EUROPEAN JOURNAL OF PURE AND APPLIED MATHEMATICS 2025, Vol. 18, Issue 4, Article Number 6693 ISSN 1307-5543 – ejpam.com Published by New York Business Global Numerical Solutions of the SIR Mathematical Model of Computer Viruses Involving Non-linear Fractional Order Differential Equation Rajratana M. Kamble1,∗, Pramod R. Kulkarni2 1 Shri Vitthal Rukmini Arts, Commerce and Science College, Sawana, Tq. Mahagoan, Dist. Yavatmal, Maharashtra, India 2 N.E.S Science College, Nanded, Maharashtra, India Abstract. In this paper, the non-linear Fractional order susceptible-infected-Recovered(SIR) math- ematical model of computer viruses is presented. For this Fractional differential transform method (FDTM) and the Laplace-Adomian decomposition method (LADM) are applied and compared the obtained results with Runge-Kutta Felhberg Method for γ = 1. Also, graphs of solutions are plotted up to five iterations from both the method. The fractional derivative used in the model is Caputo Fractional derivative. Using Lyapunov stability analysis,the stability verified of the given mathematical model. Solutions are obtained for three different fractional order values of γ. The validity of the result is confirmed by converting model into integer order. Errors from both the methods are compared. 2020 Mathematics Subject Classifications: 34A08 Key Words and Phrases: Caputo fractional derivative, fractional differential transform method, Laplace Adomian decomposition method, Lyapunov stability, Runge-Kutta Felhberg method 1. Introduction Computer viruses are harmful programs for normal functioning of computers. There are various types of computer viruses that attack computers. Different types of mathemat- ical models representing spread of computer viruses have been proposed in the literature[1] [1],[2],[3],[4],[5],[6],[7],[8],[9],[10],[11],[12],[13],[14],[15],[16][17]. These models can be solved using mathematical techniques such as the Differential Transform Method, Collection Method [13], Homotopy Analysis Method [2],[15] Variational Iterational Method[18], and others[7],[16]. Various mathematical and engineering problems are solved using semi- analytical techniques [14],[19],[20],[21],[15],[22],[23],[24],[25]. The Differntial Transform Method and Laplace Adomian Decomposition Method are the tools to solve linear and non- linear preoblems in engineering, physics, mathematics, etc [25],[26],[27],[28],[29],[30],[31] ∗Corresponding author. DOI: https://doi.org/10.29020/nybg.ejpam.v18i4.6693 Email addresses: kamblerajratna2@gmail.com (R. M. Kamble), pramodrkul@gmail.com (P. R. Kulkarni) https://www.ejpam.com 1 Copyright: © 2025 The Author(s). (CC BY-NC 4.0) R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 2 of 40 ,[32],[33],[34],[35],[36],[37],[38],[39],[40],[41],[42],[43],[44],[45],[46] In this paper, we have designed and solved the non-linear fractional order system of the Susceptible-Infected-Recovered (SIR) mathematical model of computer viruses. For this purpose, the Fractional Differential Transform Method (FDTM) and Laplace Adomian Decomposition Method (LADM) is applied. The approximate solutions are estimated for different iterations (up to five iterations), and the results are compared with those ob- tained by 4/5 Runge-Kutta Frlhberg Algorithm (RKFA). The graphs of the approximate solutions up to five iterations and the absolute errors are plotted at different values of γ and t, illustrating the evolution of the system. Comparing the solutions and errors ob- tained by FDTM and LADM with RKFA, we have concluded that as compared to the LADM, the FDTM gives more accurate results under certain conditions. The methods and results presented in this chapter on the non-linear fractional order system for modeling computer virus propagation through the Susceptible-Infected-Recovered (SIR) framework have broader implications for mathematical modeling and systems analysis. The use of non-linear fractional order models is not limited to computer viruses; similar models can be applied to biological systems such as the spread of infectious diseases in populations. The methodologies outlined in this chapter can be adapted to various epidemiological contexts, potentially improving the understanding of disease dynamics and control measures. The methods employed, particularly the Fractional Differential Transform Method (FDTM) and Differential Transform Method (DTM), can be integrated with other mathematical techniques, such as Agent-based Modeling or Network Theory to provide a more com- prehensive analysis of complex systems. This versatility allows the exploration of various dynamics and interactions in different contexts. The mathematical framework developed can be adapted for various applications. The most common and general model is the clas- sical non-linear fractional order Susceptible-Infected-Recovered (SIR) model for computer virus propagation is given below. 2. The S-I-R Model and Parameters The governing equations of the non-linear fractional-order SIR model[47] are given by: dγs(t) dtγ = f1 − λs(t)i(t)− ds(t), dγi(t) dtγ = f2 + λs(t)i(t)− εi(t)− dr(t), dγr(t) dtγ = f3 + εi(t)− dr(t). (1) with the initial conditions s(0) = s0, i(0) = i0, r(0) = r0 (2) The parameters and initial values of system 1 are given in Table 1. Here the fractional derivative used is the Caputo fractional derivative and γ ∈ (0, 1]. The generalization of integer order differentiation is known as fractional order differentia- tion. As the reader can see, calculating derivatives of fractional order is far more difficult R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 3 of 40 Table 1: List of parameters and their values Parameter Meaning Value s(t) Susceptible computers to the virus at time t s(0) = 20 i(t) Infected computers to the virus at time t i(0) = 15 r(t) Recovered computers from the virus at time t r(0) = 10 f1, f2, f3 Rate of other computers connecting to the network 0 λ Rate of virus infection for susceptible computers 0.001 ε Rate of recovery from virus for infected computers 0.1 d Rate of removing from the network 0.1 than computing derivatives of traditional integer order. Nevertheless, it has been demon- strated that fractional order mathematical models many phenomena’ attributes are better described by integrals and derivatives than by the previously employed integer order mod- els.This is because systems are typically not flawless and can be influenced by outside factors, for instance. Consequently, it might not be possible to comprehend the trajecto- ries of state variables using derivatives of integer order. With fractional derivatives, we may choose whatever fractional differential equation best captures the model’s dynamics since we have an infinite number of derivative orders at our disposal. Among other places, [48]and [49] exhibit experimental data and techniques for certain real-world events demon- strating that fractional order derivatives offer more effective solution curve modelling. In [50], Kamble, R., and Kukarni, P. have proved the existence and uniqueness of solutions for the following equation DαDβx (τ) = f (t, x (τ) , ϕx (τ) , ψx (τ)) , τ ∈ [0, 1] , x (0) = x (1) = 0 where 0 < α ≤ 1, 0 < β ≤ 1, Dα, Dβ are the Caputo fractional derivatives of order α , β respectively, f : [0, 1] × R3−→R is a continuous function λ, δ : [0, 1] × [0, 1] → [0,+∞), and ϕx (τ) = ∫ τ 0 λ (τ, s)x (s) ds, ψx (τ) = ∫ τ 0 δ (τ, s)x (s) ds ϕ∗ = sup t∈[0,1] ∣∣∣∣∫ t 0 λ (τ, s) ds ∣∣∣∣ <∞, ψ∗ = sup t∈[0,1] ∣∣∣∣∫ t 0 δ (τ, s) ds ∣∣∣∣ <∞ In [51], Kamble, R., and Kukarni, P. have proved the existence and uniqueness of solutions for the conformable fractional order Volterra-Fredholm type integro-differentail equations of the form dαx(t) dt = f (t) + ∫ t 0 p (t, s, x (s)) ds+ ∫ b 0 q (t, s, x (s)) ds with the initial condition x (0) = x0 where the term dαx(t) dt represents the conformable fractional order derivative of fractional order α ∈ (0, 1),t ∈ I = [0, b] , f : I → X, p, q : I × I ×X → X are continuous functions R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 4 of 40 and x0 is an element of a real Banach space X, with the norm ∥.∥. In [52], Kamble, R., and Kukarni, P. have given new definition and Prove there properties Definition 1. Let f : [0,∞) → R be a real valued function, α ∈ (0, 1], a > 0 ∈ R, a ̸= 1. We define the (α, a)-Extended fractional derivative(EFD) of f at x, denoted Dα a f(x), by Dα a f(x) = lim h→0 f(xahx (−α) )− f(x) h , (3) provided the limit exists. . In [53], Kamble, R., and Kukarni, P. have proved, Existence and uniqueness of solutions for exponential fractional differential equations. In [54], Kamble, R., and Kukarni, P. have developed method to solve, (α, 1) Fractional Dif- ferential Difference Equations With Conditions,Linear And Nonlinear with help of Laplace Transform And Laplace Decomposition Method. 3. Lyapunov Stability analysis of the given non Linear SIR model of Computer Viruses. Using lyapunov stability theory we have investigated the stability of given SIR frac- tional order non linear mathematical model is stable. The detail about lyapunov stability analysis of caputo fractional order nonliner system is given in [55]. Consider the following non linear system Dγ t0 Y(t) = g(t,Y(t)) = AY(t) + h(t,Y(t)),Y(t0) = Y0 where γ ∈ (0, 1),Y ∈ Rn called the state vector of the non linear system. Here A ∈ Rn×n is the constant matrix of the given system, and h : R+ ×Rn → Rn is the non linear part of the system, where h(t, 0) = 0 for all t ≥ 0. The corresponding linear system is Dγ t0 Y(t) = AY(t),Y(t0) = Y0 (4) The detailed stability of the above linear system is given in [55]. Now consider the following non-linear system Dγ t0 Y(t) = AY(t) +Bu+ h(t,Y(t)),Y(t0) = Y0 where B ∈ Rn×p is the constant matrix of the given system,u ∈ Rp is the control input to be defined. Writing the given SIR mathematical model of Computer Viruses in the form Dγ t0 Y(t) = AY(t) +Bu+ h(t,Y(t)),Y(t0) = Y0 R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 5 of 40 where A = −d 0 0 0 −ϵ −d 0 ϵ −d , B = f1f2 f3 , and Y(t) = [ s(t) i(t) r(t) ] and h(t,Y(t)) =[ −λs(t)i(t), λs(t)i(t), 0 ] . Since B = f1f2 f3 = 00 0 , the system convert into Dγ t0 Y(t) = AY(t) + h(t,Y(t)),Y(t0) = Y0 (5) Definition 2. [55] The non linear function h(t,Y) is said to be one sided Lipschitz if there exist ρ ∈ R such that ⟨h(t,Y1)− h(t,Y2),Y1 −Y2⟩ ≤ ρ(∥Y1 −Y2∥)2 Theorem 1. [55] Let Y = 0be an equilibrium point of the system 4. If the state ma- trix A is Hurwitz then the trivial solution of the fractional linear system 4 is fractional asymptotically stable. Theorem 2. [55] Let Y = 0 be an equilibrium point of the system 5. Let that the state matrix A is Hurwitz and the condition ∥h(t,Y(t))∥ < ρ holds. If there exist a positive definite matrix P such that the following inequality holds ρ < λmin(Q) 2λmax(P ) where λ is eigen value of matrix. where ATP + PA = −Q, then the trivial solution of the fractional linear system 5 is fractional asymptotically stable. Theorem 3. [55] If the function h(t,Y(t)) is Lipschitz continuous,L is Lipschitz Con- stant. Assume that the following assumption is hold : Then There exists a positive sym- metric matrix P and positive constant ϵ such that the following inequalities hold ATP + PA+ ϵI < 0 and L < ϵ 2λmaxP where λ is eigen value of matrix, then the trivial solution of fractional system 5 is asymptotically stable. The given SIR mathematical model of Computer Viruses can be written in the form Dγ t0 Y(t) = AY(t) +Bu+ h(t,Y(t)),Y(t0) = Y0 where A = −d 0 0 0 −ϵ −d 0 ϵ −d , B = f1f2 f3 , Y(t) = [ s(t) i(t) r(t) ] and h(t,Y(t)) = [ −λs(t)i(t), λs(t)i(t), 0 ] Since B = f1f2 f3 = 00 0 , the system convert into Dγ t0 Y(t) = AY(t) + h(t,Y(t)),Y(t0) = Y0 For the given system A = −d 0 0 0 −ϵ −d 0 ϵ −d = −0.1 0 0 0 −0.1 −0.1 0 0.1 0.1  A is Hurwitz matrix since the eigen values are λ1 = −0.1, R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 6 of 40 λ2 = 0.1 + 0.44721359549996i, λ3 = 0.1− 0.44721359549996i We can find positive definite matrices P and Q as given below where P = 10 0 0 0 10 0 0 0 10 , Q = 2 0 0 0 2 0 0 0 2 , ρ = 1 10 . With these values, all the conditions of theorem 2 are satisfied. Also, with the P given as above andϵ = 1 L = 1 20 all the condition of theorem 3 is satisfied. Therefore by theorem 3 the given fractional non linear system of SIR model is also asymptotically stable. 4. Numerical Methods The Fractional Differential Transform Method (FDTM) is used to solve the non-linear fractional order system of the Susceptible-Infected-Recovered mathematical model of com- puter viruses. In this section, we apply FDTM to solve the system of equations 1. The numerical solutions are compared with those obtained using the Differential Transform Method (DTM), verifying that our proposed results are valid when fractional order deriva- tive γ = 1. Additionally, we have taken five iterations of the solutions (k = 5) and compute the values of s(t), i(t), and r(t) for different time points. The Laplace Adomian Decomposition method (LADM) is also used to solve the non-linear fractional order system of the Susceptible-Infected-Recovered mathematical model of com- puter viruses. In this section, we apply LADM to solve the system of equations 1. The numerical solutions are compared, verifying that our proposed results are valid when frac- tional order derivative γ = 1. Additionally, we have taken five iterations of the solutions (k = 5) and compute the values of s(t), i(t), and r(t) for different time points. The Runge-Kutta Felhberg Algorithm (RKFA) is also used to solve the non-linear frac- tional order system of the Susceptible-Infected-Recovered mathematical model of computer viruses for fractional order derivative γ = 1. The results are visually presented through graphs that illustrate the evolution of the sus- ceptible, infected, and recovered populations over time for both methods. A comparison of results obtained from FDTM and LADM is performed to analyze differences and evaluate the effectiveness of the fractional order model in capturing the dynamics of computer virus propagation. Future work could explore higher-order fractional derivatives, incorporate more complex virus spread scenarios, or apply the model to different types of computer security threats. 5. Fractional Differential Transform Method The steps in the fractional differential transform method are given in [56]. The frac- tional differentiation in the Riemann-Liouville sense is defined as: Dγ t0 u(t) = 1 (n− γ) ∫ t t0 dm dxm (t− s)n−γ−1u(s)ds , (6) R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 7 of 40 where n − 1 ≤ γ < m, n is a positive integer, and t > t0. The expansion of an analytic and continuous function f(t) in terms of a fractional power series is given as: u(t) = ∞∑ k=0 U(k)(t− t0) k/µ, (7) where µ is the order of the fraction, and U(k) is the fractional differential transform of u(t). The relation between the Riemann-Liouville operator and the Caputo operator is given as follows: CDγ x0 u(t) = Dγ x0 [ u(t)− n−1∑ k=0 uk(t0) k! (t− t0) k ] . (8) Here, the notation C is used for the Caputo operator to distinguish it from the Riemann- Liouville operator. Since the initial conditions are implemented to the integer order differential equation, the transformed initial conditions can be obtained using the following relation: U(k) =  1 (k/µ)! [ d(k/µ)u(t) dt(k/µ) ] x=x0 , if k/µ ∈ Z+, 0, if k/µ /∈ Z+. (9) where k = 0, 1, 2, . . . , γµ−1, and γ is the order of the fractional differential equation. The parameter µ is chosen such that γµ is a positive integer. The following results[56] are applied in the proofs of the results in the next section. Theorem 4. [56] If w(t) = u(t)±v(t), then its transformed form is W (k) = U(k)±V (k). Theorem 5. [56] If w(t) = u(t)v(t), then W (k) = ∑k l=0 U(l)V (k − l). Theorem 6. [56] If w(t) = (t− t0) p, then W (k) = δ(k − λp), where: δ(k) = { 1, k = 0, 0, k ̸= 0. (10) Theorem 7. [56] If w(t) = Dγ t0 u(t), then: W (k) = Γ(γ + 1 + k/µ) Γ(1 + k/µ) U(k + γµ). (11) R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 8 of 40 6. Methodology of the Proposed Non-Linear Fractional Mathematical Model Using the transformation rules from equations theorem4–theorem7, the transformed equations are S(k + γµ) = Γ(1 + k/µ) Γ(1 + γ + k/µ) [ f1δ(k)− λ k∑ l=0 S(l)I(k − l)− dS(k) ] I(k + γµ) = Γ(1 + k/µ) Γ(1 + γ + k/µ) [ f2δ(k) + λ k∑ l=0 S(l)I(k − l)− εI(k)− dR(k) ] R(k + γµ) = Γ(1 + k/µ) Γ(1 + γ + k/µ) [f3δ(k) + εI(k)− dR(k)] (12) The initial conditions transform into: S(k) = 0, k = 1, 2, ..., γµ− 1 I(k) = 0, k = 1, 2, ..., γµ− 1 R(k) = 0, k = 1, 2, ..., γµ− 1, S(k) = 20, I(k) = 15, R(k) = 10, k = 0. (13) The approximate series solution for system 1 is: s(t) = n∑ j=0 S(j)tj/µ, i(t) = n∑ j=0 I(j)tj/µ, r(t) = n∑ j=0 R(j)tj/µ (14) Case I: γ = 1/10 For γ = 1/10, setting µ = 10, using 12, we obtain S(k + 10γ) = Γ(1 + k/10) Γ(1 + γ + k/10) [ f1δ(k)− λ k∑ l=0 S(l)I(k − l)− dS(k) ] I(k + 10γ) = Γ(1 + k/10) Γ(1 + γ + k/10) [ f2δ(k) + λ k∑ l=0 S(l)I(k − l)− εI(k)− dR(k) ] R(k + 10γ) = Γ(1 + k/10) Γ(1 + γ + k/10) [f3δ(k) + εI(k)− dR(k)] Substituting the initial conditions S(0) = 20, I(0) = 15, R(0) = 10, we obtain the values of S(k), I(k), R(k), 0 ≤ k ≤ 4 as follows. Thus, the approximate solution becomes s(t) = 20− 2.4177t1/10 + 0.3350t2/10 − 0.04716t3/10 + 0.005841t4/10 i(t) = 15− 2.3126t1/10 + 0.0996t2/10 + 0.03319t3/10 − 0.004836t4/10 (15) r(t) = 10 + 0.5255t1/10 − 0.2981t2/10 + 0.04037t3/10 − 0.00070805t4/10 R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 9 of 40 Table 2: Values of S(k), I(k), R(k), γ = 1/10. Sr. No. k S(k) I(k) R(k) 1 0 20 15 10 2 1 −2.4177 −2.3126 0.5255 3 2 0.3350 0.0996 −0.2981 4 3 −0.04716 0.03319 0.04037 5 4 0.005841 −0.004836 −0.00070805 Case II: γ = 1/2 For γ = 1/2, setting µ = 2, using (12), we obtain S(k + 2γ) = Γ(1 + k/2) Γ(1 + γ + k/2) [ f1δ(k)− λ k∑ l=0 S(l)I(k − l)− dS(k) ] I(k + 2γ) = Γ(1 + k/2) Γ(1 + γ + k/2) [ f2δ(k) + λ k∑ l=0 S(l)I(k − l)− εI(k)− dR(k) ] R(k + 2γ) = Γ(1 + k/2) Γ(1 + γ + k/2) [f3δ(k) + εI(k)− dR(k)] Using the initial conditions S(0) = 20, I(0) = 15, R(0) = 10, we obtain the values of S(k), I(k), R(k), 0 ≤ k ≤ 4 as follows. Thus, the approximate solution takes the form Table 3: Values of S(k), I(k), R(k), γ = 1/2. Sr. No. k S(k) I(k) R(k) 1 0 20 15 10 2 1 −2.5953 −2.4825 0.5642 3 2 0.3084 0.0915 −0.2699 4 3 −0.02477 0.01479 0.02718 5 4 0.002359 −0.003505 −0.001411 s(t) = 20− 2.5953t1/2 + 0.3084t− 0.02477t3/2 + 0.002359t2 i(t) = 15− 2.4825t1/2 + 0.0915t+ 0.01479t3/2 − 0.003505t2 r(t) = 10 + 0.5642t1/2 − 0.2699t+ 0.02718t3/2 − 0.001411t2 (16) Case III: γ = 1 For γ = 1, setting γµ = 1,i.e µ = 1 we obtain (12) as follows S(k + 1) = Γ(1 + k) Γ(2 + k) [ f1δ(k)− λ k∑ l=0 S(l)I(k − l)− dS(k) ] R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 10 of 40 I(k + 1) = Γ(1 + k) Γ(2 + k) [ f2δ(k) + λ k∑ l=0 S(l)I(k − l)− εI(k)− dR(k) ] R(k + 1) = Γ(1 + k) Γ(2 + k) [f3δ(k) + εI(k)− dR(k)] The table of values of S(k), I(k), R(k), 0 ≤ k ≤ 4 can be obtained as follows. The Table 4: Values of S(k), I(k), R(k), γ = 1. Sr. No. k S(k) I(k) R(k) 1 0 20 15 10 2 1 −2.3 −2.2 0.5 3 2 0.15425 0.04575 −0.135 4 3 −0.007904 0.005737 0.006025 5 4 0.0003097 −0.0004061 −0.0000216 approximate solution up to five iterations in this case is s(t) = 20− 2.3t+ 0.15425t2 − 0.007904t3 + 0.0003097t4 i(t) = 15− 2.2t+ 0.04575t2 + 0.005737t3 − 0.0004061t4 (17) r(t) = 10 + 0.5t− 0.135t2 + 0.006025t3 − 0.0000216t4 7. Laplace-Adomian Decomposition Method (LADM) Now we solve the system of equations (1) using the Laplace-Adomian Decomposition Method. Denoting the Laplace transform L[ϕ(t)] = Φ(z) and the Laplace transform of the Caputo fractional derivative of the function ϕ by L [dγϕ(t) dt ] = zγL[ϕ(t)]− n−1∑ k=0 zγ−k−1ϕ(k)(0) Since γ ∈ (0, 1] i.e. n = 1, the above equation become L [dγϕ(t) dt ] = zγL[ϕ(t)]− zγ−1ϕ(0) Using this relation and the system of equations (1), we get L[s(t)] = s(0) z − λ L[s(t)i(t)] zγ − d L[s(t)] zγ L[i(t)] = i(0) z + λ L[s(t)i(t)] zγ − ε L[i(t)] zγ − d L[r(t)] zγ R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 11 of 40 L[r(t)] = r(0) z + ε L[i(t)] zγ − d L[r(t)] zγ Setting A(t) = s(t)i(t), we have L[s(t)] = s(0) z − λ L[A(t)] zγ − d L[s(t)] zγ L[i(t)] = i(0) z + λ L[A(t)] zγ − ε L[i(t)] zγ − d L[r(t)] zγ L[r(t)] = r(0) z + ε L[i(t)] zγ − d L[r(t)] zγ The non-linear term A is called Adomian polynomial and it is given by A = ∞∑ j=0 Aj , An = n∑ j=0 s(j).i(n− j) and s = ∞∑ j=0 sj , i = ∞∑ j=0 ij , r = ∞∑ j=0 rj The terms sj , ij , rj are obtained as follows. L[s0] = s(0) z =⇒ s0 = s(0) = 20 L[i0] = i(0) z =⇒ s0 = i(0) = 15 L[r0] = r(0) z =⇒ r0 = r(0) = 10 L[s1] = −λL[s0i0] zγ − d L[s0] zγ =⇒ s1 = −2.3 tγ Γ(γ + 1) L[i1] = λ L[s0i0] zγ − ε L[i0] zγ − d L[r0] zγ =⇒ i1 = −2.2 tγ Γ(γ + 1) L[r1] = ε L[i0] zγ − d L[r0] zγ =⇒ r1 = 0.5 tγ Γ(γ + 1) L[s2] = −λL[A1] zγ − d L[s1] zγ =⇒ s2 = 0.3085 t2γ Γ(2γ + 1) L[i2] = λ L[A1] zγ − ε L[i1] zγ − d L[r1] zγ =⇒ i2 = 0.0915 t2γ Γ(2γ + 1) L[r2] = ε L[i1] zγ − d L[r1] zγ =⇒ r2 = −0.27 t2γ Γ(2γ + 1) L[s3] = −λL[A2] zγ − d L[s2] zγ =⇒ s3 = −0.0193325 t3γ Γ(3γ + 1) R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 12 of 40 L[i3] = λ L[A2] zγ − ε L[i2] zγ − d L[r2] zγ =⇒ i3 = 0.00293675 t3γ Γ(3γ + 1) L[r3] = ε L[i2] zγ − d L[r2] zγ =⇒ r3 = 0.03615 t3γ Γ(3γ + 1) L[s4] = −λL[A3] zγ − d L[s3] zγ =⇒ s4 = 0.0025250375 t4γ Γ(4γ + 1) L[i4] = λ L[A3] zγ − ε L[i3] zγ − d L[r3] zγ =⇒ i4 = −0.0045004625 t4γ Γ(4γ + 1) L[r4] = ε L[i3] zγ − d L[r3] zγ =⇒ r4 = −0.0033321325 t4γ Γ(4γ + 1) It can be verified that for j ≥ 1, we have L[sj ] = −λL[Aj−1] zγ − d L[sj−1] zγ L[ij ] = λ L[Aj−1] zγ − ε L[ij−1] zγ − d L[rj−1] zγ L[rj ] = ε L[ij−1] zγ − d L[rj−1] zγ The solution of the SIR model of computer viruses by Laplace Adomian decomposition method up to five iteration is given by s(t) = 4∑ j=0 sj = 20− 2.3 tγ Γ(γ + 1) + 0.3085 t2γ Γ(2γ + 1) − 0.0193325 t3γ Γ(3γ + 1) + 0.0025250375 t4γ Γ(4γ + 1) i(t) = 4∑ j=0 ij = 15− 2.2 tγ Γ(γ + 1) + 0.0915 t2γ Γ(2γ + 1) + 0.00293675 t3γ Γ(3γ + 1) − 0.0045004625 t4γ Γ(4γ + 1) (18) r(t) = 4∑ j=0 rj = 10 + 0.5 tγ Γ(γ + 1) − 0.27 t2γ Γ(2γ + 1) + 0.03615 t3γ Γ(3γ + 1) − 0.0033321325 t4γ Γ(4γ + 1) As in the earlier case, the solutions for different values of γ are obtained as follows. CaseI: γ = 1/10 s(t) =20− 2.4176145292t1/10 + 0.3359947896t2/10 − 0.021541986t3/10 + 0.0028458694t4/10 R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 13 of 40 i(t) =15− 2.312500854t1/10 + 0.0996548566t2/10 + 0.00322722506t3/10 − 0.0050722925t4/10 (19) r(t) =10 + 0.5255683759t1/10 − 0.2940635112t2/10 + 0.0402798531t3/10 − 0.0037555141t4/10 Case II: γ = 1/2 s(t) = 20− 2.595271866t1/2 + 0.3084t− 0.0145429311t3/2 + 0.0012625188t2 i(t) = 15− 2.4824339588t1/2 + 0.0915t+ 0.002209179t3/2 − 0.0022502313t2 (20) r(t) = 10 + 0.5641895361t1/2 − 0.27t+ 0.0271939459t3/2 − 0.0016660663t2 Case III: γ = 1 s(t) = 20− 2.3t+ 0.15425t2 − 0.0032220833t3 + 0.0001052099t4 i(t) = 15− 2.2t+ 0.04575t2 + 0.0004894583t3 − 0.0001875193t4 (21) r(t) = 10 + 0.5t− 0.135t2 + 0.006025t3 − 0.0001388389t4 8. Numerical Approximations and Estimate of Errors Using the equations (15), (16), which are obtained using the Fractional Differential Transform Method and the equations (19), (20), obtained using the Laplace Adomian Decomposition Method, the approximate values of the solutions s(t), i(t) and r(t) for the cases γ = 0.1 and γ = 0.5 are as shown by the tables 5 to 10. In these tables, the values are obtained by using the MATLAB software correct up to fourteen digits after the decimal. The notations s(t)FDTM, i(t)FDTM and r(t)FDTM are used to represent the solutions s(t), i(t) and r(t) obtained using the Fractional Differential Transform Method respectively. Similarly, the notations s(t)LADM, i(t)LADM and r(t)LADM are used to represent the solutions s(t), i(t) and r(t) obtained using the Laplace Adomian Decompo- sition Method respectively. The approximate values of the absolute errors in s(t), i(t) and r(t) are represented by Er[s(t)], Er[i(t)] and Er[r(t)] and are obtained by the formulae Er[s(t)] = |s(t)FDTM − s(t)LADM | Er[i(t)] = |i(t)FDTM − i(t)LADM | Er[r(t)] = |r(t)FDTM − r(t)LADM | R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 14 of 40 Table 5: Estimate of errors in s(t) for γ = 0.1. t s(t)FDTM s(t)LADM Er[s(t)] 0 20.00000000000000 20.00000000000000 0.00000000000000 5 17.55702229544161 17.59431154300001 0.03728924755840 10 17.40781060925223 17.45308607588309 0.04527546663086 15 17.31712461031913 17.36782451716560 0.05069990684647 20 17.25124112568540 17.30616983119194 0.05492870550654 25 17.19925180577707 17.25769584483516 0.05844403905810 30 17.15619659362801 17.21767482183604 0.06147822820803 Table 6: Estimate of errors in i(t) for γ = 0.1. t i(t)FDTM i(t)LADM Er[i(t)] 0 15.00000000000000 15.00000000000000 0.00000000000000 5 12.46558082849279 12.41676378653062 0.04881704196217 10 12.30053972810497 12.24037435176146 0.06016537634351 15 12.19982823339885 12.13183803127759 0.06799020212126 20 12.12647775783722 12.05232598332779 0.07415177450943 25 12.06849040276133 11.98917726395060 0.07931313881073 30 12.02039883376837 11.93660290522253 0.08379592854584 Table 7: Estimate of errors in r(t) for γ = 0.1. t r(t)FDTM r(t)LADM Er[r(t)] 0 10.00000000000000 10.00000000000000 0.00000000000000 5 10.27004286714835 10.26974491443414 0.00029795271420 10 10.26787884169264 10.26652744914304 0.00135139254960 15 10.26545056249648 10.26327199707570 0.00217856542077 20 10.26315827919200 10.26027696818093 0.00288131101106 25 10.26103572422611 10.25753353094654 0.00350219327957 30 10.25906856101875 10.25500465803592 0.00406390298284 R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 15 of 40 Table 8: Estimate of errors in s(t) for γ = 0.5. t s(t)FDTM s(t)LADM Er[s(t)] 0 20.00000000000000 20.00000000000000 0.00000000000000 5 15.52077075898145 15.61380112841204 0.09303036943060 10 14.32954461214130 14.55193192445817 0.22238731231687 15 13.66621435930453 14.02421111980599 0.35799676050146 20 13.28956940388280 13.77791436087322 0.48834495699041 25 13.11162500000000 13.71834853250000 0.60672353250000 30 13.08993014024754 13.79851856567137 0.70858842542383 Table 9: Estimate of errors in i(t) for γ = 0.5. t i(t)FDTM i(t)LADM Er[i(t)] 0 15.00000000000000 15.00000000000000 0.00000000000000 5 9.98419347279288 9.87505250806161 0.10914096473127 10 8.18184657457090 7.90969179323354 0.27215478133736 15 6.82841519839620 6.38011427914472 0.44830091925149 20 5.64878030720242 5.02572029367717 0.62306001352524 25 4.53312500000000 3.74508301850000 0.78804198150000 30 3.42353249758467 2.48594621404391 0.93758628354076 Table 10: Estimate of errors in r(t) for γ = 0.5. t r(t)FDTM r(t)LADM Er[r(t)] 0 10.00000000000000 10.00000000000000 0.00000000000000 5 10.18069619104760 10.17395205545793 0.00674413558967 10 9.80356412390077 9.77746541222377 0.02609871167700 15 9.39817751417899 9.34005725374527 0.05812026043372 20 8.99183221094853 8.88900625418141 0.10282595676712 25 8.58912500000000 8.42889948050000 0.16022551950000 30 8.18948040334127 7.95915496540499 0.23032543793628 9. Runge-Kutta Felhberg Algorithm An important family of predictor-corrector methods to solve linear and non-linear ordinary differential equations is known to the Runge-Kutta methods, named after the German mathematicians C. Runge (1856–1927) and M. W. Kutta (1867–1944). Consider the ordinary differential equation Y ′(t) = F [t, Y (t)], Y (0) = Y0 R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 16 of 40 where Y (t) = (y1(t), y2(t), · · · , yn(t))T , F : [a, b]× Rn → Rn is a continuous function and a, b ∈ R. In case the function F is non-linear and the analytical solutions do not exist, we need to obtain an approximate solution by dividing the interval [a, b] into n equal parts, each of length h = b−a n , n ∈ N,h is also called as the step size. Considering the mesh points ti = a + ih, i = 0, 1, · · · , n, the n + 1th approximate solution at the mth stage to the initial value problem is given by: Y (tn+1) = Yn+1 = Yn + m∑ i=1 aiki where km = F (tn + cmh+ Yn + h m−1∑ i=1 dmiki) The coefficients ci, 2 ≤ i ≤ m, dij , 1 ≤ j < i ≤ m, and ai, i ≤ i ≤ m are to be determined in the form of a table, known as Butcher Tableau. In order to improve the rate of convergence, the algorithm based on step-size adjustment was developed by Felhberg and is known as Runge-Kutta Felhberg Algorithm (RKFA). This algorithm is an adaptive algorithm where at each step, two different approximate solutions are obtained and are compared. If the two approximate solutions agree up to a desired level of accuracy, the approximate solution is accepted. In case the two approximate solutions did not agree, the step-size is reduced and the same procedure is repeated. This algorithm evaluates F [t, Y (t)] six times per step using the embedded 4th order and 5th order Runge-Kutta method. Moreover, the algorithm also evaluates the amount of errors. The approximate solution to the initial value problem by Runge-Kutta method of order 4 is given by: Yk+1 = Yk + 25k1 216 + 1408k2 2565 + 2197k4 4101 − k5 5 where at each step, the following six values are calculated. k1 = hF (tk, Yk) k2 = hF ( tk + h 4 , Yk + k1 4 ) k3 = hF ( tk + 3h 8 , Yk + 3k1 32 + 9k2 32 ) k4 = hF ( tk + 12h 13 , Yk + 1932k1 2197 − 7200k2 2197 + 7296k3 2197 ) k5 = hF ( tk + h, Yk + 439k1 216 − 8k2 + 3680k3 513 − 845k4 4104 ) k6 = hF ( tk + h 2 , Yk − 8k1 27 + 2k2 − 3544k3 2565 + 1859k4 4104 − 11k5 40 ) R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 17 of 40 A better approximate solution is given by the 5th order Runge-Kutta Felhberg Algorithm, which is given by Yk+1 = Yk + 16k1 135 + 6656k3 12825 + 28561k4 56430 − 9k5 50 + 2k6 55 It has been proved that RKFA provides more accurate solutions as compared to the Runge-Kutta method of order 4. Moreover, RKFA requires less number of iterations as compared to the R-K method to arrive at the desired level of accuracy. Using the RKFA, we have obtained the numerical values of s(t), i(t) and r(t) and compared them with the values obtained by FDTM and LADM for the case γ = 1. Moreover, we have obtained the estimates of the errors in these solutions with respect to the RKFA. The approximate values of the absolute errors in s(t), i(t) and r(t) are represented by ErFDTM [s(t)], ErFDTM [i(t)], ErFDTM [r(t)], etc. and are obtained by the formulae ErFDTM [s(t)] = |s(t)FDTM − s(t)RKFA| ErFDTM [i(t)] = |i(t)FDTM − i(t)RKFA| ErFDTM [r(t)] = |r(t)FDTM − r(t)RKFA| ErLADM [s(t)] = |s(t)LADM − s(t)RKFA|, etc. The estimate of errors in s(t), i(t), r(t) for γ = 1 are as shown in the tables 11, 12, 13. Table 11: Estimate of errors in s(t) for γ = 1. t s(t)FDTM s(t)LADM s(t)RKFA ErFDTM[s(t)] ErLADM[s(t)] 0.0 20.00000000000000 20.00000000000000 20.00000000000000 0.00000000000000 0.00000000000000 0.2 19.54610726352000 19.54614439166944 19.546107256391014 0.00000000712900 0.00003713527840 0.4 19.10418207232000 19.10447648004224 19.104181955888297 0.00000011643180 0.00029452415400 0.6 18.67386287312000 18.67484766521024 18.673862145750277 0.00000072736980 0.00098551946000 0.8 18.25480000512000 18.25711338732544 18.254797171108123 0.00000283401190 0.00231621621730 1.0 17.84665570000000 17.85113312660000 17.846647378609305 0.00000832139070 0.00448574799070 1.2 17.44910408192000 17.45677040330624 17.449083821756879 0.00002026016320 0.00768658154940 1.4 17.06183116752001 17.07389277777664 17.061787968569263 0.00004319895080 0.01210480920740 1.6 16.68453486592000 16.70237185040384 16.684451412115802 0.00008345380420 0.01792043828800 1.8 16.31692497872000 16.34208326164064 16.316775584419219 0.00014939430080 0.02530767722140 2.0 15.95872320000000 15.99290669200000 15.958471474156529 0.00025172584350 0.03443521784350 R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 18 of 40 Table 12: Estimate of errors in i(t) for γ = 1. t i(t)FDTM i(t)LADM i(t)RKFA ErFDTM[i(t)] ErLADM[i(t)] 0.0 15.00000000000000 15.00000000000000 15.00000000000000 0.00000000000000 0.00000000000000 0.2 14.56187524624000 14.56183361563552 14.561875256612106 0.00000001037210 0.00004164097660 0.4 14.12767677184000 14.12734652483712 14.127676929730777 0.00000015789070 0.00033040489360 0.6 13.69765656144000 13.69655142049152 13.697657518861158 0.00000095742110 0.00110609836960 0.8 13.27205100544000 13.26945379474432 13.272054690053119 0.00000368461310 0.00260089530880 1.0 12.85108090000000 12.84605193900000 12.851091662011378 0.00001076201130 0.00503972301130 1.2 12.43495144704000 12.42633694392192 12.538540600282305 0.10358915324230 0.11220365636040 1.4 12.02385225424000 12.01029269943232 12.023907974631463 0.00005572039140 0.01361527519910 1.6 11.61795733504000 11.59789589471232 11.618065010548600 0.00010767550860 0.02016911583630 1.8 11.21742510864000 11.18911601820192 11.217618014408080 0.00019290576800 0.02850199620610 2.0 10.82239840000000 10.78391535760000 10.822723791238749 0.00032539123870 0.03880843363870 Table 13: Estimate of errors in r(t) for γ = 1. t r(t)FDTM r(t)LADM r(t)RKFA ErFDTM[r(t)] ErLADM[r(t)] 0.0 10.00000000000000 10.00000000000000 10.00000000000000 0.00000000000000 0.00000000000000 0.2 10.09464816544000 10.09464817778578 10.094648185984170 0.00000002054410 0.00000000819840 0.4 10.17878504704000 10.17878524457242 10.178785335767941 0.00000028872790 0.00000009119550 0.6 10.25269860064000 10.25269960064786 10.252699863108273 0.00000126246820 0.00000026246040 0.8 10.31667595264000 10.31667911315866 10.316679322626605 0.00000336998660 0.00000020946800 1.0 10.37100340000000 10.37101111611000 10.371010136930472 0.00000673693040 0.00000097917960 1.2 10.41596641024000 10.41598241036570 10.415977336803497 0.00001092656340 0.00000507356230 1.4 10.45184962144000 10.45187926364818 10.451864314231031 0.00001469279100 0.00001494941710 1.6 10.47893684224000 10.47898741053850 10.478952588015369 0.00001574577530 0.00003482252320 1.8 10.49751105184000 10.49759205247634 10.497521581722806 0.00001052988280 0.00007047075350 2.0 10.50785440000000 10.50797785776000 10.507848413694944 0.00000598630510 0.00012944406510 10. Results and Discussion In the second section of this paper, we have formulated the non-linear fractional order SIR model of computer viruses with the specific initial conditions as described by the table 1. In the third section, we concluded that the system of equations 1 is asymptotically stable. In the sixth section, we have obtained the numerical values of the solutions which are given by the equations (15) and (16) for the cases γ = 0.1, 0.5. Whereas using the FDTM the solutions are obtained for the cases γ = 0.1, 0.5 as given by equations (19) and (20). To have a better understanding of the solution curves and errors, we have compared the numerical values obtained by FDTM and LADM with those obtained by RKFA. As can be noticed, we don’t get a clear picture of the solutions and the errors just from the tabulated values. For a better understanding of the system, we plot the graphs of the approximate solutions and errors for different values of γ. R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 19 of 40 Figure 1: Comparison of graphs of s(t) by FDTM and LADM for γ = 0.1 0 5 10 15 20 25 30 17 17.5 18 18.5 19 19.5 20 s(t) by FDTM and LADM for γ=0.1 t s (t ) s(t)FDTM s(t)LADM R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 20 of 40 Figure 2: Comparison of graphs of i(t) by FDTM and LADM for γ = 0.1 0 5 10 15 20 25 30 11.5 12 12.5 13 13.5 14 14.5 15 i(t) by FDTM and LADM for γ=0.1 t i( t) i(t)FDTM i(t)LADM R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 21 of 40 Figure 3: Comparison of graphs of r(t) by FDTM and LADM for γ = 0.1 0 5 10 15 20 25 30 10 10.05 10.1 10.15 10.2 10.25 10.3 10.35 r(t) by FDTM and LADM for γ=0.1 t r( t) r(t)FDTM r(t)LADM The graphs shown by figures 1, 2 and 3 represent the solution curves for s(t), i(t) and r(t) by FDTM and LADM for γ = 0.1. From these figures, it can be observed that the solutions obtained by FDTM and LADM almost agree for first few values of the variable t, to be specific, for t ∈ [0, 5]. But as t increases, slight differences in the solution curves are observed. The absolute errors in the solutions by both the methods can be observed in figure 4. R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 22 of 40 Figure 4: Comparison of errors in s(t), i(t), r(t) by FDTM and LADM for γ = 0.1 0 5 10 15 20 25 30 0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 Errors in s(t), i(t), r(t) by FDTM and LADM for γ=0.1 t E rr o rs i n s (t ), i (t ), r (t ) Er[s(t)] Er[i(t)] Er[r(t)] The phase-plane portraits of s(t), i(t), r(t) by both the methods are as plotted in figure 5. From this figure we note that the solution curves for s(t), i(t), r(t) progress almost hand- in-hand for the initial values of the variable t, but differ later on. R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 23 of 40 Figure 5: Phase plane portraits of s(t), i(t), r(t) by FDTM and LADM for γ = 0.1 0 5 10 15 20 25 30 10 11 12 13 14 15 16 17 18 19 20 Phase portratis of s(t), i(t), r(t) by FDTM and LADM for γ=0.1 t s (t ), i (t ), r (t ) s(t)FDTM s(t)LADM i(t)FDTM i(t)LADM r(t)FDTM r(t)LADM The solution curves, errors and the phase-plain portrait for γ = 0.5 are as shown by figures 6 to figure 10. In this case also we have a similar type of conclusion as in the case for γ = 0.1. This type of pattern can be observed for the both the methods for γ ∈ (0, 1). R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 24 of 40 Figure 6: Comparison of graphs of s(t) by FDTM and LADM for γ = 0.5 0 5 10 15 20 25 30 13 14 15 16 17 18 19 20 s(t) by FDTM and LADM for γ=0.5 t s (t ) s(t)FDTM s(t)LADM R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 25 of 40 Figure 7: Comparison of graphs of i(t) by FDTM and LADM for γ = 0.5 0 5 10 15 20 25 30 2 4 6 8 10 12 14 16 i(t) by FDTM and LADM for γ=0.5 t i( t) i(t)FDTM i(t)LADM R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 26 of 40 Figure 8: Comparison of graphs of r(t) by FDTM and LADM for γ = 0.5 0 5 10 15 20 25 30 7.5 8 8.5 9 9.5 10 10.5 r(t) by FDTM and LADM for γ=0.5 t r( t) r(t)FDTM r(t)LADM R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 27 of 40 Figure 9: Comparison of errors in s(t), i(t), r(t) by FDTM and LADM for γ = 0.5 0 5 10 15 20 25 30 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 Errors in s(t), i(t), r(t) by FDTM and LADM for γ=0.5 t E rr o rs i n s (t ), i (t ), r (t ) Er[s(t)] Er[i(t)] Er[r(t)] R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 28 of 40 Figure 10: Phase plane portraits of s(t), i(t), r(t) by FDTM and LADM for γ = 0.5 0 5 10 15 20 25 30 2 4 6 8 10 12 14 16 18 20 Phase portratis of s(t), i(t), r(t) by FDTM for γ=0.5 t s (t ), i (t ), r (t ) s(t)FDTM s(t)LADM i(t)FDTM i(t)LADM r(t)FDTM r(t)LADM For γ = 1, figure 11 shows solution curves for s(t) by FDTM, LADM and RKFA. In the graph, the curves are respectively named as s(t)FDTM, s(t)LADM and s(t)RKFA. In the figure, we can not find any differences in the curves just by naked eyes and the curves appear to be coincident and one can not have better understanding of which method among FDTM and LADM is close enough to RKFD. To overcome this difficulty, we have obtained a zoom-in figure of figure 11, which is shown in figure 12. From this figure, we observe that the curve obtained by FDTM is comparatively colse to the one obtained by RKFA. A similar conclusion for the curves i(t) and r(t) can be drawn form the figure 13 to figure 16. R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 29 of 40 Figure 11: Comparison of graphs of s(t) by FDTM, LADM and RKFA for γ = 1 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2 15.5 16 16.5 17 17.5 18 18.5 19 19.5 20 t s (t ) s(t) by FDTM, LADM and RKFA for γ=1 s(t)FDTM s(t)LADM s(t)RKFA Figure 12: Zoom-in s(t) by FDTM and LADM for γ = 1 1.986 1.988 1.99 1.992 1.994 1.996 1.998 2 15.965 15.97 15.975 15.98 15.985 15.99 15.995 t s (t ) s(t) by FDTM, LADM and RKFA for γ=1 s(t)FDTM s(t)LADM s(t)RKFA R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 30 of 40 Figure 13: Comparison of graphs of i(t) by FDTM and LADM for γ = 1 0 0.5 1 1.5 2 10.5 11 11.5 12 12.5 13 13.5 14 14.5 15 t i( t) i(t) by FDTM, LADM and RKFA for γ=1 i(t)FDTM i(t)LADM i(t)RKFA R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 31 of 40 Figure 14: Zoom-in i(t) by FDTM and LADM for γ = 1 1.974 1.976 1.978 1.98 1.982 1.984 1.986 1.988 10.825 10.83 10.835 10.84 10.845 10.85 10.855 t i( t) i(t) by FDTM, LADM and RKFA for γ=1 i(t)FDTM i(t)LADM i(t)RKFA Figure 15: r(t) by FDTM and LADM for γ = 1 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2 10 10.1 10.2 10.3 10.4 10.5 10.6 t r( t) r(t) by FDTM, LADM and RKFA for γ=1 r(t)FDTM r(t)LADM r(t)RKFA R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 32 of 40 Figure 16: Zoom-in r(t) by FDTM and LADM for γ = 1 1.9772 1.9773 1.9774 1.9775 1.9776 1.9777 1.9778 1.9779 1.978 1.9781 10.5066 10.5067 10.5067 10.5068 10.5068 t r( t) r(t) by FDTM, LADM and RKFA for γ=1 r(t)FDTM r(t)LADM r(t)RKFA The figure 17 shows the estimate of absolute errors in s(t) by FDTM and LADM with respect to RKFA. In the figure, we observe that the absolute error by FDTM is almost close to zero and the curve is going parallel to the x-axis while the error by LADM is though in between 10−2 and 10−4, but still growing exponentially. The figure 18 shows the error in i(t) and the figure 19 shows the error in r(t). R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 33 of 40 Figure 17: Error in s(t) by FDTM and LADM for γ = 1 0 0.5 1 1.5 2 0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 t E r[ s (t )] Error in s(t) by FDTM, LADM with respect to RKFA for γ=1 ErFDTM[s(t)] ErLADM[s(t)] R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 34 of 40 Figure 18: Error in i(t) by FDTM and LADM for γ = 1 0 0.5 1 1.5 2 0 0.02 0.04 0.06 0.08 0.1 0.12 t E r[ i( t) ] Error in i(t) by FDTM, LADM with respect to RKFA for γ=1 ErFDTM[i(t)] ErLADM[i(t)] R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 35 of 40 Figure 19: Error in r(t) by FDTM and LADM for γ = 1 0 0.5 1 1.5 2 0 0.2 0.4 0.6 0.8 1 1.2 1.4 x 10 −4 t E r[ r( t) ] Error in r(t) by FDTM, LADM with respect to RKFA for γ=1 ErFDTM[r(t)] ErLADM[r(t)] 11. Conclusion In this paper, the non-linear Fractional order susceptible-infected-Recovered(SIR) math- ematical model of computer viruses is presented.The fractional derivative used in the model is Caputo Fractional derivative. Using Lyapunov stability analysis,the stability verified of the given mathematical model. The FDTM and the LADM are two reliable and use- ful techniques that were used in this work to solve the non-linear epidemiological model of computer viruses Involving Non-linear Fractional Order Differential Equation. These models are among the useful computer engineering models that we may use to monitor, assess, and forecast computer viruses within a network. To demonstrate the effectiveness and precision of the approach that was described, the residual errors for five iterations were displayed using the LADM, FDTM, and RKFA. Additionally, residual error graphs were shown to illustrate the capabilities of the methodologies that were provided. These findings suggest that the FDTM is more easy and applicable than the LADM without R. M. Kamble, P. R. Kulkarni / Eur. J. Pure Appl. Math, 18 (4) (2025), 6693 36 of 40 adomian polynomial. From the graphical analysis of the solution curves and errors by by FDTM and LADM, we conclude that the FDTM for solving the non-linear system of equations 1 presents better solutions as compared to the LADM. However, one should note that due to the complexity of calculations, while finds the solutions by FDTM and LADM, we have considered only five iterations and a small interval for the values of the variable t. 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