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Catalytic hydrothermal liquefaction (HTL) of biomass for bio-crude production using Ni/HZSM-5 catalysts

  • Received: 01 December 2016 Accepted: 12 April 2017 Published: 20 April 2017
  • Hydrothermal liquefaction (HTL) is an effective method that can convert biomass into bio-crude, but direct use of bio-crude derived from biomass HTL remains a challenge due to the lower quality. In this study, bifunctional Ni/HZSM-5 catalysts and zinc hydrolysis were combined to produce upgraded bio-crude in an in-situ HTL process. The K2CO3 and HZSM-5 catalysts with different Ni loading ratios were tested. The effects of different catalysts on the yield and quality of bio-crude and gas were investigated. The results indicated that the catalysts improved bio-crude and gas yields, compared to pine sawdust liquefaction without catalyst. The catalysts reduced the contents of undesirable oxygenated compounds such as acids, ketones, phenols, alcohols and esters in bio-crude products while increased desirable hydrocarbons content. K2CO3 produced highest bio-crude yield and lowest solid residue yield among all catalysts. Compared to parent HZSM-5 catalyst, bifunctional Ni/HZSM-5 catalysts exhibited higher catalyst activity to improve quality of upgraded bio-crude due to its integration of cracking and hydrodeoxygenation reactions. 6%Ni/HZSM-5 catalyst produced the bio-crude with the highest hydrocarbons content at 11.02%. This catalyst can be a candidate for bio-crude production from biomass HTL.

    Citation: Shouyun Cheng, Lin Wei, Mustafa Alsowij, Fletcher Corbin, Eric Boakye, Zhengrong Gu, Douglas Raynie. Catalytic hydrothermal liquefaction (HTL) of biomass for bio-crude production using Ni/HZSM-5 catalysts[J]. AIMS Environmental Science, 2017, 4(3): 417-430. doi: 10.3934/environsci.2017.3.417

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  • Hydrothermal liquefaction (HTL) is an effective method that can convert biomass into bio-crude, but direct use of bio-crude derived from biomass HTL remains a challenge due to the lower quality. In this study, bifunctional Ni/HZSM-5 catalysts and zinc hydrolysis were combined to produce upgraded bio-crude in an in-situ HTL process. The K2CO3 and HZSM-5 catalysts with different Ni loading ratios were tested. The effects of different catalysts on the yield and quality of bio-crude and gas were investigated. The results indicated that the catalysts improved bio-crude and gas yields, compared to pine sawdust liquefaction without catalyst. The catalysts reduced the contents of undesirable oxygenated compounds such as acids, ketones, phenols, alcohols and esters in bio-crude products while increased desirable hydrocarbons content. K2CO3 produced highest bio-crude yield and lowest solid residue yield among all catalysts. Compared to parent HZSM-5 catalyst, bifunctional Ni/HZSM-5 catalysts exhibited higher catalyst activity to improve quality of upgraded bio-crude due to its integration of cracking and hydrodeoxygenation reactions. 6%Ni/HZSM-5 catalyst produced the bio-crude with the highest hydrocarbons content at 11.02%. This catalyst can be a candidate for bio-crude production from biomass HTL.


    There are some relationships between species such as predation, competition, mutualism and parasitism, while predation is a popular representative in ecosystem. Since Lotka [1] and Volterra [2] almost simultaneously proposed the Lotka-Volterra model of predation between two populations, many scholars have studied the dynamics of different types of predator-prey models (see [3,4,5,6]). They usually consider the response of the predator to the prey density changing through a functional response in the modelling of predator-prey model. A variety of models are generated due to the selection of different types of functional response functions. Holling type Ⅰ, Ⅱ and Ⅲ [7,8,9] were first proposed by Holling based on empirical field data from 1959 to 1966. The traditional predator-prey models assumed that the functional response depends only on the prey populations [10,11,12]. However, several biologists questioned functional response is determined solely by prey density. They suggested that predators might interfere with each other's foraging because predators share or compete for food with each other when predatos forage. Therefore, the functional response should depend not only on the prey density but also on the predator, see for instance [13,14,15,16,17,18,19,20,21,22]. The authors considered that the growth of population is on slow time scale (days or months) and established the ratio-dependent model. By virtue of Holling type Ⅱ function, Kesh et al.[19] proposed a ratio-dependent model and obtained the sufficient condition for permanent co-existence. Xu and Chen [20] and Tang and Chen [21] studied the local and global stability of two classes of ratio-dependent system with delay, respectively. Fan and Li [22] proposed a delayed discrete ratio-dependent model and obtained the sufficient conditions for the permanence.

    The study on providing additional food for the predator is an important topic in ecological modeling, which leads to more complex dynamics for the predator-prey model and has received extensive attentions. In recent years, many scholars have focused on the work of providing additional food for the predator to protect species or control pest, for details to see references [23,24,25,26]. Assuming that the quality of the additional food remains constant, Srinivasu and Prasad [23] found that the growth of the predator could be enhanced by the provision of extra food for the predator. Basheer et al. [24] showed that providing extra food for the predator is effective in eliminating pests. Samaddar [25] and Wu [26] investigated the Hopf bifurcation of the model which took into account the provision of extra food for the predator and time delay.

    Motivated by the view of Arditi and Ginzburg [27] and Srinivasu et al. [28], a ratio-dependent model which involves the assumption that the additional food is provided for the predator was first proposed by Kumar and Chakrabarty [29]. This extra food is considered to be available uniformly within the ecological domain [28]. The model is as follows

    {dNdT=rN(1NK)e1(NP)1+e1h1(NP)+e2h2(AP)P,dPdT=n1e1(NP)+n2e2(AP)1+e1h1(NP)+e2h2(AP)PmP. (1.1)

    Where A is the additional food for the predator, the number of preys and predators at time T is respectively represented by N(T) and P(T), here N(0)>0,P(0)>0. The intrinsic growth rate of the prey is expressed by r and m stands for natural mortality of the predator, the carrying capacity of the prey is described by K. e1 and e2 denote the coefficients of predator capture on prey and additional food, n1 and n2 represent separately the nutritional value of the prey and additional food, h1 and h2 are handling time per predator per unit of the ratio NP prey biomass and per predator per unit of the ratio AP additional food biomass, respectively.

    Another important aspect, the real ecosystem could not be denied the fact that the processes of biological development are not normally instantaneous on account of the interaction with environment or other species. Therefore, several biologists and mathematicians began to explore and study the time-delay models inspired by the dynamics of population models with time delay. From the biological and mathematical point of view, predator-prey models with delay [30,31,32,33,34,35] tend to exhibit more complex dynamics than those without that, such as local and global stability, Hopf bifurcation, limit cycle and so on. For example, the properties of the periodic solutions of the model with delay and impulse were obtained in [31]. Jiang [34] investigated the global asymptotical and the existence of Hopf bifurcation of a diffusive model with ratio-dependent function and delay. By studying the delay differential system, Tang and Zhang [35] showed that the stability of the model becomes unstable state when the time reaches a certain critical point, thus Hopf bifurcation occurs. Considering the maturation time of the prey, model (1.1) turns to the following version

    {dNdT=rN(1N(Tτ)K)e1(NP)1+e1h1(NP)+e2h2(AP)P,dPdT=n1e1(NP)+n2e2(AP)1+e1h1(NP)+e2h2(AP)PmP. (1.2)

    It is widely known that human survival and development depend on natural resources. Biological resources have the most unique development mechanism due to renewability. Over-exploitation of biological resources will not only lead to a reduction in their quantity and quality, but also may drive species to extinction. Thus, taking the path of sustainable development becomes necessary to maintain ecological balance and meets the material needs of the people. From an economic perspective, the impact of harvesting effort on ecosystem guarantees that the net economic revenue is equal to the difference between total revenue and total cost which may influence on the harvesting activities. There has been a growing literature for the modeling and analysis of bioeconomic systems. The existence of steady state was discussed in a bioeconomic model with ratio-dependent [36]. The dynamics of the delay and diffusion terms of a bioeconomic plankton model was investigated by Zhao et al. [37]. In particular, an increasing number of bioeconomic models are expressed by differential-algebraic equations [38,39,40,41,42,43,44]. A prey-predator economic model with time-delay and stage structure was proposed by Zhang et al. [38]. Through detailed proof, the results show that the model undergoes three different bifurcational phenomena. Chen [41] established a biological economic model which suggested that the model undergoes flip bifurcation and Neimark-Sacker bifurcation.

    To extend the model above, a bioeconomic model with time delay incorporating two differential equations and one algebraic equation is written as

    {dNdT=rN(1N(tτ)K)e1(NP)1+e1h1(NP)+e2h2(AP)P,dPdT=n1e1(NP)+n2e2(AP)1+e1h1(NP)+e2h2(AP)PmPq1EP,E(p1q1Pw)Q=0. (1.3)

    From an economic perspective, the impact of harvesting effort on ecosystem is expressed as: net economic revenue (NER) = total revenue (TR) - total cost (TC). TR =p1q1E(t)P(t) and TC =wE(t), where p1 is the price per unit predator biomass, q1 and E(t) stand for the harvesting capacity coefficient and harvesting effort of the predator, respectively. w represents the cost per unit predator harvesting efforts. Q means the NER. We only consider the harvesting of the predator, the catch rate function h(t) is written as h(t)=q1E(t)P(t) which meets the catch-per-unit-effort hypothesis [45]. All the parameters in model (1.3) are positive. The initial conditions for model (1.3) are given N[τ,0]C+([τ,0],R+). If P(0) is provided, E(0) can be expressed as Q/(p1q1P(0)w) thus it is content with P(0)>w/p1q1.

    Significantly, a real-life application is motivated by data from Katz [46]. We consider that prey N is represented by barnacles Balanus balanoides and predator P is expressed as snails Urosalpinx cinerea. The data strongly supports the ratio-dependent form N/P much better than that only depends on prey N. Incorporating additional food A (Ostrea gigas thunberg) into our model, our target is to address our understanding on the consequences of providing additional food for the predator on the dynamics, which brings out an explicit link between practical biological control and theoretical fruits. Besides, we investigate the optimal harvesting strategy of snails Urosalpinx cinerea due to its use as a kind of Chinese medical herbs.

    The rest of this manuscript is emerged as follows. Section 2 is devoted to discussing the local steady-state and the Hopf bifurcation by investigating the characteristic equation. In Section 3, the main results including the properties of the bifurcating periodic solutions and the formulas of the direction of Hopf bifurcation are investigated. The optimal harvesting problem of model (1.3) without time delay is analyzed in Section 4. Four numerical examples are displayed in Section 5 to explain our findings. The brief and powerful biological discussion and conclusions are provided in Section 6. The paper end with Appendices A, B and C to show some proof and calculations.

    Model (1.3) is simplified and analyzed by using the following rescaling

    x=NK,y=PKe1h1,t=rT.

    After nondimensionalizing the model (1.3) for convenience, we obtain

    {dxdt=x(1x(tτ))cxyx+y+αξ,dydt=b(x+ξ)yx+y+αξmyqEy,E(pqyw)Q=0, (2.1)

    where c=e1r, α=n1h2n2h1, ξ=γAK, γ=n2e2n1e1, b=n1rh1, m=mr, q=q1r, p=p1Ke1h1r.

    Through calculation, the internal equilibrium of the model (2.1) could be written as P0(x,y,E), where

    E=Qpqyw,  y=x2x+αξxαξ1xc

    and x is the positive solution of Ax4+Bx3+Cx2+Dx+F=0 where

    A=pqb,      B=2pqb+pqbαξ+wb+pqbc+pqbξpqmc,C=pqb2pqbαξ2wb+2wbcpqbc+pqαξbc2pqbξ+pqbαξ2+wbξ+pqbcξ+pqmc2pqαξmcwmc+qQc,D=pqbαξ+wb2wbcpqbcαξ+wbc2+pqbξpqbαξ22wbξpqbαξ2+2wbcξpqbcξ+pqbcαξ2+2pqαξmc+wmcwc2mpqα2ξ2mcwmcαξqQc+qQcαξ+qQc2,F=pqαξ2b+wbξ2wcbξpqbcαξ2+wc2bξ+pqα2ξ2mc+wmcαξwmc2αξqQcαξ+qQc2αξ.

    Remark 2.1. By Descartes sign rule [47], the possible positive roots of equation Ax4+Bx3+Cx2+Dx+F=0 are as follows.

    (ⅰ) If any one of the conditions (a), (b), (c) and (d) holds, the equation exists one positive root

    (a)  A<0,B>0,C>0,D>0,F>0;  (b)  A>0,B>0,C>0,D>0,F<0;(c)  A<0,B<0,C>0,D>0,F>0;  (d)  A>0,B>0,C>0,D<0,F<0.

    (ⅱ) If any one of the conditions (e), (f), (g), (h), (i) and (j) holds, the equation exists two positive roots or no roots

    (e)  A>0,B<0,C>0,D>0,F>0;  (f)  A>0,B>0,C<0,D>0,F>0;(g)  A>0,B>0,C>0,D<0,F>0;  (h)  A<0,B>0,C>0,D>0,F<0;(i)   A>0,B<0,C<0,D>0,F>0;  (j)  A>0,B>0,C<0,D<0,F>0.

    (ⅲ) If any one of the conditions (k), (l), (m) and (n) holds, the equation exists three positive roots or one positive root

    (k)  A<0,B>0,C<0,D>0,F>0;   (l)  A<0,B>0,C>0,D<0,F>0;(m) A>0,B<0,C>0,D>0,F<0;  (n)  A>0,B>0,C<0,D>0,F<0.

    (ⅳ) If the condition (p) holds, the equation exists four positive roots or two positive roots or no roots

    (p)  A>0,B<0,C>0,D<0,F>0.

    According to the following theorem, we know the conditions of the Hopf bifurcation occurs in model (2.1).

    Theorem 2.1. If the assumptions A1+A4>0,A3>0,A2+A3>0 and A2A3<0 are satisfied, then when τ<τ0, equilibrium P0(x,y,E) of model (2.1) is stable; equilibrium P0(x,y,E) of Eq (2.1) is unstable when τ>τ0; when τ=τ0, model (2.1) undergoes a Hopf bifurcation.

    The detailed proving process of the Theorem is given in Appendix A.

    We investigate the direction of Hopf bifurcation and the properties of the bifurcating periodic solutions at the positive equilibrium in this section.

    Theorem 3.1. If μ2>0 (μ2<0), the model undergoes a supercritical (subcritical) Hopf bifurcation at P(x1,y1,E1); moreover, if β2<0 (β2>0) then the bifurcating periodic solutions are stable (unstable); if T2>0 (T2<0), the periodic of bifurcating periodic solutions increase (decrease). Here

    c1(0)=i2ω10τk(g20g112|g11|2|g02|23)+g212,μ2=Re{c1(0)}Re{λ(τk)},     β2=2Re{c1(0)},T2=Im{c1(0)}+μ2Im{λ(τk)}ω10τk.

    The detailed proof of the Theorem is given in Appendix B.

    In order to achieve species persistence and profit maximization, optimal harvesting problem for model (1.3) without time delay is discussed in this section. We consider instantaneous annual discount rate δ, we give a continuous time stream of revenues J as follows

    J=tft0E(p1q1Pw)eδtdt. (4.1)

    The control constrain on this interval 0<E(t)<Emax. Here, Emax stands for the maximum harvesting effort. The optimal prey and predator densities and the corresponding optimal harvesting effort are represented by Noptimal, Poptimal and Eoptimal, respectively. We are committed to calculating the optimal harvesting effort Eoptimal which satisfies the following formula

    J(Eoptimal)=max{J(E)|EU}, (4.2)

    where U presents the control set written as

    U={E | E is measurable and 0EEmax for all t}. (4.3)

    The calculation procedure of Noptimal, Poptimal and Eoptimal are shown in Appendix C.

    In this section, we will employ several specific examples to simulate the solutions to model (1.3), and verify the analytical results of the existence of Hopf bifurcation. Our analytical results illustrate that Hopf bifurcation arises in model (1.3) when the value of bifurcation parameter τ crosses critical values τ=τk, where

    τk=1ω10arccos(A3A1A4)ω210A2A3A23+A24ω210+2kπω10,k=0,1,2,3,

    and ω10 is the root of equation ω14+(A212A2A24)ω12+(A22A23)=0. Here, bifurcation parameter τ is the maturation time of prey. In order to illustrate the Hopf bifurcation of (1.3). We first choose the parameter values as follows: r=1.01, K=0.91, e2=1.01, h1=0.99, h2=0.01, n1=0.85, n2=0.98, A=0.98, m=1.99, q1=0.91, p1=360, w=1.01, Q=0.51. The scientific significance of these parameters are shown in Table 1, under the above parameters, model (1.3) becomes the following model (5.1)

    {dNdT=1.01N(1N(tτ)0.91)0.45(NP)1+0.450.99(NP)+1.010.01(0.98P)P,dPdT=0.850.45(NP)+0.981.01(0.98P)1+0.450.99(NP)+1.010.01(0.98P)P1.99P0.91EP,E(3600.91P1.01)0.51=0. (5.1)

    Through maple software, we get P1(N,P,E)=(0.7191,0.2939,0.0054) and P1(x1,y1,E1)= (0.7903,0.7248,0.0108) are respectively the equilibrium of models (5.1) and (A.2) with above parameters.

    Table 1.  Meaning and dimension of the parameters.
    Parameter Biological significance Dimension
    r The intrinsic growth rate of the prey Time1
    K Carrying capacity of the prey Biomass
    e1 The coefficient of predator capture on prey Time1
    e2 The coefficient of predator capture on additional food Time1
    h1 Handing time per predator per unit of the ratio NP prey biomass Time
    h2 Handing time per predator per unit of the ratio NP additional food biomass Time
    n1 The nutritional value of the prey Percent
    n2 The nutritional value of the additional food Percent
    A The additional food for the predator Biomass
    m The natural mortality of the predator Time1
    q1 The harvesting capacity coefficient Time1
    p1 The price per unit predator biomass
    w The cost per unit predator harvesting efforts
    Q The net economic revenue

     | Show Table
    DownLoad: CSV

    Substituting the value of the positive equilibrium P1(x1,y1,E1) in the expression of A1,A2,A3 and A4 to calculate the values as follows: A1=0.81, A2=0.16, A3=0.73 and A4=0.79 which surely satisfy the conditions of Theorem 2.1 (that is A1+A4=1.60>0, A2+A3=0.56>0 and A2A3=0.89<0). In addition, we further substitute A1,A2,A3 and A4 to equation (2.8) to calculate ω10=0.74, then substituting ω10 in the expression of τk to yield τ0=1.86. A series of calculations show that g20=12.70+3.11i, g11=4.4310.67i, g02=11.053.71i, g21=106.05+74.57i, c1(0)=97.3143.88i, Re{λ(τk)}=1.01, Im{λ(τk)}=2.35, μ2=96.35>0, β2=194.62<0, T2=134.80>0. Hence, by Theorem 3.1, the periodic increase, and the direction is supercritical, and the periodic solutions are stable. By Matlab we will reveal how the model can arise Hopf bifurcation by choosing different time delays τ in the following figures.

    When τ=1.63<τ0=1.86, model (5.1) satisfies the condition of Theorem 2.1. So P1(N,P,E)=(0.7191,0.2939,0.0054) is asymptotically stable. Figure 1 reveals the time evolution and the phase trajectory of model (5.1) for τ=1.63. It is obvious that model (5.1) converges to the positive equilibrium.

    Figure 1.  Numerical simulations of model (5.1) with τ=1.63<τ0=1.86: (a) the time evolution of the prey; (b) the time evolution of the predator; (c) the time evolution of the harvesting effort of predator; (d) the phase trajectory of model (5.1). Equilibrium P1(N,P,E) is asymptotically stable.

    When τ=1.87>τ0=1.86, model (5.1) satisfies the condition of Theorem 2.1. So P1(N,P,E)=(0.7191,0.2939,0.0054) is unstable, i.e., a family of periodic solutions are bifurcated from P1(N,P,E). The periodic solutions and its stability are shown in Figure 2.

    Figure 2.  Numerical simulations of model (5.1) with τ=1.87>τ0=1.86: (a) the time evolution of the prey; (b) the time evolution of the predator; (c) the time evolution of the harvesting effort of predator; (d) the phase trajectory of model (5.1). Equilibrium P1(N,P,E) is unstable and there exist bifurcating periodic solutions.

    Combined with Figures 1 and 2, we can see that the size of maturation time τ affects the dynamic behaviors of the model, see Figure 3. This means that if time delay τ exceeds critical value, bifurcation behavior occurs at the positive equilibrium P1(N,P,E) of model (1.3).

    Figure 3.  The bifurcation diagram of model (1.3) with respect to τ. (a) the bifurcation diagram of N(t); (b) the bifurcation diagram of P(t).

    We choose the parameter values as follows: r=0.2, K=0.1, e2=0.7, h1=0.95, h2=0.8, n1=0.1, n2=3, A=0.01, m=0.9, q1=5, p1=1, w=0.01, δ=0.01. (Noptimal,Poptimal) and Eoptimal as capture rate e1 increase are shown by (a) in Figure 4. It shows that with the increase of capture rate e1, the optimal prey population decreases initially and increases afterwards, optimal predator population gradually decreasing, and the optimal harvesting effort gradually decreases. Besides, we choose the parameter values as follows: r=1, K=0.45, e1=60, e2=0.2, h1=1, h2=0.02, n1=1.5, n2=1, m=0.01, q1=1.44, p1=0.02, w=1.01, δ=0.1. (Noptimal,Poptimal) and Eoptimal as additional food A increase are shown by (b) in Figure 4. It displays that with the increase of additional food A, the corresponding optimal prey and predator populations gradually increase, and the optimal harvesting effort gradually decreases.

    Figure 4.  Optimal harvesting with respect to different parameters. (a) the coefficient of predator capture on prey e1(0,0.21); (b) additional food A(0,1.80).

    In our paper, based on a predator-prey model with additional food proposed by Kumar et al. [29], we incorporate time delay and harvesting into the above model and establish a differential-algebraic bio-economic model. Through a series of analytical analysis we obtain the results about the existence of positive equilibrium, the conditions of steady-state and Hopf bifurcation, and the direction of bifurcation as well as the stability of bifurcating periodic solutions. Firstly, the local stability condition of positive equilibrium of model (2.1) with time delay is A2A3>0, while that without time delay are A1+A4>0 and A2+A3>0. Theorem 2.1 implies that the presence of the mature delay can destabilize model (2.1). When τ<τ0, equilibrium P0(x,y,E) of model (2.1) is stable. The equilibrium is unstable when τ>τ0; when τ=τ0, model (2.1) has a Hopf bifurcation near the equilibrium. Besides, Theorem 3.1 displays that the direction of the bifurcation is determined by μ2, the stability of bifurcating periodic solutions is determined by β2, and the period of the bifurcating periodic solutions is determined by T2. Last, optimal harvesting strategies for model (1.3) without time delay are investigated. We achieve optimal harvesting equilibrium (Noptimal,Poptimal) and optimal harvesting effort Eoptimal.

    The numerical simulation of the model is carried out through Maple and Matlab software, and we find that the results of the numerical simulation agree with the theoretical results in Theorems 2.1 and 3.1. The influence of the bifurcation parameter τ on the dynamics of prey, predator and harvesting effort is discussed. The experimental results illustrate that the positive equilibrium of the model is locally asymptotically stable when bifurcation parameter τ<1.86, see Figures 1. Conversely, equilibrium P1(N,P,E) is unstable and there exist bifurcating periodic solutions which are stable {when bifurcation parameter τ>1.86, see Figure 2. The bifurcation diagram of (1.3) when τ=1.86 is presented in Figure 3, and the direction of bifurcation is supercritical. This also illustrates the influence of time delay τ which is one of the causes of population size fluctuation on the Hopf bifurcation of model (1.3), } i.e. the presence of the mature delay can destabilize model (1.3). Furthermore, we display optimal harvesting strategies in Figure 4, and depict the change of optimal harvesting equilibrium and optimal harvesting effort with respect to the rate of predator capture on prey e1 and extra food A, respectively. The phenomenon in Figure 4 (a) is expected due to the stronger impact of the coefficient of predator capture on prey e1. From Figure 4 (a), we know that optimal harvesting effort approaches zero when the coefficient of predator capture on prey e1=0.21. This means that when the coefficient of predator capture on prey e1 is beyond the level 0.21, harvesting predators should not be considered in order to prevent extinction. Figure 4 (b) shows that the optimal harvesting effort gradually decreases, while optimal prey and predator populations gradually increase, since additional food A distracts the predator from attacking the prey. At the same time, in order to prevent harmful prey from growing to uncontrollable numbers, the harvesting effort on predator should be reduced.

    There are many topics that require us to refine and further analyze our model. On the one hand, the discrete time delay is considered in this study of Hopf bifurcation while more rich dynamic behaviors are generated by incorporating the distributed delays. On the other hand, the influence of random factors could not be ignored in which we introduce white noise into our model which involving the multiplicative random excitation and additive random excitation to analyze the stochastic P-bifurcation and stochastic D-bifurcation. The model is displayed as follows

    {dNdT=rN(1NK)e1(NP)1+e1h1(NP)+e2h2(AP)P+α1Nξ(t)+η1η(t),dPdT=n1e1(NP)+n2e2(AP)1+e1h1(NP)+e2h2(AP)PmPq1EP+α2Pξ(t)+η2η(t),E(p1q1Pw)Q=0,

    where ξ(t),η(t) represent the multiplicative random excitation and additive random excitation respectively. The above mentions make our model more interesting and complicated and remain to be done in the future.

    The authors declare they have not used Artificial Intelligence (AI) tools in the creation of this article.

    The authors thank the editor and referees for their careful reading and valuable comments. The work is supported by the National Natural Science Foundation of China (No.12101211) and the Program for Innovative Research Team of the Higher Education Institution of Hubei Province (No.T201812) and the Scientific Research Project of Education Department of Hubei Province (No.B2020090) and the Program of Graduate Education Innovation of Hubei Minzu University (No.MYK2023042).

    The authors declare that there is no conflict of interest.

    In order to linearize model (2.1), we consider the following linear transformation

    (xyE)=(1000100pqEpqyw1)(x1y1E1).

    Thus model (2.1) could be rewritten as

    {dx1dt=x1(1x1(tτ))cx1y1x1+y1+αξ,dy1dt=b(x1+ξ)y1x1+y1+αξmy1q(E1pqEy1pqyw)y1,(E1pqEy1pqyw)(pqy1w)Q=0. (A.2)

    The internal equilibrium of the model (A.2) becomes P1(x1,y1,E1), we transform the equilibrium into zero by linear transformation x1=x1+x2, y1=y1+y2, E1=E1+I(x2,y2), where

    I(x2,y2)=pqE(y1+y2)pqy1w+Qpq(y1+y2)wpqEy1pqy1wE.

    Model (A.2) is expressed as the following equation according to the above transformations

    {dx2dt=(x1+x2)((1(x1+x2(tτ)))c(x1+x2)(y1+y2)x1+x2+y1+y2+αξ,dy2dt=(y1+y2)(b(x1+x2+ξ)x1+x2+y1+y2+αξmqE1qI+pq2E(y1+y2)pqyw). (A.3)

    By calculation, the Jacobian matrix of the model (A.3) at (0,0) is represented as follows

    J=(x1eλτ+cx1y1(x1+y1+αξ)2cx1(x1+αξ)(x1+y1+αξ)2by1(y1+αξξ)(x1+y1+αξ)2b(x1+ξ)y1(x1+y1+αξ)2+pq2Ey1pqy1w).

    The formula for the determination of the characteristic equation gives that λ2+A1λ+A2+(A3+A4λ)eλτ=0, where

    A1=b(x1+ξ)y1(x1+y1+αξ)2pq2Ey1pqy1wcx1y1(x1+y1+αξ)2,A2=cbx1y12(x1+ξ)(x1+y1+αξ)4+pq2cx1y12E(x1+y1+αξ)2(pqy1w)+bcx1y1(x1+αξ)(y1+αξξ)(x1+y1+αξ)4,A3=bx1y1(x1+ξ)(x1+y1+αξ)2x1y1pq2Epqy1w,A4=x1.

    When τ=0, the characteristic equation is as follows

    λ2+(A1+A4)λ+A2+A3=0. (A.4)

    By Routh-Hurwitz criterion, we know that P1(x1,y1,E1) is locally asymptotically stable provided that the conditions A1+A4>0 and A2+A3>0.

    When τ>0, the characteristic equation is yielded to

    λ2+A1λ+A2+(A3+A4λ)eλτ=0. (A.5)

    Suppose that iω1 is a solution of (A.5), one gets

    ω12+A1iω1+A2+(A3+A4iω1)eiω1τ=0. (A.6)

    Separating the real and imaginary parts of Eq (A.6), we obtain

    A4ω1sinω1τ+A3cosω1τ=ω21A2,  A4ω1cosω1τA3sinω1τ=A1ω1. (A.7)

    Furthermore,

    ω14+(A212A2A24)ω12+(A22A23)=0. (A.8)

    Let u=ω21. Then, Eq (A.8) becomes

    f(u)=u2+(A212A2A24)u+(A22A23)=0.

    If A1>0,A3>0,A2+A3>0 and A2A3<0, then Eq (A.8) exists a unique positive real root ω10, hence (A.5) has a pair of pure imaginary roots ±iω10 at the critical value τk>0, which could be denoted as

    τk=1ω10arccos(A3A1A4)ω210A2A3A23+A24ω210+2kπω10,k=0,1,2,3. (A.9)

    If A2A3>0, (A.5) has no real roots and P1(x1,y1,E1) is asymptotical stability for any τ>0.

    We have to prove that ddτReλ(τk)>0 is true for guaranteeing the existence of Hopf bifurcation. Consider the following equation

    (dλdτ)1=2λ+A1+(A3τ+A4A4τλ)eλτ(A3λ+A4λ2)eλτ. (A.10)

    Using a computation process similar to that of Tang [48] and Cooke [49], one yields

    Sign{ddτReλ}λ=iω10=Sign{Re(dλdτ)1}λ=iω10=Sign{Re[(2iω10+A1)(cos(ω10τ)+isin(ω10τ))A3τ+A4A4τiω10A3iω10A4ω210]}=Sign{2A3w210cos(w10τ)+2A4w310sin(w10τ)A1A4w210cos(w10τ)+A1A3w10sin(w10τ)A24w210A23ω210+A24ω410}=Sign{ω210(2ω210+(A212A2A24))A23ω210+A24ω410}=Sign{f(ω210)A23+A24ω210}.

    Since A2+A3>0 and A2A3<0, we know that f(u) has a unique positive real root u0=ω210. In addition it can be shown that f(u0)>0 (that is f(ω210)>0). Combined with the above analysis, we have the following theorem.

    Let u1(t)=x2(τt), u2(t)=y2(τt), τ=τk+μ (μR), then, μ=0 is the Hopf bifurcation value. The functional differential equation is considered as follows

    u(t)=Lμ(ut)+F(μ,ut), (B.1)

    where u(t)=(u1(t),u2(t))R2 and Lμ:CR2,F:R×CR2. Let us define

    Lμϕ=(τk+μ)(cx1y1(x1+y1+αξ)2cx1(x1+αξ)(x1+y1+αξ)2by1(y1+αξξ)(x1+y1+αξ)2b(x1+ξ)y1(x1+y1+αξ)2+pq2Ey1pqy1w)ϕ(0)+(τk+μ)(x1000)ϕ(1) (B.2)

    and

    F(μ,ϕ)=(τk+μ)(F1F2), (B.3)

    where

    F1=(cy1μ21cx1y1μ31)ϕ21(0)ϕ21(1)+(cx1μ21cx1y1μ31)ϕ22(0)(cαξμ21+2cx1y1μ31)ϕ1(0)ϕ2(0)+(c(x1αξ)μ31+3cx1y1μ41)ϕ1(0)ϕ22(0)+(c(y1αξ)μ31+3cx1y1μ41)ϕ21(0)ϕ2(0)+(cy1μ31+cx1y1μ41)ϕ31(0)+(cx1μ31+cx1y1μ41)ϕ32(0)+,F2=(by1μ21+b(x1+ξ)y1μ31)ϕ21(0)(b(x1+ξ)(x1+αξ)μ31+pq2Qwν31)ϕ22(0)+(b(αξξ)μ21+2b(x1+ξ)y1μ31)ϕ1(0)ϕ2(0)+(b(x1αξ+2ξ)μ313b(x1+ξ)y1μ41)ϕ1(0)ϕ22(0)+(b(y1αξ+ξ)μ313b(x1+ξ)y1μ41)ϕ21(0)ϕ2(0)+(by1μ31b(x1+ξ)y1μ41)ϕ31(0)+(b(x1+ξ)(x1+αξ)μ41+p2q3Qwν41)ϕ32(0)+, (B.4)

    in which μ1=(x1+y1+αξ), ν1=(pqy1w) and ϕ(θ)=(ϕ1(θ),ϕ2(θ))C.

    There exists a 2×2 matrix function η(θ,μ) (θ[1,0]) such that

    Lμϕ=01dη(θ,μ)ϕ(θ),ϕC. (B.5)

    At this point, bounded variation function could be chosen as

    η(θ,μ)=(τk+μ)(cx1y1(x1+y1+αξ)2cx1(x1+αξ)(x1+y1+αξ)2by1(y1+αξξ)(x1+y1+αξ)2b(x1+ξ)y1(x1+y1+αξ)2+pq2Ey1pqy1w)δ(θ)(τk+μ)(x1000)δ(θ+1). (B.6)

    Here, δ(θ) is the Dirac function.

    For ϕC1([1,0],R2), we define

    A(μ)ϕ(θ)={dϕ(θ)dθ,                  θ[1,0),01dη(θ,μ)ϕ(θ),   θ=0, (B.7)
    R(μ)ϕ={0,           θ[1,0),F(μ,ϕ),  θ=0. (B.8)

    Then, Eq (B.1) is equivalent to the following equation

    ut=A(μ)ut+R(μ)ut,  ut(θ)=u(t+θ),  θ[1,0]. (B.9)

    The bifurcating periodic solution u(t,μ) of Eq (B.1) is affected by parameter ε, solution u(t,μ(ε)) of Eq (B.1) exists amplitude o(ε), nonzero exponential β(ε) (β(0)=0) and period T(ε). Under the above assumptions, μ, T, and β have the following expansion form

    {μ=μ2ε2+μ4ε4+,T=2πω(1+T2ε2+T4ε4),β=β2ε2+β4ε4. (B.10)

    Next, we compute the coefficients μ2, T2, β2. For ψC1([0,1],(R2)), assign the conjugate operator A of A is as follows

    Aψ={dψ(s)ds,                 s(0,1],01dηT(t,0)ψ(t),   s=0, (B.11)

    the adjoint bilinear form is given by

    ψ(s),ϕ(θ)=ˉψT(0)ϕ(0)01θξ=0ˉψT(ξθ)dη(θ)ϕ(ξ)dξ,  η(θ)=η(θ,0). (B.12)

    Obviously, ±iω10τk are both eigenvalues of A(0) and A. Now we calculate the eigenvector of A(0) corresponding to iω10τk. Let q(θ)=(1,Δ)Teiω10τkθ, then, A(0)q(θ)=iω10τkq(θ). Combining Eq (B.6) and the definition of A(0), it is easy to get

    (x1eiω10τk+cx1y1μ21cx1(x1+αξ)μ21by1(y1+αξξ)μ21b(x1+ξ)y1μ21+pq2Ey1ν1)q(0)=iω10q(0), (B.13)

    we further obtain

    Δ=(iω10+x1eiω10τk)μ21cx1(x1+αξ)+y1x1+αξ. (B.14)

    By a similar argument as that in the above part, the eigenvector of A corresponding to iω10τk could be achieved. Let q(s)=D(1,Δ)eiω10τks, we also have

    Δ=(iω10+x1eiω10τk)μ21by1(y1+αξξ)cx1b(y1+αξξ). (B.15)

    From Eq (B.12) one gets

    q(s),q(θ)=ˉD(1,¯Δ)(1,Δ)T01θξ=0ˉD(1,¯Δ)eiω10τk(ξθ)dη(θ)(1,Δ)Teiω10τkξdξ=ˉD(1+¯ΔΔ)ˉD01θξ=0(1,¯Δ)eiω10τkθdη(θ)(1,Δ)Tdξ=ˉD(1+¯ΔΔ)ˉD01(1,¯Δ)θeiω10τkθdη(θ)(1,Δ)T=ˉD(1+¯ΔΔ+(1,¯Δ)τk(x1000)eiω10τk(1Δ))ˉD(1+¯ΔΔ+τkeiω10τkx1).. (B.16)

    Hence,

    D=11+¯ΔΔτk+eiω10τkx1,  ˉD=11+ΔˉΔτk+eiω10τkx1. (B.17)

    Apparently, q(s) q(θ) meets q(s),q(θ)=1 and q(s),ˉq(θ)=0. When μ=0, let μt be the solution of Eq (B.9), we set

    z(t)=q,ut,  W(t,θ)=ut(θ)2Re{z(t)q(θ)}. (B.18)

    Therefore,

    W(t,θ)=W(z(t),ˉz(t),θ), (B.19)
    W(z(t),ˉz(t),θ)=W20(θ)z22+W11(θ)zˉz+W02(θ)ˉz22+W30(θ)z36+, (B.20)

    here, the local coordinates of center manifold C0 corresponding to q and q are expressed as z and ˉz. Note that W is real if ut is real, thus only real solutions are considered. For solution utC0, since μ=0,

    z(t)=iω10τkz+¯q(0)F(0,W(z,ˉz,0))+2Re{z(t)q(θ)})=iω10τkz+¯q(0)F0(z,ˉz). (B.21)

    that is

    z(t)=iω10τkz+g(z,ˉz), (B.22)

    where

    g(z,ˉz)=¯q(0)F0(z,ˉz)=g20(θ)z22+g11(θ)zˉz+g02(θ)ˉz22+g21(θ)z2ˉz2+. (B.23)

    Comparing Eqs (B.18) and (B.20), one has

    u(t)=(u1t(θ),u2t(θ))=W(t,θ)+2Re{z(t)q(θ)}, (B.24)

    where q(θ)=(1,Δ)Teiω10τkθ, furthermore

    u1t(0)=W(1)(t,0)+z+ˉz,u2t(0)=W(2)(t,0)+Δz+ˉΔˉz,u1t(1)=W(1)(t,1)+zeiω10τk+ˉzeiω10τk. (B.25)

    Combining Eqs (B.3) and (B.4), we obtain

    g(z,ˉz)=¯q(0)F0(z,ˉz)=¯q(0)F(0,ut)=ˉDτk(1,¯Δ)(F1F2)=ˉDτk(F1+¯ΔF2)=ˉDτk{(cy1μ21cx1y1μ31)(W(1)(0)+z+ˉz)2(W(1)(1)+zeiω10τk+ˉzeiω10τk)2+(cx1μ21cx1y1μ31)(W(2)(0)+Δz+ˉΔˉz)2+(cαξμ212cx1y1μ31)(W(1)(0)+z+ˉz)(W(2)(0)+Δz+ˉΔˉz)+(cy1μ31+cx1y1μ41)(W(1)(0)+z+ˉz)3+(cx1μ31+cx1y1μ41)(W(2)(0)+Δz+ˉΔˉz)3+(c(y1αξ)μ31+3cx1y1μ41)(W(1)(0)+z+ˉz)2(W(2)(0)+Δz+ˉΔˉz)+(c(x1αξ)μ31+3cx1y1μ41)(W(1)(0)+z+ˉz)(W(2)(0)+Δz+ˉΔˉz)2+¯Δ(by1μ21+b(x1+ξ)y1μ31)(W(1)(0)+z+ˉz)2+¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)(W(2)(0)+Δz+ˉΔˉz)2+¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)(W(1)(0)+z+ˉz)(W(2)(0)+Δz+ˉΔˉz)+¯Δ(by1μ31b(x1+ξ)y1μ41)(W(1)(0)+z+ˉz)3+¯Δ(b(x1+ξ)μ31b(x1+ξ)y1μ41p2q3Qν31+p3q4Qy1ν41)(W(2)(0)+Δz+ˉΔˉz)3+¯Δ(b(y1αξ+ξ)μ313b(x1+ξ)y1μ41)(W(1)(0)+z+ˉz)2(W(2)(0)+Δz+ˉΔˉz)+¯Δ(b(x1+2ξαξ)μ313b(x1+ξ)y1μ41)(W(1)(0)+z+ˉz)(W(2)(0)+Δz+ˉΔˉz)2+}=ˉDτk{2(cy1μ21cx1y1μ31)2e2iω10τk+2Δ2(cx1μ21cx1y1μ31)+2Δ(cαξμ212cx1y1μ31)+2¯Δ(by1μ21+b(x1+ξ)y1μ31)+2Δ¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)+2Δ2¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)}z22+ˉDτk{2(cy1μ21cx1y1ν31)+2ΔˉΔ(cx1μ21cx1y1μ31)+2Re(Δ)(cαξμ212cx1y1μ31)2+2¯Δ(by1μ21+b(x1+ξ)y1μ31)+2ΔˉΔ¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)
                      +2Re(Δ)¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)}zˉz+ˉDτk{2(cy1μ21cx1y1μ31)2e2iω10τk+2ˉΔ2(cx1μ21cx1y1μ31)+2ˉΔ(cαξμ212cx1y1μ31)+2¯Δ(by1μ21+b(x1+ξ)y1μ31)+2ˉΔ2¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)+2ˉΔ¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)}ˉz22+ˉDτk{2(cy1μ21cx1y1μ31)(2W(1)11(0)+W(1)20(0))(4W(1)11(1)eiω10τk+2W(1)20(1)eiω10τk)+2(cx1μ21cx1y1μ31)(2W(2)11(0)Δ+W(2)20(0)ˉΔ)+2(cαξμ212cx1y1μ31)(W(1)11(0)Δ+12W(1)20(0)ˉΔ+W(2)11(0)+12W(2)20(0))+6(cy1μ31+cx1y1μ41)+2¯Δ(by1μ21+b(x1+ξ)y1μ31)(2W(1)11(0)+W(1)20(0))+2(c(x1αξ)μ31+3cx1y1μ41)(2ΔˉΔ+Δ2)+6(cx1μ31+cx1y1μ41)(Δ2ˉΔ)+2¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)(2W(2)11(0)Δ+W(2)20(0)ˉΔ)+2¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)(W(1)11(0)Δ+12W(1)20(0)ˉΔ+W(2)11(0)+12W(2)20(0))+6¯Δ(by1μ31b(x1+ξ)y1μ41)+6Δ2ˉΔ¯Δ(b(x1+ξ)μ31b(x1+ξ)y1μ41p2q3Qν31+p3q4Qy1ν41)+2¯Δ(b(y1αξ+ξ)μ313b(x1+ξ)y1μ41)(2Δ+ˉΔ)+2(c(y1αξ)μ31+3cx1y1μ41)(¯Δ+2Δ)+2¯Δ(b(x1αξ+2ξ)μ313b(x1+ξ)y1μ41)(2ΔˉΔ+Δ2)}z2ˉz2+. (B.26)

    Comparing with the corresponding coefficients of the Eq (B.23), it yields to

    g20=ˉDτk{2(cy1μ21cx1y1μ31)2e2iω10τk+2Δ2(cx1μ21cx1y1μ31)+2Δ(cαξμ212cx1y1μ31)+2¯Δ(by1μ21+b(x1+ξ)y1μ31)+2Δ¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)+2Δ2¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)},
    g11=ˉDτk{2(cy1μ21cx1y1μ31)2+2ΔˉΔ(cx1μ21cx1y1μ31)+2Re(Δ)(cαξμ212cx1y1μ31)+2¯Δ(by1μ21+b(x1+ξ)y1μ31)+2Re(Δ)¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)
    +2ΔˉΔ¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)},                
    g02=ˉDτk{2(cy1μ21cx1y1μ31)2e2iω10τk+2ˉΔ2(cx1μ21cx1y1μ31)+2ˉΔ(cαξμ212cx1y1μ31)+2¯Δ(by1μ21+b(x1+ξ)y1μ31)+2ˉΔ¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)+2ˉΔ2¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)},
                  g21=ˉDτk{2(cy1μ21cx1y1μ31)(2W(1)11(0)+W(1)20(0))(4W(1)11(1)eiω10τk+2W(1)20(1)eiω10τk)+2(cx1μ21cx1y1μ31)(2W(2)11(0)Δ+W(2)20(0)ˉΔ)+2(c(x1αξ)μ31+3cx1y1μ41)(2ΔˉΔ+Δ2)+2(cαξμ212cx1y1μ31)(W(1)11(0)Δ+12W(1)20(0)ˉΔ+W(2)11(0)+12W(2)20(0))+6(cy1μ31+cx1y1μ41)+6(cx1μ31+cx1y1μ41)(Δ2ˉΔ)+2(c(y1αξ)μ31+3cx1y1μ41)(¯Δ+2Δ)+2¯Δ(by1μ21+b(x1+ξ)y1μ31)(2W(1)11(0)+W(1)20(0))+2¯Δ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)(2W(2)11(0)Δ+W(2)20(0)ˉΔ)+2¯Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31)(W(1)11(0)Δ+12W(1)20(0)ˉΔ+W(2)11(0)+12W(2)20(0))+6¯Δ(by1μ31b(x1+ξ)y1μ41)+6Δ2ˉΔ¯Δ(b(x1+ξ)μ31b(x1+ξ)y1μ41p2q3Qν31+p3q4Qy1ν41)+2¯Δ(b(y1αξ+ξ)μ313b(x1+ξ)y1μ41)(2Δ+ˉΔ)+2¯Δ(b(x1αξ+2ξ)μ313b(x1+ξ)y1μ41)(2ΔˉΔ+Δ2)}. (B.27)

    In order to deduce g21, now we have to calculate W20(θ) and W10(θ). It follows from Eqs (B.9) and (B.18) that

    W=utzqˉzˉq={AW2Re{¯q(0)F0q(θ),         1θ<0,AW2Re{¯q(0)F0q(θ)+F0,  θ=0,:=AW+H(z,ˉz,θ), (B.28)

    where

    H(z,ˉz,θ)=H20(θ)z22+H11(θ)zˉz+H02(θ)ˉz22+. (B.29)

    Consider on the center manifold C0 close enough to the origin, we have

    ˙W=Wz˙z+Wˉz˙ˉz. (B.30)

    Substituting Eq (B.30) into (B.28) and comparing the coefficients on z2 and zˉz, it easy to see

    (A2iω10τkI)W20(θ)=H20(θ),AW11(θ)=H11(θ). (B.31)

    For θ[1,0), from Eq (B.28) we can get

    H(z,ˉz,θ)=¯q(0)F0q(θ)q(0)¯F0ˉq(θ)=gq(θ)ˉgˉq(θ). (B.32)

    Comparing the coefficients of Eq (B.29) gives that

    H20(θ)=g20q(θ)ˉg02ˉq(θ),H11(θ)=g11q(θ)ˉg11ˉq(θ). (B.33)

    We have from Eqs (B.31) and (B.33) that

    ˙W20(θ)=2iω10τkW20(θ)+g20q(θ)+ˉg02ˉq(θ). (B.34)

    Noticing that q(θ)=q(0)eiω10τkθ, then

    W20(θ)=ig20ω10τkq(0)eiω10τkθ+iˉg023ω10τkˉq(0)eiω10τkθ+M1e2iω10τkθ, (B.35)

    where M1=(M(1)1,M(2)1)R2 is a constant vector. By the same method as that in the above part we can calculate

    W11(θ)=ig11ω10τkq(0)eiω10τkθ+iˉg11ω10τkˉq(0)eiω10τkθ+M2, (B.36)

    where M2=(M(1)2,M(2)2)R2 is also a constant vector.

    Calculating constant vectors M1 and M2 is our main work in the following discussion. It follows from Eqs (B.28) and (B.29) that

    H20(0)=g20q(0)ˉg02ˉq(0)+2τkN1,H11(0)=g11q(0)ˉg11ˉq(0)+2τkN2, (B.37)

    where

    N1=(a11a22),   N2=(b11b22), (B.38)

    and

    a11=(cy1μ21cx1y1μ31)e2iω10τk+Δ2(cx1μ21cx1y1μ31)+Δ(cαξμ212cx1y1μ31),a22=(by1μ21+b(x1+ξ)y1μ31)+Δ2(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)+Δ(b(αξξ)μ21+2b(x1+ξ)y1μ31),b11=(cy1μ21cx1y1μ31)1+ΔˉΔ(cx1μ21cx1y1μ31)+Re(Δ)(cαξμ212cx1y1μ31),b22=(by1μ21+b(x1+ξ)y1μ31)+ΔˉΔ(b(x1+ξ)μ21+b(x1+ξ)y1μ31p2q3Qy1ν31+pq2Qν21)+Re(Δ)(b(αξξ)μ21+2b(x1+ξ)y1μ31).

    According to the definition of A and Eq (B.31) we have

    01dη(θ)W20(θ)=2iω10τkW20(0)H20(0) (B.39)

    and

    01dη(θ)W11(θ)=H11(0), (B.40)

    where η(θ)=η(0,θ). Substituting Eqs (B.35), (B.36) and (B.37) into (B.31), we notice that

    (iω10τkI01eiω10τkθdη(θ))q(0)=0, (B.41)
    (iω10τkI01eiω10τkθdη(θ))ˉq(0)=0, (B.42)

    it is easy to see

    (2iω10τkI01e2iω10τkθdη(θ))M1=2τkN1, (B.43)
    01dη(θ)M2=2τkN2. (B.44)

    Hence, we further get

    M1=2(2iω10cx1y1μ21+x1e2iω10τkcx1(x1+αξ)μ21by1(y1+αξξ)μ212iω10+b(x1+ξ)y1μ21pq2Ey1ν1)1N1 (B.45)

    and

    M2=2(cx1y1μ21+x1cx1(x1+αξ)μ21by1(y1+αξξ)μ21b(x1+ξ)y1μ21+pq2Ey1ν1)1N2. (B.46)

    From Eqs (B.35) and (B.36), we can determine the values of W20(θ) and W11(θ). g21 be represented by the parameters of Eq (B.1). Therefore, we further calculate the values of c1(0), μ2, β2 and T2, as follows

    c1(0)=i2ω10τk(g20g112|g11|2|g02|23)+g212,μ2=Re{c1(0)}Re{λ(τk)},     β2=2Re{c1(0)},T2=Im{c1(0)}+μ2Im{λ(τk)}ω10τk. (B.47)

    Before finding the maximum value of J(E), the concrete Hamiltonian function is given

    H=E(p1q1Pw)eδt+λ1(rN(1NK)e1(NP)1+e1h1(NP)+e2h2(AP)P)+λ2(n1e1(NP)+n2e2(AP)1+e1h1(NP)+e2h2(AP)PmPq1EP). (C.4)

    where λi=λi(t),i=1,2, are adjoint variables. The condition that the Hamiltonian function H satisfy is presented by

    HE=(p1q1Pw)eδtλ2q1P=0, (C.5)

    The adjoint variables λ1 and λ2 satisfy the following adjoint equations according to Pontryagin's Maximum Principle.

    dλ1dt=HN=λ1(rNKe21h1NP(1+e1h1NP+e2h2AP)2)λ2(n1e1(1+e2h2AP)e1e2h1n2AP(1+e1h1NP+e2h2AP)2),dλ2dt=HP=p1q1Eeδt+λ1(e1NP(e1h1NP+e2h2AP)(1+e1h1NP+e2h2AP)2)+λ2(e1n1NP+e2n2AP(1+e1h1NP+e2h2AP)2). (C.6)

    In order to find the solutions λ1(t), λ2(t) of Eq (C.6), we delete λ2 in Eq (C.6) to obtain a second order differential equation with respect to λ1

    d2λ1dt2+I1dλ1dt+I2λ1=C1eδt, (C.7)

    where

    I1=(rNKe21h1NP(1+e1h1NP+e2h2AP)2)e1n1NP+e2n2AP(1+e1h1NP+e2h2AP)2,I2=(n1e1+e1e2n1h2APe1e2n2h1AP)(e21h1N2P2+e1e2h2ANP2)(1+e1h1NP+e2h2AP)4+e1n1NP+e2n2AP(1+e1h1NP+e2h2AP)2(rNKe21h1NP(1+e1h1NP+e2h2AP)2),C1=(n1e1(1+e2h2AP)e1e2n2h1AP)Ep1q1(1+e1h1NP+e2h2AP)2. (C.8)

    Then, we obtain λ1(t)=O1eδt, where O1=C1δ2I1δ+I2. Set up the equation in a similar way as above d2λ2dt2+I1dλ2dt+I2λ1=C2eδt, we get λ2(t)=O2eδt, where O2=C2δ2I1δ+I2, C2=Ep1q1(δ+rNKe21h1NP(1+e1h1NP+e2h2AP)2). Substituting λ2(t) into (C.5) yields

    E=(δ2I1δ+I2)(p1q1Pw)(p1q1δ+p1q1rNKe21h1p1q1NP(1+e1h1NP+e2h2AP)2)q1P. (C.9)

    Therefore, the values of (Noptimal,Poptimal) and Eoptimal can be obtained by Eq (C.9) and solving the biological equilibrium.

    The optimal harvesting effort at any time is determined by the following optimal harvesting solution

    E(t)={Emax      if  HE>0,Eoptimal  if  HE=0,Emin      if  HE<0, (C.10)

    where Emin is the minimum harvesting effort.

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