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Article

Codimension-Two Bifurcations of a Simplified Discrete-Time SIR Model with Nonlinear Incidence and Recovery Rates

1
School of Mathematical Sciences, Qufu Normal University, Qufu 273165, China
2
Institute of Automation, Qufu Normal University, Qufu 273165, China
3
Shanghai Research Institute for Intelligent Autonomous Systems, Tongji University, Shanghai 201210, China
*
Author to whom correspondence should be addressed.
Mathematics 2023, 11(19), 4142; https://doi.org/10.3390/math11194142
Submission received: 17 August 2023 / Revised: 16 September 2023 / Accepted: 25 September 2023 / Published: 30 September 2023
(This article belongs to the Special Issue Advances in Differential Analysis and Functional Analysis)

Abstract

:
In this paper, a simplified discrete-time SIR model with nonlinear incidence and recovery rates is discussed. Here, using the integral step size and the intervention level as control parameters, we mainly discuss three types of codimension-two bifurcations (fold-flip bifurcation, 1:3 resonance, and 1:4 resonance) of the simplified discrete-time SIR model in detail by bifurcation theory and numerical continuation techniques. Parameter conditions for the occurrence of codimension-two bifurcations are obtained by constructing the corresponding approximate normal form with translation and transformation of several parameters and variables. To further confirm the accuracy of our theoretical analysis, numerical simulations such as phase portraits, bifurcation diagrams, and maximum Lyapunov exponents diagrams are provided. In particular, the coexistence of bistability states is observed by giving local attraction basins diagrams of different fixed points under different integral step sizes. It is possible to more clearly illustrate the model’s complex dynamic behavior by combining theoretical analysis and numerical simulation.

1. Introduction

Throughout time, human beings have been plagued by various epidemic diseases, such as plague [1], cholera [2], influenza [3], etc. In the process of human struggle against epidemic diseases, medical personnel have developed vaccines against various viruses and proposed many epidemic prevention measures. In addition, mathematicians have also made important contributions in curbing the spread of diseases. The time from the outbreak of the epidemic disease to its control, the number of people in contact with the disease who need to be quarantined, and the number of infected people at a certain time during the development of the epidemic disease can be more or less determined from the perspective of mathematical models. In 1927, Kermack and Mckendrick analyzed the number of patients with plague and the survival days of patients and finally put forward a landmark model in mathematical epidemiology: the SIR model [4]. Up to now, the vast majority of studies analyzing infectious diseases from a mathematical perspective have worked in the shadow of this model. In 2005, Zhang et al. proposed a compartmental model that modeled the SARS control strategies implemented by the Chinese government after the middle of April 2003 [5]. In 2011, Yang et al. used methods such as grey prediction and cellular automata to study the mathematical model of H1N1 influenza [6]. In the research and prediction of the COVID-19 epidemic, many scholars used the infectious disease dynamics model as a basic research tool and proposed various improvement methods to enrich the classical infectious disease dynamics model, enabling it to more objectively describe the actual situation of epidemic transmission and making more reasonable predictions about the development trend of the epidemic. Many effective suggestions have been provided for prevention, control, and governance [7,8,9].
In recent years, research on dynamical systems has undergone qualitative changes. Dynamical systems are an interdisciplinary field that can be applied not only to the study of epidemic diseases, but also to many other fields, such as predator–prey models [10] and tumor models [11]. For the research of epidemic diseases, we generally apply mathematical models to characterize their rich dynamic behavior [12]. Some mathematical models are designed to target specific diseases [13], but most are suitable for general studies of the laws of various epidemic diseases. Most models of epidemic disease are ordinary differential equations. However, compared to continuous models, discrete-time dynamic models are considerably more straightforward and computationally efficient. Most discrete-time epidemic models not only are simple analogies of continuous epidemic models, but also show complex dynamic behaviors that the corresponding continuous models cannot show. The discrete-time model is capable of producing extremely complicated dynamics, even in a one-dimensional instance [14]. Many interesting and important research works can be found in [15,16,17,18,19] and the references cited therein.
As we all know, bifurcation theory is a vital tool for understanding the behavioral characteristics of dynamic systems. In applied mathematics research, period-doubling bifurcation and Neimark–Sacker bifurcation are two important phenomena of the discrete-time dynamical model [19,20,21]. The period-doubling bifurcation process is a typical path to chaos, which can be considered as a way to enter chaos from the periodic window. Neimark–Sacker bifurcation is a classic tool for studying the generation and death of small-amplitude periodic solutions of discrete dynamic systems. Liu et al. discretized a discrete-time gene regulatory network system by using the forward Euler’s method. Theoretical analysis and numerical simulations illustrate some interesting dynamical behaviors such as period-doubling bifurcation, Neimark–Sacker bifurcation, and chaos [22]. Discrete-time dynamical models, however, frequently incorporate a large number of parameters, and the models are unavoidably affected by two or more parameters. Therefore, it is of more practical significance to study the complex behaviors of a nonlinear model on a two-dimensional parameter plane or even a higher-dimensional parameter space. Eskandari and Alidousti reported that an SIR model undergoes codimension-two bifurcations with 1:2 resonance, 1:3 resonance, and 1:4 resonance. The rich dynamics of the model on the two-parameter plane for the first iteration were discussed [23]. Li et al. studied multiple and generic bifurcations of a discrete Hindmarsh–Rose model. Different kinds of critical cases of codimension-one and -two bifurcations are computed by the inner product method. The richer and more complex behaviors under higher iterations and the bifurcation distributions of codimension-two bifurcation points are investigated [24]. In addition, various types of codimension-one and -two bifurcations have been investigated in [25,26,27,28,29,30,31,32,33] and the references cited therein.
For local bifurcations of nonhyperbolic fixed points, universal bifurcation diagrams are given by the topological normal form method. Bifurcation diagrams are not entirely chaotic, and different strata of bifurcation diagrams in generic systems interact by following specific rules. This makes the bifurcation diagrams of systems arising in many different applications look similar. To this end, a system should be transformed into its topological normal forms whose highest order is the second or third order by smooth reversible changes of the coordinate and the parameter. The topological equivalent systems that have qualitatively similar or equivalent bifurcation diagrams to the original system can be obtained after these transformations [34].
However, there are still many difficulties in studying codimension-two bifurcations due to the influence of higher-order nonlinear terms. The complex dynamics of even elementary dynamical systems cannot be clearly demonstrated by theoretical analysis. Some researchers have explored the use of computers to model the dynamics within the local parameter variation. Therefore, the numerical methods are helpful not only to validate our analytical results but also to better demonstrate and understand the dynamics of the model [14]. In this paper, we analyze a discrete-time model with the help of various numerical tools and techniques. For example, MatcontM is a bifurcation continuation package for discrete-time dynamical systems [35,36,37,38].
Alshmmari and Khan [39] proposed an SIR model with nonlinear incidence and nonlinear recovery rates consisting of three nonlinear differential equations as
d S d t = A β I S k + I μ S , d I d t = β I S k + I α 0 + α 1 α 0 b b + I I γ + μ I , d R d t = α 0 + ( α 1 α 0 ) b b + I I μ R ,
where S ( t ) , I ( t ) , and R ( t ) denote the numbers of susceptible, infected, and recovered individuals at time t, respectively. A , γ , and μ represent the birth rate, the death rate due to disease, and the natural death rate of each species, respectively. β I S k + I and α 0 + α 1 α 0 b b + I represent the nonlinear incidence rate and nonlinear recovery rate, respectively. α 1 and α 0 ( 0 < α 0 < α 1 ) denote the maximum and minimum per capita recovery rates, respectively. b indicates the impact of the number of hospital beds on the transmission of infectious diseases. k represents the intervention levels and determines the shape of the incidence rate.
Since R ( t ) does not appear in the first two equations of model (1), it is sufficient only to consider the following reduced model, which consists of the first two equations
d S d t = A β I S k + I μ S , d I d t = β I S k + I α 0 + α 1 α 0 b b + I I γ + μ I ,
where R ( t ) = N ( t ) S ( t ) I ( t ) , and N ( t ) is the total population.
Here, we discuss the complex dynamics of a discrete-time version SIR model, which is obtained from the simplified model (2) by adopting the forward Euler’s method and replacing S x and I y as follows:
x y N ( x , y , ϑ ) = x + h A β y x k + y μ x y + h β y x k + y α 0 + α 1 α 0 b b + y y γ + μ y ,
where A , β , α 0 , α 1 , μ , γ , b , and k are defined in model (1), h is the integral step size for discretization, and ϑ = ( h , A , β , α 0 , α 1 , μ , γ , b , k ) . In fact, we have discussed some dynamics of model (3) in [40], such as the stability of fixed points, some codimension-one bifurcations (transcritical, period-doubling, and Neimark–Sacker bifurcations) and a codimension-two bifurcation (1:2 resonance) of non-hyperbolic fixed points. In [40], through numerical continuation by using MatcontM, we found that besides the above bifurcations, the model also has other codimension-two bifurcation phenomena, such as fold-flip bifurcation, 1:3 resonance, and 1:4 resonance. However, there is no rigorous theoretical support for these codimension-two bifurcations but only numerical continuation results in our previous work. In this paper, we give a detailed theoretical analysis of these interesting codimension-two bifurcations of model (3) by constructing an approximate normal form when k and h are used as the bifurcation parameters. Some new numerical simulations of codimension-two bifurcations are also given to show that there are abundant and complex dynamical behaviors in model (3) with the change of parameters k and h by using Matlab and the standard numerical software package MatcontM (the version is Matcontm5p4). In particular, we observe the local dynamics, such as local attraction basins in the neighborhood of fixed points.
The outline of this paper is as follows. Firstly, the existence and stability of the fixed points of model (3) are given in Section 2. Secondly, theoretical analysis of the codimension-two bifurcations (fold-flip bifurcation, 1:3 resonance, and 1:4 resonance) of model (3) is discussed in Section 3. Some numerical continuation and numerical simulation results for illustrating the theoretical analysis are provided in Section 4. In particular, local attraction basin diagrams are given to demonstrate the rich dynamics in the neighborhood of the codimension-two bifurcation points. Finally, this paper ends with a brief conclusion in Section 5.

2. Existence and Stability of Fixed Points

In this section, the parameter conditions for the existence and stability of fixed points in the discrete-time model (3) are given. The detailed derivations are given in [40]. For convenience sake and quick reference, we summarize them as follows.

2.1. Existence of Fixed Points

The study of the bifurcation structures of a model usually starts from the analysis of fixed points. The fixed points of model (3) are positive solutions to
A β y x k + y μ x = 0 , β y x k + y α 0 + α 1 α 0 b b + y y γ + μ y = 0 .
There are at most two kinds of fixed points in model (3). One is the disease-free fixed point E 0 A μ , 0 , and the other is the endemic fixed points E i ( x i , y i ) ( i = 1 , 2 ) , if and only if y i ( i = 1 , 2 ) is a positive root of the following quadratic equation:
f ( y ) : = C 1 y 2 + C 2 y + C 3 ,
where
C 1 = ( β + μ ) ( α 0 + γ + μ ) , C 2 = k μ ( α 0 + γ + μ ) + b ( β + μ ) ( α 1 + γ + μ ) β A , C 3 = b k μ ( α 1 + γ + μ ) A β .
Furthermore,
x i = A ( k + y i ) ( β + μ ) y i + k μ ( i = 1 , 2 ) .
The solutions of Equation (5) are computed by
y i = C 2 ± Δ 2 C 1 ( i = 1 , 2 ) ,
where
Δ = C 2 2 4 C 1 C 3 = k μ ( α 0 + γ + μ ) + b ( β + μ ) ( α 1 + γ + μ ) β A 2 4 b ( β + μ ) ( α 0 + γ + μ ) k μ ( α 1 + γ + μ ) A β .
When Δ = 0 , the two fixed points E 1 and E 2 collide and merge into E ( x , y ) , where
x = A k ( 2 β + 3 μ ) + b ( β + μ ) ( α 1 + γ + μ ) A k ( 2 β + 3 μ ) ( α 1 α 0 ) A 2 β b ( β + μ ) + 3 k μ ( α 1 + γ + μ ) 3 k μ ( α 1 α 0 ) A β ( β + μ ) , y = β A k μ ( α 0 + γ + μ ) b ( β + μ ) ( α 1 + γ + μ ) 2 ( β + μ ) ( α 0 + γ + μ ) .
As we can see from (6), C 1 > 0 when the parameters are all positive, C 2 > 0 when b > A β k μ ( α 0 + γ + μ ) ( β + μ ) ( α 1 + μ + γ ) , and C 3 > 0 when k > β A μ ( α 1 + γ + μ ) . We obtain the following results.
Lemma 1.
The fixed points of model (3) are as follows: model (3) always has a disease-free fixed point E 0 A μ , 0 for all positive parameters. And for the endemic fixed point(s), we have:
(I) 
  C 1 > 0 and C 3 < 0 , model (3) has only one endemic fixed point E 2 .
(II) 
C 1 > 0 and C 3 = 0 ,
(i) 
When C 2 < 0 , model (3) has only one endemic fixed point E 2 .
(ii) 
When C 2 0 , model (3) has no endemic fixed points.
(III) 
C 1 > 0 and C 3 > 0 ,
(i) 
When C 2 < 0 , there are two endemic fixed points E 1 , E 2 if Δ > 0 , one endemic fixed point E if Δ = 0 , and no endemic fixed point if Δ < 0 .
(ii) 
When C 2 0 , model (3) has no endemic fixed points.
The parameter conditions for the existence of fixed points are summarized in Table 1.

2.2. Stability of Fixed Points

2.2.1. Stability of the Disease-Free Point E 0 A μ , 0

When all the parameters are positive, there is always the disease-free point E 0 A μ , 0 , whose properties are given in Table 2.

2.2.2. Stability of the Endemic Fixed Points E ( x , y )

The Jacobian matrix evaluated at E is given by
J E = 1 h β y k + y + μ β h k x ( k + y ) 2 β h y k + y 1 + h β k x ( k + y ) 2 ( α 1 α 0 ) b 2 ( b + y ) 2 α 0 γ μ .
The characteristic equation of J E is written as
F ( λ ) = λ 2 + M λ + N ,
where
M = tr ( J E ) = 2 + h β y k + y β k x ( k + y ) 2 + ( α 1 α 0 ) b 2 ( b + y ) 2 + α 0 + γ + 2 μ , N = det ( J E ) = 1 h β y k + y + μ 1 + h β k x ( k + y ) 2 ( α 1 α 0 ) b 2 ( b + y ) 2 α 0 γ μ + β 2 h 2 k x y ( k + y ) 3 = 1 + h β k x ( k + y ) 2 ( α 1 α 0 ) b 2 ( b + y ) 2 β y k + y α 0 γ 2 μ + h 2 ( α 1 α 0 ) b 2 β y ( b + y ) 2 ( k + y ) + β y k + y ( α 0 + γ + μ ) μ β k x ( k + y ) 2 + ( α 1 α 0 ) μ b 2 ( b + y ) 2 + μ ( α 0 + γ + μ ) .
Then, the stability of the positive fixed point E is concluded in Table 3.

3. Codimension-Two Bifurcation Analysis

In this section, the parameters A , β , α 0 , α 1 , μ , γ , and b are fixed and h , k are selected as the bifurcation parameters. In what follows, we analyze three cases of codimension-two bifurcations (fold-flip bifurcation, 1:3 resonance, and 1:4 resonance) at the endemic fixed point E ( x , y ) .

3.1. Fold-Flip Bifurcation

In this subsection, we will consider the fold-flip bifurcation in model (3). Model (3) has a pair of multiples, which are denoted by λ 1 = 1 and λ 2 = 1 , if
N ( x , y , ϑ ) ( x , y ) T = ( 0 , 0 ) T , det ( J ( x , y , ϑ ) ) + 1 = 0 , trace ( J ( x , y , ϑ ) ) = 0 .
The exact solution ( x , y , h , k ) of (11) is denoted by ( x , y , h f , k f ) . Therefore, model (3) may undergo a fold-flip bifurcation at E ( x , y ) when the bifurcation parameters h = h f and k = k f . Letting u ( n ) = x ( n ) x , v ( n ) = y ( n ) y , h f = h h f , k f = k k f , model (3) can be transformed into the following form with Taylor expansion at the origin ( 0 , 0 )
u n + 1 = ( h f + h f ) k f β x y ( k f + k f + y ) ( k f + y ) + 1 ( h f + h f ) A 11 u n ( h f + h f ) A 12 v n + F f ( u n , v n ) , v n + 1 = ( h f + h f ) k f β x y ( k f + k f + y ) ( k f + y ) + ( h f + h f ) A 21 u n + 1 + ( h f + h f ) A 22 v n + G f ( u n , v n ) ,
where
F f ( u n , v n ) = 2 i + j 3 a i j u n i v n j + O | u n , v n | 4 , G f ( u n , v n ) = 2 i + j 3 b i j u n i v n j + O | u n , v n | 4 ,
with A 11 , A 12 , A 21 , A 22 in (12), a i j and b i j in (13), as detailed in Appendix A.
For simplicity, let ϕ = ( h f , k f ) T . We construct a matrix T = A 12 h f A 12 A 11 2 + h f A 11 . Under the translation
u n v n = T u ˜ n v ˜ n ,
map (12) can be written as
u ˜ n + 1 v ˜ n + 1 = K 0 ( ϕ ) + K 1 ( ϕ ) u ˜ n v ˜ n + F ˜ f ( u ˜ n , v ˜ n ) G ˜ f ( u ˜ n , v ˜ n ) ,
where
K 0 ( ϕ ) = ( A 12 A 11 ) h f + 2 ( h f + h f ) k f β x y 2 A 12 ( k f + k f + y ) ( k f + y ) ( A 12 A 11 ) ( h f + h f ) k f β x y 2 A 12 ( k f + k f + y ) ( k f + y ) , K 1 ( ϕ ) = 1 h f 2 + h f ( A 22 A 11 ) 0 1 + h f ( A 22 A 11 ) , F ˜ f ( u ˜ n , v ˜ n ) = 2 i + j 3 a ˜ i j u ˜ n i v ˜ n j + O | u ˜ n , v ˜ n | 4 , G ˜ f ( u ˜ n , v ˜ n ) = 2 i + j 3 b ˜ i j u ˜ n i v ˜ n j + O | u ˜ n , v ˜ n | 4 ,
with a ˜ i j and b ˜ i j , as given in Appendix A.
The eigenvectors of K 1 ( ϕ ) corresponding to the eigenvalues λ 1 ( ϕ ) = 1 and λ 2 ( ϕ ) = 1 + h f ( A 22 A 11 ) are q f , 1 and q f , 2 , respectively, where λ 1 ( 0 ) = 1 and λ 2 ( 0 ) = 1 . In addition, the eigenvectors of K 1 ( ϕ ) T corresponding to the eigenvalues λ 1 ( ϕ ) and λ 2 ( ϕ ) are p f , 1 and p f , 2 , respectively. According to the bifurcation condition, these four vectors q f , 1 , q f , 2 , p f , 1 , p f , 2 satisfy the following equalities K 1 ( ϕ ) q f , 1 = q f , 1 , K 1 ( ϕ ) q f , 2 = q f , 2 , K 1 ( ϕ ) T p f , 1 = p f , 1 , K 1 ( ϕ ) T p f , 2 = p f , 2 , p f , 1 , q f , 1 = p f , 2 , q f , 2 = 1 , and p f , 1 , q f , 2 = p f , 2 , q f , 1 = 0 , where . , . stands for the standard scalar product in R 2 . For instance, we can select that
q f , 1 = 1 0 , q f , 2 = h f ( h f ( A 11 A 22 ) 2 ) h f ( A 11 A 22 ) + 2 , p f , 1 = 1 h f ( h f ( A 11 A 22 ) 2 ) h f ( A 11 A 22 ) + 2 , p f , 2 = 0 1 h f ( A 11 A 22 ) + 2 .
Then, any vector U ˜ n = ( u ˜ n , v ˜ n ) T R 2 can be uniquely represented as U ˜ n = x ˜ n q f , 1 + y ˜ n q f , 2 . We denote X ˜ n = ( x ˜ n , y ˜ n ) R 2 . The component of X ˜ n can be calculated explicitly as follows
x ˜ n = p f , 1 , U ˜ n , y ˜ n = p f , 2 , U ˜ n .
Under the coordinates X ˜ n , the form of map (14) can be written as
x ˜ n + 1 y ˜ n + 1 = Φ ( X ˜ n , ϕ ) = L ˜ 1 L ˜ 2 + 1 0 0 1 + h f ( A 22 A 11 ) x ˜ n y ˜ n + H ˜ f ( x ˜ n , y ˜ n ) W ˜ f ( x ˜ n , y ˜ n ) ,
where
L ˜ 1 = ( A 12 A 11 ) h f + h f h f ( A 12 A 22 ) 2 h f + 2 ( h f + h f ) k f β x y A 12 ( k f + k f + y ) ( k f + y ) , L ˜ 2 = ( A 12 A 11 ) h f ( A 11 A 22 ) + 2 ( h f + h f ) k f β x y 2 A 12 ( k f + k f + y ) ( k f + y ) , H ˜ f ( x ˜ n , y ˜ n ) = 2 i + j 3 a ˘ i j x ˜ n i y ˜ n j + O | x ˜ n , y ˜ n | 4 , W ˜ f ( x ˜ n , y ˜ n ) = 2 i + j 3 b ˘ i j x ˜ n i y ˜ n j + O | x ˜ n , y ˜ n | 4 ,
with a ˘ i j and b ˘ i j , as given in Appendix A.
When ϕ = 0 = ( 0 , 0 ) T , map (16) can be written as
x ˜ n + 1 y ˜ n + 1 = 1 0 0 1 x ˜ n y ˜ n + H ¯ f ( x ˜ n , y ˜ n ) W ¯ f ( x ˜ n , y ˜ n ) ,
where
H ¯ f ( x ˜ n , y ˜ n ) = 2 i + j 3 a ¯ i j x ˜ n i y ˜ n j + O | x ˜ n , y ˜ n | 4 , W ¯ f ( x ˜ n , y ˜ n ) = 2 i + j 3 b ¯ i j x ˜ n i y ˜ n j + O | x ˜ n , y ˜ n | 4 , a ¯ i j = a ˜ i j | ϕ = 0 , b ¯ i j = b ˜ i j | ϕ = 0 .
If
a ¯ 11 0 ,
according to Proposition 2.2.1 of [41], map (18) is smoothly equivalent to the following map near the origin
ξ 1 , n + 1 ξ 2 , n + 1 = ξ 1 , n + 1 2 σ 1 ( 0 ) ξ 1 , n 2 + 1 2 σ 2 ( 0 ) ξ 2 , n 2 + 1 6 σ 3 ( 0 ) ξ 1 , n 3 + 1 2 σ 4 ( 0 ) ξ 1 , n ξ 2 , n 2 ξ 2 , n + ξ 1 , n ξ 2 , n + O | ξ 1 , n , ξ 2 , n | 4 ,
where
σ 1 ( 0 ) = 2 a ¯ 20 b ¯ 11 , σ 2 ( 0 ) = 2 a ¯ 02 b ¯ 11 , σ 3 ( 0 ) = 6 a ¯ 30 + 3 a ¯ 11 b ¯ 20 b ¯ 11 2 , σ 4 ( 0 ) = a ¯ 02 ( 4 b ¯ 02 b ¯ 20 + 4 b ¯ 21 4 a ¯ 11 g ¯ 20 ) 4 a ¯ 20 ( b ¯ 02 2 + b ¯ 03 ) b ¯ 11 a ¯ 11 2 + 2 a ¯ 12 + a ¯ 11 b ¯ 02 4 b ¯ 02 2 4 b ¯ 03 .
We define X ˜ ϕ Γ ( X ˜ , ϕ ) = Φ ( X ˜ , ϕ ) X ˜ det Φ X ˜ ( X ˜ , ϕ ) + 1 trace Φ X ˜ ( X ˜ , ϕ ) , and X ˜ = x ˜ y ˜ . Then, from map (16), we have
Γ ( X ˜ , ϕ ) | ( X ˜ n = ϕ = 0 ) = 0 0 B 11 B 12 0 2 B 21 B 22 W 1 R 1 C 0 W 2 R 2 C 0 ,
where B 11 , B 12 , B 21 , B 22 , W 1 , R 1 , W 2 , R 2 , and C are given in Appendix A.
If
det Γ ( X ˜ , ϕ ) | ( X ˜ = ϕ = 0 ) 0 ,
then map (16) is smoothly equivalent to a fold-flip bifurcation standard form near the origin
ξ 1 , n + 1 ξ 2 , n + 1 = μ 1 + ( 1 + μ 2 ) ξ 1 , n + 1 2 σ 1 ( ϕ ) ξ 1 , n 2 + 1 2 σ 2 ( ϕ ) ξ 2 , n 2 + 1 6 σ 3 ( ϕ ) ξ 1 , n 3 + 1 2 σ 4 ( ϕ ) ξ 1 , n ξ 2 , n 2 ξ 2 , n + ξ 1 , n ξ 2 , n + O | ξ 1 , n , ξ 2 , n | 4 .
We can obtain
μ 1 = ( β x + μ ) k f h f + ( μ 1 ) y h f + 2 ( k f + y ) ( k f + y ) 2 h f + β ( y h f ) 2 k f ( x + 1 ) ( β x + μ ) k f h f + ( μ β ) y h f + 2 h f y ( k f + y ) 2 k f ( k f + y ) 2 k f + O | ϕ | 2 , μ 2 = 1 b ˘ 11 ( 0 ) ( a ˘ 11 ( 0 ) b ˘ 11 ( 0 ) 4 a ˘ 20 ( 0 ) b ˘ 02 ( 0 ) ) B 21 4 a ˘ 20 ( 0 ) B 3 h f + ( a ˘ 11 ( 0 ) b ˘ 11 ( 0 ) 4 a ˘ 20 ( 0 ) b ˘ 02 ( 0 ) ) B 22 k f μ 2 = + O | ϕ | 2 .
From Proposition 3.1.1 in [41], we can obtain the following result.
Theorem 1.
If h and k are chosen as two bifurcation parameters, then model (3) undergoes a fold-flip bifurcation at E when the parameters h , k vary in a sufficiently small neighborhood of ( h f , k f ) near the E with (19) and (22) hold. Moreover, the model (3) has the following local codimension-one bifurcation behaviors:
(I) 
There is a non-degenerate fold bifurcation curve, fold: ( ξ 1 , ξ 2 , μ 1 ) = ( μ 2 σ 1 ( 0 ) + O μ 2 2 , 0 , μ 2 2 2 σ 1 ( 0 ) + O μ 2 3 ) , if σ 1 ( 0 ) 0 ;
(II) 
There is a non-degenerate flip bifurcation curve, flip: ( ξ 1 , ξ 2 , μ 1 ) = ( 0 , 0 , 0 ) , if σ 2 ( 0 ) 0 ;
(III) 
There is a non-degenerate Neimark–Sacker bifurcation curve, NS: ( ξ 1 , ξ 2 , μ 2 ) = 0 , 2 μ 1 σ 2 ( 0 ) + O μ 1 2 3 , O μ 1 2 3 ( σ 4 ( 0 ) + 2 σ 2 ( 0 ) ) μ 1 σ 2 ( 0 ) + O μ 1 2 , if σ 2 ( 0 ) > 0 and μ 1 < 0 .

3.2. 1:3 Resonance

In this subsection, we will consider codimension-two bifurcation with 1:3 resonance in model (3). Model (3) has a pair of complex conjugate multiples, which are denoted by λ R 3 = 1 2 + 3 i 2 and λ ¯ R 3 = 1 2 3 i 2 , if
N ( x , y , ϑ ) ( x , y ) T = ( 0 , 0 ) T , det ( J ( x , y , ϑ ) ) 1 = 0 , trace ( J ( x , y , ϑ ) ) 1 = 0 .
The exact solution ( x , y , h , k ) of (25) is denoted by ( x , y , h R 3 , k R 3 ) . Therefore, model (3) may undergo a codimension-two bifurcation with 1:3 resonance at E when the bifurcation parameters h = h R 3 and k = k R 3 . Letting u ( n ) = x ( n ) x and v ( n ) = y ( n ) y , model (3) can be transformed into the following form with Taylor expansion at the origin ( 0 , 0 )
u n + 1 = 1 m ( h , k ) u n p ( h , k ) v n + F R 3 ( u n , v n ) + O | u n , v n | 4 , v n + 1 = q ( h , k ) u n + 1 + n ( h , k ) v n + G R 3 ( u n , v n ) + O | u n , v n | 4 ,
where
F R 3 ( u n , v n ) = 2 i + j 3 c i j u n i v n j , G R 3 ( u n , v n ) = 2 i + j 3 d i j u n i v n j ,
with
m ( h , k ) = h β y k + y + μ , n ( h , k ) = h β k x ( k + y ) 2 ( α 1 α 0 ) b 2 ( b + y ) 2 α 0 γ μ , p ( h , k ) = β h k x ( k + y ) 2 , q ( h , k ) = β h y k + y , c 11 = h β k ( k + y ) 2 , c 02 = h β k x ( k + y ) 3 , c 12 = h β k ( k + y ) 3 , c 03 = h β k x ( k + y ) 4 , d 11 = h β k ( k + y ) 2 , d 02 = h ( α 1 α 0 ) b 2 ( b + y ) 3 β k x ( k + y ) 3 , d 12 = h β k ( k + y ) 3 , d 03 = h β k x ( k + y ) 4 ( α 1 α 0 ) b 2 ( b + y ) 4 , c 30 = c 21 = c 20 = 0 , d 30 = d 21 = d 20 = 0 .
By (26), the Jacobian matrix of E is obtained by
J E ( h , k ) = 1 m ( h , k ) p ( h , k ) q ( h , k ) 1 + n ( h , k ) .
We denote J = J E ( h R 3 , k R 3 ) . There are eigenvector q R 3 and adjoint eigenvector p R 3 C 2 , satisfying J q R 3 = λ R 3 q R 3   J T p R 3 = λ ¯ R 3 p R 3 , p R 3 , q R 3 = 1 , where λ R 3 = 1 2 + 3 i 2 , q R 3 = ( q R 3 , 1 q R 3 , 2 ) T = p ( h R 3 , k R 3 ) 3 2 + 3 i 2 + m ( h R 3 , k R 3 ) T , and p R 3 = ( p R 3 , 1 , p R 3 , 2 ) T = q ( h R 3 , k R 3 ) , 3 2 + 3 i 2 + m ( h R 3 , k R 3 ) T .
Now, any vector U = ( u , v ) T R 2 can be represented in the form U = z q R 3 + z ¯ q ¯ R 3 , where p ¯ R 3 = ( p ¯ R 3 , 1 , p ¯ R 3 , 2 ) , and q ¯ R 3 = ( q ¯ R 3 , 1 , q ¯ R 3 , 2 ) are the conjugates of p R 3 and q R 3 , respectively. Hence, model (26) can be written in the complex form
z n + 1 z ¯ n + 1 = λ R 3 0 0 λ ¯ R 3 z n z ¯ n + 2 i + j 3 g i j z n i z ¯ n j + O | z n , z ¯ n | 4 2 i + j 3 g ¯ i j z n i z ¯ n j + O | z n , z ¯ n | 4 ,
where g i j is given in Appendix B, and g ¯ i j is the complex conjugate of g i j . Now, what we need to study is
z n + 1 = λ R 3 z n + 2 i + j 3 g i j z n i z ¯ n j + O | z n , z ¯ n | 4 ,
since the second component of (27) is simply the complex conjugate of the first component.
Some quadratic terms can be eliminated by the following transformation
z n = w n + l 20 2 w n 2 + l 11 w n w ¯ n + l 02 2 w ¯ n 2 ,
where l 20 , l 11 , and l 02 are certain unknown functions. Using (29) and its inverse transformation, model (28) can be rewritten in the following form
w n + 1 = λ R 3 w n + 2 i + j 3 s i j w n i w ¯ n j + O | w n , w ¯ n | 4 ,
where s i j is given in Appendix B.
The coefficients in front of the w 2 _ and w w ¯ _ terms are eliminated by setting
l 20 = 2 g 20 3 i , l 11 = 2 g 11 3 3 i , l 02 = 0 .
Hence, (30) becomes
w n + 1 = λ R 3 w n + g 20 w ¯ n 2 + i + j = 3 s i j w n i w ¯ n j + O | w n , w ¯ n | 4 .
The next step is to annihilate cubic terms by applying an invertible smooth transformation
w n = ϕ n + l 30 6 ϕ n 3 + l 12 2 ϕ n ϕ ¯ n 2 + l 03 6 ϕ ¯ n 3 .
Using (32) and its inverse transformation, model (31) can be rewritten in the following form
ϕ n + 1 = λ R 3 ϕ n + g 20 ϕ ¯ n 2 + i + j = 3 t i j ϕ n i ϕ ¯ n j + O | ϕ n , ϕ ¯ n | 4 ,
where
t 30 = s 30 3 3 i 12 l 30 , t 21 = s 21 , t 12 = s 12 + 3 i 2 l 12 , t 03 = s 03 3 3 i 12 l 03 .
Hence, the coefficients in front of the w 3 _ , w w ¯ 2 _ , and w ¯ 3 _ terms are eliminated by setting
l 30 = 12 s 30 3 3 i , l 21 = 0 , l 12 = 2 s 12 3 i , l 03 = 12 s 03 3 3 i .
Finally, an approximating equation of (33) should have the following form
ϕ n + 1 = λ R 3 ϕ n + g 02 ϕ ¯ n 2 + t 21 ϕ n 2 ϕ ¯ n + O | ϕ n , ϕ ¯ n | 4 .
According to Lemma 9.12 in [34], defining
B 1 = 3 ( 1 + 3 i ) 2 g 02 , C 1 = 3 | g 02 | 2 3 ( 1 + 3 i ) 2 t 21 ,
we can obtain the following theorem.
Theorem 2.
If h and k are chosen as two bifurcation parameters, then model (3) undergoes a codimension-two bifurcation with 1:3 resonance at E when the conditions (25) and B 1 0 , Re ( C 1 ) 0 hold. Re ( C 1 ) 0 determines the stability of the bifurcation invariant closed curve. Moreover, model (3) recognizes a few of the following complex codimension-one bifurcation curves:
(I) 
There is a non-degenerate Neimark–Sacker bifurcation at the trivial fixed point E of (35);
(II) 
There is a saddle cycle of periodic three corresponding to the saddle fixed points E of (35);
(III) 
There is a homoclinic structure formed by the stable and unstable invariant manifolds of the period three cycle intersecting transversally in an exponentially narrow parameter region.

3.3. 1:4 Resonance

In this subsection, we consider codimension-two bifurcation with 1:4 resonance in model (3). Model (3) has a pair of complex conjugate multiples, which are denoted by λ R 4 = i and λ ¯ R 4 = i if
N ( x , y , ϑ ) ( x , y ) T = ( 0 , 0 ) T , det ( J ( x , y , ϑ ) ) 1 = 0 , trace ( J ( x , y , ϑ ) ) = 0 .
The exact solution ( x , y , h , k ) of model (36) is denoted by ( x , y , h R 4 , k R 4 ) . Therefore, model (3) may undergo a codimension-two bifurcation with 1:4 resonance at E when the bifurcation parameters h = h R 4 and k = k R 4 . Similar to the previous subsection, the Jacobian matrix of E is given by J E ( h , k ) = 1 m ( h , k ) p ( h , k ) q ( h , k ) 1 + n ( h , k ) . We denote J = J E ( h R 4 , k R 4 ) . There are eigenvector q R 4 and adjoint eigenvector p R 4 C 2 , satisfying J q R 4 = λ R 4 q R 4 , J T p R 4 = λ ¯ R 4 p R 4 , p R 4 , q R 4 = 1 , where λ R 4 = i , q R 4 = ( q R 4 , 1 , q R 4 , 2 ) T = ( p ( k R 4 , h R 4 ) , m ( h R 4 , k R 4 ) 1 + i ) T , p R 4 = ( p R 4 , 1 , p R 4 , 2 ) T = q ( h R 4 , k R 4 ) 2 , m ( h R 4 , k R 4 ) 1 i 2 T . Now, any vector U = ( u , v ) T R 2 can be represented in the form U = z q R 4 + z ¯ q ¯ R 4 , where q ¯ R 4 is the conjugate of q R 4 . Hence, model (26) can be written in the complex form
z n + 1 = λ R 4 z n + 2 i + j 3 g i j z n i z ¯ n j + O | z n , z ¯ n | 4 ,
where λ R 4 = i and g i j ( 2 i + j 3 ) are defined as in Appendix B with q R 3 , 1 , q R 3 , 2 , p R 3 , 1 , and p R 3 , 2 replaced by q R 4 , 1 , q R 4 , 2 , p R 4 , 1 , and p R 4 , 2 , respectively. Using (29) and its inverse transformation, model (37) can be rewritten in the following form
w n + 1 = λ R 4 w n + 2 i + j 3 s ˜ i j w n i w ¯ n j + O | w n , w ¯ n | 4 ,
where s ˜ i j are given in Appendix C.
All the quadratic terms are eliminated by setting
l 20 = 2 g 20 1 + i , l 11 = g 11 1 i , l 02 = 2 g 02 1 + i .
Hence, (38) becomes
w n + 1 = λ R 4 w n + i + j = 3 s ˜ i j w n i w ¯ n j + O | w n , w ¯ n | 4 .
Using (32) and its inverse transformation, model (39) can be rewritten in the following form
ϕ n + 1 = λ R 4 ϕ n + i + j = 3 t ˜ i j ϕ n i ϕ ¯ n j + O | ϕ n , ϕ ¯ n | 4 ,
in which
t ˜ 30 = s ˜ 30 + i 3 l 30 , t ˜ 21 = s ˜ 21 , t ˜ 12 = s ˜ 12 + i l 12 , t ˜ 03 = s ˜ 03 .
Hence, the coefficients in front of the w 3 _ and w w ¯ 2 _ terms are eliminated by setting
l 30 = 12 s ˜ 30 3 3 i , l 21 = 0 , l 12 = 2 s ˜ 12 3 i , l 03 = 0 .
Finally, an approximating equation of (40) should have the following form
ϕ n + 1 = λ R 4 ϕ n + t ˜ 21 ϕ n 2 ϕ ¯ n + t ˜ 03 ϕ ¯ n 3 + O | ϕ n , ϕ ¯ n | 4 .
According to Lemma 9.14 in [34], defining
B 2 = 2 i t ˜ 21 , C 2 = 2 i 3 t ˜ 03 ,
if C 2 0 , letting
D = B 2 | C 2 | ,
we can obtain the following theorem.
Theorem 3.
If h and k are chosen as two bifurcation parameters, then model (3) undergoes a codimension-two bifurcation with 1:4 resonance at E when the conditions (36) and C 2 0 , Re ( D ) 0 , and Im ( D ) 0 hold.

4. Numerical Bifurcation Analysis

In this section, the phase portraits, bifurcation diagrams, maximum Lyapunov exponents diagrams, and the diagrams of local attraction basins in the neighborhood of fixed points for model (3) are presented to verify the correctness of the analytical results established in Theorems 1–3 by using the MATLAB and the MATLAB package MatcontM [35,36,37,38]. Let A = 2.25 , β = 0.1 , α 1 = 0.5 , α 0 = 0.2 , γ = 0.2 , b = 0.6 , and μ = 0.05 for model (3) in the following Section 4.1, Section 4.2 and Section 4.3.

4.1. Fold-Flip Bifurcation

For Equation (11), we obtain one of its exact solutions ( x , y , h f , k f ) = ( 43.664637 , 0.908638 ,   8.388521 ,   9.58437 ) . Therefore, model (3) may undergo a fold-flip bifurcation at the fixed point E ( x , y ) = ( 43.664637 , 0.908638 ) when the critical parameter values h f = 8.388521 ,   k f = 9.58437 . The eigenvalues are λ 1 , 2 = ± 1 and a ¯ 11 = 0.259668 0 , det Γ ( X ˜ , ϕ ) | ( X ˜ = ϕ = 0 ) = 0.0224769 0 . According to Theorem 1, it means that model (3) undergoes a fold-flip bifurcation at E ( 43.664637 , 0.908638 ) .
The continuation of the fold bifurcation curve for two control parameters k and h is drawn in Figure 1a. Two fold-flip (LPPD) bifurcation points are detected. Meanwhile, a cusp (CP) and 1:1 resonance (R1) bifurcation points also are detected. Figure 1b presents a three-dimensional bifurcation diagram in ( k , h , x ) space near E ( 43.664637 , 0.908638 ) when k and h vary in the neighborhood of ( h f , k f ) = ( 8.388521 , 9.58437 ) , which is the left LPPD point in Figure 1a. Figure 1c depicts a two-dimensional bifurcation diagram in ( h , x ) plane for h [ 7 , 8.5 ] when k = k f = 9.58437 . The maximum Lyapunov exponents diagram corresponding to Figure 1c is drawn in Figure 1d.

4.2. 1:3 Resonance

For Equation (25), we obtain one of its exact solutions ( x , y , h R 3 , k R 3 ) = ( 21.70367 , 2.272045 , 9.112002 , 1.961387 ) . Therefore, model (3) may undergo a 1:3 resonance at the fixed point E ( x , y ) = ( 21.70367 , 2.272045 ) when the critical parameter values h R 3 = 9.112002 , and k R 3 = 1.961387 . The eigenvalues are λ 1 , 2 = 0.5 ± 0.8660254 i and B 1 = 0.556655 0.2653575 i 0 , C 1 = 275.6926179 1616.468972 i , and Re ( C 1 ) = 275.6926179 0 . According to Theorem 2, it means that model (3) undergoes a codimension-two bifurcation with 1:3 resonance at E ( 21.70367 , 2.272045 ) .
The 1:3 resonance bifurcation point is detected in the continuation of the Neimark–Sacker curve, which is drawn in Figure 2a. Figure 2b presents a three-dimensional bifurcation diagram in ( k , h , x ) space near E ( 21.70367 , 2.272045 ) when k and h vary in a neighborhood of ( h R 3 , k R 3 ) = ( 9.112002 , 1.961387 ) . Figure 2c depicts a 2-dimensional bifurcation diagram in ( h , x ) plane when k = k R 3 = 1.961387 . The local amplification of Figure 2c for h [ 9.11 , 9.1145 ] is obtained in Figure 2d. The maximum Lyapunov exponents diagram, which corresponds to Figure 2c is drawn in Figure 2e. The maximum Lyapunov exponents are negative when h < h R 3 = 9.112002 . There is a stable fixed point for each h. However, the maximum Lyapunov exponents are positive when h > h R 3 = 9.112002 , which means model (3) has chaotic behavior near the 1:3 resonance point E ( 21.70367 , 2.272045 ) . The phase portraits for different values of h corresponding Figure 2c are drawn in Figure 3.

4.3. 1:4 Resonance

For Equation (36), we obtain one of its exact solutions ( x , y , h R 4 , k R 4 ) = ( 26.348645 , 1.773490 , 9.309313 , 3.237305 ) . Therefore, model (3) may undergo a 1:4 resonance at the fixed point E ( x , y ) = ( 26.348645 , 1.773490 ) when the critical parameter values h R 4 = 9.309313 , and k R 4 = 3.237305 . The eigenvalues are λ 1 , 2 = ± i and B 2 = 0.5463087328 0.7196720302 i , C 2 = 0.3523986225 0.2941681928 i 0 , D = 1.190105762 1.56776888 i , Re ( D ) = 1.190105762 0 , and Im ( D ) = 1.567768880 0 . According to Theorem 3, it means that model (3) undergoes a codimension-two bifurcation with 1:4 resonance at E ( 26.348645 , 1.773490 ) .
The 1:4 resonance bifurcation point has been detected in the continuation of the Neimark–Sacker curve, which is drawn in Figure 2a. Figure 4a presents a three-dimensional bifurcation diagram in ( k , h , x ) space near E ( 26.348645 , 1.773490 ) when k and h vary in the neighborhood of h R 4 = 9.309313 , and k R 4 = 3.237305 , which is the R4 point in Figure 2a. Figure 4b depicts a two-dimensional bifurcation diagram in ( h , x ) plane for h [ 9.308 , 9.316 ] when k = k R 4 = 3.237305 . The maximum Lyapunov exponents diagram corresponding to Figure 4b is drawn in Figure 4c. The maximum Lyapunov exponents are negative when h < h R 4 = 9.309313 . There is(are) stable fixed point(s) for each h. However, some maximum Lyapunov exponents are positive when h > h R 4 = 9.309313 , which means model (3) has chaotic behavior near the resonance 1:4 point E ( 26.348645 , 1.773490 ) . Phase portraits for different values of h corresponding to Figure 4b are drawn in Figure 5.

4.4. Local Attraction Basins Diagrams

To better demonstrate the dynamic behavior of the system from a more classical perspective, the problem of the attraction basins of fixed points is discussed. The attraction basin of an attractor is the set containing initial points, i.e., the trajectories from the start of this set all converge toward the attractor when t [42]. Generally, the attraction basin of an attractor is not a regular shape but is very complex. There are boundaries between the attraction basins of different attractors. Near the border, a slight change in the initial conditions will lead to entirely different results.
According to Lemma 1, we know that C 1 > 0 , C 2 < 0 , C 3 > 0 , and Δ > 0 for k = 8 , b = 0.06 , and other parameters fixed as A = 2.25 , β = 0.1 , α 1 = 0.5 , α 0 = 0.2 , γ = 0.2 , μ = 0.05 , and h = 6 ; that is, model (3) has three fixed points, two of them are positive nontrivial fixed points, a spiral sink point E 1 ( 41.087 , 0.4 ) and a saddle point E 2 ( 43.2353 , 0.16667 ) ; the other is a stable node E 0 ( 45 , 0 ) . When the value of h is increased or decreased, the number of fixed points of model (3) and the shape of the attraction basins of different fixed points will change greatly. To study the effect of the integral step size h on the discrete-time model, the local attraction basins of the corresponding continuous system (2) are exhibited in Figure 6. The local attraction basins in the x ( 0 ) y ( 0 ) plane are shown in Figure 7 for nine values of h in model (3).
With the variation in the parameters, it is obvious that a Neimark–Sacker bifurcation may occur around E 1 when h = 27.003451 and the coefficient of the normal form is 0.1615609 . Figure 7 shows the evolution of the local attraction basin of each fixed point with the change in the parameter h. Figure 7 shows some cases of the coexistence of the bistability states of model (3), such as the coexistence of two stable fixed points or the coexistence of a stable fixed point and an attracting invariant cycle. When h > 27.003451 , an attracting invariant cycle appears. The attraction basin of the fixed point E 0 becomes smaller and smaller throughout the whole evolution process. Comparing Figure 6 and Figure 7, we know that the dynamic behavior of model (3) is consistent with that of model (2) when the value of the integral step size h of model (3) is very small. However, the dynamic behaviors of model (2) and model (3) are very different as h becomes larger.

5. Conclusions

In this paper, we discussed codimension-two bifurcations of a simplified discrete-time SIR model with nonlinear incidence and recovery rates. From the perspective of infectious disease, the incidence and recovery rates are two important measurement indicators to detect the pathogenesis of infectious diseases and to prevent and control the speed of the spread of diseases. They are also important indicators reflecting the progress of national medical science and technology. We simplified system (1) to explore the impact of the intervention levels k and integral step size h on the dynamic behavior of the number of susceptible and infected individuals in the simplified discrete-time SIR model with nonlinear incidence and recovery rates. The results indicate that the codimension-two bifurcations of the discrete-time model can generate interesting and complex dynamic behaviors, such as chaos, which means that seemingly random irregular movements can occur in deterministic systems. However, in continuous systems, at least third-order differential equation systems can exhibit chaotic phenomena, such as the Lorentz system, whereas chaos can be demonstrated in low-order discrete-time systems. Hence, studying discrete-time systems can help us better explore some complex dynamics hidden in the continuous system.
Two approaches are used to localize the codimension-two bifurcation points. One is to calculate the parameter conditions for the existence of bifurcation with theoretical analysis, and the other is to draw the position of these points directly by numerical continuation. Fold-flip bifurcation and 1:3 and 1:4 resonances are analyzed theoretically in detail. A large number of numerical simulations have been used to test the correctness of the theoretical results and to demonstrate the rich dynamic behaviors in model (3). By contrasting the local attraction basins diagram at different integral step sizes of discrete-time model (3) with that of the corresponding continuous system, we can find that the dynamic behaviors of the discrete-time model and the corresponding continuous system are consistent when the integral step size is small. However, the discrete-time model can exhibit more complex dynamic behaviors, which have not been observed in the original continuous model for larger integral step sizes. That is to say, a discrete-time model can capture hidden dynamics that are not exhibited by the corresponding continuous model.
In this paper, we only conducted some basic research on the dynamic behavior of the simplified discrete-time SIR model. However, the model with higher dimensions may show higher codimension bifurcations. In addition, many influencing factors are time-varying, and the error between the study of non-autonomous systems and the actual situation may be smaller. It is very challenging to study these bifurcations and their practical applications. We leave these cases for future consideration.

Author Contributions

Conceptualization, methodology, formal analysis, writing, D.H., X.L. and X.Y.; investigation, interpretation, visualization, X.L., K.L. and M.L.; supervision, X.Y.; software, M.L.; funding acquisition, D.H., K.L. and M.L. All authors have read and agreed to the published version of the manuscript.

Funding

This work was supported by the NSF of Shandong Province (ZR2023QA003, ZR2021MA016, ZR2020QA009), the China Postdoctoral Science Foundation (2019M652349), and the Youth Creative Team Sci-Tech Program of Shandong Universities (2019KJI007).

Data Availability Statement

The codes that supports the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

The authors are grateful to the anonymous reviewers for their valuable comments and suggestions.

Conflicts of Interest

The authors declare that there are no conflict of interest regarding the publication of this manuscript.

Appendix A. A11, A12, A21, A22 in (12), aij and bij in (13), a ˜ ij and b ˜ ij in (15), a ˘ ij and b ˘ ij in (17), and B11, B12, B21, B22, W1, R1, W2, R2, C in (21)

A 11 = β y k f + k f + y μ , A 12 = β x ( k f + k f ) k f + k f + y , A 21 = β x k f + k f + y , A 22 = β x ( k f + k f ) ( k f + k f + y ) 2 ( α 1 α 0 ) b 2 ( b + y ) 2 ( α 0 + γ + μ ) , a 11 = β ( h f + h f ) ( k f + k f ) ( k f + k f + y ) 2 , a 02 = β x ( k f + k f ) ( h f + h f ) ( k f + k f + y ) 3 , a 12 = β ( h f + h f ) ( k f + k f ) ( k f + k f + y ) 3 , a 03 = β x ( k f + k f ) ( h f + h f ) ( k f + k f + y ) 4 , b 11 = β ( h f + h f ) ( k f + k f ) ( k f + k f + y ) 2 , b 02 = ( h f + h f ) ( α 1 α 0 ) b 2 ( b + y ) 3 β x ( k f + k f ) ( k f + k f + y ) 3 , b 12 = β ( h f + h f ) ( k f + k f ) ( k f + k f + y ) 3 , b 03 = ( h f + h f ) β x ( k f + k f ) ( k f + k f + y ) 4 ( α 1 α 0 ) b 2 ( b + y ) 4 , a 30 = a 21 = a 20 = 0 , b 30 = b 21 = b 20 = 0 , a ˜ 20 = A 11 2 A 12 ( A 12 a 11 A 11 a 02 ) + 1 2 A 11 h f ( A 12 b 11 A 11 b 02 ) , a ˜ 11 = A 11 h f 2 A 12 A 11 ( A 11 h f 2 ) a 02 A 12 ( A 11 h f 1 ) a 11 + h f ( A 11 h f 2 ) A 11 b 02 ( A 11 h f 1 ) A 12 b 11 , a ˜ 02 = A 11 h f 2 2 A 12 A 12 h f a 11 ( A 11 h f 2 ) a 02 + 1 2 h f ( A 11 h f 2 ) A 12 h f b 11 ( A 11 h f 2 ) b 02 , a ˜ 30 = A 11 2 ( A 11 h f 2 ) 2 A 12 A 11 a 03 A 12 a 12 + 1 2 A 11 2 h f A 11 b 03 A 12 b 12 , a ˜ 12 = 3 ( A 11 h f 2 ) 2 2 A 12 ( A 11 h f 2 ) A 11 a 03 ( A 11 h f 1 ) A 12 a 12
a ˜ 12 = + 1 2 h f ( A 11 h f 2 ) 3 ( A 11 h f 2 ) A 11 b 03 ( 3 A 11 h f 2 ) A 12 b 12 , a ˜ 21 = ( A 11 h f 2 ) A 11 2 A 12 ( 3 A 11 h f 4 ) A 12 a 12 3 ( A 11 h f 2 ) A 11 a 03 a ˜ 12 = + 1 2 h f A 11 ( 3 A 11 h f 4 ) A 12 b 12 3 ( A 11 h f 2 ) A 11 b 03 , a ˜ 03 = ( A 11 h f 2 ) 3 2 A 12 h f A 12 a 12 ( A 11 h f 2 ) a 03 + 1 2 h f ( A 12 h f 2 ) 2 A 12 h f b 12 ( A 11 h f 2 ) b 03 , b ˜ 20 = A 11 2 2 A 12 ( A 12 a 11 A 11 a 02 ) + 1 2 A 11 ( A 12 b 11 A 11 b 02 ) , b ˜ 11 = ( A 11 h f 2 ) A 11 A 11 A 12 a 02 + b 02 A 12 ( A 11 h f 1 ) A 11 A 12 a 11 + b 11 , b ˜ 02 = ( A 11 h f 2 ) 2 2 A 11 A 12 a 02 + b 02 + ( A 11 h f 2 ) h f 2 A 11 a 11 + A 12 b 11 , b ˜ 30 = A 11 3 2 ( A 11 A 12 a 03 a 12 + b 03 ) 1 2 A 11 2 A 12 b 12 , b ˜ 12 = ( A 11 h f 2 ) 2 2 3 A 11 2 a 03 A 11 ( a 12 + 3 b 03 ) A 12 b 12 + A 11 A 12 h f ( A 11 h f 2 ) ( 2 a 12 b 12 ) , b ˜ 21 = A 11 ( A 11 h f 2 ) 2 3 A 11 2 A 12 a 03 + A 11 ( 2 a 12 3 b 03 ) + A 12 b 12 + 1 2 A 11 2 h f ( A 11 a 12 + A 12 b 12 ) , b ˜ 03 = ( A 11 h f 2 ) 3 2 ( A 11 A 12 a 03 + b 03 ) + 1 2 A 12 h f ( A 11 h f 2 ) 2 A 11 A 12 a 12 + b 12 , a ˘ 20 = a ˜ 20 , a ˘ 11 = h f ( A 11 A 22 ) + 2 a ˜ 11 + 2 h f ( h f ( A 11 A 22 ) 2 ) a ˜ 20 , a ˘ 02 = h f ( A 11 A 22 ) + 2 2 a ˜ 02 + h f ( h f ( A 11 A 22 ) 2 ) h f ( A 11 A 22 ) + 2 a ˜ 11 + h f ( h f ( A 11 A 22 ) 2 ) 2 a ˜ 20 , a ˘ 30 = a ˜ 30 , a ˘ 21 = h f ( A 11 A 22 ) + 2 a ˜ 12 + 3 h f ( h f ( A 11 A 22 ) 2 ) a ˜ 30 , a ˘ 12 = h f ( A 11 A 22 ) + 2 2 a ˜ 21 + 2 h f ( h f ( A 11 A 22 ) 2 ) h f ( A 11 A 22 ) + 2 a ˜ 12 + 3 h f ( h f ( A 11 A 22 ) 2 ) 2 a ˜ 30 , a ˘ 30 = h f ( A 11 A 22 ) + 2 3 a ˜ 03 + h f ( A 11 A 22 ) + 2 2 h f ( h f ( A 11 A 22 ) 2 ) a ˜ 21 a ˘ 30 = + h f ( A 11 A 22 ) + 2 h f 2 ( h f ( A 11 A 22 ) 2 ) 2 a ˜ 12 + h f ( h f ( A 11 A 22 ) 2 ) 3 a ˜ 30 , b ˘ 20 = b ˜ 20 , b ˘ 11 = h f ( A 11 A 22 ) + 2 b ˜ 11 + 2 h f ( h f ( A 11 A 22 ) 2 ) b ˜ 20 , b ˘ 02 = h f ( A 11 A 22 ) + 2 2 b ˜ 02 + h f ( h f ( A 11 A 22 ) 2 ) h f ( A 11 A 22 ) + 2 b ˜ 11 + h f ( h f ( A 11 A 22 ) 2 ) 2 b ˜ 20 , b ˘ 30 = b ˜ 30 , b ˘ 21 = h f ( A 11 A 22 ) + 2 a ˜ 12 + 3 h f ( h f ( A 11 A 22 ) 2 ) b ˜ 30 , b ˘ 12 = h f ( A 11 A 22 ) + 2 2 b ˜ 21 + 2 h f ( h f ( A 11 A 22 ) 2 ) h f ( A 11 A 22 ) + 2 b ˜ 12 + 3 h f ( h f ( A 11 A 22 ) 2 ) 2 b ˜ 30 , b ˘ 30 = h f ( A 11 A 22 ) + 2 3 b ˜ 03 + h f ( A 11 A 22 ) + 2 2 h f ( h f ( A 11 A 22 ) 2 ) b ˜ 21 a ˘ 30 = + h f ( A 11 A 22 ) + 2 h f 2 ( h f ( A 11 A 22 ) 2 ) 2 b ˜ 12 + h f ( h f ( A 11 A 22 ) 2 ) 3 b ˜ 30 , B 11 = ( β x + μ ) k f h f + ( μ 1 ) y h f + 2 ( k f + y ) ( k f + y ) 2 , B 12 = β ( y h f ) 2 k f ( x + 1 ) ( β x + μ ) k f h f + ( μ β ) y h f + 2 h f y ( k f + y ) 2 k f ( k f + y ) 2 , B 21 = ( β x + μ ) k f y + ( μ β ) y 2 2 ( k f + y ) 2 , B 22 = ( β x + μ ) k f 2 + ( μ β ) ( 2 k f + y ) y 2 k f ( k f + y ) 3 ,
W 1 = Υ h f ( Υ + β k f ) ( k f + y ) 2 + ( Υ h f 2 ) Υ h f Υ ( k f + y ) β x k f Υ h f 2 β k f x ( Υ + β k f ) β k f h f ( Υ h f 1 ) Υ ( k f + y ) + β k f x ( k f + y ) 3 W 1 = + 2 Υ h f ( Υ h f 1 ) ( α 1 α 0 ) b 2 ( b + y ) 3 , W 2 = Υ h f ( Υ + β k f ) ( k f + y ) 2 + ( Υ h f 2 ) Υ h f Υ ( k f + y ) β x k f + Υ h f 2 β k f x ( Υ + β k f ) β k f h f ( Υ h f 1 ) Υ ( k f + y ) + β k f x ( k f + y ) 3 W 1 = 2 Υ h f ( α 1 α 0 ) b 2 ( b + y ) 3 , R 1 = β h f k f x ( Υ h f 2 ) ( β h f k f Υ h f + 2 ) + h f β k f h f x ( Υ h f 2 ) ( k f + y ) β k f ( Υ h f 1 ) + Υ h f 2 ( k f + y ) 3 W 1 = + Υ h f ( Υ h f 2 ) 2 β h f k f Υ h f ( Υ h f 2 ) ( k f + y ) 2 2 h f ( Υ h f 2 ) ( α 1 α 0 ) b 2 ( b + y ) 3 , R 2 = β h f k f x ( Υ h f 2 ) ( β h f k f Υ h f + 2 ) h f β k f h f x ( Υ h f 2 ) ( k f + y ) β k f ( Υ h f 1 ) + Υ h f 2 ( k f + y ) 3 W 1 = + Υ h f ( Υ h f 2 ) 2 β h f k f Υ h f ( Υ h f 2 ) ( k f + y ) 2 2 h f ( Υ h f 2 ) ( Υ h f 1 ) ( α 1 α 0 ) b 2 ( b + y ) 3 , C = β x k f + ( k f + y ) y ( k f + y ) 2 ( α 1 α 0 ) b 2 ( b + y ) 2 ( α 0 + γ + μ ) , Υ = β y k f + y μ .

Appendix B. gij in (27) and sij in (30)

g 20 = ( p ¯ R 3 , 1 c 02 + p ¯ R 3 , 2 d 02 ) q R 3 , 2 2 + ( p ¯ R 3 , 1 c 11 + p ¯ R 3 , 2 d 11 ) q R 3 , 1 q R 3 , 2 , g 11 = ( p ¯ R 3 , 1 c 11 + p ¯ R 3 , 2 d 11 ) ( q R 3 , 1 q ¯ R 3 , 2 + q ¯ R 3 , 1 q R 3 , 2 ) + 2 ( p ¯ R 3 , 1 c 02 + p ¯ R 3 , 2 d 02 ) q R 3 , 2 q ¯ R 3 , 2 , g 02 = ( p ¯ R 3 , 1 c 11 + p ¯ R 3 , 2 d 11 ) q ¯ R 3 , 1 q ¯ R 3 , 2 + ( p ¯ R 3 , 1 c 02 + p ¯ R 3 , 2 d 02 ) q ¯ R 3 , 2 2 , g 30 = ( p ¯ R 3 , 1 c 12 + p ¯ R 3 , 2 d 12 ) q R 3 , 1 q R 3 , 2 2 + ( p ¯ R 3 , 1 c 03 + p ¯ R 3 , 2 d 03 ) q R 3 , 2 3 , g 21 = ( p ¯ R 3 , 1 c 12 + p ¯ R 3 , 2 d 12 ) ( 2 q R 3 , 1 q R 3 , 2 q ¯ R 3 , 2 + q ¯ R 3 , 1 q R 3 , 2 2 ) + 3 ( p ¯ R 3 , 1 c 03 + p ¯ R 3 , 2 d 03 ) q R 3 , 2 2 q ¯ R 3 , 2 , g 12 = 2 ( p ¯ R 3 , 1 c 12 + p ¯ R 3 , 2 d 12 ) ( q R 3 , 1 q ¯ R 3 , 2 2 + q ¯ R 3 , 1 q R 3 , 2 2 q ¯ R 3 , 2 ) + 3 ( p ¯ R 3 , 1 c 03 + p ¯ R 3 , 2 d 03 ) q R 3 , 2 q ¯ R 3 , 2 2 , g 03 = ( p ¯ R 3 , 1 c 12 + p ¯ R 3 , 2 d 12 ) q ¯ R 3 , 1 q ¯ R 3 , 2 2 + ( p ¯ R 3 , 1 c 03 + p ¯ R 3 , 2 d 03 ) q ¯ R 3 , 2 3 , s 20 = 3 i 2 l 20 + g 20 , s 11 = 3 + 3 i 2 l 11 + g 11 , s 02 = g 02 , s 30 = 3 3 i 2 l 20 g 20 + 1 2 l ¯ 02 g 11 + g 30 + 1 3 i 2 l 11 g ¯ 02 + 3 + 3 i 4 l 20 2 , s 21 = l ¯ 02 g 02 + 5 + 3 i 2 l 11 g 20 + l ¯ 11 g 11 + 2 3 i 2 l 20 g 11 + g 21 + 3 i 2 l 11 l 20 + 1 3 i 2 l 11 g ¯ 11 + 1 + 3 i 2 l 02 g ¯ 02 s 21 = + 3 + 3 3 i 4 l 11 l 20 + 3 + 3 i 2 | l 11 | 2 , s 12 = l 02 g 02 + 3 + 3 i 2 l 11 g 11 + 2 l ¯ 11 g 02 + 1 2 l ¯ 20 g 11 + g 12 3 + 3 i 2 l 11 2 3 3 i 4 l 11 l ¯ 20 + 1 3 i 2 l 11 g ¯ 20 s 21 = + 3 i l 02 l ¯ 11 + 1 + 3 i 2 l 20 g ¯ 11 + 1 3 i 2 l 20 g 02 , s 30 = 1 2 l 02 g 11 + l ¯ 20 g 02 + g 03 + 1 + 3 i 2 l 11 g 02 + 3 3 i 4 l 20 l ¯ 20 + 1 + 3 i 2 l 02 g ¯ 20 ,
where l ¯ 20 , l ¯ 11 , l ¯ 02 are the conjugates of l 20 , l 11 , l 02 .

Appendix C. s ˜ ij in (38)

s ˜ 20 = 1 + i 2 l 20 + g 20 , s ˜ 11 = ( 1 + i ) l 11 + g 11 , s ˜ 02 = 1 + i 2 l 02 + g 02 , s ˜ 30 = 1 i 2 l 20 2 + ( 1 i ) l 20 g 20 1 + i 2 l 11 l ¯ 02 + 1 2 l ¯ 02 g 11 + i l 11 g ¯ 02 + g 30 , s ˜ 21 = 1 + 3 i 2 l 20 l 11 + ( 2 + i ) l 11 g 20 i l 11 g ¯ 11 + 1 2 i 2 l 20 g 11 + l ¯ 11 g 11 + 1 2 l ¯ 02 l 02 + i l 02 g ¯ 02 + 1 + i 2 | l 11 | 2 + g 21 , s ˜ 12 = ( 1 i ) l 11 2 + 1 + i 2 l ¯ 20 l 11 + ( 1 + i ) l 11 g 11 i g ¯ 20 l 11 + ( 1 i ) g ¯ 11 l 02 + i l 02 g ¯ 11 + 2 l 02 g 20 + 1 i 2 l 20 l 02 s 12 = i l 20 g 02 + 2 l ¯ 11 g 02 + 1 2 l ¯ 20 g 11 + g 12 , s ˜ 03 = 1 + i 2 l ¯ 20 l 02 + 1 + i 2 l 11 l 02 + i l 02 g ¯ 20 + 1 2 l 02 g 11 + i l 11 g 02 + l ¯ 20 g 02 + g 03 .

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Figure 1. (a) The continuation curve of the LP point consists of fold-flip (LPPD), cusp (CP), and resonance 1:1 (R1) bifurcation points in ( k , h ) plane. (b) Bifurcation diagram in three-dimensional ( k , h , x ) space with the change of k and h. From left to right, the values of parameter k are 9.58337 , 9.58370 , 9.58404 , and 9.58437 , respectively. (c) Fold-flip bifurcation diagram in ( h , x ) plane with k = 9.58437 and h [ 7 , 8.5 ] . (d) The maximum Lyapunov exponents diagram corresponding to (c).
Figure 1. (a) The continuation curve of the LP point consists of fold-flip (LPPD), cusp (CP), and resonance 1:1 (R1) bifurcation points in ( k , h ) plane. (b) Bifurcation diagram in three-dimensional ( k , h , x ) space with the change of k and h. From left to right, the values of parameter k are 9.58337 , 9.58370 , 9.58404 , and 9.58437 , respectively. (c) Fold-flip bifurcation diagram in ( h , x ) plane with k = 9.58437 and h [ 7 , 8.5 ] . (d) The maximum Lyapunov exponents diagram corresponding to (c).
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Figure 2. (a) The continuation curve of the Neimark–Sacker point contains Chenciner (CH) bifurcation, resonance 1:2 (R2), resonance 1:3 (R3), and resonance 1:4 (R4) points in ( h , k ) plane. (b) Bifurcation diagram in three-dimensional ( k , h , x ) space with the change of k and h. The values of parameter k are 1.960387 , 1.960720 , 1.960985 , and 1.961387 from left to right. (c) 1:3 resonance bifurcation diagram in ( h , x ) plane when k = 1.961387 and h [ 9.106 , 9.1145 ] . (d) Local amplification corresponding to (c) for h [ 9.11 , 9.1145 ] . (e) The maximum Lyapunov exponents diagram corresponding to (c).
Figure 2. (a) The continuation curve of the Neimark–Sacker point contains Chenciner (CH) bifurcation, resonance 1:2 (R2), resonance 1:3 (R3), and resonance 1:4 (R4) points in ( h , k ) plane. (b) Bifurcation diagram in three-dimensional ( k , h , x ) space with the change of k and h. The values of parameter k are 1.960387 , 1.960720 , 1.960985 , and 1.961387 from left to right. (c) 1:3 resonance bifurcation diagram in ( h , x ) plane when k = 1.961387 and h [ 9.106 , 9.1145 ] . (d) Local amplification corresponding to (c) for h [ 9.11 , 9.1145 ] . (e) The maximum Lyapunov exponents diagram corresponding to (c).
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Figure 3. Phase portraits for different values of h corresponding to Figure 3c. (a) A stable fixed point for h = 9.106 . (b) Phase portrait of period-3 for h = 9.112 . (c) Phase portrait of 1:3 resonance for h = 9.113 .
Figure 3. Phase portraits for different values of h corresponding to Figure 3c. (a) A stable fixed point for h = 9.106 . (b) Phase portrait of period-3 for h = 9.112 . (c) Phase portrait of 1:3 resonance for h = 9.113 .
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Figure 4. (a) Bifurcation diagram in three-dimensional ( k , h , x ) space with the change of k and h. The values of parameter k are 3.237305 , 3.237338 , 3.237371 , and 3.237405 from left to right. (b) 1:4 resonance bifurcation diagram in ( h , x ) plane with k = 3.237305 and h [ 9.308 , 9.316 ] . (c) The maximum Lyapunov exponents diagram corresponding to (b).
Figure 4. (a) Bifurcation diagram in three-dimensional ( k , h , x ) space with the change of k and h. The values of parameter k are 3.237305 , 3.237338 , 3.237371 , and 3.237405 from left to right. (b) 1:4 resonance bifurcation diagram in ( h , x ) plane with k = 3.237305 and h [ 9.308 , 9.316 ] . (c) The maximum Lyapunov exponents diagram corresponding to (b).
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Figure 5. Phase portraits for different values of h corresponding to Figure 4b. (a) A stable fixed point for h = 9.308 . (b) Phase portrait of period-4 for h = 9.3095 . (c) Phase portrait of 1:4 resonance for h = 9.312 . (d) Phase portrait of 1:4 resonance for h = 9.314 . (e) Chaotic attractor for h = 9.316 .
Figure 5. Phase portraits for different values of h corresponding to Figure 4b. (a) A stable fixed point for h = 9.308 . (b) Phase portrait of period-4 for h = 9.3095 . (c) Phase portrait of 1:4 resonance for h = 9.312 . (d) Phase portrait of 1:4 resonance for h = 9.314 . (e) Chaotic attractor for h = 9.316 .
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Figure 6. The local attraction basin of system (2) in the S ( 0 ) I ( 0 ) initial plane. The blue region is the attraction basins of the equilibrium E 1 , and the yellow region is for E 0 , where E 2 is a saddle point.
Figure 6. The local attraction basin of system (2) in the S ( 0 ) I ( 0 ) initial plane. The blue region is the attraction basins of the equilibrium E 1 , and the yellow region is for E 0 , where E 2 is a saddle point.
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Figure 7. For different values of the integral step size h, the local attraction basins in the x ( 0 ) y ( 0 ) initial plane are presented. (a) h = 0.01 . (b) h = 8 . (c) h = 10 . (d) h = 16 . (e) h = 17 . (f) h = 26 . (g) h = 27.4 . (h) h = 33 . (i) h = 36.3 . The blue regions are the attraction basins of the equilibrium E 1 , and the yellow regions are for E 0 , where E 2 is a saddle point. The cyanine regions are the attraction basins of the attracting invariant cycle, and the red regions are for the divergence.
Figure 7. For different values of the integral step size h, the local attraction basins in the x ( 0 ) y ( 0 ) initial plane are presented. (a) h = 0.01 . (b) h = 8 . (c) h = 10 . (d) h = 16 . (e) h = 17 . (f) h = 26 . (g) h = 27.4 . (h) h = 33 . (i) h = 36.3 . The blue regions are the attraction basins of the equilibrium E 1 , and the yellow regions are for E 0 , where E 2 is a saddle point. The cyanine regions are the attraction basins of the attracting invariant cycle, and the red regions are for the divergence.
Mathematics 11 04142 g007aMathematics 11 04142 g007b
Table 1. Existence of fixed points.
Table 1. Existence of fixed points.
ConditionsFixed Points
All the parameters are positive E 0
k < β A μ ( α 1 + γ + μ ) b > 0 E 0 , E 2
k = β A μ ( α 1 + γ + μ ) 0 < b < A β k μ ( α 0 + γ + μ ) ( β + μ ) ( α 1 + μ + γ ) E 0 , E 2
b A β k μ ( α 0 + γ + μ ) ( β + μ ) ( α 1 + μ + γ ) E 0
k > β A μ ( α 1 + γ + μ ) 0 < b < A β k μ ( α 0 + γ + μ ) ( β + μ ) ( α 1 + μ + γ ) Δ < 0 E 0
Δ = 0 E 0 , E
Δ > 0 E 0 , E 1 , E 2
b A β k μ ( α 0 + γ + μ ) ( β + μ ) ( α 1 + μ + γ ) E 0
Table 2. Stability of the disease-free fixed point E 0 .
Table 2. Stability of the disease-free fixed point E 0 .
ConditionsEigenvaluesProperties
λ 1 = 1 h μ λ 2 = 1 + h ( β A μ k α 1 γ μ )
0 < h < 2 μ β A μ ( α 1 + γ + μ ) < k < β A μ ( α 1 + γ + μ 2 h ) , h > 2 α 1 + γ + μ | λ 1 | < 1 | λ 2 | < 1 Stable
k = β A μ ( α 1 + γ + μ 2 h ) , h > 2 α 1 + γ + μ | λ 2 | = 1 Non-hyperbolic
k = β A μ ( α 1 + γ + μ )
k > β A μ ( α 1 + γ + μ 2 h ) , h > 2 α 1 + γ + μ or k < β A μ ( α 1 + γ + μ ) | λ 2 | > 1 Unstable
h = 2 μ β A μ ( α 1 + γ + μ ) < k < β A μ ( α 1 + γ ) | λ 1 | = 1 | λ 2 | < 1 Non-hyperbolic
k = β A μ ( α 1 + γ ) | λ 2 | = 1
k = β A μ ( α 1 + γ + μ )
k > β A μ ( α 1 + γ ) or k < β A μ ( α 1 + γ + μ ) | λ 2 | > 1 Unstable
h > 2 μ k < β A μ ( α 1 + γ + μ 2 h ) or k > β A μ ( α 1 + γ + μ ) | λ 1 | > 1 | λ 2 | < 1
k = β A μ ( α 1 + γ + μ 2 h ) | λ 2 | = 1
k = β A μ ( α 1 + γ + μ )
β A μ ( α 1 + γ + μ 2 h ) < k < β A μ ( α 1 + γ + μ ) | λ 2 | > 1
Table 3. Stability of the fixed point E .
Table 3. Stability of the fixed point E .
ConditionsEigenvalues ( λ 1 λ 2 )Properties
M 2 > 4 N N 1 < M < N + 1 , N < 1 1 < λ 2 < λ 1 < 1 Stable
N > 1 , M = N + 1 λ 2 = 1 , 1 < λ 1 < 1 Non-hyperbolic
N > 1 , M = N 1 1 < λ 2 < 1 , λ 1 = 1
M > N + 1 λ 2 < 1 Unstable
M < N 1 λ 1 > 1
M 2 = 4 N 2 < M < 2 , 0 < N < 1 1 < λ 1 , 2 < 1 Stable
M = 2 λ 1 , 2 = 1 Non-hyperbolic
M = 2 λ 1 , 2 = 1
M > 2 λ 1 , 2 < 1 Unstable
M < 2 λ 1 , 2 > 1
M 2 < 4 N 0 < N < 1 | λ 1 , 2 | < 1 Stable
2 < M < 2 , N = 1 | λ 1 , 2 | = 1 Non-hyperbolic
N > 1 | λ 1 , 2 | > 1 Unstable
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Hu, D.; Liu, X.; Li, K.; Liu, M.; Yu, X. Codimension-Two Bifurcations of a Simplified Discrete-Time SIR Model with Nonlinear Incidence and Recovery Rates. Mathematics 2023, 11, 4142. https://doi.org/10.3390/math11194142

AMA Style

Hu D, Liu X, Li K, Liu M, Yu X. Codimension-Two Bifurcations of a Simplified Discrete-Time SIR Model with Nonlinear Incidence and Recovery Rates. Mathematics. 2023; 11(19):4142. https://doi.org/10.3390/math11194142

Chicago/Turabian Style

Hu, Dongpo, Xuexue Liu, Kun Li, Ming Liu, and Xiao Yu. 2023. "Codimension-Two Bifurcations of a Simplified Discrete-Time SIR Model with Nonlinear Incidence and Recovery Rates" Mathematics 11, no. 19: 4142. https://doi.org/10.3390/math11194142

APA Style

Hu, D., Liu, X., Li, K., Liu, M., & Yu, X. (2023). Codimension-Two Bifurcations of a Simplified Discrete-Time SIR Model with Nonlinear Incidence and Recovery Rates. Mathematics, 11(19), 4142. https://doi.org/10.3390/math11194142

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