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Finite-time stability and optimal control of an impulsive stochastic reaction-diffusion vegetation-water system driven by Lˊevy process with time-varying delay


  • In this paper, a reaction-diffusion vegetation-water system with time-varying delay, impulse and Lˊevy jump is proposed. The existence and uniqueness of the positive solution are proved. Meanwhile, mainly through the principle of comparison, we obtain the sufficient conditions for finite-time stability which reflect the effect of time delay, diffusion, impulse, and noise. Besides, considering the planting, irrigation and other measures, we introduce control variable into the vegetation-water system. In order to save the costs of strategies, the optimal control is analyzed by using the minimum principle. Finally, numerical simulations are shown to illustrate the effectiveness of our theoretical results.

    Citation: Zixiao Xiong, Xining Li, Ming Ye, Qimin Zhang. Finite-time stability and optimal control of an impulsive stochastic reaction-diffusion vegetation-water system driven by Lˊevy process with time-varying delay[J]. Mathematical Biosciences and Engineering, 2021, 18(6): 8462-8498. doi: 10.3934/mbe.2021419

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  • In this paper, a reaction-diffusion vegetation-water system with time-varying delay, impulse and Lˊevy jump is proposed. The existence and uniqueness of the positive solution are proved. Meanwhile, mainly through the principle of comparison, we obtain the sufficient conditions for finite-time stability which reflect the effect of time delay, diffusion, impulse, and noise. Besides, considering the planting, irrigation and other measures, we introduce control variable into the vegetation-water system. In order to save the costs of strategies, the optimal control is analyzed by using the minimum principle. Finally, numerical simulations are shown to illustrate the effectiveness of our theoretical results.



    Vegetation and water resources are important components of the ecosystem. In arid regions, the lack of water resources and the destruction of vegetation lead to desertification. If desertification is formed, it will seriously affect human survival and economic development. From [1], worldwide, economic losses caused by desertification are more than 40 billion dollars every year. On the other hand, in the rainforest ecosystem, abundant vegetation and water resources provide sufficient oxygen for the survival of life on earth. If the rainforest ecosystem is destroyed, life on earth will inevitably suffer the disaster. Therefore, it is of great significance to model a reasonable dynamic system and analyze its dynamic behavior. Meanwhile, studying the optimal control strategy is helpful for the reasonable and effective protection of vegetation ecology.

    In the natural environment, the vegetation-water systems are usually disturbed by human activities and natural disasters, such as planting vegetation, irrigation, pruning vegetation regularly, and so on. These phenomena can be more accurately described by impulsive differential equations. Therefore, in recent years, some results were proposed on modelling impulsive vegetation systems [2,3,4,5]. In these references, only some impulse events that reduce the biomass density of vegetation were considered, such as forest fires. In vegetation restoration and protection, we mainly adopt measures, including planting and irrigation, etc. Obviously, these behaviors can increase the density of vegetation and water. However, the corresponding impulsive vegetation-water systems are rarely analyzed.

    On the other hand, in ecosystem, delay is also a ubiquitous phenomenon that may cause a dramatic changes on dynamic behavior [6,7,8]. In recent years, delay has been taken into consideration in research on vegetation systems [9,10,18]. In [9], Han et al. took constant delay into the vegetation water system and studied the dynamic behavior. In [10], Wang et al. analyzed the asymptotic stability of the equilibrium and Hopf bifurcation in a constant delay vegetation ecosystem. In [11], the authors considered the delay into vegetation-water system and studied the stability and Hopf bifurcation. However, the papers mentioned all consider constant delay. In fact, in real ecology, the delay can be affected by various factors such as temperature, soil moisture content and so on. Therefore, the delay of penetration is related to time. In this paper, we consider the time-varying delay into the vegetation-water system.

    In addition to impulse and delay, there are many achievements evidence that noise also plays a major role in vegetation systems [12,13]. In the real world, it is known to all that there are various environmental factors (such as organic matter, climate and so on) that can affect the ecosystem, which is manifested by fluctuating ecological material density. Recent research results support the importance of stochastic processes in ecosystems [14,15,16]. For example, Pan et al. [17] studied the near-optimal control of a stochastic vegetation-water system. Zeng et al. [18] analyzed the catastrophic regime shifts of a stochastic grazing ecosystem to explore the impact of noise on vegetation degradation. However, the stochastic process they mainly consider is Gaussian white noise in the system. The Gaussian noise is suitable to simulate non-abrupt and uniform environmental disturbances such as small-scale rainfall, temperature change, etc. It is worth noting that the phenomenon of large disturbance exists in nature, such as volcanic eruptions and earthquakes [19]. Meanwhile, there is evidence that the transition from forest to drought will not be smooth but will exhibit sudden transitions. For example, in [20,21], a large-scale, long-term experiment showed that the mortality of vegetation will increase abruptly to 226 and 462 percent in the dry season. These sudden changes may have a profound impact on the natural ecosystems and cannot be ignored [22]. The scholars have done some researches and shown that for abrupt random pulsing phenomenons can be described by the Lˊevy process [23,24]. There are several existing works on the impact of the Lˊevy process on ecosystems. For instance, Zhang et al. [25] considered the Lˊevy process into the grazing ecosystem and analyzed its impact on system dynamics. Larissa et al. [26] introduced Lˊevy process to model the Amazon vegetation ecosystem and analyzed metastability of system. However, there been no research that introduced Lˊevy process into vegetation-water system to analyze dynamic behavior.

    In the last several years, the dynamic behaviors of vegetation system were extensively investigated. For example, R. Lefever and O.Lejeune [30] introduced a single-equation (vegetation biomass density) system and studied the bifurcation theory and the stability of the steady-state solution. Klausmeier et al. established a vegetation-water (soil water) system and explored the Turing instability of the system [31]. Rietkerk et al. proposed a vegetation-water (soil water and surface water) system and analyzed the stability of steady-state solution [32]. Obviously, they mainly paid attention to long-term dynamic behaviors. Noteworthy, finite-time stability plays a significant role in modeling real-life problems and arises in a wide range of applications, such as economic-controlled system, neural networks and so on [33,34,35,36,37]. In arid ecosystems, the density of vegetation and water is closely related to eco-quality. Low-level vegetation and water density means desertification. Meanwhile, because the environmental capacity is limited, the high density of vegetation and water will also harm the ecological environment. Therefore, it is of significance to study the finite-time stability of vegetation-water system.

    On the other hand, as is known to all that controlling drought land and rainforest degradation have posed a huge economic burden. Because of the large affected area, it is costly to use control strategy, such as planting vegetation, rational irrigation, etc. Therefore, from the perspective of ecological economics, how to formulate optimal control strategies to balance the costs and benefits is an important and meaningful question. However, there are few papers introducing control strategies to study optimal control problems in the vegetation system.

    In this paper, we propose a new vegetation-water system and analyze finite-time stability by using comparative principles. Then, we introduce the control variables into the system and analyze the optimal control of the controlled vegetation system by using the minimum principle. In summary, our main contributions are as follows:

    (i) We propose an impulsive stochastic reaction-diffusion vegetation-water system driven by Lˊevy process with time-varying delay. Our model is an extension of literature [2,9,32].

    (ii) The sufficient conditions for finite-time stability are given as theoretical results which reflect the effects of diffusion, impulse, delay, and noise disturbance. Compared with existing work, in the analysis of finite-time stability, our contribution is the study of system with time-varying delay and Lˊevy noise. In order to deal with time-varying delay, we use the idea of classification.

    (iii) The control strategies are considered into the impulsive stochastic vegetation-water system with delay, such as planting vegetation, irrigation, applying chemicals etc. Then, the explicit expression of optimal control is obtained through the minimum principle.

    The remaining structure of the paper is organized as follows: in section 2, a stochastic diffusion vegetation-water system, with varying-time delay, impulse, and Lˊevy jump is established. In section 3, we complete the proof of the existence and uniqueness of the global positive solution. Further, we analyze the finite-time stability of the system and give sufficient conditions for the establishment of stability theorem. In section 4, we analyze the optimal control problem by using the minimum principle under the vegetation-water system with control. In section 5, a numerical simulation is presented to illustrate theoretical results. In section 6, we discuss and summarize the main results of this paper.

    In this section, a vegetation-water system with spatial diffusion, time-varying delay, impulse, noise is proposed. Before driving our system, let us recall a classic vegetation-water system proposed by Rietkerk in [32]

    {ˉu(x,t)t=dˉuΔˉu(x,t)+cgmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)dˉu(x,t),ˉv(x,t)t=dˉvΔˉv(x,t)+k0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,t)gmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)bˉv(x,t),ˉw(x,t)t=dˉwΔˉw(x,t)+Rok0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,t), (2.1)

    here ˉu(x,t), ˉv(x,t), ˉw(x,t) represent the vegetation biomass density, soil water density and surface water density, respectively. Δ is the Laplace operator. The Γ is the boundary of ΓR2. All parameters in model (2.1) are assumed non-negative constants and are described in Table 1. In the following, we complete the construction of the new vegetation system.

    Table 1.  Parameters description.
    Symbol Physical significance Units
    ˉu Plant density g/m2
    ˉv Soil water mm
    ˉw Surface water mm
    dˉu Plant dispersal m2/d
    dˉv Diffusion coefficient for soil water m2/d
    dˉw Diffusion coefficient for surface water m2/d
    c Conversion of water uptake by plants to plant growth gmm1m2
    gm Maximum specific water uptake mmg1m2d1
    d Natural loss rate of plant density due to mortality d1
    k1 Half saturation constant of plant growth and water uptake mm
    k2 Rate at which infiltration increases with specific plant density g/m2
    b Natural loss rate of soil water due to drainage d1
    p Natural loss rate of surface water water due to evaporation d1
    Ro Rainfall mm/d
    f Minimum water infiltration in the absence of plants
    k0 Proportion of surface water available for infiltration d1
    y Perturbation of Poisson process to loss rate d1
    σi (i=1,2,3) Perturbation of random Brownian motion to loss rate d1
    ρi (i=1,2,3) Intensity of the Lˊevy process
    Iku Intensity of the impulse applied to the vegetation
    Ikv Intensity of the impulse applied to the soil water
    Ikw Intensity of the impulse applied to the surface water

     | Show Table
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    (1) Surface water evaporation

    In the real world, it is ubiquity for surface water (mainly refers to rivers) to evaporate under the influence of some factors such as temperature, wind, etc. In arid regions, the problems of low rainfall and high evaporation are widespread. The evaporation of surface water can hinder the supply of soil water and further affects the growth of plants. Therefore, they may be the cause of ecological degradation. For example, in Yinchuan, China, the annual evaporation reaches 2000 mm, but the rainfall is only 200-300 mm and the desertification situation here is serious [38]. For this phenomenon, we take the loss rate of surface water into account in vegetation-water system. The system (2.1) can be transformed to

    {ˉu(x,t)t=dˉuΔˉu(x,t)+cgmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)dˉu(x,t),ˉv(x,t)t=dˉvΔˉv(x,t)+k0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,t)gmˉv(x,t)ˉu(x,t)+k1ˉv(x,t)bˉv(x,t),ˉw(x,t)t=dˉwΔˉw(x,t)+Rok0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,t)pˉw(x,t). (2.2)

    (2) Time-varying delay

    The transfer of surface water to soil water is considered as a time delay process. Meanwhile, because the infiltration rate of surface water is affected by the water content of soil, we take time-varying delay into system (2.2). In Figure 1, we show the time delay from surface water to soil water. Thereby, in infiltration item of system (2.2), we replace ˉw(t) with ˉw(tτ(t)) and get the following system

    {ˉu(x,t)t=dˉuΔˉu(x,t)+cgmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)dˉu(x,t),ˉv(x,t)t=dˉvΔˉv(x,t)+k0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,tτ(t))gmˉv(x,t)ˉu(x,t)+k1ˉv(x,t)bˉv(x,t),ˉw(x,t)t=dˉwΔˉw(x,t)+Rok0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,tτ(t))pˉw(x,t), (2.3)
    Figure 1.  The time delay between surface water and soil water.

    where the τ(t) is bounded, which implies that there is a constant ˉτ>0, such that 0<τ(t)ˉτ. Besides, we assume that 0˙τ(t)η<1. In fact, the hypothesis about ˙τ(t)0 fits the real situation. Because the time required for surface water to penetrate will increase with time. And when there is enough soil water, the time required surface water infiltration will tend to a fixed value ˉτ.

    (3) Impulse phenomenon

    Impulsive phenomena are very common in vegetation ecosystem. For example, human behavior such as planting and felling vegetation, irrigation and so on can be described by impulse differential equations. In this subsection, we introduce the impulse into the vegetation system. The details are as follows:

    (i) We define Iku as the impulse intensity that affects vegetation biomass density. It is worth noting that the planting trees, planting grass and other events correspond to Iku>0 and felling plants correspond to Iku<0. However, based on practical factors, vegetation can not be completely destroyed by impulse events. Meanwhile, the impulse intensity can not be too large. We have reason to assume that 1<IkuImu, where Imu is the maximum allowable impulse on vegetation.

    (ii) We define Ikv, Ikw as the impulse intensities that affects soil water density and surface water density, respectively. Irrigation, rainfall and other events correspond to Ikv>0, Ikw>0 and industrial water, drainage and other events correspond to Ikv<0, Ikw<0. However, from reality, soil water and surface water never thoroughly disappear due to impulse events and the impulse intensity can not be too large, which means that 1<IkvImv, 1<IkwImw, where Imv and Imw are the maximum allowable impulse on soil water and surface water, respectively.

    Therefore, the system (2.3) rewrites as

    {ˉu(x,t)t=dˉuΔˉu(x,t)+cgmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)dˉu(x,t),ˉv(x,t)t=dˉvΔˉv(x,t)+k0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,tτ(t))gmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)du(x,t)=bˉv(x,t),ˉw(x,t)t=dˉwΔˉw(x,t)+Rok0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,tτ(t))pˉw(x,t),}ttk,(kN),t>0,xΓ,ˉu(x,t+k)=(1+Iku)ˉu(x,tk),ˉv(x,t+k)=(1+Ikv)ˉv(x,tk),ˉw(x,t+k)=(1+Ikw)ˉw(x,tk),}t=tk (kN). (2.4)

    where {tk} (kN) is impulsive sequence satisfies 0=t0<t1<t2<<tk<<t=, ϑ(x,t+k)=limtt+kϑ(x,t) (ϑ=u,v,w). We define dm=maxkN{tktk1}, ds=minkN{tktk1}. xΓR2 is a bounded measurable set which means that there are constants bi>0, such that |xi|bi, where xi (i=1,2) are components of spatial variables x.

    (4) Lˊevy processes

    In the real world, there are physical environmental disturbances such as volcanic eruptions, sudden sandstorms, temperature surges and so on, and biological environmental disturbances such as mass migration of herbivores. It can affect the natural loss rate of species, can be modeled by the Lˊevy noise. Therefore, we let

    dd+ρ1dL1(t), bb+ρ2dL2(t), pp+ρ3dL3(t),

    where Li(t) is Lˊevy process which is composed of a Brownian motion with a linear drift term and a superposition of centered (independent) Poisson processes with different jump sizes ˉyY. It follows from the Lˊevy-Itˆo decomposition theorem that

    dLi(t)=¯aidt+¯σidBi(t)+Yˉy˜N(dt,dˉy) (i=1,2,3),

    where ¯ai (day1)R, ¯σi (day1)0, Bi(t) is standard Brownian motion, ˜N(dt,dˉy)=N(dt,dˉy)λ(dˉy)dt is a compensated Poisson process and N(dt,dˉy) is a poisson counting measure with characteristic measure λ on a measurable subset Y(0,) with λ(Y)<. Thus, the model becomes

    {ˉu(x,t)t=(dˉuΔˉu(x,t)+cgmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)¯l1ˉu(x,t))dtρ1¯σ1ˉu(x,t)dB1(t)du(x,t)=ρ1ˉu(x,t)Yˉy˜N(dt,dˉy),ˉv(x,t)t=dˉvΔˉv(x,t)+k0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,tτ(t))gmˉv(x,t)ˉv(x,t)+k1ˉu(x,t)du(x,t)=¯l2ˉv(x,t))dtρ2¯σ2ˉv(x,t)dB2(t)ρ2ˉv(x,t)Yˉy˜N(dt,dˉy),ˉw(x,t)t=dˉwΔˉw(x,t)+Rok0(ˉu(x,t)+k2f)ˉu(x,t)+k2ˉw(x,tτ(t))¯l3ˉw(x,t))dtdu(x,t)=ρ3¯σ3ˉw(x,t)dB3(t)ρ3ˉw(x,t)Yˉy˜N(dt,dˉy), }ttk,(kN),t>0,xΓ,ˉu(x,t+k)=(1+Iku)ˉu(x,tk),ˉv(x,t+k)=(1+Ikv)ˉv(x,tk),ˉw(x,t+k)=(1+Ikw)ˉw(x,tk),}t=tk (kN). (2.5)

    where ¯l1=d+ρ1¯a1, ¯l2=b+ρ2¯a2, ¯l3=p+ρ3¯a3. Besides, we assume that Bi(t) is in dependent of N(t,dˉy). The initial value and boundary condition of system (2.5) are given as follows

     ϑ(x,s)=ψϑ(x,s) (ϑ=u,v,w), xΓ, s(ˉτ,0],
    ϑ(x,t)n=(ϑ(x,t)x1,ϑ(x,t)x2)=0 (ϑ=u,v,w), xΓ, t>0,

    where n is the out normal vector of Γ; ψϑ(x,s) (ϑ=u, v, w) are bounded and continuous functions on (ˉτ,0]×Γ.

    In order to facilitate the subsequent theoretical analysis, we implement the dimensionless processing for the system (2.5) using the method of Zelnik et.al. [12]. Therefore, we obtain the following non-dimensional vegetation-water system with time delay and impulse

    {du(x,t)=(duΔu(x,t)+v(x,t)v(x,t)+1u(x,t)l1u(x,t))dtρ1σ1u(x,t)dB1(t)du(x,t)=ρ1u(x,t)Yy˜N(dt,dy),dv(x,t)=(dvΔv(x,t)+αu(x,t)+fu(x,t)+1w(x,tτ(t))γv(x,t)v(x,t)+1u(x,t)du(x,t)=l2v(x,t))dtρ2σ2v(x,t)dB2(t)ρ2v(x,t)Yy˜N(dt,dy),dw(x,t)=(dwΔw(x,t)+Rαu(x,t)+fu(x,t)+1w(x,tτ(t))l3w(x,t))dtdu(x,t)=ρ3σ3w(x,t)dB3(t)ρ3w(x,t)Yy˜N(dt,dy),}ttk,(kN),t>0,xΓ,u(x,t+k)=(1+Iku)u(x,tk),v(x,t+k)=(1+Ikv)v(x,tk),w(x,t+k)=(1+Ikw)w(x,tk),}t=tk (kN), (2.6)

    where u=ˉuk2, v=ˉvk1, w=k0ˉwcgmk1, du=k0duodwocgm, dv=k0dvodwocgm, dw=1, l1=¯l1cgm, γ=k2ck1, l2=¯l2cgm, R=Rocgmk1, α=k0cgm,  l3=¯l3cgm,  f=f,  σi=¯σicgm (i=1,2,3),  ˉy=ˉycgm,  t=cgmtoriginnal,  x=dwok0xoriginnal. The toriginnal and xoriginnal are the time and space variables before the dimensionless transformation processing.

    Let X={(u,v,w)W2,2,(u,v,w)n=0onΩ}. Define Cb+ as a family of bounded and continuous functions. M+=L2(Γ×[0,),R3+) represents the set of square integrable functions defined on Γ×[0,), which is equipped with the norm , where y(x,t)=(Γy(x,t)yT(x,t)dx)12. y(x,t)=(u(x,t),v(x,t),w(x,t)). Let (Ω, F, (Ft)0tT, P) be a complete filtered probability space with a filtration {(Ft)0tT}. E denotes the probability expectation corresponding to P. Additionally, there is a hypothesis that needs to be given.

    Assumption 2.1 There is a positive constant Li such that Yρiy(ρiy+2m(Γ)2)λ(dy))<Li<+ (i=1,2,3), where m(Γ) is the measure of Γ.

    Remark 2.1 The assumption 2.1 implies that the intensity of random noise is constrained, which follows the biological background.

    In this section, the positivity, existence and uniqueness of the global solution of system (2.6) is analyzed by a method similar to [39,40]. Then, we study the finite-time stability of vegetation-water system. In the end, we introduce control variables into the vegetation-water system and study the optimal control of the control system.

    Theorem 3.1 For any given initial data (ψu(x,s),ψv(x,s),ψw(x,s))Cb+, there is a unique global positive solution (u(x,t),v(x,t),w(x,t)) of system (2.6) on t0 almost surely, which means the solution will remain in M+ with probability 1.

    The proof of Theorem 3.1 is given in Appendix.

    Definition 3.2 Given positive number T, B1, B2 with B1<B2, system is said to be finite-time stabile with respect to (T,B1,B2), if any t[0,T],

    y(0)=supˉτs0Γy(x,t)yT(x,t)dxB1Ey(t)=EΓy(x,t)yT(x,t)B2,

    where y(x,t)=(u(x,t),v(x,t),w(x,t)).

    Remark 3.3 Definition 3.2 implies that when the initial value of the state variable is within a given limit, it does not exceed the given threshold in a finite time. The image of finite-time stability is displayed in Figure 2.

    Figure 2.  Illustration of finite-time stability. P is the initial value of the state variable.

    In the following, we give the theorem of finite-time stability of impulsive stochastic reaction-diffusion system with time-varying delay. We present some parallel sufficient conditions of finite-time stability of the system. These conditions reflect the influence of random disturbance and spatial diffusion on finite-time stability. Before proposing the theorem, assign

    c1=lnθdm+|K3|, c2=lnθdm, c3=lnθds+K3, c4=lnθds, ω=lnB2ln(B1+|K2K3|),θ=max{(1+Iku)2,(1+Ikv)2,(1+Ikw)2},  K2=m(Γ), K4=α(1+f),K3u=1+ρ21σ21+L1l12du2i=1b2i, K3v=α(1+f)+ρ22σ22+L2l22dv2i=1b2i,K3w=R2+α(1+f)+ρ23σ23+L3l32dw2i=1b2i, K3=max{K3u,K3v,K3w}.

    Theorem 3.4 The system (2.6) is finite-time stable with respect to (T,B1,B2) if one of the following condition holds:

    C1:0<θ<1, K30, c1θK4ec2ˉτ<0, lnθω,

    C2:0<θ<1, K30, K4ec1ˉτc2θ0,  (c1+K4θ(1η)ec2ˉτ)T+K4θ(1η)ec2ˉτˉτlnθω, 

    C3:0<θ<1, K3>0, c1>0, (K4+c1)Tlnθω,

    C4:θ1,K3>0, c3>0, (K4+c3)Tω,

    C5:θ1,K3<0, c3>0, (K4+c4)Tω,

    C6:θ1,K3<0, c3<0, (c4+K41ηec4ˉτ)T+K4ˉτ1ηec4ˉτω.

    Proof. For a given number B1, letting supˉτs0Γu2(x,s)+v2(x,s)+w2(x,s)dxB1. Set

    V(t)=Γu2(x,t)dx+Γv2(x,t)dx+Γw2(x,t)dx.

    An application of Itˆo formula yields that

    dV(t)d=2Γduu(x,t)Δu(x,t)+v(x,t)v(x,t)+1u(x,t)2l1u2(x,t)dx+2Γdvv(x,t)Δv(x,t)dV(t)+αu(x,t)+fu(x,t)+1w(x,tτ(t))v(x,t)γv(x,t)v(x,t)+1u(x,t)v(x,t)l2v2(x,t)dxdV(t)+2Γdww(x,t)Δw(x,t)+Rw(x,t)αu(x,t)+fu(x,t)+1w(x,tτ(t))w(x,t)l3w2(x,t)dxdV(t)+YΓ(1ρ1y)2u2(x,t)dxΓu2(x,t)dx+ρ1u(x,t)yΓ2u(x,t)dxdλ(dy)dV(t)+YΓ(1ρ2y)2v2(x,t)dxΓv2(x,t)dx+ρ2v(x,t)yΓ2v(x,t)dxdλ(dy)dV(t)+YΓ(1ρ3y)2w2(x,t)dxΓw2(x,t)dx+ρ3w(x,t)yΓ2w(x,t)dxdλ(dy)dV(t)Γρ1σ1u2(x,t)dB1(x,t)dxΓρ2σ2v2(x,t)dB2(x,t)dxΓρ3σ3w2(x,t)dB3(x,t)dxdV(t)+YΓ(1ρ1y)2u2(x,t)dxΓu2(x,t)dx˜N(dt,dy)+YΓ(1ρ2y)2v2(x,t)dxdV(t)Γv2(x,t)dx˜N(dt,dy)+YΓ(1ρ3y)2w2(x,t)dxΓw2(x,t)dx˜N(dt,dy)dV(t)+Γρ21σ21u2(x,t)+ρ22σ22v2(x,t)+ρ23σ23w2(x,t)dx.

    By using some basic inequalities and applying of Green identity (lemma 2, [41]), we have

    dV(t)d2(mi=1b2iΓduu2(x,t)dx+mi=1b2iΓdvv2(x,t)dx+mi=1b2iΓdww2(x,t)dx)+Γu2(x,t)dxdV(t)Γl1u2(x,t)dx+Γα(1+f)(w2(x,tτ(t))+v2(x,t))dxΓl2v2(x,t)dx+m(Γ)dV(t)+ΓR2w2(x,t)dx+Γα(1+f)(w2(x,tτ(t))+w2(x,t))dxΓl3w2(x,t)dxdV(t)+ΓYρ1y(ρ1y+2m(Γ)2)dλ(dy)u2(x,t)dx+ΓYρ2y(ρ2y+2m(Γ)2)dλ(dy)v2(x,t)dxdV(t)+ΓYρ3y(ρ3y+2m(Γ)2)dλ(dy)w2(x,t)dx+ΓYρ1y(ρ1y2)˜N(dt,dy)u2(x,t)dxdV(t)+ΓYρ2y(ρ2y2)˜N(dt,dy)v2(x,t)dx+ΓYρ3y(ρ3y2)˜N(dt,dy)w2(x,t)dxdV(t)Γρ1σ1u2(x,t)dB1(x,t)dxΓρ2σ2v2(x,t)dB2(x,t)dxΓρ3σ3w2(x,t)dB3(x,t)dxdV(t)+Γρ21σ21u2(x,t)+ρ22σ22v2(x,t)+ρ23σ23w2(x,t)dx (3.1)
    dK2+K3(Γu2(x,t)dx+Γv2(x,t)dx+Γw2(x,t)dx)+K4(Γu2(x,tτ(t))dxdV(t)+Γv2(x,tτ(t))dx+Γw2(x,tτ(t))dx)+ΓYρ1y(ρ1y2)˜N(dt,dy)u2(x,t)dxdV(t)+ΓYρ2y(ρ2y2)˜N(dt,dy)v2(x,t)dx+ΓYρ3y(ρ3y2)˜N(dt,dy)w2(x,t)dxdV(t)Γρ1σ1u2(x,t)dB1(x,t)dxΓρ2σ2v2(x,t)dB2(x,t)dxΓρ3σ3w2(x,t)dB3(x,t)dx.

    where K2=m(Γ), K4=α(1+f), K3=max{1+ρ21σ21+L1l12du2i=1b2i,α(1+f)+ρ22σ22+L2l22dv2i=1b2i,R2+α(1+f)+ρ23σ23+L3l32dw2i=1b2i}.

    For t=tk, one can derive that

    V(u(x,t+k),v(x,t+k),w(x,t+k))d=Γ(1+Iku)2u2(x,tk)dx+Γ(1+Ikv)2v2(x,tk)dx+Γ(1+Ikw)2w2(x,tk)dxdθΓV(tk)dx. (3.2)

    where θ=max{(1+Iku)2,(1+Ikv)2,(1+Ikw)2}. Taking expectation on Eq.(3.1), Eq.(3.2), we get

    dEV(t)K2+K3EV(t)+K4EV(tτ(t)), ttk kN+,
     EV(t+k)θEV(tk).

    Next, we choose b(t) satisfies

    {˙b(t)=K2+K3b(t)+K4b(tτ(t))        ttk,b(t+k)=θb(tk)   t=tk,b(s)=EV(s)  ˉτs0. (3.3)

    It follows from comparison lemma [42] that

    EV(t)b(t).

    According to the method of variation of constant on (3.3), we have

    b(t)=θN(t,0)K2K3+θN(t,0)eK3t(b(0)+K2K3)+t0θN(t,s)[K4b(sτ(s))eK3(ts)]ds, (3.4)

    for t0. Noting that

    tsdmdmN(t,s)tsds.

    Therefore, a direct computation gives that

    exp{N(t,s)lnθ+K3(ts)}dexp{tsdmdmlnθ+K3(ts)}d=exp{(lnθdm+K3)(ts)lnθ}.

    Hence, based on (3.4), for t0, there is

    b(t)θN(t,0)K2K3+e(lnθdm+K3)tθ(b(0)+K2K3)+1θt0e(lnθdm+K3)(ts)[K4b(sτ(s))]ds. (3.5)

    In the following, we continue our analysis under two situations.

    Situation1: 0<θ<1.

    Case C11: K3>0.

    Take a continuous function h(λ)=K4eλˉτθ(λlnθdmK3). We have h()=+, h(0)=K4+θ(K3+lnθdm). Form C1, we can know θ(lnθdm+K3)<K4e(lnθdm+K3)ˉτ. Therefore, we can easily yield that h(0)=θ(lnθdm+K3)+K4<0. Besides, ˙h(λ)=ˉτK4eλˉτθ<0. Therefore, there is at least one number λ1<0 such that K4eλ1ˉτ=θ(λ1lnθdmK3). It is clearly that

    b(t)1θ(b(0)+K2K3)eλ1t,ˉτt<0.

    In the following, we prove the inequality

    b(t)1θ(b(0)+K2K3)eλ1t,t0. (3.6)

    If the inequality is not true, there is a t such that

    b(t)>1θ(b(0)+K2K3)eλ1t, (3.7)

    and

    b(t)1θ(b(0)+K2K3)eλ1t,t<t.

    However, it follows from (3.4) that

    b(t)θN(t,0)K2K3+e(lnθdm+K3)tθ(b(0)+K2K3)+1θt0e(lnθdm+K3)(ts)[K4b(sτ(s))]dsb(t)e(lnθdm+K3)tθ(b(0)+K2K3)+1θt0e(lnθdm+K3)(ts)[K4b(sτ(s))]dsb(t)=e(lnθdm+K3)tθ(b(0)+K2K3+t0e(lnθdm+K3)s[K4b(sτ(s))]ds)b(t)e(lnθdm+K3)tθ(b(0)+K2K3+t0e(lnθdm+K3)s[K4θ(b(o)+K2K3)eλ1(sτ(s))]ds)b(t)e(lnθdm+K3)tθ(b(0)+K2K3+K4θ(b(0)+K2K3)eλ1ˉτt0e(λ1(lnθdm+K3))sds)b(t)e(lnθdm+K3)tθ(b(0)+K2K3+K4(b(o)+K2K3)eλ1ˉτθ(λ1(lnθdm+K3))(e(λ1(lnθdm+K3))t1))b(t)1θ(b(0)+K2K3)eλ1t. (3.8)

    It contradicts (3.7), so (3.6) holds. Furthermore, we have

    EV(t)b(t)1θ(b(0)+K2K3)eλ1t1θ(B1+K2K3).

    Based on C1, we have lnθlnB2ln(B1+K2K3) for K3>0. This implies that EV(t)B2. It shows the desired result.

    Case C12: K3<0.

    From (3.4), we have

    b(t)=θN(t,0)K2K3+θN(t,0)eK3t(b(0)+K2K3)+t0θN(t,s)[K4b(sτ(s))eK3(ts)]ds==exp{(lnθdm)(tdm)}(b(0)K2K3)+1θt0e(lnθdm+K3)(ts)[K4b(sτ(s))]ds==1θelnθdmt(b(0)K2K3)+1θt0e(lnθdm)(ts)[K4b(sτ(s))]ds. (3.9)

    Based on C1, we can obtain θ(lnθdm)<K4e(lnθdm)ˉτ<0. By the same discussion as in C11, we obtain that

    b(t)1θ(b(0)K2K3)eλ2t,t0, (3.10)

    where λ2 is the root of equation h(λ)=K4eλˉτθ(λlnθdm) and λ2<0. C1 implies that lnθlnB2ln(B1K2K3) for K3<0. This means that

    EV(t)b(t)1θ(b(0)K2K3)B2.

    It is the desired result.

    Case C21: K3>0.

    Contrary to C1-1, we consider K4e(lnθdm+K3)ˉτθ(lnθdm+K3)0. Assign

    q1(t)=b(t)e(lnθdm+K3)t>0.

    Form (3.5), 0η<1 and Gronwall inequality [43], one has

    q1(t)1θ(b(0)+K2K3)+1θt0e(lnθdm+K3)(sτ(s))e(lnθdm+K3)τ(s)[K4b(sτ(s))]dsq1(t)1θ(b(0)+K2K3)+1θe(lnθdm+K3)ˉτt0e(lnθdm+K3)(sτ(s))[K4b(sτ(s))]dsq1(t)1θ(b(0)+K2K3)+1θ(1η)e(lnθdm+K3)ˉτtˉτ[K4q1(s)]dsq1(t)1θ(b(0)+K2K3)exp{K4θ(1η)e(lnθdm+K3)ˉτ(t+ˉτ)}.

    Then, there is

    EV(t)b(t)=q1(t)e(lnθdm+K3)t===1θ(B1+K2K3)exp{(lnθdm+K3+K4θ(1η)e(lnθdm+K3)ˉτ)t+K4ˉτθ(1η)e(lnθdm+K3)ˉτ}. (3.11)

    C2 gives that ((lnθdm+K3)+K4θ(1η)e(lnθdm+K3)ˉτ)T+K4ˉτθ(1η)e(lnθdm+K3)ˉτlnθlnB2ln(B1+K2K3). Therefore, we obtain EV(t)B2. It means that the system (2.6) is finite-time stability under condition C1.

    Case C22:  K3<0.

    Contrary to C1-2, we consider K4e(lnθdm)ˉτθ(lnθdm). In this case, choosing

    q2(t)=b(t)elnθdmt.

    Similar discussion as in C21, one obtains

    q2(t)=b(t)elnθdmt==(θN(t,0)K2K3+θN(t,0)eK3t(b(0)+K2K3)+t0θN(t,s)[K4b(sτ(s))eK3(ts)]ds)elnθdmt=1θ(b(0)K2K3)+1θt0elnθdms[K4b(sτ(s))]ds=1θ(b(0)K2K3)+K4(1η)θelnθdmˉτtˉτelnθdmsb(s)ds=1θ(b(0)K2K3)exp{K4(1η)θelnθdmˉτ(t+ˉτ)}

    Further, we can compute that

    EV(t)b(t)=q2(t)elnθdmt=1θ(B1K2K3)exp{(lnθdm+K4(1η)θelnθdmˉτ)T+K4ˉτ(1η)θelnθdmˉτ}. (3.12)

    In view of C2, one can calculate that (lnθdm+K4(1η)θe(lnθdm)ˉτ)T+K4ˉτ(1η)θe(lnθdm)ˉτlnθlnB2ln(B1K2K3). Therefore, EV(t)B2.

    Case C31: K3>0.

    Contrary to the above case, we consider K3+lnθdm>0. Let f(t) satisfy the following equation

    {f(t)=θN(t,0)K2K3+e(lnθdm+K3)tθ(˜f(0)+K2K3)+1θt0e(lnθdm+K3)(ts)[K4f(sτ(s))]ds,  t>0,f(s)=EV(s),ˉτt0, (3.13)

    where ˜f=supˉτ<s<0f(s). By virtue of (3.5) and (3.13), we derive 0b(t)f(t) for tˉτ. Before the following proof, setting

    A1={t |tτ(t), t(0,ˉτ]},A2={t |t>τ(t), t(0,ˉτ]}.

    It is obvious that A1A2=(0,ˉτ]. For tA1, one can obtain

    f(t)f(tτ(t))f(t)1θ(˜f(0)+K2K3)f(t)f(tτ(t))=1θ(˜f(0)+K2K3)(e(lnθdm+K3)t1)+1θt0e(lnθdm+K3)(ts)[K4f(sτ(s))]ds0.

    For tA2(ˉτ,T], a direct calculation leads that

    f(t)f(tτ(t))==(θN(t,0)+θN(tτ(t),0))K2K3+(1θe(lnθdm+K3)t1θe(lnθdm+K3)(tτ(t)))(˜f(0)+K2K3)==+1θt0e(lnθdm+K3)(ts)[K4f(sτ(s))]ds1θtτ(t)0e(lnθdm+K3)(tτ(t)s)[K4f(sτ(s))]ds==(θN(t,0)+θN(tτ(t),0))K2K3+1θe(lnθdm+K3)t(11exp{(lnθdm+K3)τ(t)})(˜f(0)+K2K3)==+1θe(lnθdm+K3)tt0e(lnθdm+K3)s[K4f(sτ(s))]ds1θe(lnθdm+K3)(tτ(t))tτ(t)0e(lnθdm+K3)s×==[K4f(sτ(s))]ds=(θN(t,0)+θN(tτ(t),0))K2K3+1θe(lnθdm+K3)t(11exp{(lnθdm+K3)τ(t)})(˜f(0)+K2K3)==+1θe(lnθdm+K3)(tτ(t))ttτ(t)e(lnθdm+K3)s[K4f(sτ(s))]ds0.

    This implies that f(t)f(tτ(t)) when t>0. Then, in light of (3.13), we can deduce the following inequality

    f(t)1θ(˜f(0)+K2K3)e(lnθdm+K3)t+1θt0e(lnθdm+K3)(ts)[K4f(s)]ds.

    The Gronwall inequalities [43] gives that

    f(t)e(lnθdm+K3)t1θ(˜f(0)+K2K3)eK4t.

    That is to say

    EV(t)b(t)f(t)1θ(˜f(0)+K2K3)e(K4+lnθdm+K3)t1θ(B1+K2K3)e(K4+lnθdm+K3)T.

    By virtue of C3, one can see that (K4+lnθdm+K3)TlnθlnB2ln(B1+K2K3). This implies that EV(t)B2. Then we can obtain the required statement.

    Situation 2: θ1.

    In this situation, one can calculate that

    exp{N(t,s)lnθ+K3(ts)}exp{tsdslnθ+K3(ts)}exp{N(t,s)lnθ+K3(ts)}=exp{(lnθds+K3)(ts)}, (3.14)

    and

    b(t)θN(t,0)K2K3+e(lnθds+K3)t(b(0)+K2K3)+t0e(lnθds+K3)(ts)[K4b(sτ(s))]ds. (3.15)

    It is clear that inequalities (3.15) and (3.5) have the same form and properties. We can use the same method as the discussions in Situation 1, and yield the desired result. For the sake of simplicity, we omit the details.

    Remark 3.5 In the theorem 3.4, we have dealt with sufficient conditions that are more stringent than the actual situation. For example, in C1, we show the system 2.6 is finite-time stable when the condition c1θK4ec2ˉτ<0 holds. In fact, in our proof, we put forward that the system 2.6 is finite time stable under the condition c1θK4ec1ˉτ<0. It is clearly that K4ec2ˉτ<K4ec1ˉτ.

    Remark 3.6 For an ecosystem, the initial material (vegetation and water) density B1 can be estimated. Similarly, the desired maximum density B2 of vegetation and water can also be given. In addition, the desired time T to keep the density of plants and water between B1 and B2 can also be given. Therefore, we can judge whether the system is finite-time stable through the relationship between the parameters.

    Desertification can bring great economic losses. We need to adopt some control strategies to increase the amount of vegetation and water density. There are many strategies for the management of vegetation systems such as replanting, irrigation, and so on. The cost of strategy is inevitable. It is easy to think that the way to save costs is the search for optimal control. In the following, we mainly use the principle of minimum value to find the optimal control in the vegetation system.

    Consider (u(x,t),v(x,t),w(x,t))X where X is defined in preparations. We define a control function set as U=U1U2={πi=πi(x,t)  where (x,t)Γ×{t|[0,T]{tk, (kN)}}|i=1,2,3}{πi=πi(x,tk) where xΓ, tk[0,T] and k{1,N}|i=4,5,6} where the meaning of πi are listed as follows:

    (a) π1 indicates that the planting strategy is used to increase vegetation density.

    (b) π2 is the strategy of applying aquasorb which can reduce the infiltration and loss of soil water [44].

    (c) π3 is the use of chemical substances such as Hexadecanol, Octadecanol, Cetyl and Stearyl alcohols strategy which can inhibit the evaporation of surface water [45,46,47].

    (d) The control strategy of πi (i=4,5,6) can be explained by human control or government intervention.

    Due to the limitation of technology or cost, each control strategy πi has an upper bound πmax. A vegetation model with control strategy can be given as

    {du(x,t)=(duΔu(x,t)+π1u(x,t)+v(x,t)v(x,t)+1u(x,t)l1u(x,t))dtdu(x,t)=ρ1σ1u(x,t)dB1(t)ρ1u(x,t)Yy˜N(dt,dy),dv(x,t)=(dvΔv(x,t)+αu(x,t)+fu(x,t)+1w(x,tτ(t))γv(x,t)v(x,t)+1u(x,t)du(x,t)=(l2π2)v(x,t))dtρ2σ2v(x,t)dB2(t)ρ2v(x,t)Yy˜N(dt,dy),dw(x,t)=(dwΔw(x,t)+Rαu(x,t)+fu(x,t)+1w(x,tτ(t))(l3π3)w(x,t))dtdu(x,t)=ρ3σ3w(x,t)dB3(t)ρ3w(x,t)Yy˜N(dt,dy),}t[0,T],ttk,kN,xΓ,u(x,t+k)u(x,tk)=Ikuπ4u(x,tk),v(x,t+k)v(x,tk)=Ikvπ5v(x,tk),w(x,t+k)w(x,tk)=Ikwπ6w(x,tk),}t=tk (kN), (4.1)

    The conditions of initial value and boundary are the same as system (4.1). The set X is admissible trajectories is given by

    X={X()W2,2(Γ×[0,T];R3)| (4.1) is satisfied},

    and the admissible control set U is given by

    U={U()L(Γ×[0,T];R6)|0<πi(x,t)πmax<1, (x,t)Γ×[0,T]}.

    We consider the objective function

    J(X(),U1())=Nk=1tktk1Γ(P1uP2vP3w+123i=1Qiπi(x,t)2)dxdt,
    J(X(),U2())=Nk=1ΓˉP1uˉP2vˉP3w+126i=4Qiπi(x,tk)2dx.

    It is worth noting that Qi (i=1,26) are the weight constants for control strategies, Pi (ˉPi) (i=1,2,3) are positive weight constant of vegetation, soil water, surface water, respectively. 12Qiπ2i (i=1,2,6) is the cost of control strategies. The square of the control variables means that the cost of strategies is gradually increasing [48]. Our goal is to obtain the most plants and the lowest cost of corresponding control strategy. Therefore, optimal control problem is equivalent to finding the optimal control U in the allowable control set U and determining the corresponding vector function (u,v,w)X to satisfy the objective function:

    J(X(),U())=min(X(),U())X×U(J(X(),U1())+J(X(),U2())). (4.2)

    Further, we introduce adjoint equation and Hamiltonian function [49,50,51,52]

    {H(t,u,v,w,p1,p2,p3)=p1[duΔu+π1u+vv+1ul1u]+p2[dvΔv+αu+fu+1w(tτ(t))dH=γvv+1u(l2π2)v]+p3[dwΔw+Rαu+fu+1w(tτ(t))(l3π3)w]dH=q1ρ1σ1uq2ρ2σ2vq3ρ3σ3wYρ1uyr1(y)λ(dy)Yρ2vyr2(y)λ(dy)dH=Yρ3wyr3(y)λ(dy)P1uP2vP3w+123i=1Qiπ2iIH(tk,u,v,w,p1,p2,p3)=126i=4Qiπi(tk)2+p1(tk)Ikuπ4(tk)u+p2(tk)Ikvπ5(tk)vdH=+p3(tk)Ikwπ6(tk)wˉP1uˉP2vˉP3w.

    Theorem 4.1 The optimal control problem (4.2) with fixed time T admits a unique optimal solution (u,v,w) associated with an optimal control U(x,t) for (x,t)Γ×[0,T]. Moreover, there are adjoint functions pi(,) (i=1,2,3) such as

    {dp1=[duΔp1+(π1l1)p1+vv+1(p1γp2)+α1f(u+1)2w(tτ(t))(p2p3)dp1=ρ1σ1q1Yρ1yr1(y)λ(dy)P1]dt+q1dB1(t)+Yr1(y)˜N(dt,dy)dp2=[dvΔp2+u(v+1)2(p1γp2)(l2π2)p2ρ2σ2q2Yρ2yr2(y)λ(dy)dp1=P2]dt+q2dB2(t)+Yr2(y)˜N(dt,dy)dp3=[dwΔp3+χ[0,Tτ(T)](t)1˙τ(t+ς(t))(p2(t+ς(t))p3(t+ς(t))αu(t+ς(t))+fu(t+ς(t))+1l3p3dp1=+π3p3ρ3σ3q3Yρ3yr3(y)λ(dy)P3]dt+q3dB3(t)+Yr3(y)˜N(dt,dy)}t[0,T],ttk,(kN),xΓ,p1(t+k)p1(tk)=Ikuπ4(tk)p1(tk)ˉP1,p2(t+k)p2(tk)=Ikvπ5(tk)p2(tk)ˉP2,p3(t+k)p3(tk)=Ikwπ6(tk)p3(tk)ˉP3,}t=tk (kN) xΓ,pi(T)=0pix=0}(i=1,2,3), (4.3)

    where ς(t) is introduced to take into account the function dependence of the time-varying delay τ(t) on time; if s=tτ(t), 0tT, is solved for t, ς(t) is given by t=s+ς(s). Additionally, the χ[a,b](t) is a characteristic function defined by

    χ[a,b](t)={1, if t[a,b],0, otherwise.

    Furthermore,

    πi=max[0,min(~πi,πmax)] (i=1,2,3,4,5,6), (4.4)

    where

    ~π1=p1uQ1, ~π2=p2vQ2, ~π3=p3wQ3,~π4=p1IkuuQ4, ~π5=p2IkvvQ5, ~π6=p3IkwwQ6. (4.5)

    The proof is omitted. Interested readers can see the reference [49].

    In this section, numerical simulations are given to illustrate our theoretical results. We select the parameters from the Table 2.

    Table 2.  Parameters Value.
    Symbol Value Reference Symbol Value Reference
    duo 0.1 m2/d [53] c 10 gmm1m2 [53]
    dvo 0.1 m2/d [53] gm 0.05 mmg1m2d1 [53]
    dwo 100 m2/d [53] d (0, 0.5) d1 [32]
    k1 2 mm [32] Ro (0, 3) mm/d [53]
    k2 2 g/m2 [32] f 0.2 [53]
    b (0, 0.5) d1 [53] p (0, 1) d1 Estimated
    k0 (0.05, 0.2) d1 Estimated ρi (i=1,2,3) [0,1] Estimated
    ai (i=1,2,3) [0,1] Estimated σi (i=1,2,3) [0,1] Estimated
    Iϑ (ϑ=u,v,w) (1,1) Estimated

     | Show Table
    DownLoad: CSV

    In this section, we discuss that the system is finite time stable when the sufficient conditions are satisfied. We take Γ=[0.25,0.25], d=0.1, k0=0.05, Ro=3, ρi=0.3, ai=0.5, σi=0.9 (i=1,2,3). Then, one can obtain the m=1, L1=L2=L3=0.09, K2=0.500, K3=0.78090, K4=0.12. Letting B1=1.44, B2=8.41, T=4, (u0(x,t),v0(x,t),w0(x,t)=(0.9,0.9,1) where t(ˉτ,0) and taking Iu=Iv=Iw=0.2, we can get c1=0.3348, θ=0.64(0,1) and y(0)=1.144 by simple calculation. We set the impulse sequence tk={0.4,0.8,1.2,1.6,2,2.4,2.8,3.2,3.6,4,4.4}. Therefore, dm=0.4, ds=0.4. Additionally, we choose

    τ(t)={110fsin(25f2π2t),     t[0,1],1/10f,    t[1,T], (5.1)

    and noise (Figure 3(a)). Through calculation, we have ˉτ=110f=1/2, η=5fπ4=π/4. For noise, we choose a α stable Lˊevy process which is randomly generated and shown in Figure 3(a). A directly calculation shows c1θ=0.2143<K4ec2ˉτ=0.2096<K4ec1ˉτ=0.1419<0, and ln(θ)=0.4463<ln(B2)ln(B1+K2K3)=2.8619. Therefore, the condition C1 is holds. From Figure 4, we can know y(x,0)=1.144<B1=1.2<maxΓ×[0,T]y(x,t)=2.8814<B2=2.9, which means the system (2.6) is finite-time stable.

    Figure 3.  The different state trajectories of α stable lˊevy process where α = 0.9.
    Figure 4.  State trajectories of vegetation-water system which is finite-time stable. The unit of time is d (day) and unit of space is m (meter).

    (1) The role of impulse

    In this section, we consider the impact of impulses on finite-time stability. Obviously, from sufficient conditions, we can find that the finite time stability of system (2.6) can be effected by impulse. In order to intuitively indicate the effect of the impulses through numerical simulation, we keep the system parameters, time delay function τ(t) and noise (Figure 3 (a)) unchanged and show the variation of the finite-time stability of the system (2.6) under different impulse intensities. Therefore, we choose Iu=Iv=Iw=0.

    Through simple calculations, we can get θ=1, c3=0.7809>, K2=0.5, K3=0.7809>0, K4=0.12 and (K4+c3)T=4.0541>ln(B2)+ln(B1+K2/K3)=1.3969. Therefore, the conditions of theorem 3.4 is not satisfied. The results of the numerical simulation of Iu=Iv=Iw=0 are shown in Figure 5. We can find y(1.9154)=4.0297>B2=2.9 which means system (2.6) is not finite time stable. Comparing with the results of Iu=Iv=Iw=0.2 which are shown in Figure 4, we can know that the impulse can affect the finite-time stability.

    Figure 5.  State trajectories of vegetation-water system with Iu=Iv=Iw=0. The unit of time is d (day) and unit of space is m (meter).

    (2) The role of time delay

    Time delay does affect the finite-time stability of system (2.6). For example, in details, the larger ˉτ plays an opposite role in satisfying the inequality c1θK4ec2ˉτ in C1. Retaining the system parameters, the impulse intensity and noise (Figure 3 (a)) unchanged, we choose τ2(t)=ˉτ2=4.5.

    Through a direct calculation, it can be known that η=0, θ=0.64<1, K2=0.5, K3=0.7809>0, K4=0.12, c1=0.3348 and (c1+K4/θ/(1η)exp(c1ˉτ))T+K4ˉτ/θ/(1η)exp(c1ˉτ)ln(θ)=6.5531>ln(B2)+ln(B1+K2/K3)=1.3969, which means the conditions of theorem 3.4 is not satisfied. Further, from Figure 6, we find y(3.3980)=4.0454>2.9=B2 which implies the system is not finite-time stable. Compared with ˉτ=1/2 in Figure 4, the change of delay affects the finite-time stability.

    Figure 6.  State trajectories of vegetation-water system with ˉτ=4.5. The unit of time is d (day) and unit of space is m (meter).

    (3) The role of noise

    It is essential to analyze the impact of environmental noise. For comparison, we choose ρi=0 and ρi=0.5 (i=1,2,3) to carry out numerical simulation. The time delay function τ(t), noise path as Figure 3(a) and system parameters except ρi (i=1,2,3) are also unchanged.

    When ρi=0 (i=1,2,3), we have ln(θ)=0.4463<ln(B2)ln(B1+K2K3)=1.3918 which means the system is finite time stable. Meanwhile, through calculation, when ρi=0.5 (i=1,2,3), the sufficient condition for finite-time stability also is not satisfied. The results of the numerical simulation are shown in Figures 7 and 8. Comparing with the ρi=0.3 (i=1,2,3) in Figure 4, we can observe that noise intensity does affect the finite-time stability.

    Figure 7.  State trajectories of vegetation-water system with noise intensity ρi=0 (i=1,2,3). The unit of time is d (day) and unit of space is m (meter).
    Figure 8.  State trajectories of vegetation-water system with noise intensity ρi=0.5 (i=1,2,3). The unit of time is d (day) and unit of space is m (meter).

    (4) The role of diffusion

    In this section we mainly analyze the impact of the diffusion on finite-time stability. In the ecological environment, different types of plants have different diffusion intensities. The vegetation structure of the area can be changed through human planting, etc. However, the diffusion strength of water is fixed and not easily changed. Therefore, we adjust the diffusion coefficient of vegetation to analyze the impact of diffusion. We choose duo=10 (m2/d) while keeping all other parameters unchanged.

    Through calculation, it can be obtain that du=0.1, θ=0.64<1, K2=0.5, K3=0.0991 and ln(θ)=0.4463>ln(B2)ln(B1+K2K3)=0.2599. This is obvious that the conditions of theorem 3.4 is not hold. The results of the numerical simulation are shown in Figure 9 which confirmed the analysis. Comparing with the results of duo=0.1 (m2/d) which are shown in Figure 4, we know that diffusion can affect the finite-time stability.''

    Figure 9.  State trajectories of vegetation-water system with duo=10. The unit of time is d (day) and unit of space is m (meter).

    In this section, we mainly show optimal control through numerical simulation. We choose t[0,300], x[5,5], d=0.35, b=0.5, z=0.7, ai=0.2, σi=0.2, ρi=0.1, qi=0.2, ri=0.2, Pi=1, ˉPi=1, Qi=1 (i=1,2,4,5,6), Q3=5, Iku=Ikv=Ikw=0.2 where i=1,2,3. We set the impulse sequence tk={25,50,75,100,125,150,175,200,225,250,275} and choose noise (Figure 3 (b)). Other parameters can be found in Table 2. Because of technical limitations, we set the maximum value of the control variable π1(0,0.3), π2(0,0.4), π3(0,0.5), π4(0,2), π5(0,2), π6(0,2).

    From (4.1), (4.3), (4.5), we can get the numerical solution of optimal control which are shown in Figures 9 and 10. Meanwhile, under optimal control, state trajectories of vegetation-water system is shown in Figure 11 (a). For comparison, we give state trajectories of vegetation-water system without control, which is shown in Figure 11(b). Obviously, the biomass density of vegetation has increased significantly under control. From the view of ecology, this is beneficial to the ecological environment.

    Figure 10.  The three-dimensional diagram of control variable π1, π2, π3.
    Figure 11.  The two-dimensional cross section of control variable π1, π2, π3 and control variable for impulse π4, π5, π6.
    Figure 12.  State trajectories of vegetation-water system under optimal control.

    The desertification phenomenon caused by the destruction of the ecological environment by human beings is becoming more and more serious. Severe desertification may cause a food crisis and bring the disaster. Therefore, it is necessary for us to study the dynamics of vegetation-water system in arid areas and consider control strategies. In this paper, we propose a vegetation-water system with delay, impulse and noise. Through the proof, we show that the system has a unique global positive solution. Different from the analysis of the long-term dynamic behavior, we give the sufficient conditions for the finite-time stability of the system. It is worth noting that what we analyze is the finite-time stability of the system with time-varying delay. Some simulations are provided to support the theoretical results. Furthermore, we considered several control strategies and formulated an optimal control strategy to increase the density of vegetation. Through numerical algorithm, the numerical path for optimal control is given.

    It is well-known that the initial values and parameters can affect the dynamic behavior of the system [54,55]. Obviously, this phenomenon can also be observed from the conditions of Theorem 3.4. For example, from C2, we can find that delay has a negative impact on the finite-time stability. As the delay increases, the system may lose finite-time stability, which is shown in Figure 6. The effect of diffusion coefficients du, dv, dw, noise intensities σi, Li (i=1,2,3) and impulse intensities Iu, Iv, Iw on the finite-time stability also can be obtained from Theorem 3.4 via similar discussion. Furthermore, through the analysis, we naturally raise a question. Whether changes in parameters can cause more complex dynamics of the system, such as the change of basins of attraction [54] and the generation of branching phenomena [55]. These will also be our further investigation.

    The authors thank the editor and referees for their careful reading and valuable comments. The research was supported in part by the National Natural Science Foundation of China (No. 12161068) and Ningxia Natural Science Foundation (No. 2020AAC03065).

    The authors declare there is no conflict of interest.

    The proof of Theorem 3.1 is as follows

    Proof Considering the following stochastic partial differential equation without impulse:

    {dX(x,t)=(duΔX(x,t)+Av(t)Y(x,t)Av(t)Y(x,t)+1X(x,t)(l1Au(t)ln(1+Iku))X(x,t))dtdX(x,t)=ρ1σ1X(x,t)dB1(t)ρ1X(x,t)Yy˜N(dt,dy),dY(x,t)=(dvΔY(x,t)+αAv(t)1Au(t)X(x,t)+fAu(t)X(x,t)+1Aw(tτ(t))Z(x,tτ(t))dY(x,t)=(l2Av(t)ln(1+Ikv))Y(x,t)γAv(t)1Av(t)Y(x,t)Av(t)Y(x,t)+1Au(t)X(x,t))dtdY(x,t)=ρ2σ2Y(x,t)dB2(t)ρ2Y(x,t)Yy˜N(dt,dy),dZ(x,t)=(dwΔZ(x,t)+RAw(t)1αAu(t)X(x,t)+fAu(t)X(x,t)+1Aw(tτ(t))Aw(t)Z(x,tτ(t))dZ(x,t)=(l3Aw(t)ln(1+Ikw))Z(x,t))dtρ3σ3Z(x,t)dB3(t)ρ3Z(x,t)Yy˜N(dt,dy), (6.1)

    with initial value (X(0),Y(0),Z(0))=(u(0),v(0),w(0)), where Aϑ (ϑ=u,v,w) can be defined by

    Aϑ(t)={  1  t[ˉτ,0),(1+Ikϑ)[t]t ttk(1+Ikϑ)1t=tk}t0 (kN). (6.2)

    Clearly, Aϑ (ϑ=u,v,w) is left-continuous, bounded and 1-periodic when t0. Next, we explain that system (2.6) and system (6.1) are equivalent. Let (u(x,t),v(x,t),w(x,t))=(Au(t)X(x,t),Av(t)Y(x,t),Aw(t)Z(x,t)). It can be easily checked that (X(x,t),Y(x,t),Z(x,t)) are continuous on (k,k+1)[0,), kN. For ttk, one can compute

    du=Au(t)X(x,t)+Au(t)dX(x,t)du=Au(t)((duΔX(x,t)+Av(t)Y(x,t)Av(t)Y(x,t)+1X(x,t)(l1Au(t)ln(1+Iku))X(x,t))dtdu=ρ1σ1X(x,t)dB1(t)ρ1X(x,t)Yy˜N(dt,dy))Au(t)ln(1+Iku)X(x,t)du=(duΔu(x,t)+v(x,t)v(x,t)+1u(x,t)l1u(x,t))dtρ1σ1u(x,t)dB1(t)ρ1u(x,t)Yy˜N(dt,dy)). (6.3)

    For k, we have

    u(x,k)=limtkAu(t)X(x,t)=(1+Iku)(k1)kX(x,k)=(1+Iku)1X(x,k)=u(x,k),u(x,k+)=limtk+Au(t)X(x,t)=(1+Iku)kkX(x,k)=X(x,k).

    This means that u(x,k+)=(1+Iku)u(x,k) for t=tk. Similarly, we can derive that

    dv(x,t)=(dvΔv(x,t)+αu(x,t)+fu(x,t)+1w(x,t)(x,tτ(t))γv(x,t)v(x,t)+1u(x,t)l2v(x,t))dtdu(x,t)ρ2σ2v(x,t)dB2(t)ρ2v(x,t)Yy˜N(dt,dy),dw(x,t)=(dwΔw(x,t)+Rαu(x,t)+fu(x,t)+1w(x,tτ(t))l3w(x,t))dtdu(x,t)ρ3σ3w(x,t)dB3(t)ρ2w(x,t)Yy˜N(dt,dy). (6.4)

    In this way, we have shown that the system (6.1) without impulse is equivalent to system (2.6). Therefore, in the following, we just need to analyze the solution of system (6.1).

    Obviously, the coefficients of the system conforming to the local Lipschitz continuous, for any given initial data (X(x,s), Y(x,s), Z(x,s))C(Γ×[ˉτ,0]; R3+), the system (6.1) has a unique maximal local solution (X(x,t),Y(x,t),Z(x,t))) on Γ×[ˉτ,τe), where τe is explosion time. Make k0>0 be sufficiently large number for

    1k0<minΓ×[ˉτ,0]{X(x,t),Y(x,t),Z(x,t)}maxΓ×[ˉτ,0]{X(x,t),Y(x,t),Z(x,t)}<k0.

    Define the stopping time

    τk=inf{t[0,τe):minxΓ,t[0,τe){X(x,t),Y(x,t),Z(x,t)}1k0 or maxxΓ,t[0,τe){X(x,t),Y(x,t),Z(x,t)}k0},

    for each kk0, kN. We set inf = (usually is the empty set). We can easily know that τk is increasing as k. Besides, we set limkτk=τ, whence τ<τe. Hence, if we can show that τ=, then τe= and the solution of system (6.1) is positive.

    Define a C2(R+;R) function

    V(t)=ΓX2(x,t)dx+ΓY2(x,t)dx+ΓZ2(x,t)dx.

    For 0t<τkT, Applying Itˆo formula to V(t) leads to

    dV(t)=2ΓX(x,t)((duΔX(x,t)+Av(t)Y(x,t)Av(t)Y(x,t)+1X(x,t)(l1Au(t)ln(1+Iku))X(x,t))dtρ1σ1X(x,t)×=dB1(t))dx+2ΓY(x,t)((dvΔY(x,t)+αAv(t)1Au(t)X(x,t)+fAu(t)X(x,t)+1Aw(tτ(t))Z(x,tτ(t))
    =(l2Av(t)ln(1+Ikv))Y(x,t)γAv(t)1Av(t)Y(x,t)Av(t)Y(x,t)+1Au(t)X(x,t))dtρ2σ2Y(x,t)dB2(t))dx=+2ΓZ(x,t)((dwΔZ(x,t)+RAw(t)1αAu(t)X(x,t)+fAu(t)X(x,t)+1Aw(tτ(t))Aw(t)Z(x,tτ(t))=(l3Aw(t)ln(1+Ikw))Z(x,t))dtρ3σ3Z(x,t)dB3(t))dx+Γ(ρ21σ21X2(x,t)+ρ22σ22Y2(x,t)=+ρ23σ23Z2(x,t))dtdx+Y[Γ(1ρ1y)2X2(x,t)dxΓX2(x,t)dx]˜N(dt,dy)+Y[Γ(1ρ2y)2Y2(x,t)dx=ΓY2(x,t)dx]˜N(dt,dy)+Y[Γ(1ρ3y)2Z2(x,t)dxΓZ2(x,t)dx]˜N(dt,dy)=+Y[Γ(1ρ1y)2X(x,t)2dxΓX(x,t)2dx+Γ2X(x,t)dxρ1yX(x,t)]λ(dy)dtdx=+ΓY[Γ(1ρ2y)2Y(x,t)2dxΓY(x,t)2dx+Γ2Y(x,t)dxρ2yY(x,t)]λ(dy)dtdx=+ΓY[Γ(1ρ3y)2Z(x,t)2dxΓZ(x,t)2dx+Γ2Z(x,t)dxρ3yZ(x,t)]λ(dy)dtdx.

    Through some simple calculations and Holder inequality, we can get

    dV(t)=2ΓX(x,t)((duΔX(x,t)+Av(t)Y(x,t)Av(t)Y(x,t)+1X(x,t)(l1Au(t)ln(1+Iku))X(x,t))dt=ρ1σ1X(x,t)dB1(t))dx+2ΓY(x,t)((dvΔY(x,t)+αAv(t)1Au(t)X(x,t)+fAu(t)X(x,t)+1×=Aw(tτ(t))Z(x,tτ(t))(l2Av(t)ln(1+Ikv))Y(x,t)γAv(t)1Av(t)Y(x,t)Av(t)Y(x,t)+1×=Au(t)X(x,t))dtρ2σ2Y(x,t)dB2(t))dx+2ΓZ(x,t)((dwΔZ(x,t)+RAw(t)1=αAw(tτ(t))Aw(t)Au(t)X(x,t)+fAu(t)X(x,t)+1Z(x,tτ(t))(l3Aw(t)ln(1+Ikw))Z(x,t))dt=ρ3σ3Z(x,t)dB3(t))dx+Γ(ρ21σ21X2(x,t)+ρ22σ22Y2(x,t)+ρ23σ23Z2(x,t))dtdx=+ΓYρ1y(ρ1y2)˜N(dt,dy)X2(x,t)dx+ΓYρ2y(ρ2y2)˜N(dt,dy)Y2(x,t)dx=+ΓYρ3y(ρ3y2)˜N(dt,dy)Z2(x,t)dx+ΓYρ1y(ρ1y+2m(Γ)2)λ(dy)X(x,t)2dtdx=+ΓYρ2y(ρ2y+2m(Γ)2)λ(dy)Y(x,t)2dtdx+ΓYρ3y(ρ3y+2m(Γ)2)λ(dy)Z(x,t)2dtdx.

    Assign

    LV(t)=ΓX(x,t)(duΔX(x,t)+Av(t)Y(x,t)Av(t)Y(x,t)+1X(x,t)(l1Au(t)ln(1+Iku))X(x,t))dxLV(t)=+ΓY(x,t)(dvΔY(x,t)+αAv(t)1Au(t)X(x,t)+fAu(t)X(x,t)+1Aw(tτ(t))Z(x,tτ(t))LV(t)=(l2Av(t)ln(1+Ikv))Y(x,t)γAv(t)1Av(t)Y(x,t)Av(t)Y(x,t)+1Au(t)X(x,t))dxLV(t)=+ΓZ(x,t)(dwΔZ(x,t)+RAw(t)1αAw(tτ(t))Aw(t)Au(t)X(x,t)+fAu(t)X(x,t)+1Z(x,tτ(t))LV(t)=(l3Aw(t)ln(1+Ikw))Z(x,t))dx+Γ(ρ21σ21X2(x,t)+ρ22σ22Y2(x,t)+ρ23σ23Z2(x,t))dx
    LV(t)=+ΓYρ1y(ρ1y+2m(Γ)2)λ(dy)X(x,t)2dx+ΓYρ2y(ρ2y+2m(Γ)2)λ(dy)Y(x,t)2dxLV(t)=+ΓYρ3y(ρ3y+2m(Γ)2)λ(dy)Z(x,t)2dx.

    In view of the partial integral formula, some basic inequalities and hypothesis (H1), we deduce that

    LV(t)Γdu(X(x,t))2dx+ΓX(x,t)Av(t)Y(x,t)Av(t)Y(x,t)+1X(x,t)dx+ΓAu(t)ln(1+Iku)X2(x,t)dx=ΓY(x,t)dv(Y(x,t))2dx+ΓY(x,t)αAv(t)1Au(t)X(x,t)+fAu(t)X(x,t)+1Aw(tτ(t))Z(x,tτ(t))dx=+ΓγAv(t)1Av(t)Y(x,t)Av(t)Y(x,t)+1Au(t)X(x,t)Y(x,t)dx+ΓAv(t)ln(1+IkvY2(x,t)dx=Γdw(Z(x,t))2dx+ΓRAw(t)1Z(x,t)dx+ΓαAu(t)X(x,t)+fAu(t)X(x,t)+1Aw(tτ(t))Aw(t)Z(x,tτ(t))=Z(t)dx+ΓAw(t)ln(1+Ikw)Z2(x,t)dx+Γ(ρ21σ21X2(x,t)+ρ22σ22Y2(x,t)+ρ23σ23Z2(x,t))dx=+ΓYρ1y(ρ1y+2m(Γ)2)λ(dy)X(x,t)2dx+ΓYρ2y(ρ2y+2m(Γ)2)λ(dy)Y(x,t)2dx=+ΓYρ3y(ρ3y+2m(Γ)2)λ(dy)Z(x,t)2dxΓ(1+Au(t)ln(1+Iku)+γAv(t)1Au(t)+ρ21σ21)X2(x,t)dtdx+RAw(t)1m(Γ)=+Γα(Av(t)1(1+f)Aw(tτ(t))+Av(t)ln(1+Ikv)+γAv(t)1Au(t)+ρ22σ22)Y2(x,t)dtdx=+Γ(αAv(t)1(1+f)Aw(tτ(t))+α(1+f)Aw(tτ(t))A1w(t))Z2(x,tτ(t))dtdx=+Γ(1+Aw(t)ln(1+Ikw)+α(1+f)Aw(tτ(t))A1w(t))Z2(x,tτ(t)+ρ23σ23)Z2(x,t)dtdx=+ΓYρ1y(ρ1y+2m(Γ)2)λ(dy)X(x,t)2dx+ΓYρ2y(ρ2y+2m(Γ)2)λ(dy)Y(x,t)2dx=+ΓYρ3y(ρ3y+2m(Γ)2)λ(dy)Z(x,t)2dxK0(1+ΓX2(x,t)dx+ΓY2(x,t)dx+ΓZ2(x,t)dx+ΓZ2(x,tτ(t))dx)

    where

    K0=max{supt[0,τkT)(1+Au(t)ln(1+Iku)+ρ21σ21+γAv(t)1Au(t)+L1),K0=max{supt[0,τkT)(Av(t)1(1+f)Aw(tτ(t))+α(1+f)+ρ22σ22+γAv(t)1Au(t)+L2),K0=max{supt[0,τkT)(1+Aw(t)ln(1+Ikw)+α(1+f)Aw(tτ(t))A1w(t))+ρ23σ23+L3),K0=max{supt[0,τkT)(αAv(t)1(1+f)Aw(tτ(t))+α(1+f)Aw(tτ(t))A1w(t)),K0=max{supt[0,τkT)(RAw(t)1m(Γ)).}.

    Therefore, we can know that

    dV(t)=LV(t)dt2Γρ1σ1X(x,t)2dB1(t)+ρ2σ2Y(x,t)2dB2(t)+ρ3σ3Z(x,t)2dB3(t)dxdV(t)+Yρ1y(ρ1y2)˜N(dt,dy)X2(x,t)+Yρ2y(ρ2y2)˜N(dt,dy)Y2(x,t)dV(t)+Yρ3y(ρ3y2)˜N(dt,dy)Z2(x,t) (6.5)

    Integrating bosh sides of (6.5) from 0 to t1τk and taking expectations gives that

    EV(t1τK)=V(0)+Et1τk0(K0(1+V(s)+ΓZ2(x,sτ(s))dx))dsEV(t1τK)V(0)+Et1τk0K0ds+Et1τk0K01ηΓZ2(x,sτ(s))dxd(sτ(s))+Et1τk0K0V(s)dsEV(t1τK)V(0)+E0ˉτK01η(ΓZ2(x,s)dx)ds+Et1τk0K01η(ΓZ2(x,s)dx)dsEV(t1τK=)+K0T+Et1τk0K0V(s)dsEV(t1τK)C1+Et1τk0ΓK0X2(x,s)dx+ΓK0Y2(x,s)dx+ΓK0(1+11η)Z2(x,s)dxdsEV(t1τK)C1+K1t1τk0V(s)ds

    where C1=V(0)+E0ˉτK1η(ΓZ2(x,s)dx)ds+KT<, K1=max{K,K+K1η}. Further, we can drive that

    EV(t1τk)C1+K1Et1τk0V(t)dtC1+K1Et10V(tτk)dtC1+K1t10EV(tτk)dt. (6.6)

    For  t1[0,T], (6.6) holds, then, it follows from Gronwall inequalities [43] that

    EV(t1τk)C1eK1T,0t1T, (6.7)

    for any kk0. Particularly,

    EV(Tτk)C1eK1T, kk0. (6.8)

    Define

    β(k)=infmin{u(x,t),v(x,t),v(x,t)}k, 0tV(t), kk0.

    Thus, (6.8) implies that

    β(k)P(τkT)E(V(τk)IτkT)EV(τkT)C1eK1T. (6.9)

    However, we can easily see that

    limkβ(k)=.

    Letting k in (6.9), one can deduce that P(τT)=0, that is

    P(τT)=1. (6.10)

    For the arbitrariness of T, we must have τ=. Then, the system (6.1) has a unique global positive solution. Therefore, we complete the proof.

    Algorithm

    Step1: for i=1:Nx
         for j=Ntau:0
          ui,j=u0; vi,j=v0; wi,j=w0;
         end
         for j=Nt+1:Nt+Ntau
          p1i,j=0; p2i,j=0; p3i,j=0;
         end
        end
        o=[o1,o2,o3,]     τ(j)=tau
    Step2for i=1:Nx1
         for j=0:Nt1
          ui,j+1=ui,j+State1;  vi,j+1=vi,j+State2;  wi,j+1=wi,j+State3;
         for k=Ntj+1
          p1i,k1=p1i,kAdjoint1;  p2i,k1=p2i,k+1Adjoint2;  p3i,k1=p3i,kAdjoint3;
          for m=1:length(o)
           if j+1=o(m)
            ui,j+1=(1+Ikuπ4i,j)ui,j+1;  vi,j+1=(1+Ikvπ5i,j)vi,j+1;  wi,j+1=(1+Ikwπ6i,j)wi,j+1;
           else
            ui,j+1=ui,j+1;  vi,j+1=vi,j+1;  wi,j+1=wi,j+1;
           end
         end
           if k1=o(m)
            p1i,k1=(1Ikuπ4i,j)p1i,k1+¯P1;  p2i,k1=(1Ikvπ5i,j)p2i,k1+¯P2;
            p3i,k1=(1Ikwπ6i,j)p3i,k1+¯P3;
           else
            p1i,k1=p1i,k1;  p1i,k1=p1i,k1;  p1i,k1=p1i,k1;
           end
          end
         π1i,j=p1i,kui,jQ1; π2i,j=p2i,kvi,jQ2; π3i,j=p3i,kwi,jQ3;
         π4i,j=p4i,kIkuui,jQ4; π5i,j=p5i,kIkvvi,jQ5; π6i,j=p6i,kIkwwi,jQ6;
          end
         u1,j=u2,j; v1,j=v2,j; w1,j=w2,j;uNx,j=uNx1,j; vNx,j=vNx1,j; wNx,j=wNx1,j;
         p11,j=p12,j; p21,j=p22,j; p31,j=p32,j;p1Nx,j=p1Nx1,j; p2Nx,j=p2Nx1,j; p3Nx,j=p3Nx1,j;
         end
         end

     | Show Table
    DownLoad: CSV

    where

    State1=[duui+1,j2ui,j+ui1,jΔ2x+π1ui,j+vi,jui,jvi,j+1l1ui,j]Δt
    State1=ρ1σ1ui,jrandΔtρ212σ1u2i,j(rand21)ΔtZ(n)State2=[dvvi+1,j2vi,j+vi1,jΔ2x+αui,j+fui,j+1wi,jτ(j)γvi,jvi,j+1ui,j(l2π2)vi,j]ΔtState1=ρ2σ2vi,jrandΔtρ222σ2v2i,j(rand21)ΔtZ(n)State3=[dwwi+1,j2wi,j+wi1,jΔ2x+Rαui,j+fui,j+1wi,jτ(j)(l3π3)wi,j]ΔtState1=ρ3σ3wi,jrandΔtρ232σ3w2i,j(rand21)ΔtZ(n)Adjoint1=[dup1i+1,k2p1i,k+p1i1,kΔ2x+(π1l1)p1i,k+vi,jvi,j+1(p1i,kγp2i,k)Adjoint1=+α1f(ui,j+1)2wi,jτ(j)(p2i,kp3i,k)ρ1σ1q1ρ1r1P1]Δt+q1randΔtZ(n)Adjoint2=[dvp2i+1,k2p2i,k+p2i1,kΔ2x+(l2π2)p2i,k+ui,j(vi,j+1)2(p1i,kγp2i,k)ρ2σ2q2ρ2r2P2]ΔtAdjoint1=+q2randΔtZ(n)Adjoint3=[dwp3i+1,k2p3i,k+p3i1,kΔ2x+χ[0,Ntτ(Nt)](p2i,k+τp3i,k+τ)αui,j+fui,j+1+(π3i,jl3)p3i,kρ3σ3q3Adjoint1=ρ3r3P3]Δt+q3randΔtZ(n)


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