The equivalent linearization method (ELM) is one of the most
commonly used methods and is an effective method for nonlinear
systems with weak nonlinear coefficients. For nonlinear systems
with larger nonlinear coefficients, the accuracy of this method is
significantly reduced. The dissertation focuses on researching and
developing EL method to improve errors when analyzing nonlinear
oscillations.
                
              
                                            
                                
            
 
            
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covariance. 
1.3 Some special stochastic processes 
There are definitions of: Stationary random processes and 
Ergodic process; Normal random process or Gaussian process; White 
noise process; colored noise process; Wiener process and Markov 
process. 
1.4 Some approximately analytical methods for analyzing 
random oscillation 
Numerical methods, approximately analytical methods are very 
popular methods. In detail, there are some useful methods in this 
dissertation [29-31]: 
- Perturbation technique. 
- Fokker-Planck-Kolmogorov (FPK) equation technique. 
- Stochastic averaging technique. 
- Statistical linearization technique. 
 1.5 Fokker-Planck-Kolmogorov (FPK) equation technique and 
Stochastic averaging technique 
1.6 Overview of studies on random oscillations 
 The problem of random vibrations has been studied and 
presented in many textbooks [26–33]. Oscillation analysis based on 
nonlinear mathematical models requires appropriate methods. In the 
theory of random oscillation, the stochastic equivalent linearization 
method (ELM) replacing the nonlinear system by an equivalent 
linear system is a common method because it preserves some 
essential properties of the original nonlinear system. This method has 
been described in many review papers [42, 43] and summarized in 
monographs [29] and [44]. 
4 
Although the accuracy of EL methods may not be high, this is 
overcome by improved techniques [43]. Canor et al. [45] also wrote: 
Thanks to its easy and fast implementation technique, the equivalent 
linearization method has become a universal probability approach for 
analyzing large nonlinear structures. The EL method has been used 
in many research papers. A EL based on analytic method was 
developed in [46, 47] to analyze nonlinear energy extraction 
systems. The nonlinear oscillation system of the wing profile was 
studied in [48, 49] by using EL method. Silva - Gonzlez et al. [52] 
used the stochastic EL method to study elastic non-linear structure of 
seismic load. 
 In Vietnam, the dissertation of Nguyen Ngoc Linh [4] analyzed 
the nonlinear random oscillation of systems of 1 degree of freedom 
by the stochastic EL method according to the weighted duality 
criteria. The dissertation of Nguyen Nhu Hieu [5] has developed the 
duality criterion in EL method for multi-degree-of-freedom nonlinear 
systems with random excitation. Nguyen Minh Triet has conducted a 
doctoral dissertation on the analysis of the response of the airplane 
wing profile according to the duality approach, in which the study of 
nonlinear periodic oscillation by EL method [6]. In his PhD 
dissertation in 2002 [7] Luu Xuan Hung developed the Local Mean 
Square Error Criterion (LOMSEC) based on the idea of replacing 
integral over infinite domain (-∞ , + ∞) equals the integral over a 
finite domain [-rx, + rx] where the system's response is 
concentrated. Continuing development of this research direction, the 
dissertation carried out by the PhD student will develop the Global-
Local Mean Square Error Criterion (GLOMSEC) of the EL method 
to nonlinear MDOF systems subjected to random excitation. In this 
development, a dual approach is used to address the finite domain of 
integration [-rx, + rx]. 
Conclusion of chapter 1 
Chapter 1 introduced some basic concepts and formulas for 
probability theory and random processes, and some methods of 
nonlinear random oscillation analysis. Some research results on 
nonlinear random oscillations related to the dissertation have also 
been reviewed and analyzed as the basis for the next chapters. 
5 
CHAPTER 2. EQUIVALENT LINEARIZATION METHOD 
AND GLOBAL-LOCAL MEAN SQUARE ERROR 
CRITERION 
2.1. The classical criterion of equivalent linearization 
We present the EL method for 1 DOF nonlinear random oscillator 
systems of type [9, 29, 44]: 
2
02 ( , ) ( )x hx x g x x t    
  
(2.10) 
Where, x , x and x are displacement, velocity and acceleration, 
respectively; h is damping coefficient, ( , )g x x is a nonlinear 
function, ( )t is Gaussian white noise excitation with intensity 
2 ; 0 is the natural frequency for 0h  , ( , ) 0g x x  . The 
equivalent linearization equation of (2.10) is as follows: 
2
02 ( )x hx x bx kx t     
  
(2.11) 
where b, k are equivalent linearization coefficients. The error 
between (2.10) và (2.11) satisfies the Mean Square Error Criterion 
proposed by Caughey [10]: 
 
2
d
,
( , ) mink
b k
S g x x bx kx    (2.14) 
Hence: 
kd kd0; 0
S S
b k
 
 
 
 (2.15) 
Assuming that the solution is a random process, the response x , x 
should be independent, that is 0xx  , solving the system of 
equations (2.15) we obtain 
 
2
,xg x x
b
x
 
,  
2
,xg x x
k
x
 (2.17) 
6 
Equations (2.11) và (2.17) forms a system of equations for 3 
unknowns x(t), b, k. Iterative algorithms are usually applied proposed 
by Atalik and Utku [59] as follows: 
a) Assign the initial value to the second order moments 2 2,x x . 
b) Use (2.17) to determine the linear coefficients. 
c) Solve equation (2.11) to find the new instantaneous second order 
moments 2 2,x x . 
d) Repeat b) and c) until the specified accuracy is reached. 
We consider the nonlinear system with multi degrees of freedom 
under random excitation 
   , ,Mx + Cx + Kx + Φ x,x x = Q t   
(2.20) 
where x , x , x are displacement, velocity and acceleration 
vectors, respectively , ,M C Kij ij ijn n n n n nm c k  
             are 
mass, damping and stiffness matrices;  ,Φ x,x x  - nonlinear function 
vector,  Q t is Gaussian white noise excitation vector with zero 
intensity and spectral density matrix    S ij n nS     where  ijS  is 
cross spectral density function of 
iQ and jQ . The equivalent 
linearization system is as follows: 
         ,t  
e e eM + M q C + C q K + K q Q 
(2.21) 
where e e eM , C , K are the equivalent matrices of mass, damping 
and stiffness. In equation (2.21) we use the notation  q t to show 
that this is only an approximation to  x t in the original nonlinear 
equation (2.20). The error between the system (2.20) and the system 
(2.21) is 
   .  e e ee Φ q, q, q M q + C q + K q    
(2.22) 
7 
The error e satisfies the Mean Square Error Criterion upon 
e e eM , C , K : 
min .E     e e e
T
M ,C ,K
e e
(2.24) 
Where the expectation in the left side of (2.24) is calculated by the 
probability density function of (2.21). Atalik and Utku (1976) [59] 
show that the criterion (2.24) leads to the following equation: 
  ,
TT e e e Tzz M C K zΦ zE E           
(2.25) 
2.2. Some improved equivalent linearization criteria 
 For decades, many studies on equivalent linearization criteria have 
been proposed to improve the accuracy of the equivalent 
linearization method [11-24, 20-24, 67, 68]. 
2.3 Criterion of global-local mean square error 
 In this section, we propose a new equivalent linearization criterion 
called the global-local mean square error criterion. We consider a 
nonlinear random oscillation of one degree of freedom: 
2
02 ( , ) ( )x hx x g x x t    
   
(2.47) 
Where, the notation is defined as above. The equivalent 
linearization equation of (2.47) takes the form: 
2
02 ( )x hx x x x t       
   
(2.48) 
where λ, μ are linearization coefficients. The error between 
(2.47) và (2.48) is: 
     xxxxgxxe    ,, (2.49) 
The classical criterion gives [29, 44] 
2
,
( , ) ( , ) mine x x P x x dxdx
 
 
 
    
(2.51) 
Where ( , )P x x is the probability density function (PDF) of x and 
x : 
8 
2 2
( , ) ( , )
, .
g x x x g x x x
x x
  
  
(2.53) 
Since the integration domain in (2.51) is (  , ), the criterion 
(2.51) is called the global mean square error criterion. With the 
assumption that the integration should focus for a more accurate 
solution, Anh and Di Paola proposed the local mean square error 
criterion (LOMSEC) [15]: 
0 0
0 0
2
,
( , ) ( , ) min
x x
x x
e x x P x x dxdx
 
 
 
 
  
(2.54) 
Where, 00, xx  are positive values. The integration (2.54) is 
transformed into the non-dimension one by introducing 
0 0,x xx r x r    where r is a positive value, x and x  are 
standard deviations of x and x : 
2 2
,
[ ( , )] ( , ) ( , ) min
x x
x x
r r
r r
e x x e x x P x x dxdx
 
 
 
 
 
  
   
(2.55) 
where [.] denotes: 
[ . ] ( . ) ( , )
x x
x x
r r
r r
P x x d xd x
 
 
 
 
  
 
(2.56) 
We have analogously: 
   
2 2
( , ) ( , )
( ) , ( ) .
g x x x g x x x
r r
x x
  
      
  
 
(2.57) 
It is seen from (2.57) the local equivalent linearization 
coefficients (LOMSEC) are functions of r, ( ), ( )r r     .Using 
the dual viewpoint, we can propose that r change across the non-
negative domain and the EL coefficients ,  can be chosen as the 
following[24]: 
9 
0
0
1
( ) ( ) ,
1
( ) ( ) .
s
s
s
s
r Lim r dr
s
r Lim r dr
s
  
  
 
   
 
 
   
 
(2.60) 
We have found from LOMSEC a new EL criterion called the 
global-local mean square error criterion (GLOMSEC). 
Next we develop the global-local mean square error criterion 
(GLOMSEC) to MDOF systems: 
    tfzgz  (2.61) 
 1 2, ,...,
T
nz z z z are vector of state variables, n is a natural 
number, g is a nonlinear function of z, f(t) is a Gausian stochastic 
process with zero mean. Denote: 
      tfzgzze   (2.62) 
Introduce new linearization terms into (2.62): 
      tfzgAzAzzze   (2.64) 
where  ijaA  is matrix n×n. Let y is a stationary solution of: 
   0 tfAyy (2.65) 
From (2.64) and (2.65) we have: 
    ygAyye  (2.66) 
Denote p(y) probability density function (PDF) of y of (2.65). 
According to the LOMSEC we have: 
         ,min
0
0
1
0
1
1
0
1
22
ij
ynn
ynn
y
y a
y
y
i
y
y
i dyypyenye  
 i,j = 1,,n 
It gives: 
     
1
 TT yyyygA (2.72) 
10 
The iterative algorithm is applied similarly to the one proposed by 
Atalik and Utku [59]. According to the GLOMSEC, the EL 
coefficients aij can be chosen as the following 
00
1
0 0 0
1 2
0 0 0
1 2
0 0 0 0 0 0
1 2 1 20 0 0, ,..... 1 2 0 0
( , , ..... )
1
.... ( , , ..... ) .....
.....
n
n
ij ij n
yy
ij n n
y y y n
a a y y y
Lim a y y y dy dy dy
y y y
 
 
 
 
 
 
Conclusion of chapter 2 
 The second chapter deals with the development of the criterion of 
Global – local mean squared error (GLOMSEC) for the systems of 
one and multi degrees of freedom. The results in chapter 2 are 
presented in the articles [1,6] of the List of publication of 
dissertation. 
CHAPTER 3. APPLICATION OF GLOMSEC IN ANALYSIS 
OF RANDOM ONE DEGREE OF FREEDOM SYSTEMS 
3.1. Analysis of domain of concentred response of nonlinear 
systems 
3.1.1. Duffing oscillation system subjected to white noise excitation 
3.1.2 Nonlinear damped oscillation system subjected to white noise 
excitation 
We consider a nonlinear damped oscillation system subjected to 
white noise excitation: 
    
2 21x x x x x d t         
(3.6) 
The exact PDF two-dimensional probability density function of the 
system [29, 44]: 
     
22 2 2 2, exp 0.5p x x C x x x x
d
         
  
(3.7) 
11 
where C is the normalized constant. If  Prob a x a   is 
chosen then the domain  aa, will be detemined by: 
    Prob ,aaa x a p x x dx dx
 
       
(3.8) 
Suppose we choose  Prob 0.98a x a    and consider the 
parameter d = 2 while the nonlinear parameter  changes. Then the 
values a will be obtained (Table 3.2). From Table 3.2 we also find 
that the finite domain [-a, a] in which the responses are concentrated 
with probability 0.98. Observations show that the response domain 
shrinks as the nonlinear parameter  increases as shown in Table 
3.2. and Figure 3.2 as follows: 
Tab. 3.2. Values of a depending on  
 0.1 0.5 1 5 10 30 50 80 100 
a 2.92 2.04 1.78 1.36 1.26 1.15 1.11 1.08 1.07 
-4
-2
0
2
4
x -4
-2
0
2
4
x 
0
0.02
0.04
p
-1
0
1
x -1
0
1
x 
0
0.1
0.2
0.3
0.4
p
 a.  =0.1 b.  =100 
Fig.3.2. Graphics of PDF
of nonlinear damped system ( =0.1; 100) 
12 
3.2. Application examples of global-local mean square error 
criterion (GLOMSEC) 
3.2.1 Vibration with 3-order nonlinear damping 
Consider a nonlinear damped oscillation system subjected to 
white noise excitation: 
   3 22 ox h x x x t         (3.11) 
where , , ,oh    are positive values. The corresponding 
linearization system is as follows: 
   22 ox h b x x t       (3.12) 
where b is the linear coefficient. The mean square response of (3.12) 
is: 
 
2
2
22 2 o
x
h b
 (3.13) 
The coefficient b defined by the classical criterion is: 
26b h x  
(3.15) 
By GLOMSEC is: 
2,2 2
1,0
1
( ) 2 2.4119* 2
s
r
s
r
T
b b r h x Lim dr h x
s T
 
 
        
 
  (3.22) 
Substituting (3.22) into (3.13) gives: 
2 2
2
2
2.4119
2*2.4119GL o
h h h
x
h
  
(3.23) 
To evaluate approximate solutions we use the solution 
2
ENL
x [29]. The relative errors of 2
GL
x , 
2
kd
x compared to the 
solution 2
ENL
x are defined by (3.24): 
13 
2 2 2 2
( ) ( )2 2
*100%, *100%kd cx GL cxC GL
cx cx
x x x x
Err Err
x x
 
 
 (3.24)
In Table 3.4, the results show that the solution 2
GL
x has better 
accuracy than the solution 2
kd
x , in particular the largest error of 
GLOMSEC is only 1.93%. 
Table 3.4. The second moment of the response of the nonlinear 
damping oscillator system 0.05, 1, 4oh h    , and γ changes 
γ 
2
ENL
x 2
kd
x 
( )
%
CErr
2
GL
x 
( )
%
GLErr
1 0.4603 0.4342 5.61 0.4692 1.93 
3 0.3058 0.2824 7.65 0.3090 1.05 
5 0.2479 0.2270 8.32 0.2495 0.77 
8 0.2025 0.1844 8.99 0.2032 0.35 
10 0.1835 0.1667 9.16 0.1839 0.22 
3.2.2. Van der Pol system to white noise 
Consider Van der Pol system 
    
2 2
ox x x x t       
 
(3.25) 
where , , , ,o     are positive values,  t is white noise with 
unit intensity. We replace   2,g x x x x  by the linear one bx , 
where b is the linear coefficient: 
   2ox b x x t         (3.26) 
14 
The coefficient b defined by the classical criterion is: 
 2b x   (3.29)
 By GLOMSEC is:
1,2 2
0,0
1
( ) 0.8371
s
r
s
r
T
b b r x Lim dr x
s T
 
 
        
 
(3.34) 
Mean square response 2
GL
x of Van der Pol system (3.25) by 
GLOMSEC is: 
2
2 2 2
2
1 1,6742
1,6742GL o
x
  
 
  
    
   
(3.36) 
To evaluate approximate solutions, we use the Monte Carlo 
simulation solution, [29]. The relative error between the approximate 
solutions 2
GL
x , 
2
kd
x , compared to the simulation solutions 
2
MC
x is calculated by the formula (3.24). 
Table 3.5. Mean square responses of Van der Pol oscillator with 
α*ε=0.2; 
0 =1;  =2; σ
2 changes 
2 
2
MC
x 2
kd
x 
( )
%
CErr
2
GL
x 
( )
%
GLErr
0.02 0.2081 0.1366 34.33 0.1574 24.32 
0.20 0.3608 0.2791 22.46 0.3113 13.52 
1.00 0.7325 0.5525 24.58 0.6095 16.79 
2.00 1.0310 0.7589 26.40 0.8349 19.02 
4.00 1.4540 1.0513 27.70 1.1544 20.61 
15 
In Table 3.5, the results 2
GL
x have better accuracy than 2
kd
x , in 
which the largest error values respectively are 24.32% compared to 
34.33% 
3.2.3 Vibration in Duffing system to random excitation 
Consider Duffing system subjected to white noise excitation: 
 2 32 ox hx x x t        (3.37) 
The notation is the same as in the previous example. The exact 
solution is [29, 44] 
2 2 2 4
2
2
x
2 2 4
2
4 1 1
exp
2 4
4 1 1
exp
2 4
o
c
o
h
x x x dx
x
h
x x dx
 
 
  
   
  
  
   
  
(3.39) 
The equivalent liner system is: 
 22 ox hx x kx t      (3.40) 
The linearization coefficient by GLOMSEC is: 
2, 2
1,0 0
2,2 2
1,0
1 1
( ) ( )
1
2.4119
s s
r
s s
r
s
r
s
r
T
k k r Lim k r dr Lim x dr
s s T
T
x Lim dr x
s T
 
 
  
         
   
 
       
 
 
(3.48) 
Mean square response 2
GL
x of Duffing system (3.37) by 
GLOMSEC: 
2
2 2 41 2.4119
2* 2.4119
o oGL
x
h
 
 
    
 
 
(3.49) 
16 
The relative error between the approximate solutions 2
GL
x , 
2
kd
x with the exact one 2
xc
x defined by (3.24) and presented in 
Tab. 3.6. 
Table 3.6 Mean square responses of Duffing system, 
1, 0.25, 1o h    ;  changes 
 2
xc
x 2
kd
x 
( )
%
CErr
2
GL
x 
( )
%
GLErr
0.1 0.8176 0.8054 1.49 0.8327 1.857 
1.0 0.4680 0.4343 7.194 0.4692 0.263 
10 0.1889 0.1667 11.768 0.1839 2.626 
100 0.0650 0.0561 13.704 0.0624 4.076 
 The results show that the approximation determined by the 
classical criterion has good accuracy with small nonlinear elastic 
coefficient , the error increases to over 13% as the nonlinear elastic 
coefficient increases. Accuracy of GLOMSEC criterion is better with 
maximum error of 4.1%. 
3.2.4. Duffing system with nonlinear damping to white noise 
3.2.5. Vibration of ship 
 The rolling motion of the ship in random waves has been 
considered by [55], [56], [57]. The equation of the ship's motion is of 
the form [56-57] 
2 2 ( )D t          
(3.63) 
The system (3.63) is replaced by the linear one 
 2 ( )
ec D t        (3.66) 
17 
The linearization coefficient ec by GLOMSEC is: 
3 ,2 1/ 2 2 1/2
1,0 0
1 1
( ) ( ) { } 1.49705 { }
s s
t re e e
s s
r
T
c c r Lim c r dr E Lim dr E
s s T
   
 
  
       
   
  
Mean square response by GLOMSEC is: 
    
2/3
2 2
2 1/2
0.76415
1.49705 { }eGL GL
D D D
E E
c E
 
  
 
     
 
 
Mean square response by the classical criterion is: 
    
2/3
2 2
2 1/2
0.7323
1.5958 { }eC C
D D D
E E
c E
 
  
 
     
 
 
Mean square response by the nonlinear equivalent linearization 
method is: 
    
2/3
2 2 0.765
ENL ENL
D
E E 
 
   
 
 
The relative error between the approximate solutions 2
GL
x , 
2
C
x , compared to the nonlinear equivalent linearization method, is 
calculated by the formula (3.24). We have: 
( ) ( )4.314%; 0.130%C GLErr Err  
The results show that GLOMSEC gives the good agreement with 
the ENL solution and GLOMSEC improves the accuracy of the 
classical criterion. 
Conclusion of chapter 3 
 In Chapter 3, the GLOMSEC was applied to analyze the mean 
square responses for a number of 1-order-freedom random 
oscillating systems. The examples applied confirmed the outstanding 
advantages proposed in the GLOMSEC. The results are presented in 
[1,3,5] of List of publications of the dissertation. 
18 
CHAPTER 4. APPLICATION OF GLOMSEC TO THE 
ANALYSIS OF RANDOM MDOF SYSTEMS 
4.1. Two-degree-freedom nonlinear oscillation system 
Consider the two-degree-freedom nonlinear oscillation system 
described by: 
 
 
332
1 1 1 21 1 1 1 11
2 33
2 1 2 2 2 22 2 2 2 1
0 ( )1 0
0 ( )0 1
x b x xx x x w ta
x x x w ta x b x x
 
   
              
                                  
 
  
 (4.1) 
where: , , , ,i i ia b   (i=1, 2) are constants. 1 2( ), ( )w t w t are white 
noise processes with zero mean and  ( ) ( ) 2 ( )i i iE w t w t S     (i=1, 
2), ( )  is Delta Dirac function, 
1 2,S S = const. The equivalent linear 
system is: 
2
1 1 1 11 11 12 1 11 12
2
2 2 2 221 1 2 22 21 2 22
( )1 0
( )0 1
e e e e
e e e e
x x x w tc c k a k
x x x w tc c a k k
 
  
              
             
                
 
 
 (4.4) 
where , ; ( , 1,2)e eij ijc k i j  
 are equivalent linear coefficients. The 
equation error is: 
 ( , )
e eC X K Xx x     (4.5) 
 
 
33
1 1 1 21
33
2 2 2 2 1
( , )
x b x x
x x
x b x x
   
          
111 12 11 12
221 22 21 22
; ; ;e eC X K
e e e e
e e e e
xc c k k
xc c k k
    
      
    
1
2
;X
x
x
 
  
  
(4.6) 
To simplify the calculation we suppose that 1 2,x x 
are 
independent. Using the Appendix of dissertation and noting 
2 1 2 1 0 ( )n mi jE x x i j
     
 GLOMSEC gives: 
19 
  2,211 11 1 1
1,0
1
( )
s
re e
s
r
T
c c r E x Lim dr
s T
 
    
 
 , 
  2,222 22 2 2
1,0
1
( )
s
re e
s
r
T
c c r E x Lim dr
s T
 
    
 
 
   2, 1,2 211 11 1 2
1, 0,0 0
1 1
( ) 3 .
s s
r re e
s s
r r
T T
k k r b E x Lim dr E x Lim dr
s T s T 
    
          
    
 
   2, 1,2 212 12 2 1
1, 0,0 0
1 1
( ) 3 .
s s
r re e
s s
r r
T T
k k r b E x Lim dr E x Lim dr
s T s T 
    
           
    
 
   2, 1,2 221 21 1 2
1, 0,0 0
1 1
( ) 3 .
s s
r re e
s s
r r
T T
k k r b E x Lim dr E x Lim dr
s T s T 
    
           
    
 
   2, 1,2 222 22 2 1
1, 0,0 0
1 1
( ) 3 .
s s
r re e
s s
r r
T T
k k r b E x Lim dr E x Lim dr
s T s T 
    
          
    
 
 (4.11) 
The limits in (4.11) equal to: 
2,
1,0
1
lim 2.41189
s
r
s
r
T
dr
s T
 
  
 
,
 1,
00
1
lim 0.83706
s
r
s
r
T
dr
s T
 
 
 
 (4.12) 
 To evaluate the approximate solution while the original nonlinear 
system does not have an exact solution, we use the approximate 
probability density function by the equivalent nonlinear method 
(ENL) [77]. Table 4.1 presents the approximate mean square 
responses and their relative errors compared to ENL solutions. 
20 
Table 4.1. The mean square responses of 1 2,x x follow 1 2  với 
1 2 1 2 0 1a b S          . 
1
2
,
 21 ENLE x
 21 CE x
( )
%
CErr
 21 GLE x
( )
%
GLErr  
2
2 ENL
E x
 22 CE x
( )
%
CErr
 22 GLE x
( )
%
GLErr
0.1 1.573 1.216 22.68 1.407 10.54 1.573 1.151 26.83 1.327 15.64 
1 0.496 0.422 15.07 0.488 1.59 0.496 0.370 25.51 0.419 15.50 
5 0.253 0.220 13.19 0.254 0.268 0.253 0.205 19.19 0.234 7.573 
10 0.194 0.171 12.07 0.197 1.533 0.194 0.162 16.48 0.186 4.178 
It is seen that GLOMSEC gives good improvements for the 
accuracy of approximate solutions when the nonlinearity increases. 
4.2. Nonlinear oscillation systems subjected to color noise 
 The introduction of the 1-DOF system subjected to color noise 
excitation in Chapter 4 is because the color noise random process is 
described as a white noise process passing through a second-order 
differential filter. The oscillation equation is solved with the filter 
equation so it can be considered as a system of multi-degrees-of- 
freedom. 
4.2.1. Extend GLOMSEC to the case of random color noise 
excitation 
4.2.2. Duffing system to color noise excitation 
Consider Duffing system to random color noise excitation: 
2 3( )z z z z f      (4.41) 
where f is the color noise random process 
2 2
f ff f f w    
  . (4.22) 
The nonlinear system is replaced by the linear one 
 x cx kx f    (4.27) 
21 
The linear coefficients by GLOMSEC are: 
2 2 22.41189 , .xk c     (4.45) 
By the classical criterion: 
2 2 23 ,xk c     
(4.46) 
By the Energy criterion: 
2 2 22.5 ,xk c    
(4.50) 
The relative errors between approximate solutions 2,x GL , 
2
,x C 
compared to 2,x E are presented in Table 4.3. The results show the 
solution 2,x GL is much better accurate then the solution 
2
,x C , namely 
with the bigest errors 2.392% compared to 11.398%, respectively. 
 Tab. 4.3. Mean square response with 2 2f, ,S, , 1     
 changes. 
 2
,x E 
2
,x C %CErr 
2
,x GL %GLErr 
0.1 
1 
10 
100 
1.86038 
0.66376 
0.16687 
0.03720 
1.75024 
0.60015 
0.14855 
0.03296 
5.920 
9.583 
10.979 
11.398 
1.88195 
0.67688 
0.17072 
0.03809 
1.159 
1.977 
2.307 
2.392 
4.2.3. Duffing system with nonlinear damping to color noise 
excitation 
Consider Duffing syste
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