Startseite Technik Computational analysis of the Covid-19 model using the continuous Galerkin–Petrov scheme
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Computational analysis of the Covid-19 model using the continuous Galerkin–Petrov scheme

  • Rahila Naz , Aasim Ullah Jan , Attaullah , Salah Boulaaras EMAIL logo und Rafik Guefaifia
Veröffentlicht/Copyright: 15. Oktober 2024
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Abstract

Epidemiological models feature reliable and valuable insights into the prevention and transmission of life-threatening illnesses. In this study, a novel SIR mathematical model for COVID-19 is formulated and examined. The newly developed model has been thoroughly explored through theoretical analysis and computational methods, specifically the continuous Galerkin–Petrov (cGP) scheme. The next-generation matrix approach was used to calculate the reproduction number ( R 0 ) . Both disease-free equilibrium (DFE) ( E 0 ) and the endemic equilibrium ( E ) points are derived for the proposed model. The stability analysis of the equilibrium points reveals that ( E 0 ) is locally asymptotically stable when R 0 < 1 , while E is globally asymptotically stable when R 0 > 1 . We have examined the model’s local stability (LS) and global stability (GS) for endemic equilibrium   and DFE based on the number ( R 0 ) . To ascertain the dominance of the parameters, we examined the sensitivity of the number ( R 0 ) to parameters and computed sensitivity indices. Additionally, using the fourth-order Runge–Kutta (RK4) and Runge–Kutta–Fehlberg (RK45) techniques implemented in MATLAB, we determined the numerical solutions. Furthermore, the model was solved using the continuous cGP time discretization technique. We implemented a variety of schemes like cGP(2), RK4, and RK45 for the COVID-19 model and presented the numerical and graphical solutions of the model. Furthermore, we compared the results obtained using the above-mentioned schemes and observed that all results overlap with each other. The significant properties of several physical parameters under consideration were discussed. In the end, the computational analysis shows a clear image of the rise and fall in the spread of this disease over time in a specific location.

1 Introduction

Infections caused by viruses have consistently posed a significant danger to humanity throughout our collective history. Several recent epidemics have caused significant loss of life and widespread devastation worldwide. For example, the Spanish Flu pandemic, for instance, which tragically devastated the lives of millions of people across the globe. Numerous diseases, such as HIV/AIDS, have a devastating impact on countless lives each year as they rapidly spread among populations. Recently, instances of coronavirus pandemics have been documented [1,2,3,4,5]. A respiratory disorder was apparently identified in 2019 in the Hubei, province of China as an infectious illness brought on by a novel strain of the COVID-19 viral infection, also known as Respiratory Syndrome COVID-19, previously known as 2019-nCoV [6,7,8]. SARS, a coronavirus outbreak that destroyed more than 800 lives and caused more than 8,000 positive cases. Middle East Respiratory Syndrome (MERS) is thought to have spread from its original location in the Kingdom of Saudi Arabia to other nearby and far-off nations, particularly those along the Persian Gulf. In a few situations, MERS is already a contributing cause [9]. World Health Organization (WHO) initially received the report on December 31, 2019, regarding the outbreak of a contagious disease. On January 30, 2020, WHO formally identified it as COVID-19, a pandemic that exists and adversely affects the whole planet [10,11]. According to reports, the illness first affected animals before moving on to people. It was asserted by the media that, in the initial stage of the pandemic, the disease is transmitted by bats [12]. When the entire region was sealed in Wuhan in January and February 2020, the pandemic expanded rapidly. Later, reports of positive cases also came from the USA and other countries on both sides of the Pacific and Atlantic. Then, it was discovered that the illness was contagious and could spread through physical contact between individuals. In the middle of March 2020, the WHO proclaimed the virus to be a pandemic [13]. CoV-2 can remain on a surface for hours or days, depending on how sunshine, climatic change, and the surface material affect it. By engaging with a virus-contaminated object or material and then touching one’s lips, nose, or eyes, COVID-19 could be transmitted. Sadly, there are other ways for the virus to spread as well. Social isolation outside of the home decreases the chances of coming into contact with infectious objects or contagious people [14]. The government implemented a series of control measures, including strict lockdowns, social distancing, limits on gatherings, and the mandatory use of face masks to effectively reduce the transmission of COVID-19. Many countries implemented rigorous measures to verify the interactions of individuals who were known to be infected with COVID-19. This was done in order to effectively control the spread of the virus, and any incidents were promptly isolated for medical attention [15].

On March 7, 2021, sources stated that the pandemic has spread to numerous nations, with 116.17 million and above confirmed cases and 2.58 million losses [16]. Forty-one registered admitted positive events were confirmed as COVID-19 positive in China on January 2, 2020. More than 25 different Chinese provinces confirmed 571 COVID-19 incidents on January 22, 2020 [7,17]. On January 30, 2020, China had 7,734 COVID-19 occurrences that tested positive, as well as 90 overseas cases that were exported to roughly 13 other nations, including India, France, Germany, Canada, the UAE, and the USA. Over 4,667,780 positive cases were discovered worldwide by October 31, 2020 (Asia: 13,461,293 COVID patients, Africa: 1,776,595 COVID patients, Europe: 9,840,736 cases, America: 20,546,580 cases, Oceania: 41,880 cases, and others: 696 cases), resulting in 1,189,499 casualties (Asia: 239,675 losses, Africa: 42,688 losses, Europe: 265,565 losses, America: 640,513 losses, and others: 7 deaths) [18,19].

For better comprehension of how infectious and contagious diseases spread, mathematical models are useful. It is an effective instrument for assessing processes and phenomena in the actual world [2024]. In 1760, Bernoulli became the first mathematician to suggest a novel mathematical model that depicts how infectious and contagious diseases spread. Later, the subject caught the interest of numerous scientists and researchers. These models make it easier to comprehend a wide range of physical and biological events and how they work. Models in this subject now range from the straightforward to the complex and intricate. Using mathematical models, many infectious and non-infectious diseases have been studied (see, for example, previous studies [21,22]). Computational equations are used by researchers to comprehend and examine the dynamics of a disease; see previous studies [25,26] for more information.

The local stability (LS) and global stability (GS) of the endemic and negative pool equilibria (disease-free equilibria [DFE]) were evaluated by the researchers using nonlinear numerical analytic approaches. Similar to this, researchers have carried out a thorough analysis of the innovative COVID-19 mathematical models that cover several perspectives of the disease. Global and local dynamics are studied along with stability theory and numerical simulations. In this area, we have been introduced to several outstanding studies [2733]. Epidemiological models were used to obtain accurate and valuable information regarding the prevention and spread of illness. Consequently, our objective is to investigate the COVID-19 problem. In order to describe the COVID-19 epidemic, this work seeks to develop a SEQIRP model originating from the SIR model. Based on the reproduction number (R 0), the model’s analysis will provide an understanding of the stable and unstable states [3436]. Additionally, sensitivity analysis identifies the parameter that the system relies on the most, and numerical simulation illustrates how parameters change over time to forecast the COVID-19 outbreak. Ben Makhlouf et al. [37] investigated the existence and uniqueness of Hadamard Itô–Doob Stochastic delay fractional integral equations (HIDSDFIE) under non-Lipschitz conditions and by using the successive approximation. Rhaima et al. [38] discussed the existence and uniqueness properties pertaining to a class of fractional Hadamard Itô–Doob stochastic integral equations (FHIDSIE). Our study centers around the utilization of the Picard iteration technique (PIT), which not only establishes these fundamental properties but also unveils the remarkable averaging principle within FHIDSIE. Makhlouf et al. [39] developed a systematic discussion of the existence and uniqueness of the solution of a family of proportional Liouville–Caputo fractional stochastic differential equations by applying the Banach fixed point technique. Makhlouf et al. [40] investigated the existence and Ulam–Hyers stability (UHS) results in the context of mixed Hadamard and Riemann–Liouville fractional stochastic differential equations (HRFSDEs).

2 Model formulation

The overall human population N(t) is divided into six categories: susceptible ( S ), exposed ( E ), under quarantine ( Q ), infected ( I ), and death (P). The part of the population that gets healthy is denoted by R . The variables S(t) stands for the susceptible group, E ( t ) for diseased but not contagious individuals, and Q ( t ) for quarantine, which has the potential to produce either uninfected, infected outcomes, or fatal outcomes depending on the circumstances, I ( t ) stands for the number of infected individuals who are cured or they would die, and R ( t ) stands for those who have recovered and been cured of the illness. The variable P ( t ) depicts the disease that results in death. The population as a whole is represented by N ( t ) . The flowchart of the SEQIRP mathematical model is represented in Figure 1.

Figure 1 
               The graphical representation of the SEQIRP model.
Figure 1

The graphical representation of the SEQIRP model.

All of the categories that make up the population ( N ) are Sus ( S ), Exp ( E ), Qua ( Q ), Inf ( I ), Rec ( R ), and death ( P ). Mathematically,

N ( t ) = S ( t ) + E ( t ) + Q ( t ) + I ( t ) + R ( t ) + P ( t ) .

The modified framework comprises a system of differential equations, which is illustrated as follows:

(1) d S d t = ( β 1 + β 2 ) SI N + β 1 SE + ϵ Q ,

(2) d E d t = β 1 SI N ( γ + μ + η + σ ) E ,

(3) d Q d t = β 2 SI N + γ E ( μ + ν + τ ) Q ,

(4) d I d t = η E + ν Q ( δ + μ + r ) I ,

(5) d R d t = r I μ R ,

(6) d P d t = μ ( E + Q + S ) + δ I .

Figure 1 shows the pictorial diagram of the model.

Table 1 defines the parameters used in the model. Knowing that S ( t ) , E(t), Q(t), I(t), R(t), and P(t) are portions of all the population, we may state the following:

s ( t ) + e ( t ) + q ( t ) + i ( t ) + r ( t ) + p ( t ) = 1 ,

where s(t) = S ( t ) N , e(t) = E ( t ) N , q(t) = Q ( t ) N , i(t) = I ( t ) N , r(t) = R ( t ) N , p(t) = P ( t ) N .

Table 1

Description of variables used in the model

Parameters Physical interpretation Values
τ Death rates for classes that were exposed to death 0.0002
β 1 Rate of contact between exposed and susceptible classes 0.0517901
β 2 Rate of contact between susceptible and quarantine classes 0.2
δ Mortality rate due to corona viruses in infected individual class 1.6728 × 10−5
γ Transfer rate of exposed people to quarantine 2.0138 × 10−4
η Rate of people shifting from the Exp class to the Inf class 0.4478
μ Rate of natural death 0.0106
ν Transfer ratio of quarantined people to the class of infected people 3.2084 × 10−4
σ Quarantine class to death class mortality ratio 0.01
r Recovering rate of those who are infected 5.7341 × 10−5
ϵ Transfer ratio from the quarantine class to the susceptible class 0.6

Now, we can assume the system of Eqs. (1)–(6) as follows:

(7) d s ( t ) d t = ( β 1 + β 2 ) s ( t ) i ( t ) + β 1 e ( t ) + ϵ q ( t ) ,

(8) d e ( t ) d t = β 1 s ( t ) i ( t ) ( γ + μ + η + σ ) e ( t ) ,

(9) d q ( t ) d t = β 2 s ( t ) i ( t ) + γ e ( t ) ( μ + ν + τ ) q ( t ) ,

(10) d i ( t ) d t = η e ( t ) + ν q ( t ) ( δ + μ + r ) i ( t ) ,

(11) d r ( t ) d t = r i ( t ) μ r ( t ) ,

(12) d p ( t ) d t = μ ( e ( t ) + q ( t ) + s ( t ) ) + δ i ( t ) .

3 Numerical analysis of the model

Here, we perform the computational analysis of the system consisting of Eqs. (7)–(12).

3.1 Equilibria

At equilibrium, the left-hand side (LHS) of the system of Eqs. (7)–(12) will be zero, i.e.,

d s ( t ) d t = 0 , d e ( t ) d t = 0 , d q ( t ) d t = 0 , d i ( t ) d t = 0 , d r ( t ) d t = 0 .

DFEs ( E 0 ) are equilibrium points without an infection. Consequently, the system of Eqs. (7)–(12) always maintains an equilibrium at E 0 = ( S 0 , 0, 0, 0, 0) = (1, 0, 0, 0, 0). The equilibrium points with an infection called endemic equilibrium   ( E ) . Therefore, point ( E ) from the system of Eqs. (7)–(12) is given by

s = β 1 e + ϵ q ( β 1 + β 2 ) i = S ,

e = β 1 s i ( γ + μ + η + σ ) = E ,

q = β 2 s i + γ e ( μ + ν + τ ) = Q ,

i = η e + ν q ( δ + μ + r ) = I ,

r = r μ i = R .

Thus, E = ( S , E , Q , I , R ) is the unique endemic equilibrium of the system of Eqs. (7)–(12).

3.2 Basic reproduction number ( R 0 )

The basic transmission rate, or the basic reproduction number R 0 , is an essential indicator for analyzing disease transmission patterns. It provides insights into the dynamics of disease spread and the effectiveness of control measures. If R 0 < 1 , then the DFE is stable, and the disease ceases to exist in the community. If R 0 > 1 , the endemic equilibrium exists because the disease spreads throughout the community. The number R 0 is obtained by the method known as the next-generation matrix.

Let X = ( E , Q , I ) , then it follows from the system of Eqs. (7)–(12) that

d X d t = V ,

where = β 1 s i β 2 s i 0 and V = ( γ + μ + η + σ ) e γ e + ( μ + ν + τ ) q η e ν q + ( δ + μ + r ) i .

The Jacobian of the matrices and V , which are symbolized by F and V, are given as follows:

F = 0 0 β 1 0 0 β 2 0 0 0 ,   V = γ + μ + η + σ 0 0 γ μ + ν + τ 0 η ν δ + μ + r .

The multiplicative inverse of the matrix V is

V 1 = 1 γ + μ + η + σ 0 0 γ ( γ + μ + η + σ ) ( μ + ν + τ ) 1 μ + ν + τ 0 γ ν + η ( μ + ν + τ ) ( γ + μ + η + σ ) ( μ + ν + τ ) ( δ + μ + r ) ν ( μ + ν + τ ) ( δ + μ + r ) 1 δ + μ + r .

The next-generation matrix for the system of Eqs. (7)–(12) is

F V 1 = β 1 ( γ ν + η ( μ + ν + τ ) ) ( γ + μ + η + σ ) ( μ + ν + τ ) ( δ + μ + r ) β 1 ν ( μ + ν + τ ) ( δ + μ + r ) β 1 δ + μ + r β 2 ( γ ν + η ( μ + ν + τ ) ) ( γ + μ + η + σ ) ( μ + ν + τ ) ( δ + μ + r ) β 2 ν ( μ + ν + τ ) ( δ + μ + r ) β 2 δ + μ + r 0 0 0 .

The eigenvalues of the matrix F V 1 is λ 1 = λ 2 = 0 and

λ 3 = 1 ( μ + ν + τ ) ( δ + μ + r ) β 1 ( γ ν + η ( μ + ν + τ ) ) ( γ + μ + η + σ ) + β 2 ν . Therefore, R 0 is the highest (dominant) among the two eigenvalues of F V 1 . As a result, we have

(13) R 0 = 1 ( μ + ν + τ ) ( δ + μ + r ) β 1 ( γ ν + η ( μ + ν + τ ) ) ( γ + μ + η + σ ) + β 2 ν .

This is the system’s necessary reproductive number R 0 .

3.3 Stability analysis

The stability of the equilibrium points E 0 and E on a local and global basis are discussed in this section.

Theorem 1

When R 0 < 1 , the DFE E 0 is locally asymptotically stable. If R 0 = 1 , E 0 is locally stable. When R 0 > 1 , then point E 0 is an unstable saddle point.

Proof

The Jacobian matrix at point E 0 is given by

(14) J ( E 0 ) = 0 β 1 ϵ ( β 1 + β 2 ) 0 0 ( γ + μ + η + σ ) 0 β 1 0 0 γ ( μ + ν + τ ) β 2 0 0 η ν ( δ + μ + r ) 0 0 0 0 r μ ,

E 0 is locally asymptotically stable [34] if all the eigenvalues of J ( E 0 ) have a negative real part, which means R 0 < 1 . Again, E 0 is unstable if at least one of the eigenvalues of J ( E 0 ) has a positive real part, which means R 0 > 1 . Now, from J ( E 0 ) , we obtain the two eigenvalues: λ 1 = 0 ,   λ 2 = μ ; the other eigenvalues of J ( E 0 ) are determined by the following equation:

(15) λ 3 + C 3 λ 2 + C 4 λ + C 5 = 0 ,

where A = ( γ + μ + η + σ ) ,   B = ( μ + ν + τ ) ,   C = ( δ + μ + r ) ,

C 3 = ( A + B + C ) > 0 ,

C 4 = ( A B + A C + B C β 1 η β 2 ν ) ,

C 5 = A B C B β 1 η A β 2 ν β 1 γ ν ,

C 4 = A B + A C ( 1 R 0 ) + B C ( 1 R 0 ) + B A β 1 η > 0 if  R 0 < 1 ,

C 5 = A B C ( 1 R 0 ) > 0 if  R 0 < 1 ,

C 3 C 4 C 5 = C C 4 + C ( A 2 + B 2 ) ( 1 R 0 ) + B 2 C β 1 η + A 2 C β 2 ν + A B 2 + A 2 B + A B C > 0 if  R 0 < 1   .

The Routh–Hurwitz criterion is satisfied as C 3 > 0 , C 4 > 0 ,   C 5 > 0 ,  and  C 3 C 4 C 5 > 0   if R 0 < 1 .

Therefore, all eigenvalues of Eq. (15) have a negative real part. On the other hand, one eigenvalue is zero, which means the reproductive number R 0 = 1 ( μ + ν + τ ) ( δ + μ + r ) β 1 ( γ ν + η ( μ + ν + τ ) ) ( γ + μ + η + σ ) + β 2 ν leads us to a value 1, which is the precise information of system (14) based on the study of Shahrear et al. [34]. The remaining eigenvalues of system (14) have a negative real part. This concludes the analysis of the DFE of system (14), which means E 0 is locally stable [34].□

Theorem 2

When R 0 > 1 , E (endemic equilibrium) is locally asymptotically stable.

Proof

The Jacobian matrix of the model (7)–(12) at E = ( S , E , Q , I , R ) is

J ( E ) = ( β 1 + β 2 ) I β 1 ϵ ( β 1 + β 2 ) S 0 β 1 I ( γ + μ + η + σ ) 0 β 1 S 0 β 2 I γ ( μ + ν + τ ) β 2 S 0 0 η ν ( δ + μ + r ) 0 0 0 0 r μ .

Trace

J ( E ) = ( β 1 + β 2 ) I ( γ + μ + η + σ ) ( μ + ν + τ ) ( δ + μ + r ) μ < 0 .

Now, det

J ( E ) = μ ( β 1 + β 2 ) ( γ + μ + η + σ ) ( μ + ν + τ ) ( δ + μ + r ) I + β 1 2 μ ( μ + ν + τ ) ( δ + μ + r ) I + ϵ μ β 1 γ ( δ + μ + r ) I + ϵ μ β 2 ( γ + μ + η + σ ) ( δ + μ + r ) I .

From the study of Shahrear et al. [34], the equilibrium E of the system of Eqs. (7)–(12) has a negative real part. Thus, we conclude that E of the system is locally asymptotically stable, so R 0 > 1. This finalizes the proof.□

Theorem 3

The system of Eqs. (7)–(12) has no periodic orbits.

Proof

We apply Dulac’s criterion to prove this. Now, let X = ( S , E , Q , I , R ) . Pursing the Dulac’s function

G = 1 S E ,

in the case,

G d S d t = ( β 1 + β 2 ) I E + β 1 S + ϵ Q S E   ,

G d E d t = β 1 I E ( γ + μ + η + σ ) S   ,

G d Q d t = β 2 I E + γ S ( μ + ν + τ ) Q S E   ,

G d I d t = η S + ν Q S E ( δ + μ + r ) I S E   ,

G d R d t = r I S E μ R S E   .

Thus,

d G X d t = S G d S d t + E G d E d t + Q G d Q d t + I G d I d t + R G d R d t ,

d G X d t = S ( β 1 + β 2 ) I E + β 1 S + ϵ Q S E + E β 1 I E ( γ + μ + η + σ ) S + Q β 2 I E + γ S ( μ + ν + τ ) Q S E + I η S + ν Q S E ( δ + μ + r ) I S E + R r I S E μ R S E ,

d G X d t = β 1 S ⁎2 ϵ Q S ⁎2 E β 1 I E ⁎2 ( μ + ν + τ ) S E ( δ + μ + r ) S E μ S E ,

d G X d t = β 1 S ⁎2 + ϵ Q S ⁎2 E + β 1 I E ⁎2 + ( δ + 3 μ + ν + τ + r ) S E < 0 .

There is no periodic orbit in the system of Eqs. (7)–(12) as a result. The proof is now complete.□

Theorem 4

The endemic equilibrium E for the system of Eqs. (7)–(12) is globally asymptotically stable whenever R 0 > 1.

3.4 Sensitivity analysis

The reproductive number R 0 clearly identifies the start of disease transmission. To identify which model parameters have an important impact on the fundamental reproduction number ( R 0 ) and, subsequently, the spread of disease, we calculate the sensitivity indices of R 0 to those values. Assuming parameter P i , the normalized sensitivity indices of R 0 are given by

I P i R 0 = R 0 P i P i R 0 .

In this study, we examine the sensitivity analysis of R 0 to the model parameters. We use the parameter values from Table 1 in this case. We obtained R 0 from Eq. (13), which contains an explicit formula for

R 0 = 1 ( μ + ν + τ ) ( δ + μ + r ) β 1 ( γ ν + η ( μ + ν + τ ) ) ( γ + μ + η + σ ) + β 2 ν .

The parameters’ sensitivity is determined as follows:

I β 1 R 0 = R 0 β 1 β 1 R 0 = γ ν + η ( μ + ν + τ ) ( γ + μ + η + σ ) ( μ + ν + τ ) ( δ + μ + r ) β 1 R 0 ,

when the parameter values from Table 1 were used, we obtained 0.44.

I β 2 R 0 = R 0 β 2 β 2 R 0 = ν ( μ + ν + τ ) ( δ + μ + r ) β 2 R 0 ,

after using the parameter values from Table 1, we obtained a value of −0.80.

I δ R 0 = R 0 δ δ R 0 = 1 ( μ + ν + τ ) ( δ + μ + r ) 2 β 1 ( γ ν + η ( μ + ν + τ ) ) ( γ + μ + η + σ ) + β 2 ν δ R 0 ,

after using the parameter values from Table 1, we obtained a value of −0.16.

We may argue that if β 1 increases by 10%, then R 0 increases by 10% |0.44| = 0.044, which can cause an outbreak. Likewise, if β 1 drops by 10%, then R 0 falls by 10% |0.44| = 0.044, indicating that the value of β 1 significantly affects the value of R 0 . For controlling the sickness, it is necessary to lower the rate of β 1 . The WHO and the government encouraged quarantine and other preventative measures to deal with the pandemic. Additionally, the number R 0 can be affected by changing the values of β 2 and δ .

3.5 Numerical schemes

3.5.1 Continuous Galerkin–Petrov (cGP) technique

The Galerkin technique is a powerful tool for numerically exploring significant difficulties in various real-world problems. This approach is often used for complex problems and can handle nonlinear systems and complicated issues (refer previous studies [4152] for more information). This section discusses the numerical schemes used to solve the aforesaid model to assess the dynamic behavior of the model. The system of ODEs for the considered model can be written as follows:

Find V ˜ : [ 0 , t max ] V = d ; then d t V ˜ ( t ) = F ( t , V ˜ ( t ) ) t R ,

(16) V ˜ ( 0 ) = V ˜ 0 ,

where d t is the time derivative of V ˜ ( t ) , R = [ 0 , T ] is the whole interval, V ˜ ( t ) = ( V ˜ 1 ( 0 ) , V ˜ 2 ( 0 ) , V ˜ 3 ( 0 ) ) V V ˜ ( 0 ) = ( V ˜ 1 ( 0 ) , V ˜ 2 ( 0 ) , V ˜ 3 ( 0 ) ) V are the initial values of V ˜ ( t ) at t = 0 .

We further assume that ( V ˜ 1 ( 0 ) , V ˜ 2 ( 0 ) , V ˜ 3 ( 0 ) ) = ( T ( t ) , R ( t ) , V ( t ) ) , which implies that ( V ˜ 1 ( 0 ) , V ˜ 2 ( 0 ) , V ˜ 3 ( 0 ) )   = ( T ( 0 ) , R ( 0 ) , V ( 0 ) ) . The function F =   ( f 1 , f 2 , f 3 ) is nonlinear and is defined as F :   R × S S .

The weak formulation (see previous studies [10,11,12,13,14,15,17] for explanation) of problem (16) is as follows: Find V ˜ X such that V ˜ ( 0 ) = V ˜ 0 and

(17) I d t V ˜ ( t ) ,   v ( t ) d t = I F ( t , V ˜ ( t ) , v ( t ) ) d t for all  v ϵ Y ,

where the test space and solution, respectively, are represented by X and Y in order to describing the time discretization of a variation kind problem (16).

Identify the function t V ˜ ( t ) ;  then , we describe the space C ( R , S ) = C 0 ( R , S ) .   It is the continuous function space V ˜ : R S possessing the following standard norm:

V ˜ C ( R , S ) = t I Sup V ˜ K .

We shall utilize the space L 2 ( R , S )   as the space of the functions that are discontinuous and defined as

L 2 ( R ,   S ) = V ˜ :   R S :   V ˜ L 2 ( R , S ) = R V ˜ S 2 d t < 1 / 2 .

During time discretization, the intervals R are divided into N subintervals R τ =   [ t τ 1 , t τ ] ,   where τ =   1 , , N and   0   =   t 0   < t 1   < t 2   < < t N 1   < t N = T . The parameter j indicates the time discretization with the largest time step size j = max j τ 1 τ N , where j τ = t τ t τ 1 , the length of the nth time interval R τ . The time step is calculated from the following collection of time intervals M j = { R 1 , , R N } . We perceive the solution V ˜ :   R S on all time intervals R τ through a function V ˜ j : R S described by

X j l = { V ˜ C ( R , S ) :   V ˜ I τ l ( R τ , S )  for all  I τ M j } ,

where

l ( R τ , S ) = V ˜ :   R τ   S :   V ˜ ( t ) = s = 0 l U s t s , for all  t R τ , U s S ,   s .

The discrete test space for V ˜ j is Y j l Y and is defined by

(18) Y j k = { v L 2 ( R , S ) : v | R τ k 1 ( R τ , S )   R τ M j } ,

which is made up of l − 1 piecewise polynomials (see previous studies [4152] for details) and at time step ending nodes, it is discontinuous. Multiplying Eq. (16) with test functions v j Y j k and then integrating in excess of the interval R, we obtain the discrete-time case. Find V ˜ X j k , so that V ˜ j ( 0 ) = 0 and

(19) R V ˜ j '   ( t ) ,   v j ( t ) d t = R F ( t ,   V ˜ j ( t ) ,   v j ( t ) ) d t   v j ϵ Y j l .

Using the test functions v j ( t )   =   ν ψ ( t )   with ν ∈ S and a scalar function ψ :   R R ,   which is zero on R | R τ and a polynomial of order less than or equal to l 1   on the time interval R τ = [ t τ 1 , t τ ] . Now, we find   V ˜ j | I τ k 1 ( R τ , S ) such that

(20) R τ d t   V ˜ j ( t ) ,   v j ( t )   φ ( t ) d t = R τ F ( t ,   V ˜ j ( t ) ,   v ) φ ( t ) d t v ϵ S   φ l 1 ( R τ ) ,

with the initial conditions   V ˜ j | R τ ( t τ 1 ) =   V ˜ j | R τ 1 ( t τ 1 ) for τ 2   and   V ˜ j | R τ ( t τ 1 ) =   V ˜ 0 for τ = 1 . To determine cGP(l), we will find   V ˜ j | R τ 1 l ( R τ , S )   such that   V ˜ j ( t τ 1 ) =   V ˜ τ 1 . This leads us to

(21) s = 0 l w ˆ s d t   V ˜ j ( t τ , s ) φ ( t τ , s ) = s = 0 k w ˆ s F ( t τ , s ,   V ˜ j ( t τ , s ) ) φ ( t τ , s ) φ l 1 ( R τ ) ,

where the weights are denoted by w ˆ s . These weights are represented by t ˆ  [ 1 , 1 ] , s =   0 , 1 , 2 , 3 , , l . We utilize a polynomial ansatz to determine   V ˜ j for every time interval R τ as follows:

(22)   V ˜ j ( t ) = s = 0 k U τ s ϕ τ , s ( t ) t   R τ ,

where the coefficients U τ s are the components of S and the functions ϕ τ , s l ( R τ ) are the Lagrange basis functions (see previous studies [4152] for more details) w.r.t. l +   1   appropriate nodal points t τ , s R τ satisfying the conditions specified below:

(23) ϕ τ , s ( t τ , r ) = δ r , s   , r ,   s   =   0 , 1 , 2 ,     ,   l .

where δ r , s denotes the Kronecker delta and is defined as follows:

δ r , s = 1 , if r = s , 0 , if r s .

Here, t τ , s are described as the quadrature points [46] of “ ( l +   1 ) - point Gauß-Lobatto” formula (for more information, see previous studies [4152]) on the R τ interval. Choosing initial conditions is important, we can therefore set   t τ , 0 = t τ 1 which indicates the initial conditions for Eq. (20):

U τ 0 = V ˜ j | R τ 1 if  τ 2 ,

for  τ = 1 U τ 0 = V ˜ 0 .

We define the basis functions ϕ τ , s l ( R τ ) via the affine reference transformation (see previous studies [4152] for detailed explanation) T ¯   : R ˆ R τ   where R ˆ = [ 1 ,   1 ]   and

t = T ¯ ( t ˆ ) = t τ t τ 1 2 + j τ 2 t ˆ R τ t ˆ R τ   , τ = 1 ,   2 ,   3   ,   N .

Let ϕ ˆ s l ( R ˆ ) , s = 0 ,   1 , ,   l , illustrate the basis functions that satisfy

ϕ ˆ s (   t ˆ r ) = δ r , s r ,   s   =   0 ,   1 ,   2 , ,   l ,

in which t ˆ 0 = 1 and t ˆ r ,   r =   1 , 2 , , l , are the quadrature points based on the interval R ˆ . The basis functions on the specified interval R τ are defined by the mapping

ϕ τ , s ( t ) = ϕ ˆ s (   t ˆ r ) with  t ˆ = T ¯ τ 1 ( t ) = 2 j τ t + t τ 1 t τ 2 R ˆ .

Similarly, the appropriate reference basis functions φ ˆ l 1 ( R ˆ ) also define the test basis functions, which are denoted by φ τ , r , i.e.,

φ τ , r ( t ) = φ ˆ r ( T ¯ τ 1 ( t ) ) t R τ   ,   r   =   1 ,   2 ,   ,   l .

According to the illustration (22), we learn that d t V ˜ j

(24) d t   V ˜ j ( t ) = s = 0 k U τ s   ϕ τ , s ' ( t ) t   R τ .

By substituting Eq. (24) into Eq. (20), we obtain

R τ d t   V ˜ j ( t ) , v φ ( t ) d t = R τ s = 0 k U τ s ϕ τ ( t )   φ ( t )  d t .

Next, the integral is converted into the referral interval R ˆ and calculated using the “ ( l +   1 ) -point Gauß–Lobatto quadrature” formula, which results in all test basis functions having the value ϕ l 1   and for every ν ∈ S,

R τ s = 0 l U τ s , v ϕ ˆ s ( t ˆ )   φ ˆ ( t ˆ ) d t ˆ = R τ F w τ ( t ˆ ) ,   s = 0 l U τ s ( t ˆ ) , v φ ˆ ( t ˆ ) d t ˆ v S ,

μ = 0 l w ˆ μ μ = 0 l U τ s , v ϕ ˆ s ' ( t ˆ μ )   φ ˆ ( t ˆ μ ) = μ = 0 l w ˆ μ F w τ ( t ˆ ) , s = 0 l U τ s ( t ˆ ) , v φ ˆ ( t ˆ μ ) ,

where t ˆ μ [ 1 , 1 ]   is the integration point with t ˆ 0 = 1 and t ˆ l = 1 and w ˆ μ represents the weights. If we pick the test functions φ τ , i l 1 ( R τ ) such that

φ ˆ ( t ˆ μ ) = ( w ˆ ) 1 δ r , μ r , μ   =   1 ,   2 , ,   l .

The undetermined coefficient U τ s S for s = 1 l , are found by using

s = 0 l α r , s U τ s = j τ 2 { F ( t τ , r ,   U τ s ) + β r F ( t τ , 0 , U τ s ) } i = 1 ,   2 , ,   l ,

where U τ s = U τ 1 s  for  τ > 1  and  U 1 0 =   V ˜ 0  for  τ = 1  and

α r , s = ϕ ˆ s ( t ˆ r ) + β r ϕ ˆ s ( t ˆ 0 )   ,   β r =   w ˆ 0 φ ˆ r ( t ˆ 0 ) .

We will discuss the cGP(k) approach for two cases k =   1  and k =   2 .

The cGP(1) method

The “two-point Gauß–Lobatto” formula was employed with   t τ , 0 = t τ 1 , t τ , 1 = t τ , and weights w ˆ 0 = w ˆ 1 = 1 that provides the famous Trapezoidal rule. We obtained α 1 , 0 = 1 , α 1 , 1 = 1 , and β 1 = 1 . For just one coefficient   U τ 1 = V ˜ j ( t τ ) S , the issue generates the block equation as follows:

α 1 , 1 U τ 1 α τ , 0 U τ 0 = j τ 2 { F ( t τ   ,   U τ 1 ) + F ( t τ 1   ,   U τ 0 ) } .

The cGP(2) method

The weighted quadratic basis functions w ˆ 0 = w ˆ 2 = 1 / 3 , w ˆ 1 = 4 / 3 , and t ˆ 0 = 1 , t ˆ 1 = 0 , t ˆ 2 = 1 are defined using the three-point Gauß–Lobatto formula (Simpson rule). Then, we obtain

α r , s = 5 4 1 1 4 2 4 2 ,   β r = 1 2 1 ,   r = 1 , 2 ,   s = 0 , 1 , 2 .

Therefore, the system that needs to be fixed for U τ 1 , U τ 2 K from the well-known U τ 0 = U τ 1 2 is as follows:

α 1 , 1 U τ 1 + α 1 , 2 U τ 2 = α 1 , 0 U τ 0 + j τ 2 { F ( t τ ,   1   , U τ 1 ) + β 1 F ( t τ ,   0   , U τ 0 ) } ,

α 2 , 1 U τ 1 + α 2 , 2 U τ 2 = α 2 , 0 U τ 0 + j τ 2 { F ( t τ ,   2   , U τ 2 ) + β 2 F ( t τ ,   0   , U τ 0 ) } ,

where U τ 0 indicates the initial conditions at the current time interval.

4 Numerical comparison and discussion

This section focuses on the numerical solution of the novel model of COVID-19 using the Galerkin scheme. The parameters listed in Table 1 are used to construct the model. In order to gain insight into the behavior of specific parameters in the suggested model, we explore different values for some of the parameters while keeping all other parameters constant. The model illustrates the geometric representation of the interactions and correlation between all parameters. It is clear from the figures that changing the values of the parameters will result in different effects on the dynamic behavior of the system. We only planned for the situation where one quantity (parameter) was varied. We explored the variations of ( η ) and ( μ ), as shown in Figures 213, across the six compartments S ( t ) , E ( t ) , Q ( t ) , I ( t ) , R ( t ) , and P ( t ) , respectively. Figures 2, 49 show an increasing behavior in the sensitive population over time as the value of η is increased, while they show the decreasing behavior for population dynamics of exposed class E ( t ) , as shown in Figure 3. The effects of various μ values on the exposed population are analyzed in Figures 8 and 13. Figures 8 and 12 illustrate the decreasing behavior for the population dynamics of S , E , Q , I , and R by increasing the values of μ . By increasing the values of μ , the concentration of   P increases, as displayed in Figure 13. Figures 1419 show the comparison graphs for the Galerkin method, RK methods, and Runge–Kutta–Fehlberg method solutions, respectively. Additionally, the Galerkin, fourth-order Runge–Kutta (RK4) and Runge–Kutta–Fehlberg methods are used for numerical computations in a certain manner and throughout a range of time intervals t [ 0 , 1 ] , as shown by the arithmetic values for various step sizes in Figures 1419.

Figure 2 
               Influence of 
                     
                        
                        
                           η
                        
                        \eta 
                     
                   on 
                     
                        
                        
                           S
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        S(t)
                     
                  .
Figure 2

Influence of η on S ( t ) .

Figure 3 
               Influence of 
                     
                        
                        
                           η
                        
                        \eta 
                     
                   on 
                     
                        
                        
                           E
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        E(t)
                     
                  .
Figure 3

Influence of η on E ( t ) .

Figure 4 
               Impact of 
                     
                        
                        
                           η
                        
                        \eta 
                     
                   on 
                     
                        
                        
                           Q
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        Q(t)
                     
                  .
Figure 4

Impact of η on Q ( t ) .

Figure 5 
               Impact of 
                     
                        
                        
                           η
                        
                        \eta 
                     
                   on 
                     
                        
                        
                           I
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        I(t)
                     
                  .
Figure 5

Impact of η on I ( t ) .

Figure 6 
               Effect of 
                     
                        
                        
                           η
                        
                        \eta 
                     
                   on 
                     
                        
                        
                           R
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        R(t)
                     
                  .
Figure 6

Effect of η on R ( t ) .

Figure 7 
               Effect of 
                     
                        
                        
                           η
                        
                        \eta 
                     
                   on 
                     
                        
                        
                           P
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        P(t)
                     
                  .
Figure 7

Effect of η on P ( t ) .

Figure 8 
               Influence of 
                     
                        
                        
                           μ
                        
                        \mu 
                     
                   on 
                     
                        
                        
                           S
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        S(t)
                     
                  .
Figure 8

Influence of μ on S ( t ) .

Figure 9 
               Influence of 
                     
                        
                        
                           μ
                        
                        \mu 
                     
                   on 
                     
                        
                        
                           E
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        E(t)
                     
                  .
Figure 9

Influence of μ on E ( t ) .

Figure 10 
               Impact of 
                     
                        
                        
                           μ
                        
                        \mu 
                     
                   on 
                     
                        
                        
                           Q
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        Q(t)
                     
                  .
Figure 10

Impact of μ on Q ( t ) .

Figure 11 
               Impact of 
                     
                        
                        
                           μ
                        
                        \mu 
                     
                   on 
                     
                        
                        
                           I
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        I(t)
                     
                  .
Figure 11

Impact of μ on I ( t ) .

Figure 12 
               Effect of 
                     
                        
                        
                           μ
                        
                        \mu 
                     
                   on 
                     
                        
                        
                           R
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        R(t)
                     
                  .
Figure 12

Effect of μ on R ( t ) .

Figure 13 
               Effect of 
                     
                        
                        
                           μ
                        
                        \mu 
                     
                   on 
                     
                        
                        
                           P
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        P(t)
                     
                  .
Figure 13

Effect of μ on P ( t ) .

Figure 14 
               Comparison results for 
                     
                        
                        
                           S
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        S(t)
                     
                  .
Figure 14

Comparison results for S ( t ) .

Figure 15 
               Comparison results for 
                     
                        
                        
                           E
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        E(t)
                     
                  .
Figure 15

Comparison results for E ( t ) .

Figure 16 
               Comparison results for 
                     
                        
                        
                           I
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        I(t)
                     
                  .
Figure 16

Comparison results for I ( t ) .

Figure 17 
               Comparison results for 
                     
                        
                        
                           Q
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        Q(t)
                     
                  .
Figure 17

Comparison results for Q ( t ) .

Figure 18 
               Comparison results for 
                     
                        
                        
                           R
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        R(t)
                     
                  .
Figure 18

Comparison results for R ( t ) .

Figure 19 
               Comparison results for 
                     
                        
                        
                           P
                           
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                        
                        P(t)
                     
                  .
Figure 19

Comparison results for P ( t ) .

Here, we graphically depict and match the outcomes. Figures 1419 compare the results of the Galerkin and RK techniques, which are substantially more similar. In Figures 2022, the mesh grid graphs are presented. Ultimately, we conclude that the numerical method presented in this study may be relied upon to provide solutions that are quite adaptable and precise when applied to situations of a similar nature.

Figure 20 
               The mesh grid graph of the Galerkin scheme.
Figure 20

The mesh grid graph of the Galerkin scheme.

Figure 21 
               The mesh grid graph of the RK4 scheme.
Figure 21

The mesh grid graph of the RK4 scheme.

Figure 22 
               The mesh grid graph of the RK45 scheme.
Figure 22

The mesh grid graph of the RK45 scheme.

5 Conclusion

In the present study, an innovative mathematical model was developed to illustrate the dynamics of different population groups, including susceptible, exposed, infected, quarantined, recovered, and deceased individuals. This model leads to a system of differential equations. The LS and GS of the DFE ( E 0 ) and endemic equilibrium ( E ) are examined for the proposed model. The number ( R 0 ) is evaluated using the next-generation matrix procedure. It is observed that when R 0 < 1 and R 0 > 1 , the DFE ( E 0 ) is found to be locally asymptotically stable and unstable, respectively. Additionally, the endemic equilibrium E for the system is globally asymptotically stable when R 0 > 1 . The model is solved numerically using the Galerkin–Petrov scheme and discusses the influence of different clinical parameters on the variation of state variables. The process of determining the sensitivity indices involves partial derivative analysis, which computes the partial derivatives of the model output ( R 0 ) with respect to the model parameters, aims to quantify the importance of each parameter in determining the behavior of the system based on the updated SIR model that has been demonstrated. Additionally, in order to assess the accuracy and dependability of the scheme, we numerically solved the model using the well-known traditional RK4 method and Runge–Kutta–Fehlberg (RK45) method. This simulation illustrates how the rates of infection, recovery, and death can change over time. Graphical illustrations of each result are displayed. It can be noted that the results obtained through all methods coincide with each other. Our future plans are focused on applying the proposed Galerkin scheme to a variety of mathematical models in population biology and epidemiology and other complex real-world problems consisting of non-linear differential equations.

Acknowledgment

The authors are thankful to the editor and anonymous reviewers for meticulously reading the manuscript, and giving us valuable comments and suggestions, which helped us to improve the quality of the manuscript.

  1. Funding information: There is no funding source available for this research.

  2. Author contributions: All the authors contributed equally.

  3. Conflict of interest: All the authors declare that they have no conflicts of interest.

  4. Data availability statement: No new data were created or analyzed in this study. Data sharing is not applicable to this article.

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Received: 2024-05-26
Revised: 2024-07-30
Accepted: 2024-04-12
Published Online: 2024-10-15

© 2024 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

Artikel in diesem Heft

  1. Editorial
  2. Focus on NLENG 2023 Volume 12 Issue 1
  3. Research Articles
  4. Seismic vulnerability signal analysis of low tower cable-stayed bridges method based on convolutional attention network
  5. Robust passivity-based nonlinear controller design for bilateral teleoperation system under variable time delay and variable load disturbance
  6. A physically consistent AI-based SPH emulator for computational fluid dynamics
  7. Asymmetrical novel hyperchaotic system with two exponential functions and an application to image encryption
  8. A novel framework for effective structural vulnerability assessment of tubular structures using machine learning algorithms (GA and ANN) for hybrid simulations
  9. Flow and irreversible mechanism of pure and hybridized non-Newtonian nanofluids through elastic surfaces with melting effects
  10. Stability analysis of the corruption dynamics under fractional-order interventions
  11. Solutions of certain initial-boundary value problems via a new extended Laplace transform
  12. Numerical solution of two-dimensional fractional differential equations using Laplace transform with residual power series method
  13. Fractional-order lead networks to avoid limit cycle in control loops with dead zone and plant servo system
  14. Modeling anomalous transport in fractal porous media: A study of fractional diffusion PDEs using numerical method
  15. Analysis of nonlinear dynamics of RC slabs under blast loads: A hybrid machine learning approach
  16. On theoretical and numerical analysis of fractal--fractional non-linear hybrid differential equations
  17. Traveling wave solutions, numerical solutions, and stability analysis of the (2+1) conformal time-fractional generalized q-deformed sinh-Gordon equation
  18. Influence of damage on large displacement buckling analysis of beams
  19. Approximate numerical procedures for the Navier–Stokes system through the generalized method of lines
  20. Mathematical analysis of a combustible viscoelastic material in a cylindrical channel taking into account induced electric field: A spectral approach
  21. A new operational matrix method to solve nonlinear fractional differential equations
  22. New solutions for the generalized q-deformed wave equation with q-translation symmetry
  23. Optimize the corrosion behaviour and mechanical properties of AISI 316 stainless steel under heat treatment and previous cold working
  24. Soliton dynamics of the KdV–mKdV equation using three distinct exact methods in nonlinear phenomena
  25. Investigation of the lubrication performance of a marine diesel engine crankshaft using a thermo-electrohydrodynamic model
  26. Modeling credit risk with mixed fractional Brownian motion: An application to barrier options
  27. Method of feature extraction of abnormal communication signal in network based on nonlinear technology
  28. An innovative binocular vision-based method for displacement measurement in membrane structures
  29. An analysis of exponential kernel fractional difference operator for delta positivity
  30. Novel analytic solutions of strain wave model in micro-structured solids
  31. Conditions for the existence of soliton solutions: An analysis of coefficients in the generalized Wu–Zhang system and generalized Sawada–Kotera model
  32. Scale-3 Haar wavelet-based method of fractal-fractional differential equations with power law kernel and exponential decay kernel
  33. Non-linear influences of track dynamic irregularities on vertical levelling loss of heavy-haul railway track geometry under cyclic loadings
  34. Fast analysis approach for instability problems of thin shells utilizing ANNs and a Bayesian regularization back-propagation algorithm
  35. Validity and error analysis of calculating matrix exponential function and vector product
  36. Optimizing execution time and cost while scheduling scientific workflow in edge data center with fault tolerance awareness
  37. Estimating the dynamics of the drinking epidemic model with control interventions: A sensitivity analysis
  38. Online and offline physical education quality assessment based on mobile edge computing
  39. Discovering optical solutions to a nonlinear Schrödinger equation and its bifurcation and chaos analysis
  40. New convolved Fibonacci collocation procedure for the Fitzhugh–Nagumo non-linear equation
  41. Study of weakly nonlinear double-diffusive magneto-convection with throughflow under concentration modulation
  42. Variable sampling time discrete sliding mode control for a flapping wing micro air vehicle using flapping frequency as the control input
  43. Error analysis of arbitrarily high-order stepping schemes for fractional integro-differential equations with weakly singular kernels
  44. Solitary and periodic pattern solutions for time-fractional generalized nonlinear Schrödinger equation
  45. An unconditionally stable numerical scheme for solving nonlinear Fisher equation
  46. Effect of modulated boundary on heat and mass transport of Walter-B viscoelastic fluid saturated in porous medium
  47. Analysis of heat mass transfer in a squeezed Carreau nanofluid flow due to a sensor surface with variable thermal conductivity
  48. Navigating waves: Advancing ocean dynamics through the nonlinear Schrödinger equation
  49. Experimental and numerical investigations into torsional-flexural behaviours of railway composite sleepers and bearers
  50. Novel dynamics of the fractional KFG equation through the unified and unified solver schemes with stability and multistability analysis
  51. Analysis of the magnetohydrodynamic effects on non-Newtonian fluid flow in an inclined non-uniform channel under long-wavelength, low-Reynolds number conditions
  52. Convergence analysis of non-matching finite elements for a linear monotone additive Schwarz scheme for semi-linear elliptic problems
  53. Global well-posedness and exponential decay estimates for semilinear Newell–Whitehead–Segel equation
  54. Petrov-Galerkin method for small deflections in fourth-order beam equations in civil engineering
  55. Solution of third-order nonlinear integro-differential equations with parallel computing for intelligent IoT and wireless networks using the Haar wavelet method
  56. Mathematical modeling and computational analysis of hepatitis B virus transmission using the higher-order Galerkin scheme
  57. Mathematical model based on nonlinear differential equations and its control algorithm
  58. Bifurcation and chaos: Unraveling soliton solutions in a couple fractional-order nonlinear evolution equation
  59. Space–time variable-order carbon nanotube model using modified Atangana–Baleanu–Caputo derivative
  60. Minimal universal laser network model: Synchronization, extreme events, and multistability
  61. Valuation of forward start option with mean reverting stock model for uncertain markets
  62. Geometric nonlinear analysis based on the generalized displacement control method and orthogonal iteration
  63. Fuzzy neural network with backpropagation for fuzzy quadratic programming problems and portfolio optimization problems
  64. B-spline curve theory: An overview and applications in real life
  65. Nonlinearity modeling for online estimation of industrial cooling fan speed subject to model uncertainties and state-dependent measurement noise
  66. Quantitative analysis and modeling of ride sharing behavior based on internet of vehicles
  67. Review Article
  68. Bond performance of recycled coarse aggregate concrete with rebar under freeze–thaw environment: A review
  69. Retraction
  70. Retraction of “Convolutional neural network for UAV image processing and navigation in tree plantations based on deep learning”
  71. Special Issue: Dynamic Engineering and Control Methods for the Nonlinear Systems - Part II
  72. Improved nonlinear model predictive control with inequality constraints using particle filtering for nonlinear and highly coupled dynamical systems
  73. Anti-control of Hopf bifurcation for a chaotic system
  74. Special Issue: Decision and Control in Nonlinear Systems - Part I
  75. Addressing target loss and actuator saturation in visual servoing of multirotors: A nonrecursive augmented dynamics control approach
  76. Collaborative control of multi-manipulator systems in intelligent manufacturing based on event-triggered and adaptive strategy
  77. Greenhouse monitoring system integrating NB-IOT technology and a cloud service framework
  78. Special Issue: Unleashing the Power of AI and ML in Dynamical System Research
  79. Computational analysis of the Covid-19 model using the continuous Galerkin–Petrov scheme
  80. Special Issue: Nonlinear Analysis and Design of Communication Networks for IoT Applications - Part I
  81. Research on the role of multi-sensor system information fusion in improving hardware control accuracy of intelligent system
  82. Advanced integration of IoT and AI algorithms for comprehensive smart meter data analysis in smart grids
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