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Dynamic analysis, circuit realization, and its synchronization of a new chaotic hyperjerk system

  • Junhong Li EMAIL logo , Ning Cui , Huibin Wu and Lin He
Published/Copyright: July 17, 2025

Abstract

This article presents a new chaotic hyperjerk system by adding nonlinear term to an existing model. The dissipativity and invariance, equilibrium points, and their stability conditions, as well as the conditions for the existence of Hopf bifurcations at the equilibrium points, are analyzed. Meanwhile, we investigate the rich dynamical phenomena of the hyperjerk system, and the results show that the system exhibits chaos over a wide range of parameter variations and demonstrates complex dynamical characteristics such as periodic orbits, multi-periodic orbits, and quasi-periodic orbits under different parameter conditions. Furthermore, the chaotic synchronization, and circuit implementation of the hyperjerk system are also studied. Finally, the application of the hyperjerk system in chaotic encryption and decryption is discussed.

1 Introduction

Generally, the study of chaos theory is always based on a specific nonlinear system. Depending on various characteristics, many chaotic systems have been investigated by scholars, such as Duffing systems [1,2], Chen systems [3,4], Genesio systems [5,6], Chua systems [7,8], and Lorenz systems [9,10]. In 2000, Sprott proposed a general form of the jerk system [11], whose general expression is x = J ( x ¨ , x ˙ , x ) , where J is referred to as the jerk function. From physical point of view, x , x ˙ , and x ¨ denote the displacement, velocity, and acceleration, respectively. The jerk system has garnered the attention of many researchers due to the simplicity of its equation form and complex dynamical properties. Scholars have presented and studied various versions of the jerk model (see, e.g., [1214] and references therein). The 4D hyperjerk system can be defined in a form as x ( 4 ) = J ( x , x ¨ , x ˙ , x ) , where x ( 4 ) can be regarded as “snap” [15]. The hyperjerk system, as an extension of the jerk system, also possesses a simple algebraic structure in its equational expression, yet exhibits more complex dynamical characteristics compared to the jerk system. Vaidyanathan et al. [16] presented a new 4D chaotic hyperjerk system having two exponential nonlinearities. The study explored the dissipativity, equilibrium points, stability of the system, as well as its practical circuit implementation and engineering applications. Kaya and Salih [17] analyzed the security of a random number generator based on the 4D the study by Vaidyanathan et al. [16]. Jiang et al. [18] constructed a new 4D hyperjerk system with antimonotonicity and studied the bifurcations and chaos dynamics of the hyperjerk system. From these, it is evident that the new chaotic model is helpful for a more in-depth exploration of the essence and characteristics of the chaotic system. In addition, due to the high sensitivity of chaos to initial values, it also leads to the difficulty in controlling and predicting chaotic systems. In practical applications, the initial conditions cannot be completely and precisely controlled. Therefore, the research on chaotic synchronization is of great necessity. However, the research on the synchronization phenomenon of the hyperjerk system still needs to be further enriched [19]. Based on the aforementioned reasons, this article further expands the existing models (see previous studies [12,18]) and investigates the complex dynamic characteristics of the new chaotic system and the realization of chaotic synchronization. The circuit implementation of the new hyperjerk system is also studied. In addition, the application of the new chaotic hyperjerk system in information encryption and decryption was analyzed.

The rest of the article is organized as follows. In Section 2, the dissipativity and invariance, equilibria, and their stability of 4D hyperjerk system are discussed. The complex dynamical behaviors such as the exists of Hopf bifurcation and quasi-periodicity and chaos are also analyzed. The circuit realization, and chaos synchronization are introduced in Section 3 and 4, respectively. The chaotic encryption and decryption using the hyperjerk system are investigated in Section 5. The conclusions are summarized in Section 6.

2 Model and dynamical analysis

A new 4D chaotic hyperjerk system is considered in this article and is described as follows:

(1) x ˙ = y , y ˙ = z , z ˙ = a u , u ˙ = b x c z e y f u g x 3 g 0 x 2 u ,

where a , c , e , f , g , and g 0 are the positive parameters and b R . x , y , z , and u are the state variables. The hyperjerk system (1) can be represented as

x ( 4 ) + ( f + g 0 x 2 ) x + a c x ¨ + a e x ˙ + a g x 3 a b x = 0 .

The equation in [18] can be considered as a special case of the hyperjerk model (1) at b = 1 , e = 1 , and g 0 = 0 . The 4D hyperjerk system (1) will be transformed into the 3D jerk system in [12], when f = g = 1 , g 0 = 0 , and y = z .

2.1 Dissipativity and invariance

It can be seen that system (1) is invariant for the coordinate transformation

( x , y , z , u ) ( x , y , z , u ) .

Thus, the nonzero equilibria of (1) are symmetric with respect to origin. The divergence of the vector field of states of (1) is

V = x ˙ x + y ˙ y + z ˙ z + u ˙ u = f g 0 x 2 .

Thus, (1) is a dissipative chaotic system.

2.2 Equilibria and their stability

Obviously, (1) always has zero-equilibrium point P 0 = (0, 0, 0, 0), and the characteristic equation of Jacobi matrix at P 0 is

(2) f ( λ ) = λ 4 + f λ 3 + a c λ 2 + a e λ a b .

When b < 0 , the real parts of eigenvalues are negative if and only if

f c > e , c e f + b f 2 > a e 2 .

P 0 is locally asymptotically stable. When b > 0 , P 0 is unstable and system (1) has other two nonzero equilibrium points P 1,2 = ( ± b g , 0 , 0 , 0 ) . The characteristic equation of Jacobi matrix at P 1,2 is

(3) f ( λ ) = λ 4 + f + g 0 b g λ 3 + a c λ 2 + a e λ + 2 a b .

The real parts of eigenvalues are negative if and only if

g f c + g 0 b c > g e , ( f g + b g 0 ) ( a c e g 2 b g f 2 g 0 b 2 ) > a g 2 e 2

[20], then P 1,2 are locally asymptotically stable. Therefore, for system (1), one has

Theorem 1

  1. When f c > e , c e f + b f 2 > a e 2 , b < 0 , the zero equilibrium point P 0 is asymptotically stable. Otherwise, some roots of (2) have nonnegative real parts, and P 0 is unstable.

  2. When g f c + g 0 b c > g e , ( f g + b g 0 ) ( a c e g 2 b g f 2 g 0 b 2 ) > a g 2 e 2 , and b > 0 , the two nonzero equilibrium points P 1,2 symmetric with respect to the origin are asymptotically stable. Otherwise, some roots of (3) have nonnegative real parts, and P 1,2 is unstable.

2.3 Existence of Hopf bifurcations

Assume that system (1) has a pure imaginary root λ = i ω , ( ω R + ) . From (2), we obtain

ω 4 a c ω 2 a b = 0 , a e f ω 2 = 0 ,

then ω = a e f , c = c * = a e 2 b f 2 a f e .

Substituting c = c * into (2), we obtain

λ 1,2 = ± a e f i , λ 3,4 = f e ± e 2 f 2 + 4 b e f 2 e ,

where e f + 4 b > 0 , b < 0 . From (2), we have

Re ( λ ( c * ) ) λ = i ω = a 2 e 3 f 2 2 ( a 2 e 4 + 2 a b e 2 f 2 + b 2 f 4 a e 3 f 3 ) > 0 .

Thus, the first condition and second condition for a Hopf bifurcation [21] are satisfied. Hence, as c varies and passes through the critical value c * , (1) undergoes Hopf bifurcations at P 0 .

From (3), we obtain

ω = i a e g f g + b g 0 , c = c * = a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 + 2 b f 2 g 2 a ( b g 0 + f g ) g e .

Substituting c = c * into (3), we obtain

λ 1,2 = ± a e g f g + b g 0 i , λ 3,4 = b e g 0 e f g ± b 2 e 2 g 0 2 + 2 b e 2 f g g 0 + e 2 f 2 g 2 8 b 2 e g g 0 8 b e f g 2 2 e g ,

where, b e g 0 + f g e 8 b g > 0 . Furthermore,

Re ( λ ( c * ) ) λ = i ω = a 2 e 3 g 2 ( g 0 b + f g ) 2 2 [ a 2 e 4 g 4 e 2 g ( g 0 b + f g ) 2 ( b e g 0 + e f g + 4 b g ) a + 4 b 2 ( g 0 b + f g ) 4 ] > 0 .

Thus, Hopf bifurcation exists at nonzero-equilibrium point [21,22].

Next, we use the method described in [22] to calculate the first Lyapunov coefficients at P 0 and P 1,2 . When c = c * , the Jacobia matrix at point P 0 and its inverse matrix are

A 1 = 0 1 0 0 0 0 1 0 0 0 0 a b e a e 2 b f 2 a f e f , A 1 1 = e b a e 2 b f 2 a f e b f a b b 1 1 0 0 0 0 1 0 0 0 0 a 1 0 .

Through complex calculations, we obtain

η = i f e a e f i a e f e f 2 a e 2 b f 2 f e i a e f e f 2 a e 2 b f 2 i a i a e f e f 2 a e 2 b f 2 a e f 1 i a e f e f 2 a e 2 b f 2 , ξ = i b a e 2 2 a e f 1 2 e f i a e f e + b e 2 2 f i a e f 2 a e f 1 a e f 1 2 a e 2 ,

which satisfy A 1 η = i ω η , A 1 T ξ = i ω ξ , and < ξ , η > = 1 . Furthermore, one has the bilinear and trilinear functions in terms of η as

B ( η , η ) = B ( η , η ¯ ) = 0 0 0 0 , C ( η , η , η ¯ ) = 0 0 0 2 i a e f e g 0 3 f g i a e 2 + i b f 2 a e f e f 2 f 3 a ( a e 3 f 3 + a 2 e 4 + 2 a b e 2 f 2 + b 2 f 4 ) 2 a e f e 4 .

Therefore, the first Lyapunov coefficient at P 0 is

l 10 = 1 2 ω Re ( ξ , C ( η , η , η ¯ ) ) = f 4 a e f ( 3 f 3 g a e 2 g 0 b f 2 g 0 ) 2 a e 2 ( a e 3 f 3 + a 2 e 4 + 2 a b e 2 f 2 + b 2 f 4 ) 2 .

When c = c * = a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 + 2 b f 2 g 2 a ( b g 0 + f g ) g e , the Jacobia matrix at point P 1,2 and their inverse matrix are

A 2 = 0 1 0 0 0 0 1 0 0 0 0 a 2 b e c * b g 0 + f g g , A 2 1 = e 2 b c * 2 b b g 0 + f g 2 g a b 1 2 b 1 0 0 0 0 1 0 0 0 0 1 a 0 .

From A 2 θ = i ω θ , A 2 T ζ = i ω ζ , and ζ , θ = 1 , one has

θ = ( θ 11 , θ 21 , θ 31 , θ 41 ) T , ζ = ( ζ 11 , ζ 21 , ζ 31 , ζ 41 ) T ,

where

θ 11 = i ( b g 0 + f g ) θ 41 a e g b g 0 + f g e g , θ 21 = ( b g 0 + f g ) θ 41 e g , θ 31 = i a θ 41 a e g b g 0 + f g , θ 41 = i a e 2 g ( b g 0 + f g ) + a e g b g 0 + f g θ 0 a e g θ 0 2 b g 0 + f g a 2 e 4 g 2 ( b g 0 + f g ) 2 , θ 0 = a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 + 2 b f 2 g 2 , ζ 11 = i b a e 2 g 2 , ζ 21 = i 2 e g a e g b g 0 + f g ζ 0 , ζ 31 = 1 2 i a e g b g 0 + f g g + b g 0 + f g e 2 g a e g b g 0 + f g , ζ 41 = 1 2 a e g b g 0 + f g a e 2 g 2 , ζ 0 = 2 i b 2 g 0 + 2 i b f g a e g b g 0 + f g b e g 0 a e g b g 0 + f g e f g .

Therefore, we obtain

h 20 = ( 2 i ω E A 2 ) 1 B ( θ , θ ) = 0 , 0 , a h 20 * , 2 i a e g b g 0 + f g b g 0 g f h 20 * T , h 20 * = 2 b g ( b g 0 + f g ) h 201 2 3 a e g b g 0 + f g b 2 g 0 2 + 6 a e g b g 0 + f g b f g g 0 + 3 a e g b g 0 + f g f 2 g 2 + 2 i g 0 a e 2 g h 202 2 a e 3 a e g b g 0 + f g , h 201 = i a e 2 g ( b g 0 + f g ) + a e g b g 0 + f g ( 2 b f 2 g 2 a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 ) , h 202 = a e g ( a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 + 2 b f 2 g 2 ) 2 b g 0 + f g a 2 e 4 g 2 ( b g 0 + f g ) 2 , h 11 = A 2 1 B ( θ , θ ¯ ) = 3 b g ( b g 0 + f g ) 4 ) h 0 h 1 b e 4 g 2 a 2 a e g b g 0 + g f h 2 2 , 0 , 0 , 0 T , h 0 = i a e g b g 0 + f g e ( b g 0 + f g ) 2 + a e 2 g 2 2 b 3 g 0 2 4 b 2 f g g 0 2 b f 2 g 2 , h 1 = a e g b g 0 + f g ( 2 b f 2 g 2 a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 ) + i a b e 2 g g 0 + i a e 2 f g 2 , h 2 = ( 4 b 2 f 4 a e 3 f 3 + a 2 e 4 4 a b e 2 f 2 ) g 4 + ( 16 b 3 f 3 g 0 3 a b e 3 f 2 g 0 8 a b 2 e 2 f g 0 ) g 3 ( 3 a b 2 e 3 f g 0 2 + 4 a b 3 e 2 g 0 2 24 b 4 f 2 g 0 2 ) g 2 + ( 16 b 5 f g 0 3 a b 3 e 3 g 0 3 ) g + 4 b 6 g 0 4 ,

C ( θ , θ , θ ¯ ) = 2 ( b g 0 + f g ) 4 a e g b g 0 + f g ( 2 b f 2 g 2 a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 ) + i a b e 2 g g 0 + i a e 2 f g 2 2 c 0 a e g b g 0 + f g g 7 e 7 a 4 c 1 3 ,

c 0 = i a e g b g 0 + f g ( a e 3 g 2 g 0 3 a e 2 g 2 + 6 b 3 g 0 2 + 12 b 2 f g g 0 + 6 b f 2 g 2 ) ( b g 0 + f g ) 3 a e 2 g ( b g 0 + f g ) × [ ( 3 g 0 3 2 g g 0 3 ) b 3 + ( 9 f g g 0 2 4 f g 2 g 0 2 ) b 2 + ( 9 f 2 g 2 g 0 2 f 2 g 3 g 0 ) b + a e 2 g 3 g 0 + 3 f 3 g 3 , c 1 = 4 b 6 g 0 4 + 16 b 5 f g g 0 3 + 24 b 4 f 2 g 2 g 0 2 + ( 16 f 3 g 3 g 0 a e 3 g g 0 3 4 a e 2 g 2 g 0 2 ) b 3 ( 3 a e 3 f g 2 g 0 2 + 8 a e 2 f g 3 g 0 4 f 4 g 4 ) b 2 ( 3 a e 3 f 2 g 3 g 0 + 4 a e 2 f 2 g 4 ) b a e 3 f 3 g 4 + a 2 e 4 g 4 .

Then, the first Lyapunov coefficient at P 1,2 is

l 20 = 1 2 ω Re [ ζ , C ( θ , θ , θ ¯ ) 2 ζ , B ( θ , h 11 ) + ζ , B ( θ ¯ , h 20 ) ] = 1 2 e 3 g 2 a 2 ( b g 0 + f g ) 2 L 1 L 2 ,

where

L 1 = 18 f 5 g 8 + 90 b f 4 g 7 g 0 + ( 12 b f 4 g 0 6 a b e 2 f 3 g 0 12 b 2 f 5 g 0 + 180 b 2 f 3 g 0 2 6 a e 2 f 2 g 0 ) g 6 + ( 180 b 3 f 2 g 0 3 18 a b 2 e 2 f 2 g 0 2 60 b 3 f 4 g 0 2 12 a b e 2 f g 0 2 + 48 b 2 f 3 g 0 2 a e 2 f 2 g 0 + 2 b f 4 g 0 + 3 f 5 ) g 5 + ( 4 a b e 3 f 3 g 0 2 18 a b 3 e 2 f g 0 3 120 b 4 f 3 g 0 3 + 8 a 2 b e 4 g 0 2 16 a b 2 e 2 f 2 g 0 2 + 90 b 4 f g 0 4 6 a b 2 e 2 g 0 3 + 72 b 3 f 2 g 0 3 2 a b e 2 f g 0 2 + 8 b 2 f 3 g 0 2 + 15 b f 4 g 0 ) g 4 + ( 12 a b 2 e 3 f 2 g 0 3 6 a b 4 e 2 g 0 4 120 b 5 f 2 g 0 4 32 a b 3 e 2 f g 0 3 + 18 b 5 g 0 5 + 48 b 4 f g 0 4 a b 2 e 2 g 0 3 + 12 b 3 f 2 g 0 3 + 30 b 2 f 3 g 0 2 ) g 3 + ( 12 a b 3 e 3 f g 0 4 60 b 6 f g 0 5 16 a b 4 e 2 g 0 4 + 12 b 5 g 0 5 + 8 b 4 f g 0 4 + 30 b 3 f 2 g 0 3 ) g 2 + ( 4 a b 4 e 3 g 0 5 12 b 7 g 0 6 + 2 b 5 g 0 5 + 15 b 4 f g 0 4 ) g + 3 b 5 g 0 5 ,

L 2 = ( a e 3 f 3 + a 2 e 4 4 a b e 2 f 2 + 4 b 2 f 4 ) g 4 + ( 3 a b e 3 f 2 g 0 8 a b 2 e 2 f g 0 + 16 b 3 f 3 g 0 ) g 3 + ( 3 a b 2 e 3 f g 0 2 4 a b 3 e 2 g 0 2 + 24 b 4 f 2 g 0 2 ) g 2 + ( a b 3 e 3 g 0 3 + 16 b 5 f g 0 3 ) g + 4 b 6 g 0 4 .

Thus, we derive the following conclusions.

Theorem 2

(I) Suppose f e + 4 b > 0 , b < 0 . Therefore, when l 10 < 0 ( l 10 > 0 ), the Hopf bifurcation is supercritical (subcritical) and a stable (unstable) periodic orbit bifurcating from P 0 exists for sufficiently small 0 < c c * = c a e 2 b f 2 a f e .

(II) Suppose b e g 0 + f g e 8 b g > 0 , b > 0 . Therefore, when l 20 < 0 ( l 20 > 0 ), the Hopf bifurcation is supercritical (subcritical) and a stable (unstable) periodic orbit bifurcating from P 1,2 exists for sufficiently small 0 < c c * = c a e 2 g 2 + 2 b 3 g 0 2 + 4 b 2 f g g 0 + 2 b f 2 g 2 a ( b g 0 + f g ) g e .

Assume

a = 10 , b = 0.01 , f = 10 , e = 2 , g 0 = 0.01 , g = 0.01 ,

then as c varies and passes through the critical value c * = 0.205 , (1) undergoes Hopf bifurcations at P 0 . A bifurcation periodic solution exists for c = 0.20499 < c * . The corresponding Hopf periodic orbit with c = 0.20499 is given in Figure 1. Here, l 10 = 7.872 × 1 0 7 > 0 , then the Hopf bifurcation is subcritical and a unstable periodic orbit bifurcating from P 0 .

Figure 1 
                  Phase portraits of (1) in 
                        
                           
                           
                              y
                              −
                              z
                           
                           y-z
                        
                      plane and 
                        
                           
                           
                              z
                              −
                              u
                           
                           z-u
                        
                      plane, respectively.
Figure 1

Phase portraits of (1) in y z plane and z u plane, respectively.

2.4 Complex dynamical phenomena of hyperjerk system

In this section, some properties of (1) are investigated and the simulation results are further obtained by using numerical methods. In the following, we assume

a = 10.5 , b = 1.5 , c = 1.55 , e = 5 , f = 100 , g = 110 .

Figure 2 shows that the maximum Lyapunov exponent of system (1) is greater than zero as g 0 varies in [0.5, 100]. Therefore, chaos exists in the hyperjerk system over a large range of parameter variations. when g 0 = 0.5 , system (1) has unstable node-focus (0, 0, 0, 0) point and unstable saddle-focus points ( ± 3 220 , 0, 0, 0). The Lyapunov exponents are 0.04, 0.00, 0.20 , and 99.80 , Kaplan–Yorke dimension is 2.9984, and the hyperjerk system is chaotic. The chaotic attractors in x y plane and z u plane are depicted in Figures 3 and 4, respectively.

Figure 2 
                  Lyapunov spectrum with the variation of parameter 
                        
                           
                           
                              
                                 
                                    g
                                 
                                 
                                    0
                                 
                              
                              ∈
                              
                                 [
                                 
                                    0.5
                                    ,
                                    100
                                 
                                 ]
                              
                           
                           {g}_{0}\in \left[0.5,100]
                        
                     .
Figure 2

Lyapunov spectrum with the variation of parameter g 0 [ 0.5 , 100 ] .

Figure 3 
                  Chaotic attractor of (1) in 
                        
                           
                           
                              x
                              −
                              y
                           
                           x-y
                        
                      plane.
Figure 3

Chaotic attractor of (1) in x y plane.

Figure 4 
                  Chaotic attractor of (1) in 
                        
                           
                           
                              z
                              −
                              u
                           
                           z-u
                        
                      plane.
Figure 4

Chaotic attractor of (1) in z u plane.

The attractors in the 3D spaces ( x , y , z ) , ( y , z , u ) , ( x , z , u ) , and ( x , y , u ) are shown in Figures 5, 6, 7, 8, respectively. The power spectrum of time series y ( t ) and Poincaré mapping on the x y plane are given in Figures 9 and 10, respectively. Assume ( b , c , e , g , f , g 0 ) = ( 1.5 , 1.55 , 5 , 110 , 100 , 0.5 ) , Figure 11 indicates the bifurcation diagram of variables x , y , z , and u with a [ 0.5 , 15 ] . One can see that multi-windows and chaotic attractors can occur as a varies.

Figure 5 
                  Phase portrait of (1) on 
                        
                           
                           
                              x
                              −
                              y
                              −
                              z
                           
                           x-y-z
                        
                      space.
Figure 5

Phase portrait of (1) on x y z space.

Figure 6 
                  Phase portrait of (1) on 
                        
                           
                           
                              y
                              −
                              z
                              −
                              u
                           
                           y-z-u
                        
                      space.
Figure 6

Phase portrait of (1) on y z u space.

Figure 7 
                  Phase portrait of (1) on 
                        
                           
                           
                              x
                              −
                              z
                              −
                              u
                           
                           x-z-u
                        
                      space.
Figure 7

Phase portrait of (1) on x z u space.

Figure 8 
                  Phase portrait of (1) on 
                        
                           
                           
                              x
                              −
                              y
                              −
                              u
                           
                           x-y-u
                        
                      space.
Figure 8

Phase portrait of (1) on x y u space.

Figure 9 
                  Power spectrum of time series 
                        
                           
                           
                              y
                              
                                 (
                                 
                                    t
                                 
                                 )
                              
                           
                           y\left(t)
                        
                      for (1).
Figure 9

Power spectrum of time series y ( t ) for (1).

Figure 10 
                  Poincaré mapping on the 
                        
                           
                           
                              x
                              −
                              y
                           
                           x-y
                        
                      plane.
Figure 10

Poincaré mapping on the x y plane.

Figure 11 
                  Bifurcation diagram of system (1) with 
                        
                           
                           
                              a
                              ∈
                              
                                 [
                                 
                                    0.5
                                    ,
                                    15
                                 
                                 ]
                              
                           
                           a\in \left[0.5,15]
                        
                     .
Figure 11

Bifurcation diagram of system (1) with a [ 0.5 , 15 ] .

Here, multi-period windows of (1) occur when the parameter a varies in the intervals (13.072, 13.71). When a = 13.2 , the phase diagrams on x y plane and z u plane are shown in Figures 12 and 13, respectively.

Figure 12 
                  Phase diagram of (1) on 
                        
                           
                           
                              x
                              −
                              y
                           
                           x-y
                        
                      plane.
Figure 12

Phase diagram of (1) on x y plane.

Figure 13 
                  Phase diagram of (1) on 
                        
                           
                           
                              z
                              −
                              u
                           
                           z-u
                        
                      plane.
Figure 13

Phase diagram of (1) on z u plane.

When

( a , b , c , e , f , g , g 0 ) = ( 10,1,8.45,10,1,50,10 ) ,

(1) has unstable saddle-focus point ( 0 , 0 , 0 , 0 ) and stable node-focus points ( ± 1 50 , 0 , 0 , 0 ) . The Lyapunov exponents are 0.00 , 0.00 , 0.25 , and 0.93 ; system (1) is quasi-periodic. The corresponding quasi-periodic orbits in y z plane and z u plane are shown in Figures 14 and 15, respectively. Overall, it can be seen that the hyperjerk system (1) has rich and complex dynamical characteristics.

Figure 14 
                  Chaotic attractor of (1) in 
                        
                           
                           
                              x
                              −
                              y
                           
                           x-y
                        
                      plane.
Figure 14

Chaotic attractor of (1) in x y plane.

Figure 15 
                  Chaotic attractor of (1) in 
                        
                           
                           
                              z
                              −
                              u
                           
                           z-u
                        
                      plane.
Figure 15

Chaotic attractor of (1) in z u plane.

3 Chaos synchronization

Since Pecora and Carroll [23,24] first realized experiments on secure communication and information processing using chaotic synchronization, more and more researchers had a thorough research to chaos synchronization [2527]. In this section, chaos synchronization of the hyperjerk system will be investigated using a nonlinear feedback control. Let the drive system be (1), and the response system is

(4) x ˙ 1 = y 1 + δ 1 , y ˙ 1 = z 1 + δ 2 , z ˙ 1 = a u 1 + δ 3 , u ˙ 1 = b x 1 c z 1 e y 1 f u 1 g x 1 3 g 0 x 1 2 u 1 + δ 4 ,

where ( δ 1 , δ 2 , δ 3 , δ 4 ) T is the nonlinear controller to be designed. Subtracting system (1) from system (4), we obtain the error equations as follows:

(5) e ˙ 1 = e 2 + δ 1 , e ˙ 2 = e 3 + δ 2 , e ˙ 3 = a e 4 + δ 3 , e ˙ 4 = b e 1 c e 3 e e 2 f e 4 + δ 0 + δ 4

where

e 1 = x 1 x , e 2 = y 1 y , e 3 = z 1 z , e 4 = u 1 u , δ 0 = ( e 1 2 g 0 + 2 e 1 g 0 x 1 g 0 x 1 2 ) e 4 g e 1 3 + ( 3 g x 1 + g 0 u 1 ) e 1 2 + ( 3 g x 1 2 2 g 0 u 1 x 1 ) e 1 .

Choose the Lyapunov function V = 1 2 i = 1 4 e i , the time derivative of V along the trajectory of (5) is

V ˙ = ( e 1 2 g 0 + 2 e 1 g 0 x 1 g 0 x 1 2 f ) e 4 2 + ( g e 1 3 + 3 g e 1 2 x 1 3 g e 1 x 1 2 + g 0 u 1 e 1 2 2 g 0 u 1 x 1 e 1 + a e 3 + b e 1 c e 3 e e 2 + δ 4 ) e 4 + δ 1 e 1 + δ 2 e 2 + δ 3 e 3 + e 1 e 2 + e 2 e 3 .

Therefore, if we choose δ i , ( i = 1 , 2 , 3 , 4 ) as follows:

δ 1 = e 1 2 e 4 g ( 3 g x 1 + g 0 u 1 ) e 4 e 1 e 1 , δ 2 = e e 4 e 2 , δ 3 = ( c a ) e 4 e 3 , δ 4 = 2 g 0 x 1 e 1 e 4 ( 3 g x 1 2 2 g 0 u 1 x 1 + b ) e 1 ,

then

V ˙ = e 1 2 e 4 2 g 0 e 4 2 g 0 x 1 2 f e 4 2 e 1 2 + e 1 e 2 e 2 2 + e 2 e 3 e 3 2 f e 4 2 e 1 2 + e 1 e 2 e 2 2 + e 2 e 3 e 3 2 = ( e 1 , e 2 , e 3 , e 4 ) C ( e 1 , e 2 , e 3 , e 4 ) T ,

where

C = 1 1 2 0 0 1 2 1 1 2 0 0 1 2 1 0 0 0 0 f .

Obviously, C is negative definite. Hence, the states of drive system (1) and response system (4) are globally synchronized asymptotically. The phase planes of system (4) in x 1 y 1 plane and z 1 u 1 plane are depicted in Figure 16. Dynamics of synchronization errors ( e 1 , e 2 ) and ( e 3 , e 4 ) for drive system and response system are given in Figures 17 and 18, respectively. From these figures, one can see that the synchronization errors converge to zero and the two systems of (1) and (4) do indeed achieve synchronization of chaos.

Figure 16 
               Phase portraits of (4) in 
                     
                        
                        
                           
                              
                                 x
                              
                              
                                 1
                              
                           
                           −
                           
                              
                                 y
                              
                              
                                 1
                              
                           
                        
                        {x}_{1}-{y}_{1}
                     
                   plane and 
                     
                        
                        
                           
                              
                                 z
                              
                              
                                 1
                              
                           
                           −
                           
                              
                                 u
                              
                              
                                 1
                              
                           
                        
                        {z}_{1}-{u}_{1}
                     
                   plane, respectively.
Figure 16

Phase portraits of (4) in x 1 y 1 plane and z 1 u 1 plane, respectively.

Figure 17 
               Synchronization errors 
                     
                        
                        
                           
                              
                                 e
                              
                              
                                 1
                              
                           
                        
                        {e}_{1}
                     
                   and 
                     
                        
                        
                           
                              
                                 e
                              
                              
                                 2
                              
                           
                        
                        {e}_{2}
                     
                   versus time.
Figure 17

Synchronization errors e 1 and e 2 versus time.

Figure 18 
               Synchronization errors 
                     
                        
                        
                           
                              
                                 e
                              
                              
                                 3
                              
                           
                        
                        {e}_{3}
                     
                   and 
                     
                        
                        
                           
                              
                                 e
                              
                              
                                 4
                              
                           
                        
                        {e}_{4}
                     
                   versus time.
Figure 18

Synchronization errors e 3 and e 4 versus time.

4 Circuit realization

From the aforementioned analysis, we can see that the new hyperjerk system can exhibit complex dynamical behaviors. The hardware implementation of theoretical chaotic models is an important topic in practical applications, such as circuit realization [2830]. This section presents a suitable electronic circuit that emulates the proposed system (1). Figure 19 presents the schematic of the circuit that emulates system (1). Here, each of the four channels corresponds to one of the four variables x , y , z , and u , respectively.

Figure 19 
               Electronic circuit implementation of 4D hyperjerk system (1).
Figure 19

Electronic circuit implementation of 4D hyperjerk system (1).

The circuit equations are presented as follows:

(6) C 1 d x d τ = R 2 R 1 R 3 y , C 2 d y d τ = R 7 R 6 R 8 z , C 3 d z d τ = R 12 R 11 R 13 u , C 4 d u d τ = R 016 R 22 R 16 x R 016 R 10 R 19 R 16 R 9 y R 016 R 15 R 20 R 16 R 14 z R 016 R 24 R 21 R 16 R 23 u R 016 R 5 R 19 R 16 R 4 x 3 R 016 R 24 R 18 R 23 u x 2 ,

where U i ( i = 1 , 2 , , 12 ) are implemented with the operational amplifier LM675T. The electronic components values have been selected as follows:

R 1 = R 2 = 50 K Ω , R 3 = R 8 = R 11 = R 13 = R 16 = R = 1 K Ω , C 1 = C 2 = C 3 = C 4 = C = 0.1 μ F , R 4 = R 5 = R 6 = R 7 = R 9 = R 10 = R 14 = R 15 = R 23 = R 24 = 10 K Ω , R 12 = 10.5 K Ω , R 20 = 66 K Ω , R 17 = 0.93 K Ω , R 18 = 204.6 K Ω , R 19 = 20.46 K Ω , R 21 = 1.023 K Ω , R 22 = 68.2 K Ω , R 016 = 102.3 K Ω .

The power supplies of all active devices are ± 11 V and the experimental time τ = R C t . A i , ( i = 1 , 2 , 3 , 4 ) are analog multipliers with gain of one. For these chosen components, the system’s (1) parameters are as follows:

a = 10.5 , b = 1.5 , c = 1.55 , e = 5 , f = 100 , g = 110 , g 0 = 0.5 .

Figure 20 depicts the experimental observation of circuit’s chaotic phenomena in x y plane (left) and z u plane (right), respectively. Compared to Figures 3 and 4, one can see that a good agreement between the numerical simulation and the experimental realization is obtained.

Figure 20 
               Experimental observation of circuit’s chaotic phenomena in different phase portraits.
Figure 20

Experimental observation of circuit’s chaotic phenomena in different phase portraits.

5 Chaotic encryption and decryption

Due to the complexity and unpredictability of chaotic systems, chaotic encryption provides a new technical approach for information communication security and has achieved very good results, such as previous studies [2931]. In this section, taking the sine function as an example, the application of the modified new chaotic hyperjerk system in encryption is illustrated.

Figure 21 indicates the time domain waveforms of the new chaotic hyperjerk system state variables x , y , z , and u . Here, we set the hyperjerk system parameters as a = 10.5 , b = 1.5 , c = 1.55 , e = 5 , f = 100 , g = 110 , g 0 = 90 , and the initial values as ( 0.01 , 0.01 , 0.01 , 0.092 ) . During the encryption of the sine sequence, to ensure that the chaotic sequence can mask the plaintext signal and prevent noise from overwhelming or information leakage, the dynamic range of the chaotic sequence used for encryption must cover or modulate the amplitude of the sine sequence. As shown in Figure 21, x has a larger numerical variation range, which facilitates maintaining a uniform distribution when quantizing it into the integer range. Additionally, the higher-order terms in (1) make x more difficult to predict than other variables. Thus, to ensure strong randomness and high security of the chaotic sequence during encryption, we select the chaotic sequence generated by the state variable x for encrypting the sine sequence. Figure 22 shows the principles of encryption and decryption using the new chaotic hyperjerk system (1). The first row is using chaos to encrypt the sine signal. The specific encryption process is as follows: (I) a sine sequence is generated as the plaintext to be encrypted using the equation S = sin ( 2 π h t ) , where the time t [ 0 , 1 ] , the sequence length is 3,000, and the sine wave frequency h = 10 Hz ; (II) normalize the sine signal from [ 1 , 1 ] to [ 0 , 255 ] , and the mapping equation is S 1 = round ( ( S + 1 ) × 127.5 ) ; (III) the new chaotic hyperjerk system is discretized using the fourth-order Runge–Kutta method, and x is extracted as the signal for encryption. Furthermore, the chaotic sequence C = mod ( [ x × 1 0 5 ] , 256 ) is generated. Here, we select the same parameter values and initial conditions as those in Figure 21; (IV) both S 1 and C are converted to the unit8 type, and then the sine sequence is encrypted through the XOR encryption algorithm C S 1 to generate the ciphertext S E ; (V) transmit the ciphertext. The second row is using chaos for decryption. The specific decryption process is as follows: (P1) generate a chaotic sequence C d identical to that in (III); (P2) receive the ciphertext S E ; (P3) decrypt S E using the XOR algorithm C d S E to obtain the signal sequence D E ; (P4) use the inverse mapping to obtain the plaintext S D = D E 127.5 1 ; (P5) output the decrypted signal sequence S D . The effect of chaotic encryption and decryption using the hyperjerk system is shown in Figure 23. It can be seen that the encrypted chaotic sequence effectively conceals the original sequence data, and the decrypted sequence is highly consistent with the original sequence.

Figure 21 
               Time domain waveform of the state variables 
                     
                        
                        
                           x
                           ,
                           y
                           ,
                           z
                        
                        x,y,z
                     
                  , and 
                     
                        
                        
                           u
                        
                        u
                     
                  .
Figure 21

Time domain waveform of the state variables x , y , z , and u .

Figure 22 
               Principle diagram of chaos encryption and decryption.
Figure 22

Principle diagram of chaos encryption and decryption.

Figure 23 
               Chaotic encryption and decryption using the hyperjerk system.
Figure 23

Chaotic encryption and decryption using the hyperjerk system.

6 Conclusions

Based on the model in Jiang et al. [18], this article reports a new chaotic hyperjerk system by adding nonlinear term. The models in Jiang et al. [18] and Elsonbaty et al. [12] can be seen as special cases of the proposed model. The results of the study show that the system is a dissipative system symmetric with respect to the origin. When b < 0 , the system has only one zero equilibrium point; when b > 0 , the system exhibits two nonzero equilibrium points, which are symmetric about the origin. Hopf bifurcations occur at these equilibrium points under certain conditions. Simulation results indicate that the system exhibits various complex dynamical phenomena under different parameter conditions, including periodic orbits, multi-periodic orbits, quasi-periodic orbits, and chaotic attractors. This article not only generalizes the models in existing references and discovers new complex dynamical phenomena, but also achieves chaotic synchronization by selecting appropriate nonlinear controllers and realizes the chaotic hyperjerk system using electronic components. Moreover, it explores the practical application of the new hyperjerk system in chaotic encryption and decryption, with good results.

Acknowledgments

The project was supported by the University Characteristic Innovation Project of Guangdong Province (No. 2023KTSCX079) and by the Doctoral Scientific Research Foundation of Hanshan Normal University (No. QD202130).

  1. Funding information: The authors state no funding involved.

  2. Author contributions: Junhong Li – original draft; Ning Cui – review and editing; Huibin Wu and Lin He – supervision. 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 generated or analyzed during this study are included in this published article.

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Received: 2025-01-25
Revised: 2025-05-04
Accepted: 2025-05-06
Published Online: 2025-07-17

© 2025 the author(s), published by De Gruyter

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

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