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Article

Extinctions in a Metapopulation with Nonlinear Dispersal Coupling

by
Alexander Korotkov
1,* and
Sergei Petrovskii
1,2,*
1
Faculty of Science, Peoples Friendship University of Russia (RUDN University), 6 Miklukho-Maklaya St., Moscow 117198, Russia
2
School of Computing and Mathematical Sciences, University of Leicester, Leicester LE1 7RH, UK
*
Authors to whom correspondence should be addressed.
Mathematics 2023, 11(20), 4337; https://doi.org/10.3390/math11204337
Submission received: 22 July 2023 / Revised: 12 September 2023 / Accepted: 3 October 2023 / Published: 18 October 2023
(This article belongs to the Section Mathematical Biology)

Abstract

:
Major threats to biodiversity are climate change, habitat fragmentation (in particular, habitat loss), pollution, invasive species, over-exploitation, and epidemics. Over the last decades habitat fragmentation has been given special attention. Many factors are causing biological systems to extinct; therefore, many issues remain poorly understood. In particular, we would like to know more about the effect of the strength of inter-site coupling (e.g., it can represent the speed with which species migrate) on species extinction or persistence in a fragmented habitat consisting of sites with randomly varying properties. To address this problem we use theoretical methods from mathematical analysis, functional analysis, and numerical methods to study a conceptual single-species spatially-discrete system. We state some simple necessary conditions for persistence, prove that this dynamical system is monotone and we prove convergence to a steady-state. For a multi-patch system, we show that the increase of inter-site coupling leads to the formation of clusters—groups of populations whose sizes tend to align as coupling increases. We also introduce a simple one-parameter sufficient condition for a metapopulation to persist.

1. Introduction

In recent decades, significant attention has been directed towards the factors and processes that lead to the survival or extinction of natural populations [1]. This focus has been spurred by ongoing global environmental changes, including the impact of global warming on populations and communities [2]. One specific consequence of global warming is the alteration of species ranges and the fragmentation of habitats. Additionally, habitat fragmentation can occur due to human activities such as forest logging and the construction of new roads. Both habitat fragmentation and general habitat loss have a noticeably detrimental impact on corresponding populations, often leading to species extinctions [3,4]. In fact, habitat fragmentation is widely recognized as the most significant threat to biodiversity on a global scale [5,6].
That is why it is importaint to understand population dynamics in a complex or fragmented habitat and there is indeed a large number empirical and theoretical studies addressing this issue [7,8,9,10,11,12,13,14,15,16]. The most widely used models of population dynamics in a fragmented habitat are metapopulation models [4,17,18,19,20,21,22]. In this framework, a fragmented habitat is viewed as a collection of separate sites, with subpopulations of a species residing in these sites. The subpopulations can be connected either through dispersal between sites or by a shared external factor with spatial correlations, such as weather fluctuations [23,24]. Metapopulation models can either be spatially implicit, where the state of the metapopulation is described by a single global variable, for example the fraction of occupied sites [4,17,18,19], or spatially explicit, where each site is characterized by its own ’local’ variables, such as the size of a specific subpopulation [10,16,25], the propability of a patch being inhabited [26] etc. The former case sometimes can show results similar to lattice models [27,28] and network models [29,30], particularly when the relative locations of sites are explicitly considered.
Numerous studies have investigated the persistence or extinction of metapopulations in relation to habitat geometry [26,31,32], as well as environmental and demographic stochasticity [33,34]. However, there is a noticeable scarcity of research that specifically explores the impact of coupling strength between different sites on persistence or extinction, even though it may be implicitly accounted for through habitat geometry, where coupling strength generally diminishes with greater inter-site distance. Nevertheless, understanding the impact of coupling strength is critical, especially in light of evidence suggesting that inter-site coupling might be altered due to climate change [35,36].
It should be noted that the possibility of extinction depends on the type of density-dependence observed in local population growth. In deterministic models, in a closed system (i.e., without outward migration), populations with logistic growth cannot go extinct because the extinction state is unstable [37,38,39]. However, natural populations rarely conform to logistic growth patterns. Instead, growth rates often exhibit the Allee effect [40,41,42,43], which can be caused by many factors that are often present in real-life situations [44]. The presence of a strong Allee effect significantly alters population dynamics [40,42,43,45,46,47,48]. Notably, the extinction state becomes stable, thus allowing for the possibility of extinction within a closed population.
For a two-site system studied previously [49], it was demonstrated that, subject to certain limitations, an increase in coupling strength can potentially trigger a population outbreak, where the system transitions from a low-density steady state to a high-density one. Mathematically, this transition corresponds to a saddle-node bifurcation, in which the low-density steady state vanishes as a consequence of increased coupling. Although with the model proposed below we focus on extinction rather than outbreaks, It will be shown that the extinction may follow a sufficiently large increase in the coupling strength due to essentially the same mechanism as in [49].
This paper complements the research done in [50] with linear coupling. Here we consider two types of coupling: linear and quadratic. This work differs from the work done in [50] in the sence that we use analytic methods from mathematical analysis, nonlinear functional analysis, monotone dynamical systems theory etc. The methods are used to prove some sufficient conditions for metapopulation persistence. We also show that the solutions are bounded and analytic and we study the asymptotic behavior for some initial conditions. In the end we present a one parameter criterion for a system to persist and estimate the parameter.

2. Materials and Methods

The existence of a non-zero steady-state point for the case with logistic growth will be proved analytically.
For the Allee effect we simulate both types of coupling using the RK45 method, which is programmed in Python using scipy.integrate.solve_ivp. This method with standard settings is perfect for the model with quadratic coupling; for linear coupling we will change the settings, see this section below. The Euler method is not very efficient here because of its slow convergence to the solution. Also the use of higher order methods can be motivated by analyticity of solutions. We do not consider Runge-Kutta methods of higher order because it is not necessary for our tasks. The RK45 method has global error on the order of O ( h 5 ) [51].
We let u i ( 0 ) = max k j and change q with a step size of 0.5 from 0.5 to 20. It was checked in simulations that t = 200 was sufficiently large to ensure the system’s convergence to its steady-state distribution. For linear case we had to set the value of related tolerance to an error r t o l = 10 6 instead of default r t o l = 10 3 to ensure the convergence for large q.
In the section “Two-Patch System” we assume that the solution to the Cauchy problem exists and is unique and continuously differentiable for t 0 , it will be proved in the section “Multi-Patch System”, which is written more formally and states all necessary proofs. The section “Two-Patch System” helps become better acquainted with the model in a simpler case.

3. Two-Patch System

In this section we consider the systems with a linear and quadratic coupling. The linear coupling between two populations u and v is written as q ( u v ) for some coefficient q. The quadratic coupling between two populations u and v is written as q ( u 2 v 2 ) for some coefficient q.
The quadratic coupling is also called density-dependent dispersal. It is due to the fact that u 2 v 2 = ( u + v ) ( u v ) . So the strength of the coupling depends on the total population u + v .
Here we begin with a quadratic coupling as a continuation of the paper [50] with linear model. Then we list some additional properties for a linear coupling which can be analogously proven.
The dynamics of the two-patch system with a quadratic coupling is described by the following equations:
d u 1 d t = f 1 ( u 1 ) + q ( u 2 2 u 1 2 ) , d u 2 d t = f 2 ( u 2 ) + q ( u 1 2 u 2 2 ) ,
where f 1 ,   f 2 are polynomials of the same form such that f 1 ( 0 ) = f 2 ( 0 ) = f 1 ( k 1 ) = f 2 ( k 2 ) = 0 for some positive real numbers k 1 ,   k 2 . Here we are considering polynomials of the forms f i ( u i ) = α i u i ( 1 u i k i ) (logistic growth) and f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) (logistic growth with an Allee effect) with positive coefficients, where β i < k i .
The properties of the system (1) are determined by its steady states; in particular, a long-term persistence of the two subpopulations is only possible if there exists a stable ‘coexistence’ steady state, i.e., a positive solution of the following system:
f 1 ( u 1 ) + q ( u 2 2 u 1 2 ) = 0 , f 2 ( u 2 ) + q ( u 1 2 u 2 2 ) = 0 .
From (2) we readly get:
f 1 ( u 1 ) + f 2 ( u 2 ) = 0 .
If q 0 , the system (2) can be rewritten as
u 2 2 = u 1 2 1 q f 1 ( u 1 ) , u 1 2 = u 2 2 1 q f 2 ( u 2 )
When q , we get u 1 = u 2 .
Let u 1 ( 0 ) = u 01 , u 2 ( 0 ) = u 02 . By u ^ 1 , u ^ 2 further we will denote the steady state values for these initial conditions if they exist ( in a sence that u 1 ( t ) u ^ 1 , u 2 ( t ) u ^ 2 , when t ).
If there are steady state values, then f 1 ( u ^ 1 ) + f 2 ( u ^ 2 ) = 0 . So the Equation (3) is a necessary condition for a point ( u ^ 1 , u ^ 2 ) to be a steady state point.
We also define u ¯ = u 1 + u 2 2 , u ¯ 0 = u ¯ ( 0 ) , d u ¯ d t = f 1 ( u 1 ) + f 2 ( u 2 ) 2 , Z ( f ) = { u | f ( u ) = 0 } .
The case q = 0 is not very interesting because the system (2) is simplified to f ( u 1 ) = 0 , f ( u 2 ) = 0 , hence, a point ( u ^ 1 , u ^ 2 ) is a steady state point iff ( u ^ 1 , u ^ 2 ) Z ( f 1 ) × Z ( f 2 ) = { ( u 1 , u 2 ) | f ( u 1 ) = 0 , f ( u 2 ) = 0 } .
There is another trivial case which is covered by Lemma 1.
Lemma 1.
Let Z ( f ) = { u | f ( u ) = 0 } . Then for any u ^ Z ( f 1 ) Z ( f 2 ) we have a steady state point ( u ^ , u ^ ) .
Proof. 
We fix any u ^ Z ( f 1 ) Z ( f 2 ) . Let u 01 = u ^ , u 02 = u ^ . Then d u 1 d t ( 0 ) = d u 2 d t ( 0 ) = 0 , hence, the point ( u ^ , u ^ ) is a steady state point. □
Now we consider more specific models: logistic growth and logistic growth with an Allee effect. For the logistic growth the case k 1 = k 2 is trivial, for other two cases it is enough to consider an example 1 below because another one becomes the example 1, if we change indexes.
Example 1.
f i ( u i ) = α i u i ( 1 u i k i ) , i = 1 , 2 , k 1 > k 2 ; u 1 ( 0 ) = k 2 , u 2 ( 0 ) = k 2 , q 0 . Then there is a non-zero steady state point.
Proof. 
We know that d u 1 d t | u 1 = u 2 0 > 0 for u 1 = u 2 < k 1 , hence, for all t > 0 we have u 1 ( t ) > u 2 ( t ) . We note that d u ¯ d t > 0 when u 1 [ 0 ; k 1 ] , u 2 [ 0 ; k 2 ] . This means that the population cannot extinct because u ¯ ( t ) > k 2 for all t > 0 , in other words, we got that for all t > 0   u 1 ( t ) > u 2 ( t ) > k 2 .
Let us now consider the behavior as t (Figure 1). We know that d u 1 d t ( 0 ) > 0 , the function d u 1 d t is continuous, hence, it is positive in some neighborhood. It is also clear that for i = 1 there exists t i > 0 ( t i may be infinity) such that d u 1 d t ( t i ) = 0 , otherwise there would be some constant C i > 0 such that d u 1 d t > C i that would lead to u 1 —it is a contradiction. So we have d u 1 d t ( t i ) = 0 , and two cases: t i = , and t i . If we have more than one point t i we number the set T = { t i R { } | d u 1 d t ( t i ) = 0 } in such way that for any integer i between 2 and c a r d ( T ) we will have t i 1 < t i (the set T is no more than countable because d u 2 d t > 0 ).
Let us first assume that t i . d u 2 d t > 0 while d u 1 d t > 0 , nontrivial solution of an autonomous system cannot approach a fixed point in finite time, hence, we have
d u 1 d t ( t i ) = 0 , d u 2 d t ( t i ) > 0 ,
hence, for some ε i > 0 for all ε ( 0 ; ε i ] we have d u 1 d t ( t i + ε ) > 0 , d u 2 d t ( t i + ε ) > 0 . Repeating these actions again, if the function d u 1 d t has infinite number of t i such that d u 1 d t ( t i ) = 0 and d u 1 d t > 0 in some deleted neighborhood, we get that for any i N { 1 } t i 1 < t i and
d u 1 d t ( t i ) = 0 , d u 2 d t ( t i ) > 0 .
It means that d u ¯ d t ( t ) > 0 for all t [ 0 ; ) . The derivative d u ¯ d t ( t ) must approach zero, otherwise there would be a constant C > 0 such that d u ¯ d t ( t ) > C for all t [ 0 ; ] , leading to u 1 ( u ¯ < u 1 ) , which contradicts with u 1 k 1 . Therefore, d u ¯ d t ( ) = d u 1 d t ( ) = d u 2 d t ( ) = 0 because all the derivatives were non-negative. It means that there is a non-zero steady-state point ( u ¯ 1 , u ¯ 2 ) . Moreover, we also prooved that T , and that d u 2 d t > 0 while d u 1 d t 0 .
We are left to prove that there is a non-zero steady-state point ( u ^ 1 , u ^ 2 ) in case of finite number of zeros of the derivative d u 1 d t . If we let t 0 = 0 there is an index i such that t i 1 < t i = , ε i = , for all ε ( 0 ; ) we have d u 1 d t ( t i 1 + ε ) > 0 , d u 2 d t ( t i 1 + ε ) > 0 . It means again that d u ¯ d t ( t ) > 0 for all t [ 0 ; ) , hence, d u ¯ d t ( ) = d u 1 d t ( ) = d u 2 d t ( ) = 0 , and there is a non-zero steady-state point ( u ^ 1 , u ^ 2 ) . □
All stated above gives us a proof of a following theorem:
Theorem 1.
The system (1) with logistic growth functions has a non-zero steady state point.
Remark. 
Another proof of Theorem 1 is given in the Section 4.1 (Theorem 6).
Example 2.
f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) , i = 1 , 2 , k 1 > k 2 , β 1 < k 2 ; u 1 ( 0 ) = k 2 , u 2 ( 0 ) = k 2 . There is a non-zero steady state point—the proof is identical to the proof in the Example 1.
Further we will consider the system with f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) , i = 1 , 2 , k 1 > k 2 ,   β 1 > k 2 .
Firstly, we note that if q max u 2 ( β 2 ; k 2 ) f 2 ( u 2 ) u 2 2 , then there is a steady state point ( u ¯ 1 ; u ¯ 2 ) , u ¯ 1 < u ¯ 2 ( β 2 ; k 2 ] . For q = 0 it is obvious. For q > 0 , indeed, this means that there exists u 02 ( β 2 ; k 2 ) (that will be the initial condition for u 2 , and 0 for u 1 ) such that f 2 ( u 20 ) q u 20 2 0 . d u 2 d t d u 2 d t | u 1 0 0 , f 2 ( k 2 ) + q ( u 1 2 k 2 2 ) = q ( u 1 2 k 2 2 ) , d u 1 d t | u 2 = u 1 k 2 < 0 , hence u 1 ( t ) < u 2 ( t ) k 2 for all t > 0 . The function u 2 as a monotone bounded continiously differentiable function has a limit u ^ 2 [ u 02 ; k 2 ] as t . d u 1 d t > d u 1 d t | u 2 = c o n s t > 0 for all t, but d u 1 d t must approach 0, otherwise it contradicts with the condition d u 1 d t | u 2 = u 1 k 2 < 0 , hence, there is a limit u ^ 1 ( 0 , u ^ 2 ] .
Now we consider a system with a linear coupling:
d u 1 d t = f 1 ( u 1 ) + q ( u 2 u 1 ) , d u 2 d t = f 2 ( u 2 ) + q ( u 1 u 2 ) ,
where f 1 ,   f 2 are of the same types as in (1).
In this case Examples 1 and 2 will have the same proofs as in (1) because we used only monotone property of the functions and their transitional points, which are the same.
Further for the case f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) , i = 1 , 2 , k 1 > k 2 , β 1 > k 2 we in the same way get that if q max u 2 ( β 2 ; k 2 ) f 2 ( u 2 ) u 2 then we have a non-zero steady state point.
Remark. 
Local extrema of the functions f i in the system with the Allee effect can be easily computed:
f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) = α i k i u i 3 + α i ( β i + k i ) k i u i 2 α i β i u i
f ( u i ) = 3 α i k i u i 2 + 2 α i ( β i + k i ) k i u i α i β i
u i m a x = β i + k i + ( β i + k i ) 2 3 β i k i 3
u i m i n = β i + k i ( β i + k i ) 2 3 β i k i 3
That helps us to state the following theorem.
Theorem 2.
Let q 0 . For both systems (1) and (5) there is a sufficient condition for the case with f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) , i = 1 , 2 , k 1 > k 2 , β 1 > k 2 :
f 1 ( u 1 m a x ) + min u 2 [ β 1 ; u 1 m a x ] f 2 ( u 2 ) 0
then we have a non-zero steady state ( u 1 * , u 2 * ) with u 1 * , u 2 * [ β 1 ; u 1 m a x ] .
We note that the condition does not include the parameter q meaning that the system will have a non-zero steady-state point for all q > 0 . Now let us prove this sufficient condition.
Proof. 
Let Q i = max u i [ β 1 ; u 1 m a x ] f i ( u i ) , R i = min u i [ β 1 ; u 1 m a x ] f i ( u i ) . Then we have Q 1 R 2 .
We need to prove that there is always an intersection of curves l 1 ,   l 2 on [ 0 ; + ) × [ 0 ; + ) { ( 0 , 0 ) } , where the curves are defined by the following implicit equations:
l 1 : f 1 ( u 11 ) + q d ( u 21 , u 11 ) = 0 ;
l 2 : f 2 ( u 22 ) + q d ( u 12 , u 22 ) = 0 ;
where d ( u 1 , u 2 ) = u 1 u 2 for the case without the Allee effect and d ( u 1 , u 2 ) = u 1 2 u 2 2 for the case with the Allee effect. This is equivalent to
q d ( u 11 , u 21 ) = f 1 ( u 11 ) ; q d ( u 12 , u 22 ) = f 2 ( u 22 ) .
Then on the set [ β 1 ; k 1 ] × [ β 1 ; k 1 ] we have
0 R 1 q d ( u 11 , u 21 ) Q 1 q ; 0 < Q 2 q d ( u 12 , u 22 ) R 2 q ;
moreover, d may take all values in between R 1 q , Q 1 q , and Q 2 q , R 2 q respectively due to continuity of all functions. We have an inequality Q 1 R 2 , hence, 0 d ( u 12 , u 22 ) Q 1 q .
Therefore, letting u 1 = u 11 = u 12 and getting u 21 ( u 1 ) and u 22 ( u 1 ) from (7) and (8) for u 1 [ β 1 ; k 1 ] (for the (7) we firstly get u 1 ( u 21 ) and then use the Cardano method (see [52], p. 135–140) to get the inverse of a cubic function), we finally get that we have a continuous function of one variable g ( u 1 ) = d ( u 1 , u 21 ( u 1 ) ) d ( u 1 , u 22 ( u 1 ) ) such that g ( β 1 ) = d ( β 1 , β 1 ) d ( β 1 , u 22 ( u 1 ) ) = d ( β 1 , u 22 ( u 1 ) ) < 0 because u 22 ( u 1 ) < β 1 , and for u 1 m a x we have g ( u 1 m a x ) = d ( u 1 m a x , u 21 ( u 1 m a x ) ) d ( u 1 m a x , u 22 ( u 1 m a x ) ) = 1 q ( f 1 ( u 1 m a x ) + f 2 ( u 22 ( u 1 m a x ) ) ) 1 q ( Q 1 + R 2 ) 0 because u 22 ( u 1 m a x ) [ k 2 ; u 1 m a x ] , hence, f 2 ( u 22 ( u 1 m a x ) ) > R 2 . Therefore, if g ( u 1 m a x ) > 0 then, by the intermediate value theorem [53], there is a point u 1 * ( β 1 ; u 1 m a x ) or if g ( u 1 m a x ) = 0 then there is a point u 1 * = u 1 m a x such that d ( u 1 * , u 21 ( u 1 * ) ) = d ( u 1 * , u 22 ( u 1 * ) ) and ( u 1 * , u 21 ( u 1 * ) ) is a point on a curve l 1 and ( u 1 , u 22 ( u 1 * ) ) is a point on a curve l 2 . But that means that u 21 ( u 1 * ) = u 22 ( u 1 * ) = : u 2 * . So there is a point ( u 1 * , u 2 * ) [ β 1 ; u 1 m a x ] × [ β 1 ; u 1 m a x ] that lies on both curves. □

4. Multi-Patch System

4.1. Existence and Uniqueness, Steady-State Points

Let N + be the set of positive integers, N N + , R n (for n N + , n N ) be a n-dimentional (topological) vector space over real numbers with a standard euclidean topology (with a norm | | · | | defined for x = ( x 1 , , x n ) R n as | | x | | = i = 1 n x i 2 ). We define R + = [ 0 , ) , 1 , N ¯ = { 1 , , N } . We can define a ball with a center at x R n and with a radius r R + : B ( x , r ) = { ξ R n | | | ξ x | | < r } .
Here we will consider a system of N equations:
d u i d t = f i ( u i ) + j = 1 N q i j d ( u j , u i ) = F i ( u 1 , , u N ) , i 1 , N ¯ ,
where all f i ( u i ) = α i u i ( 1 u i k i ) , α i > 0 , k i > 0 or all f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) , α i > 0 , k i > β i > 0 , d ( u j , u i ) = u j u i or d ( u j , u i ) = u j 2 u i 2 , for all i , j we have q i j 0 .
Or in a shorter form:
d u d t = F ( u ) .
Let u ¯ = 1 N ( u 1 + + u N ) .
Further we sometimes will use a notation u ( t , u 0 ) for the solution of a Cauchy problem
d u d t = F ( u ) , u ( 0 ) = u 0 .
Now we prove the boundedness of solutions with initial conditions u 0 [ a , max k j + a ] N for some a 0 and get some important corollaries from that. We will need a parallelepiped [ a , max k j + a ] N with a 0 in the next section.
Lemma 2.
Let u be a solution for the system (9), let a R be a non-negative constant. If for some t 0 R , i 0 1 , N ¯ we have u i 0 ( t 0 ) = a or u i 0 ( t 0 ) = max k j + a and u j ( t 0 ) [ a , max k j + a ] for all j i 0 then for the case u i 0 ( t 0 ) = a we have d u i 0 d t ( t 0 ) 0 and for the case u i 0 ( t 0 ) = max k j + a we have d u i 0 d t ( t 0 ) 0 .
Proof. 
(1) u i 0 ( t 0 ) = a , hence, f ( u i 0 ( t 0 ) ) 0 and for all j 1 , N ¯ u i 0 ( t 0 ) u j ( t 0 ) [ a , max k j + a ] ; therefore, d u i 0 d t ( t 0 ) = f ( u i 0 ( t 0 ) ) + j = 1 N q i 0 j d ( u j , u i 0 ) 0 .
(2) u i 0 ( t 0 ) = max k j + a , hence, f ( u i 0 ( t 0 ) ) 0 , for all j 1 , N ¯ u i 0 ( t 0 ) u j ( t 0 ) [ a , max k j + a ] and d u i 0 d t ( t 0 ) = f ( u i 0 ( t 0 ) ) + j = 1 N q i 0 j d ( u j , u i 0 ) 0 .  □
Lemma 3.
Let d x d t = g ( x ) be an autonomous system, g : R n R n is a continuously differentiable mapping, n N + . For any solution x of the system we define a set O ( x ) = { ξ | t h e r e i s t 0 R : x ( t 0 ) = ξ } , which is called the orbit of a solution x. Then for any two solutions x 1 , x 2 we either have O ( x 1 ) O ( x 2 ) = or O ( x 1 ) = O ( x 2 ) .
Proof. 
Let x 1 , x 2 be solutions of the system and O ( x 1 ) O ( x 2 ) . Then there are t 1 , t 2 such that x 1 ( t 1 ) = x 2 ( t 2 ) . Let x ( t ) = x 2 ( t + ( t 2 t 1 ) ) . We have d x d t ( t ) = d x 2 d t ( t + ( t 2 t 1 ) ) = g ( x 2 ( t + ( t 2 t 1 ) ) ) = g ( x ( t ) ) , hence, it is a solution. Moreover, x ( t 1 ) = x 2 ( t 2 ) = x 1 ( t 1 ) . Hence, x 2 ( t + ( t 2 t 1 ) ) = x ( t ) = x 1 ( t ) by the Picard-Lindelöf theorem (see [54], p. 86) and O ( x 1 ) = O ( x 2 ) . □
Theorem 3.
Let u be a solution for the system (9), and u ( 0 ) = u 0 [ a ; max k j + a ] N for some a 0 . Then we have a u i ( t ) max k j + a for all i 1 , N ¯ , for all t 0 .
Proof. 
Let us assume that it is true not for all t 0 , S = { τ 0 | for all 0 t τ a u i ( t ) max k j + a for all i 1 , N ¯ } , t 0 = max S . By the definition of t 0 we have the inequality a u i ( t 0 ) max k j + a for all i, but for every neighborhood of the time t 0 we have some points at which the inequality is not true.
All functions u i , i 1 , N ¯ are differential (in particular, continuous) because u is a solution, hence (see [55], p. 61]):
u i ( t 0 + h ) u i ( t 0 ) = ( d u i d t ( t 0 ) + ϕ i ( h ) ) h , lim h 0 ϕ i ( h ) = 0 .
For i such that d u i d t ( t 0 ) 0 we can choose h i > 0 such that for all h : 0 < h < h i the sign of a number d u i d t ( t 0 ) + ϕ i ( h ) is the same as the sign of a number d u i d t ( t 0 ) .
For i such that u i ( t 0 ) ( a ; max k j + a ) we can choose h i > 0 such that for all h : 0 < h < h i we have u i ( t 0 + h ) ( a ; max k j + a ) due to continuity of the function u i .
Let H = min h j . For i such that u i ( t 0 ) ( a ; max k j + a ) for all h : 0 < h < H we have u i ( t 0 + h ) ( a ; max k j + a ) . By the lemma 2 for i such that u i ( t 0 ) = a we have d u i d t ( t 0 ) 0 and for i such that u i ( t 0 ) = max k j + a we have d u i d t ( t 0 ) 0 . Hence, if d u i d t ( t 0 ) > 0 then u i ( t 0 + h ) u i ( t 0 ) > 0 , if d u i d t ( t 0 ) < 0 then u i ( t 0 + h ) u i ( t 0 ) < 0 ; therefore, for all i 1 , N ¯ , for all h : 0 < h < H we have a u i ( t 0 + h ) max k j + a – it is a contradiction.
Now we consider a case when d u i d t ( t 0 ) = 0 . From the system (9) we have d u i d t ( t 0 ) = f i ( u i ( t 0 ) ) + j = 1 N q i j d ( u j ( t 0 ) , u i ( t 0 ) ) . If u i ( t 0 ) = a then we have d ( u j ( t 0 ) , u i ( t 0 ) ) 0 , hence, f i ( u i ( t 0 ) ) = 0 . If u i ( t 0 ) = max k j + a then we have d ( u j ( t 0 ) , u i ( t 0 ) ) 0 , hence, f i ( u i ( t 0 ) ) = 0 . This is only possible when a = 0 .
So now we have d u i d t ( t 0 ) = j = 1 N q i j d ( u j ( t 0 ) , u i ( t 0 ) ) = 0 . Since for all j we have q i j 0 and d ( u j ( t 0 ) , u i ( t 0 ) ) are all of the same sign, we have that for all j it is true that q i j d ( u j ( t 0 ) , u i ( t 0 ) ) = 0 , so either q i j = 0 or u j ( t 0 ) = u i ( t 0 ) , and again by the Lemma 2 for all j such that q i j 0 we get that the sign of a number d u j d t ( t 0 ) is the same as the sign of a number d u i d t ( t 0 ) .
d 2 u i d t 2 ( t 0 ) = j i q i j d u j d t ( t 0 ) for linear coupling , d 2 u i d t 2 ( t 0 ) = 2 j i q i j u j ( t 0 ) d u j d t ( t 0 ) for quadratic coupling .
Let J i = { j | q i j 0 } .
(1) u i ( t 0 ) = 0 . Then if there is j 0 J i such that d u j 0 d t ( t 0 ) > 0 then d 2 u i d t 2 ( t 0 ) > 0 , hence, the function u i has a strict local maximum at a point t 0 [53]—it is a contradiction. In the other case d 2 u i d t 2 ( t 0 ) = 0 . So for all j J i we have d 2 u j d t 2 ( t 0 ) = 0 (in particular, f j ( u j ) ( t 0 ) = 0 ) and d 2 u i d t 2 ( t 0 ) = 0 . We consider an autonomous system
d u i d t = f i ( u i ) + j J i q i j d ( u j , u i ) , d u j d t = f j ( u j ) + l J j q l j d ( u l , u i ) , j J i .
By the Lemma 3 any two of its orbits are either disjoint or coinciding. The system has a steady-state solution u ^ ( t ) = ( 0 , , 0 ) , but we also have u i ( t 0 ) = 0 , u j ( t 0 ) = 0 for all j J i . Therefore, for all t R we have u i ( t ) = 0 , u j ( t ) = 0 for all j J i —it is a contradiction.
(2) u i ( t 0 ) = max k j . Then if there is j 0 J i such that d u j 0 d t ( t 0 ) < 0 then d 2 u i d t 2 ( t 0 ) < 0 , hence, the function u i has a strict local minimum at a point t 0 [53]—it is a contradiction. In the other case d 2 u i d t 2 ( t 0 ) = 0 . So for all j J i we have d 2 u j d t 2 ( t 0 ) = 0 (in particular, f j ( u j ) ( t 0 ) = 0 ) and d 2 u i d t 2 ( t 0 ) = 0 . We consider an autonomous system
d u i d t = f i ( u i ) + j J i q i j d ( u j , u i ) , d u j d t = f j ( u j ) + l J j q l j d ( u l , u i ) , j J i .
By the Lemma 3 any two of its orbits are either disjoint or coinciding. The system has a steady-state solution u ^ ( t ) = ( max k j , , max k j ) , but we also have u i ( t 0 ) = max k j , u j ( t 0 ) = max k j for all j J i . Therefore, for all t R we have u i ( t ) = max k j , u j ( t ) = max k j for all j J i – it is a contradiction. □
Corollary. 
For u ( 0 ) = u 0 [ a ; max k j + a ] N we have a u ¯ k 1 + + k N N max k j + a .
Corollary 
(Picard–Lindelöf theorem). There is b < 0 such that the solution u ( · , u 0 ) : [ b , ) [ a ; max k j + a ] N to the Cauchy problem (10) with an initial condition u ( 0 ) = u 0 [ a ; max k j + a ] N for some a 0 exists and is unique. Moreover, the dynamical system u ( t , ξ ) : [ b , ) × [ a ; max k j + a ] N [ a ; max k j + a ] N is continuous.
Proof. 
The function of the right part of the system and its derivative are bounded on a compact set [ a ; max k j + a ] N (see [55], p. 33]). Then, informally speaking, we can get local solutions (Picard-Lindelöf theorem) [54] with the same parameters and then cover the set [ b , ) × [ a ; max k j + a ] N with the parallelepipeds (of the same “sizes”) from the theorem.
Let us write out a more detailed proof. We write the family of solutions u ( t , ξ ) as a sum u ( t , ξ ) = ξ + v ( t , ξ ) . Then we have an equivalent Cauchy problem
v t ( t , ξ ) = F ( ξ + v ( t , ξ ) ) = G ( t , ξ , v ) , v ( 0 , ξ ) = 0 .
Indeed, let u ( t , ξ ) be a solution to the Cauchy problem (10). Then 0 = u ( 0 , ξ ) ξ = v ( 0 , ξ ) and v t ( t , ξ ) = ( u ξ ) t ( t , ξ ) = u t ( t , ξ ) = F ( u ( t , ξ ) ) = F ( ξ + v ( t , ξ ) ) .
Now let v ( t , ξ ) be a solution to the Cauchy problem (11). Then u ( 0 , ξ ) = ξ + v ( 0 , ξ ) = ξ and u t ( t , ξ ) = ( ξ + v ) t ( t , ξ ) = v t ( t , ξ ) = F ( ξ + v ( t , ξ ) ) = F ( u ( t , ξ ) ) .
Now we consider an equivalent integral equation
v ( t , ξ ) = 0 t G ( τ , ξ , v ( τ , ξ ) ) d τ .
Indeed, let v ( t , ξ ) be a solution to the problem (11). Then v ( t , ξ ) = v ( t , ξ ) v ( 0 , ξ ) = 0 t v t ( τ , ξ ) d τ = 0 t G ( τ , ξ , v ( τ , ξ ) ) d τ (by the fundamental theorem of calculus, see [53]).
Now let v ( t , ξ ) be a solution to the integral Equation (12). Then v ( 0 , ξ ) = 0 and v t ( t , ξ ) = t 0 t G ( τ , ξ , v ( τ , ξ ) ) d τ = G ( t , ξ , v ( t , ξ ) ) [53]. In particular, the solution v ( · , ξ ) is differentiable.
Further we prove that the solution to the integral Equation (12) exists and is unique.
On a compact set Ω = [ d , d ] × [ a c , max k j + a + c ] 2 N [ d , d ] × [ a , max k j + a ] 2 N for some c , d ( 0 , ) the function G is bounded by some constant K. | G ( t , ξ , v 1 ) G ( t , ξ , v 2 ) | = | F ( ξ + v 1 ( t , ξ ) ) F ( ξ + v 2 ( t , ξ ) ) | ( sup v [ a c ; max k j + a + c ] N | | F ( v ) | | ) * | | v 1 v 2 | | . Let M = sup v [ a c ; max k j + a + c ] N | | F ( v ) | | .
We fix ξ [ a , max k j + a ] N .
We choose d > 0 such that
(1) ( t , ξ , v ) Ω , if | t | d , | | ξ ξ | | d and | | v | | K d ;
(2) M d < 1 .
Let C * be a space of continuous functions defined on a “rectangle” R = { ( t , ξ ) | | t | d , | | ξ ξ | | d } such that ρ ( v , 0 ) K d where ρ is a metric on this space defined as ρ ( v ( 1 ) , v ( 2 ) ) = max ( t , ξ ) | v ( 1 ) ( t , ξ ) v ( 2 ) ( t , ξ ) | (the maximum of the continuous function v ( 1 ) v ( 2 ) is correctly defined because the set R is compact). The space C * is a complete metric space as a closed subset of a complete metric space of all continuous functions on R.
We consider another integral equation
ψ ( t , ξ ) = 0 t G ( τ , ξ , ϕ ( τ , ξ ) ) d τ = : ( A ϕ ) ( t , ξ ) , ( t , ξ ) R , ϕ C * ,
which defines an operator A such that ψ = A ϕ . Now we prove that A : C * C * is a contraction mapping ([54], p. 82]) from the complete metric space C * to itself and use the contraction mapping theorem [54] to show that there is a unique fixed point u C * such that u = A u .
For ϕ C * and ( t , ξ ) R we have
| ψ ( t , ξ ) | = 0 t G ( t , ξ , ϕ ( τ , ξ ) ) d τ K d .
Hence, ρ ( ψ , 0 ) K d and ψ C * . That means that A ( C * ) C * . Moreover, for ϕ 1 , ϕ 2 C * and ψ 1 , ψ 2 such that ψ 1 = A ϕ 1 , ψ 2 = A ϕ 2 we have ρ ( ψ 1 , ψ 2 ) 0 d max ( t , ξ ) | G ( t , ξ , ϕ 1 ( τ , ξ ) ) G ( t , ξ , ϕ 2 ( τ , ξ ) ) | d τ M d ρ ( ϕ 1 , ϕ 2 ) . Since M d < 1 , the operator A is a contraction mapping.
So we have a contraction mapping of a complete metric space to itself. Then by the contraction mapping theorem there exists a unique solution v C * to the equation v = A v . So, due to the arbitrarity of ξ [ a , max k j + a ] N , for all ξ [ a , max k j + a ] N there exists a unique solution v ( t , ξ ) for | t | d which is continuously differentiable in t and continuous in ξ .
Now we consider the following sequences of solutions to the problem (11): { v ( m ) ( t , ξ ( m ) ) } m = 0 , where ξ ( m ) = ξ ( m 1 ) + v ( m 1 ) ( d , ξ ( m 1 ) ) for m N + , ξ ( 0 ) = ξ [ a , max k j + a ] N . We note that ξ ( m ) = ξ + 0 i < m v ( i ) ( d , ξ ( i ) ) .
We define a mapping v ( t , ξ ) = ξ ( m ) ξ + v ( m ) ( t m d , ξ ( m ) ) for t [ m d , ( m + 1 ) d ) for some m. It is a continuous mapping in t by the definition of a sequence.
For t [ m 0 d , ( m 0 + 1 ) d ) for some m 0 we have
m N + : m m 0 ε m > 0 ε 0 > 0 : ξ : | | ξ ξ | | < ε 0 | | ξ ( m ) ξ ( m ) | | < ε m
by continuity of all mappings. Hence, v ( t , ξ ) is a continuous mapping in ξ .
v ( t , ξ ) is a unique solution to the problem (11) in ( m 0 d , ( m 0 + 1 ) d ) by the definition of a sequence. On the boundary we have:
v t ( m d , ξ ) = v ( m ) t ( 0 , ξ ( m ) ) = G ( 0 , ξ ( m ) , 0 ) = F ( ξ ( m ) ) = F ( ξ + ξ ( m ) ξ ) = F ( ξ + v ( m d , ξ ) ) = G ( m d , ξ , v ( m d , ξ ) ) .
Moreover, the derivative v t is continuous with respect to t on the boundary:
lim t m d 0 v t ( t , ξ ) = lim t m d 0 v ( m 1 ) t ( t ( m 1 ) d , ξ ( m 1 ) ) = lim t m d 0 F ( ξ ( m 1 ) + v ( m 1 ) ( t ( m 1 ) d , ξ ( m 1 ) ) ) = F ( ξ ( m ) ) .
 □
Remark 
(to the Cauchy problem (10)). Let the conditions of the previous corollary be true. Then u ( t 2 , u ( t 1 , u 0 ) ) = u ( t 2 + t 1 , u 0 ) for all t 1 , t 2 [ b 2 , ) ( b < 0 , see the previous corollary).
Proof. 
Let u ( 1 ) ( t ) = u ( t , u ( t 1 , u 0 ) ) , u ( 2 ) ( t ) = u ( t + t 1 , u 0 ) . Then u ( 1 ) ( 0 ) = u ( 0 , u ( t 1 , u 0 ) ) = u ( t 1 , u 0 ) and u ( 2 ) ( 0 ) = u ( t 1 , u 0 ) . But by the assumption the solution to the Cauchy problem (10) is unique, hence, u ( 1 ) ( t ) = u ( 2 ) ( t ) for all t [ b 2 , ) . □
Theorem 4.
There is b < 0 such that the solution u C ( ( b , ) ; [ a ; max k j + a ] N ) to the Cauchy problem (10) with an initial condition u ( 0 ) = u 0 [ a ; max k j + a ] N for some a 0 exists and is unique and analytic for all t ( b , ) (its Taylor series at every point of the interval ( b , ) converge uniformly to the mapping u in some neighborhood of that point; see [53], p. 219).
Proof. 
All the functions F i are analytic (their Taylor series converge because the functions F i are polynomials), hence, F is an analytic vector field. Then by the Cauchy-Kovalevskaya theorem [56] we have a solution for any initial condition v 0 [ a ; max k j + a ] N which is analytic on some open interval J ( v 0 ) , containing zero.
Let J ( u 0 ) be the maximal interval of convergence of the Taylor series of the solution u ( t , u 0 ) , and let us assume that S J = sup J ( u 0 ) < . From the previous remark we have that u ( t , u ( S J , u 0 ) ) = u ( t + S J , u 0 ) and from the prevoius part of this proof we have that the solution u ( t , u ( S J , u 0 ) ) is analytic on some open interval J ( u ( S J , u 0 ) ) , containing zero. But that means that d n u ( 0 , u ( S J , u 0 ) ) d t n = d n u ( S J , u 0 ) d t n and there is a neighborhood U J ( u ( S J , u 0 ) ) of zero such that for all t U
u ( t + S J , u 0 ) = n = 0 d n u ( S J , u 0 ) d t n n ! ( ( t + S J ) S J ) n = n = 0 d n u ( S J , u 0 ) d t n n ! t n .
—it is a contradiction. Hence, the solution is analytic for all t > 0 . In particular, the solution is smooth. □
Theorem 5.
If q i j = q for all i , j and q max i max u i ( β i ; k i ) f i ( u i ) u i 2 for quadratic coupling or q max i max u i ( β i ; k i ) f i ( u i ) u i for linear coupling, then there is a non-zero steady-state point.
Proof. 
The proof is the same as in the case of the two-patch system. □
Theorem 6.
The system with logistic growth always has a non-zero steady-state point.
To prove the theorem we have to prove a lemma about approximation of a steady-state point by periodic points.
Lemma 4.
For a dynamical system u ( t , ξ ) induced by the problem (10) let M be a compact set such that for all ξ M for all t 0 we have u ( t , ξ ) M , let { ξ n } n = 1 M be a sequence of periodic points where each point ξ n has a period T n > 0 and there are limits lim t ξ n = ξ 0 , lim t T n = 0 . Then the point ξ 0 is a steady-state (fixed) point of the dynamical system u ( t , ξ ) .
Proof. 
We prove the lemma by contradiction: we asume that the point ξ 0 is not a steady-state point, meaning that there is t 0 > 0 such that u ( t 0 , ξ 0 ) ξ 0 . Let γ = | | u ( t 0 , ξ 0 ) ξ 0 | | . Then the balls B ( ξ 0 , γ 4 ) and B ( u ( τ , ξ 0 ) , γ 4 ) do not intersect. Let us choose T such that 0 < T < t 0 and | | u ( t , ξ 0 ) ξ 0 | | < γ 8 for 0 t T . By continuity of u ( t , ξ ) there is δ > 0 such that choosing any ψ such that | | ψ ξ 0 | | < δ implies that | | u ( T , ψ ) u ( T , ξ 0 ) | | < γ 8 for 0 < t < T . In particular, we notice that if | | ψ ξ 0 | | < δ then | | u ( t , ψ ) ξ 0 | | = | | u ( t , ψ ) u ( t , ξ 0 ) + u ( t , ξ 0 ) ξ 0 | | | | u ( t , ψ ) u ( t , ξ 0 ) | | + | | u ( t , ξ 0 ) ξ 0 | | γ 8 + γ 8 = γ 4 for all t such that 0 t T .
There is N 0 N + such that for all n > N 0 we have T n < T and | | ξ n ξ 0 | | < δ . Hence, | | u ( t , ξ n ) ξ 0 | | < γ 4 for 0 t T n < T . And as the orbit O ( ξ n ) is periodic of period T n , we have | | u ( t , ξ n ) ξ 0 | | < γ 4 for all t R . But this contradicts with the fact that | | u ( t , ξ n ) u ( t , ξ 0 ) | | < γ 4 because the last two statements mean that u ( t , ξ n ) B ( ξ 0 , γ 4 ) and u ( t , ξ n ) B ( u ( τ , ξ 0 ) , γ 4 ) and from the assumption we know that B ( ξ 0 , γ 4 ) B ( u ( τ , ξ 0 ) , γ 4 ) = . □
Proof of Theorem 6.
Firstly we note that if for some t 0 we have 0 < u ¯ ( t 0 ) < min j k j N then d u ¯ d t ( t 0 ) > 0 because u i ( t 0 ) [ 0 ; k i ] , i 1 , N ¯ and at least one of the populations is greater than zero at the time t 0 . But that means that the metapopulation cannot extinct.
Let us consider a family of mappings Π t u 0 = u ( t , u 0 ) for any u 0 [ min k j 2 N , max k j ] N , where Π t : [ min k j 2 N , max k j ] N [ min k j 2 N , max k j ] N .
To apply the Brouwer fixed-point theorem [57,58,59] we need the set [ min k j 2 N , max k j ] N to be compact and convex, which is obviously true, and the mapping Π t : [ min k j 2 N , max k j ] N [ min k j 2 N , max k j ] N to be continious. The statement “all mappings Π t are continuous” means that
t > 0 v 0 [ min k j 2 N , max k j ] N ε > 0 δ > 0 : v | | v v 0 | | < δ | | u ( t , v ) u ( t , v 0 ) | | < ε
or equivalently that means the continuous dependence on initial conditions. But that is true due to the Picard-Lindelöf theorem, hence, all mappings Π t are continuous.
Let { T n } n = 1 R + be a monotone sequence such that there is a limit lim n T n = 0 . And by the Brower fixed-point theorem for every n N + there is a fixed point ξ n [ min k j 2 N , max k j ] N of the mapping Π T n . So we have Π T n ( ξ n ) = u ( T n , ξ n ) = ξ n . The sequence { ξ n } n = 1 [ min k j 2 N , max k j ] N is bounded, hence, there is a subsequence { ξ n m } m = 1 [ min k j 2 N , max k j ] N such that there is a limit lim m ξ n m = ξ 0 [ min k j 2 N , max k j ] N . Then by the Lemma 4 we conclude that the point ξ 0 is a steady-state point. □

4.2. Solutions as a Monotone Dynamical System

From the previous section we know that the dynamical system u ( t , u 0 ) , defined by the Cauchy problem (10), is bounded in R + N for u 0 [ a , max k j + a ] N for some a 0 in the sence that for all t 0 each component of a vector u ( t , u 0 ) is bounded by a and max k j + a in R + . The dynamical system u ( t , u 0 ) is continuous. It is analytical in the first variable t.
In this section we prove that the dynamical system u ( t , u 0 ) is strongly-monotone; moreover, we prove that it is asymptotically stable (as t ) for some initial conditions, that are important for us, for example, in computer simulations. Here the asymptotical stability means the convergence to some steady-state point.
On a topological vector space R N from the previous section we define non-strict partial orders ≤ and < and a strict partial order ≪ by the following rules:
x , y R N , x y iff for all i 1 , N ¯ x i y i ; x , y R N , x < y iff for all i 1 , N ¯ x i y i and x y ; x , y R N , x y iff for all i 1 , N ¯ x i < y i .
Remark. 
Let x , y R N . If x y then there are neighborhoods U and V of x and y respectively, such that for all u U , v V we have u v (We will denote it as U V ).
Proof. 
By definition, x y means for all i 1 , N ¯ we have x i < y i . Then for all i 1 , N ¯ for all u i ( x i y i x i 2 , x i + y i x i 2 ) and v i ( y i y i x i 2 , y i + y i x i 2 ) we have u i v i , hence, u = ( u 1 , , u N ) v = ( v 1 , , v N ) .
So we can choose U = ( x 1 y 1 x 1 2 , x 1 + y 1 x 1 2 ) × × ( x N y N x N 2 , x N + y N x N 2 ) , V = ( y 1 y 1 x 1 2 , y 1 + y 1 x 1 2 ) × × ( y N y N x N 2 , y N + y N x N 2 ) . □
Theorem 7.
Let a 0 . Let u ( m ) be a solution for an initial value problem u ( m ) ( 0 ) = u 0 ( m ) [ a ; max k j + a ] N , m = 1 , 2 . If we have u ( 1 ) ( 0 ) u ( 2 ) ( 0 ) then for all t 0 we have u ( 1 ) ( t ) u ( 2 ) ( t ) .
Proof. 
Due to continuity of the solutions the inequality u ( 1 ) ( t ) u ( 2 ) ( t ) is true for t in some neighborhood of 0. Let us prove the rest of the statement by contradiction: we suppose that there is t 0 > 0 and there are indexes i 1 , , i r 0 ( r 0 N + ) such that we have u i r ( 1 ) ( t 0 ) = u i r ( 2 ) ( t 0 ) for all r 1 , r 0 ¯ and t 0 is such that for all t < t 0 we have u ( 1 ) ( t ) u ( 2 ) ( t ) .
We fix i 0 { i j | j 1 , r 1 ¯ } . From the system (9) we have
d u i 0 ( m ) d t = f i 0 ( u i 0 ( m ) ) + j = 1 N q i 0 j d ( u j ( m ) , u i 0 ( m ) ) , m = 1 , 2 .
For the following Cauchy problems
d u i 0 ( m ) d t = f i 0 ( u i 0 ( m ) ) , u i 0 ( 1 ) ( 0 ) u i 0 ( 2 ) ( 0 ) , m = 1 , 2 ,
we would have u i 0 ( 1 ) ( t ) < u i 0 ( 2 ) ( t ) for all t due to uniquness of the solution, Theorem 4.
Then we note that
j = 1 N q i 0 j d ( u j ( 1 ) ( t 0 ) , u i 0 ( 1 ) ( t 0 ) ) = j = 1 N q i 0 j d ( u j ( 1 ) ( t 0 ) , u i 0 ( 2 ) ( t 0 ) ) < j = 1 N q i 0 j d ( u j ( 2 ) ( t 0 ) , u i 0 ( 2 ) ( t 0 ) ) if j = 1 , j i 0 N q i 0 j 2 0 .
So if j = 1 , j i 0 N q i 0 j 2 0 then for all t in some neighborhood of t 0 we have d u i 0 ( 1 ) d t ( t ) < d u i 0 ( 2 ) d t ( t ) , hence, d ( u i 0 ( 1 ) u i 0 ( 2 ) ) d t ( t ) < 0 and ( u i 0 ( 1 ) u i 0 ( 2 ) ) ( t ) < 0 , in particular, u i 0 ( 1 ) ( t 0 ) u i 0 ( 2 ) ( t 0 ) —it is a contradiction.
If j = 1 , j i 0 N q i 0 j 2 = 0 then the functions u i 0 ( 1 ) and u i 0 ( 2 ) are the solutions to the Cauchy problems (13), hence, we have u i 0 ( 1 ) ( t ) < u i 0 ( 2 ) ( t ) for all t—it is a contradiction. □
Corollary 1.
Let u ( m ) be a solution for an initial value problem u ( m ) ( 0 ) = u 0 ( m ) [ 0 ; max k j ] N , m = 1 , 2 . If we have u ( 1 ) ( 0 ) < u ( 2 ) ( 0 ) then for all t 0 we have u ( 1 ) ( t ) < u ( 2 ) ( t ) .
Proof. 
Let us choose neighborhoods U 1 and U 2 of u ( 1 ) ( 0 ) and u ( 2 ) ( 0 ) respectively which does not intersect. We can choose v ( 1 ) ( 0 ) U 1 and v ( 2 ) ( 0 ) U 2 in such a way that v ( 1 ) ( 0 ) v ( 2 ) ( 0 ) . Then for all t 0 we have v ( 1 ) ( t ) v ( 2 ) ( t ) , it means that there are some neighborhoods V 1 ( t ) of v ( 1 ) ( t ) and V 2 ( t ) of v ( 2 ) ( t ) such that V 1 ( t ) V 2 ( t ) for all t 0 .
We fix t 0 0 . The dynamical system u ( t , ξ ) is continious with respect to the second variable ξ , when ξ [ a , max k j + a ] , a > 0 . Hence, there is ε 0 > 0 such that for all ε ( 0 , ε 0 ] such that V 1 ( t 0 ) = { x R N | | | x v ( 1 ) ( t 0 ) | | < ε } and V 2 ( t 0 ) = { x R N | | | x v ( 1 ) ( t 0 ) | | < ε } there is δ > 0 such that for all ξ 1 U 1 = { x R N | | | x u ( 1 ) ( 0 ) | | < δ } and ξ 2 U 2 = { x R N | | | x u ( 2 ) ( 0 ) | | < δ } we have u ( t 0 , ξ 1 ) V 1 ( t 0 ) and u ( t 0 , ξ 2 ) V 2 ( t 0 ) , in particular, u ( 1 ) ( t 0 ) V 1 ( t 0 ) and u ( 2 ) ( t 0 ) V 2 ( t 0 ) , but V 1 ( t 0 ) V 2 ( t 0 ) , hence, u ( 1 ) ( t 0 ) u ( 2 ) ( t 0 ) . Due to the arbitrarity of t 0 0 we conclude that for all t 0 we have u ( 1 ) ( t ) u ( 2 ) ( t ) . □
Remark. 
Here we used the fact that for sufficiently small ε 0 > 0 the initial values lie in some open set containing [ 0 ; max k j ] N in which the solution exists and is unique.
Corollary 2.
Let u ( m ) be a solution for an initial value problem u ( m ) ( 0 ) = u 0 ( m ) [ 0 ; max k j ] N , m = 1 , 2 . If we have u ( 1 ) ( 0 ) u ( 2 ) ( 0 ) then for all t 0 we have u ( 1 ) ( t ) u ( 2 ) ( t ) .
Proof. 
If u ( 1 ) ( 0 ) = u ( 2 ) ( 0 ) then it is obviously true. The case u ( 1 ) ( 0 ) u ( 2 ) ( 0 ) follows from the previous corollary. □
Corollary 3.
Let U R N . We define a set u ( t , U ) = { v R N | there is u 0 U : v = u ( t , u 0 ) } . Then the dynamical system u ( t , ξ ) is strongly order-preserving, meaning that for u ( 1 ) ( 0 ) < u ( 2 ) ( 0 ) there are neighborhoods U 1 and U 2 respectively such that for all t 0 u ( t , U 1 ) u ( t , U 2 ) .
Proof. 
The proof is done in the proof of Corollary 1. □
Corollary 4.
If for two solutions u ( 1 ) ( t ) , u ( 2 ) ( t ) we have u i ( 1 ) ( t 0 ) R u i ( 2 ) ( t 0 ) for R { , < , } and some t 0 R then u i ( 1 ) ( t ) R u i ( 2 ) ( t ) for all t t 0 .
Proof. 
Let v ( m ) ( t ) = u ( m ) ( t + t 0 ) , m = 1 , 2 . Then d v ( m ) d t ( t ) = d u ( m ) d t ( t + t 0 ) = F ( u ( m ) ( t + t 0 ) ) = F ( v ( m ) ( t ) ) , v ( m ) ( 0 ) = u ( m ) ( t 0 ) , m = 1 , 2 . For all i we have v i ( 1 ) ( 0 ) = u i ( 1 ) ( t 0 ) R u i ( 2 ) ( t 0 ) = v i ( 2 ) ( 0 ) . □
Theorem 8.
Let the function of two variables u ( t , u 0 ) represent the solution of the Cauchy problem (10). Then setting for all i 1 , N ¯ u 0 i = max k j there is a limit lim t u ( t , u 0 ) = u ^ which is a steady-state of the system (9), lim t d u d t ( t , u 0 ) = 0 . Moreover, for all e E (the set of all equilibrium points) we have u ^ e .
Proof. 
u ( t , u 0 ) [ 0 , max k j ] N for all t 0 , hence, there is t 0 > 0 such that for all T ( 0 , t 0 ) we have u ( T , u 0 ) u 0 . Hence, there is a limit lim t u ( t , u 0 ) = u ^ ; see [60], p. 248, Theorem 1.4 (Convergence Criterion).
For all v 0 [ 0 , max k j ] N we have v 0 u 0 , hence, u ( t , v 0 ) u ( t , u 0 ) for all t 0 . For v 0 E we have v 0 u ( t , u 0 ) , and as t we have v 0 u ^ . □
Theorem 9.
If for the Cauchy problem (10) there is at least one point u 0 > 0 such that d u d t ( 0 ) 0 then there is a non-zero steady-state point u ^ such that lim t u ( t , u 0 ) = u ^ .
Proof. 
The function d u d t is continuous as a derivative of a solution to the problem (10), hence, there is T > 0 such that d u d t ( t ) 0 for all t [ 0 ; T ] , hence, u ( T , u 0 ) u 0 , in particular, u ( T , u 0 ) > u 0 . But by the corollary 3 the dynamical system u is strongly order-preserving, hence, there is a limit lim t u ( t , u 0 ) = u ^ > u 0 > 0 ([60], Theorem 1.4). □

5. Computer Simulations

Here we will consider a system of N equations representing a chain of populations:
d u 1 d t = f 1 ( u 1 ) + q d ( u 2 , u 1 ) , d u i d t = f i ( u i ) + q d ( u i 1 , u i ) + q d ( u i + 1 , u i ) , i 2 , N 1 ¯ , d u N d t = f N ( u N ) + q d ( u N 1 , u N ) ,
where f i ( u i ) = α i u i ( u i β i ) ( 1 u i k i ) and d ( y , x ) = y x or d ( y , x ) = y 2 x 2 .
In this section we focus on finding one global parameter p ( β , k ) which somewhat characterize the system for all q. Here we will let α i = 1 for all i. We consider { k i } to be uniformly distributed on interval [ k m i n , k m a x ] , { β i } to be uniformly distribited, where each β i is uniformly distributed on interval [ 0 ; k i ] , { k i } and { β i } are independent. So { k i } and { β i } can be defined by the following formulas:
k i = k m i n + ( k m a x k m i n ) ϕ , β i = k i ψ , i 1 , N ¯ ,
where ϕ , ψ are two independent random variables uniformly distributed on [ 0 , 1 ] .
Let p = k ¯ 2 β ¯ = 1 N ( ( k 1 + + k N ) 2 ( β 1 + + β N ) ) . By the weak law of large numbers [61] we have p E ( k ) 2 E ( β ) = k m a x + k m i n 2 2 ( k m i n E ( ψ ) + ( k m a x k m i n ) E ( ϕ ) E ( ψ ) ) = k m a x + k m i n 2 k m i n k m a x k m i n 2 = 0 . Here we will show that slightly changing p around 0 leads to bifurcation in most of the systems, in particular, there is a “small” constant p * > 0 such that if p > p * then we can guarantee the persistence. Analytically the constant is still unknown, but here we try to find it approximately using examples.
An optimal value for N is 100, for this N the parameter p is not too large, not too small. We simulate both types of coupling using the RK45 method, which is programmed in Python using scipy.integrate.solve_ivp. We let u i ( 0 ) = max k j and change q with a step size of 0.5 from 0.5 to 20. It was checked in simulations that t = 200 was sufficiently large to ensure the system’s convergence to its steady-state distribution, for linear case we had to set the value of related tolerance to an error r t o l = 10 6 instead of default r t o l = 10 3 to ensure the convergence for large q.
For the quadratic coupling we have 5 test trials then we generate 5 random values of k and β in a predetermined range of p. From the data we conclude that the constant p 2 0.52 and p 2 > 0.514 .
For linear coupling we run the simulation on the same data then add other trials in a predetermined range of p. For linear coupling we have p 1 0.0164 .
We focus on the asymptotical steady-state behaviour of the system and hence show only the final metapopulation distribution. Figure 2 shows the examples of persistence and extinction.
Below are Table 1 with cases which demonstrated persistence and Table 2 with extinct cases for q = 20 with their last q which gave the persistence, we also may show the distribution for a smaller parameter q. We note that for a better precision in a linear case we have to consider larger qs or more examples because in a quadratic model the absolute value of a coupling term grows faster. Here for the sake of uniformity we have chosen the second option. We begin both tables with the quadratic model as it is simpler in these ranges. We skip some of the examples.
Now we show Figure 3 corresponding to Table 1 and Figure 4 corresponding to Table 2.

6. Discussion and Concluding Remarks

Nature has many complex and fragmented environments and there are still many open theoretical problems [11,12,15,22,32,46,62]; conditions resulting in population collapse and species extinction in a fragmented habitat have long been a focus of the metapopulation theory. Previous research has identified specific factors, such as habitat geometry and demographic/environmental stochasticity, which can contribute to metapopulation collapse under certain conditions [31,32,33,34]. This study aims to contribute to this ongoing discourse by presenting another factor that could potentially result in metapopulation extinction. We investigate a system of arbitrary connected populations; we are primarily concerned with the conditions which correspond to persistaince and extinction.
We first considered a baseline two-patch metapopulation. We continued the research done in [50] giving more sufficient conditions which can be subdivided into a condition on a system type (systems without Allee effect), a condition on extrema of growth functions f i , conditions on q. Then we considered an arbitrary multi-patch system and showed that some of the conditions on q can be extended on the multi-patch system. We showed that the solution to the Cauchy problem exists and is unique, analytic and bounded. We showed that the model belongs to the class of so called monotone dynamical systems, which is very common in mathematical biology [60], and got some important corollaries from that, including another sufficient condition.
We then considered a 1D random metapopulation: a string of patches coupled by a short-distance dispersal (i.e., where each patch is coupled to its immediate neighbours) where the carrying capacity and the Allee threshold of the local population growth is a random function of space and stated a one-parameter sufficient condition. Computer simulations were supported by theoretical results. In particular, Theorem 8 basically tells us that we indeed converge to some steady-state point in Section 4. From the numerical results it can be seen that an increase in coupling may either lead to metapopulation collapse and global species extinction or to the formation of ‘persistence clusters’ (groups of patches where the subpopulations persist) separated by large stretches of empty space where the subpopulations go extinct. We emphasize that the persistence clusters are completely self- organized, as our model does not include any long-distance correlations. A slight change in the vector α causes a slight change in the boundary p * of the parameter p = k ¯ 2 β ¯ , so this sufficient coundition is also applicable to more general systems where α ( 1 , , 1 ) T .
Thus, the study of this conceptual model can be considered complete. This paper continues the study done in the paper [50] of the mechanism that may lead to, on one hand, metapopulation extinction or, on the other hand, pattern formation through creating persistence clusters. Although the model used in this paper is very simple, it may give a rise to some important ecological interpretations and stimulate further study. Real ecosystems are usually much more complex: there can be multiple mechanisms; moreover, they can turn on and off independently from each other under specific conditions. A single-species model is typically only applicable on certain timescales [63]. Therefore, it is worth considering more complex models to reveal whether there is similar mechanism as in this model. Despite useful insights from previous work [15,16,19], this issue remains controversial. For example adding other species with some interaction laws to the model may cause the appearence of periodic and chaotic solutions. Coupling different habitats may greatly change the dynamics leading to appearence of new mechanisms or to synchronization of mechanisms between the habitats. All these issues should be studied further in future research.

Author Contributions

S.P. created and introduced the methematical model, designed numerical methodology; A.K. designed analytical methodology, found appropriate literatire for analysis of the model by S.P., proved theorems, performed numerical simulations and visualization (as part of his Bachelor’s degree under the supervision of S.P.); A.K. and S.P. analysed the data; A.K. prepared the first draft of the manuscript; S.P. finalized the manuscript. All authors have read and agreed to the published version of the manuscript.

Funding

This research received no external funding.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

This paper does not use or generate any data.

Acknowledgments

S.P. was supported by the RUDN University Strategic Academic Leadership Program.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. The functions u 1 , u 2 are monotonically increasing, the function d u ¯ d t is monotonically decreasing and has a limit 0, that leads to an existence of a non-zero steady-state point. The first coordinate of the ends of the lines is the value of u 1 and u 2 at the particular time:time = const. The second coordinate of the centres of the lines is d u ¯ d t .
Figure 1. The functions u 1 , u 2 are monotonically increasing, the function d u ¯ d t is monotonically decreasing and has a limit 0, that leads to an existence of a non-zero steady-state point. The first coordinate of the ends of the lines is the value of u 1 and u 2 at the particular time:time = const. The second coordinate of the centres of the lines is d u ¯ d t .
Mathematics 11 04337 g001
Figure 2. On the graphs the black line represents the population on each site when t = 200 . The blue line is a carrying capacity of each site. The orange line is an Allee threshold of each site. The steady state is generally near the corresponding value of k for a small q, it can drop to 0 on a rare occasion. An increase in the coupling strength q eventually leads to the formation of clusters. The populations of the same cluster tend to align as q increases.
Figure 2. On the graphs the black line represents the population on each site when t = 200 . The blue line is a carrying capacity of each site. The orange line is an Allee threshold of each site. The steady state is generally near the corresponding value of k for a small q, it can drop to 0 on a rare occasion. An increase in the coupling strength q eventually leads to the formation of clusters. The populations of the same cluster tend to align as q increases.
Mathematics 11 04337 g002aMathematics 11 04337 g002b
Figure 3. Persistence cases. On the graphs the black line represents the population on each site when t = 200 . The blue line is a carrying capacity of each site. The orange line is an Allee threshold of each site.
Figure 3. Persistence cases. On the graphs the black line represents the population on each site when t = 200 . The blue line is a carrying capacity of each site. The orange line is an Allee threshold of each site.
Mathematics 11 04337 g003aMathematics 11 04337 g003b
Figure 4. Extinction cases. On the graphs the black line represents the population on each site when t = 200 . The blue line is a carrying capacity of each site. The orange line is an Allee threshold of each site.
Figure 4. Extinction cases. On the graphs the black line represents the population on each site when t = 200 . The blue line is a carrying capacity of each site. The orange line is an Allee threshold of each site.
Mathematics 11 04337 g004aMathematics 11 04337 g004b
Table 1. Persistence cases. The letter in the index in the column “Which k ( m ) , β ( m ) ” represents the dataset we use (L for linear, Q for quadratic), the number represents the iteration, the test dataset is marked by just a number.
Table 1. Persistence cases. The letter in the index in the column “Which k ( m ) , β ( m ) ” represents the dataset we use (L for linear, Q for quadratic), the number represents the iteration, the test dataset is marked by just a number.
Case No.ModelqWhich k ( m ) ,   β ( m ) k ¯ β ¯ p
1Quadratic207Q6.08292.78240.5180
2Quadratic208Q6.33362.90240.5287
3Quadratic209Q6.10392.79390.5161
4Linear515.99312.74750.4981
5Linear2015.99312.74750.4981
6Linear556.19513.2314−0.2678
7Linear2056.19513.2314−0.2678
8Linear56L5.85182.91760.0166
9Linear206L5.85182.91760.0166
10Linear59L5.95942.97150.0163
11Linear209L5.95942.97150.0163
12Linear2010L6.17073.07720.0162
13Linear2011L5.94652.96550.0155
14Linear513L5.96632.97500.0163
15Linear2013L5.96632.97500.0163
16Linear514L5.79672.89020.0164
17Linear2014L5.79672.89020.0164
18Linear2015L5.89422.93890.0165
19Linear517L6.10193.04280.0163
20Linear2017L6.10193.04280.0163
Table 2. Extinction cases. The letter in the index in the column “Which k ( m ) ,   β ( m ) ” represents the dataset we use (L for linear, Q for quadratic), the number represents the iteration, the test dataset is marked by just a number. NI marks trivial cases that are not interesting.
Table 2. Extinction cases. The letter in the index in the column “Which k ( m ) ,   β ( m ) ” represents the dataset we use (L for linear, Q for quadratic), the number represents the iteration, the test dataset is marked by just a number. NI marks trivial cases that are not interesting.
Case No.ModelqWhich k ( m ) , β ( m ) k ¯ β ¯ p
21Quadratic515.99312.74750.4981
22Quadratic11.515.99312.74750.4981
23 (NI)Quadratic1.525.83223.2905−0.7489
24 (NI)Quadratic0.535.98833.0180−0.0477
25 (NI)Quadratic135.98833.0180−0.0477
26 (NI)Quadratic3.546.47933.22300.0333
27Quadratic0.556.19513.2314−0.2678
28Quadratic4.556.19513.2314−0.2678
29Quadratic4.56Q6.02802.75740.5132
30Quadratic7.510Q6.06602.77560.5147
31Linear9.525.83223.2905−0.7489
32Linear535.98833.0180−0.0477
33Linear546.47923.22300.0333
34Linear1346.47923.22300.0333
35 (NI)Linear137L5.46772.72610.0156
36Linear108L5.91012.94690.0163
37Linear128L5.91012.94690.0163
38 (NI)Linear8.512L5.97832.98120.0159
39Linear516L5.66872.82610.0164
40Linear1116L5.66872.82610.0164
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Korotkov, A.; Petrovskii, S. Extinctions in a Metapopulation with Nonlinear Dispersal Coupling. Mathematics 2023, 11, 4337. https://doi.org/10.3390/math11204337

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Korotkov A, Petrovskii S. Extinctions in a Metapopulation with Nonlinear Dispersal Coupling. Mathematics. 2023; 11(20):4337. https://doi.org/10.3390/math11204337

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Korotkov, Alexander, and Sergei Petrovskii. 2023. "Extinctions in a Metapopulation with Nonlinear Dispersal Coupling" Mathematics 11, no. 20: 4337. https://doi.org/10.3390/math11204337

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Korotkov, A., & Petrovskii, S. (2023). Extinctions in a Metapopulation with Nonlinear Dispersal Coupling. Mathematics, 11(20), 4337. https://doi.org/10.3390/math11204337

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