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Hopf bifurcations in a three-species food chain system with multiple delays

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Published/Copyright: April 26, 2017

Abstract

This paper is concerned with a three-species Lotka-Volterra food chain system with multiple delays. By linearizing the system at the positive equilibrium and analyzing the associated characteristic equation, the stability of the positive equilibrium and existence of Hopf bifurcations are investigated. Furthermore, the direction of bifurcations and the stability of bifurcating periodic solutions are determined by the normal form theory and the center manifold theorem for functional differential equations. Finally, some numerical simulations are carried out for illustrating the theoretical results.

MSC 2010: 34C23; 34C25

1 Introduction

The study on the dynamics of predator-prey system is one of the dominant subjects in ecology and mathematical ecology due to its universal existence and importance. As to our knowledge, delay differential equations exhibit much more complicated dynamics than ordinary differential equations since a time delay could cause a stable equilibrium to become unstable and cause the populations to fluctuate. Thus, time delays of one type or another have been incorporated into mathematical models of population dynamics due to maturation time, capturing time or other reasons. In the last decades, many authors have explored the dynamics of systems with time delay and many interesting results have been obtained [1-13].

However, there may be more species in a habitat and they can construct a food chain. Therefore, it is more realistic to consider a multiple-species predator-prey system. Recently, Baek and Lee [14] proposed the following three-species food chain model with the Lotka-Volterra functional response

dx(t)dt=x(t)(abx(t)cy(t)),dy(t)dt=y(t)(d1+c1x(t)e1z(t)),dz(t)dt=z(t)(d2+e2y(t)), (1)

where x(t), y(t), z(t) denote the population densities of the lowest-level prey, mid-level predator and top-level predator at time t, respectively. The constant a > 0 is called the intrinsic growth rate of the prey species; b > 0 measures the intraspecific competition of the prey; c1 > 0 and e2 > 0 represent the conversion rates of the lowest-level prey to the mid-level predator and the mid-level predator to the top-level predator, respectively; c1 > 0 and e1 > 0 measure the hunting of the mid-level predator to the lowest-level prey and the top-level predator to the mid-level predator; d1 > 0 and d2 > 0 denote the death rates of the mid-level and top-level predator, respectively.

In system (1), the gestation periods and maturation time of some species are all omitted. However, some species need to take time to have the ability to reproduce and capture food. Based on this fact, by incorporating time delays into the maturation time, Cui and Yan considered the following delayed differential system in [15]

dx(t)dt=x(t)(abx(t)cy(t)),dy(t)dt=y(t)(d1+c1x(t)e1z(tτ1)),dz(t)dt=z(t)(d2+e2y(tτ2)), (2)

where τ1≥0 denotes the time from birth to having the ability to predate for top-level predator and τ2 ≥ 0 represents the maturation time that the mid-level predator can be served as food for the top-level predator, respectively. Delayed models similar to (2) have been investigated widely by many authors and lots of interesting results have been obtained. For more details see [16-18].

In system (2), the author just considered the time for the top-level predator to have the ability to predate and the maturation time for the mid-level predator to be served as food for the top-level predator. But the time for the mid-level predator to have the ability to predate and the maturation time for the lowest-level prey to be served as food for the mid-level predator are omitted. Based on this fact, by incorporating delays into the above terms, we consider a more complicated system with multiple delay

dx(t)dt=x(t)(abx(t)cy(tτ1)),dy(t)dt=y(t)(d1+c1x(tτ2τ3)e1z(tτ2)),dz(t)dt=z(t)(d2+e2y(tτ1τ3)), (3)

where τ1≥0 and τ2≥0 denote the time from birth to having the ability to predate for the mid-level predator and the top-level predator. For a special case, we assume that τ2+τ3 and τ1+τ3 represent the maturation time for the lowest-level prey to be served as food for the mid-level predator and the maturation time for the mid-level predator to be served as food for the top-level predator, respectively. We address the question how the time delays that we incorporated affect the dynamical properties of the system (3). So the aim of this paper is to study the dynamical behaviors of the system (3), for which we investigate the stability and Hopf bifurcation of a three-species food chain system with multiple delays. We would like to mention that the bifurcation in a predator-prey system with a single or multiple delays had been investigated by many researchers [19-22]. However, to the best of our knowledge, few results for system (3) have been obtained. Therefore, the research of this case is worth considering.

2 Stability of positive equilibrium and existence of local Hopf bifurcations

For convenience, we introduce new variables x1(t) = x(t), y1(t) = y(tτ1), z1(t) = z(tτ1τ2) and assume that τ = τ1+τ2+τ3, so that system (3) can be written as the following system with a single delay:

dx1(t)dt=x1(t)(abx1(t)cy1(t)),dy1(t)dt=y1(t)(d1+c1x1(tτ)e1z(t)),dz1(t)dt=z1(t)(d2+e2y1(tτ)). (4)

It is easy to see that the system (3) has a unique positive equilibrium E:(x0,y0,z0) provided that the condition (H)ae2c1d2cc1d1be2>0

holds, where x0=ae2d2cbe2,y0=d2e2,z0=ae2c1d2cc1d1be2be1e2.

Let u~1(t)=x1(t)x0,u~2(t)=y1(t)y0,u~3(t)=z1(t)z0, and use relations abx0cy0=0,d1+c1x0e1z0=0,d2+e2y0=0, then system (4) can be rewritten as the following equivalent system

du~1(t)dt=(u~1(t)+x0)(bu~1(t)cu~2(t)),du~2(t)dt=(u~2(t)+y0)(c1u~1(tτ)e1u~3(t)),du~3(t)dt=(u~3(t)+z0)(e2u~2(tτ)). (5)

To study the stability of the equilibrium E*, it is sufficient to study the stability of the origin for system (5). The linearized system of system (5) at origin is

du~1(t)dt=bx0u~1(t)cx0u~2(t),du~2(t)dt=c1y0u~1(tτ)e1y0u~3(t),du~3(t)dt=e2z0u~2(tτ). (6)

The characteristic equation of system (6) is

λ3+Aeλτλ+Bλ2+Ceλτ+Deλτλ=0, (7)

where A=e1e2y0z0>0,B=bx0>0,C=be1e2x0y0z0>0,D=cc1x0y0>0.

Next, we will investigate the distribution of roots of Eq.(7). 0bviously, λ = 0 is not a root of Eq.(7). When τ = 0, the characteristic equation becomes

λ3+Bλ2+(A+D)λ+C=0. (8)

It can be seen that B > 0, B(A+D)−C > 0, and C > 0. Therefore, if follows from the Routh-Hurwitz criteria that all roots of (8) have negative real parts and thus the zero equilibrium of system (5) is asymptotically stable when τ = 0.

Now, we examine when the characteristic equation has pairs of purely imaginary roots. For τ > 0, if (ω > 0) is a root of Eq.(7), then ω should satisfy the following equations

(A+D)ωsin(ωτ)+Ccos(ωτ)=Bω2,Csin(ωτ)(A+D)ωcos(ωτ)=ω3. (9)

Thus

sin(ωτ)=(AB+BDC)ω3(A+D)2ω2+C2,cos(ωτ)=(A+D)ω4+BCω2(A+D)2ω2+C2.

Squaring and adding both the equations of (9), we have

(A+D)2ω8+[(AB+BD)2+C2]ω6+[B2C2(A+D)4]ω42C2(A+D)2ω2C4=0. (10)

Let z = ω2, a1=(AB+BD)2+C2(A+D)2,a2=B2C2(A+D)4(A+D)2,a3=2C2,a4=c4(A+D)2, then Eq. (10) becomes

h(z):=z4+a1z3+a2z2+a3z+a4=0.

Thus

dh(z)dz=4z3+3a1z2+2a2Z+a3:=4f(z),

where

f(z)=z3+34a1z2+12a2z+14a3.

Let m=8a23a1216,n=a134a1a2+8a332,D0=n24+m327. Similar to discussion in [24], assume that D0 > 0, then from the Cardano’s formula for the third-degree algebra equation we know that the equation f(z) = 0 had only one real root z1 . If D0 = 0, then the equation f(z) = 0 has three real roots z1, z2 and Z3 (where z2 = z3), and in this case we define z2 by max {z1, z2}. If D0 < 0, we know that the equation f(z) = 0 has three different real roots denoted by s1,s2 and s3. In this case,we define z3=max{s1,s2,s3}. According to Lemma 2.2 in [24], without loss of generality, we can suppose that Eq. (10) has four positive real roots, denoted by z1, z2, z3, z4, respectively. Then Eq. (9) should also have four positive real roots ω1=z1,ω2=z2,ω3=z3,ω4=z4. Define

τkj=1ωk[arctan((AB+BDC)ωk(A+D)ωk2+BC)+jπ],k=1,2,3,4.j=0,1,2, (11)

Then (τkj,ωk) are solutions of Eq.(7) and λ = ± i ωk are a pair of purely imaginary roots of Eq.(7) with τ=τkj. Define τ0=τk00=min1k4{τk0},ω0=ωk0, where k0∊ {1, 2, 3, 4}. Then τ0 is the first value of τ such that Eq.(7) has purely imaginary roots. In the following discussions, for the sake of convenience, we denoted τkj by τj(j = 0,1,2, …) for fixed k ∊ {1,2,3,4}. Let λ(τ) = α(τi ω(τ) be the root of Eq.(7) near τ = τj satisfying α(τj) = 0, ω(τj) = ω0(j = 0, 1, 2, …).

Lemma 2.1

dReλ(τ)dτ|τ=τj>0.

Proof

Differentiate the two sides of Eq. (7) with respect to τ. For the sake of simplicity, we denote τj and ω0 by τ, ω, respectively, then

(dλdτ)1=3λ2+Aeλτ+2Bλ+DeλτAλ2eλτ+Cλeλτ+Dλ2eλττλ=3λ2+Aeλτ+2Bλ+Deλτλ4Bλ3=τλ.

Thus

Re(dλdτ)1|λ=iω=Re[(3(iω)2+A(cos(ωτ)isin(ωτ))+2B(iω)+D(cos(ωτ)isin(ωτ))(iω)4B(iω)3τiω]=2(A+D)2ω8+(3C2+A2B2+2AB2D+B2D2)ω6+2B2C2ω4>0.

This completes the proof of Lemma 2.1.     □

Since the multiplicity of roots with positive real roots of Eq. (7) can change only if a root appears on or crosses the imaginary axis as time delay τ varies, similarly to Lemma 2.4 and Theorem 2.5 in [24], we have the following results

Theorem 2.2

Suppose that (H) hold, then the following statements are true.

  1. All roots of Eq. (7) have negative real parts and the E:(x0,y0,z0) of system (4) is absolutely stable, if a4 ≥ 0 and one of the following conditions is satisfied: (i) D0 > 0 and z1 ≤ 0, (ii)D0 = 0 and z2 ≤ 0, (iii) D0 < 0 and z3 ≤ 0;

  2. All roots of Eq. (9) have negative real parts and the E:(x0,y0,z0) of system (4) is asymptotically stable for τ ∈ [0, τ0), if a4 < 0 or a4 ≥ 0 and one of the following conditions is satisfied: (i) D0 > 0, z1 > 0 and h( z1 ) < 0, (ii) D0 = 0, z2 > 0 and h( z2 ) < 0, (iii) D0 < 0, z3 ≤ 0 and h( z3 ) < 0;

  3. τ = τj(j = 0,1,2, ⋯) are Hopf bifurcation values for system (4) if the conditions as stated in (II) are satisfied.

3 Direction of Hopf bifurcations and stability of bifurcating periodic solutions

In the previous section, we have already obtained that, under certain conditions, the system (4) can undergo Hopf bifurcation at the positive equilibrium E:(x0,y0,z0) when τ takes some critical values τ = τj, (j = 0, 1, 2, ⋯). In this section, by employing the normal form theory and center manifold theorem introduced by Hassard et al. [23], we shall present the formula determining the direction of the Hopf bifurcation and the stability of bifurcating periodic solutions of (4).

Let ui(t) = ũi(τ t), τ = τj + μ, μR, then μ = 0 is the Hopf bifurcation value for system (4), dropping the bars for simplification of notations, system (4) becomes the following functional differential equation in C = C([−1,0], R3),

u˙(t)=Lμ(ut)+f(μ,ut), (12)

where u(t) = (u1(t), u2(t), u3(t))TR3, and Lμ : CR3, f : R × CR3 are given by

Lμ(ϕ)=(τj+μ)MN000Q000ϕ1(0)ϕ2(0)ϕ3(0)+(τj+μ)000P000G0ϕ1(1)ϕ2(1)ϕ3(1), (13)

and

f(μ,ϕ)=(τj+μ)a11ϕ12(0)+a12ϕ1(0)ϕ2(0)a21ϕ1(1)ϕ2(0)+a22ϕ2(0)ϕ3(0)a31ϕ2(1)ϕ3(0), (14)

where

M=bx0,N=cx0,a11=b,a12=c,P=c1y0,Q=e1y0,a21=c1,a22=e1,G=e2z0,a31=e2.

By the Riesz representation theorem, there exists a function η(θ, μ) of bounded variation for θ ∈ [− 1, 0], such that

Lμ(ϕ)=10dη(θ,μ)ϕ(θ)forϕC. (15)

In fact, we can choose

η(θ,μ)=(τj+μ)MN000Q000δ(θ)+(τj+μ)000P000G0δ(θ+1), (16)

where δ is the Dirac delta function. For ϕC([− 1,0], R3), define

A(μ)ϕ=dϕ(θ)dθ,θ[1,0),10dη(s,μ)ϕ(s),θ=0,

and

R(μ)ϕ=0,θ[1,0),f(μ,ϕ),θ=0.

Then system (12) is equivalent to

u˙t=A(μ)ut+R(μ)ut, (17)

where ut(θ) = u(t + θ) for θ ∈ [− 1, 0]. For ψC1([0,1], (R3)*), define

Aψ(s)=dψ(s)ds,s(0,1],10ψ(t)dη(t,0),s=0,

and a bilinear inner product

ψ(s),ϕ(θ)=ψ¯(0)ϕ(0)10ξ=0θψ¯(ξθ)dη(θ)ϕ(ξ)dξ, (18)

where η(θ) = η(θ, 0). Then A(0) and A* are adjoint operators. By the discussion in section 2, we know that ±iω0τj are eigenvalues of A(0). Hence, they are also eigenvalues of A*. We first need to compute the eigenvectors of A(0) and A* corresponding to iω0τj and −iω0τj, respectively. Suppose q(θ) = (1, q1, q2)Teiω0τjθ is the eigenvector of A(0) corresponding to iω0τj, then A(0)q(0) = iω0τjq(0). From the definition of A(0) and (13), (15), (16) we have

τjMN000Q000q(0)+τj000P000G0q(1)=iω0τjq(0).

For q(− 1) = q(0)eiω0τj, then we obtain

q1=iω0MN,q2=G(iω0M)eiω0τjiω0N

Similarly, we can obtain the eigenvector q(s)=D(1,q1,q2)eiω0τjs of A* corresponding to −iω0τj, where

q1=iω0MPeiω0τj,q2=(iω0+M)Qiω0Peiω0τj.

In order to assure 〈q*(s), q(θ)〉 = 1, we need to determine the value of D. By (18), we have

q(s),q(θ)=q¯(0)q(0)10ξ=0θq¯(ξθ)dη(θ)q(ξ)dξ=D¯{1+q1q¯1+q2q¯2(1,q¯1,q¯2)10θeiω0τjθdη(θ)(1,q1,q2)T}=D¯{1+q1q¯1+q2q¯2+τj(Pq¯1+Gq1q¯2)eiω0τj}.

Therefore, we can choose D as

D=[1+q¯1q1+q¯2q2+τj(Pq1+Gq¯1q2)eiω0τj]1.

Next we will compute the coordinate to describe the center manifold C0 at μ = 0. Let ut be the solution of (17) when μ = 0. Define

z(t)=q,ut,W(t,θ)=ut(θ)2Re{z(t)q(θ)}. (19)

On the center manifold C0, we have

W(t,θ)=W(z(t),z¯(t),θ),

where

W(z(t),z¯(t),θ)=W20(θ)z22+W11(θ)zz¯+W02(θ)z¯22+. (20)

z and z¯ are local coordinates for center manifold C0 in the direction of q* and q¯ . Note that W is real if ut is real. We only consider real solutions for solutions utC0 of (17). Since μ = 0, we have

z˙(t)=iω0τjz+g(z,z¯), (21)

where

g(z,z¯)=q¯(0)f0(z,z¯)=g20z22+g11zz¯+g02z¯22+g21z2Z¯2+. (22)

Following from (19), (20), (14) and using the algorithms given in [23], we can get the coefficients which will be used to determine the important quantities

g20=2τjD¯(a11+a12q1+a21q¯1q1eiω0τj+a22q¯1q1q2+a31q¯2q1q2eiω0τj),g11=2τjD¯a11+2τjD¯a12Re{q1}+2τjD¯a21q¯1Re{q1eiω0τj}+2τjD¯a22q¯1Re{q1q¯2}+2τjD¯a31q¯2Re{q¯1q2eiω0τj},g02=2τjD¯(a11+a12q¯1+a21q¯1q¯1eiω0τj+a22q¯1q¯1q¯2+a31q¯2q¯1q¯2eiω0τj),g21=τjD¯(2a11+a12q¯1)W20(1)(0)+2τjD¯(2a11+a12q1)W11(1)(0)+2τjD¯(a12+a21q¯1eiω0τj+a22q¯1q2)W11(2)(0)+τjD¯(a12+a21q¯1eiω0τj+a22q¯1q¯2)W20(2)(0)+τjD¯a21q¯1q¯1W20(1)(1)+2τjD¯a21q¯1q1W11(1)(1)+2τjD¯(a22q¯1q1+a31q¯2q1eiω0τj)W11(3)(0)+τjD¯(a22q¯1q¯1+a31q¯2q¯1eiω0τj)W20(3)(0)+τjD¯a31q¯2q¯2W20(2)(1)+2τjD¯a31q¯2q2W11(2)(1), (23)

where

W20(θ)=ig20ω0τjq(0)eiω0τjθ+ig¯023ω0τjq¯(0)eiω0τjθ+E1e2iω0τjθ, (24)

W11(θ)=ig11ω0τjq(0)eiω0τjθ+ig¯11ω0τjq¯(0)eiω0τjθ+E2, (25)

and E1=(E1(1),E1(2),E1(3))T,E2=(E2(1),E2(2),E2(3))T are both constant vectors.

Similarly to the algorithms given in [25], we can obtain

E1(1)=2M1a11+a12q1N0a21q1eiω0τj+a22q1q22iω0Qa31q1q2eiω0τjGe2iω0τj2iω0,E1(2)=2M12iω0Ma11+a12q10Pe2iω0τja21q1eiω0τj.+a22q1q2Q0a31q1q2eiω0τj2iω0,E1(3)=2M12iω0MNa11+a12q1Pe2iω0τj2iω0a21q1eiω0τj+a22q1q20Ge2iω0τja31q1q2eiω0τj,

where

M1=2iω0MN0Pe2iω0τj2iω0Q0Ge2iω0τj2iω0.

Similarly, we get

E2(1)=1M22a11+a12(q1+q¯1)N0a21(q1eiω0τj+q¯1eiω0τj)+a22(q1q¯2+q¯1q2)0Qa31(q1q¯2eiω0τj˙+q¯1q2eiω0τj)G0,E2(2)=1M2M2a11+a12(q1+q¯1)0Pa21(q1eiω0τj+q¯1eiω0τj)+a22(q1q¯2+q¯1q2)Q0a31(q1q¯2eiω0τj+q¯1q2eiω0τj)0,E2(3)=1M2MN2a11+a12(q1+q¯1)P0a21(q1eiω0τj+q¯1eiω0τj)+a22(q1q¯2+q¯1q2)0Ga31(q1q¯2eiω0τj+q¯1q2eiω0τj),

where

M2=MN0P0Q0G0.

Thus, we can determine W20(θ) and W11(θ) from (24) and (25). Furthermore, we can compute g21 by (23). Thus we can compute the following values:

c1(0)=i2ω0τj(g20g112|g11|2|g02|23)+g212,μ2=Re{C1(0)}Re{dλ(τj)dτ},β2=2Re{C1(0)},T2=Im{C1(0)}+μ2Im{dλ(τj)dτ}ω0τj,(k=0,1,2,).

Theorem 3.1

  1. μ2 determines the direction of the Hopf bifurcation: if μ2 > 0(μ2 < 0), then the Hopf bifurcation is supercritical(subcritical) and the bifurcating periodic solutions exist for τ > τj(τ < τj);

  2. β2 determines the stability of the bifurcating periodic solutions: if β2 < 0(β2 > 0), then the bifurcating periodic solutions are stable(unstable);

  3. T2 determines the period of the bifurcating periodic solutions: if T2 > 0(T2 < 0), then the period increase (decrease).

4 Numerical simulations

In this section, we give some numerical simulations supporting our theoretical predictions. As an example, we consider the following system

dx(t)dt=x(t)(0.90.6x(t)0.6y(tτ1)),dy(t)dt=y(t)(0.6+0.9x(tτ2τ3)0.9z(tτ2)),dz(t)dt=z(t)(0.7+0.9y(tτ1τ3)), (26)

Obviously, the hypothesis (H) is satisfied because ae2c1d2cc1d1be2 = 0.027 > 0 and therefore system (3) has only one positive equilibrium E* : (0.7222222222, 0.7777777778, 0.05555555556). In addition, h(z) has the following form

h(z)=z4+0.1897872903z30.1140921027z20.0004600555558z4.622436920107. (27)

Theorem 4.1

The positive equilibrium E* : (0.7222222222, 0.7777777778, 0.05555555556) of system (26) is asymptotically stable when τ1 + τ2 + τ3 < τ0 = 1.966861973 while it is unstable when τ1 + τ2 + τ3 > τ0 = 1.966861973, and system (26) can undergo a Hopf bifurcation at the positive equilibrium E* : (0.7222222222, 0.7777777778, 0.05555555556) when τ1 + τ2 + τ3 passes through the critical values τj =1.966861973 + 0.5084240855 (j = 0,1,2,…) (see Figs. 1-8).

Figure 1 
The trajectory graph of system (26) in t − x plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).
Figure 1

The trajectory graph of system (26) in tx plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

Figure 2 
The trajectory graph of system (26) in t − y plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).
Figure 2

The trajectory graph of system (26) in ty plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

Figure 3 
The trajectory graph of system (26) in t − z plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) =  0.8, y(0) = 0.8, z(0) = 0.7).
Figure 3

The trajectory graph of system (26) in tz plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

Figure 4 
The phase graph of system (26) in x − y − z plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) =  0.8, y(0) = 0.8, z(0) = 0.7).
Figure 4

The phase graph of system (26) in xyz plane with τ1 = 0.5, τ2 = 0.4 and τ3 = 0.3. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

Figure 5 
The trajectory graph of system (26) in t − x plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) =  0.8, y(0) = 0.8, z(0) = 0.7).
Figure 5

The trajectory graph of system (26) in tx plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

Figure 6 
The trajectory graph of system (26) in t − y plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) =  0.8, y(0) = 0.8, z(0) = 0.7).
Figure 6

The trajectory graph of system (26) in ty plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

Figure 7 
The trajectory graph of system (26) in t − z plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) =  0.8, y(0) = 0.8, z(0) = 0.7).
Figure 7

The trajectory graph of system (26) in tz plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

Figure 8 
The phase graph of system (26) in x − y − z plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) =  0.8, y(0) = 0.8, z(0) = 0.7).
Figure 8

The phase graph of system (26) in xyz plane with τ1 = 0.9, τ2 = 0.7 and τ3 = 0.4. The initial value is (x(0) = 0.8, y(0) = 0.8, z(0) = 0.7).

  1. Competing interests

    The authors declare that they have no competing interests.

  2. Authors's contributions

    All authors contributed equally to the writing of this paper. All authors read and approved the final manuscript.

Acknowledgement

This paper was supported by the Natural Science Foundation of Hunan Province (Nos:2017JJ2130, 2017JJ3131), and Social Science Foundation of Hunan Province (No:16YBA243), and Key project of Education Department for Hunan Province.

The authors would like to thank the referees for their valuable suggestions and comments, which led to the improvement of the manuscript.

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Received: 2016-11-2
Accepted: 2017-2-7
Published Online: 2017-4-26

© 2017 Xie and Zhang

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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