# Delayed phenomenon of loss of stability of solutions in a second-order quasi-linear singularly perturbed boundary value problem with a turning point

- Zheyan Zhou
^{1}Email author and - Jianhe Shen
^{1}

**2011**:35

**DOI: **10.1186/1687-2770-2011-35

© Zhou and Shen; licensee Springer. 2011

**Received: **6 March 2011

**Accepted: **14 October 2011

**Published: **14 October 2011

## Abstract

Based on the method of differential inequalities, by constructing the upper ad lower solutions suitably, delayed phenomenon of loss of stability of solutions in a second-order quasi-linear singularly perturbed Dirichlet boundary value problem with a turning point is found in this paper. An illustrating example is performed to verify the obtained results.

### Keywords

Upper and lower solutions singular perturbation turning point delay of loss of stability## §1 Introduction

In real-world applications, there are numerous examples, from biology, chemistry, neurophysiology, fluid dynamics, automation, semiconductor laser, etc., are described in dynamical systems with singular perturbation. The process evolving more than one scale in time and/or space is a typical feature of such type of dynamical systems.

The studies of singular perturbation can be traced back to nineteenth century stimulated greatly by celestial mechanics at that time. The Lindstedt-Poincar*é* method could be regarded as the first invention to deal with the secular term problems, which is one of the two broad categories of singularly perturbed problems [1, 2]. Another broad category of singularly perturbed problems is the boundary layer problems [1, 2]. The idea of boundary layer was proposed by Prandtl in the setting of fluid dynamics and aerodynamics. Matching principle was an invention of Prandtl to obtain uniformly valid asymptotic solutions of boundary layer problems.

In the process of developing the theory of singular perturbation, Tikhonov's limit theory [3, 4] and Fenichel's geometric theory [5, 6] are two seminal works. Both the two theories tell us that the solutions of singularly perturbed problems tend to the stable solutions of the corresponding reduced problems with the small parameter approaching to zero under the normally hyperbolic condition. Since then, under this essential condition of normal hyperbolicity, the theory of singular perturbation finds applications in many problems including boundary value problems [7], existence of solitons [8], and biological models [9], etc.

However, there are many practical situations in which the normal hyperbolicity of the reduced solutions lose. That is, in geometrical speaking, there exist turning points on the critical curve. The existence of turning points leads to several new phenomena in singularly perturbed systems such as exchange of stability and delay of exchange of stability [10]. In general speaking, both exchange of stability and delay of exchange of stability have tight relationship with relaxation oscillations and the latter may lead to canards.

Delay of loss (or exchange) of stability is a typical characteristic of canards detected first in singularly perturbed systems before 30 years ago by the technique of nonstandard analysis [11]. Eckhaus [12] applied standard asymptotic analysis and found the canard phenomenon too. From then on, canard has been studied extensively and several methods including matching asymptotic expansion and blow-up, etc., have been developed. Nowadays, it has been well known that canards are not the exotic objects, but occur frequently in a great deal of real-world applications including chemical reactions [13] and neuron dynamics [14] and so on.

*x*= 0 is the turning point. Shchepakina et al. [17] gave also several systems for illustrating canards. However, as far as the authors know, there are rare contributions concerning canards in nonlinear singularly perturbed boundary value problems. In fact, the solution of a second-order linear two-point boundary value problem as follows, contained in the monograph of Kevorkian and Cole [1], is a canard,

in which, *x* = 0 is the turning point. This canard was approximated by matching asymptotic expansion with the aid of the variational approach.

*x*, 0 <

*ε*≪ 1 is a small parameter,

*a, b, A*, and

*B*are constants with

*a*< 0 <

*b*and

In other words, existence of canard solutions in boundary value problem (1-3) is obtained in this paper.

The paper is arranged as follows. In the next section, the asymptotic solution of (1-3) is constructed formally. The uniform validity and the error of the asymptotic solution are given in Section 3, which form the main results of the present paper. By the dynamical behavior of the asymptotic solution, we know that the solution of (1-3) approximated by this asymptotic solution has the feature of delay of loss of stability, i.e., it is a canard. In Section 4, an illustrating example is provided for verifying the correctness of the main results in the paper.

**Remark 1**. If the solution of boundary value problem (1-3) changes sign in the interval (*a, b*), then it is said that boundary value problem (1-3) has a turning point.

**Remark 2**. Although there have been many works concentrating on singularly perturbed problems with turning points, however, as far as the authors know, it seems so far that rare works are concerning with canard solutions in quasi-linear singularly perturbed boundary value problems.

## §2 Construction of the asymptotic solution

where *C* is a constant of integration to be determined and a particular solution *u*_{
p
} (*x*) ≡ 0.

Obviously, the trivial solution *u*_{
p
} (*x*) ≡ 0 is lack of attraction. Hence, in general, it is not reasonable to expect that there exist the solutions of (1-3) to be attracted by this particular solution.

On the other hand, by direct linear stability analysis, it can be seen that the solutions defined in (6) are attracted for *x* < *C* and repelled for *x* > *C*. Hence, *x* = *C* is viewed as a turning point, where *a* < *C* < *b* is assumed. However, in the next section, utilizing the method of upper and lower solutions, we will prove that there exists at least one solution of (1-3) tending to one of the family of solutions (6) on the whole interval (*a, b*) with *ε* → 0. This is the delayed phenomenon of loss of stability of solutions occurring particularly in singularly perturbed systems with turning points.

The solutions defined in (6) can be regarded as the outer solutions. Generally, they cannot satisfy the boundary conditions (2) and (3). Consequently, there will be two boundary layers at the ended points of the interval. Hence, for obtaining the uniformly valid asymptotic solution, corrections must be performed at the regions of boundary layers.

*ε*→ 0 in (7) yields

which is solvable. The solution of Equation (9) satisfying condition (8), denoted by *V*_{
L
} (*τ*_{1}), can be regarded as the zero-order approximation to the solution of (7) and (8). In other words, *V*_{
L
} (*τ*_{1}) is a zero-order approximation to the left boundary layer. Of course, at present, this zero-order approximation contains a constant to be determined by matching.

*P*≡ 0 which is discarded, and

where *C*_{1} is a nonzero constant of integration.

*a*

_{1}∈

*R*. Hence,

*C*

_{1}> 0 is meant. Consequently, Equation (12) can be rewritten as

where *M*_{1} > 0 is a constant of integration. There are two cases to be discussed.

*V*

_{ L }| > |

*a*

_{1}|. In this case, we have

*d*

_{1}is a constant determined by

*V*

_{ L }| < |

*a*

_{1}|. In this case,

where *d*_{1} is defined in Equation (15).

Obviously, it follows from Equations (14) and (16) that the function *V*_{
L
} (*τ*_{1}) given in cases I and II is, respectively, the monotone decreasing and increasing functions.

*a*

_{1}< 0, since

*a*

_{1}> 0, since

*a*

_{1}< 0 and

*a*

_{1}> 0 cases are possible for matching. Therefore, without loss of generality, the

*a*

_{1}> 0 case can be adopted. Consequently, we have the hyperbolic coth function

Both of them are possible to be the left boundary layer correction.

*τ*

_{1}= 0 in Equations (17) and (18) and taking Equation (8) into account, we obtain from (17) and (18), respectively, that

by which, the constant *M*_{1} is determined, i.e., equivalently, the constant *d*_{1} in (15) is determined. Till now, *V*_{
L
} (*τ*_{1}) defined in (17) and (18) have been determined completely.

*u*(

*b*) = -

*b*+

*C*< 0,

*d*

_{2}is a constant to be determined by the following equality

Similarly, the function *V*_{
R
} (*τ*_{2}) defined in Equations (21) and (22) is, respectively, the monotone decreasing and increasing functions.

by which, the constant *M*_{2}, i.e., the constant *d*_{2} is determined. Consequently, the function *V*_{
R
} (*τ*_{2}) in Equations (21) and (22) is completely known.

Now, it has been clearly known that, near the left- and right-ended points of the interval, there both have two candidates, possible to be the boundary layer corrections. Which pair of the hyperbolic functions in Equations (17-18) and (21-22) is chosen depending on the practical situations like the boundary conditions. In the following of the paper, we will show that the hyperbolic coth functions defined in Equations (17) and (21) must be selected to be the left and right boundary layer corrections, respectively.

in which, *u*(*t*), *V*_{
L
} (*τ*_{1}), and *V*_{
R
} (*τ*_{2}) are defined in Equations (6, 17), and (21), respectively, and the constant *C* in Equation (6) will be determined later. In the following section, based on the theory of differential inequalities, by constructing the upper and lower solutions suitably, we will prove that this asymptotic solution is uniformly valid with certain order. Consequently, by the dynamical behavior of the asymptotic solution (25), delay loss of stability of solution in (1-3) can be seen, i.e., existence of canard solutions in (1-3) is known and this canard is approximated uniformly by the asymptotic solution (25).

## §3 A lemma and the main results

To prove the main results of the current paper, the following lemma is needed.

**Lemma 1**[18] Consider second-order nonlinear boundary value problems with Dirichlet boundary conditions,

in which *a, b, A*, and *B* are constants.

- (1)there exist the upper and lower solutions, i.e., there are functions
*β*(*x*),*α*(*x*) ∈*C*^{2}[*a*,*b*] with*β*(*x*) ≥*α*(*x*) such that$\begin{array}{c}{\beta}^{\u2033}\le f\left(x,\beta ,{\beta}^{\prime}\right),\phantom{\rule{1em}{0ex}}x\in \left(a,b\right),\\ \beta \left(a\right)\ge A,\phantom{\rule{1em}{0ex}}\beta \left(b\right)\ge B\end{array}$

- (2)the function
*f*(*x, y, y*') satisfies the Nagumo condition with respect to*β*(*t*) and*α*(*t*), then there exists at least one solution*y*(*x*) ∈*C*^{2}[*a*,*b*] with the following estimate:$\alpha \left(x\right)\le y\left(x\right)\le \beta \left(x\right),\phantom{\rule{1em}{0ex}}x\in \left[a,b\right].$

Based on Lemma 1, we turn to prove the following theorems.

**Theorem 1**There exists at least one solution of boundary value problem (1-3) such that

*γ*is a positive constant,

*y*

_{asy}(

*x*,

*ε*) is given by Equation (25) in which

i.e., *C* = 0 in Equation (6) is determined.

By Theorem 1 and the dynamical behavior of *y*_{asy}(*x*, *ε*), the following Theorem 2 can be concluded directly.

**Theorem 2**There exist at least one solution of boundary value problem (1-3) with the following asymptotic behavior:

Theorems 1 and 2 together mean Theorem 3 as follows.

**Theorem 3** Boundary value problem (1-3) has at least one canard solution, whose zero-order approximation is given by Equation (25).

**Proof of Theorem 1**Define the upper and lower solutions as follows:

in which, *γ* is a positive constant.

Since the right-hand side function in Equation (1) satisfies the Nagumo condition, thus, to obtain Theorem 1, it is left to verify that the upper and lower solutions (31) and (32) satisfy the condition (1) in Lemma 1.

in which as well as in the following of the paper, the prime and the dot always denote the derivations with respect to the slow scale *x* and the fast scales *τ*_{1}, *τ*_{2}, respectively.

We want to prove that the quantity defined in Equation (30) is not positive. The proof is completed by dividing the interval [*a, b*] into five parts.

Part I. *x* ∈ [*a, a* + *δ*_{1}), where *δ*_{1} > 0 is a sufficiently small constant independent of *ε*.

*ε*sufficiently small, $O\left({e}^{-u\left(b\right)\frac{a-b}{\epsilon}}\right)$ denotes a quantity that is exponentially small and negative, and

which is a exponential small quantity too.

*a*+

*b*= 0 into account yields

*ε*sufficiently small, the sign of Equation (34) is determined by its first part, i.e.,

Consequently, when *x* = *a*, the quantity defined in (30) is negative if the inequality (36) holds and *ε* is sufficiently small. Hence, there exists a sufficiently small constant *δ*_{1} > 0 independent of *ε* such that the quantity defined in (30) is negative for *x* ∈ [*a, a* + *δ*_{1}).

Therefore, in what follows, *C* = 0 is set in Equation (6). Thus, *u*(*x*) = -*x* turns out to be the reduced solution.

Part II. *x* = 0.

*a*= -

*b*has been noted, which finally implies that

*x*= 0 in Equation (30), one gets

in which, *a* = -*b* and *M*_{1} = *M*_{2} have been taken into account. Thus, when *x* = 0, the inequality (29) holds.

Part III. *x* ∈ [*a* = *δ*_{1}, 0].

*x** ∈ (

*a*=

*δ*

_{1}, 0) such that

*ε*sufficiently small, since ${\dot{V}}_{L}$, ${\dot{V}}_{R}$ and

*V*

_{ L }+

*V*

_{ R }are exponentially small in this region, thus, it can be shown by direct calculations that

which is a contradiction.

Part IV. *x* ∈ (*b* - *δ*_{2}, *b*], where *δ*_{2} > 0 is a sufficiently small constant independent of *ε*.

In this region, the proof of the inequality (29) is parallel to Part I completely. Like the deductions of Equations (31-33), the values of ${V}_{L}\left({\tau}_{1}\right){|}_{x=b}$, ${\dot{V}}_{L}\left({\tau}_{1}\right){|}_{x=b}$, ${V}_{R}\left({\tau}_{2}\right){|}_{x=b}$, and ${\dot{V}}_{R}\left({\tau}_{2}\right){|}_{x=b}$ can be calculated. Consequently, we can see that, when *x* = *b*, the other parts in Equation (30) are the higher-order small quantities compared with its second part. Thus, the sign of Equation (30) is determined by its second part, which is a negative quantity. Accordingly, the inequality (29) is proved.

Part V. *x* ∈ (0, *b* - *δ*_{2},], In this region, the proof of the inequality (29) is parallel to Part III completely.

So far the proof of the differential inequality (29) has been finished for *x* ∈ [*a*, *b*]. In the same way, the differential inequality (37) can be proved.

*ε*sufficiently small, we have

in which, *u*(*a*) = -*a*, *u*(*b*) = -*b*, and *a* + *b* = 0 have been used.

and accordingly, Theorem 1 is derived.

**Remark 3**. From the proof of Theorem 1, we know that the construction of the upper and lower solutions defined in (27) and (28), respectively, is essential. The error term *x*^{4}*γε* introduced in (27) and (28) seems necessary for discussing the existence of canard solutions in singularly perturbed problems (1-3).

## § 4 An illustrating example

in which, the boundary points and the boundary values satisfy the conditions (4).

*M*

_{1}and

*M*

_{2}are, respectively, determined by

are derived.

*ε*. In the figure, the solid, dashing, and dotted lines represent, respectively, the reduced solution, the asymptotic solutions with

*ε*= 0.1 and

*ε*= 0.01. From this figure, we can see that

- (1)
delayed phenomenon of loss of stability of solutions really occurs, that is, existence of canards in this boundary value problem is verified. This canard solution is approximated by (43) with the accuracy of zero-order;

- (2)
with

*ε*→ 0, the asymptotic solution approaches more and more to the reduced solution in the whole interval (*a*,*b*). Therefore, the zero-order approximation is sufficiently accurate for the small*ε*.

## Declarations

## Authors’ Affiliations

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