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Article

Analytical Study of Fractional Epidemic Model via Natural Transform Homotopy Analysis Method

1
Industrial Technical Institute, Medium Valley Technological College, Ministry of Higher Education, Sohag 82786, Egypt
2
Mathematics Department, College of Science, King Khalid University, Abha 61413, Saudi Arabia
3
Department of Mathematics, Faculty of Science, Sohag University, Sohag 82524, Egypt
4
Department of Mathematics, Faculty of Science, Islamic University of Madinah, Madinah 42351, Saudi Arabia
*
Author to whom correspondence should be addressed.
Symmetry 2022, 14(8), 1695; https://doi.org/10.3390/sym14081695
Submission received: 1 July 2022 / Revised: 2 August 2022 / Accepted: 9 August 2022 / Published: 15 August 2022

Abstract

:
In this study, we present a new general solution to a rational epidemiological mathematical model via a recent intelligent method called the natural transform homotopy analysis method (NTHAM), which combines two methods: the natural transform method (NTM) and homotopy analysis method (HAM). To assess the precision and the reliability of the present method, we compared the obtained results with those of the Laplace homotopy perturbation method (LHPM) as well as the q-homotopy analysis Sumudu transform method (q-HASTM), which revealed that the NTHAM is more reliable. The Caputo fractional derivative is employed. It not only gives initial conditions with obvious natural interpretation but is also bounded, meaning that there is no derivative of a constant. The results show that the proposed technique is superior in terms of simplicity, quality, accuracy, and stability and demonstrate the effectiveness of the rational technique under consideration.

1. Introduction

Recently, there have been important efforts to enhance mathematical models in order to study the outbreak of transmissible disease [1,2,3]. Researchers have obtained important data for distinct contagious viruses via analyses of stochastic and deterministic models. Kermack and McKendrick [4] suggested a model beneficial for implementing and enhancing knotted epidemic models, which have been considered major models in the aspect of epidemiology to date. In recent years, there have been numerous epidemiological models, such as SIR [5,6,7,8], SIS [9], SEIR [10,11], SIRC [12], and other models [13,14,15,16,17], which generally depend on compartments. Many effective methods for obtaining numerical and analytical solutions for epidemic mathematical models with fractional-order derivatives have recently been used, for example, the Adomian decomposition method [18,19], homotopy perturbation technique [20], modified Laplace decomposition algorithm [21,22,23], homotopy analysis method (HAM) [24,25,26], q-HAM [27,28], q-homotopy analysis transform method [29], natural transform (NT) method [30], fractional residual power series method [31], q-homotopy analysis Sumudu transform method (q-HASTM) [32], q-homotopy analysis transform method (q-HATM) [33,34], Laplace Adomian decomposition method [35], natural transform decomposition method [36], fractional exponential function method [37], and Laplace homotopy perturbation method (LHPM) [38].
In this paper, we investigate a significant fractional mathematical model using a novel smart technique called the natural transform homotopy analysis method (NTHAM). It has general solutions for the NT method and HAM. The generalization of the proposed method is revealed by studying the current model using other techniques, such as the LHPM, and comparing the results. Now, we recall some fundamental notions. The Riemann–Lowville fractional integral operator of order α of a function g ( t ) is defined by [39,40]:
I α g ( t ) = 1 Γ ( α ) 0 t ( t τ ) α 1 g ( τ ) d τ , ( α > 0 ) , I 0 g ( t ) = g ( t ) ,
where Γ is the gamma function, and α is an arbitrary but fixed base point. The integral is well-defined provided that g is a locally integrable function, and α is a complex number in the half-plane Re ( α ) > 0 . The dependence on the base point α is often suppressed and represents freedom in the constant of integration. For the Riemann-Lowville fractional integral, we have: I α t γ = Γ ( λ + 1 ) Γ ( α + λ + 1 ) t α + λ . The fractional derivative of g ( t ) in the Caputo sense is defined by [39,40]. D α g ( x ) = J n α D n g ( x ) = 1 Γ ( n α ) a x ( x t ) n α 1 g ( n ) ( t )   d t , ( α > 0 ) ; n 1 < α < n , n N , α > 0 , a , α , t R , for example, the Caputo derivative t n is
D α t n = { 0 , ( n α 1 ) , Γ ( n + 1 ) Γ ( n α + 1 ) t n α , ( n > α 1 ) . } .
The fractional Caputo–Fabrizio derivative of order α is defined in [41] as follows:
Let b > a ,   f H 1 ( a , b )   , and α ( 0 , 1 ) . The fractional Caputo–Fabrizio derivative of order α for a function f is defined by
C F D α f ( t ) =   M ( α ) ( 1 α ) a t exp ( α 1 α ( t s ) ) f ( s )   d s ,
where t 0 ,   M ( α ) , which is a normalization function that depends on α , and M ( 0 ) = M ( 1 ) = 1 .
If f H 1 ( a , b )   , and 0 < α < 1 , this derivative can be presented for f L 1 ( , b )   as C F D α f ( t ) = α   M ( α ) ( 1 α ) a t ( f ( t ) f ( s ) ) exp ( α 1 α ( t s ) ) d s .
The Mittag-Leffler function E α ( z ) with α > 0 is defined by the series representation, valid in the whole complex plane [42] E α ( z ) = k = 0 z k Γ ( α k + 1 ) . A generalization of the Mittag-Leffler function E α ( z ) = k = 0 z k Γ ( α k + 1 ) , α C ,   R ( α ) > 0 , was introduced by Wiman [43] in the general form:
E α , β ( z ) = k = 0 z k Γ ( α k + β ) ,   α ,   β C ,   R ( α ) > 0 , R ( α ) > 0 .
Local fractional calculus is a modern field of mathematics that deals with derivatives and integrals of functions defined on fractal sets. Local fractional calculus (also called fractal calculus) was first presented by Kolwankar and Gangal [44]. In fractal space, the Gao-Yang-Kang local derivative of g ( x ) of order α ,   0 < α 1 at x = x 0 , is defined as [45,46,47]:
D x α g ( x ) = g α ( x ) = d α g d x α | x = x 0 = lim x x 0 Δ α ( g ( x ) g ( x 0 ) ) ( x x 0 ) α ,
where Δ α ( g ( x ) g ( x 0 ) ) Γ ( Θ + 1 )   Δ   ( g ( x ) g ( x 0 ) ) .
LFD via the Caputo fractional derivative D α of order α of a function g ( x ) at point x = a is usually defined by the following equation [48]:
( D α g ) ( a ) = lim x a D a R L x α ( g ( x ) k = 0 n 1 g ( k ) ( a ) k ! ( x a ) k ) , n 1 < α n ,
where D a R L x α g ( x ) is the left side of the R-L fractional derivative of order α , which is defined by [49]:
D a R L x α g ( x ) = 1 Γ ( n α )   d n d x n a x g ( ζ ) ( x ζ ) α d ζ , n 1 < α n .
A time scale is an arbitrary nonempty closed subset of real numbers. We denote a time scale [50] by the symbol T. The time-scale fractal derivative or Hausdorff derivative on the time fractal is defined as   T t σ = lim x B x A T ( t B ) T ( t A ) ( t B ) σ ( t A ) σ , where σ is the fractal dimension of time. Another definition of the time-scale fractal derivative is introduced in [51,52,53,54,55]. There are significant roles for fractional differential equations (FDEs) in solving real-world problems [56,57,58]. This becomes obvious when using numerical approaches and comparing the relationships between various situations. Many studies have shown that using fractional-order derivatives produces better results in obtaining actual data for various models. The newly formulated Atangana–Baleanu derivative produces good results in many real-world problems. Fractional derivatives not only take into account the local characteristics of the dynamics but also consider the global evolution of the system; for that reason, when dealing with certain phenomena, they provide more accurate models of real-world behavior than standard derivatives. There are many applications of FDEs to different real-world problems, including chaotic ones, which have been reported in some fractional models.

2. Integral Transform Techniques

Integral transform techniques are frequently used for solving FDEs in various aspects of science. The major concepts of Laplace, Sumudu, and natural integral transforms are discussed using the following main concepts:
Definition 1.
The Laplace transform of a function g ( t ) ,   t ( 0 , ) is defined by [39]:
L [ f ( t ) ] ( s ) = F ( s ) = 0 f ( t )   e s t   d t ,   s C .
Definition 2.
The Laplace transform of the derivative of an integernof the function f ( t ) [39] is:
L [ D n f ( t ) ] = s n F ( s ) k = 0 n 1 s n k 1 f k ( 0 )
Definition 3.
The Laplace transform of the Caputo fractional derivative is defined by [39]:
L [ D α f ( t ) ] = s α F ( s ) k = 0 n 1 s α k 1 f k ( 0 ) , n 1 < α n
Definition 4.
In the early 1990s, Watugala [59] offered a new integral transform called the Sumudu transform, which has been applied to determine solutions of ODEs in control engineering problems. This Sumudu transform is defined over the set of functions:
A = { f ( t ) : M , τ 1 , τ 2 > 0 , | f ( t ) | < M e | t | / τ j ,   i f   t ( 1 ) j × [ 0 , ) }
The Sumudu transform of f ( t ) is:
G ( u ) = S [ f ( t ) ; u ] = 0 f ( u t ) e t d t ,   u ( τ 1 , , τ 2 ) .
Definition 5.
The Sumudu transform of the derivative of an integer n of the function f ( t ) [60,61,62] is:
S [ D t n f ( t ) ] = u n S [ f ( t ) ] k = 0 n 1 u α + k f ( k ) ( 0 + )
Definition 6.
The Sumudu transform of the Caputo fractional derivative is [60,61,62]:
S [ D t α f ( t ) ] = u α S [ f ( t ) ] k = 0 n 1 u α + k f ( k ) ( 0 + ) .
Definition 7.
The natural transform method was initially defined by Khan and Khan [63], who studied its properties and applications. The main concepts of the natural transform (NT) and its characteristics are presented in [63,64,65,66,67,68,69,70,71].
Assume that f ( t ) is a real function, f ( t ) > 0 and f ( t ) = 0 at t < 0 , section-wise continuous, of exponential order, and defined over the set of functions
A = { f ( t ) : M , τ 1 , τ 2 > 0 , | f ( t ) | < M e | t | / τ j ,   i f   t ( 1 ) j × [ 0 , ) } The natural transform of f ( t ) is defined by:
N [ f ( t ) ] = R ( s , u ) = 0 f ( u t ) e s t d t ,   u > 0 ,   s = 0
where N [ f ( t ) ] = R ( s , u ) is the natural transformation of the time function f ( t ) , and the variables u and s are the natural transform variables.
Definition 8.
Natural transform of n -derivative. If f n ( t ) is the n th derivative of function f ( t ) , then the natural transform of the n-derivative is given by:
N [ f n ( t ) ] = R n ( s , u ) = s n u n R ( s , u ) k = 0 n 1 s n ( k + 1 ) u n k f ( k ) ( 0 ) ,   n 1 .
Definition 9.
If N [ f ( t ) ] is the natural transform of a function, the natural transform of the fractional derivative of order α is defined as:
N [ f α ( t ) ] = s α u α R ( s , u ) k = 0 α 1 s α ( k + 1 ) u α k f ( k ) ( 0 ) .
Definition 10.
If R ( s , u ) is the natural transform and F ( s ) is the Laplace transform of function f ( t ) in A, then:
N [ f ( t ) ] = R ( s , u ) = 1 u 0 f ( t ) e s t u d t = 1 u F ( s u ) .
This is named the natural-Laplace duality (NLD).
Definition 11.
If R ( s , u ) is the natural transform and G ( u ) is the Sumudu transform of function f ( t ) in A, then:
N [ f ( t ) ] = R ( s , u ) = 1 s 0 f ( u t s ) e t d t = 1 s G ( u s )
This is called the natural-Sumudu duality (NSD).
By studying the relations between the Laplace, Sumudu, and natural transforms, we conclude that the NT is the general transform of both the ST and LT. At u = 1 in Equations (8) and (9), we have the LT in Equations (2) and (3), and at s = 1 in Equations (8) and (9), we have the ST in Equations (5) and (6). In sum, we can say that the LT, ST, and NT are symmetric to each other, as clarified in Equations (10) and (11).

3. Fractional Epidemic Model

Chen et al. [72] introduced a model and simulated data on transmission from the source of infection to the infection in people. In the present study, we assume that all parameters and variables involved in the model are non-negative in the individual community. The total population of individuals is considered N ( t ) , which is separated into five compartments: susceptible E ( t ) , exposed H ( t ) , symptomatic infected Y ( t ) , asymptomatic infected O ( t ) , and recovered populations F ( t ) . The following assumptions were made in the model:
  • The recruitment of individuals increases the size of the susceptible group at a constant rate Π .
  • The childbirth rate and natural mortality rate of individuals are indicated by parameters μ and δ , respectively.
  • A susceptible individual is infected over numerous contacts with infected individuals Y ( t ) via the given term β E ( t ) Y ( t ) N , where the contact rate β is the disease transmission coefficient.
  • Transmission from an asymptotic infected individual O ( t ) to a susceptible individual E ( t )   can take place in the form β E ( t ) Y ( t ) N , where ψ [ 0 , 1 ] is a transmissibility multiple of O ( t ) to Y ( t ) ; if ψ = 0 , no transmissibility multiple will exist and thus vanish, and if ψ = 1 , then a transmissibility multiple will exist.
  • The parameter ϕ is the proportion of asymptotic infections. The parameters θ and ϑ respectively indicate the transmission rate after the incubation period and joining classes Y ( t ) and O ( t ) .
  • Individuals in the symptomatic group Y ( t ) and asymptomatic group O ( t ) are removed at recovery rates of γ and τ and are added to the recovered F ( t ) compartment.
  • A susceptible individual will be infected after interaction with the reservoir or the seafood place or market class G ( t )   through the term given by η E ( t ) Y ( t ) N , where η is the disease transmission coefficient from E ( t )   to G ( t )   . Y ( t ) and O ( t ) individuals transmit the virus to the reservoir or the seafood place or market class G ( t )   at constant rates of σ and ε , respectively.
  • The removal rate of the virus from the reservoir or the seafood place or market class G ( t )   is indicated by k . Using the above assumptions, the mathematical representation of the model comprising the fractional-order dynamical system is [32,33]:
D t α E ( t )   = Π β E Y N   β ψ E O N η E G N δ   E   D t α H ( t ) = β E Y N + β ψ E O N + η E G N ( 1 ϕ )   θ   H ϕ   ϑ H δ   H   D t α Y ( t ) = ( 1 ϕ )   θ   H γ   Y δ   Y   D t α   O ( t ) = ϕ   ϑ   H a   O δ   O   D t α   F ( t ) = γ   Y + a   O δ   F   D t α G ( t ) = σ   Y + ε   O k   G , 0 < α 1
with the initial conditions
E ( 0 )   = E 0   ,   H ( 0 ) = H 0   ,   Y ( 0 ) = Y 0   ,   O ( 0 ) = O 0 , F ( 0 ) = 0 , G ( 0 ) = 0 .
The population compartments can be normalized by N by adopting the current state variables:
M = E N , Q = H N , R = Y N , S = O N , ϖ = F N , Ζ = G N , ξ = Π N .
The population is normalized and transformed into the non-dimensional form as follows:
D t α M   = ξ β   M   R   β   ψ   M   S η   M   Ζ δ   M D t α Q = β   M   R + β   ψ   M   S + η   M   Ζ ( 1 ϕ )   θ   Q ϕ   ϑ   Q δ   Q D t α R = ( 1 ϕ )   θ   Q γ   R δ   R D t α   S = ϕ   ϑ   Q a   S δ   S D t α   ϖ = γ   R + a   S δ   ϖ D t α Ζ = σ   R + ε   S k   Ζ 0 < α 1
with the following initial conditions:
M ( 0 ) = M o 0   , Q ( 0 ) = Q 0 0 ,   R ( 0 ) = R 0 0 , S ( 0 ) =   S 0 0 ,   ϖ ( 0 ) =   ϖ 0 0 ,   Ζ ( 0 ) =   Ζ 0 0 .
The fitted and estimated values of parameters and the initial conditions for the model with the fractional-order derivative are taken from Ref. [32].

4. Methodology of the Proposed Method

Consider the following nonlinear differential equation:
  Ψ + Ψ + Ψ = δ ( x ) ,
where is a linear differential operator, is the residual of the linear operator, is the nonlinear term, and δ ( x ) is the source term. Applying NT to both sides of Equation (17), we obtain:
N [   Ψ + Ψ + Ψ ] = N [ δ ( x ) ] .
After simplifying, we have
N [ Ψ ] u m s m η = 0 m 1 s m ( η + 1 ) u m η Ψ t ( η ) ( x , 0 ) + u m s m [ N [ Ψ ] + N [ Ψ ] N [ δ ( x ) ] ] = 0 ,
We define the nonlinear operator
[ Φ ( x , t ; q ) ] = N [ Φ ( x , t ; q ) ] u m s m η = 0 m 1 s m ( η + 1 ) u m η Φ t ( η ) ( x , 0 ; q ) + u m s m [ N [ Φ ( x , t ; q ) ] + N [ Φ ( x , t ; q ) ] N [ δ ( x ) ] ] + N [ Φ ( x , t ; q ) ] N [ δ ( x ) ] ] ,
where q [ 0 , 1 ] , and Φ ( x , t ; q ) is a real function of x , t and q .
We set a homotopy as follows:
( 1 q )   N   [ Φ ( x , t ; q ) Ψ 0 ( x , t ) ]   = q   ħ   H ( x , t )   [ Φ ( x , t ; q ) ] ,
where q [ 0 , 1 ] represents the embedding parameter, and ħ 0 is an auxiliary parameter. The role of the auxiliary parameter ħ is based on homotopy, a basic concept of topology. The nonzero auxiliary parameter is introduced to construct the so-called zero-order deformation equation, which gives a more general homotopy than the traditional one. N denotes the natural transform, Ψ 0 ( x , t ) is the initial guess of Ψ ( x , t ) , Φ   ( x , t ; q ) denotes an unknown function of x ,   t , and   H ( x , t )   is a nonzero auxiliary function. When the embedding parameters are q = 0 and q = 1 , it respectively holds that
Φ ( x , t ; 0 ) = Ψ 0 ( x , t ) , Φ ( x , t ; 1 ) = Ψ 1 ( x , t ) .
Thus, as q increases from 0 to 1 , the solution Φ   ( x , t ; q ) varies from the initial guess Ψ 0 ( x , t ) to the solution Φ ( x , t ; q ) . If we expand Φ ( x , t ; q ) in the Taylor series with respect to q , we have
Φ   ( x , t , q ) = Ψ 0 ( x , t ) + n = 1 Ψ n ( x , t )   q n     ,
where
Ψ n ( x , t ) = 1 n ! n Φ ( x , t , q ) q n | q = 0
If the auxiliary linear operator, initial guess, auxiliary parameter ħ , and auxiliary function are properly chosen, Series (24) converges at
Ψ ( x , t ) = Ψ 0 ( x , t ) + n = 1 Ψ n ( x , t ) .
The vectors are defined as follows:
Ψ n = { Ψ 0 ( x , t ) , Ψ 1 ( x , t ) , Ψ 2 ( x , t ) , , Ψ n ( x , t ) } .
Differentiating Equation (20) n times with respect to q , dividing by n ! , and setting q = 0 , we obtain the following n th-order deformation equation:
N [ Ψ n ( x , t ) x n   Ψ n 1 ( x , t ) ] = ħ   Ω n ( Ψ n 1 ) ,
where
Ω n ( Ψ n 1 ) = 1 n ! n 1   [ Φ ( x , t , q ) ] q n 1 | q = 0 ,   x n = { 0 ,   n 1 1 ,   n > 1
Applying the inverse natural transform, we have
Ψ n ( x , t ) = x n   Ψ n 1 ( x , t ) + ħ   N 1 [ Ω n ( Ψ n 1 ) ] , n = 1 , 2 , 3 ,

5. Solution of the Fractional Epidemiological Model (FEM) via NTHAM

Applying the NT of Equation (15), we obtain:
N [ M ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ M τ ( υ ) ( 0 ) u α s α N [ ξ β   M   R   β   ψ   M   S η   M   Ζ δ   M ] = 0 , N [ Q ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ Q τ ( υ ) ( 0 ) u α s α N [ β   M   R + β   ψ   M   S + η   M   Ζ , ( 1 ϕ )   θ   Q ϕ   ϑ   Q δ   Q ] = 0 N [ R ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ R τ ( υ ) ( 0 ) u α s α N [ ( 1 ϕ )   θ   Q γ   R δ   R ] = 0 ,
N [ S ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ S τ ( υ ) ( 0 ) u α s α N [ ϕ   ϑ   Q a   S δ   S ] = 0 N [ ϖ ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ ϖ τ ( υ ) ( 0 ) u α s α N [ γ   R + a   S δ   ϖ ] = 0 N [ Ζ ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ Ζ τ ( υ ) ( 0 ) u α s α N [ σ   R + ε   S k   Ζ   ] = 0 .
Now, we define the nonlinear operator as follows:
  [ Θ 1 ( t ; q ) ] = N [ Θ 1 ( t ; q )   ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ Θ 1 , t ( υ ) ( 0 ) u α s α N [ ξ β   Θ 1 ( t ; q )   Θ 3 ( t ; q )   β   ψ   Θ 1 ( t ; q )   Θ 4 ( t ; q ) η   Θ 1 ( t ; q )   Θ 6 ( t ; q ) δ   Θ 1 ( t ; q ) ]   [ Θ 2 ( t ; q ) ] = N [ Θ 2 ( t ; q ) ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ Θ 2 , t ( υ ) ( 0 ) u α s α N [ β   Θ 1 ( t ; q )   Θ 3 ( t ; q ) + β   ψ   Θ 1 ( t ; q )   Θ 4 ( t ; q ) + η   Θ 1 ( t ; q )   Θ 6 ( t ; q ) ( 1 ϕ )   θ   Θ 2 ( t ; q )   ϕ   ϑ   Θ 2 ( t ; q ) δ   Θ 2 ( t ; q ) ] ,
  [ Θ 3 ( t ; q ) ] = N [ Θ 3 ( t ; q ) ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ   Θ   3 , t ( υ ) ( 0 ) u α s α N [ ( 1 ϕ )   θ   Θ 2 ( t ; q ) γ   Θ 3 ( t ; q ) δ   Θ 3 ( t ; q ) ]   [ Θ 4 ( t ; q ) ] = N [ Θ 4 ( t ; q ) ] u α s α υ = 0 α 1 s υ ( υ + 1 ) u Λ υ   Θ 4 , t ( υ ) ( 0 ) u α s α N [ ϕ   ϑ   Θ 2 ( t ; q ) a   Θ 4 ( t ; q ) δ   Θ 4 ( t ; q ) ] ,
  [ Θ 5 ( t ; q ) ] = N [ Θ 5 ( t ; q ) ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ   Θ 5 , t ( υ ) ( 0 ) u α s α N [ γ   Θ 3 ( t ; q ) + a   Θ 4 ( t ; q ) δ   Θ 5 ( t ; q ) ] ,
  [ Θ 6 ( t ; q ) ] = N [ Θ 6 ( t ; q ) ] u α s α υ = 0 α 1 s α ( υ + 1 ) u α υ Θ 6 , t ( υ ) ( 0 ) u α s α N [ σ   Θ 3 ( t ; q ) + ε   Θ 5 ( t ; q ) k   Θ 6 ( t ; q ) ] .
Thus,
n   [ M n 1 ] = N [ M n 1 ] ( 1 x n ) 1 s M 0 u α s α N [ ξ β   [ r = 0 n 1 M r R n r 1 ]   β   ψ   [ r = 0 n 1 M r S n r 1 ] η   [ r = 0 n 1 M r Ζ n r 1 ] δ   r = 0 n 1 M r ] n   [ Q n 1 ] = N [ Q n 1 ] ( 1 x n ) 1 s Q 0 u α s α N [ β   [ r = 0 n 1 M r R n r 1 ]   + β   ψ   [ r = 0 n 1 M r S n r 1 ] + η   [ r = 0 n 1 M r Ζ n r 1 ] ( 1 ϕ )   θ r = 0 n 1 Q r   ϕ   ϑ   r = 0 n 1 Q r δ   r = 0 n 1 Q r   ] ,
n [ R n 1 ] = N [ R n 1 ] ( 1 x n ) 1 s R 0 u α s α N [ ( 1 ϕ )   θ r = 0 n 1 Q r   γ   r = 0 n 1 R r δ   r = 0 n 1 R r ] n [ S n 1 ] = N [ S n 1 ] ( 1 x n ) 1 s S 0 u α s α N [ ϕ   ϑ   r = 0 n 1 Q r   a   r = 0 n 1 S r δ   r = 0 n 1 S r ] n   [ ϖ n 1 ] = N [ ϖ n 1 ] ( 1 x n ) 1 s ϖ 0 u α s α N [ γ   r = 0 n 1 R r + a   r = 0 n 1 S r   δ   r = 0 n 1 ϖ r ] n   [ Ζ n 1 ] = N [ Ζ n 1 ] ( 1 x n ) 1 s Ζ 0 u α s α N [ σ   r = 0 n 1 R r + ε r = 0 n 1 ϖ r   k   r = 0 n 1 Ζ r ]
Applying the inverse NT and using Relation (29), we have
M n ( t ) = x n M n 1 + ħ N 1 [ n [ M n 1 ] ] , Q n ( t ) = x n Q n 1 + ħ N 1 [ n [ Q n 1 ] ] R n ( t ) = x n R n 1 + ħ N 1 [ n [ R n 1 ] ] ,   S n ( t ) = x n S n 1 + ħ N 1 [ n [ S n 1 ] ] ϖ n ( t ) = x n ϖ n 1 + ħ N 1 [ n   [ ϖ n 1 ] ] ,   Ζ n ( t ) = x n Ζ n 1 + ħ N 1 [ n   [ Ζ n 1 ] ]
i.e.,
M 1   ( t ) = x 1 M 0 + ħ N 1 [ 1 [ M 0 ] ] = x 1 M 0 + ħ   N 1 [ 1 s M 0 ( 1 x 1 ) 1 s M 0 u α s α N [ ξ β   M 0   R 0   β   ψ   M 0   S 0   η   M 0 Ζ 0 δ   M 0 ] ] Q 1 ( t ) = x 1 Q 0 + ħ N 1 [ 1   [ Q 0 ] ] = x 1 Q 0 + ħ N 1 [ 1 s Q 0 ( 1 x 1 ) 1 s Q 0 u α s α N [ β   M 0   R 0   + β   ψ   M 0   S 0 + η   M 0 Ζ 0   ( 1 ϕ )   θ   Q 0   ϕ   ϑ   Q 0 δ   Q 0   ] R 1 ( t ) = x 1 R 0 + ħ   N 1 [ 1 [ R 0 ] ] = x 1 R 0 + ħ N 1 [ 1 s R 0 ( 1 x 1 ) 1 s R 0 u α s α N [ ( 1 ϕ )   θ   Q 0 γ   R 0 δ   R 0 ] ]
S 1 ( t ) = x 1   S 0 + ħ N 1 [ 1 [ S 0 ] ] = x 1 S 0 + ħ N 1 [ 1 s S 0 ( 1 x 1 ) 1 s S 0 u α s α N [ ϕ   ϑ   Q 0   a   S 0 δ   S 0 ] ] ϖ 1 ( t ) = x 1 ϖ 0 + ħ N 1 [ n   [ ϖ 0 ] ] = x 1 ϖ 0 + ħ N 1 [ 1 s ϖ 0 ( 1 x 1 ) 1 s ϖ 0 u α s α N [ γ   R 0 + a   S 0 δ   ϖ 0 ] ] Ζ 1 ( t ) = x 0   Ζ 0 + ħ N 1 [ 1   [ Ζ 0 ] ] = x 1 Ζ 0 + ħ N 1 [ 1 s Ζ 0 ( 1 x 1 ) 1 s Ζ 0 u α s α N [ σ   R 0 + ε   ϖ 0 k   Ζ 0 ] .
Thus,
M 1 ( t ) =   ħ N 1 [ u α s α N [ ξ β   M 0   R 0   β   ψ   M 0   S 0   η   M 0 Ζ 0 δ   M 0 ] ] Q 1 ( t ) =   ħ N 1 [ u α s α N [ β   M 0   R 0   + β   ψ   M 0   S 0 + η   M 0 Ζ 0   ( 1 ϕ )   θ   Q 0   ϕ   ϑ   Q 0 δ   Q 0   ] R 1 ( t ) = ħ N 1 [ u α s α N [ ( 1 ϕ )   θ   Q 0 γ   R 0 δ   R 0 ] ] S 1 ( t ) = ħ N 1 [ u α s α N [ ϕ   ϑ   Q 0   a   S 0 δ   S 0 ] ] ϖ 1 ( t ) = ħ N 1 [ u α s α N [ γ   R 0 + a   S 0 δ   ϖ 0 ] ] Ζ 1 ( t ) = ħ N 1 [ u α s α N [ σ   R 0 + ε   ϖ 0 k   Ζ 0 ] ] .
Setting n = 2 in Equation (38), we obtain
M 2 = x 2 M 1 + ħ N 1 [ 2   [ M 1 ] ] , Q 2 = x 2 Q 1 + ħ   N 1 [ 2   [ Q 1 ] ] R 2 = x 2 R 1 + ħ N 1 [ 2 [ R 1 ] ] , S 2 = x 2 S 1 + ħ N 1 [ 2 [ S 1 ] ] ϖ 2 = x 2 ϖ 1 + ħ N 1 [ 2   [ ϖ 1 ] ] , Z 2 = x 2 Z 1 + ħ N 1 [ 2   [ Ζ 1 ] ] .
i.e.,
M 2 = x 2 M 1 + ħ N 1 [ N [ M 1 ] ( 1 x 2 ) 1 s M 0 u α s α N [ ξ β   [ r = 0 n M r R n r 1 ]   β   ψ   [ r = 0 n 1 M r S n r 1 ] η   [ r = 0 n M r Ζ n r 1 ] δ   r = 0 n M r ] ] Q 2 = x 2 Q 1 + ħ N 1 [ N [ Q 1 ] ( 1 x 2 ) 1 s Q 0 u α s α N [ β   [ r = 0 n M r R n r 1 ]   + β   ψ   [ r = 0 n M r S 1 r ] + η   [ r = 0 n M r Ζ n r 1 ] ( 1 ϕ )   θ r = 0 n Q r   ϕ   ϑ   r = 0 n Q r δ   r = 0 n Q r   ] ] R 2 = x 2 R 1 + ħ N 1 [ [ N [ R 1 ] ( 1 x 2 ) 1 s R 0 u α s α N [ ( 1 ϕ )   θ r = 0 n Q r   γ   r = 0 n R r δ   r = 0 n R r ] ] S 2 = x 2 S 1 + ħ N 1 [ N [ S 1 ] ( 1 x 2 ) 1 s S 0 u α s α N [ ϕ   ϑ   r = 0 n Q r   a   r = 0 n S r δ   r = 0 n S r ] ] ] ϖ 2 = x 2 ϖ 1 + ħ N 1 [ N [ ϖ 1 ] ( 1 x 2 ) 1 s ϖ 0 u α s α N [ γ   r = 0 n R r + a   r = 0 n S r   δ   r = 0 n ϖ r ] ] Z 2 = x 2 Z 1 + ħ N 1 [ N [ Ζ 1 ] ( 1 x 2 ) 1 s Ζ 0 u α s α N [ σ   r = 0 n R r + ε r = 0 n ϖ r   k   r = 0 n Ζ r ] ] .
After simplifying, we obtain
M 2 = M 1 ( 1 + ħ ) ħ t α Γ ( α + 1 ) ξ + ħ 1 ,   Q 2 = Q 1 ( 1 + ħ ) ħ 2 R 2 = R 1 ( 1 + ħ ) ħ 3 ,   S 2 = S 1 ( 1 + ħ ) ħ 4 ϖ 2 = ϖ 1 ( 1 + ħ ) ħ 5 ,   Z 2 = Z 1 ( 1 + ħ ) ħ 6 ,
where
1 = N 1 [ u α s α N [ β   [ r = 0 n M r R n r 1 ] +   β   ψ   [ r = 0 n 1 M r S n r 1 ] + η   [ r = 0 n M r Ζ n r 1 ] + δ   r = 0 n M r ] ] 2 = N 1 [ u α s α N [ β   [ r = 0 n M r R n r 1 ]   + β   ψ   [ r = 0 n M r S 1 r ] + η   [ r = 0 n M r Ζ n r 1 ]   ( 1 ϕ )   θ r = 0 n Q r   ϕ   ϑ   r = 0 n Q r δ   r = 0 n Q r   ] ] 3 = N 1 [ u α s α N [ ( 1 ϕ )   θ r = 0 n Q r   γ   r = 0 n R r δ   r = 0 n R r ] ] 4 = N 1 [ u α s α N [ ϕ   ϑ   r = 0 n Q r   a   r = 0 n S r δ   r = 0 n S r ] ] ] 5 = N 1 [ u α s α N [ γ   r = 0 n R r + a   r = 0 n S r   δ   r = 0 n ϖ r ] ] 6 = N 1 [ u α s α N [ σ   r = 0 n R r + ε r = 0 n ϖ r   k   r = 0 n Ζ r ] ] .
Then, we can write the solution of the epidemic model in series form as follows:
M ( t ) = M 0 + M 1 + M 2 + , Q ( t ) = Q 0 + Q 1 + Q 2 + R ( t ) = R 0 + R 1 + R 2 + , S ( t ) = S 0 + S 1 + S 2 + ϖ ( t ) = ϖ 0 + ϖ 1 + ϖ 2 + , Ζ ( t ) = Ζ 0 + Ζ 1 + Ζ 2 +
Then, for n = 1, we have
M   ( t ) =   M 0 ( 2 + ħ ) ( ħ t α Γ ( α + 1 ) [ ξ β   M 0   R 0   β   ψ   M 0   S 0   η   M 0 Ζ 0 δ   M 0 ] ) ħ t α Γ ( α + 1 ) ξ + ħ 11 Q ( t ) = Q 0 ( 2 + ħ ) ( ħ t α Γ ( α + 1 ) [ β   M 0   R 0   + β   ψ   M 0   S 0 + η   M 0 Ζ 0   ( 1 ϕ )   θ   Q 0   ϕ   ϑ   Q 0 δ   Q 0   ] ) ħ 22 R ( t ) = R 0 ( 2 + ħ ) ( ħ t α Γ ( α + 1 ) [ ( 1 ϕ )   θ   Q 0 γ   R 0 δ   R 0 ] ) ħ 33 S ( t ) = S 0 ( 2 + ħ ) ( ħ t α Γ ( α + 1 ) [ ϕ   ϑ   Q 0   a   S 0 δ   S 0 ] ) ħ 44 ϖ ( t ) = ϖ 0 ( 2 + ħ ) ( ħ t α Γ ( α + 1 ) [ γ   R 0 + a   S 0 δ   ϖ 0 ] ) ħ 55 Ζ ( t ) = Z 0 ( 2 + ħ ) ( ħ t α Γ ( α + 1 ) [ σ   R 0 + ε   ϖ 0 k   Ζ 0 ] ) ħ 66 ,
11   = t 2 α Γ ( 2 α + 1 ) [ β ( M 1 R 0 + M 0 R 1 ) +   β   ψ   ( M 0 S 1 + M 1 S 0 ) + η   ( M 0 Ζ 1 + M 1 Ζ 0 ) ] 22 = t 2 α Γ ( 2 α + 1 ) [ β ( M 1 R 0 + M 0 R 1 ) + β   ψ ( M 0 S 1 + M 1 S 0 ) + η   ( M 1 Ζ 0 + M 0 Ζ 1 ) ( 1 ϕ )   θ   Q 1 ϕ   ϑ   Q 1 ( δ   Q 1 ) ] 33 = t 2 α Γ ( 2 α + 1 ) [ ( 1 ϕ )   θ   Q 1 γ   R 1 δ   R 1 ] 44 = t 2 α Γ ( 2 α + 1 ) [ ϕ   ϑ   Q 1   t   S 1 δ   S 1 ] 55 = t 2 α Γ ( 2 α + 1 ) [ γ   R 1 + t   S 1 δ   ϖ 1 ] 66 = t 2 α Γ ( 2 α + 1 ) [ σ   R 1 + ε   ϖ 1 k   Ζ 1 ] .
It is obvious that the solution of FEM depends on the value of the auxiliary parameter ħ . This gives us a family of solution expressions in the auxiliary parameter ħ , even if a nonlinear problem has a unique solution [24]. The convergence region and rate of each solution expression among the family can be evaluated via the auxiliary parameter ħ . By means of so-called ħ -curves, it is easy to deduce the so-called valid regions of ħ to obtain a convergent solution series. The HAM uses a specific auxiliary parameter ħ = 1 to control the region of convergence. Thus, setting ħ = 1 and n = 1 produces excellent agreement with the convergent solution series.
M ( t ) =   M 0 + t α Γ ( α + 1 ) [ 2 ξ β   M 0   R 0   β   ψ   M 0   S 0   η   M 0 Ζ 0 δ   M 0 ]   t 2 α Γ ( 2 α + 1 ) [ β ( M 0 R 1 + M 1 R 0 ) + β   ψ ( M 0 S 1 + M 1 S 0 ) + η ( M 0 Z 1 + M 1 Z 0 ) ] Q ( t ) = Q 0 + t α Γ ( α + 1 ) [ β   M 0   R 0   + β   ψ   M 0   S 0 + η   M 0 Ζ 0   ( 1 ϕ )   θ   Q 0   ϕ   ϑ   Q 0 δ   Q 0   ] t 2 α Γ ( 2 α + 1 ) [ β ( M 0 R 1 + M 1 R 0 ) + β ψ ( M 0 S 1 + M 1 S 0 ) + η ( M 0 Z 1 + M 1 Z 0 ) ( 1 ϕ ) θ   Q 1 ϕ   ϑ   Q 1 δ   Q 1 ]
R ( t ) = R 0 + t α Γ ( α + 1 ) [ ( 1 ϕ )   θ   Q 0 γ   R 0 δ   R 0 ] t 2 α Γ ( 2 α + 1 ) [ ( 1 ϕ )   θ   Q 1 γ   R 1 δ   R 1 ] , S ( t ) = S 0 + t α Γ ( α + 1 ) [ ϕ   ϑ   Q 0   a   S 0 δ   S 0 ] t 2 α Γ ( 2 α + 1 ) [ ϕ ϑ   Q 1 a   S 1 δ   S 1 ] , ϖ ( t ) = ϖ 0 + t α Γ ( α + 1 ) [ γ   R 0 + a   S 0 δ   ϖ 0 ] t 2 α Γ ( 2 α + 1 ) [ γ   R 1 + a   S 1 δ   ϖ 1 ] , Ζ ( t ) = Z 0 + t α Γ ( α + 1 ) [ σ   R 0 + ε   ϖ 0 k   Ζ 0 ] t 2 α Γ ( 2 α + 1 ) [ σ   R 1 + ε ϖ 1 k   Z 1 ] .
Using the initial conditions in [32], it follows that
M ( t ) =   0.6 0.0905700   t α Γ ( α + 1 ) 0.0204752 t 2 α Γ ( 2 α + 1 ) Q ( t ) = 0.25 0.07802 t α Γ ( α + 1 )   + 0.00979208 t 2 α Γ ( 2 α + 1 ) +
R ( t ) = 0.2 0.015786 t α Γ ( α + 1 ) 0.009842472 t 2 α Γ ( 2 α + 1 ) + S ( t ) = 0.05 0.100974   t α Γ ( α + 1 ) + 0.00197334   t 2 α Γ ( 2 α + 1 ) + ϖ ( t ) = 0.02 + 0.035102   t α Γ ( α + 1 ) 0.00847892   t 2 α Γ ( 2 α + 1 ) + Ζ ( t ) = 0.01 + 0.02090000   t α Γ ( α + 1 ) 0.00003216   t 2 α Γ ( 2 α + 1 ) +

6. Solution via LHPM

In order to demonstrate the generalization of the NTHAM, we solve the suggested model using other techniques, such as the LHPM [38], and discuss the outcomes. Applying the Laplace transform to both sides of Equation (15), we obtain
L [ D t α M ]   = L [ ξ β   M   R   β   ψ   M   S η   M   Ζ δ   M ] , L [ D t α Q ] = L [ β   M   R + β   ψ   M   S + η   M   Ζ ( 1 ϕ )   θ   Q ϕ   ϑ   Q δ   Q ] , L [ D t α R ] = L [ ( 1 ϕ )   θ   Q γ   R δ   R ] , L [ D t α   S ] = L [ ϕ   ϑ   Q a   S δ   S ] , L [ D t α   ϖ ] = L [ γ   R + a   S δ   ϖ ] , L [ D t α Ζ ] = L [ σ   R + ε   S k   Ζ ]   . 0 < α 1
By simplifying, we obtain
L [ M ] 1 s M 0 s α L [ ξ β   M   R   β   ψ   M   S η   M   Ζ δ   M ] = 0 , L [ Q ] 1 s Q 0 s α L [ β   M   R + β   ψ   M   S + η   M   Ζ ( 1 ϕ )   θ   Q ϕ   ϑ   Q δ   Q ] = 0 L [ R ] 1 s R 0 s α L [ ( 1 ϕ )   θ   Q γ   R δ   R ] = 0 , L [ S ] 1 s S 0 s α L [ ϕ   ϑ   Q a   S δ   S ] = 0 , L [ ϖ ] 1 s ϖ 0 s α υ = 0 n 1 s α υ 1 ϖ τ ( υ ) ( 0 ) s α L [ γ   R + a   S δ   ϖ ] = 0 , L [ Ζ ] 1 s Z 0 s α υ = 0 n 1 s α υ 1 Ζ τ ( υ ) ( 0 ) s α L [ σ   R + ε   S k   Ζ   ] = 0 .
Applying the inverse Laplace transform on both sides of Equation (54), we obtain:
M ( t ) = M 0 + s α L [ ξ β   M   R   β   ψ   M   S η   M   Ζ δ   M ] , Q ( t ) = Q 0 + s α L [ β   M   R + β   ψ   M   S + η   M   Ζ ( 1 ϕ )   θ   Q ϕ   ϑ   Q δ   Q ] , R ( t ) = R 0 + s α L [ ( 1 ϕ )   θ   Q γ   R δ   R ] , S ( t ) = S 0 + s α L [ ϕ   ϑ   Q a   S δ   S ] , ϖ ( t ) = ϖ 0 + s α L [ γ   R + a   S δ   ϖ ] , Ζ ( t ) = Z 0 + s α L [ σ   R + ε   S k   Ζ   ] .
Now, applying the classical homotopy perturbation technique, the solution can be expressed as a power series in p , as given below.
g ( x , t ) = n = 0 p n g n ( x , t ) ,
where p is considered a small parameter, p [ 0 , 1 ] . We can decompose the nonlinear term as:
F g ( x , t ) = n = 0 p n H n ( g ) ,
where H n is a He’s polynomial of g 0 ( x , t ) , g 1 ( x , t ) , g 2 ( x , t ) , , g n ( x , t ) , and it can be calculated by the following formula.
H n ( g 0 ( x , t ) , g 1 ( x , t ) , g 2 ( x , t ) , , g n ( x , t ) ) = 1 n ! n p n [ F ( i = 0 p i g i ) ] p = 0   , n = 0 , 1 , 2 ,
Substitution of (56) and (57) into (58) yields:
n = 0 p n M n   ( t ) = M 0 + L 1 [ s α L [ ξ β   M   R   β   ψ   M   S η   M   Ζ δ   M ] ] n = 0 p n   Q n ( t ) = Q 0 + L 1 [ s α L [ β   M   R + β   ψ   M   S + η   M   Ζ ( 1 ϕ )   θ   Q ϕ   ϑ   Q δ   Q ] ] n = 0 p n   R n ( t ) = R 0 + L 1 [ s α L [ ( 1 ϕ )   θ   Q γ   R δ   R ] ] n = 0 p n   S n ( t ) = S 0 + L 1 [ s α L [ ϕ   ϑ   Q a   S δ   S ] ] n = 0 p n   ϖ n ( t ) = ω 0 + L 1 [ s α L [ γ   R + a   S δ   ϖ ] ] n = 0 p   n   Ζ n ( t ) = Z 0 + L 1 [ s α L [ σ   R + ε   S k   Ζ   ] ]
By equating the coefficients of the corresponding power of p on both sides of Equation (59), the following approximations are obtained:
p 0 : M 0 = M ( 0 ) ,   p 0 : Q 0 = Q ( 0 ) , P 0 : R 0 = R ( 0 ) ,   p 0 : S n = S ( 0 ) , p 0 : ϖ 0 = ϖ ( 0 ) ,   p 0 : Z 0 = Z ( 0 )   ,
and
p : M 1   = L 1 [ 1 s α L [ ξ β   M 0   R 0   β   ψ   M 0   S 0 η   M 0   Ζ 0 δ   M 0 ] ] p : Q 1 = L 1 [ 1 s α L [ β   M 0   R 0 + β   ψ   M 0   S 0 + η   M 0   Ζ 0 ( 1 ϕ )   θ   Q ϕ   ϑ   Q 0 δ   Q 0 ] ] p : R 1 = L 1 [ 1 s α L [ ( 1 ϕ )   θ   Q 0 γ   R 0 δ   R 0 ] ] p : S 1 = L 1 [ 1 s α L [ ϕ   ϑ   Q 0 a   S 0 δ   S 0 ] ] ,
p : ϖ 1 = L 1 [ 1 s α L [ γ   R 0 + a   S 0 δ   ϖ 0 ] ] p :   Ζ 1 = L 1 [ 1 s α L [ σ   R 0 + ε   S 0 k   Ζ 0   ] ] .
Moreover,
p 2 : M 2   = L 1 [ 1 s α L [ ξ β   ( M 0   R 1 + M 1 R 0 )   β   ψ   ( M 0 S 1 + M 1   S 0 ) η   ( M 0 Z 1 + M 1   Ζ 0 ) δ   M 1 ] ] p : Q 2 = L 1 [ 1 s α L [ β   ( M 0 R 1 + M 1   R 0 ) + β   ψ (   M 0 S 1 + M 1   S 0 ) + η   ( M 0   Z 1 + M 1 Ζ 0 ) ( 1 ϕ )   θ   Q 1 ϕ   ϑ   Q 1 δ   Q 1 ] ] p 2 : R 2 = L 1 [ 1 s α L [ ( 1 ϕ )   θ   Q 1 γ   R 1 δ   R 1 ] ] p 2 : S 2 = L 1 [ 1 s α L [ ϕ   ϑ   Q 1 a   S 1 δ   S 1 ] ] p 2 : ϖ 2 = L 1 [ 1 s α L [ γ   R 1 + a   S 1 δ   ϖ 1 ] ] p 2 :   Ζ 2 = L 1 [ 1 s α L [ σ   R 1 + ε   S 1 k   Ζ 1   ] ] .
Then,
M 2   = t α Γ ( α + 1 ) ξ t 2 α Γ ( 2 α + 1 ) [ β   ( M 0   R 1 + M 1 R 0 ) +   β   ψ   ( M 0 S 1 + M 1   S 0 ) + η   ( M 0 Z 1 + M 1   Ζ 0 ) + δ   M 1 ] Q 2 = t 2 α Γ ( 2 α + 1 ) [ β   ( M 0 R 1 + M 1   R 0 ) + β   ψ (   M 0 S 1 + M 1   S 0 ) + η   ( M 0   Z 1 + M 1 Ζ 0 ) ( 1 ϕ )   θ   Q 1 ϕ   ϑ   Q 1 δ   Q 1 ] R 2 = t 2 α Γ ( 2 α + 1 ) [ ( 1 ϕ )   θ   Q 1 γ   R 1 δ   R 1 ] S 2 = t 2 α Γ ( 2 α + 1 ) [ ϕ   ϑ   Q 1 a   S 1 δ   S 1 ] ϖ 2 = t 2 α Γ ( 2 α + 1 ) [ γ   R 1 + a   S 1 δ   ϖ 1 ]   Ζ 2 = t 2 α Γ ( 2 α + 1 ) [ σ   R 1 + ε   S 1 k   Ζ 1   ] .
Proceeding in the same manner, the rest of the components g n ( x , t ) can be completely obtained, and the series solution is thus entirely determined. The approximate solution g ( x , t ) is obtained via Equations (46)–(52). This is the same solution obtained via NTHAM and similar to the solution in [32,33] (see Figure 1 and Figure 2).

7. Discussion

This research proposes a new technique called NTHAM for appropriately obtaining novel fractional solutions for the fractional epidemic model (15) based on a mixture of the NT method and HAM. The Mathematica program was used to conduct the calculations. Figure 1 shows various fractional values of M ( t ) , Q ( t ) , R ( t ) , S ( t ) , ϖ ( t ) , Z ( t ) using initial conditions in [32], and the result is identical to the solution in Ref. [32]. Figure 2 shows all compartments for various fractional orders that correspond to the integer-order solution. Figure 1 and Figure 2 show a comparison of the current solution with fractional solutions produced by q-HASTM [32] and LHPM [38]. In Equations (8) and (9) at u = 1, we have the LT as in Equations (2) and (3). In addition, at s = 1 in Equations (8) and (9), we have the ST as in Equations (5) and (6). Setting u = 1 in (30) and (31) leads to the solution via the LTHPM in Equation (59) [32]. Additionally, at S = 1, we have the solution reported in the literature via STHAM [33]. It is obvious that the proposed technique in this paper is a generalization of the LT and ST. On the other hand, at alpha = 1, the present solution is the same as the standard solution obtained by Yadav et al. [32]. The NTHAM is characterized by simplicity in producers, does not require strenuous efforts for calculations, and produces high-quality solutions comparable to other techniques.

8. Conclusions

Generic solutions of the FSIRD model are provided by the present technique. It is a combination of the NTM and the HAM. The NTM is considered a generalization of the LTM and STM. Compared with perturbation techniques and non-perturbation methods such as Lyapunov’s artificial small parameter method, the δ-expansion method, and the homotopy perturbation method, the homotopy analysis method has some or all of the following advantages. Firstly, unlike all other analytic techniques, the homotopy analysis method allows substantial freedom to obtain explicit solutions of a given nonlinear problem by means of various base functions. Therefore, we can approximate a nonlinear problem more efficiently by choosing a common group of basic functions. This is because the convergence region and rate of a series are chiefly evaluated via the basic functions used to obtain the explicit solution. The HAM provides us with a family of solution expressions in the auxiliary parameter ħ , even if a nonlinear problem has a unique solution. The convergence region and rate of each solution expression among the family might be limited by the auxiliary parameter ħ . Thus, the auxiliary parameter gives us an additional way to conveniently adjust and control the convergence region and rate of the solution series. By means of so-called ħ -curves, it is easy to find the so-called actual regions of ħ to obtain a convergent solution series. Unlike perturbation techniques, the HAM is independent of any small or large quantities. Furthermore, the proposed technique can be applied to a variety of scientific fields. In the future, we will employ the NTHAM to solve FDES in various aspects of science.

Author Contributions

Formal analysis, H.R.A.-R., M.Z. and G.M.I.; data curation, H.R.A.-R., M.Z. and G.M.I.; writing—original draft preparation, H.R.A.-R., M.Z. and G.M.I.; writing—review and editing, H.R.A.-R., M.Z. and G.M.I.; funding acquisition, H.R.A.-R., M.Z. and G.M.I. All authors have read and agreed to the published version of the manuscript.

Funding

This research is funded by King Khalid University, grant number R.G.P.2/207/43.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

M. Zayed and G.M. Ismail extend their appreciation to the Deanship of Scientific 142 Research at King Khalid University, Saudi Arabia, for funding this work through the research group 143 program under grant R.G.P.2/207/43.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Plots of (a) M ( t ) , (b) Q ( t ) , (c) R ( t ) , (d) S ( t ) , (e) ϖ ( t ) , (f) Ζ ( t ) using specified initial conditions for various fractional values. The result is identical to the solution in [28,38].
Figure 1. Plots of (a) M ( t ) , (b) Q ( t ) , (c) R ( t ) , (d) S ( t ) , (e) ϖ ( t ) , (f) Ζ ( t ) using specified initial conditions for various fractional values. The result is identical to the solution in [28,38].
Symmetry 14 01695 g001aSymmetry 14 01695 g001b
Figure 2. Plots of all four compartments for various fractional orders, (a) 0.8, (b) 0.9, and (c) 1, corresponding to the integer-order solution.
Figure 2. Plots of all four compartments for various fractional orders, (a) 0.8, (b) 0.9, and (c) 1, corresponding to the integer-order solution.
Symmetry 14 01695 g002
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Abdl-Rahim, H.R.; Zayed, M.; Ismail, G.M. Analytical Study of Fractional Epidemic Model via Natural Transform Homotopy Analysis Method. Symmetry 2022, 14, 1695. https://doi.org/10.3390/sym14081695

AMA Style

Abdl-Rahim HR, Zayed M, Ismail GM. Analytical Study of Fractional Epidemic Model via Natural Transform Homotopy Analysis Method. Symmetry. 2022; 14(8):1695. https://doi.org/10.3390/sym14081695

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Abdl-Rahim, Hamdy R., Mohra Zayed, and Gamal M. Ismail. 2022. "Analytical Study of Fractional Epidemic Model via Natural Transform Homotopy Analysis Method" Symmetry 14, no. 8: 1695. https://doi.org/10.3390/sym14081695

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