to evaluate its disturbance suppression performance. Therefore, the PPFR controller which is designed using 4-mode system model is applied to 20-mode system model to verify closed-loop stability and vibration suppression performance results. First, it is assumed that a disturbance voltage signal is applied from the PEA to the beam. The disturbance signals that will lead to the worst oscillations in the system are the perturbations acting at the resonance frequency of the system [34]. Therefore, a periodic disturbance signal w(t)=sin(ω1t)+sin(ω2t) is applied, where ω1 and ω2 are the first two resonance frequencies of the system modes given in Table 5. The periodic disturbance response of the open-loop system and of the closed-loop system obtained for 20-mode system model (22) with the parametrized controllers is presented in Figs. 9 and 10, respectively. It is seen that the PPFR controller supresses the vibration faster.

Fig. 9
Open-loop system response under periodic disturbance of sinusoidal signals with system resonant frequencies
Fig. 9
Open-loop system response under periodic disturbance of sinusoidal signals with system resonant frequencies
Close modal
Fig. 10
Responses of closed-loop systems controlled with PPFR and MMPPF under periodic disturbance of sinusoidal signals with system resonant frequencies
Fig. 10
Responses of closed-loop systems controlled with PPFR and MMPPF under periodic disturbance of sinusoidal signals with system resonant frequencies
Close modal

Remark 4. Note that the PPFR controller, designed using a 4-mode system model for vibration suppression of the first two modes of the system and shown to be NI according to Lemma 1, is applied to the 20-mode system model known to be SNI by Property 1. The closed-loop system remains stable despite an increasing number of system modes. The aim is to demonstrate both the validity of Lemma 2 and the applicability of Corollary 1 to our problem, via stable simulation results obtained with the highest possible number of system modes.

We demonstrate the designed controller performances for impulsive disturbance which is realized as a 1.25 V impulsive signal applied to the PEA at t=0. The open-loop and the closed-loop system responses are given in Fig. 11. Based on the time-domain simulation results given in Figs. 10 and 11, we calculate the integral square error (ISE) of voltage from PES as the amount of vibration energy as given in Table 7. It is clearly seen that the PPFR controller provides better performance for both transient and steady-state responses as compared to the MMPPF controller.

Fig. 11
Responses of closed-loop systems controlled with PPFR and MMPPF under impulsive disturbance
Fig. 11
Responses of closed-loop systems controlled with PPFR and MMPPF under impulsive disturbance
Close modal
Table 7

ISE values for vibration energy

ControllerISE (periodic)ISE (impulsive)
PPFR0.34930.19
MMPPF0.66210.2542
ControllerISE (periodic)ISE (impulsive)
PPFR0.34930.19
MMPPF0.66210.2542

To evaluate the control effort of both PPFR and MMPPF controllers, the control signals are presented in Figs. 12 and 13 for suppressing periodic and impulsive disturbances, respectively. Also, the energy of the control signals in terms of ISE is provided in Table 8. Evaluating Tables 7 and 8 together, we observe that PPFR provides better vibration suppression for periodic disturbance signal with less control energy, while it requires more energy for better suppression of impulsive disturbance compared to MMPPF. Nevertheless, the differences between the energy consumptions of the controllers are not significantly high for both types of disturbances.

Fig. 12
PPFR and MMPPF control signals under periodic disturbance of sinusoidal signals with system resonant frequencies
Fig. 12
PPFR and MMPPF control signals under periodic disturbance of sinusoidal signals with system resonant frequencies
Close modal
Fig. 13
PPFR and MMPPF control signals under impulsive disturbance
Fig. 13
PPFR and MMPPF control signals under impulsive disturbance
Close modal
Table 8

ISE values for control energy

ControllerISE (periodic)ISE (impulsive)
PPFR20.330.2588
MMPPF20.390.2176
ControllerISE (periodic)ISE (impulsive)
PPFR20.330.2588
MMPPF20.390.2176

The characteristic slopes (38) for the first two resonance frequencies (ω1 and ω2) of the 20-mode system model are given in Table 9 in order to compare the robustness of the PPFR and MMPPF controllers against variations in the system's first two resonance frequencies. The robustness of PPFR compared to MMPPF is slightly worse for the first resonance frequency and slightly better for the second resonance frequency. The reduction in robustness of a controller with enhanced performance, i.e., tradeoff between robustness and performance, which we face with just the first resonance mode frequency for PPFR, is an expected fact. Considering the significant suppression enhancement with PPFR for the periodic disturbance with the resonance frequencies presented in Table 7, we conclude that the robustness results are in PPFR's favor.

Table 9

Robustness performance of controllers

Controllerκ1(ω1)κ2(ω2)
PPFR0.0068020.007865
MMPPF0.0058860.008935
Controllerκ1(ω1)κ2(ω2)
PPFR0.0068020.007865
MMPPF0.0058860.008935

7 Conclusion

A new lemma for NI characteristics of TDS of retarded and neutral type is proposed. A sufficient condition in terms of an LMI is provided. The lemma is utilized to ensure the stability of infinite-mode NI systems with time-delayed positive feedback. The truncated system model of the infinite-mode system is not needed to perform the stability analysis. The proposed analysis is verified over a flexible beam system controlled with a time-delay controller named PPFR which is proposed to enhance vibration suppression of flexible structures with a collocated PES–PEA pair. PPFR is parametrized effectively via the presented H-norm based optimization procedure. The parametrized controller performance is shown to be better via simulations as compared to a state-of-the-art work. Furthermore, the robustness analysis of the controller is performed. In some studies such as Refs. [70] and [71], it is shown that the usage of PES–PEA pair networks is more efficient to suppress or to estimate vibrations on flexible structures. In future work, we plan to extend the proposed approach in this paper to such networked, i.e., multi-agent, systems on flexible structures utilizing possibly the PPFR controller.

Data Availability Statement

The datasets generated and supporting the findings of this article are obtainable from the corresponding author upon reasonable request.

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