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Dynamics and chaos control in a discrete-time ratio-dependent Holling-Tanner model

Journal of the Egyptian Mathematical Society volume 27, Article number: 48 (2019) Cite this article

Abstract

A discrete-time Holling-Tanner model with ratio-dependent functional response is examined. We show that the system experiences a flip bifurcation and Neimark-Sacker bifurcation or both together at positive fixed point in the interior of \(\mathbb {R}^{2}_{+}\) when one of the model parameter crosses its threshold value. We concentrate our attention to determine the existence conditions and direction of bifurcations via center manifold theory. To validate analytical results, numerical simulations are employed which include bifurcations, phase portraits, stable orbits, invariant closed circle, and attracting chaotic sets. In addition, the existence of chaos in the system is justified numerically by the sign of maximum Lyapunov exponents and fractal dimension. Finally, we control chaotic trajectories exists in the system by feedback control strategy.

Introduction

Mathematical modeling is a promising approach to understand and analyze the dynamics of ecological systems. In population ecology, the classical and significant studied theme is the interaction between predator and prey species. In recent year, the Leslie type predator-prey model has received more interest to investigate the dynamical behaviors between the species. The dynamic complexity of predator-prey system depends on predator’s functional response. Holling type II functional response is mostly used functional response among arthropod predators. The Leslie predator-prey model with Holling type II functional response is called Holling-Tanner model. A number of famous ecologist and mathematician have been given attention and investigated extensively Holling-Tanner models [1–3]. Their empirical works found complex dynamical behaviors including stable or unstable limit cycle, stability states around positive equilibrium. They showed that the asymptotic stability of the positive equilibrium does not imply the global stability. They also showed that the model may undergo the Bogdanov-Takens bifurcation and the subcritical Hopf bifurcation if parameters vary in a small vicinity of critical values. But Holling-Tanner models with ratio-dependent functional response (1) has been studied in [4]. The authors established the global stability conditions of the model near positive equilibrium with the help of Lyapunov function. It is also proved that the model (1) possess a unique stable limit cycle at the positive equilibrium showing coexistence of predator and prey in the sense of oscillatory balance behavior.

However, lots of exploratory works have recommend that if population size is small, or population generations are relatively discrete (nonoverlapping), or population changes within certain time intervals, one can consider the difference equation model rather than differential equation model to reveal chaotic dynamics [5–15]. These researches explored many complex properties including flip and Neimark-Sacker bifurcations, stable orbits and chaotic attractors which had been derived either by numerically or by normal form and center manifold theory.

Recently, a little works in literature studied discrete-time Holling-Tanner models [16–18] and its chaotic behaviors. For instance, a discrete-time Holling and Leslie type predator-prey system with constant-yield prey harvesting analyzed in [16], in [17] the authors investigated a discrete Holling-Tanner model and a discrete predator-prey model with modified Holling-Tanner functional response discussed in [18]. These studies paid their attention to determine the stability and directions of flip and Neimark-Sacker bifurcations via use of center manifold theory.

The following ratio-dependent Holling-Tanner model [4] is considered in this paper:

$$ \begin{array}{lcl} \dot{x} &=& rx \left(1-\frac{x}{K} \right)- \frac{mx}{x+Ay}y\\ \dot{y} &=& sy\left(1-h\frac{y}{x}\right) \end{array} $$
(1)

where x and y represent prey and predator population densities, respectively; r and s are the intrinsic growth rates of the prey and predator, respectively. K is the prey environment carrying capacity. The predator consumes prey according to the ratio-dependent Holling type II functional response \(\frac {mx}{x+Ay}\). The carrying capacity x/h of predator is proportional to the population size of the prey. The parameter h is the number of preys required to support predator births. m is the maximal predator per capita consumption rate; A is the number of prey necessary to achieve one-half of the maximum rate m; the constants r,K,A,m,s and, h all are being positive.

We introduce the new variables and parameters by the following scaling transformations:

$$\frac{x}{K} \rightarrow x, \frac{my}{rK} \rightarrow y, rt \rightarrow t \; \text{and}, \; a = \frac{rA}{m}, d = \frac{sh}{m}, b = \frac{m}{hr}.$$

Then, the system (1) becomes

$$ \begin{array}{lcl} \dot{x} &=& x \left(1-x \right)-\frac{xy}{x+ay}\\ \dot{y} &=& dy\left(b-\frac{y}{x}\right) \end{array} $$
(2)

To get following two-dimensional discrete system, forward Euler scheme with integral step size δ is applied to system (2):

$$ \left(\begin{array}{l} x \\ y \end{array}\right) \mapsto \left(\begin{array}{ll} x&+\delta x \left[ \left(1-x \right)-\frac{y}{x+ay} \right]\\ &y+\delta y \left[d\left(b-\frac{y}{x}\right) \right] \end{array}\right) $$
(3)

This study will mainly focus on how model parameters affect on the dynamics of system (3). Especially, we discuss systematically to show the existence condition of Flip bifurcation and Neimark-Sacker bifurcation using bifurcation theory and center manifold theory [19]. Because in the discrete predator-prey system, Flip bifurcation and Neimark-Sacker bifurcation both are the important mechanisms for the generation of complex dynamics and both bifurcations cause the system to jump from stable window to chaotic states through periodic and quasi-periodic states, and trigger a route to chaos.

The outlines of this paper is as follows. The existence condition for fixed points of system (3) in the interior of \(\mathbb {R}^{2}_{+}\) and their stability analysis are given in “Existence conditions and stability analysis of fixed points” section. In “Direction and stability analysis of bifurcation” section, we determine direction of bifurcation for system (3) under certain parametric condition. The bifurcation diagrams, phase portraits, maximum Lyapunov exponents, and Fractal dimensions are presented numerically in “Numerical simulations” section by changing one or more control parameters values. In “Controlling chaos” section, a feedback control technique has been used to stabilize unstable trajectories. A short conclusion is presented in the “Discussions” section.

Existence conditions and stability analysis of fixed points

To find fixed points of system (3), we set

$$ \left\{\begin{array}{lcl} x+\delta x \left[ \left(1-x \right)-\frac{y}{x+ay} \right] &=& x \\ y+\delta y \left[d\left(b-\frac{y}{x}\right) \right] &=& y \end{array}\right. $$
(4)

By solving system of non-linear Eqs. 4 we obtain the following result.

Lemma 1

For all feasible values of parameters, the system (3)

(i) always has axial fixed point E1(1,0),

(ii) has a unique coexistence fixed point E2(x∗,y∗) if b<1+ab where \(x^{*} = \frac {1-b+ab}{1+ab} \quad \text {and} \quad y^{*} = b x^{*}.\)

Next, we analyze local stability at each fixed points for system (3). The Jacobian matrix of system (3) around arbitrary fixed point E(x,y) is given by

$$ J(x,y)= \left(\begin{array}{ll} j_{11} & j_{12}\\ j_{21} & j_{22} \end{array}\right) $$
(5)

where

$$j_{11}=1+\delta \left(1-2x + \frac{xy}{(x + ay)^{2}} - \frac{y}{x + ay} \right), j_{12}=\delta \left(\frac{a xy}{(x + ay)^{2}} - \frac{x}{x + ay} \right) $$
$$j_{21}=\frac{d \delta y^{2}}{x^{2}}, j_{22}=1- \frac{d \delta y}{x} + d \delta \left(b-\frac{y}{x} \right). $$

The characteristic equation of matrix J is

$$ \lambda^{2} +p(x,y) \lambda +q(x,y)=0 $$
(6)

where p(x,y)=−trJ=−(j11+j22) and detJ=j11j22−j12j21.

Now, the topological classification of stability around fixed points by using Jury’s criterion [20] are expressed as follows.

Proposition 1

For predator free fixed point E1(1,0), the following topological classification true

(i) E1 is a saddle if 0<δ<2,

(ii) E1 is a source if δ>2,

(iii) E1 is a non-hyperbolic if δ=2.

Let

$$FB_{E_{1}} = \left\{(a, b, d, \delta): \delta =2, a, b, d>0 \right\}. $$

It is obvious that when parameters are in \(FB_{E_{1}}\), then one of the eigenvalues of J(E1): λ1=1−δ and λ2=1+bdδ is −1 and the other is not equal to ±1. Therefore, system (3) experience a flip bifurcation when parameters change in small vicinity of \(FB_{E_{1}}\).

At E2(x∗,y∗), the Eq. 6 becomes

$$F(\lambda):=\lambda^{2} - (2 + L \delta) \lambda +(1 + L \delta + M \delta^{2})=0, $$

where

$$\begin{aligned} L &= 1 + bd - 2 x^{*} - \frac{2 d y^{*}}{x^{*}} - \frac{a {y^{*}}^{2}}{\left(x^{*} + {a y^{*}}^{2}\right. } {,} \\ M &= d (b - 2b x^{*} + 4y^{*}) - \frac{2 d y^{*}}{x^{*}} - \frac{(2+ab) d {y^{*}}}{(x^{*} + a y^{*})^{2}} + \frac{(3x^{*}+2ay^{*}) d {y^{*}}^{2}}{x^{*} (x^{*} + a y^{*})^{2}}. \end{aligned} $$

Therefore, F(1)=Mδ2>0 and F(−1)=4+2Lδ+Mδ2.

For topological classification of E2, we state following Proposition.

Proposition 2

Suppose b<1+ab holds. Then for coexistence fixed point E2(x∗,y∗) of system (3), the following topological classification true

(i) E2 is a sink if one of the following conditions holds

(i.1) \(L^{2} - 4 M \geq 0 \;\; \text {and} \;\; \delta <\frac {- L - \sqrt {L^{2} - 4 M}}{M}\);

(i.2) \(L^{2} - 4 M<0 \;\; \text {and} \;\; \delta <- \frac {L}{M}\);

(ii) E2 is a source if one of the following conditions holds

(ii.1) \(L^{2} - 4 M \geq 0 \;\; \text {and} \;\; \delta >\frac {- L + \sqrt {L^{2} - 4 M}}{M}\);

(ii.2) \(L^{2} - 4 M<0 \;\; \text {and} \;\; \delta >- \frac {L}{M}\);

(iii) E2 is a non-hyperbolic if one of the following conditions holds

(iii.1) \(L^{2} - 4 M \geq 0 \;\; \text {and} \;\; \delta =\frac {- L \pm \sqrt {L^{2} - 4 M}}{M}\);

(iii.2) \(L^{2} - 4 M<0 \;\; \text {and} \;\; \delta =- \frac {L}{M}\);

(iv) E2 is a saddle if otherwise.

From Proposition 2, it can be easily seen that if condition (iii.1) holds then eigenvalues of J(E2) are λ1=−1 and λ2≠±1. If (iii.2) is true, then eigenvalues of J(E2) are complex having modulus one.

Let

$$FB^{1}_{E_{2}} = \left\{(a, b, d, \delta): \delta=\frac{- L - \sqrt{L^{2} - 4 M}}{M}, \; L^{2} - 4 M \geq0, a, b, d>0 \right\}, $$

or

$$FB^{2}_{E_{2}} = \left\{(a, b, d, \delta): \delta=\frac{- L + \sqrt{L^{2} - 4 M}}{M}, \; L^{2} - 4 M \geq0, a, b, d>0 \right\}. $$

Then system (3) experience a flip bifurcation at E2 when parameters (a,b,d,δ) vary in a small vicinity of either set \(FB^{1}_{E_{2}}\) or set \(FB^{2}_{E_{2}}\).

Also let

$${\text{NSB}}_{E_{2}} = \left\{(a, b, d, \delta): \delta=- \frac{L}{M}, \; L^{2} - 4 M<0, a, b, d>0 \right\},$$

then system (3) experience a NS bifurcation at E2 if the parameters (a,b,d,δ) change around the set \({\text {NSB}}_{E_{2}}\).

Direction and stability analysis of bifurcation

Here, we will pay attention to determine the direction and stability of flip bifurcation and Neimark-Sacker bifurcation of system (3) around E2 via application of center manifold theory [19]. The integral step size δ is being taken as a real bifurcation parameter.

Flip bifurcation: direction and stability

We take the parameters (a,α,β,δ) arbitrarily locate in \({\text {FB}}^{1}_{E_{2}}\). For other set \({\text {FB}}^{2}_{E_{2}}\), one can apply similar reasoning. Consider the system (3) at fixed point E2(x∗,y∗) with parameters lie in \({\text {FB}}^{1}_{E_{2}}\).

Let

$$\delta=\delta_{F}=\frac{- L - \sqrt{L^{2} - 4 M}}{M},$$

then the eigenvalues of J(E2) are

$$\lambda_{1}(\delta_{F})=-1 \;\; \text{and} \;\; \lambda_{2}(\delta_{F})=3 + L \delta_{F}.$$

In order for |λ2(δF)|≠1, we have

$$ L \delta_{F} \ne -2, -4. $$
(7)

Assume that \(\tilde {x}=x-x^{*}, \;\;\tilde {y}=y-y^{*}\), and set A(δ)=J(x∗,y∗). Then, we transform the fixed point (x∗,y∗) of system (3) to the origin. By Taylor expansion, system (3) can be written as

$$ \left(\begin{array}{l} \tilde{x} \\ \tilde{y} \end{array}\right) \rightarrow A(\delta) \left(\begin{array}{l} \tilde{x} \\ \tilde{y} \end{array}\right) + \left(\begin{array}{l} F_{1}(\tilde{x}, \tilde{y}, \delta) \\ F_{2}(\tilde{x}, \tilde{y}, \delta) \end{array}\right) $$
(8)

where \(X=(\tilde {x}, \tilde {y})^{T}\) is the vector of the transformed system and

$$ {\begin{aligned} F_{1}(\tilde{x}, \tilde{y}, \delta) &= \frac{1}{6} \left[-\frac{6 a \delta {y^{*}}^{2}}{(x^{*}+ay^{*})^{4}} \tilde{x}^{3} - \frac{6 a^{2} \delta {x^{*}}^{2}}{(x^{*}+ay^{*})^{4}} \tilde{x}^{3} - \frac{6a \delta y^{*}(-2x^{*} +a y^{*})}{(x^{*}+ay^{*})^{4}} \tilde{x}^{2} \tilde{y} + \frac{6a \delta x^{*}(-x^{*} + 2a y^{*})}{(x^{*}+ay^{*})^{4}} \tilde{x} \tilde{y}^{2} \right] \\ & + \frac{1}{2} \left[\delta \left(-2 - \frac{2x^{*} y^{*}}{(x^{*}+ay^{*})^{3}} + \frac{2y^{*}}{(x^{*}+ay^{*})^{2}} \right) \tilde{x}^{2} + \frac{2a \delta {x^{*}}^{2}}{(x^{*}+ay^{*})^{3}} \tilde{y}^{2} - \frac{4 a \delta x^{*} y^{*}}{(x^{*}+ay^{*})^{3}} \tilde{x} \tilde{y} \right] \\ & \qquad+ O(\|X\|^{4}) \\ F_{2}(\tilde{x}, \tilde{y}, \delta) &= \frac{d \delta}{{x^{*}}^{4}} \tilde{x} \left({x^{*} \tilde{y} - y^{*} \tilde{x}} \right)^{2} - \frac{d \delta}{{x^{*}}^{3}} \tilde{x} \left({x^{*} \tilde{y} - y^{*} \tilde{x}} \right)^{2} + O(\|X\|^{4}) \end{aligned}} $$
(9)

The system (8) can be expressed as \(X_{n+1}=AX_{n} + \frac {1}{2}B(X_{n},X_{n}) + \frac {1}{6}C(X_{n},X_{n},X_{n}) + O({X_{n}}^{4})\) where \( B(x, y) = \left (\begin {array}{l} B_{1}(x, y) \\ B_{2}(x, y) \end {array}\right) \) and \( C(x, y, u) = \left (\begin {array}{l} C_{1}(x, y, u) \\ C_{2}(x, y, u) \end {array}\right) \)are symmetric multi-linear vector functions of \(x, y, u \in \mathbb {R}^{2}\) and defined as follows:

$${\begin{aligned} B_{1}(x, y) & = \sum_{j, k=1}^{2} \left. \frac{\delta^{2} F_{1}(\xi, \delta)}{\delta \xi_{j} \delta \xi_{k}} \right|_{\xi=0}\; {x_{j} y_{k}} = -\frac{2a \delta x^{*}y^{*}}{(x^{*}+ay^{*})^{3}} ({x_{1} y_{2}} + {x_{2} y_{1}}) + \frac{2a \delta {x^{*}}^{2}}{(x^{*}+ay^{*})^{3}}{x_{2} y_{2}}\\ & \qquad + \delta \left(-2 - \frac{2x^{*} y^{*}}{(x^{*}+ay^{*})^{3}} + \frac{2y^{*}}{(x^{*}+ay^{*})^{2}} \right) {x_{1} y_{1}}, \\ B_{2}(x, y) & = \sum_{j, k=1}^{2} \left. \frac{\delta^{2} F_{2}(\xi, \delta)}{\delta \xi_{j} \delta \xi_{k}} \right|_{\xi=0}\; {x_{j} y_{k}} = - \frac{2 d \delta}{x^{*}} {x_{2} y_{2}} + \frac{2 d \delta y^{*}}{{x^{*}}^{2}} ({x_{1} y_{2}} + {x_{2} y_{1}}) - \frac{2 d \delta {y^{*}}^{2}}{{x^{*}}^{3}} {x_{1} y_{1}}, \end{aligned}} $$
$${\begin{aligned} C_{1}(x, y, u) & = \sum_{j, k, l=1}^{2} \left. \frac{\delta^{2} F_{1}(\xi, \delta)}{\delta \xi_{j} \delta \xi_{k} \delta \xi_{l}} \right|_{\xi=0}\; {x_{j} y_{k} u_{l}} = - \frac{6a \delta {y^{*}}^{2}}{(x^{*}+ay^{*})^{4}} {x_{1} y_{1} u_{1}} - \frac{6a^{2} \delta {x^{*}}^{2}}{(x^{*}+ay^{*})^{4}} {x_{2} y_{2} u_{2}}\\ & \qquad - \frac{2ay^{*} (-2x^{*} + ay^{*}) \delta}{(x^{*}+ay^{*})^{4}} (x_{1} y_{2} u_{1} + x_{2} y_{1} u_{1} + x_{1} y_{1} u_{2}) \\ & \qquad + \frac{2ax^{*} (-x^{*} + 2ay^{*}) \delta}{(x^{*}+ay^{*})^{4}} (x_{1} y_{2} u_{2} + x_{2} y_{1} u_{2} + x_{2} y_{2} u_{1}),\\ C_{2}(x, y, u) & = \sum_{j, k, l=1}^{2} \left. \frac{\delta^{2} F_{2}(\xi, \delta)}{\delta \xi_{j} \delta \xi_{k} \delta \xi_{l}} \right|_{\xi=0}\; {x_{j} y_{k} u_{l}} = \frac{2 d \delta}{{x^{*}}^{2}} (x_{1} y_{2} u_{2} + x_{2} y_{1} u_{2} + x_{2} y_{2} u_{1}) \\ & \qquad - \frac{4 d \delta {y^{*}}}{{x^{*}}^{3}} (x_{1} y_{1} u_{2} + x_{1} y_{2} u_{1} + x_{2} y_{1} u_{1}) + \frac{6 d \delta {y^{*}}^{2}}{{x^{*}}^{4}} {x_{1} y_{1} u_{1}}. \end{aligned}} $$

Let \(p, q \in \mathbb {R}^{2}\) be eigenvectors of A and transposed matrix AT respectively for λ1(δF)=−1 Then, we have

$$A(\delta_{F})q=-q \quad \text{and} \quad A^{T}(\delta_{F})p=-p.$$

Direct computation shows

$$\begin{array}{*{20}l} q & \sim \left(2 + bd \delta_{F} - \frac{2 d \delta_{F} {y^{*}}}{x^{*}}, - \frac{d \delta_{F} {y^{*}}^{2}}{{x^{*}}^{2}} \right)^{T}, \\ p & \sim \left(2 + bd \delta_{F} - \frac{2d \delta_{F} {y^{*}}}{x^{*}}, \frac{\delta_{F} {x^{*}}^{2}}{(x^{*}+ay^{*})^{2}} \right)^{T}. \end{array} $$

We use 〈p,q〉=p1q1+p2q2, standard scalar product in \(\mathbb {R}^{2}\) to normalize the vectors p and q. Setting the normalized vectors as

$$\begin{array}{*{20}l} q & = \left(2 + bd \delta_{F} - \frac{2 d \delta_{F} {y^{*}}}{x^{*}}, - \frac{d \delta_{F} {y^{*}}^{2}}{{x^{*}}^{2}} \right)^{T}, \\ p & = \gamma_{1} \left(2 + bd \delta_{F} - \frac{2d \delta_{F} {y^{*}}}{x^{*}}, \frac{\delta_{F} {x^{*}}^{2}}{(x^{*}+ay^{*})^{2}} \right)^{T}. \end{array} $$

where \(\gamma _{1} =\frac {1}{(2 + bd \delta _{F} - \frac {2d \delta _{F} {y^{*}}}{x^{*}})^{2} - \frac {d \delta ^{2}_{F} {y^{*}}^{2}}{(x^{*}+ay^{*})^{2}}}.\) We see that 〈p,q〉=1.

The sign of coefficient l1(δF) determines the direction of flip bifurcation and is computed by

$$ l_{1}(\delta_{F}) = \frac{1}{6} \langle p, C(q, q, q) \rangle - \frac{1}{2} \langle p, B(q, (A-I)^{-1} B(q, q)) \rangle $$
(10)

We summarize above discussion into the following theorem for direction and stability of flip bifurcation.

Theorem 1

Assume that (7) holds. Then, if l1(δF)≠0 and the parameter δ varies its value in a small vicinity of \(FB^{1}_{E_{2}}\), the system (3) experiences a flip bifurcation at positive fixed point E2(x∗,y∗). Moreover, if l1(δF)>0 (resp., l1(δF)<0), then there exists stable (resp., unstable) period-2 orbits bifurcate from E2(x∗,y∗).

Neimark-Sacker bifurcation: direction and stability

Next, we take the parameters (a,α,β,δ) arbitrarily located in \({\text {NSB}}_{E_{2}}\). Consider the system (3) at fixed point E2(x∗,y∗) with parameters vary in the vicinity of \({\text {NSB}}_{E_{2}}\). Then, the roots (eigenvalues) of Eq. 6 are pair of complex conjugate and given by

$$\lambda, \bar{\lambda}=\frac{-p(\delta) \pm i \sqrt{4q(\delta)-p(\delta)^{2}}}{2}=1 + \frac{L \delta}{2} \pm \frac{i \delta}{2} \sqrt{4M - L^{2}}.$$

Let

$$ \delta = \delta_{{\text{NS}}} =- \frac{L}{M} $$
(11)

Then, we have \(|\lambda |=\sqrt {q(\delta _{{\text {NS}}})}=1.\)

From the transversality condition, we get

$$ \frac{d|\lambda(\delta)|}{d\delta}|_{\delta = \delta_{{\text{NS}}}} =-\frac{L}{2} \ne 0 $$
(12)

Moreover, the nonresonance condition p(δNS)≠0,1 obviously satisfies

$$ \frac{L^{2}}{M}\ne 2, 3 $$
(13)

and we have

$$ \lambda^{k}(\delta_{{\text{NS}}}) \ne 1 \;\; \text{for} \; k=1, 2, 3, 4 $$
(14)

Let \(q, p \in \mathbb {C}^{2}\) be eigenvectors of A(δNS) and AT(δNS) for eigenvalues λ(δNS) and \(\bar {\lambda }(\delta _{{\text {NS}}})\) respectively such that

$$A(\delta_{{\text{NS}}}) q = \lambda(\delta_{{\text{NS}}}) q, \;\quad A(\delta_{{\text{NS}}}) \bar{q} = \bar{\lambda}(\delta_{{\text{NS}}}) \bar{q} $$

and

$$A^{T}(\delta_{{\text{NS}}}) p = \bar{\lambda}(\delta_{{\text{NS}}}) p, \;\quad A^{T}(\delta_{{\text{NS}}}) \bar{p} = \lambda(\delta_{{\text{NS}}}) \bar{p}. $$

By direct calculation, we obtain

$$\begin{array}{*{20}l} q & \sim \left(1 + bd \delta_{{\text{NS}}} - \frac{2d \delta_{{\text{NS}}} y^{*}}{x^{*}} - \lambda, - \frac{d \delta_{{\text{NS}}} {y^{*}}^{2}}{{x^{*}}^{2}} \right)^{T}, \\ p & \sim \left(1 + bd \delta_{{\text{NS}}} - \frac{2 d \delta_{{\text{NS}}} y^{*}}{x^{*}} - \bar{\lambda}, \frac{\delta_{{\text{NS}}} x^{*}}{(x^{*}+ay^{*})^{2}} \right)^{T}. \end{array} $$

For normalization of the vectors p and q, we set \(p = \gamma _{2} \left (1 + bd \delta _{{\text {NS}}} - \frac {2 d \delta _{{\text {NS}}} y^{*}}{x^{*}} - \bar {\lambda }, \frac {\delta _{{\text {NS}}} x^{*}}{(x^{*}+ay^{*})^{2}} \right)^{T}\) where

$$\gamma_{2} =\frac{1}{(1 + bd \delta_{{\text{NS}}} - \frac{2 d \delta_{{\text{NS}}} y^{*}}{x^{*}} - \bar{\lambda})^{2} - \frac{d \delta^{2}_{{\text{NS}}} {x^{*}}^{2} {y^{*}}^{2}}{x^{*}(x^{*}+ay^{*})^{2}}}.$$

Then we see that \(\langle p, q \rangle =\bar {p_{1}} q_{2} + \bar {p_{2}} q_{1}=1\).

When δ close to δNS and \(z \in \mathbb {C}\), the vector \(X \in \mathbb {R}^{2}\) can be decomposed uniquely as \(X = zq + \bar {z}\bar {q}\).

It is obvious that z=〈p,X〉. Thus, we obtain the following transformed form of system (8) for all sufficiently small |δ| near δNS:

$$z \mapsto \lambda(\delta)z + g(z, \bar{z}, \delta),$$

where λ(δ)=(1+φ(δ))eiθ(δ) with φ(δNS)=0 and \(g(z, \bar {z}, \delta)\) is a smooth complex-valued function. According to Taylor expression, the function g can be written as

$$g(z, \bar{z}, \delta) = \sum_{k+l \ge2} {\frac{1}{k! l!}} g_{kl}(\delta) z^{k} {\bar{z}}^{l}, \;\; \text{with} \;\; g_{kl} \in \mathbb{C}, \; k, l = 0, 1,\cdots.$$

By symmetric multi-linear vector functions, the Taylor coefficients gkl are obtained as

$$\begin{array}{*{20}l} g_{20}(\delta_{{\text{NS}}}) & = \langle p, B(q, q) \rangle,\\ g_{11}(\delta_{{\text{NS}}}) & = \langle p, B(q, \bar{q}) \rangle\\ g_{02}(\delta_{{\text{NS}}}) & = \langle p, B(\bar{q}, \bar{q}) \rangle,\\ g_{21}(\delta_{{\text{NS}}}) & = \langle p, C(q, q, \bar{q}) \rangle, \end{array} $$

The coefficient l2(δNS) which determines the direction of Neimark-Sacker bifurcation in a generic system exhibiting invariant closed curve can be calculated via

\(\phantom {\dot {i}\!}l_{2}(\delta _{{\text {NS}}}) = \text {Re} \left (\frac {e^{- i \theta (\delta _{{\text {NS}}})} g_{21}}{2} \right) - \text {Re} \left (\frac {(1-2e^{i \theta (\delta _{{\text {NS}}})}) e^{-2 i \theta (\delta _{{\text {NS}}})}}{2(1-e^{i \theta (\delta _{{\text {NS}}})})} g_{20} g_{11} \right) - \frac {1}{2} |g_{11}|^{2} - \frac {1}{4} |g_{02}|^{2},\) where \(\phantom {\dot {i}\!}e^{i \theta (\delta _{{\text {NS}}})} = \lambda (\delta _{{\text {NS}}})\).

Summarizing above analysis, we present the following theorem for direction and stability of Neimark-Sacker bifurcation.

Theorem 2

Suppose that (13) holds and l2(δNS)≠0. If the parameter δ varies its value in small neighborhood of \({\text {NSB}}_{E_{2}}\), then system (3) experiences a Neimark-Sacker bifurcation at positive fixed point E2. Moreover, if the sign of l2(δNS) is negative (resp., positive), then a unique invariant closed curve bifurcates from E2 which is attracting (resp., repelling) and the Neimark-Sacker bifurcation is supercritical (resp., subcritical).

Numerical simulations

In this section, numerical simulation are performed to validate our theoretical results, especially diagrams for bifurcation of system (3) at fixed point E2, phase portraits, maximum Lyapunov exponents and fractal dimension corresponding to bifurcation diagrams. For bifurcation analysis, we consider different sets for parameter values as given in Table 1 :

Table 1 Parameter values
Full size table

Example 1

Flip bifurcation with bifurcation parameter δ covering [ 2.6,3.86]

We set values of parameter as given in case (i). By calculation, we obtain a unique fixed point E2(0.75,0.75) of system (3). A flip bifurcation point is evaluated as δF=2.95569. It is observed that the system (3) experiences a flip bifurcation around E2 when δ passes its critical value δF. Also, at δ=δF the corresponding eigenvalues are λ1=− 1,λ2=0.672397,a(δF)=20.5735 and \((a, b, d, \delta) \in {\text {FB}}^{1}_{E_{2}}\). This shows the correctness of Theorem 1.

The bifurcation diagrams shown in Fig. 1a, b reveal that fixed point E2 is stable for δ<δF, loses its stability at δ=δF and for δ>δF there exists a period doubling phenomena leading to chaos. It is also seen that the period −2, −4, −8, and −16 orbits emerging for δ∈[ 2.6,3.668], chaotic set for δ∈[ 3.69,3.86] and the period −12 orbit occurs at δ=3.7924 which is in chaotic window δ∈[ 3.69,3.86] causing dynamic transition from periodic behaviors to chaos. The maximum Lyapunov exponents (MLE) and fractal dimension (FD) related to Fig. 1a, b are displayed in Fig. 1c, d which confirm stable, periodic, or chaotic states exists in system (3).

Fig. 1
figure1

Flip bifurcation of system (3). a Bifurcation in prey. b Bifurcation in predator. c Maximum Lyapunov exponents related to a, b. d FD corresponding to a. (x0,y0)=(0.74,0.74)

Full size image

Example 2

Neimark-Sacker (NS) bifurcation with bifurcation parameter δ covering [ 2.0,4.5]

With the variation of parameter a, the predator-prey system (3) exhibits much richer dynamics through the emergence of NS bifurcation. We take parameters as given in case (ii). After calculation, we find a unique fixed point E2(0.375,0.375) of system (3). A NS bifurcation point is obtained as δNS=2.25. It is seen that a NS bifurcation emerges around fixed point E2 when δ passes through δNS. Also, we have \(\lambda, \bar {\lambda }~=~0.905078~~\pm ~0.425245 i, g_{20} = 0.359863~+~0.156709 i, g_{11}~=~0.50625~-~0.499099 i, g_{02}~=~-~1.27625~+~0.58727 i, g_{21}~=~-~ 1.27332~+~1.64876 i, a(\delta _{{\text {NS}}})~=~-~0.742379\) and \((a, b, d, \delta) \in {\text {NSB}}_{E_{2}}\). The correctness of Theorem 2 is verified.

The bifurcation diagrams are depicted in Fig. 2a, b which illustrate that the fixed point E2 is stable for δ<δNS, loses its stability near δ=δNS and an attracting invariant closed cycle appears if δ>δNS. The maximum Lyapunov exponents related to Fig. 2a, b are disposed in Fig. 2c, which exhibits the existences of periodic orbits and chaos as parameter δ increases. These results indicate that NS bifurcation instigates a route to chaos, through a dynamic transition from a stable state, to invariant closed cycle, with periodic and quasi-periodic states occurring in between, to chaotic sets. For instance, chaotic set is observed when δ∼4.15 which is consistent with the sign of maximum Lyapunov exponent. Figure 2d is a local amplification of Fig. 2a for δ∈[ 3.5,4.0].

Fig. 2
figure2

NS bifurcation of system (3). a NS bifurcation in prey, b NS bifurcation in predator, c maximum Lyapunov exponents corresponding to a, b. d Local amplification diagram in a for δ∈[3.5,4.0].e FD associated with a. (x0,y0) = (0.37,0.37)

Full size image

Figure 3 explicitly shows that as the values of δ increases, there are alternation between periodic or quasi-periodic behaviors and invariant cycle or chaotic behavior. For different values of δ, phase portraits of system (3) associated with Fig. 2a, b are plotted in Fig. 3 illustrating the existence of period −10, −19, −38, and −9 orbits, and chaos in system (3) at δ∼3.6,δ∼3.9,δ∼3.95,δ∼4.075, and δ∼4.5, respectively.

Fig. 3
figure3

Phase portraits for different values of δ corresponding to Fig. 2a, b

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Example 3

Flip-NS bifurcation with bifurcation parameter a covering [ 0.6,3.0]

When we set the parameter values as in case (iii), a new bifurcation diagrams is obtained as plotted in Fig. 4. This illustrates that the predator-prey system (3) experiences Neimark-Sacker bifurcation and flip bifurcation both together when parameter a passes its critical value. The system firstly enters chaotic dynamics for small value of a. However, with the increase of a value, the chaotic dynamics of the predator-prey system suddenly disappear through a NS bifurcation occurring first at a∼0.691714, and then the system dynamics jump to a stable state. Thereafter, we find that the predator-prey system undergoes a flip bifurcation occurs at a∼1.92452 and then period doubling phenomena trigger a route to chaos. The maximum Lyapunov exponents (MLE) and fractal dimension (FD) related to Fig. 4a, b are displayed in Fig. 4c, d which confirm dynamic transition in system (3) from chaotic set to stable window and vice versa.

Fig. 4
figure4

NS-flip bifurcation of system (3). a Bifurcation for prey, b bifurcation for predator, c maximum Lyapunov exponents related to a, b. d FD associated with a. (x0,y0)=(0.37,0.37)

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Example 4

Bifurcation for parameters δ and a

Suppose parameters are considered as given in case (iv). When two more parameters change through its critical values, then system (3) can exhibit complex dynamic behavior. Under this parametric condition, the 3D bifurcation diagrams in (δ,a,x)-space are displayed in Fig. 5a. Figure 5b shows the 2D projected maximum Lyapunov exponents onto (δ,a) plane. It is now easy to determine values of bifurcation parameters to see how does the dynamics of system (3) change from non-chaotic state to periodic or chaotic state. For instance, unstable chaotic trajectories appear in the system for parameters δ = 4.15, a = 0.6 whereas stable trajectories appear for δ = 3.6, a = 0.6 (see Fig. 3), which are conformable with the signs presented in Fig. 5b. It is also remarkable from Fig. 5a that with the growth of parameter a, the predator-prey system (3) experiences NS bifurcation first and then flip bifurcation, and in between there is a stable window appears showing that the predator and prey coexist at a oscillatory balance behavior.

Fig. 5
figure5

Bifurcation diagram in (δ−a−x) space. (a) the transition between NS bifurcation and flip bifurcation for prey when δ∈[2.0,4.5], a = 0.6,1.0,1.5,2.0,2.5,3.0∈[0.6,3.0]. b The 2D projection of 3D maximum Lyapunov exponents onto (δ,a) plane. (x0,y0) = (0.37,0.37)

Full size image

Fractal dimension

In order to characterize the strange attractors exists in a system, one can measure fractal dimensions (FD) [21, 22] which is defined by

$$d_{L} = j + \frac{\sum_{i=1}^{j} h_{i}}{|h_{j}|} $$

where h1,h2,...,hn are Lyapunov exponents and j is the largest integer such that \(\sum _{i=1}^{j} h_{i} \ge 0\) and \(\sum _{i=1}^{j+1} h_{i} < 0\).

For system (3), the fractal dimension dL takes the form

$$d_{L} =1 + \frac{h_{1}}{|h_{2}|}, \quad h_{1}>0>h_{2} \quad \text{and} \quad h_{1}+h_{2}<0. $$

Considering parameter values as given in case (ii), FD of system (3) is plotted in Fig. 2e. The strange attractors of system (3) (see Fig. 3) and its corresponding FD (see Fig. 2e) confirms that growth of parameter δ causes a chaotic dynamics for the discrete-time ratio-dependent Holling-Tanner system.

Controlling chaos

We will apply state feedback control method [20] to control chaos exists in system (3) at the state of unstable trajectories. By adding a feedback control law as the control force un to system (3), the controlled system becomes

$$ \begin{aligned} x_{n+1} &=& x_{n}+\delta x_{n} \left[ \left(1-x_{n} \right)-\frac{y_{n}}{x_{n}+ay_{n}} \right] + u_{n} \\ y_{n+1} &=& y_{n}+\delta y_{n} \left[d\left(b-\frac{y_{n}}{x_{n}}\right) \right] \end{aligned} $$
(15)

and

$$u_{n} = -k_{1}(x_{n} - x^{*}) - k_{2}(y_{n} - y^{*}) $$

where the feedback gains are denoted by k1and k2 and (x∗,y∗) represent coexistence fixed point of system (3).

The Jacobian matrix Jc of the controlled system(15) is

$$ \begin{aligned} J_{c}(x^{*}, y^{*})= \left(\begin{array}{cc} j_{11}-k_{1} & j_{12}-k_{2} \\ \quad j_{21} & \quad j_{22} \end{array}\right) \end{aligned} $$
(16)

where \(j_{11}=1+\delta \left (1-2x + \frac {xy}{(x + ay)^{2}} - \frac {y}{x + ay} \right), j_{12}=\delta \left (\frac {a xy}{(x + ay)^{2}} - \frac {x}{x + ay} \right), j_{21}=\frac {d \delta y^{2}}{x^{2}}, j_{22}=1- \frac {d \delta y}{x} + d \delta \left (b-\frac {y}{x} \right)\) are evaluated at (x∗,y∗). The characteristic equation of Jc(x∗,y∗) is

$$ \lambda^{2}-(trJ_{c}) \lambda +detJ_{c}=0 $$
(17)

where

$$\begin{array}{*{20}l} trJ_{c} & = j_{11} + j_{22} - k_{1},\\ detJ_{c} & = j_{22}(j_{11} - k_{1}) - j_{21}(j_{12} - k_{2}). \end{array} $$

Let λ1 and λ2 be the roots of (17). Then,

$$ \lambda_{1} + \lambda_{2}=j_{11} + j_{22} - k_{1} $$
(18)

and

$$ \lambda_{1} \lambda_{2}= j_{22}(j_{11} - k_{1}) - j_{21}(j_{12} - k_{2}) $$
(19)

The solution of the equations λ1 = ± 1 and λ1λ2 = 1 determines the lines of marginal stability. These conditions confirm that |λ1,2| < 1. Suppose that λ1λ2=1, then from (19), we have

$$l_{1}: j_{22} k_{1}-j_{21} k_{2}=j_{11} j_{22}-j_{12} j_{21}-1.$$

Now assume that λ1=1, then from (18) and (19), we get

$$l_{2}: (1-j_{22}) k_{1}+j_{21} k_{2}=j_{11} + j_{22}-1-j_{11} j_{22}+j_{12} j_{21}.$$

Next, assume that λ1 = − 1, then from (18) and (19), we obtain

$$l_{3}: (1+j_{22}) k_{1}-j_{21} k_{2}=j_{11} + j_{22}+1+j_{11} j_{22}-j_{12} j_{21}.$$

Then, the lines l1,l2,and l3 (see Fig. 6a) in the (k1,k2) plane determine a triangular region which keeps |λ1,2|<1.

Fig. 6
figure6

Controlling chaos in system (15). a Stability region in (k1,k2) plane, (b, c). Time series for states x and y, respectively

Full size image

We have carried out numerical simulations to check how the implementation of feedback control method works and controls chaos at unstable state. Taking parameter values as in case (ii) with fixed δ = 2.126. We consider the feedback gains are as k1 = − 1.3 and k2=0.16 and initial value as (x0,y0)=(0.65,0.95). Region of stable eigenvalues in (k1,k2) plane is plotted in Fig. 6a. We numerically show that at the fixed point (0.662032,0.993048), the chaotic trajectory is stabilized, see Fig. 6b, c.

Discussions

This work is concerned with the dynamics and chaos control of a discrete-time ratio-dependent Holling-Tanner model in \(\mathbb {R}^{2}_{+}\). By the center manifold theory, we determine the existence condition and direction of flip and NS bifurcations of system (3) around coexistence fixed point. In particular, we show that system (3) experiences a flip or NS bifurcation at unique coexistence fixed point if parameter δ varies in the neighborhood of \({\text {FB}}^{1}_{E_{2}}\) or \({\text {NSB}}_{E_{2}}\). Based on Figs. 1 and 2, we notice that the small integral step size δ can stabilize the dynamical system (3), but the large integral step size may destabilize the system producing more complex dynamical behaviors. To see how does the integral step size play a key role in exploring the dynamical behaviors, we carry out numerical simulations to reveal unpredictable dynamics of the system including periods −2, −4, −8, −12, and −16 orbits via flip bifurcation and periods −9, −10, −19, and −38 orbits, invariant closed cycle, and chaotic sets via NS bifurcation, respectively. In addition, from Fig. 4, we can see that the appropriate choice of parameter a can stabilize the dynamical system (3). However, for the low or high values of a may destabilize system (3). Thus, with the increase of parameter a, it is shown that system (3) experiences NS and flip bifurcations both together. The two bifurcations cause the system to jump from steady state to chaotic dynamical behavior via periodic and quasi-periodic states and trigger routes to chaos, and vice-versa; that is, chaotic dynamics appear or disappear along with the emergence of bifurcations.

Moreover, in 3D bifurcation diagrams, we observe a dynamic transition between NS bifurcation and flip bifurcation. Through the two-dimensional parameter-spaces, we also notice that system dynamics can be periodic, quasi-periodic and chaotic. These complex dynamic behaviors of populations occurred by the flip and NS bifurcations can be explained ecologically, that is, the predator and prey population densities can fluctuate at regular or irregular intervals or the predator-prey system become unstable [23, 24]. We can also say that when the prey population are abundant, the consumption of prey by predator may have a marginal effect on the dynamics of prey. The presence of chaos is verified by the sign of maximum Lyapunov exponents and fractal dimension. Finally, we provide state feedback control method to control chaos at unstable trajectories. We would expect to explore more analytical results on multiple-parameter bifurcation of the system in future.

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Acknowledgements

The author would like to thank the editor and the referees for their valuable comments and suggestions, which led to the improvements of the paper.

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    Sarker Md. Sohel Rana

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Sohel Rana, S.M. Dynamics and chaos control in a discrete-time ratio-dependent Holling-Tanner model. J Egypt Math Soc 27, 48 (2019). https://doi.org/10.1186/s42787-019-0055-4

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Keywords

  • Holling-Tanner model
  • Ratio-dependent
  • Bifurcations
  • Chaos
  • Feedback control

MSC

  • (2010) 39A33
  • 37D45
  • 39A28
  • 92B05