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Article

PSD and Cross-PSD of Responses of Seven Classes of Fractional Vibrations Driven by fGn, fBm, Fractional OU Process, and von Kármán Process

1
Ocean College, Zhejiang University, Zhoushan 316021, China
2
East China Normal University, Shanghai 200062, China
Symmetry 2024, 16(5), 635; https://doi.org/10.3390/sym16050635
Submission received: 11 April 2024 / Revised: 6 May 2024 / Accepted: 8 May 2024 / Published: 20 May 2024
(This article belongs to the Special Issue Symmetry in the Advanced Mechanics of Systems)

Abstract

:
This paper gives its contributions in four stages. First, we propose the analytical expressions of power spectrum density (PSD) responses and cross-PSD responses to seven classes of fractional vibrators driven by fractional Gaussian noise (fGn). Second, we put forward the analytical expressions of PSD and cross-PSD responses to seven classes of fractional vibrators excited by fractional Brownian motion (fBm). Third, we present the analytical expressions of PSD and cross-PSD responses to seven classes of fractional vibrators driven by the fractional Ornstein–Uhlenbeck (OU) process. Fourth, we bring forward the analytical expressions of PSD and cross-PSD responses to seven classes of fractional vibrators excited by the von Kármán process. We show that the statistical dependences of the responses to seven classes of fractional vibrators follow those of the excitation of fGn, fBm, the OU process, or the von Kármán process. We also demonstrate the obvious effects of fractional orders on the responses to seven classes of fractional vibrations. In addition, we newly introduce class VII fractional vibrators, their frequency transfer function, and their impulse response in this research.

1. Introduction

We start with three topics in the field, as follows. First, the topic of fractional vibrations attracts the interests of researchers; see, e.g., Uchaikin [1], Achar et al. [2,3,4], Duan [5], Coccolo et al. [6], Sidorov et al. [7], Pirrotta et al. [8,9], Lewandowski and Wielentejczyk [10], Spanos and Malara [11], Blaszczyk [12], Blaszczyk and Ciesielski [13], Blaszczyk et al. [14,15], Al-Rabtah et al. [16], Zurigat [17], Rossikhin and Shitikova [18,19,20,21], Rossikhin [22], Shitikova et al. [23], Shitikova [24,25], El-Nabulsi et al. [26], Banerjee [27], Sofi [28], Sofi and Muscolino [29], Molina-Villegas et al. [30], Parovik [31], Li et al. [32,33], Li [34,35,36], and references therein, to mention a few.
Second, the topic of fractional processes remains in the interest of researchers; see, e.g., Mandelbrot [37,38], Beran [39], Levy-Vehel and Lutton [40], Lévy-Véhel and Rams [41], Bender et al. [42], Guével and Lévy-Véhel [43], Lebovits et al. [44], Corlay et al. [45], Ayache et al. [46], Park et al. [47], Luks and Xiao [48], Li and Xiao [49], Flandrin [50,51], Zao et al. [52], Borgnat et al. [53,54], Salcedo-Sanz et al. [55], Levin et al. [56], Marković and Gros [57], Eliazar and Shlesinger [58], Campa et al. [59], Pinchas and Avraham [60,61], Mirás-Avalos et al. [62], Kaulakys et al. [63], Lubashevsky [64], Starchenko [65], Gorev et al. [66], Sheluhin et al. [67], Sousa-Vieira and Fernández-Veiga [68], Beskardes et al. [69], Ercan and Kavvas [70], Lee et al. [71], Li [72,73,74], to cite a few.
The third topic concerns fractional equation-driven fractional random functions; see, e.g., Li and Yan [75], Gao et al. [76], Guo et al. [77], Gao and Sun [78], Pei and Zhang [79], Barth and Stüwe [80], Kim and Park [81], Noupelah et al. [82], Massing [83], Lee [84], Fa et al. [85], Freundlich and Sado [86], Burlon [87], Wang et al. [88], Hu and Zhou [89], and Liu et al. [90], to simply mention a few. However, reports regarding the analytical expressions of the responses of seven classes of fractional vibrators (see the next Section) driven by fractional processes (fractional Gaussian noise (fGn), fractional Brownian motion (fBm), the fractional Ornstein–Uhlenbeck (OU) process, and the von Kármán process) are rarely seen. This paper aims at bringing forward the analytical expressions of the power spectrum density (PSD) and cross-PSD responses to seven classes of fractional vibrators driven by those fractional processes.
The rest of the paper is organized as follows. In Section 2, we explain the motion equations of seven classes of fractional vibrators, their frequency transfer functions, and their impulse response functions. In Section 3, Section 4, Section 5 and Section 6, we put forward the analytical expressions of the response to seven classes of fractional vibrators driven by fGn, fBm, the fractional OU process, and the von Kármán process, respectively. Discussions and conclusions are given in Section 7.

2. Seven Classes of Fractional Vibrators

The author’s previous work (Li [34]) addressed the first three classes of fractional vibrations in this paper. Further, Li [35,36] discusses the first six classes of fractional vibrations in this paper. The seventh class of fractional vibrators, as shown below, as well as their frequency transfer functions and impulses, are newly introduced in this research.

2.1. Motion Equations

Let m, c, and k be the primary mass, damping, and stiffness of a vibration system, respectively. We refer to a class I fractional vibrator when its motion equation is, for 0 < α < 3, in the form
m d α x 1 ( t ) d t α + k x 1 ( t ) = f ( t ) .
A system is called a class II fractional vibrator when its motion equation is, for 0 < β < 2, given by
m d 2 x 2 ( t ) d t 2 + c d β x 2 ( t ) d t β + k x 2 ( t ) = f ( t ) .
We call a system class III fractional vibrator if its motion equation is, for 0 < α < 3 and 0 < β < 2, expressed by
m d α x 3 ( t ) d t α + c d β x 3 ( t ) d t β + k x 3 ( t ) = f ( t ) .
We term a system a class IV fractional vibrator if its motion equation is, for 0 < α < 3 and 0 ≤ λ < 1, represented by
m d α x 4 ( t ) d t α + k d λ x 4 ( t ) d t λ = f ( t ) .
A system is called a class V fractional vibrator if its motion equation is, for 0 ≤ λ < 1, expressed by
m d 2 x 5 ( t ) d t 2 + k d λ x 5 ( t ) d t λ = f ( t ) .
We call a system a class VI fractional vibrator if its motion equation is, for 0 < α < 3, 0 < β < 2 and 0 ≤ λ < 1, in the form
m d α x 6 ( t ) d t α + c d β x 6 ( t ) d t β + k d λ x 6 ( t ) d t λ = f ( t ) .
A system is called a class VII fractional vibrator when its motion equation is, for 0 < β < 2 and 0 ≤ λ < 1, given by
m d 2 x 7 ( t ) d t 2 + c d β x 7 ( t ) d t β + k d λ x 7 ( t ) d t λ = f ( t ) .

2.2. Frequency Transfer Functions

Theorem 1. 
Let F(ω) be the Fourier transform. Let Xj(ω) be the Fourier transform of the jth class response xj(t) (j = 1, 2, …, 7). Let Hj(ω) be the frequency transfer function of a fractional vibrator of the jth class. Then,  H j ( ω ) = X j ( ω ) F ( ω ) .  For j = 1,
H 1 ( ω ) = 1 k + ( i ω ) α m .
If j = 2,
H 2 ( ω ) = 1 k ω 2 m + ( i ω ) β c .
When j = 3,
H 3 ( ω ) = 1 k + ( i ω ) α m + ( i ω ) β c .
For j = 4,
H 4 ( ω ) = 1 ( i ω ) α m + ( i ω ) λ k .
When j = 5,
H 5 ( ω ) = 1 ω 2 m + ( i ω ) λ k .
If j = 6,
H 6 ( ω ) = 1 ( i ω ) α m + ( i ω ) β c + ( i ω ) λ k .
For j = 7, we have
H 7 ( ω ) = 1 ω 2 m + ( i ω ) β c + ( i ω ) λ k .
Proof. 
Solving the Fourier transforms on both sides of (1)–(7) produces (8)–(14), respectively. The proof is finished. □
Corollary 1. 
Let ωn be the primary damping free natural angular frequency. Let ζ be the primary damping ratio. Denote the primary frequency ratio with γ. Then, Hj(ω) (j = 1, 2, …, 7) can be expressed in the following forms. If j = 1,
H 1 ( ω ) = 1 k 1 ω α ω n 2 cos α π 2 + i ω α ω n 2 sin α π 2 .
For j = 2,
H 2 ( ω ) = 1 / k 1 γ 2 1 c m ω β 2 cos β π 2 + i 2 ς ω β sin β π 2 ω n .
When j = 3,
H 3 ( ω ) = 1 / k 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 .
For j = 4,
H 4 ( ω ) = 1 k ω λ cos λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 + i 2 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 .
If j = 5,
H 5 ( ω ) = 1 k ω λ cos λ π 2 1 γ 2 ω λ cos λ π 2 + i 2 γ k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 .
When j = 6,
H 6 ( ω ) = 1 k ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 .
For j = 7,
H 7 ( ω ) = 1 k ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 + i γ 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 .
Proof. 
Taking into account the principal branch of iα or iβ or iλ, (8)–(14) can be expressed by (15)–(21), respectively. This finishes the proof. □

2.3. Impulse Response Functions

Theorem 2. 
Let hj(t) be the impulse response function of the fractional vibrator of the jth class (j = 1, 2, …, 7). Then, when j = 1,
h 1 ( t ) = e ω sin α π 2 2 cos α π 2 t sin ω n ω α 2 cos α π 2 1 ω 2 α sin 2 α π 2 4 ω n 2 cos α π 2 t m ω n ω α 2 cos α π 2 1 ω 2 α sin 2 α π 2 4 ω n 2 cos α π 2 u ( t ) ,
where u(t) is the unit step function. For j = 2,
h 2 ( t ) = e ς ω n ω β 1 sin β π 2 1 c m ω β 2 cos β π 2 t sin ω n 1 ς 2 ω 2 ( β 1 ) sin 2 β π 2 1 c m ω β 2 cos β π 2 1 c m ω β 2 cos β π 2 t ω n m 1 c m ω β 2 cos β π 2 1 ς 2 ω 2 ( β 1 ) sin 2 β π 2 1 c m ω β 2 cos β π 2 u ( t ) .
If j = 3,
h 3 ( t ) = = 1 m e m ω α 1 sin α π 2 + c ω β 1 sin β π 2 2 m ω α 2 cos α π 2 + c ω β 2 cos β π 2 t ω n m ω α 2 cos α π 2 + c ω β 2 cos β π 2 1 ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 2 4 ω n 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 2 sin ω n 1 ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 2 4 ω n 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 2 ω α 2 cos α π 2 + c m ω β 2 cos β π 2 t u ( t ) .
When j = 4,
h 4 ( t ) = e m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω λ cos λ π 2 ω α 2 cos α π 2 ω n t ω n m ω α 2 cos α π 2 ω λ cos λ π 2 1 m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 2 sin ω n ω λ cos λ π 2 ω α 2 cos α π 2 1 m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 2 t u ( t ) .
For j = 5,
h 5 ( t ) = e k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 ω λ cos λ π 2 ω n t sin ω n ω λ cos λ π 2 1 k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 2 t u ( t ) m ω n ω λ cos λ π 2 1 k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 2 .
If j = 6,
h 6 ( t ) = e ς eq 6 ω eqn 6 t 1 m eq 6 ω eqd 6 sin ω eqd 6 t u ( t ) ,
where
m eq 6 = m eq 3 = m ω α 2 cos α π 2 + c ω β 2 cos β π 2 , ς eq 6 = m ω α 1 sin α π 2 + c ω β 1 sin β π 2 + k ω λ 1 sin λ π 2 2 m ω α 2 cos α π 2 + c ω β 2 cos β π 2 k ω λ cos λ π 2 , ω eqd 6 = k ω λ cos λ π 2 m ω α 2 cos α π 2 + c ω β 2 cos β π 2 1 m ω α 1 sin α π 2 + c ω β 1 sin β π 2 + k ω λ 1 sin λ π 2 2 m ω α 2 cos α π 2 + c ω β 2 cos β π 2 k ω λ cos λ π 2 2 .
When j = 7, we have
h 7 ( t ) = e ς eq 7 ω eqn 7 t 1 m eq 7 ω eqd 7 sin ω eqd 7 t , t 0 ,
where
m eq 7 = m c ω β 2 cos β π 2 ,         ς eq 7 = c ω β 1 sin β π 2 + k ω λ 1 sin λ π 2 2 m c ω β 2 cos β π 2 k ω λ cos λ π 2 , ω eqn 7 = k ω λ cos λ π 2 m c ω β 2 cos β π 2 ,         ω eqd 7 = k ω λ cos λ π 2 m c ω β 2 cos β π 2 1 c ω β 1 sin β π 2 + k ω λ 1 sin λ π 2 2 m c ω β 2 cos β π 2 k ω λ cos λ π 2 2 .
Proof. 
Solving the inverse Fourier transforms of (15)–(21) yields (22)–(28), respectively. The proof is finished. □

3. PSD and Cross-PSD Responses to Seven Classes of Fractional Vibrations Driven by fGn

This section describes the contributions in three sections. First, we present the analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibration systems driven by fGn. Second, we show that the orders of fractional vibrators have considerable effects on the responses. Lastly, we show that the statistical dependences of the responses follow those of fGn.

3.1. Background

The literature regarding systems driven by fractional Gaussian noise (fGn) is quite rich; see, e.g., Wang et al. [88], Hu and Zhou [89], and Liu et al. [90]. However, closed-form expressions of PSD and cross-PSD responses to the excitation of fGn regarding seven classes of fractional vibration systems are seldom seen. This section demonstrates the closed-form expressions of PSD and cross-PSD responses to seven classes of fractional vibration systems driven by fGn.
The rest of the section is organized as follows. In Section 3.2, Section 3.3, Section 3.4, Section 3.5, Section 3.6, Section 3.7 and Section 3.8, we present the closed-form expressions of PSD and cross-PSD responses to fractional vibration systems from classes I to VII under the excitation of fGn. A summary is given in Section 3.9.

3.2. Responses of Class I Fractional Vibrators Driven by fGn

3.2.1. Computations

Let x1(t) be the response of a class I fractional vibrator driven by f(t) of fGn. Let Sff(ω) be the PSD of f(t). Then,
S f f ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H ,
where H ∈ (0, 1) is the Hurst parameter and
V H = Γ ( 1 2 H ) cos π H π H
is the strength of fGn (Li and Lim [91]). Figure 1 indicates some plots of Sff(ω).
Theorem 3 (PSD response I). 
Denote the PSD of x1(t) with Sxx1(ω). Then,
S x x 1 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k 2 1 ω α ω n 2 cos α π 2 2 + ω α ω n 2 sin α π 2 2 .
Proof. 
Note that Sxx1(ω) = Sff(ω)|H1(ω)|2. Thus, Theorem 3 is the result. The proof is finished. □
Theorem 4 (cross-PSD response I). 
Let Sfx1(ω) be the cross-PSD between f(t) of fGn and x1(t). Then,
S f x 1 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k 1 ω α ω n 2 cos α π 2 + i ω α ω n 2 sin α π 2 .
Proof. 
Solving the operation of (33) below
Sfx1(ω) = Sff(ω)H1(ω)
yields (32). This finishes the proof. □
In the time domain, the autocorrelation function (ACF) response, denoted by rxx1(τ), is given by
rxx1(τ) = rff(τ) * h1(τ) * h1(−τ).
In (34), rff(τ) is the inverse Fourier transform of Sff(ω). Denote the cross-correlation response between f(t) of fGn and x1(t) with rfx1(τ). Then,
rfx1(τ) = rff(τ) * h1(τ).
In (35), rfx1(τ) is the inverse Fourier transform of Sfx1(ω).

3.2.2. Effects of α on Responses

Figure 2 indicates some plots of |H1(ω)|2. Some plots of Sxx1(ω) are shown in Figure 3.
When α = 2, a class I fractional vibrator reduces to be a conventional damping-free vibrator. Note that H has considerable effects on the responses; see Figure 4.
In Figure 5, we illustrate some plots of Sfx1(ω).
According to the generation method of fractional time series (Li [70], Li and Chi [92]), we illustrate some plots of driven fGn and response ones in Figure 6. From Figure 6, we can see that there are noticeable effects of the fractional order α on the responses of class I fractional vibration systems driven by fGn.

3.3. Responses of Class II Fractional Vibrators Driven by fGn

3.3.1. Computation Methods

Theorem 5 (PSD response II). 
Denote with x2(t) the response to a class II fractional vibrator driven by f(t) of fGn. Let Sxx2(ω) be the PSD of x2(t). Then,
S x x 2 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k 2 1 γ 2 1 c m ω β 2 cos β π 2 2 + 2 ς ω β ω n sin β π 2 2 .
Proof. 
Let Sff(ω) be the PSD of f(t) of fGn. Considering the operation of (37),
Sxx2(ω) = Sff(ω)|H2(ω)|2
produces (36). The proof is complete. □
Theorem 6 (cross-PSD response II). 
Denote with Sfx2(ω) the cross-PSD between f(t) of fGn and x2(t). Then,
S f x 2 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k 1 γ 2 1 2 ς ω n ω β 2 cos β π 2 + i 2 ς ω β ω n sin β π 2 .
Proof. 
Solving the operation in (39)
Sfx2(ω) = Sff(ω)H2(ω)
yields (38). The proof ends. □
Denote the ACF response with rxx2(τ). It is the inverse Fourier transform of Sxx2(ω). It is expressed by
rxx2(τ) = rff(τ) * h2(τ) * h2(−τ).
In (40), rff(τ) is the ACF of f(t) of fGn. The cross-correlation response between f(t) of fGn and x2(t), denoted by rfx2(τ), is
rfx2(τ) = rff(τ) * h2(τ).
In (41), rfx2(τ)is the inverse Fourier transform of Sfx2(ω).

3.3.2. Effects of β on Responses

Some plots of |H2(ω)|2 are indicated in Figure 7. Figure 8 shows some plots of PSD response Sxx2(ω). Figure 9 shows a resonance curve when β = 1. Figure 10 illustrates some plots of the cross-PSD response of Sfx2(ω).
There are effects of the fractional order β on the responses of class II fractional vibration systems driven by fGn. Figure 11 exhibits the effects of β on the fluctuation range of the response x2(t).

3.4. Responses of Class III Fractional Vibrators Driven by fGn

3.4.1. Computations

Theorem 7 (PSD response III). 
Let x3(t) be the response to a class III fractional vibrator driven by f(t) of fGn. Let Sxx3(ω) be the PSD of x3(t). Then,
S x x 3 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k 2 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 + γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 .
Proof. 
Considering the operation of (43),
Sxx3(ω) = Sff(ω)|H3(ω)|2
results in (42). The proof is finished. □
Theorem 8 (cross-PSD response III). 
Let Sfx3(ω) be the cross-PSD between the excitation of f(t) of fGn and x3(t). Then,
S f x 3 ( ω ) = k 1 V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 .
Proof. 
Performing Sfx3(ω) = Sff(ω)H3(ω) produces (44). The proof is complete. □
Let rxx3(τ) be the ACF of x3(t). It is expressed by
rxx3(τ) = rff(τ) * h3(τ) * h3(−τ).
In (45), rxx3(τ) is the ACF response of a class III fractional vibrator driven by fGn. Denote with rfx3(τ) the cross-correlation between the excitation f(t) of fGn and x3(t). Then,
rfx3(τ) = rff(τ) * h3(τ).
In (46), rfx3(τ) is the cross-correlation response of a class III fractional vibrator driven by fGn.

3.4.2. Effects of α and β on Responses

Some plots of |H3(ω)|2 are shown in Figure 12. Figure 13 indicates some plots of Sxx3(ω). Some plots of Sfx3(ω) are indicated in Figure 14. Figure 13 and Figure 14 show that there are significant effects of (α, β) on the responses of a class III fractional vibrator driven by fGn.

3.5. Responses of Class IV Fractional Vibrators Driven by fGn

3.5.1. Computations

Theorem 9 (PSD response IV). 
Let x4(t) be the response to a class IV fractional vibrator excited by f(t) of fGn. Let Sxx4(ω) be the PSD of x4(t). Then,
S x x 4 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 + 4 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 .
Proof. 
Solving the operation of (48) below
Sxx4(ω) = Sff(ω)|H4(ω)|2
yields (47). The proof is finished. □
Theorem 10 (cross-PSD response IV). 
Denote the cross-PSD between f(t) of fGn and x4(t) with Sfx4(ω). Then,
S f x 4 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k ω λ cos λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 + i 2 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 .
Proof. 
Solving the operation of (50)
Sfx4(ω) = Sff(ω)H4(ω)
yields (49). This finishes the proof. □
Let rxx4(τ) be the inverse Fourier transform of Sxx4(ω). According to the convolution theory, one has
rxx4(τ) = rff(τ) * h4(τ) * h4(−τ).
In (51), rxx4(τ) is the ACF response of a class IV fractional vibrator driven by fGn. Let rfx4(τ) be the cross-correlation between the excitation f(t) and the response x4(t). Then,
rfx4(τ) = rff(τ) * h4(τ).
In (52), rfx4(τ) is the cross-correlation response of a class IV fractional vibrator driven by fGn.

3.5.2. Effects of α and λ on Responses

We illustrate some plots of |H4(ω)|2 in Figure 15. Figure 16 indicates some plots of PSD response Sxx4(ω). Some plots of cross-PSD response Sfx4(ω) are shown in Figure 17. Figure 16 and Figure 17 exhibit that there are noticeable effects of (α, λ) on the responses of a class IV fractional vibrator excited by fGn.

3.6. Responses of Class V Fractional Vibrators Driven by fGn

3.6.1. Computation Methods

Theorem 11 (PSD response V). 
Let x5(t) be the response to a class V fractional vibrator driven by f(t) of fGn. Denote with Sxx5(ω) the PSD of x5(t). Then,
S x x 5 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω λ cos λ π 2 2 + 4 γ 2 k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 2 .
Proof. 
Because of Equation (54)
Sxx5(ω) = Sff(ω)|H5(ω)|2,
(53) holds. The proof ends. □
Theorem 12 (cross-PSD response V). 
Let Sfx5(ω) be the cross-PSD between f(t) of fGn and x5(t). Then,
S f x 5 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k ω λ cos λ π 2 1 γ 2 ω λ cos λ π 2 + i 2 γ k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 .
Proof. 
Due to Equation (56)
Sfx5(ω) = Sff(ω)H5(ω),
Equation (55) is true. This finishes the proof. □
Let rxx5(τ) be the ACF of x5(t). Then,
rxx5(τ) = rff(τ) * h5(τ) * h5(−τ).
In Equation (57), rxx5(τ) is the ACF response of a class V fractional vibrator driven by fGn. Let rfx5(τ) be the cross-correlation between f(t) of fGn and x5(t). Then,
rfx5(τ) = rff(τ) * h5(τ).
In Equation (58), rfx5(τ) is the cross-correlation response of a class V fractional vibrator driven by fGn.

3.6.2. Effects of λ on Responses

Figure 18 illustrates some plots of |H5(ω)|2. Figure 19 shows some plots of the PSD response Sxx5(ω). Figure 20 indicates some plots of the cross-PSD response Sfx5(ω). Figure 19 and Figure 20 show that the effects of the fractional order λ on the responses of a class V fractional vibration system under the excitation of fGn are considerable.

3.7. Responses of Class VI Fractional Vibrators Driven by fGn

3.7.1. Computations

Theorem 13 (PSD response VI). 
Let x6(t) be the response to a class VI fractional vibrator driven by f(t) of fGn. Let Sxx6(ω) be the PSD of x6(t). Then,
S x x 6 ( ω ) = 1 k 2 V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 2 + γ 2 ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 2 .
Proof. 
Solving the operation of Equation (60)
Sxx6(ω) = Sff(ω)|H6(ω)|2
yields Equation (59). This finishes the proof. □
Theorem 14 (cross-PSD response VI). 
Denote with Sfx6(ω) the cross-PSD between f(t) of fGn and x6(t). Then,
S f x 6 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 .
Proof. 
Solving the operation of Equation (62)
Sfx6(ω) = Sff(ω)H6(ω)
results in Equation (61). The proof ends. □
Applying the Wiener–Khinchin relation, the Wiener–Lee relation, and the convolution theory to Sxx6(ω) = Sff(ω)|H6(ω)|2 and Sfx6(ω) = Sff(ω)H6(ω) produces
rxx6(τ) = rff(τ) * h6(τ) * h6(−τ),
where rxx6(τ) is the ACF of x6(t), and
rfx6(τ) = rff(τ) * h6(τ),
where rfx6(τ) is the cross-correlation between f(t) of fGn and x6(t). In (63), rxx6(τ) is the ACF response of a class VI fractional vibrator driven by fGn, while in (64), rfx6(τ) is the cross-correlation response of a class VI fractional vibrator driven by fGn.

3.7.2. Effects of α, β, λ on Responses

Figure 21 demonstrates some plots of |H6(ω)|2. Figure 22 indicates some plots of Sxx6(ω). Figure 23 illustrates some plots of Sfx6(ω). Figure 22 and Figure 23 show that the effects of (α, β, λ) on the responses of a class VI fractional vibrator driven by fGn are significant.

3.8. Responses of Class VII Fractional Vibrators Driven by fGn

3.8.1. Computations

Theorem 15 (PSD response VII). 
Let x7(t) be the response to a class VII fractional vibrator excited by f(t) of fGn. Denote with Sxx7(ω) the PSD of x7(t). Then,
S x x 7 ( ω ) = 1 k 2 V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 2 + γ 2 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 2 .
Proof. 
Considering the operation of Equation (66)
Sxx7(ω) = Sff(ω)|H7(ω)|2,
Equation (65) is true. Thus, Theorem 15 holds. The proof ends. □
Theorem 16 (cross-PSD response VII). 
Let Sfx7(ω) be the cross-PSD between f(t) of fGn and x7(t). Then,
S f x 7 ( ω ) = V H sin ( H π ) Γ ( 2 H + 1 ) ω 1 2 H k ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 + i γ 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 .
Proof. 
Performing the operation of Equation (68)
Sfx7(ω) = Sff(ω)H7(ω)
produces Equation (67). The proof is finished. □
In the time domain, one has the ACF response in the form
rxx7(τ) = rff(τ) * h7(τ) * h7(−τ).
In (69), rxx7(τ) is the ACF of x7(t). The cross-correlation response is given by
rfx7(τ) = rff(τ) * h7(τ).
In Equation (70), rfx7(τ) is the cross-correlation between f(t) of fGn and x7(t).

3.8.2. Effects of β, λ on Responses

Figure 24 indicates some plots of |H7(ω)|2, Figure 25 shows some plots of Sxx7(ω), and Figure 26 illustrates some plots of Sfx7(ω). Figure 25 and Figure 26 indicate that the effects of (β, λ) on the responses of class VII fractional vibrators excited by fGn are significant.

3.9. Summary

We have presented the analytic expressions of the PSD and cross-PSD responses of seven classes of fractional vibrators driven by fGn. We have shown that there are noticeable effects of fractional orders, say, α, β, or λ on responses. In addition, the statistical dependences (long-range dependence or short-range dependence) of the responses rely on the excitation fGn because Sxxj(0) = ∞ when 0.5 < H < 1 or Sxxj(0) < ∞ when 0 < H < 0.5 for j = 1, …, 7.

4. PSD and Cross-PSD Responses to Seven Classes of Fractional Vibrations Driven by fBm

This section studies the issue of a fractional Brownian motion (fBm) passing through seven classes of fractional vibration systems. The contributions given in this section are twofold. One brings forward the closed-form expressions of the PSD and cross-PSD responses to seven classes of fractional vibrators driven by fBm in Theorems 17 and 18, respectively. The other demonstrates that there are considerable effects of the fractional orders of seven classes of vibration systems on the responses. In addition, we show that the responses of seven classes of fractional vibrators driven by fBm are of long-range dependence.

4.1. Background

The topic of differential equations driven by fBm has received interest from researchers; see, e.g., Li and Yan [75], Gao et al. [76], Guo et al. [77], Gao and Sun [78], Pei and Zhang [79], Sun et al. [85], He et al. [93,94], Liu [95], Tuan et al. [96,97], Sharma et al. [98], Fan et al. [99], Zhang and Yuan [100], Sun et al. [9], Shahnazi-Pour et al. [101], Araya et al. [102], Gairing et al. [103], Xu et al. [104], and Heydari et al. [105,106], to mention a few. However, reports with respect to the closed-form analytic representations of the responses to seven classes of fractional vibration systems under the excitation of fBm are seldom seen. This section gives its contributions in closed-form analytic representations of the PSD and cross-PSD responses to seven classes of fractional vibration systems driven by fBm.
The rest of the section is organized as follows. In Section 4.2, Section 4.3, Section 4.4, Section 4.5, Section 4.6, Section 4.7 and Section 4.8, we put forward the analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibration systems driven by fBm. A summary is given in Section 4.9.

4.2. Responses of Class I Fractional Vibrators Driven by fBm

4.2.1. Computations

Let f(t) be a driven signal of fBm and Sff(t, ω) be the PSD of f(t) in this section. Then (Flandrin [51], Li [72,74]),
S f f ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t ,
where
0 < H < 1.
Figure 27 shows some plots of Sff(t, ω).
Theorem 17 (PSD response I). 
Denote the PSD of the response of a class I fractional vibrator x1(t) with Sxx1(t, ω). Then,
S x x 1 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k 2 1 ω α ω n 2 cos α π 2 2 + ω α ω n 2 sin α π 2 2 .
Proof. 
Considering the operation of Equation (74),
Sxx1(t, ω) = Sff(t, ω)|H1(ω)|2
results in Equation (73). The proof is finished. □
Theorem 18 (cross-PSD response I). 
Let Sfx1(t, ω) be the cross-PSD between f(t) of fBm and x1(t). Then,
S f x 1 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k 1 ω α ω n 2 cos α π 2 + i ω α ω n 2 sin α π 2 .
Proof. 
Solving Sfx1(t, ω) = Sff(t, ω)H1(ω) yields Equation (75). The proof ends. □
Let rxx1(t, τ) be the inverse Fourier transform of Sxx1(t, ω). Denote with rfx1(t, τ) the inverse Fourier transform of Sfx1(t, ω). Then, applying the convolution theory to Sxx1(t, ω) = Sff(t, ω)|H1(ω)|2 results in the ACF response given by (72), in the form:
rxx1(t, τ) = rff(t, τ) * h1(τ) * h1(−τ).
Similarly, applying the convolution theory to
Sfx1(t, ω) = Sff(t, ω)H1(ω)
yields Equation (78), which is the cross-correlation response in the form:
rfx1(t, τ) = rff(t, τ) * h1(τ).

4.2.2. Effects of α on Responses

Figure 28 indicates some plots of |H1(ω)|2. Some plots of the PSD response Sxx1(t, ω) are shown in Figure 29.
When α = 2, a class I fractional vibrator reduces to be a conventional damping-free vibrator. In general, there are three parameters affecting the response Sxx1(t, ω). From a system perspective, the parameter is the fractional order α. From the view of fractional processes, the parameter H is crucial to Sxx1(t, ω). Figure 30 shows the H effects on Sxx1(t, ω). In Figure 31, we illustrate some plots of the cross-PSD response Sfx1(t, ω). In Figure 32, we show the H effects on Sfx1(t, ω). Figure 29 and Figure 31 indicate that there are significant effects of the fractional order α on the responses to class I fractional vibration systems driven by fBm.

4.3. Responses of Class II Fractional Vibrators Driven by fBm

4.3.1. Computations

Theorem 19 (PSD response II). 
Let x2(t) be the response to a class II fractional vibrator driven by f(t) of fBm. Let Sxx2(t, ω) be the PSD of x2(t). Then,
S x x 2 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k 2 1 γ 2 1 c m ω β 2 cos β π 2 2 + 2 ς ω β ω n sin β π 2 2 .
Proof. 
Solving the operation of Equation (80)
Sxx2(t, ω) = Sff(t, ω)|H2(ω)|2,
we have Equation (79). This finishes the proof. □
Theorem 20 (cross-PSD response II). 
Denote with Sfx2(t, ω) the cross-PSD between f(t) of fBm and x2(t). Then,
S f x 2 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k 1 γ 2 1 2 ς ω n ω β 2 cos β π 2 + i 2 ς ω β ω n sin β π 2 .
Proof. 
Because of Equation (82),
Sfx2(t, ω) = Sff(t, ω)H2(ω),
Equation (81) holds. The proof ends. □
Let rxx2(t, τ) be the ACF of x2(t). Denote with rfx2(t, τ) the cross-correlation between the excitation f(t) of fBm and the response x2(t). According to the convolution theory with respect to Sxx2(t, ω) = Sff(t, ω)|H2(ω)|2, one has the ACF response, expressed by
rxx2(t, τ) = rff(t, τ) * h2(τ) * h2(−τ).
In Equation (83), rxx2(t, τ) is the inverse Fourier transform of Sxx2(t, ω). Similarly, taking into account the convolution theory with respect to Sfx2(t, ω) = Sff(t, ω)H2(ω) produces the cross-correlation response in the form
rfx2(t, τ) = rff(t, τ) * h2(τ).
In Equation (84), rfx2(t, τ) is the inverse Fourier transform of Sfx2(t, ω).

4.3.2. Effects of β on Responses

Some plots of |H2(ω)|2 are indicated in Figure 33. Figure 34 shows some plots of the PSD response Sxx2(t, ω). Figure 35 shows the H effects on Sxx2(t, ω). Figure 36 illustrates some plots of the cross-PSD response Sfx2(t, ω). We use Figure 37 to exhibit the effects of β on |Sfx2(t, ω)|. Figure 35, Figure 36 and Figure 37 show that the effects of β and H on the responses to class II fractional vibration systems driven by fBm are considerable.

4.4. Responses of Class III Fractional Vibrators Driven by fBm

4.4.1. Computations

Theorem 21 (PSD response III). 
Let x3(t) be the response to a class III fractional vibrator driven by f(t) of fBm. Let Sxx3(t, ω) be the PSD of x3(t). Then,
S x x 3 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k 2 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 + γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 .
Proof. 
With Equation (86) below,
Sxx3(t, ω) = Sff(t, ω)|H3(ω)|2,
we have Equation (85). The proof is finished. □
Theorem 22 (cross-PSD response III). 
Let Sfx3(t, ω) be the cross-PSD between f(t) of fBm and x3(t). Then,
S f x 3 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 .
Proof. 
Solving the operation of Equation (88)
Sfx3(t, ω) = Sff(t, ω)H3(ω)
yields Equation (87). The proof ends. □
Denote with rxx3(t, τ) the ACF of x3(t). Let rfx3(t, τ) be the cross-correlation between f(t) of fBm and x3(t). According to the Wiener–Khinchin relation and the Wiener–Lee relation, we have the ACF response, expressed by
rxx3(t, τ) = rff(t, τ) * h3(τ) * h3(−τ),
and the cross-correlation response, given by
rfx3(t, τ) = rff(t, τ) * h3(τ).
In Equation (89), rxx3(t, τ) is the inverse Fourier transform of Sxx3(t, ω) while rfx3(t, τ) in Equation (90) is the inverse Fourier transform of Sfx3(t, ω).

4.4.2. Effects of α and β on Responses

Some plots of |H3(ω)|2 are shown in Figure 38. Figure 39 indicates some plots of the PSD response Sxx3(ω). Some plots of |Sfx3(ω)| are indicated in Figure 40. Figure 39 and Figure 40 exhibit that the effects of (α, β) and H on the responses to class III fractional vibrators driven by fBm are significant.

4.5. Responses of Class IV Fractional Vibrators Driven by fBm

4.5.1. Computations

Theorem 23 (PSD response IV). 
Let x4(t) be the response to a class IV fractional vibrator driven by f(t) of fBm. Let Sxx4(t, ω) be the PSD of x4(t). Then,
S x x 4 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 + 4 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 .
Proof. 
Performing the operation in Equation (92)
Sxx4(t, ω) = Sff(t, ω)|H4(ω)|2
yields Equation (91). This finishes the proof. □
Theorem 24 (cross-PSD response IV). 
Denote with Sfx4(t, ω) the cross-PSD between f(t) of fBm and x4(t). Then,
S f x 4 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k ω λ cos λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 + i 2 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 .
Proof. 
Solving the operation in Equation (94)
Sfx4(t, ω) = Sff(t, ω)H4(ω)
produces Equation (93). This finishes the proof. □
Solving the inverse Fourier transform on both sides of Sxx4(t, ω) = Sff(t, ω)|H4(ω)|2 yields
rxx4(t, τ) = rff(t, τ) * h4(τ) * h4(−τ).
In Equation (95), rxx4(t, τ) is the ACF response of a class IV fractional vibrator. Performing the inverse Fourier transform on the both sides of Sfx4(t, ω) = Sff(t, ω)H4(ω) results in
rfx4(t, τ) = rff(t, τ) * h4(τ).
In Equation (96), rfx4(t, τ) is the cross-correlation response of a class IV fractional vibrator.

4.5.2. Effects of α and λ on Responses

Figure 41 illustrates some plots of |H4(ω)|2. Figure 42 shows some plots of the PSD response Sxx4(t, ω). Some plots of |Sfx4(t, ω)| are given in Figure 43. Figure 42 and Figure 43 show that there are noticeable effects of (α, λ) on the responses to class IV fractional vibrators driven by fBm.

4.6. Responses of Class V Fractional Vibrators Driven by fBm

4.6.1. Computation Methods

Theorem 25 (PSD response V). 
Let x5(t) be the response to a class V fractional vibrator driven by f(t) of fBm. Denote the PSD of x5(t) with Sxx5(t, ω). Then,
S x x 5 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω λ cos λ π 2 2 + 4 γ 2 k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 2 .
Proof. 
Solving the operation in Equation (98)
Sxx5(t, ω) = Sff(t, ω)|H5(ω)|2
yields Equation (97). The proof ends. □
Theorem 26 (cross-PSD response V). 
Let Sfx5(t, ω) be the cross-PSD between f(t) of fBm and x5(t). Then,
S f x 5 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k ω λ cos λ π 2 1 γ 2 ω λ cos λ π 2 + i 2 γ k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 .
Proof. 
When solving the operation in Equation (100),
Sfx5(t, ω) = Sff(t, ω)H5(ω),
we have Equation (99). This finishes the proof. □
Solving the inverse Fourier transform on the both sides of Sxx5(t, ω) = Sff(t, ω)|H5(ω)|2 produces
rxx5(t, τ) = rff(t, τ) * h5(τ) * h5(−τ).
In Equation (101), rxx5(t, τ) is the ACF response of a class V fractional vibrator. Considering the convolution theory with respect to Sfx5(t, ω) = Sff(t, ω)H5(ω) yields the cross-correlation response, given by
rfx5(t, τ) = rff(t, τ) * h5(τ).
In Equation (102), rfx5(t, τ) is the cross-correlation between f(t) of fBm and x5(t).

4.6.2. Effects of λ on Responses

Figure 44 illustrates some plots of |H5(ω)|2, Figure 45 shows some plots of the PSD response Sxx5(t, ω), and Figure 46 shows some plots of |Sfx5(t, ω)|. Figure 45 and Figure 46 show that the effects of λ on the responses to class V fractional vibration systems driven by fBm are considerable.

4.7. Responses of Class VI Fractional Vibrators Driven by fBm

4.7.1. Computations

Theorem 27 (PSD response VI). 
Let x6(t) be the response to a class VI fractional vibrator excited by f(t) of fBm. Let Sxx6(t, ω) be the PSD of x6(t). Then,
S x x 6 ( t , ω ) = 1 k 2 V H ω 2 H + 1 1 2 1 2 H cos 2 ω t ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 2 + γ 2 ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 2 .
Proof. 
Solving the operation in Equation (104)
Sxx6(t, ω) = Sff(t, ω)|H6(ω)|2
yields Equation (103). The proof ends. □
Theorem 28 (cross-PSD response VI). 
Denote with Sfx6(t, ω) the cross-PSD between f(t) of fBm and x6(t). Then,
S f x 6 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 .
Proof. 
Performing the operation in Equation (106)
Sfx6(t, ω) = Sff(t, ω)H6(ω)
results in Equation (105). The proof is finished. □
Solving the inverse Fourier transform on the both sides of Sxx6(t, ω) = Sff(t, ω)|H6(ω)|2 produces
rxx6(t, τ) = rff(t, τ) * h6(τ) * h6(−τ).
In Equation (107), rxx6(t, τ) is the ACF of x6(t). It is the ACF response of a class VI fractional vibrator driven by fBm. The cross-correlation response is given by
rfx6(t, τ) = rff(t, τ) * h6(τ).
In Equation (108), rfx6(t, τ) is the cross-correlation between f(t) of fBm and x6(t).

4.7.2. Effects of α, β, λ on Responses

Figure 47 illustrates some plots of |H6(ω)|2. Figure 48 shows some plots of the PSD response Sxx6(t, ω). Figure 49 demonstrates some plots of |Sfx6(t, ω)|. Figure 48 and Figure 49 imply that the effects of (α, β, λ) on the responses to class VI fractional vibrators under the excitation of fBm are significant.

4.8. Responses of Class VII Fractional Vibrators Driven by fBm

4.8.1. Computations

Theorem 29 (PSD response VII). 
Let x7(t) be the response to a class VII fractional vibrator driven by f(t) of fBm. Denote with Sxx7(t, ω) the PSD of x7(t). Then,
S x x 7 ( t , ω ) = 1 k 2 V H ω 2 H + 1 1 2 1 2 H cos 2 ω t ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 2 + γ 2 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 2 .
Proof. 
Solving the operation in Equation (110)
Sxx7(t, ω) = Sff(t, ω)|H7(ω)|2
results in Equation (109). The proof is complete. □
Theorem 30 (cross-PSD response VII). 
Let Sfx7(t, ω) be the cross-PSD between f(t) of fBm and x7(t). Then,
S f x 7 ( t , ω ) = V H ω 2 H + 1 1 2 1 2 H cos 2 ω t k ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 + i γ 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 .
Proof. 
Solving the operation in (112)
Sfx7(ω) = Sff(ω)H7(ω)
yields Equation (111). The proof ends. □
Solving the inverse Fourier transform on both sides of Sxx7(t, ω) = Sff(t, ω)|H7(ω)|2 produces
rxx7(t, τ) = rff(t, τ) * h7(τ) * h7(−τ).
In Equation (113), rxx7(t, τ) is the ACF of x7(t). This is the ACF response to a class VII fractional vibrator. Similarly, performing the inverse Fourier transform on both sides of Sfx7(ω) = Sff(ω)H7(ω) yields
rfx7(t, τ) = rff(t, τ) * h7(τ).
In Equation (114), rfx7(t, τ) is the cross-correlation between f(t) of fBm and x7(t). This is the cross-correlation response of a class VII fractional vibrator.

4.8.2. Effects of β, λ on Responses

Figure 50 indicates some plots of |H7(ω)|2, Figure 51 shows some plots of the PSD response Sxx7(t, ω), and Figure 52 demonstrates some plots of |Sfx7(t, ω)|. The above figures imply that the effects of (β, λ) on the responses to class VII fractional vibration systems driven by fBm are significant.

4.9. Summary

The analytic expressions of PSD and cross-PSD responses to seven classes of fractional vibrators driven by fBm are given in Theorems 17–30, respectively. The noticeable effects of fractional orders of vibration systems on the responses are illustrated. The responses are of long-range dependence for 0 < H < 0.5 and 0.5 < H < 1 because Sxxj(t, 0) = ∞ when 0 < H < 0.5 and 0.5 < H < 1 for j = 1, …, 7.

5. PSD and Cross-PSD Responses to Seven Classes of Fractional Vibrations Driven by Fractional OU Processes

This section describes the analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibrators driven by fractional OU processes. The results exhibit that the fractional orders of vibration systems as well as the order of fractional OU processes have effects on the responses. The responses of seven classes of fractional vibrators driven by fractional OU processes are of short-range dependence.

5.1. Background

The Langevin equation and the OU process, which is the solution to the Langevin equation under the excitation of white noise, remain research interests in various fields (Eliazar and Shlesinger [58], Pavliotis [107], Coffey et al. [108]). Naturally, fractional Langevin equations attract researchers (Li et al. [32], West [109], Lim et al. [110,111]). Accordingly, fractional OU processes have paid attention to, e.g., Coffey et al. [108], Shao [112], Cheridito et al. [113], Magdziarz [114], Gehringer and Li [115], and Patel and Sharma [116], to mention a few.
In the field, analytic expressions of the responses to seven classes of fractional vibrators driven by fractional OU processes are rarely reported. In this section, we contribute the closed-form analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibrators under the excitation of fractional OU processes. The present results exhibit that there are considerable effects of the fractional order, α, β, and λ, on responses.
The rest of the section is organized as follows. In Section 5.2, Section 5.3, Section 5.4, Section 5.5, Section 5.6, Section 5.7 and Section 5.8, we address the analytic expressions of the PSD and cross-PSD responses to the fractional vibration systems from classes I to VII that are driven by the fractional OU processes. A summary is given in Section 5.9.

5.2. Responses of Class I Fractional Vibrators Driven by Fractional OU Processes

5.2.1. Computations

Let f(t) be a fractional OU process of order b and Sff(ω) be the PSD of f(t) in this section. Then (Li et al. [32], Lim et al. [110,111]),
S f f ( ω ) = 1 λ 2 + ω 2 b ,
where b > 0, λ > 0. Without losing the generality, in what follows, we set λ = 1. Figure 53 illustrates some plots of Sff(ω).
Theorem 31 (PSD response I). 
Let x1(t) be the response to a class I fractional vibrator driven by f(t) of fractional OU processes. Denote with Sxx1(ω) the PSD of x1(t). Then,
S x x 1 ( ω ) = 1 λ 2 + ω 2 b k 2 1 ω α ω n 2 cos α π 2 2 + ω α ω n 2 sin α π 2 2 .
Proof. 
Considering the operation in Equation (117)
Sxx1(ω) = Sff(ω)|H1(ω)|2,
we have Equation (116). The proof is finished. □
Theorem 32 (cross-PSD response I). 
Let Sfx1(ω) be the cross-PSD between f(t) of fractional OU processes and x1(t). Then,
S f x 1 ( ω ) = 1 λ 2 + ω 2 b k 1 ω α ω n 2 cos α π 2 + i ω α ω n 2 sin α π 2 .
Proof. 
Taking into account the operation in Equation (119),
Sfx1(ω) = Sff(ω)H1(ω),
we have Equation (118). The proof ends. □
Let rxx1(τ) be the ACF of x1(t). Let rff(τ) be the ACF of f(t) of fractional OU processes. Let rfx1(τ) be the cross-correlation between the excitation f(t) and the response x1(t). Then, the ACF response is given by
rxx1(τ) = rff(τ) * h1(τ) * h1(−τ).
In Equation (120), rxx1(τ) is the inverse Fourier transform of Sxx1(ω). The cross-correlation response is
rfx1(τ) = rff(τ) * h1(τ).
In Equation (121), rfx1(τ) is the inverse Fourier transform of Sfx1(ω).

5.2.2. Effects of α on Responses

Figure 54 indicates some plots of |H1(ω)|2. Some plots of the PSD response Sxx1(ω) are shown in Figure 55.
When α = 2, a class I fractional vibrator reduces to be a conventional damping-free vibrator. Figure 56 shows the effect of b on Sxx1(ω).
Figure 57 illustrates some plots of the cross-PSD response Sfx1(ω). Figure 56 and Figure 57 exhibit that the order α of class I fractional vibration systems and the order b of the fractional OU processes have noticeable effects on the responses to class I fractional vibrators. We illustrate some plots of driven fractional OU processes and response ones in Figure 58.

5.3. Responses of Class II Fractional Vibration Systems Driven by Fractional OU Processes

5.3.1. Computation Methods

Theorem 33 (PSD response II). 
Let x2(t) be the response to a class II fractional vibrator driven by fractional OU processes. Let Sxx2(ω) be the PSD of x2(t). Then,
S x x 2 ( ω ) = 1 λ 2 + ω 2 b k 2 1 γ 2 1 c m ω β 2 cos β π 2 2 + 2 ς ω β ω n sin β π 2 2 .
Proof. 
Solving the operation Equation (123) below
Sxx2(ω) = Sff(ω)|H2(ω)|2
yields Equation (122). This finishes the proof. □
Theorem 34 (cross-PSD response II). 
Denote with Sfx2(ω) the cross-PSD between f(t) of fractional OU processes and x2(t). Then,
S f x 2 ( ω ) = 1 λ 2 + ω 2 b k 1 γ 2 1 2 ς ω n ω β 2 cos β π 2 + i 2 ς ω β ω n sin β π 2 .
Proof. 
Because of Equation (125) below,
Sfx2(ω) = Sff(ω)H2(ω),
(124) holds. The proof ends. □
Let rxx2(τ) be the ACF of x2(t). Let rfx2(τ) be the cross-correlation between the excitation f(t) of fractional OU processes and the response x2(t). According to the convolution theory, the ACF response is expressed by
rxx2(τ) = rff(τ) * h2(τ) * h2(−τ).
In Equation (126), rxx2(τ) is the inverse Fourier transform of Sxx2(ω). The cross-correlation response is given by
rfx2(τ) = rff(τ) * h2(τ).
In Equation (127), rfx2(τ) is the inverse Fourier transform of Sfx2(ω).

5.3.2. Effects of β on Responses

Some plots of |H2(ω)|2 are indicated in Figure 59. Figure 60 shows some plots of the PSD response Sxx2(ω). Figure 61 shows that the order b of the fractional OU processes does not obviously affect Sxx2(ω). Figure 62 illustrates some plots of |Sfx2(ω)|. Figure 60 and Figure 62 show that there are effects of β on the responses to class II fractional vibrators driven by the fractional OU processes. Figure 63 exhibits the effects of β on the fluctuation range of x2(t).

5.4. Responses of Class III Fractional Vibrators Driven by Fractional OU Processes

5.4.1. Computations

Theorem 35 (PSD response III). 
Let x3(t) be the response to a class III fractional vibrator excited by f(t) of fractional OU processes. Let Sxx3(ω) be the PSD of x3(t). Then,
S x x 3 ( ω ) = 1 λ 2 + ω 2 b k 2 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 + γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 .
Proof. 
With Equation (129) below,
Sxx3(ω) = Sff(ω)|H3(ω)|2,
we have Equation (128). The proof is finished. □
Theorem 36 (cross-PSD response III). 
Let Sfx3(ω) be the cross-PSD between f(t) of fractional OU processes and x3(t). Then,
S f x 3 ( ω ) = 1 λ 2 + ω 2 b 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 .
Proof. 
Using Equation (131) below
Sfx3(ω) = Sff(ω)H3(ω)
yields Equation (130). The proof ends. □
Let rxx3(τ) be the ACF of x3(t). Let rfx3(τ) be the cross-correlation between the excitation f(t) of fractional OU processes and the response x3(t). Applying the convolution theory to Sxx3(ω) = Sff(ω)|H3(ω)|2 produces the ACF response, expressed by
rxx3(τ) = rff(τ) * h3(τ) * h3(−τ).
Similarly, applying the convolution theory to Sfx3(ω) = Sff(ω)H3(ω) results in the cross-correlation response
rfx3(τ) = rff(τ) * h3(τ).

5.4.2. Effects of α and β on Responses

Some plots of |H3(ω)|2 are shown in Figure 64. Figure 65 indicates some plots of the PSD response Sxx3(ω). Some plots of |Sfx3(ω)| are given in Figure 66. Figure 65 and Figure 66 exhibit that the effects of (α, β) on the responses to class III fractional vibration systems driven by the fractional OU processes are significant.

5.5. Responses of Class IV Fractional Vibration Systems Driven by Fractional OU Processes

5.5.1. Computations

Theorem 37 (PSD response IV). 
Let x4(t) be the response to a class IV fractional vibrator excited by f(t) of fractional OU processes. Let Sxx4(ω) be the PSD of x4(t). Then,
S x x 4 ( ω ) = 1 λ 2 + ω 2 b k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 + 4 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 .
Proof. 
Performing the operation Equation (135) below
Sxx4(ω) = Sff(ω)|H4(ω)|2
yields Equation (134). This finishes the proof. □
Theorem 38 (cross-PSD response IV). 
Denote with Sfx4(ω) the cross-PSD between f(t) of fractional OU processes and x4(t). Then,
S f x 4 ( ω ) = 1 λ 2 + ω 2 b k ω λ cos λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 + i 2 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 .
Proof. 
Solving the operation Equation (137) below
Sfx4(ω) = Sff(ω)H4(ω)
produces Equation (136). This finishes the proof. □
Solving the inverse Fourier transform on both sides of Sxx4(ω) = Sff(ω)|H4(ω)|2 yields
rxx4(τ) = rff(τ) * h4(τ) * h4(−τ).
In Equation (138), rxx4(τ) is the ACF of x4(t). It is the ACF response of a class IV fractional vibrator driven by the fractional OU process. In addition,
rfx4(τ) = rff(τ) * h4(τ).
In Equation (139), rfx4(τ) is the cross-correlation between f(t) of the fractional OU process and x4(t). It is the cross-correlation response of a class IV fractional vibrator driven by the fractional OU process.

5.5.2. Effects of α and λ on Responses

Figure 67 illustrates some plots of |H4(ω)|2. Figure 68 indicates some plots of the PSD response Sxx4(ω). Some plots of the cross-PSD response Sfx4(ω) are shown in Figure 69. They exhibit that the effects of (α, λ) and b on the responses to class IV fractional vibration systems driven by the fractional OU processes are noticeable.

5.6. Responses of Class V Fractional Vibrators Driven by Fractional OU Processes

5.6.1. Computation Methods

Theorem 39 (PSD response V). 
Let x5(t) be the response to a class V fractional vibrator driven by f(t) of the fractional OU processes. Denote with Sxx5(ω) the PSD of x5(t). Then,
S x x 5 ( ω ) = 1 λ 2 + ω 2 b k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω λ cos λ π 2 2 + 4 γ 2 k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 2 .
Proof. 
Solving the operation Equation (141) below
Sxx5(ω) = Sff(ω)|H5(ω)|2
yields Equation (140). The proof is finished. □
Theorem 40 (cross-PSD response V). 
Let Sfx5(ω) be the cross-PSD between f(t) of fractional OU processes and x5(t). Then,
S f x 5 ( ω ) = 1 λ 2 + ω 2 b k ω λ cos λ π 2 1 γ 2 ω λ cos λ π 2 + i 2 γ k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 .
Proof. 
When solving the operation Equation (143) below,
Sfx5(ω) = Sff(ω)H5(ω),
we have Equation (142). This finishes the proof. □
Performing the inverse Fourier transform on both sides of Sxx5(ω) = Sff(ω)|H5(ω)|2 produces
rxx5(τ) = rff(τ) * h5(τ) * h5(−τ).
In Equation (144), rxx5(τ) is the ACF of x5(t). It is the ACF response of a class V fractional vibrator driven by the fractional OU process. In addition,
rfx5(τ) = rff(τ) * h5(τ).
In Equation (145), rfx5(τ) is the cross-correlation between f(t) of the fractional OU process and x5(t). It is the cross-correlation response of a class V fractional vibrator driven by the fractional OU process.

5.6.2. Effects of λ on Responses

Figure 70 illustrates some plots of |H5(ω)|2. Figure 71 indicates some plots of Sxx5(ω). Figure 72 shows some plots of |Sfx5(ω)|. From these figures, we can see that the effects of λ and b on the responses to class V fractional vibrators driven by the fractional OU process are considerable.

5.7. Responses of Class VI Fractional Vibrators Driven by Fractional OU Processes

5.7.1. Computations

Theorem 41 (PSD response VI). 
Let x6(t) be the response to a class VI fractional vibrator excited by f(t) of fractional OU processes. Let Sxx6(ω) be the PSD of x6(t). Then,
S x x 6 ( ω ) = 1 k 2 1 λ 2 + ω 2 b ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 2 + γ 2 ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 2 .
Proof. 
Considering Equation (147) below
Sxx6(ω) = Sff(ω)|H6(ω)|2
yields Equation (146). The proof ends. □
Theorem 42 (cross-PSD response VI). 
Denote with Sfx6(ω) the cross-PSD between f(t) of the fractional OU process and x6(t). Then,
S f x 6 ( ω ) = 1 λ 2 + ω 2 b k ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 .
Proof. 
Performing the operation Equation (149) below
Sfx6(ω) = Sff(ω)H6(ω)
results in Equation (148). The proof is finished. □
Solving the inverse Fourier transform on both sides of Sxx6(ω) = Sff(ω)|H6(ω)|2 produces
rxx6(τ) = rff(τ) * h6(τ) * h6(−τ).
In Equation (150), rxx6(τ) is the ACF of x6(t). It is the ACF response of a class VI fractional vibrator driven by the fractional OU process. Furthermore,
rfx6(τ) = rff(τ) * h6(τ).
In Equation (151), rfx6(τ) is the cross-correlation between f(t) of the fractional OU process and x6(t). It is the cross-correlation response of a class VI fractional vibrator driven by the fractional OU process.

5.7.2. Effects of α, β, λ on Responses

Figure 73 illustrates some plots of |H6(ω)|2. Figure 74 shows some plots of r Sxx6(ω). Figure 75 demonstrates some plots of |Sfx6(ω)|. Figure 73 and Figure 74 show that the effects of (α, β, λ) on the responses to class VI fractional vibration systems driven by the fractional OU process are significant.

5.8. Responses of Class VII Fractional Vibrators Driven by Fractional OU Processes

5.8.1. Computations

Theorem 43 (PSD response VII). 
Let x7(t) be the response to a class VII fractional vibrator driven by f(t) of the fractional OU process. Denote with Sxx7(ω) the PSD of x7(t). Then,
S x x 7 ( ω ) = 1 k 2 1 λ 2 + ω 2 b ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 2 + γ 2 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 2 .
Proof. 
Solving the operation in Equation (153)
Sxx7(ω) = Sff(ω)|H7(ω)|2
results in Equation (152). The proof is complete. □
Theorem 44 (cross-PSD response VII). 
Let Sfx7(ω) be the cross-PSD between f(t) of the fractional OU process and x7(t). Then,
S f x 7 ( ω ) = 1 λ 2 + ω 2 b k ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 + i γ 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 .
Proof. 
Solving the operation in Equation (155)
Sfx7(ω) = Sff(ω)H7(ω)
yields Equation (154). The proof ends. □
Solving the inverse Fourier transform on both sides of Sxx7(ω) = Sff(ω)|H7(ω)|2 produces
rxx7(τ) = rff(τ) * h7(τ) * h7(−τ).
In Equation (156), rxx7(τ) is the ACF of x7(t). It is the ACF response of a class VII fractional vibrator driven by the fractional OU process. Additionally,
rfx7(τ) = rff(τ) * h7(τ).
In Equation (157), rfx7(τ) is the cross-correlation between f(t) of the fractional OU process and x7(t). It is the cross-correlation response of a class VII fractional vibrator driven by the fractional OU process.

5.8.2. Effects of β, λ on Responses

Figure 76 shows some plots of |H7(ω)|2. Figure 77 indicates some plots of Sxx7(ω). Figure 78 illustrates some plots of |Sfx7(ω)|. Figure 77 and Figure 78 exhibit that the effects of (β, λ) on the responses to class VII fractional vibration systems driven by the fractional class VII vibrators are considerable.

5.9. Summary

We present the analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibrators driven by the fractional OU process in Theorems 31–44, respectively. We illustrate that there are considerable effects of orders of fractional vibrators on the responses. The responses of seven classes of fractional vibrators under the excitation of the fractional OU processes are short-range-dependent due to Sxxj(0) < ∞ for j = 1, …, 7.

6. PSD and Cross-PSD Responses to Seven Classes of Fractional Vibrations Driven by the von Kármán Process

This section describes the analytic expressions of PSD responses and cross-PSD ones to seven classes of fractional vibrators driven by the von Kármán process. It shows that there are considerable effects of orders of fractional vibrators on responses driven by the von Kármán process. The responses of seven classes of fractional vibrators driven by the von Kármán process are of short-range dependence.

6.1. Background

The processes that follow the von Kármán spectrum are widely used in wind, ship, and ocean engineering (Faltinsen [117], Holmes [118]). Recently, Li [36] reported the point of view that processes on the von Kármán spectrum can be taken as a type of fractional OU process with the fractal dimension 5/3. Nonetheless, how to analytically represent the PSD and cross-PSD responses to seven classes of fractional vibrators driven by the von Kármán process remains an unsolved problem. This section gives the closed-form analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibrators driven by the von Kármán process.
The rest of the section is organized as follows. In Section 6.2, Section 6.3, Section 6.4, Section 6.5, Section 6.6, Section 6.7 and Section 6.8, we put forward the analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibrators excited by the von Kármán process. A summary is given in Section 6.9.

6.2. Responses of Class I Fractional Vibrators Driven by von Kármán Process

6.2.1. Computations

Let f(t) be a process with the von Kármán spectrum and Sff(ω) be the PSD of the von Kármán type. Then,
S f f ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 ,
where
A vk = 4 σ u 2 70.8 5 / 6 L u x U 2 / 3
and
B vk = U 70.8 1 / 2 L u x ,
where L u x is the turbulence integral scale, U is the mean speed, uf is the friction velocity (ms−1), bv is the friction velocity coefficient such that the variance of wind speed is σ u 2 = b v u f 2 .  Figure 79 illustrates the plots of Sff(ω). In this section, L u x = 1 is used simply for facilitating the illustrations. This does not cause the generality to describe the issue of the von Kármán process passing through seven classes of fractional vibration systems to be lost.
Theorem 45 (PSD response I). 
Let x1(t) be the response to a class I fractional vibrator excited by f(t) of the von Kármán process. Denote with Sxx1(ω) the PSD of x1(t). Then,
S x x 1 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k 2 1 ω α ω n 2 cos α π 2 2 + ω α ω n 2 sin α π 2 2 .
Proof. 
Solving the operation in Equation (162)
Sxx1(ω) = Sff(ω)|H1(ω)|2
results in Equation (161). The proof is finished. □
Theorem 46 (cross-PSD response I). 
Let Sfx1(ω) be the cross-PSD between f(t) of the von Kármán process and x1(t). Then,
S f x 1 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k 1 ω α ω n 2 cos α π 2 + i ω α ω n 2 sin α π 2 .
Proof. 
Solving the operation in Equation (164)
Sfx1(ω) = Sff(ω)H1(ω)
produces Equation (163). The proof ends. □
Denote with rxx1(τ) the ACF of x1(t). Let rff(τ) be the ACF of f(t). Let h1(τ) be the impulse response of a class I fractional vibrator. Applying the convolution theory to Sxx1(ω) = Sff(ω)|H1(ω)|2 yields the ACF response
rxx1(τ) = rff(τ) * h1(τ) * h1(−τ).
Similarly, applying the convolution theory to Sfx1(ω) = Sff(ω)H1(ω) produces the cross-correlation response
rfx1(τ) = rff(τ) * h1(τ).

6.2.2. Effects of α on Responses

Figure 80 indicates some plots of |H1(ω)|2. Some plots of the PSD response Sxx1(ω) are shown in Figure 81.
When α = 2, a class I fractional vibrator reduces to be a conventional damping-free vibrator. In general, there are three parameters affecting the response Sxx1(ω). From a system perspective, the parameter is the fractional order α. From an engineering perspective, the parameter U is crucial to Sxx1(ω). Figure 82 shows the effect of U on Sxx1(ω). In Figure 83, we illustrate the plots of |Sfx1(ω)|. The plots of the driven signal with the von Kármán spectrum and the response ones are indicated in Figure 84. Figure 82, Figure 83 and Figure 84 show that there are noticeable effects of α on the responses to class I fractional vibration systems driven by the von Kármán process.

6.3. Responses of Class II Fractional Vibration Systems Driven by von Kármán Process

6.3.1. Computation Methods

Theorem 47 (PSD response II). 
Let x2(t) be the response to a class II fractional vibrator driven by f(t) of the von Kármán process. Let Sxx2(ω) be the PSD of the response x2(t). Then,
S x x 2 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k 2 1 γ 2 1 c m ω β 2 cos β π 2 2 + 2 ς ω β ω n sin β π 2 2 .
Proof. 
Using the operation in Equation (168)
Sxx2(ω) = Sff(ω)|H2(ω)|2
yields Equation (167). This finishes the proof. □
Theorem 48 (cross-PSD response II). 
Denote with Sfx2(ω) the cross-PSD between f(t) and x2(t). Then,
S f x 2 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k 1 γ 2 1 2 ς ω n ω β 2 cos β π 2 + i 2 ς ω β ω n sin β π 2 .
Proof. 
Using the operation in Equation (170)
Sfx2(ω) = Sff(ω)H2(ω)
produces Equation (169). The proof ends. □
Let rxx2(τ) be the ACF of x2(t). Denote with rfx2(τ) the cross-correlation between f(t) of the von Kármán process and x2(t). Applying the Wiener–Khinchin relation to Sxx2(ω) = Sff(ω)|H2(ω)|2 results in the ACF response
rxx2(τ) = rff(τ) * h2(τ) * h2(−τ).
Note that rxx2(τ) in Equation (171) is the ACF response of a class II fractional vibrato driven by the von Kármán process. Similarly, applying the Wiener–Lee relation to Sfx2(ω) = Sff(ω)H2(ω) yields the cross-correlation
rfx2(τ) = rff(τ) * h2(τ).
In Equation (172), rfx2(τ) is the cross-correlation response of a class II fractional vibrato driven by the von Kármán process.

6.3.2. Effects of β on Responses

Some plots of |H2(ω)|2 are indicated in Figure 85. Figure 86 shows some plots of the PSD response Sxx2(ω). Figure 87 shows the U effects on Sxx2(ω). Figure 88 illustrates some plots of |Sfx2(ω)|. Figure 87 and Figure 88 exhibit that there are effects of β on the responses to class II fractional vibration systems driven by the von Kármán process. We also use Figure 89 to exhibit the effects of β on the fluctuation range of x2(t).

6.4. Responses of Class III Fractional Vibrators Driven by von Kármán Process

6.4.1. Computations

Theorem 49 (PSD response III). 
Let x3(t) be the response to a class III fractional vibrator driven by the von Kármán process. Let Sxx3(ω) be the PSD of x3(t). Then,
S x x 3 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k 2 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 + γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 2 .
Proof. 
Considering the operation in Equation (174),
Sxx3(ω) = Sff(ω)|H3(ω)|2,
we have Equation (173). The proof ends. □
Theorem 50 (cross-PSD response III). 
Let Sfx3(ω) be the cross-PSD between f(t) of the von Kármán process and x3(t). Then,
S f x 3 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 1 γ 2 ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ς ω n ω β 1 sin β π 2 ω n ω α 2 cos α π 2 2 ς ω n ω β 2 cos β π 2 .
Proof. 
Solving the operation in Equation (176)
Sfx3(ω) = Sff(ω)H3(ω)
results in Equation (175). The proof ends. □
Let rxx3(τ) be the ACF of x3(t). Denote with rfx3(τ) the cross-correlation between f(t) and x3(t). According to the Wiener–Khinchin relation and the Wiener–Lee relation, we have
rxx3(τ) = rff(τ) * h3(τ) * h3(−τ).
In Equation (177), rxx3(τ) is the ACF response of a class III fractional vibrator driven by the von Kármán process. The cross-correlation response of a class III fractional vibrator driven by the von Kármán process is expressed by
rfx3(τ) = rff(τ) * h3(τ).

6.4.2. Effects of α and β on Responses

Some plots of |H3(ω)|2 are shown in Figure 90. Figure 91 indicates some plots of the PSD response Sxx3(ω). Some plots of |Sfx3(ω)| are indicated in Figure 92. Figure 91 and Figure 92 exhibit that the effects of (α, β) on the responses of class III fractional vibrators driven by the von Kármán process are significant.

6.5. Responses of Class IV Fractional Vibration Systems Driven by the von Kármán Process

6.5.1. Computations

Theorem 51 (PSD response IV). 
Let x4(t) be the response to a class IV fractional vibrator driven by f(t) of the von Kármán process. Let Sxx4(ω) be the PSD of the response x4(t). Then,
S x x 4 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 + 4 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 2 .
Proof. 
Solving the operation in Equation (180)
Sxx4(ω) = Sff(ω)|H4(ω)|2
produces Equation (177). This finishes the proof. □
Theorem 52 (cross-PSD response IV). 
Denote with Sfx4(ω) the cross-PSD between f(t) of the von Kármán process and x4(t). Then,
S f x 4 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k ω λ cos λ π 2 1 γ 2 ω α 2 cos α π 2 ω λ cos λ π 2 + i 2 γ m ω α 1 sin α π 2 + k ω λ 1 sin λ π 2 2 m k ω α + λ 2 cos α π 2 cos λ π 2 ω α 2 cos α π 2 ω λ cos λ π 2 .
Proof. 
Solving the operation in Equation (182)
Sfx4(ω) = Sff(ω)H4(ω)
produces Equation (181). The proof is finished. □
In the time domain, we have
rxx4(τ) = rff(τ) * h4(τ) * h4(−τ).
In Equation (183), rxx4(τ) is the ACF of x4(t). In addition,
rfx4(τ) = rff(τ) * h4(τ).
In Equation (184), rfx4(τ) is the cross-correlation between the excitation f(t) of the von Kármán process and the response x4(t).

6.5.2. Effects of α and λ on Responses

We illustrate some plots of |H4(ω)|2 in Figure 93. Figure 94 indicates some plots of the PSD response Sxx4(ω). Some plots of |Sfx4(ω)| are indicated in Figure 95. Figure 94 and Figure 95 demonstrate that the effects of (α, λ) on the responses of class VI fractional vibrators driven by the von Kármán process are noticeable.

6.6. Responses of Class V Fractional Vibrators Driven by von Kármán Process

6.6.1. Computation Methods

Theorem 53 (PSD response V). 
Let x5(t) be the response to a class V fractional vibrator driven by f(t) of the von Kármán process. Denote with Sxx5(ω) the PSD of the response x5(t). Then,
S x x 5 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k 2 ω 2 λ cos 2 λ π 2 1 γ 2 ω λ cos λ π 2 2 + 4 γ 2 k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 2 .
Proof. 
Solving the operation in Equation (186)
Sxx5(ω) = Sff(ω)|H5(ω)|2
results in Equation (185). The proof ends. □
Theorem 54 (cross-PSD response V). 
Let Sfx5(ω) be the cross-PSD between f(t) of the von Kármán process and x5(t). Then,
S f x 5 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k ω λ cos λ π 2 1 γ 2 ω λ cos λ π 2 + i 2 γ k ω λ 1 sin λ π 2 2 m k ω λ cos λ π 2 1 ω λ cos λ π 2 .
Proof. 
Solving the operation in (188) below
Sfx5(ω) = Sff(ω)H5(ω)
yields Equation (187). This finishes the proof. □
In the time domain, we have
rxx5(τ) = rff(τ) * h5(τ) * h5(−τ).
In Equation (189), rxx5(τ) is the ACF of x5(t). In addition,
rfx5(τ) = rff(τ) * h5(τ).
In Equation (190), rfx5(τ) is the cross-correlation between the excitation f(t) of the von Kármán process and the response x5(t).

6.6.2. Effects of λ on Responses

Figure 96 illustrates some plots of |H5(ω)|2. Figure 97 shows some plots of the PSD response Sxx5(ω), and Figure 98 shows some plots of |Sfx5(ω)|. Figure 97 and Figure 98 illustrate the considerable effects of λ on the responses of class V fractional vibrators driven by the von Kármán process.

6.7. Responses of Class VI Fractional Vibrators Driven by von Kármán Process

6.7.1. Computations

Theorem 55 (PSD response VI). 
Let x6(t) be the response to a class VI fractional vibrator excited by the von Kármán process. Let Sxx6(ω) be the PSD of the response x6(t). Then,
S x x 6 ( ω ) = 1 k 2 A vk ( B vk ) 2 + ω 2 5 / 6 ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 2 + γ 2 ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 2 .
Proof. 
Considering the operation in Equation (192)
Sxx6(ω) = Sff(ω)|H6(ω)|2
produces Equation (191). The proof ends. □
Theorem 56 (cross-PSD response VI). 
Denote with Sfx6(ω) the cross-PSD between f(t) of the von Kármán process and x6(t). Then,
S f x 6 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k ω λ cos λ π 2 + γ 2 ω α 2 cos α π 2 + 2 ς ω n ω β 2 cos β π 2 + i γ ω α 1 sin α π 2 + 2 ζ ω n ω β 1 sin β π 2 + ω n 2 ω λ 1 sin λ π 2 .
Proof. 
Solving the operation in Equation (194)
Sfx6(ω) = Sff(ω)H6(ω)
results in Equation (193). The proof is finished. □
Applying the Wiener–Khinchin relation and the Wiener–Lee relation, respectively, to Sxx6(ω) = Sff(ω)|H6(ω)|2 and Sfx6(ω) = Sff(ω)H6(ω), we have
rxx6(τ) = rff(τ) * h6(τ) * h6(−τ).
In Equation (195), rxx6(τ) is the ACF of x6(t). In addition,
rfx6(τ) = rff(τ) * h6(τ).
In Equation (196), rfx6(τ) is the cross-correlation between f(t) of von Kármán process and x6(t).

6.7.2. Effects of α, β, λ on Responses

Figure 99 illustrates some plots of |H6(ω)|2. Figure 100 shows some plots of the PSD response Sxx6(ω). Figure 101 indicates some plots of |Sfx6(ω)|. Figure 100 and Figure 101 show the significant effects of fractional orders (α, β, λ) on the responses to class VI fractional vibration systems under the excitation of the von Kármán process.

6.8. Responses of Class VII Fractional Vibrators Driven by the von Kármán Process

6.8.1. Computations

Theorem 57 (PSD response VII). 
Let x7(t) be the response to a class VII fractional vibrator driven by the von Kármán process. Denote with Sxx7(ω) the PSD of x7(t). Then,
S x x 7 ( ω ) = 1 k 2 A vk ( B vk ) 2 + ω 2 5 / 6 ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 2 + γ 2 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 2 .
Proof. 
Solving the operation in Equation (198)
Sxx7(ω) = Sff(ω)|H7(ω)|2
yields Equation (197). The proof is finished. □
Theorem 58 (cross-PSD response VII). 
Let Sfx7(ω) be the cross-PSD between f(t) of the von Kármán process and x7(t). Then,
S f x 7 ( ω ) = A vk ( B vk ) 2 + ω 2 5 / 6 k ω λ cos λ π 2 γ 1 2 ς ω n ω β 2 cos β π 2 + i γ 2 ς ω β 1 sin β π 2 + ω n ω λ 1 sin λ π 2 .
Proof. 
Solving the operation in Equation (200)
Sfx7(ω) = Sff(ω)H7(ω)
yields Equation (199). The proof ends. □
According to the Wiener–Khinchin relation and the Wiener–Lee relation, we have
rxx7(τ) = rff(τ) * h7(τ) * h7(−τ),
where rxx7(τ) is the ACF of x7(t), and
rfx7(τ) = rff(τ) * h7(τ),
where rfx7(τ) is the cross-correlation between f(t) of the von Kármán process and x7(t).

6.8.2. Effects of β, λ on Responses

Figure 102 indicates some plots of |H7(ω)|2. Figure 103 gives some plots of the PSD response Sxx7(ω). Figure 104 shows some plots of |PSD Sfx7(ω)|. Figure 103 and Figure 104 exhibit the noticeable effects of fractional orders (β, λ) on the responses to class VII fractional vibrators under the excitation of the von Kármán process.

6.9. Summary

We present the closed-form analytic expressions of the PSD and cross-PSD responses to seven classes of fractional vibrators driven by the von Kármán process in Theorems 45–58, respectively. We demonstrate that the orders of fractional vibrators noticeably affect the responses. The responses of seven classes of fractional vibrators are short-range-dependent due to Sxxj(0) < ∞ for j = 1, …, 7.

7. Discussions and Conclusions

Vibrations in random environments are usually called random vibrations (Crandall and Mark [119], Elishakoff and Lyon [120]). Since structures may often suffer from random loading, such as ocean waves, random vibrations are paid close attention (Rothbart and Brown [121], Jensen [122], Harris [123], Lalanne [124]). That is the motivation of studying fractionally random vibrations in this research.
Note that a main aim of studying random vibrations is to study the fatigue damage of structures in random environments (Crandall and Mark [119], Harris [123], Lalanne [125,126], Li [127,128]). Our future work will focus on fatigue damage to structures using fractionally random vibrations.
We introduced the class VII fractional vibrators in Section 2, in addition to six classes of fractional vibrators. The frequency transfer functions and impulse response functions of seven classes of fractional vibrators are given in Section 2. The analytical expressions of the PSD responses and cross-PSD ones to seven classes of fractional vibrators driven by fGn, fBm, the OU processes, and the von Kármán process are proposed in Section 3, Section 4, Section 5 and Section 6, respectively. Our demonstrations exhibit that the effects of fractional orders on the responses of seven classes of fractional vibrators, which are excited by fGn, fBm, the OU processes, and the von Kármán process, are noticeable.

Funding

This research received no external funding.

Data Availability Statement

Data are contained within the article.

Conflicts of Interest

The author declares no conflict of interest.

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Figure 1. Plots of PSD of fGn for H = 0.8 (solid), 0.6 (dot), 0.4 (dash), and 0.2 (dash dot).
Figure 1. Plots of PSD of fGn for H = 0.8 (solid), 0.6 (dot), 0.4 (dash), and 0.2 (dash dot).
Symmetry 16 00635 g001
Figure 2. Plots of |H1(ω)|2 with α = 1.8 (solid), 1.9 (dot), and 2.1 (dash) when m = 1 and k = 36.
Figure 2. Plots of |H1(ω)|2 with α = 1.8 (solid), 1.9 (dot), and 2.1 (dash) when m = 1 and k = 36.
Symmetry 16 00635 g002
Figure 3. PSD response Sxx1(ω) with α = 1.8 (solid), 1.9 (dot), and 2.1 (dash) when m = 1, k = 36, and H = 0.75.
Figure 3. PSD response Sxx1(ω) with α = 1.8 (solid), 1.9 (dot), and 2.1 (dash) when m = 1, k = 36, and H = 0.75.
Symmetry 16 00635 g003
Figure 4. H effects the response of PSD Sxx1(ω) when α = 1.8, m = 1, and k = 36 for H = 0.95 (solid), 0.75 (dot), 0.55 (dash), and 0.35 (dash dot).
Figure 4. H effects the response of PSD Sxx1(ω) when α = 1.8, m = 1, and k = 36 for H = 0.95 (solid), 0.75 (dot), 0.55 (dash), and 0.35 (dash dot).
Symmetry 16 00635 g004
Figure 5. Cross-PSD response Sfx1(ω) with α = 1.8 (solid), 2.4 (dot), and 2.8 (dash) when m = 1, k = 36, and H = 0.75. (a) |Sfx1(ω)|. (b) Phase of Sfx1(ω).
Figure 5. Cross-PSD response Sfx1(ω) with α = 1.8 (solid), 2.4 (dot), and 2.8 (dash) when m = 1, k = 36, and H = 0.75. (a) |Sfx1(ω)|. (b) Phase of Sfx1(ω).
Symmetry 16 00635 g005
Figure 6. Plots of driven fGn and response signals when m = 1, k = 36, and H = 0.75. (a) Driven fGn. (b) Response x1(t) for α = 1.8. (c) Response x1(t) for α = 2.4. (d) Response x1(t) for α = 2.8.
Figure 6. Plots of driven fGn and response signals when m = 1, k = 36, and H = 0.75. (a) Driven fGn. (b) Response x1(t) for α = 1.8. (c) Response x1(t) for α = 2.4. (d) Response x1(t) for α = 2.8.
Symmetry 16 00635 g006
Figure 7. Plots of |H2(ω)|2 (log) with β = 0.01 (solid) and 1.99 (dot) when m = 1, c = 0.1, and k = 36.
Figure 7. Plots of |H2(ω)|2 (log) with β = 0.01 (solid) and 1.99 (dot) when m = 1, c = 0.1, and k = 36.
Symmetry 16 00635 g007
Figure 8. PSD response Sxx2(ω) (log) with β = 0.4 (solid) and 1.8 (dot) when m = 1, c = 0.1, and k = 36. (a) Sxx2(ω) when H = 0.95. (b) Sxx2(ω) when H = 0.75. (c) Sxx2(ω) when H = 0.55. (d) Sxx2(ω) when H = 0.35.
Figure 8. PSD response Sxx2(ω) (log) with β = 0.4 (solid) and 1.8 (dot) when m = 1, c = 0.1, and k = 36. (a) Sxx2(ω) when H = 0.95. (b) Sxx2(ω) when H = 0.75. (c) Sxx2(ω) when H = 0.55. (d) Sxx2(ω) when H = 0.35.
Symmetry 16 00635 g008
Figure 9. Resonance when with β = 1, m = 1, c = 0.1, k = 36, and V = 15. (a) Plot of |H2(ω)|2 (log). (b) PSD response Sxx2(ω) (log) for H = 0.95 (solid), 0.75 (dot), 0.35 (dash), and 0.15 (dash dot).
Figure 9. Resonance when with β = 1, m = 1, c = 0.1, k = 36, and V = 15. (a) Plot of |H2(ω)|2 (log). (b) PSD response Sxx2(ω) (log) for H = 0.95 (solid), 0.75 (dot), 0.35 (dash), and 0.15 (dash dot).
Symmetry 16 00635 g009
Figure 10. Cross-PSD response Sfx2(ω) with β = 0.2 (solid), 1 (dot), and 1.9 (dash) when m = 1, c = 0.1, k = 36, and H = 0.75. (a) |Sfx2(ω)| (log). (b) Phase of Sfx2(ω).
Figure 10. Cross-PSD response Sfx2(ω) with β = 0.2 (solid), 1 (dot), and 1.9 (dash) when m = 1, c = 0.1, k = 36, and H = 0.75. (a) |Sfx2(ω)| (log). (b) Phase of Sfx2(ω).
Symmetry 16 00635 g010
Figure 11. Response of x2(t) when m = 1, c = 0.1, k = 36, and H = 0.75. (a) x2(t) for β = 0.4. (b) x2(t) for β = 1.4.
Figure 11. Response of x2(t) when m = 1, c = 0.1, k = 36, and H = 0.75. (a) x2(t) for β = 0.4. (b) x2(t) for β = 1.4.
Symmetry 16 00635 g011
Figure 12. Plots of |H3(ω)|2 in log when m = 1, c = 0.1, and k = 36 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), (2.5, 0.8) (dash), and (2.8, 1.8) (dash dot).
Figure 12. Plots of |H3(ω)|2 in log when m = 1, c = 0.1, and k = 36 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), (2.5, 0.8) (dash), and (2.8, 1.8) (dash dot).
Symmetry 16 00635 g012
Figure 13. Response of PSD Sxx3(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), (2.5, 0.8) (dash), and (2.8, 1.8) (dash dot).
Figure 13. Response of PSD Sxx3(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), (2.5, 0.8) (dash), and (2.8, 1.8) (dash dot).
Symmetry 16 00635 g013
Figure 14. Cross-PSD responses of Sfx3(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β) = (1.3, 0.8) (solid), (1.3, 1.8) (dot), (2.5, 0.8) (dash), and (2.8, 1.8) (dash dot). (a) |Sfx3(ω)|. (b) Phase of Sfx3(ω).
Figure 14. Cross-PSD responses of Sfx3(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β) = (1.3, 0.8) (solid), (1.3, 1.8) (dot), (2.5, 0.8) (dash), and (2.8, 1.8) (dash dot). (a) |Sfx3(ω)|. (b) Phase of Sfx3(ω).
Symmetry 16 00635 g014
Figure 15. Plots of |H4(ω)|2 in log when m = 1, c = 0, and k = 36, for (α, λ) = (1.6, 0.2) (solid), (1.6, 0.4) (dot), (2.5, 0.2) (dash), (2.5, 0.4) (dash dot).
Figure 15. Plots of |H4(ω)|2 in log when m = 1, c = 0, and k = 36, for (α, λ) = (1.6, 0.2) (solid), (1.6, 0.4) (dot), (2.5, 0.2) (dash), (2.5, 0.4) (dash dot).
Symmetry 16 00635 g015
Figure 16. PSD response Sxx4(ω) in log when m = 1, c = 0, k = 36, and H = 0.75 for (α, λ) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), (2.5, 0.8) (dash), (2.8, 1.8) (dash dot).
Figure 16. PSD response Sxx4(ω) in log when m = 1, c = 0, k = 36, and H = 0.75 for (α, λ) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), (2.5, 0.8) (dash), (2.8, 1.8) (dash dot).
Symmetry 16 00635 g016
Figure 17. Cross-PSD Sfx4(ω) when m = 1, c = 0, k = 36, and V = 15 for (α, λ) = (1.6, 0.2) (solid), (1.6, 0.4) (dot), (2.45, 0.2) (dash), (2.45, 0.4) (dash dot). (a) |Sfx4(ω)|. (b) Phase of Sfx4(ω).
Figure 17. Cross-PSD Sfx4(ω) when m = 1, c = 0, k = 36, and V = 15 for (α, λ) = (1.6, 0.2) (solid), (1.6, 0.4) (dot), (2.45, 0.2) (dash), (2.45, 0.4) (dash dot). (a) |Sfx4(ω)|. (b) Phase of Sfx4(ω).
Symmetry 16 00635 g017
Figure 18. Plots of |H5(ω)|2 (log) when m = 1, c = 0, and k = 36 for λ = 0.1 (solid), 0.3 (dot), 0.5 (dash), and 0.7 (dash dot).
Figure 18. Plots of |H5(ω)|2 (log) when m = 1, c = 0, and k = 36 for λ = 0.1 (solid), 0.3 (dot), 0.5 (dash), and 0.7 (dash dot).
Symmetry 16 00635 g018
Figure 19. Response of PSD Sxx5(ω) in log when m = 1, c = 0, k = 36, and H = 0.75 for λ = 0.1 (solid), 0.3 (dot), 0.5 (dash), and 0.7 (dash dot).
Figure 19. Response of PSD Sxx5(ω) in log when m = 1, c = 0, k = 36, and H = 0.75 for λ = 0.1 (solid), 0.3 (dot), 0.5 (dash), and 0.7 (dash dot).
Symmetry 16 00635 g019
Figure 20. Cross-PSD response Sfx5(ω) when m = 1, c = 0, k = 36, and H = 0.75 for λ = 0.1 (solid), 0.3 (dot), 0.5 (dash), and 0.7 (dash dot). (a) |Sfx5(ω)| in log. (b) Phase of Sfx5(ω).
Figure 20. Cross-PSD response Sfx5(ω) when m = 1, c = 0, k = 36, and H = 0.75 for λ = 0.1 (solid), 0.3 (dot), 0.5 (dash), and 0.7 (dash dot). (a) |Sfx5(ω)| in log. (b) Phase of Sfx5(ω).
Symmetry 16 00635 g020
Figure 21. Plots of |H6(ω)|2 (log) when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (1.6, 0.5, 0.2) (solid), (1.6, 1.5, 0.4) (dot), (2.5, 0.5, 0.2) (dash), and (2.5, 0.5, 0.4) (dash dot).
Figure 21. Plots of |H6(ω)|2 (log) when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (1.6, 0.5, 0.2) (solid), (1.6, 1.5, 0.4) (dot), (2.5, 0.5, 0.2) (dash), and (2.5, 0.5, 0.4) (dash dot).
Symmetry 16 00635 g021
Figure 22. Response of PSD Sxx6(ω) in log when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β, λ) = (1.6, 0.8, 0.2) (solid), (1.6, 1.8, 0.4) (dot), (2.5, 0.4, 0.2) (dash), and (2.5, 0.8, 0.4) (dash dot).
Figure 22. Response of PSD Sxx6(ω) in log when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β, λ) = (1.6, 0.8, 0.2) (solid), (1.6, 1.8, 0.4) (dot), (2.5, 0.4, 0.2) (dash), and (2.5, 0.8, 0.4) (dash dot).
Symmetry 16 00635 g022
Figure 23. Cross-PSD response Sfx6(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β, λ) = (1.6, 0.5, 0.2) (solid), (1.6, 1.5, 0.4) (dot), (2.5, 0.5, 0.2) (dash), and (2.5, 0.5, 0.4) (dash dot). (a) |Sfx6(ω)| in log. (b) Phase of Sfx6(ω).
Figure 23. Cross-PSD response Sfx6(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (α, β, λ) = (1.6, 0.5, 0.2) (solid), (1.6, 1.5, 0.4) (dot), (2.5, 0.5, 0.2) (dash), and (2.5, 0.5, 0.4) (dash dot). (a) |Sfx6(ω)| in log. (b) Phase of Sfx6(ω).
Symmetry 16 00635 g023
Figure 24. Plots of |H7(ω)|2 (log) when m = 1, c = 0.1, and k = 36 for (β, λ) = (0.5, 0.2) (solid), (0.5, 0.3) (dot), (1.5, 0.4) (dash), and (1.5, 0.1) (dash dot).
Figure 24. Plots of |H7(ω)|2 (log) when m = 1, c = 0.1, and k = 36 for (β, λ) = (0.5, 0.2) (solid), (0.5, 0.3) (dot), (1.5, 0.4) (dash), and (1.5, 0.1) (dash dot).
Symmetry 16 00635 g024
Figure 25. Response of PSD Sxx7(ω) in log when m = 1, c = 0.1, k = 36, and H = 0.75 for (β, λ) = (0.5, 0.2) (solid), (0.5, 0.3) (dot), (1.5, 0.4) (dash), and (1.5, 0.1) (dash dot).
Figure 25. Response of PSD Sxx7(ω) in log when m = 1, c = 0.1, k = 36, and H = 0.75 for (β, λ) = (0.5, 0.2) (solid), (0.5, 0.3) (dot), (1.5, 0.4) (dash), and (1.5, 0.1) (dash dot).
Symmetry 16 00635 g025
Figure 26. Cross-PSD response Sfx7(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (β, λ) = (0.5, 0.2) (solid), (0.5, 0.3) (dot), (1.5, 0.4) (dash), and (1.5, 0.1) (dash dot). (a) |Sfx7(ω)|. (b) Phase of Sfx7(ω).
Figure 26. Cross-PSD response Sfx7(ω) when m = 1, c = 0.1, k = 36, and H = 0.75 for (β, λ) = (0.5, 0.2) (solid), (0.5, 0.3) (dot), (1.5, 0.4) (dash), and (1.5, 0.1) (dash dot). (a) |Sfx7(ω)|. (b) Phase of Sfx7(ω).
Symmetry 16 00635 g026
Figure 27. Plots of PSD of Sff(t, ω) when writing Sff(t, ω) = Sff for ω = 0, …, 6 and t = 0, …, 120, and H = 075. (a) PSD in surface plot. (b) PSD in contour plot.
Figure 27. Plots of PSD of Sff(t, ω) when writing Sff(t, ω) = Sff for ω = 0, …, 6 and t = 0, …, 120, and H = 075. (a) PSD in surface plot. (b) PSD in contour plot.
Symmetry 16 00635 g027
Figure 28. Plots of |H1(ω)|2 with α = 1.6 (solid), 2.3 (dot), and 2.5 (dash) when m = 1 and k = 36.
Figure 28. Plots of |H1(ω)|2 with α = 1.6 (solid), 2.3 (dot), and 2.5 (dash) when m = 1 and k = 36.
Symmetry 16 00635 g028
Figure 29. Plots of Sxx1(t, ω) for m = 1, k = 36, and H = 0.75 when writing Sxx1(t, ω) = Sxx1 for ω = 0, …, 6 and t = 0, …, 120. (a) PSD in surface plot (α = 1.8). (b) PSD in contour plot (α = 1.8). (c) PSD in contour plot (α = 2.8).
Figure 29. Plots of Sxx1(t, ω) for m = 1, k = 36, and H = 0.75 when writing Sxx1(t, ω) = Sxx1 for ω = 0, …, 6 and t = 0, …, 120. (a) PSD in surface plot (α = 1.8). (b) PSD in contour plot (α = 1.8). (c) PSD in contour plot (α = 2.8).
Symmetry 16 00635 g029
Figure 30. H effects on Sxx1(t, ω) when α = 1.8, m = 1, k = 36 when writing Sxx1(t, ω) = Sxx1 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx1(t, ω) for H = 0.95. (b) Sxx1(t, ω) for H = 0.15.
Figure 30. H effects on Sxx1(t, ω) when α = 1.8, m = 1, k = 36 when writing Sxx1(t, ω) = Sxx1 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx1(t, ω) for H = 0.95. (b) Sxx1(t, ω) for H = 0.15.
Symmetry 16 00635 g030
Figure 31. Illustrations of cross-PSD responses for m = 1, k = 36, and H = 0.75 with α = 1.8 when writing |Sfx1(t, ω)| = Sfx1 for ω = 0, …, 6 and t = 0, …, 120.
Figure 31. Illustrations of cross-PSD responses for m = 1, k = 36, and H = 0.75 with α = 1.8 when writing |Sfx1(t, ω)| = Sfx1 for ω = 0, …, 6 and t = 0, …, 120.
Symmetry 16 00635 g031
Figure 32. H effects on |Sfx1(t, ω)| when m = 1, k = 36 and α = 1.8 when writing |Sfx1(t, ω)| = Sfx1 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx1(t, ω)| for H = 0.95. (b) |Sfx1(t, ω)| for H = 0.55. (c) |Sfx1(t, ω)| for H = 0.35. (d) |Sfx1(t, ω)| for H = 0.15.
Figure 32. H effects on |Sfx1(t, ω)| when m = 1, k = 36 and α = 1.8 when writing |Sfx1(t, ω)| = Sfx1 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx1(t, ω)| for H = 0.95. (b) |Sfx1(t, ω)| for H = 0.55. (c) |Sfx1(t, ω)| for H = 0.35. (d) |Sfx1(t, ω)| for H = 0.15.
Symmetry 16 00635 g032aSymmetry 16 00635 g032b
Figure 33. Plots of |H2(ω)|2 (log) with β = 0.1 (solid) and 1.9 (dot) when m = 1, c = 0.1, and k = 36.
Figure 33. Plots of |H2(ω)|2 (log) with β = 0.1 (solid) and 1.9 (dot) when m = 1, c = 0.1, and k = 36.
Symmetry 16 00635 g033
Figure 34. Plots of Sxx2(t, ω) with m = 1, c = 0.1, and k = 36 for H = 0.75 when writing Sxx2(t, ω) = Sxx2 for ω = 0, …, 6 and t = 0, …, 120. (a) Surface plot of Sxx2(t, ω) for β = 0.8. (b) Contour plot of Sxx2(t, ω) for β = 0.8. (c) Surface plot of Sxx2(t, ω) for β = 1.8. (d) Contour plot of Sxx2(t, ω) for β = 1.8.
Figure 34. Plots of Sxx2(t, ω) with m = 1, c = 0.1, and k = 36 for H = 0.75 when writing Sxx2(t, ω) = Sxx2 for ω = 0, …, 6 and t = 0, …, 120. (a) Surface plot of Sxx2(t, ω) for β = 0.8. (b) Contour plot of Sxx2(t, ω) for β = 0.8. (c) Surface plot of Sxx2(t, ω) for β = 1.8. (d) Contour plot of Sxx2(t, ω) for β = 1.8.
Symmetry 16 00635 g034
Figure 35. Plots of H effects on Sxx2(t, ω) with β = 1.8, m = 1, c = 0.1, and k = 36 when writing Sxx2(t, ω) = Sxx2 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx2(t, ω) for H = 0.95. (b) Sxx2(t, ω) for H = 0.15.
Figure 35. Plots of H effects on Sxx2(t, ω) with β = 1.8, m = 1, c = 0.1, and k = 36 when writing Sxx2(t, ω) = Sxx2 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx2(t, ω) for H = 0.95. (b) Sxx2(t, ω) for H = 0.15.
Symmetry 16 00635 g035
Figure 36. Plots of |Sfx2(t, ω)| when m = 1, c = 0.1, k = 36, and (β, H) = (0.8, 0.75) when writing |Sfx2(t, ω)| = Sfx2 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx2(t, ω)| in surface plot. (b) Sfx2(t, ω) in contour plot.
Figure 36. Plots of |Sfx2(t, ω)| when m = 1, c = 0.1, k = 36, and (β, H) = (0.8, 0.75) when writing |Sfx2(t, ω)| = Sfx2 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx2(t, ω)| in surface plot. (b) Sfx2(t, ω) in contour plot.
Symmetry 16 00635 g036
Figure 37. Response of |Sfx2(t, ω)| when m = 1, c = 0.1, k = 36, and H = 0.75 when writing |Sfx2(t, ω)| = Sfx2 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx2(t, ω)| for β = 1.2. (b) |Sfx2(t, ω)| for β = 1.8.
Figure 37. Response of |Sfx2(t, ω)| when m = 1, c = 0.1, k = 36, and H = 0.75 when writing |Sfx2(t, ω)| = Sfx2 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx2(t, ω)| for β = 1.2. (b) |Sfx2(t, ω)| for β = 1.8.
Symmetry 16 00635 g037
Figure 38. Plots of |H3(ω)|2 when m = 1, c = 0.1, and k = 36, for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.4, 0.8) (dash).
Figure 38. Plots of |H3(ω)|2 when m = 1, c = 0.1, and k = 36, for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.4, 0.8) (dash).
Symmetry 16 00635 g038
Figure 39. Plots of Sxx3(t, ω) with m = 1, c = 0.1, and k = 36 when writing Sxx3(t, ω) = Sxx3 for ω = 0, …, 6 and t = 0, …, 120. (a) PSD in surface plot for (α, β) = (1.8, 0.8) and H = 0.75. (b) PSD in contour plot for (α, β) = (1.8, 0.8) and H = 0.75. (c) PSD in contour plot for (α, β) = (2.8, 1.8) and H = 0.75. (d) PSD in contour plot for (α, β) = (2.8, 0.8) and H = 0.35.
Figure 39. Plots of Sxx3(t, ω) with m = 1, c = 0.1, and k = 36 when writing Sxx3(t, ω) = Sxx3 for ω = 0, …, 6 and t = 0, …, 120. (a) PSD in surface plot for (α, β) = (1.8, 0.8) and H = 0.75. (b) PSD in contour plot for (α, β) = (1.8, 0.8) and H = 0.75. (c) PSD in contour plot for (α, β) = (2.8, 1.8) and H = 0.75. (d) PSD in contour plot for (α, β) = (2.8, 0.8) and H = 0.35.
Symmetry 16 00635 g039
Figure 40. Plots of |Sfx3(t, ω)| with m = 1, c = 0.1, and k = 36 when writing |Sfx3(t, ω)| = Sfx3 for ω = 0, …, 6 and t = 0, …, 120. (a) Surface plot when H = 0.75 for (α, β) = (1.8, 0.8). (b) Contour plot when H = 0.75 for (α, β) = (1.8, 0.8). (c) Surface plot when H = 0.35 for (α, β) = (1.8, 0.8). (d) Contour plot when H = 0.35 for (α, β) = (1.8, 0.8).
Figure 40. Plots of |Sfx3(t, ω)| with m = 1, c = 0.1, and k = 36 when writing |Sfx3(t, ω)| = Sfx3 for ω = 0, …, 6 and t = 0, …, 120. (a) Surface plot when H = 0.75 for (α, β) = (1.8, 0.8). (b) Contour plot when H = 0.75 for (α, β) = (1.8, 0.8). (c) Surface plot when H = 0.35 for (α, β) = (1.8, 0.8). (d) Contour plot when H = 0.35 for (α, β) = (1.8, 0.8).
Symmetry 16 00635 g040
Figure 41. Plots of |H4(ω)|2 when m = 1, c = 0, and k = 36, for (α, λ) = (2.1, 0.1) (solid), (2.3, 0.3) (dot), and (2.5, 0.5) (dash).
Figure 41. Plots of |H4(ω)|2 when m = 1, c = 0, and k = 36, for (α, λ) = (2.1, 0.1) (solid), (2.3, 0.3) (dot), and (2.5, 0.5) (dash).
Symmetry 16 00635 g041
Figure 42. Plots of Sxx4(t, ω) with m = 1, c = 0, and k = 36 when writing Sxx4(t, ω) = Sxx4 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx4(t, ω) when H = 0.75 for (α, λ) = (1.8, 0.8). (b) Sxx4(t, ω) when H = 0.35 for (α, λ) = (1.8, 0.8). (c) Sxx4(t, ω) when H = 0.75 for (α, λ) = (1.8, 0.2).
Figure 42. Plots of Sxx4(t, ω) with m = 1, c = 0, and k = 36 when writing Sxx4(t, ω) = Sxx4 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx4(t, ω) when H = 0.75 for (α, λ) = (1.8, 0.8). (b) Sxx4(t, ω) when H = 0.35 for (α, λ) = (1.8, 0.8). (c) Sxx4(t, ω) when H = 0.75 for (α, λ) = (1.8, 0.2).
Symmetry 16 00635 g042
Figure 43. Plots of |Sfx4(t, ω)| with m = 1, c = 0, and k = 36 when writing |Sfx4(t, ω)| = Sfx4 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx4(t, ω)| for (α, λ) = (1.8, 0.8) and H = 0.75. (b) |Sfx4(t, ω)| for (α, λ) = (1.8, 0.8) and H = 0.95.
Figure 43. Plots of |Sfx4(t, ω)| with m = 1, c = 0, and k = 36 when writing |Sfx4(t, ω)| = Sfx4 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx4(t, ω)| for (α, λ) = (1.8, 0.8) and H = 0.75. (b) |Sfx4(t, ω)| for (α, λ) = (1.8, 0.8) and H = 0.95.
Symmetry 16 00635 g043
Figure 44. Plots of |H5(ω)|2 when m = 1, c = 0, and k = 36, for λ = 0.2 (solid), 0.10 (dot), 0.15 (dash), and 0.20 (dash dot).
Figure 44. Plots of |H5(ω)|2 when m = 1, c = 0, and k = 36, for λ = 0.2 (solid), 0.10 (dot), 0.15 (dash), and 0.20 (dash dot).
Symmetry 16 00635 g044
Figure 45. Plots of Sxx5(t, ω) with m = 1, c = 0, and k = 36 when writing Sxx5(t, ω) = Sxx5 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx5(t, ω) when H = 0.75 and λ = 0.2. (b) Sxx5(t, ω) when H = 0.75 and λ = 0.8. (c) Sxx5(t, ω) when H = 0.35 and λ = 0.2.
Figure 45. Plots of Sxx5(t, ω) with m = 1, c = 0, and k = 36 when writing Sxx5(t, ω) = Sxx5 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx5(t, ω) when H = 0.75 and λ = 0.2. (b) Sxx5(t, ω) when H = 0.75 and λ = 0.8. (c) Sxx5(t, ω) when H = 0.35 and λ = 0.2.
Symmetry 16 00635 g045
Figure 46. Plots of |Sfx5(t, ω)| with m = 1, c = 0, and k = 36 when writing |Sfx5(t, ω)| = Sfx5 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx5(t, ω)| when H = 0.75 and λ = 0.2. (b) |Sfx5(t, ω)| when H = 0.35 and λ = 0.2.
Figure 46. Plots of |Sfx5(t, ω)| with m = 1, c = 0, and k = 36 when writing |Sfx5(t, ω)| = Sfx5 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx5(t, ω)| when H = 0.75 and λ = 0.2. (b) |Sfx5(t, ω)| when H = 0.35 and λ = 0.2.
Symmetry 16 00635 g046
Figure 47. Plots of |H6(ω)|2 when m = 1, c = 0.1, and k = 36, for (α, β, λ) = (2.1, 0.8, 0.15) (solid), (2.2, 1.2, 0.20) (dot), and (2.3, 1.6, 0.25) (dash).
Figure 47. Plots of |H6(ω)|2 when m = 1, c = 0.1, and k = 36, for (α, β, λ) = (2.1, 0.8, 0.15) (solid), (2.2, 1.2, 0.20) (dot), and (2.3, 1.6, 0.25) (dash).
Symmetry 16 00635 g047
Figure 48. Plots of Sxx6(t, ω) with m = 1, c = 0.1, and k = 36 when writing Sxx6(t, ω) = Sxx6. (a) Sxx6(t, ω) when H = 0.75 and (α, β, λ) = (1.8, 0.8, 0.2) when writing Sxx6(t, ω) = Sxx6 for ω = 0, …, 6 and t = 0, …, 120. (b) Sxx6(t, ω) when H = 0.75 and (α, β, λ) = (1.8, 1.8, 0.8). (c) Sxx6(t, ω) when H = 0.35 and (α, β, λ) = (1.8, 0.8, 0.2).
Figure 48. Plots of Sxx6(t, ω) with m = 1, c = 0.1, and k = 36 when writing Sxx6(t, ω) = Sxx6. (a) Sxx6(t, ω) when H = 0.75 and (α, β, λ) = (1.8, 0.8, 0.2) when writing Sxx6(t, ω) = Sxx6 for ω = 0, …, 6 and t = 0, …, 120. (b) Sxx6(t, ω) when H = 0.75 and (α, β, λ) = (1.8, 1.8, 0.8). (c) Sxx6(t, ω) when H = 0.35 and (α, β, λ) = (1.8, 0.8, 0.2).
Symmetry 16 00635 g048
Figure 49. Plots of |Sfx6(t, ω)| with m = 1, c = 0.1, and k = 36 when writing |Sfx6(t, ω)| = Sfx6 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx6(t, ω)| when H = 0.75 and (α, β, λ) = (1.8, 0.8, 0.2). (b) |Sfx6(t, ω)| when H = 0.35 and (α, β, λ) = (1.8, 0.8, 0.2).
Figure 49. Plots of |Sfx6(t, ω)| with m = 1, c = 0.1, and k = 36 when writing |Sfx6(t, ω)| = Sfx6 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx6(t, ω)| when H = 0.75 and (α, β, λ) = (1.8, 0.8, 0.2). (b) |Sfx6(t, ω)| when H = 0.35 and (α, β, λ) = (1.8, 0.8, 0.2).
Symmetry 16 00635 g049
Figure 50. Plots of |H7(ω)|2 (log) when m = 1, c = 0.1, and k = 36, for (β, λ) = (0.5, 0.20) (solid), (1.0, 0.25) (dot), and (1.5, 0.30) (dash).
Figure 50. Plots of |H7(ω)|2 (log) when m = 1, c = 0.1, and k = 36, for (β, λ) = (0.5, 0.20) (solid), (1.0, 0.25) (dot), and (1.5, 0.30) (dash).
Symmetry 16 00635 g050
Figure 51. Plots of Sxx7(t, ω) with m = 1, c = 0.1, and k = 36 when writing Sxx7(t, ω) = Sxx7 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx7(t, ω) when H = 0.75 and (β, λ) = (0.8, 0.2). (b) Sxx7(t, ω) when H = 0.75 and (β, λ) = (0.8, 0.8). (c) Sxx7(t, ω) when H = 0.35 and (β, λ) = (0.8, 0.8).
Figure 51. Plots of Sxx7(t, ω) with m = 1, c = 0.1, and k = 36 when writing Sxx7(t, ω) = Sxx7 for ω = 0, …, 6 and t = 0, …, 120. (a) Sxx7(t, ω) when H = 0.75 and (β, λ) = (0.8, 0.2). (b) Sxx7(t, ω) when H = 0.75 and (β, λ) = (0.8, 0.8). (c) Sxx7(t, ω) when H = 0.35 and (β, λ) = (0.8, 0.8).
Symmetry 16 00635 g051
Figure 52. Plots of |Sfx7(t, ω)| with m = 1, c = 0.1, and k = 36 when writing |Sfx7(t, ω)| = Sxx7 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx7(t, ω)| for H = 0.75 and (β, λ) = (0.8, 0.2). (b) |Sfx7(t, ω)| for H = 0.35 and (β, λ) = (0.8, 0.2). (c) |Sfx7(t, ω)| for H = 0.75 and (β, λ) = (1.8, 1.8). (d) |Sfx7(t, ω)| for H = 0.35 and (β, λ) = (1.8, 1.8).
Figure 52. Plots of |Sfx7(t, ω)| with m = 1, c = 0.1, and k = 36 when writing |Sfx7(t, ω)| = Sxx7 for ω = 0, …, 6 and t = 0, …, 120. (a) |Sfx7(t, ω)| for H = 0.75 and (β, λ) = (0.8, 0.2). (b) |Sfx7(t, ω)| for H = 0.35 and (β, λ) = (0.8, 0.2). (c) |Sfx7(t, ω)| for H = 0.75 and (β, λ) = (1.8, 1.8). (d) |Sfx7(t, ω)| for H = 0.35 and (β, λ) = (1.8, 1.8).
Symmetry 16 00635 g052
Figure 53. Plots of PSD of fractional OU processes for b = 0.2 (solid), 0.6 (dot), 1 (dash), and 1.3 (dash dot).
Figure 53. Plots of PSD of fractional OU processes for b = 0.2 (solid), 0.6 (dot), 1 (dash), and 1.3 (dash dot).
Symmetry 16 00635 g053
Figure 54. Plots of |H1(ω)|2 with α = 1.7 (solid), 1.8 (dot), and 1.9 (dash) when m = 1 and k = 36.
Figure 54. Plots of |H1(ω)|2 with α = 1.7 (solid), 1.8 (dot), and 1.9 (dash) when m = 1 and k = 36.
Symmetry 16 00635 g054
Figure 55. Plots of Sxx1(ω) for m = 1 and k = 36 when (α, b) = (1.7, 0.2) (solid), (1.8, 0.2) (dot), (1.5, 1) (dash), and (1.9, 0.2) (dash dot).
Figure 55. Plots of Sxx1(ω) for m = 1 and k = 36 when (α, b) = (1.7, 0.2) (solid), (1.8, 0.2) (dot), (1.5, 1) (dash), and (1.9, 0.2) (dash dot).
Symmetry 16 00635 g055
Figure 56. Observing the effects of b on Sxx1(ω) with α = 2.5 for b = 0.2 (solid), 0.6 (dot), 1 (dash), and 1.3 (dash dot).
Figure 56. Observing the effects of b on Sxx1(ω) with α = 2.5 for b = 0.2 (solid), 0.6 (dot), 1 (dash), and 1.3 (dash dot).
Symmetry 16 00635 g056
Figure 57. Illustrations of |Sfx1(ω)|. (a) |Sfx1(ω)| for m = 1 and k = 36 when (α, b) = (1.4, 0.2) (solid), (1.8, 0.2) (dot), (2.2, 0.2) (dash), and (2.6, 0.2) (dash dot). (b) |Sfx1(ω)| for m = 1 and k = 36 when (α, b) = (1.4, 0.8) (solid), (1.8, 0.8) (dot), (2.2, 0.8) (dash), and (2.6, 0.8) (dash dot).
Figure 57. Illustrations of |Sfx1(ω)|. (a) |Sfx1(ω)| for m = 1 and k = 36 when (α, b) = (1.4, 0.2) (solid), (1.8, 0.2) (dot), (2.2, 0.2) (dash), and (2.6, 0.2) (dash dot). (b) |Sfx1(ω)| for m = 1 and k = 36 when (α, b) = (1.4, 0.8) (solid), (1.8, 0.8) (dot), (2.2, 0.8) (dash), and (2.6, 0.8) (dash dot).
Symmetry 16 00635 g057
Figure 58. Plots of driven fractional OU signal and response signal when m = 1, k = 36. (a) Driven fractional OU signal for b = 0.2. (b) Driven fractional OU signal for b = 0.8. (c) Response of x1(t) for (α, b) = (1.8, 0.2). (d) Response of x1(t) for (α, b) = (1.2, 0.8).
Figure 58. Plots of driven fractional OU signal and response signal when m = 1, k = 36. (a) Driven fractional OU signal for b = 0.2. (b) Driven fractional OU signal for b = 0.8. (c) Response of x1(t) for (α, b) = (1.8, 0.2). (d) Response of x1(t) for (α, b) = (1.2, 0.8).
Symmetry 16 00635 g058
Figure 59. Plots of |H2(ω)|2 (log) with β = 0.1 (solid) and 1.9 (dot) when m = 1, c = 0.1, and k = 36.
Figure 59. Plots of |H2(ω)|2 (log) with β = 0.1 (solid) and 1.9 (dot) when m = 1, c = 0.1, and k = 36.
Symmetry 16 00635 g059
Figure 60. Plots of Sxx2(ω) (log) with β = 0.1 (solid) and 1.9 (dot) when m = 1, c = 0.1, and k = 36 for b = 0.2.
Figure 60. Plots of Sxx2(ω) (log) with β = 0.1 (solid) and 1.9 (dot) when m = 1, c = 0.1, and k = 36 for b = 0.2.
Symmetry 16 00635 g060
Figure 61. Plots of Sxx2(ω) (log) with β = 1, m = 1, c = 0.1, and k = 36 for b = 0.2 (solid), 1 (dot), and 10 (dash).
Figure 61. Plots of Sxx2(ω) (log) with β = 1, m = 1, c = 0.1, and k = 36 for b = 0.2 (solid), 1 (dot), and 10 (dash).
Symmetry 16 00635 g061
Figure 62. Plots of |Sfx2(ω)| when m = 1, c = 0.1, and k = 36. (a) |Sfx2(ω)| (log) with (β, b) = (0.1, 0.5) (solid), (1, 0.5) (dot), and (1.9, 0.5) (dash). (b) |Sfx2(ω)| (log) with (β, b) = (1, 0.2) (solid), (1, 0.8) (dot), and (1, 1.5) (dash).
Figure 62. Plots of |Sfx2(ω)| when m = 1, c = 0.1, and k = 36. (a) |Sfx2(ω)| (log) with (β, b) = (0.1, 0.5) (solid), (1, 0.5) (dot), and (1.9, 0.5) (dash). (b) |Sfx2(ω)| (log) with (β, b) = (1, 0.2) (solid), (1, 0.8) (dot), and (1, 1.5) (dash).
Symmetry 16 00635 g062
Figure 63. Response of x2(t) when m = 1, c = 0.1, and k = 36, and b = 0.5. (a) x2(t) for β = 0.4. (b) x2(t) for β = 1.4.
Figure 63. Response of x2(t) when m = 1, c = 0.1, and k = 36, and b = 0.5. (a) x2(t) for β = 0.4. (b) x2(t) for β = 1.4.
Symmetry 16 00635 g063
Figure 64. Plots of |H3(ω)|2 when m = 1, c = 0.1, and k = 36, for (α, β) = (1.6, 0.1) (solid), (1.8, 1.8) (dot), and (2.2, 0.1) (dash).
Figure 64. Plots of |H3(ω)|2 when m = 1, c = 0.1, and k = 36, for (α, β) = (1.6, 0.1) (solid), (1.8, 1.8) (dot), and (2.2, 0.1) (dash).
Symmetry 16 00635 g064
Figure 65. Plots of Sxx3(ω) when m = 1, c = 0.1, and k = 36 when (α, β) = (1.6, 0.1) (solid), (1.8, 1.8) (dot), and (2.2, 0.1) (dash) for b = 0.8.
Figure 65. Plots of Sxx3(ω) when m = 1, c = 0.1, and k = 36 when (α, β) = (1.6, 0.1) (solid), (1.8, 1.8) (dot), and (2.2, 0.1) (dash) for b = 0.8.
Symmetry 16 00635 g065
Figure 66. Plots of |Sfx3(ω)| when m = 1, c = 0.1, and k = 36 for (α, β) = (1.6, 0.1) (solid), (1.8, 1.8) (dot), and (2.2, 0.1) (dash) when b = 0.8.
Figure 66. Plots of |Sfx3(ω)| when m = 1, c = 0.1, and k = 36 for (α, β) = (1.6, 0.1) (solid), (1.8, 1.8) (dot), and (2.2, 0.1) (dash) when b = 0.8.
Symmetry 16 00635 g066
Figure 67. Plots of |H4(ω)|2 when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.3, 0.4) (dot), and (2.3, 0.3) (dash).
Figure 67. Plots of |H4(ω)|2 when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.3, 0.4) (dot), and (2.3, 0.3) (dash).
Symmetry 16 00635 g067
Figure 68. Plots of Sxx4(ω) when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.3, 0.4) (dot), and (2.5, 0.3) (dash) for b = 0.2.
Figure 68. Plots of Sxx4(ω) when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.3, 0.4) (dot), and (2.5, 0.3) (dash) for b = 0.2.
Symmetry 16 00635 g068
Figure 69. Plots of |Sfx4(ω)| when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.3, 0.4) (dot), and (2.5, 0.3) (dash) for b = 0.2.
Figure 69. Plots of |Sfx4(ω)| when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.3, 0.4) (dot), and (2.5, 0.3) (dash) for b = 0.2.
Symmetry 16 00635 g069
Figure 70. Plots of |H5(ω)|2 when m = 1, c = 0, and k = 36 for λ = 0.15 (solid), 0.17 (dot), and 0.19 (dash).
Figure 70. Plots of |H5(ω)|2 when m = 1, c = 0, and k = 36 for λ = 0.15 (solid), 0.17 (dot), and 0.19 (dash).
Symmetry 16 00635 g070
Figure 71. Plots of Sxx5(ω) when m = 1, c = 0, and k = 36 for λ = 0.15 (solid), 0.17 (dot), and 0.19 (dash) for b = 0.2.
Figure 71. Plots of Sxx5(ω) when m = 1, c = 0, and k = 36 for λ = 0.15 (solid), 0.17 (dot), and 0.19 (dash) for b = 0.2.
Symmetry 16 00635 g071
Figure 72. Plots of |Sfx5(ω)| when m = 1, c = 0, and k = 36 for λ = 0.15 (solid), 0.17 (dot), and 0.19 (dash) when b = 0.2.
Figure 72. Plots of |Sfx5(ω)| when m = 1, c = 0, and k = 36 for λ = 0.15 (solid), 0.17 (dot), and 0.19 (dash) when b = 0.2.
Symmetry 16 00635 g072
Figure 73. Plots of |H6(ω)|2 when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.7, 0.2) (solid), (2.2, 0.8, 0.3) (dot), and (2.3, 0.9, 0.4) (dash).
Figure 73. Plots of |H6(ω)|2 when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.7, 0.2) (solid), (2.2, 0.8, 0.3) (dot), and (2.3, 0.9, 0.4) (dash).
Symmetry 16 00635 g073
Figure 74. Plots of PSD response Sxx6(ω) when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.7, 0.2) (solid), (2.2, 0.8, 0.3) (dot), and (2.3, 0.9, 0.4) (dash) when b = 0.2.
Figure 74. Plots of PSD response Sxx6(ω) when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.7, 0.2) (solid), (2.2, 0.8, 0.3) (dot), and (2.3, 0.9, 0.4) (dash) when b = 0.2.
Symmetry 16 00635 g074
Figure 75. Plots of |Sfx6(ω)| when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.7, 0.2) (solid), (2.2, 0.8, 0.3) (dot), and (2.3, 0.9, 0.4) (dash) when b = 0.2.
Figure 75. Plots of |Sfx6(ω)| when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.7, 0.2) (solid), (2.2, 0.8, 0.3) (dot), and (2.3, 0.9, 0.4) (dash) when b = 0.2.
Symmetry 16 00635 g075
Figure 76. Plots of |H7(ω)|2 when m = 1, c = 0.1, and k = 36 for (β, λ) = (1.5, 0.12) (solid), (1.6, 0.14) (dot), and (1.6, 0.16) (dash).
Figure 76. Plots of |H7(ω)|2 when m = 1, c = 0.1, and k = 36 for (β, λ) = (1.5, 0.12) (solid), (1.6, 0.14) (dot), and (1.6, 0.16) (dash).
Symmetry 16 00635 g076
Figure 77. Plots of PSD response Sxx7(ω) when m = 1, c = 0.1, and k = 36 for (β, λ) = (1.5, 0.12) (solid), (1.6, 0.14) (dot), and (1.6, 0.16) (dash) for b = 0.2.
Figure 77. Plots of PSD response Sxx7(ω) when m = 1, c = 0.1, and k = 36 for (β, λ) = (1.5, 0.12) (solid), (1.6, 0.14) (dot), and (1.6, 0.16) (dash) for b = 0.2.
Symmetry 16 00635 g077
Figure 78. Plots of cross-PSD response |Sfx7(ω)| when m = 1, c = 0.1, and k = 36 for (β, λ) = (1.5, 0.12) (solid), (1.6, 0.14) (dot), and (1.6, 0.16) (dash) for b = 0.2.
Figure 78. Plots of cross-PSD response |Sfx7(ω)| when m = 1, c = 0.1, and k = 36 for (β, λ) = (1.5, 0.12) (solid), (1.6, 0.14) (dot), and (1.6, 0.16) (dash) for b = 0.2.
Symmetry 16 00635 g078
Figure 79. Plots of von Kármán spectrum with σu = 10 when U = 45 (solid), 30 (dot), and 15 (dash).
Figure 79. Plots of von Kármán spectrum with σu = 10 when U = 45 (solid), 30 (dot), and 15 (dash).
Symmetry 16 00635 g079
Figure 80. Plots of |H1(ω)|2 with α = 1.6 (solid), 1.7 (dot), and 1.8 (dash) when m = 1 and k = 36.
Figure 80. Plots of |H1(ω)|2 with α = 1.6 (solid), 1.7 (dot), and 1.8 (dash) when m = 1 and k = 36.
Symmetry 16 00635 g080
Figure 81. Plots of Sxx1(ω) for m = 1, k = 36, and U = 15 when α = 1.6 (solid), 1.7 (dot), and 1.8 (dash).
Figure 81. Plots of Sxx1(ω) for m = 1, k = 36, and U = 15 when α = 1.6 (solid), 1.7 (dot), and 1.8 (dash).
Symmetry 16 00635 g081
Figure 82. Observing U effects on Sxx1(ω) when α = 1.8, m = 1, and k = 36 for U = 40 (solid), 30 (dot), and 15 (dash).
Figure 82. Observing U effects on Sxx1(ω) when α = 1.8, m = 1, and k = 36 for U = 40 (solid), 30 (dot), and 15 (dash).
Symmetry 16 00635 g082
Figure 83. Illustrations of |Sfx1(ω)| for m = 1, k = 36, and U = 20 when α = 2.1 (solid), 2.2 (dot), and 2.3 (dash).
Figure 83. Illustrations of |Sfx1(ω)| for m = 1, k = 36, and U = 20 when α = 2.1 (solid), 2.2 (dot), and 2.3 (dash).
Symmetry 16 00635 g083
Figure 84. Plots of driven signal with the von Kármán spectrum and response series when m = 1, k = 36, and α = 1.8. (a) Driven signal for U = 45. (b) Driven signal for U = 5. (c) Response x1(t) for (α, U) = (1.2, 20). (d) Response x1(t) for (α, U) = (1.8, 20).
Figure 84. Plots of driven signal with the von Kármán spectrum and response series when m = 1, k = 36, and α = 1.8. (a) Driven signal for U = 45. (b) Driven signal for U = 5. (c) Response x1(t) for (α, U) = (1.2, 20). (d) Response x1(t) for (α, U) = (1.8, 20).
Symmetry 16 00635 g084
Figure 85. Plots of |H2(ω)|2 (log) with β = 0.001 (solid) and 1.999 (dot), when m = 1, c = 0.1, and k = 36.
Figure 85. Plots of |H2(ω)|2 (log) with β = 0.001 (solid) and 1.999 (dot), when m = 1, c = 0.1, and k = 36.
Symmetry 16 00635 g085
Figure 86. Plots of Sxx2(ω) (log) with β = 0.001 (solid) and 1.999 (dot) when m = 1, c = 0.1, k = 36, and U = 15.
Figure 86. Plots of Sxx2(ω) (log) with β = 0.001 (solid) and 1.999 (dot) when m = 1, c = 0.1, k = 36, and U = 15.
Symmetry 16 00635 g086
Figure 87. Plots of U effects on Sxx2(ω) with β = 1, m = 1, c = 0.1, and k = 36 for U = 45 (solid), 25 (dot), and 5 (dash).
Figure 87. Plots of U effects on Sxx2(ω) with β = 1, m = 1, c = 0.1, and k = 36 for U = 45 (solid), 25 (dot), and 5 (dash).
Symmetry 16 00635 g087
Figure 88. Plots of |Sfx2(ω)| (log) when m = 1, c = 0.1, and k = 36. with (β, U) = (0.001, 15) (solid), (β, U) = (1, 25) (dot), and (β, U) = (1.999, 35) (dash).
Figure 88. Plots of |Sfx2(ω)| (log) when m = 1, c = 0.1, and k = 36. with (β, U) = (0.001, 15) (solid), (β, U) = (1, 25) (dot), and (β, U) = (1.999, 35) (dash).
Symmetry 16 00635 g088
Figure 89. Response x2(t) when m = 1, c = 0.1, k = 36, and U = 35. (a) x2(t) for β = 0.4. (b) x2(t) for β = 1.4.
Figure 89. Response x2(t) when m = 1, c = 0.1, k = 36, and U = 35. (a) x2(t) for β = 0.4. (b) x2(t) for β = 1.4.
Symmetry 16 00635 g089
Figure 90. Plots of |H3(ω)|2 when m = 1, c = 0.1, and k = 36 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.3, 0.8) (dash).
Figure 90. Plots of |H3(ω)|2 when m = 1, c = 0.1, and k = 36 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.3, 0.8) (dash).
Symmetry 16 00635 g090
Figure 91. Plots of Sxx3(ω) when m = 1, c = 0.1, k = 36, and U = 15 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.3, 0.8) (dash).
Figure 91. Plots of Sxx3(ω) when m = 1, c = 0.1, k = 36, and U = 15 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.3, 0.8) (dash).
Symmetry 16 00635 g091
Figure 92. Plots of |Sfx3(ω)| when m = 1, c = 0.1, k = 36, and U = 15 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.3, 0.8) (dash).
Figure 92. Plots of |Sfx3(ω)| when m = 1, c = 0.1, k = 36, and U = 15 for (α, β) = (1.6, 0.8) (solid), (1.6, 1.8) (dot), and (2.3, 0.8) (dash).
Symmetry 16 00635 g092
Figure 93. Plots of |H4(ω)|2 when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.2, 0.3) (dot), and (2.3, 0.4) (dash).
Figure 93. Plots of |H4(ω)|2 when m = 1, c = 0, and k = 36 for (α, λ) = (2.1, 0.2) (solid), (2.2, 0.3) (dot), and (2.3, 0.4) (dash).
Symmetry 16 00635 g093
Figure 94. Plots of Sxx4(ω) when m = 1, c = 0, k = 36, and U = 15 for (α, λ) = (2.1, 0.2) (solid), (2.2, 0.3) (dot), and (2.3, 0.4) (dash).
Figure 94. Plots of Sxx4(ω) when m = 1, c = 0, k = 36, and U = 15 for (α, λ) = (2.1, 0.2) (solid), (2.2, 0.3) (dot), and (2.3, 0.4) (dash).
Symmetry 16 00635 g094
Figure 95. Plots of |Sfx4(ω)| when m = 1, c = 0, k = 36, and U = 15 for (α, λ) = (2.1, 0.2) (solid), (2.2, 0.3) (dot), and (2.3, 0.4) (dash).
Figure 95. Plots of |Sfx4(ω)| when m = 1, c = 0, k = 36, and U = 15 for (α, λ) = (2.1, 0.2) (solid), (2.2, 0.3) (dot), and (2.3, 0.4) (dash).
Symmetry 16 00635 g095
Figure 96. Plots of |H5(ω)|2 when m = 1, c = 0, and k = 36 for λ = 0.2 (solid), 0.3 (dot), and 0.4 (dash).
Figure 96. Plots of |H5(ω)|2 when m = 1, c = 0, and k = 36 for λ = 0.2 (solid), 0.3 (dot), and 0.4 (dash).
Symmetry 16 00635 g096
Figure 97. Plots of Sxx5(ω) when m = 1, c = 0, and k = 36 and U = 25 for λ = 0.2 (solid), 0.3 (dot), and 0.4 (dash).
Figure 97. Plots of Sxx5(ω) when m = 1, c = 0, and k = 36 and U = 25 for λ = 0.2 (solid), 0.3 (dot), and 0.4 (dash).
Symmetry 16 00635 g097
Figure 98. Plots of e |Sfx5(ω)| when m = 1, c = 0, k = 36, and U = 25 for λ = 0.2 (solid), 0.3 (dot), and 0.4 (dash).
Figure 98. Plots of e |Sfx5(ω)| when m = 1, c = 0, k = 36, and U = 25 for λ = 0.2 (solid), 0.3 (dot), and 0.4 (dash).
Symmetry 16 00635 g098
Figure 99. Plots of |H6(ω)|2 when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.8, 0.2) (solid), (2.2, 1.2, 0.4) (dot), and (2.3, 1.6, 0.4) (dash).
Figure 99. Plots of |H6(ω)|2 when m = 1, c = 0.1, and k = 36 for (α, β, λ) = (2.1, 0.8, 0.2) (solid), (2.2, 1.2, 0.4) (dot), and (2.3, 1.6, 0.4) (dash).
Symmetry 16 00635 g099
Figure 100. Plots of Sxx6(ω) when m = 1, c = 0.1, k = 36, and U = 15 for (α, β, λ) = (2.1, 0.8, 0.2) (solid), (2.2, 1.2, 0.3) (dot), and (2.3, 1.6, 0.4) (dash).
Figure 100. Plots of Sxx6(ω) when m = 1, c = 0.1, k = 36, and U = 15 for (α, β, λ) = (2.1, 0.8, 0.2) (solid), (2.2, 1.2, 0.3) (dot), and (2.3, 1.6, 0.4) (dash).
Symmetry 16 00635 g100
Figure 101. Plots of |Sfx6(ω)| when m = 1, c = 0.1, k = 36, and U = 15 for (α, β, λ) = (2.1, 0.8, 0.2) (solid), (2.2, 1.2, 0.3) (dot), and (2.3, 1.6, 0.4) (dash).
Figure 101. Plots of |Sfx6(ω)| when m = 1, c = 0.1, k = 36, and U = 15 for (α, β, λ) = (2.1, 0.8, 0.2) (solid), (2.2, 1.2, 0.3) (dot), and (2.3, 1.6, 0.4) (dash).
Symmetry 16 00635 g101
Figure 102. Plots of |H7(ω)|2 when m = 1, c = 0.1, and k = 36 for (β, λ) = (0.5, 0.15) (solid), (0.6, 0.20) (dot), and (0.7, 0.25) (dash).
Figure 102. Plots of |H7(ω)|2 when m = 1, c = 0.1, and k = 36 for (β, λ) = (0.5, 0.15) (solid), (0.6, 0.20) (dot), and (0.7, 0.25) (dash).
Symmetry 16 00635 g102
Figure 103. Plots of Sxx7(ω) when m = 1, c = 0.1, k = 36, and U = 15 for (β, λ) = (0.01, 0.03) (solid), (1.00, 0.06) (dot), and (1.99, 0.09) (dash).
Figure 103. Plots of Sxx7(ω) when m = 1, c = 0.1, k = 36, and U = 15 for (β, λ) = (0.01, 0.03) (solid), (1.00, 0.06) (dot), and (1.99, 0.09) (dash).
Symmetry 16 00635 g103
Figure 104. Plots of |Sfx7(ω)| when m = 1, c = 0.1, k = 36, and U = 15 for (β, λ) = (0.01, 0.03) (solid), (1.00, 0.06) (dot), and (1.99, 0.09) (dash).
Figure 104. Plots of |Sfx7(ω)| when m = 1, c = 0.1, k = 36, and U = 15 for (β, λ) = (0.01, 0.03) (solid), (1.00, 0.06) (dot), and (1.99, 0.09) (dash).
Symmetry 16 00635 g104
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MDPI and ACS Style

Li, M. PSD and Cross-PSD of Responses of Seven Classes of Fractional Vibrations Driven by fGn, fBm, Fractional OU Process, and von Kármán Process. Symmetry 2024, 16, 635. https://doi.org/10.3390/sym16050635

AMA Style

Li M. PSD and Cross-PSD of Responses of Seven Classes of Fractional Vibrations Driven by fGn, fBm, Fractional OU Process, and von Kármán Process. Symmetry. 2024; 16(5):635. https://doi.org/10.3390/sym16050635

Chicago/Turabian Style

Li, Ming. 2024. "PSD and Cross-PSD of Responses of Seven Classes of Fractional Vibrations Driven by fGn, fBm, Fractional OU Process, and von Kármán Process" Symmetry 16, no. 5: 635. https://doi.org/10.3390/sym16050635

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