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Novel dynamics of the fractional KFG equation through the unified and unified solver schemes with stability and multistability analysis

  • Noor Alam , Mohammad Safi Ullah EMAIL logo , Taher A. Nofal , Hamdy M. Ahmed , Karim K. Ahmed and Mahmoud A. AL-Nahhas
Published/Copyright: October 19, 2024
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Abstract

The nonlinear fractional Klein–Fock–Gordon (KFG) equation represents an advanced theoretical physics and applied mathematical tool that provides a more extraordinary framework for studying fields with complex and non-standard behaviors. Here, we aim to delve into the new wave profiles of this fractional KGF equation. Initially, this system is successfully converted into an ordinary differential equation (ODE) with the help of wave conversion, and the ODE is solved through the unified and unified solver techniques for the first time. In addition, the 3D and 2D plots of these solutions are drawn using a mathematical software package for different parameters with different values. Therefore, some unique waveforms can be found in these solutions. Moreover, stability and multistability analyses are prepared and shown graphically to confirm the converging limitations of appropriate parameters. This work will be practiced more effectively in future research on nonlinear partial differential models.

1 Introduction

Nonlinear partial differential models play a vibrant role in detecting the conduct of physical science. During the last two decades, this field has enriched its branches more and more in physical science, namely mathematical physics [1], electromagnetism [2], magnetohydrodynamic [3,4], plasma science [5], solidary physics [6], laser science [7], etc.

The researchers of these fields recognized a vast number of nonlinear models, including the generalized KP model [8], chikungunya infection model [9], the Benjamin–Ono equation [10], the Hirota–Maccari equation [11], the Zoomeron equation [12], the Bogoyavlenskii system [13], the Biswas–Arshed system [14], fractional-calculus [15,16], and Kundu–Eckhaus model [17,18]. In 1995, Doktorov used Klein–Fock–Gordon (KFG) equations to analyze the integrability of this equation [19]. Subsequently, many authors investigated different models with this equation [20,21,22].

The nonlinear equations are solved by various effective methods, such as the WBBM model [23], generalized KP equation [24], new Kudryashov’s methods [25,26,27], the generalized CBS-BK model [28], (G′/G) expansion technique [29], (G′/G 2) expansion technique [30], lie group technique [31], enhanced Kudryashov scheme [32], he first integral method [33], unified technique [34], unified solver technique [35], etc. [36,37].

The nonlinear fractional KFG equation is an elegant expansion of the classical KFG equation, which integrates fractional calculus in field theory. This generalized equation can be applied in various fields, which include quantum mechanics, cosmology, and nonlinear optics [38]. One of the most important factors of this equation is it enhances the understanding level by offering insights into the behavior of fields with fractional dynamics where traditional models have some backlogs. This study explores the soliton outcomes of the fractional KFG model through the unified and unified solver methods with stability and multistability analysis for the conditions of various parameters.

The design of this article is as follows. Section 2 covers the translation of an ordinary differential equation (ODE) from the fractional KFG model. The solution processes are discussed through unified and unified solver methods in Sections 3 and 4. Subsequently, the graphical discussion of the outcomes is shown in Section 5. In Sections 6 and 7, the stability and multistability analyses with a graphical representation of the limitations of the existence of the parameters are explored for the suggested model. Moreover, the novelty of our work is discussed in Section 8. Finally, some conclusions are given in the last section.

The originality of this study is that the outcome from our suggested model through the unified and unified solver methods has not been explored by any other scholars before.

2 Fractional KFG model

The nonlinear fractional KFG time-dependent model [20,39,40] can be written as follows:

(1) D t 2 β w ( x , t ) + c 1 w x x ( x , t ) + c 2 w 3 ( x , t ) + c 3 w ( x , t ) = 0 , 0 < β 1 .

Here, c 3, c 2, and c 1 are arbitrary parameters, and w(x, t) indicates a wave amplitude that relies on x, t. Eq. (1) is a nonlinear equation of a relativistic wave in energy-relevant physics. Here, the comfortable fractional derivative [41,42] is represented by D t 2 β and defined by

(2) D t β f ( t ) = lim h 0 f ( t + h t 1 β ) f ( t ) h ,

where f is a function whose domain is non-negative real and whose range is a real number, t > 0, and 0 < β ≤ 1. The consequent formula is found and constructed on the explanation of Eq. (2) as

(3) D t β f ( g ( t ) ) = t 1 β D t g ( t )   D t f ( g ( t ) )

Some other characteristics are discussed below for r (any constant) and s, m (real constants):

  1. D t β t n = n t n β n .

  2. D t β ( r ) = 0 .

  3. D t β s f ( t ) = s D t β f ( t ) .

  4. D t β ( s f ( t ) + m g ( t ) ) = s D t β f ( t ) + cm g ( t ) .

  5. D t β ( g ( t ) f ( t ) ) = g ( t ) D t β f ( t ) + f ( t ) D t β g ( t ) .

  6. D t β f ( t ) g ( t ) = g ( t ) D t β f ( t ) f ( t ) D t β g ( t ) g 2 ( t ) , g ( t ) 0 .

To convert Eq. (1) into an ODE form, consider the following relation:

(4) w ( x , t ) = R ( χ ) , χ = x b t β β ,

Eq. (1) will be converted into the following ODE:

(5) ( b 2 + c 1 ) R ( χ ) + c 2 R 3 ( χ ) + c 3 R ( χ ) = 0 ,

with arbitrary constants b, c 3, c 2, and c 1. Here “′” denotes derivative with respect to χ.

3 Unified technique for the fractional KFG model

Assume a trial solution with an auxiliary equation (Eq. (1)) as follows [43,44]:

(6) R ( χ ) = n i = n a i λ ( χ ) i

and

(7) λ ( χ ) = λ 2 ( χ ) + s .

Eq. (6) gives the following solutions.

Group 1: Hyperbolic function (for s < 0):

(8) λ ( χ ) = ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) .

Group 2: Trigonometric function (for s > 0):

(9) λ ( χ ) = ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B i s 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) .

Group 3: Rational function (for s = 0):

(10) λ ( χ ) = 1 χ + E ,

when A ≠ 0, s, E, and B are arbitrary constants.

By balancing R 3 and R″ and taking n = 1, we obtain Eq. (6):

(11) R ( χ ) = a 0 + a 1 λ ( χ ) + a 1 λ ( χ ) 1 .

Plugging Eqs. (11) and (7) into Eq. (5),

(12) b = ± 1 4 2 s ( 8 c 1 s + c 3 ) s ; a 1 = 1 2 c 3 s s c 2 c 3 ; a 0 = 0 ; a 1 = ± 1 2 c 2 c 3 s c 2 s ,

(13) b = ± 1 2 s ( 4 c 1 s c 3 ) s ; a 1 = c 3 s 2 s c 2 c 3 ; a 0 = 0 ; a 1 = ± 1 2 2 c 2 c 3 s c 2 s ,

(14) b = ± 1 2 2 s ( 2 c 1 s + c 3 ) s ; a 1 = 0 ; a 0 = 0 ; a 1 = ± s c 2 c 3 s c 2 ,

(15) b = ± 1 2 2 s ( 2 c 1 s + c 3 ) s ; a 1 = ± c 2 s c 3 c 2 ; a 0 = 0 ; a 1 = 0 .

From Eqs. (4), (5), (8)–(11), and (12), we obtain

w 1 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 2 c 3 s s c 2 c 3 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 , s > 0 ,

w 2 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 2 c 3 s s c 2 c 3 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 , s > 0 ,

w 3 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 2 c 3 s s c 2 c 3 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 , s > 0 ,

w 4 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 2 c 3 s s c 2 c 3 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 , s > 0 ,

w 5 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 2 c 3 s s c 2 c 3 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 , s < 0 ,

w 6 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 2 c 3 s s c 2 c 3 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 , s < 0 ,

w 7 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 2 c 3 s s c 2 c 3 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 , s < 0 ,

w 8 ( x , y ) = ± 1 2 s c 2 c 3 s c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 2 c 3 s s c 2 c 3 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 , s < 0 ,

where χ = x b t β β and b = ± 1 4 2 s ( 8 s c 1 + c 3 ) s .

From Eqs. (4), (5), (8)–(11) and (13), we obtain

w 9 ( x , y ) = ± 1 2 2 s c 2 c 3 s c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B c 3 s 2 s c 2 c 3 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 , s > 0 ,

w 10 ( x , y ) = ± 1 2 2 s c 2 c 3 s c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B c 3 s 2 s c 2 c 3 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 , s > 0 ,

w 11 ( x , t ) = ± 1 2 2 s c 2 c 3 s c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) c 3 s 2 s c 2 c 3 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 , s > 0 ,

w 12 ( x , y ) = ± 1 2 2 s c 2 c 3 s c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) c 3 s 2 s c 2 c 3 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 , s > 0 ,

w 13 ( x , y ) = ± 1 2 2 s c 2 c 3 s c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B c 3 s 2 s c 2 c 3 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 , s < 0 ,

w 14 ( x , y ) = ± 1 2 2 s c 2 c 3 s c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B c 3 s 2 s c 2 c 3 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 , s < 0 ,

w 15 ( x , y ) = ± 1 2 2 s c 2 c 3 s c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) c 3 s 2 s c 2 c 3 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 , s < 0 ,

w 16 ( x , y ) = ± 1 2 2 s c 2 c 3 s c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) c 3 s 2 s c 2 c 3 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 , s < 0 ,

where χ = x b t β β and b = ± 1 2 s ( 4 s c 1 c 3 ) s .

From Eqs. (4), (5), (8)–(11) and (14), we obtain

w 17 ( x , y ) = ± s c 2 c 3 s c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B , s > 0 ,

w 18 ( x , y ) = ± s c 2 c 3 s c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B , s > 0 ,

w 19 ( x , y ) = ± s c 2 c 3 s c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) , s > 0 ,

w 20 ( x , y ) = ± s c 2 c 3 s c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) , s > 0 ,

w 21 ( x , y ) = ± s c 2 c 3 s c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B , s < 0 ,

w 22 ( x , y ) = ± s c 2 c 3 s c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B , s < 0 ,

w 23 ( x , y ) = ± s c 2 c 3 s c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) isin ( 2 s ( χ + E ) ) , s < 0 ,

w 24 ( x , y ) = ± s c 2 c 3 s c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) isin ( 2 s ( χ + E ) ) , s < 0 ,

where χ = x b t β β and b = ± 1 2 2 s ( 2 s c 1 + c 3 ) s .

From Eqs. (4), (5), (8)–(11), and (15), we obtain

w 25 ( x , y ) = ± c 2 s c 3 c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 , s > 0 ,

w 26 ( x , y ) = ± c 2 s c 3 c 2 ( A 2 + B 2 ) s A s cosh ( 2 s ( χ + E ) ) A sinh ( 2 s ( χ + E ) ) + B 1 , s > 0 ,

w 27 ( x , y ) = ± c 2 s c 3 c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 , s > 0 ,

w 28 ( x , y ) = ± c 2 s c 3 c 2 s + 2 A s A + cosh ( 2 s ( χ + E ) ) sinh ( 2 s ( χ + E ) ) 1 , s > 0 ,

w 29 ( x , y ) = ± c 2 s c 3 c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 , s < 0 ,

w 30 ( x , y ) = ± c 2 s c 3 c 2 ( A 2 B 2 ) s A s cos ( 2 s ( χ + E ) ) A sin ( 2 s ( χ + E ) ) + B 1 , s < 0 ,

w 31 ( x , y ) = ± c 2 s c 3 c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 , s < 0 ,

w 32 ( x , y ) = ± c 2 s c 3 c 2 i s + 2 i A s A + cos ( 2 s ( χ + E ) ) i sin ( 2 s ( χ + E ) ) 1 , s < 0 ,

where χ = x b t β β and b = ± 1 2 2 s ( 2 s c 1 + c 3 ) s .

4 Unified solver method for the proposed system

From the obtainable solver process in previous studies [45,46], the results for Eq. (5) are shown as follows:

Group 1: Rational function outcomes (for c 3 = 0):

w 33 ( x , t ) = c 2 2 ( b 2 + c 1 ) ( χ + ξ ) 1 ,

w 34 ( x , t ) = c 2 2 ( b 2 + c 1 ) ( χ + ξ ) 1 ,

where χ = x b t β β , and ξ and b are arbitrary constants.

Group 2: Trigonometric function outcomes (for c 3 b 2 + c 1 < 0 ):

w 35 ( x , t ) = c 3 c 2 tan c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

w 36 ( x , y ) = c 3 c 2 tan c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

w 37 ( x , t ) = c 3 c 2 cot c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

w 38 ( x , y ) = c 3 c 2 cot c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

where χ = x b t β β , and ξ, and b are arbitrary constants.

Group 3: Hyperbolic function outcomes (for c 3 b 2 + c 1 > 0 ):

w 39 ( x , t ) = c 3 c 2 tanh c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

w 40 ( x , y ) = c 3 c 2 tanh c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

w 41 ( x , t ) = c 3 c 2 coth c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

w 42 ( x , y ) = c 3 c 2 coth c 3 2 ( b 2 + c 1 ) ( χ + ξ ) ,

where χ = x b t β β , and ξ and b are arbitrary constants.

5 Results and discussion

The unified and unified solver techniques have been effectively applied to the KFG equation to obtain the solutions of this model. All the outcomes attained by these methods are novel dynamical outcomes, as these methods have never been applied in the proposed system. These outcomes are shown graphically by plotting 3D and 2D curves.

The 3D and 2D visualization of the outcomes Re(w 33) is shown in Figure 1 using the parameters c 3 = 0, ξ = 1, b = 1.5, c 1 = 2, c 2 = 2.5, and β = 0.1 for (a, d), β = 0.4 for (b, e), and β = 0.8 for (c, f) with −20 ≤ t, x ≤ 20. These curves represent a bright soliton, and the changes for the different values of β are seen clearly. Conversely, a dark soliton is exposed as shown in Figure 2 with the parameters β = 0.1, 0.4, 0.8; c 3 = 0; ξ = 1, b = 1.5, c 1 = 2, and c 2 = 2.5 of the solution Re(w 34).

Figure 1 
               3D and 2D visualization of bright soliton outcome w
                  33 for the parameters c
                  3 = 0, ξ = 1, b = 1.5, c
                  1 = 2, c
                  2 = 2.5. (a) 3D curve for β = 0.1, (b) 3D curve for β = 0.4, (c) 3D curve for β = 0.8, (d) 2D curve for β = 0.1, (e) 2D curve for β = 0.4, and (f) 2D curve for β = 0.8.
Figure 1

3D and 2D visualization of bright soliton outcome w 33 for the parameters c 3 = 0, ξ = 1, b = 1.5, c 1 = 2, c 2 = 2.5. (a) 3D curve for β = 0.1, (b) 3D curve for β = 0.4, (c) 3D curve for β = 0.8, (d) 2D curve for β = 0.1, (e) 2D curve for β = 0.4, and (f) 2D curve for β = 0.8.

Figure 2 
               3D and 2D visualization of the dark soliton solution w
                  34 for the parameters c
                  3 = 0, ξ = 1, b = 1.5, c
                  1 = 2, and c
                  2 = 2.5. (a) 3D curve for β = 0.1, (b) 3D curve for β = 0.4, (c) 3D curve for β = 0.8, (d) 2D curve for β = 0.1, (e) 2D curve for β = 0.4, and (f) 2D curve for β = 0.8.
Figure 2

3D and 2D visualization of the dark soliton solution w 34 for the parameters c 3 = 0, ξ = 1, b = 1.5, c 1 = 2, and c 2 = 2.5. (a) 3D curve for β = 0.1, (b) 3D curve for β = 0.4, (c) 3D curve for β = 0.8, (d) 2D curve for β = 0.1, (e) 2D curve for β = 0.4, and (f) 2D curve for β = 0.8.

In contrast, a mathematical simulation is shown in Figure 3 to discuss the visual profile of the results Im (w 20) for the parameters β = 0.01, 0.35, 0.70, 1.0; s = −1; A = ξ = b = c 1 = c 2 = c 3 = 1; and B = E = a 0 = a −1 = 0. This figure indicates a kinky breather wave, whereas Figure 4 represents an anti-kink wave with a breather wave of the outcomes Im(w 28) for the parameters β = 0.30, 0.55, 0.75, 1.0; s = −1; A = ξ = b = c 1 = c 2 = c 3 = 1; and B = E = a 0 = a 1 = 0.

Figure 3 
               3D and 2D visualization of the kinky breather wave w
                  20 for the parameters s = −1, A = ξ = b = c
                  1 = c
                  2 = c
                  3 = 1, and B = E = a
                  0 = a
                  −1 = 0. (a) 3D curve for β = 0.01, (b) 3D curve for β = 0.35, (c) 3D curve for β = 0.70, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.01, (f) 2D curve for β = 0.35, (g) 2D curve for β = 0.70, and (h) 2D curve for β = 1.0.
Figure 3

3D and 2D visualization of the kinky breather wave w 20 for the parameters s = −1, A = ξ = b = c 1 = c 2 = c 3 = 1, and B = E = a 0 = a −1 = 0. (a) 3D curve for β = 0.01, (b) 3D curve for β = 0.35, (c) 3D curve for β = 0.70, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.01, (f) 2D curve for β = 0.35, (g) 2D curve for β = 0.70, and (h) 2D curve for β = 1.0.

Figure 4 
               3D and 2D visualization of the anti-kink wave with the breather wave w
                  28 for the parameters s = −1, A = ξ = b = c
                  1 = c
                  2 = c
                  3 = 1, and B = E = a
                  0 = a
                  1 = 0. (a) 3D curve for β = 0.30, (b) 3D curve for β = 0.55, (c) 3D curve for β = 0.75, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.30, (f) 2D curve for β = 0.55, (g) 2D curve for β = 0.75, and (h) 2D curve for β = 1.0.
Figure 4

3D and 2D visualization of the anti-kink wave with the breather wave w 28 for the parameters s = −1, A = ξ = b = c 1 = c 2 = c 3 = 1, and B = E = a 0 = a 1 = 0. (a) 3D curve for β = 0.30, (b) 3D curve for β = 0.55, (c) 3D curve for β = 0.75, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.30, (f) 2D curve for β = 0.55, (g) 2D curve for β = 0.75, and (h) 2D curve for β = 1.0.

Furthermore, we investigate the parameter values β = 0.10, 0.35, 0.70, 1.0; A = s = ξ = b = c 1 = c 2 = c 3 = 1; and B = E = a 0 = 0. In Figure 5, the profile of Im(w 8) is portrayed, which represents a lump-type breather wave. Finally, a local breather wave can be found in the solution abs(w 4) for the values β = 0.2, 0.4, 0.8, 1.0; s = −1, A = ξ = b = c 1 = c 2 = c 3 = 1, and B = E = a 0 = 0, as shown in Figure 6.

Figure 5 
               3D and 2D visualization of the lump-type breather wave w
                  8 for the parameters A = s = ξ = b = c
                  1 = c
                  2 = c
                  3 = 1, and B = E = a
                  0 = 0. (a) 3D curve for β = 0.10, (b) 3D curve for β = 0.35, (c) 3D curve for β = 0.70, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.10, (f) 2D curve for β = 0.35, (g) 2D curve for β = 0.70, and (h) 2D curve for β = 1.0.
Figure 5

3D and 2D visualization of the lump-type breather wave w 8 for the parameters A = s = ξ = b = c 1 = c 2 = c 3 = 1, and B = E = a 0 = 0. (a) 3D curve for β = 0.10, (b) 3D curve for β = 0.35, (c) 3D curve for β = 0.70, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.10, (f) 2D curve for β = 0.35, (g) 2D curve for β = 0.70, and (h) 2D curve for β = 1.0.

Figure 6 
               3D and 2D visualization of the local breather wave w
                  4 for the parameters s = −1, A = ξ = b = c
                  1 = c
                  2 = c
                  3 = 1, and B = E = a
                  0 = 0. (a) 3D curve for β = 0.20, (b) 3D curve for β = 0.40, (c) 3D curve for β = 0.80, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.20, (f) 2D curve for β = 0.40, (g) 2D curve for β = 0.80, and (h) 2D curve for β = 1.0.
Figure 6

3D and 2D visualization of the local breather wave w 4 for the parameters s = −1, A = ξ = b = c 1 = c 2 = c 3 = 1, and B = E = a 0 = 0. (a) 3D curve for β = 0.20, (b) 3D curve for β = 0.40, (c) 3D curve for β = 0.80, (d) 3D curve for β = 1.0, (e) 2D curve for β = 0.20, (f) 2D curve for β = 0.40, (g) 2D curve for β = 0.80, and (h) 2D curve for β = 1.0.

6 Stability study for the equilibrium points

By plugging R = X and X′ = Y into the proposed system to explore the phase plan, we can re-write Eq. (5) as follows [47]:

(16) d X d χ = Y = h ( X , Y ) d Y d χ = c 2 b 2 + c 1 X 3 c 3 b 2 + c 1 X = g ( X , Y ) .

The outcomes of the phase plan of the KFG equation are represented by system (16), which originates from the Hamiltonian system:

(17) X = H Y and Y = H X H ( X , Y ) = c 2 4 ( b 2 + c 1 ) X 4 + c 3 2 ( b 2 + c 1 ) X 2 + Y 2 2 .

By taking c 3 = 0, we obtain an equilibrium point from Eq. (16) as (X 1, Y 1) = (0,0). In contrast, for c 3 ≠ 0, we obtain three equilibrium points: ( 0 , 0 ) , c 3 c 2 , 0 , and c 3 c 2 , 0 , where c 2 ≠ 0.

We can write the Jacobian matrix as follows:

J ( X , Y ) = ( h , g ) ( X , Y ) = h X h Y g X g Y ( X 1 , Y 1 ) = 0 1 3 c 2 b 2 + c 1 X 2 c 3 b 2 + c 1 0 .

The characteristics equation of J is

(18) J γ I = 0 , or , γ 2 tr ( J ) γ + det ( J ) = 0 , or, γ 2 + 3 c 2 b 2 + c 1 X 2 + c 3 b 2 + c 1 = 0 .

Case 1: Stability at (0,0)

At (0,0), the characteristic roots of Eq. (18) are γ 1 = c 3 b 2 + c 1 and γ 2 = c 3 b 2 + c 1 . For c 3 b 2 + c 1 < 0 , these eigenvalues are real with a reverse sign. Hence, point (0,0) is an unstable saddle, as shown in Figures 7 and 8. For c 3 b 2 + c 1 > 0 , the eigenvalues γ 1 = i c 3 b 2 + c 1 and γ 2 = i c 3 b 2 + c 1 are imaginary, which provides a stable center, as shown in Figures 9 and 10. Hence, for different values of the parameter, the stability of the equilibrium point (0, 0) is moved from an unstable saddle to stable centers.

Figure 7 
               Phase portraits of Eq. (16) for b = 4, c
                  1 = −4, c
                  2 = 2, and c
                  3 = −2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.
Figure 7

Phase portraits of Eq. (16) for b = 4, c 1 = −4, c 2 = 2, and c 3 = −2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.

Figure 8 
               Phase portraits of Eq. (16) for b = 4, c
                  1 = −4, c
                  2 = 2, and c
                  3 = 2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.
Figure 8

Phase portraits of Eq. (16) for b = 4, c 1 = −4, c 2 = 2, and c 3 = 2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.

Figure 9 
               Phase portraits of Eq. (16) for b = 4, c
                  1 = −4, c
                  2 = −2, and c
                  3 = 2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.
Figure 9

Phase portraits of Eq. (16) for b = 4, c 1 = −4, c 2 = −2, and c 3 = 2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.

Figure 10 
               Phase portraits of Eq. (16) for b = 4, c
                  1 = −4, c
                  2 = −2, and c
                  3 = −2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.
Figure 10

Phase portraits of Eq. (16) for b = 4, c 1 = −4, c 2 = −2, and c 3 = −2. (a) trajectories with isoclines and nullclines, (b) corresponding outcomes for wave variable χ.

Case 2: Stability at ± c 3 c 2 , 0

Here, the roots of Eq. (18) are γ 1 = 2 c 3 b 2 + c 1 and γ 2 = 2 c 3 b 2 + c 1 . For c 3 b 2 + c 1 < 0 , the eigenvalues γ 1 = i 2 c 3 b 2 + c 1 and γ 2 = i 2 c 3 b 2 + c 1 are imaginary, and thus, the points ± c 3 c 2 , 0 are stable centers (refer to Figure 7). Moreover, if c 3 b 2 + c 1 > 0 , then the eigenvalues γ 1 = 2 c 3 b 2 + c 1 and γ 2 = 2 c 3 b 2 + c 1 are real with a reverse sign. Hence, the points ± c 3 c 2 , 0 are unstable saddles point (shown in Figure 9). Corresponding to the first case, for different values of the parameter, the stability is moved from stable centers to unstable saddles of the equilibrium point ± c 3 c 2 , 0 .

7 Multistability analysis

Next, we added the term P cos() as a perturbation in Eq. (16) to investigate the multistability of the system as follows:

(19) d X d χ = Y = h ( X ,   Y ) d Y d χ = c 2 b 2 + c 1 X 3 c 3 b 2 + c 1 X + P cos ( Q χ ) ,

where P and Q represent the intensity and frequency of the perturbation. Now, the multistability of Eq. (19) is discussed [48,49].

The model reveals a convincing ability to show multistability when it suffers perturbation. Under some definite parameter configurations with different primary conditions, a set of different simultaneous wave shapes, such as periodic, quasi-periodic, and chaotic behavior, can be found in this phenomenon. This phenomenon is displayed visually in Figure 11 for b = 1, c 2 = −3.3, c 1 = −2, c 3 = −2, P = 1.4, and Q = 3.9 and Figure 12 for b = 1, c 2 = −3.3, c 1 = −2, c 3 = −2, P = 3.1, and Q = 3.9, which explains the various situations of the model for different initial values. A periodic wave, shown in green color, is shown in Figure 11 for the initial value (−0.1, −0.1). In addition, by taking (0.4, 0.5) and (1.05, 0) as initial values, the blue and red plots of quasi-periodic shapes can also be seen in this figure. Considering (−0.1, −0.1) as an initial value, the green plot in Figure 12 depicts the periodic profile, whereas the blue and red colors in this figure show quasi-periodic and chaotic behaviors for (0.4, 0.5) and (1.05, 0), respectively.

Figure 11 
               Multistability of system (19) for b = 1, c
                  1 = −2, c
                  2 = −3.3, c
                  3 = −2, P = 1.4, and Q = 3.9. (a) 2D phase portrait and (b) Poincaré section.
Figure 11

Multistability of system (19) for b = 1, c 1 = −2, c 2 = −3.3, c 3 = −2, P = 1.4, and Q = 3.9. (a) 2D phase portrait and (b) Poincaré section.

Figure 12 
               Multistability of system (19) for b = 1, c
                  1 = −2, c
                  2 = −3.3, c
                  3 = −2, P = 3.1, and Q = 3.9. (a) 2D phase portrait and (b) Poincaré section.
Figure 12

Multistability of system (19) for b = 1, c 1 = −2, c 2 = −3.3, c 3 = −2, P = 3.1, and Q = 3.9. (a) 2D phase portrait and (b) Poincaré section.

8 Comparison

Akram and Arshed have scrutinized six wave outcomes of the KGF model using the generalized projective Riccati equation technique and obtained bright and dark solitons [40]. In addition, Alyousef and co-workers obtained bright soliton only by solving the KFG model using the fractional homotopy perturbation transform approach [50]. Moreover, the Kudryashov-expansion method has been used to solve the KFG equation by Alquran and his collaborators and they obtained 15 solutions with bright dark breather waves [51]. However, we have used unified and unified solver methods for the first time to solve the KFG equation model and obtained 42 solutions with bright soliton, dark soliton, kink and anti-kink waves, lump-type, and local breather waves, which are different and more effective than the above-mentioned studies.

9 Conclusion

The unified and unified solver techniques were effectively applied to the fractional KFG equation and we obtained some novel dynamical patterns. Therefore, these outcomes provide various soliton profiles: bright and dark solitons, kink and anti-kink waves with breather waves, lump-type breather waves, and local breather waves. In addition, 2D and 3D plots are drawn for these dynamic patterns. In addition, stability and multistability analysis are conducted for the proposed model to confirm the converging limitations of parameters, and chaotic and quasi-periodic profiles of this analysis are shown graphically. These rich mathematical structures of our solutions are used to describe the biological system, population dynamics, fluid flow, image processing, etc. We strongly believe that these novel dynamical patterns of the results can be used to progress different nonlinear models.

Acknowledgements

The authors extend their appreciation to Taif University, Saudi Arabia, for supporting this work (project number TU-DSPP-2024-46).

  1. Funding information: This research was funded by Taif University, Saudi Arabia (Project No. TU-DSPP-2024-46).

  2. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Conflict of interest: The authors state no conflict of interest.

  4. Data availability statement: All data are included within the manuscript.

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Received: 2024-07-01
Revised: 2024-08-01
Accepted: 2024-08-30
Published Online: 2024-10-19

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

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

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  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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