# Exponential and polynomial stabilization of the Kirchhoff string by nonlinear boundary control

- Yuhu Wu
^{1}Email author and - Jianmin Wang
^{2}

**2013**:215

https://doi.org/10.1186/1687-2770-2013-215

© Wu and Wang; licensee Springer 2013

**Received: **22 April 2013

**Accepted: **6 August 2013

**Published: **21 October 2013

## Abstract

This paper addresses the stabilization problem of the nonlinear Kirchhoff string using nonlinear boundary control. Nonlinear boundary control is the negative feedback of the transverse velocity of the string at one end, which satisfies a polynomial-type constraint. Employing the multiplier method, we establish explicit exponential and polynomial stability for the Kirchhoff string. The theoretical results are assured by numerical results of the asymptotic behavior for the system.

## 1 Introduction

Stabilization and vibration controllability of string or beam systems arising from different engineering backgrounds has attracted attention of many researchers [1–4]. In particular, boundary feedback stabilization of string and beam systems has become an important research area [5–7]. This is because, in a practice system, vibration is more easily controlled through a boundary point than using point sensors or actuators away from the boundaries [8, 9].

which was proposed by Kirchhoff [10]. Here *l* is the length of the string; *E* is Young’s modulus of the material; *ρ* is density; *h* is the area of the cross section; $y(x,t)$ is the transversal displacement of the point *x* of the string at time *t*. This model has been studied by researchers from the physical and mathematical points of view; see, *e.g.*, references [11–13] and the references therein.

*t*. The boundary condition in equation (2) implies that the string is fixed at $x=0$. The boundary condition in equation (3) represents the balance of the transversal component of the tension in the string and the control input

*u*which is applied transversally at $x=1$. Because the tension in the string represented by equation (1) is not constant and is given by

*u*has a linear negative velocity feedback form

for all $t\ge 0$, where *L* is a positive constant. They established exponential stability. In [15], the absolute stability of the Kirchhoff string (1) with linear sector boundary control was considered. It is well known that linear strings represented by equation (1), for which $b=0$, can be stabilized by the control law in equation (6); see *e.g.*, references [16–18]. Moreover, Shahruz [19], Fung *et al.* [5], and Li and Hou [20] developed linear boundary control laws for axially moving strings. It is worth mentioning that Kobayashi [21] designed a linear parallel compensator based on boundary displacement observer and proved the string (1) can be stabilized by parallel compensator control.

In the literature mentioned above, such as [13, 16] and [20], the exponential stabilization result for various string systems by linear boundary control mainly relies on the Lyapunov direct method. In this work, we investigate the stabilization of string (1) with a more general and ‘flexible’ boundary control (see hypothesis (H) in Section 2). The feedback function *u* is not required to satisfy a strict control law such as (6), but just satisfies some appropriate polynomial-type constraint. In this general boundary control case, it seems that the Lyapunov direct method is no more applicable. So, we need to use a more meticulous method to deal with the stabilization problem. Applying the multiplier method, we establish not only exponential stability result but also polynomial stability result for Kirchhoff string (1).

The remainder of this technical paper is arranged as follows. Section 2 describes the model of the Kirchhoff nonlinear string and introduces the control assumption. The problem of exponential and polynomial stability is addressed in Section 3. Finally, a numerical example is demonstrated where the nonlinear distributed parameter infinite-dimensional equation is solved by applying the finite element method in Section 4.

## 2 Problem formulation

for all $x\in (0,1)$ and $t\ge 0$. Here $f(x)$ and $g(x)$ in equation (7d) are the initial displacement and velocity of the string, respectively. We assume that $f\in {C}^{1}[0,1]$, $g\in C[0,1]$ and that at least one of the functions *f* or *g* is not identically zero over $[0,1]$.

- (H)There exist constants ${L}_{2}\ge {L}_{1}>0$ and $r\ge 1$ such that$u(w)\in \overline{\mathrm{\Omega}}(w):=\{\begin{array}{ll}-Co\{{L}_{1}w,{L}_{2}w\},& |w|>1,\\ -Co\{{L}_{1}{w}^{r},{L}_{2}{w}^{\frac{1}{r}}\},& |w|\le 1.\end{array}$(8)

**Remark 2.1**Obviously, condition (H) is equivalent to, for all $w\in R$,

*u*to vary in an appropriate geometric region given by a polynomial-type constraint. For example, Figure 2 illustrates a feedback control

*u*satisfying a linear sector constraint (H) with $r=1$, ${L}_{1}=1$, ${L}_{2}=2$, and Figure 3 shows a feedback control

*u*satisfying a nonlinear constraint (H) with $r=2$, ${L}_{1}=1$, ${L}_{2}=2$. Since $u({y}_{t}(1,t)){y}_{t}(1,t)\le 0$, for all $t\ge 0$, the boundary control (7c) is the negative feedback of transversal velocity of the string at $x=1$.

For the existence and uniqueness of the solution of the general Kirchhoff equation, we refer to [11, 12] and references therein. In this work, we study the stabilization of the string in (7a) by this negative feedback boundary control *u*, which provides a dissipative effect.

**Remark 2.2**According to boundary condition (7b) at $x=0$, we easily get

*E*is defined as

Since at least one of the functions *f* and *g* is not identically zero over $(0,1)$ we have $E(0)>0$.

## 3 Stabilization by boundary control

In this section we state and prove our main result. For this purpose we establish several lemmas.

**Lemma 3.1**

*Let*$y(\cdot ,\cdot )$

*be the solution for system*(7a)-(7d).

*Then*

*Proof* See the Appendix. □

Now, we give a property of the energy function *E*.

**Proposition 3.1**

*The time*-

*derivative of the energy function*

*E*

*in equation*(10),

*along the solution of system*(7a)-(7d)

*satisfies*

*for all* $t\ge 0$.

*Proof*Differentiating the energy function (10) with respect to

*t*, we get

for all $t\ge 0$. We obtain equation (14). □

**Remark 3.1**From Proposition 3.1, we obtain the energy identity for system (7a)-(7d),

Therefore, the energy *E* is a decreasing function of time.

During the subsequent stability analysis, we utilize the following inequality.

**Lemma 3.2**

*Let*$y(\cdot ,\cdot )$

*be the solution for system*(7a)-(7d).

*Then*

*for all* $t\ge 0$.

*Proof*Applying the Cauchy-Schwarz inequality, we get

Together with (19) and (20), we get equation (18). Hence we complete the proof of Lemma 3.2. □

Now, we present a Gronwall-type lemma (see Komornik [22], pp.124), which will play an essential role when establishing the stabilization result.

**Lemma 3.3**

*Let*$G:{R}_{+}\to {R}_{+}$

*be a non*-

*increasing function*.

*Assume that there exists a constant*$\omega >0$

*such that*

*Then the following estimation is true*,

*for all*$t\ge 0$,

We give *a priori* estimation for the energy function $E(t)$, which was established in [15]. For the sake of completeness, we give the proof here.

**Lemma 3.4**

*The energy function*

*E*

*in equation*(10),

*along the solution of system*(7a)-(7d),

*satisfies*

*for all* $t\ge 0$.

*Proof*We multiply equation (7a) by $x{y}_{x}(x,t)$ and do integration over $[0,1]$, with respect to

*x*. We obtain

Since $\frac{b}{4}{[{\int}_{0}^{1}{y}_{x}^{2}\phantom{\rule{0.2em}{0ex}}dx]}^{2}\ge 0$, we complete the proof of Lemma 3.4. □

**Lemma 3.5**

*For any constant*$q\ge 0$,

*the energy function*

*E*

*along the solution of system*(7a)-(7d)

*satisfies the following estimation*,

*for all*$S>T\ge 0$,

*where* ${C}_{1}=\frac{3q+2}{q+1}max\{1,\frac{1}{a}\}$.

*Proof*According to inequality (21) in Lemma 3.4, we have, for all $0\le T<S$,

Finally, inserting the two inequalities, (28) and (29), in (27), we get inequality (25). This completes the proof of Lemma 3.5. □

We now state the main stabilization result for system (7a)-(7d).

**Theorem 3.1**

*Assume that assumption*(H)

*holds*.

*Then there exist three constants*${k}_{1},{k}_{2},\sigma >0$

*such that*,

*for all*$t\ge 0$,

**Remark 3.2** It is worth to mention that Theorem 2.4 in [13] can be viewed as a special cases of Theorem 3.1. Indeed, in the linear control case (6), the exponential stability in Theorem 3.1 coincides with the result in [13].

*Proof of Theorem 3.1* We distinguish two cases related to the parameter *r* to establish the energy decay rate.

Case (I): $r=1$;

Case (II): $r>1$.

where ${C}_{2}={C}_{1}+\frac{1}{2}(\frac{1}{{L}_{1}}+\frac{{L}_{2}}{a})$ and ${C}_{1}$ is given in Lemma 3.5.

Now we deal with Case (II). In this case, we choose $q=\frac{r-1}{2}>0$. We first admit the following fact (the proof is given in the Appendix).

**Claim 1**

*For any*$\delta >0$,

*we have the following estimates*,

*for all*$S>T\ge 0$,

where the last inequality follows from Remark 3.1. Finally, by letting $S\to +\mathrm{\infty}$ in (31), (35) and using Lemma 3.3 with $G(t)=E(t)$, we complete the proof of Theorem 3.1. □

**Remark 3.3** According to the proof of Theorem 3.1, it is easy to see that the constants *σ*, ${k}_{1}$ and ${k}_{2}$ in Theorem 3.1 can be chosen as, respectively, ${\sigma}^{-1}=2max\{1,\frac{1}{a}\}+\frac{1}{2}(\frac{1}{{L}_{1}}+\frac{{L}_{2}}{a})$, ${k}_{1}=eE(0)$, and ${k}_{2}=E(0){[2\frac{r+1}{r-1}({C}_{3}{E}^{\frac{r-1}{2}}(0)+{C}_{4})]}^{\frac{2}{r-1}}$ with ${C}_{3}=\frac{3r-1}{r+1}max\{1,\frac{1}{a}\}+\frac{a+{L}_{1}{L}_{2}}{a(r+1){L}_{1}}$, ${C}_{4}=\frac{1}{r+1}(\frac{1}{{L}_{1}}+\frac{{L}_{2}^{r}}{a}){[(1+\frac{1}{a})\frac{r-1}{r+1}]}^{\frac{r-1}{2}}$. This means that the coefficients of the exponential or polynomial decay rate are exactly determined only by the initial tension *a*, the initial energy $E(0)$ and the feedback control *u*. However, in the polynomial decay case, the order of decay rate is determined only by the feedback control *u*.

Finally, it is shown that the boundary control *u* stabilizes the nonlinear Kirchhoff string.

**Theorem 3.2**

*Assume that assumption*(H)

*holds*.

*Then there exist two constants*${k}_{1}^{\prime},{k}_{2}^{\prime}>0$

*such that for all*$x\in (0,1)$

*and*$t\ge 0$,

*where* ${k}_{1}^{\prime}=\sqrt{\frac{2{k}_{1}}{a}}$, ${k}_{2}^{\prime}=\sqrt{\frac{2{k}_{2}}{a}}$ *and* ${k}_{1}$, ${k}_{2}$, *σ* *are given in Theorem * 3.1.

*Proof*According to the fact that ${y}_{x}(0,t)=0$, for all $t\ge 0$, we get

for all $x\in (0,1)$ and $t\ge 0$. By combining (37) with (30) in Theorem 3.1, we complete the proof of Theorem 3.2. □

## 4 Numerical results

From Figures 4 and 5, it can bee seen that, in the case of control law ${u}_{2}$, the decay of the transverse vibration relatively slow compared to the case of control law ${u}_{1}$. Indeed, from Figure 6 and Figure 7, we know that in the case of control law ${u}_{1}$, the transverse vibration has been suppressed exponentially ($|y(0.5,t)|\le {K}_{2}{e}^{-\sigma t}$), whereas in the case of control law ${u}_{2}$, the transverse vibration has been suppressed polynomially ($|y(0.5,t)|\le {K}_{3}{t}^{-1}$). It is coincident with the results of Theorem 3.2.

## Appendix

### A.1 Proof of Lemma 3.1

for all $t\ge 0$. Substituting equation (40) into equation (39), we obtain equation (13). Thus the proof of Lemma 3.1 is complete.

### A.2 Proof of Claim 1

Inserting (47) into (46), we get inequality (33) in Claim 1.

## Declarations

### Acknowledgements

This work is supported by the National Natural Science Foundation of China (Grant 11226128) and the Natural Science Foundation of Heilongjiang Province of China (Grant F201113).

## Authors’ Affiliations

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