Global residue harmonic balance method for Helmholtz-Duffing oscillator
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Transcript of Global residue harmonic balance method for Helmholtz-Duffing oscillator
Accepted Manuscript
Global residue harmonic balance method for Helmholtz-Duffing oscillator
Peijun Ju
PII: S0307-904X(14)00513-7DOI: http://dx.doi.org/10.1016/j.apm.2014.10.029Reference: APM 10182
To appear in: Appl. Math. Modelling
Received Date: 26 January 2013Revised Date: 2 April 2014Accepted Date: 13 October 2014
Please cite this article as: P. Ju, Global residue harmonic balance method for Helmholtz-Duffing oscillator, Appl.Math. Modelling (2014), doi: http://dx.doi.org/10.1016/j.apm.2014.10.029
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Global residue harmonic balance method for Helmholtz-Duffing
oscillator
Peijun Ju *
School of Control Science and Engineering, Shandong University, Jinan 250061, China
Abstract
In this paper, an improved harmonic balance method was proposed to solve the
Duffing-harmonic equation. This method is called the global residue harmonic
balance method (GRHBM). Unlike other harmonic balance methods, all the former
global residual errors are introduced in the present approximation to improve the
accuracy. A maximum absolute value of the relative errors for the second-order
approximation is less than 0.1165%. Comparison of the result obtained using this
approach with the exact one and existing results reveals that the high accurate,
simplicity and efficiency of the proposed procedure. The method can be easily
extended to other strongly nonlinear oscillators.
Key words: Global residue harmonic balance method, Duffing-harmonic equation,
Approximate solutions, Nonlinear oscillators
* Tel: +08613325277995 E-mail address: [email protected]
1. Introduction
The study of nonlinear equations has drawn much attention in recent years.
Various powerful mathematical techniques were used to obtain approximate analytical
solutions, such as harmonic balance method [1-7], energy balance method [8-11],
Hamiltonian approach [12-13], the homotopy perturbation method [15-19] and other
new methods[20-24].
As a class of dynamical systems with strong nonlinearities and larger oscillation
amplitudes, Duffing-harmonic oscillator system has been recently the focus of a great
deal of research. Many techniques have been developed to determine analytical
approximations to the periodic solution of Duffing-harmonic oscillator system.
Mickens [1] and Hu and Tang [2] used the harmonic balance method to investigate the
analytical approximation. Radhakrishnan et al. solve Duffing-harmonic oscillator
system by numerical integration of its energy relation [3]. Lim et al. presented a
Newton’s harmonic balance method to solve the Duffing-harmonic oscillator system,
and their approximations give accurate results for a large range of the initial
amplitudes [4,5]. By using He’s energy balance method, Õzis and Yildirim obtained
an accurate result [8]. Beléndez et al. obtain small relative error between the
approximate frequency and the exact one, by introducing a cubication method and the
modified homotopy perturbation method [16-18]. D.D. Ganji et al. obtained the
approximate frequency by He’s energy balance method (HEBM) [10], while S.S.
Ganji et al. by max-min approach (MMA) [21]. Guo et al. presented an Iterative
homotopy harmonic balancing approach to solve the system, and their second-order
approximation give accurate results [6].
In this paper, based on the ideas of homotopy perturbation and the residue
harmonic balance method [7], we put forward a novel approximate method, namely
the global residue harmonic balance method, to determine the periodic solutions of
Duffing-harmonic oscillator systems. To obtain higher-order analytical
approximations, all the former residual errors are considered in the solving process of
present order approximation.
2....Basic ideas of the global iterative harmonic balance approach
For the sake of simplicity, we have been considered systems governed by
equations having the form
( )u f u=&& , (0)u A= , (0) 0u =& , (1)
where du
udt
=& and f is a nonlinear function. For convenience, we assume
( ) ( )f u f u− = − .
With a new independent variable tτ ω= , where ω is the frequency of system,
Eq. (1) becomes
2 ( )u f uω ′′ = , (0)u A= , (0) 0u′ = , (2)
where du
udτ
′ = .
Considering the periodic solution does exist, it may be better to approximate the
solution by finite sums of trigonometric functions, i.e.
1
( ) cos( ),M
k
k
u A kτ τ=
=∑ (3)
where 2
0
1( )cos( )kA f t kt dt
π
π= ∫ .
First, we consider only one-term expansion into Eq. (3), and take the initial
approximation of ( )u τ and ω satisfying initial conditions in Eq. (2) as
0 ( ) cos( ),u Aτ τ= 2 20ω ω= , (4)
Substituting Eq. (4) into Eq. (2) and equating the coefficient of cos( )τ to zero, we
can determine the parameter 0ω . Then, the zero-order approximation is in the form of
Eq. (4), where 0tτ ω= .
Using Eq. (3) and the harmonic balance method, in order to obtain the k th-order
( 1,2, ,k = L ) approximation, we may assume
1
( )0
( ) ( ) ( )k
i k
i
u u puτ τ τ−
=
= +∑ ,1
2 20 ( )
1
,k
i k
i
pω ω ω ω−
=
= + +∑ (5)
where p is the order parameter, and
(0) 0( ) ( )u uτ τ= , 1
( ) ( )0
( ) ( ) ( )i
i j i
j
u u uτ τ τ−
=
= +∑ , 1,..., 1i k= − ,
3, 5, 2 1,( ) (cos( ) cos(3 )) (cos( ) cos(5 )) (cos( ) cos((2 1) ))i i i i iu a a a iτ τ τ τ τ τ τ+= − + − + + − +L ,
1,...,i k= , (6)
(0) 0ω ω= , 1
2 2( ) 0 ( )
1
i
i j i
j
ω ω ω ω−
=
= + +∑ , 1,..., 1i k= − , (7)
where 3,ia , 5,ia , … , 2 1,i ia + and i
ω ( 1,...,i k= ) are unknown parameters to be
determined. We first substitute Eq. (5) into Eq. (3) to obtain the coefficient of p as a
function 3 5 2 1,( , , , , , )k k k k k k
F a a aτ ω+
L . Then, calculating the residual errors of
( 1)k − th-order approximation, i.e.
21 ( 1) ( 1) ( 1)( ) ( ).k k k kR u f uτ ω− − − −
′′= − (8)
If 1( ) 0k
R τ−
= then ( 1) ( )ku τ− happens to be the exact solution. Generally such
case will not arise for nonlinear problems. At this moment, we will use this residual
error to obtain a more accurate higher-order approximation. Our option is taking a
new equation:
3 5 2 1, 1( , , , , , ) ( ) 0.k k k k k k kF a a a Rτ ω τ+ −+ =L (9)
Equating the coefficients of cos( )τ , cos(3 )τ , … , cos((2 1) )k τ+ to zero in Eq.
(9), we can easily obtain the unknown parameters 3,ka , 5,ka , … , 2 1,k ka + and k
ω for
the number of equations equal to the number of the parameters.
Then, the k th-order approximate periodic solution and frequency can be
obtained in the form
( ) (0) (1) ( 1)( ) ( ) ( ) ( ) ( )k k ku u u u uτ τ τ τ τ−= + + + +L , 2 2( ) 0 (1) ( 1)k k kω ω ω ω ω−= + + +L . (10)
3. Duffing-harmonic oscillator
Conservative nonlinear oscillatory systems can often be modeled by potentials
having a rational form for the potential energy, which lead to the equation of motion
3
20.
1
uu
u+ =
+&& (11)
For small u , the equation is that of a Duffing-type nonlinear oscillator, while for
large u ,the equation approximates that of a linear harmonic oscillator, hence Eq. (11)
is called the Duffing-harmonic oscillator. The above system has no possible small
parameters. Therefore, the classical perturbation methods do not apply to such a
problem.
If ω is the frequency of Duffing-harmonic oscillator, Eq. (11) can be rewritten
as
2 2 3( ) 0.u u u uω ′′ ′′+ + = (12)
where
,tτ ω= du
udτ
′ = , (13)
with the initial conditions
(0) ,u A= (0) 0u′ = . (14)
3.1 Zero-order approximation
First, we consider
0 ( ) cos( ),u Aτ τ= 2 20ω ω= , (15)
Substituting Eq. (15) into Eq. (12), yields
2 2 3 3 2 3 30 0 0
3 3 1 1cos( ) cos(3 ) 0
4 4 4 4A A A A Aω ω τ ω τ
− − + + − + =
. (16)
Equating the coefficient of cos( )τ to zero, we obtain
220 2
3
4 3
A
Aω =
+. (17)
At this time, we know the zero-order approximate periodic solution in the form
Eq. (15).
3.2 First-order approximation
To obtain the rest of the nonlinear correction, we consider
0 1( ) ( ) ( )u u puτ τ τ= + , 2 20 1,pω ω ω= + (18)
where p is a bookkeeping parameter. We assume
1 31( ) (cos( ) cos(3 ))u aτ τ τ= − , (19)
where 31a and the former parameter 1ω are two unknown constants that will be
determined later.
Substituting Eq. (18) into Eq. (12) and taking the coefficients of the p , we obtain
a function 1 31 1( , , )F aτ ω .
( )
( ) ( )( )
2 4 4 2 21 31 1 31 31 12
22 2 2 2 2
31 31 1 312
1( , , ) 12 24 (9 16 24 ) cos( )
16 12
48 96 (4 3 ) cos(3 ) 24 12 cos(5 )16 12
F a A a A a A A A tA
AA a a A A t A A a t
A
τ ω ω
ω
= + − − −+
+ + − − + −+
(20)
Now, substituting Eq. (15) and Eq. (17) into Eq. (12) it results the following
residual
2 3 30 0
1 1( ) cos(3 ).
4 4R A Aτ ω τ
= − +
(21)
Following Eq. (9), we have
1 31 1 0( , , ) ( ) 0.F a Rτ ω τ+ = (22)
Equating the coefficients of cos( )τ and cos(3 )τ to zero in Eq. (22), we obtain
2 2
1 2 4 2
4 (1 2 ),
(39 10 32)(4 3 )
A A
A A Aω
+= −
+ + +
2
31 2 4
1 (4 3 ),
3 39 10 32
A Aa
A A
+= −
+ + (23)
and the first-order approximate periodic solution in the form
(1) 0 1 31 31( ) ( ) ( ) ( ) cos( ) cos(3 ),u u u A a aτ τ τ τ τ= + = + − (24)
2 2(1) 0 1,ω ω ω= + (25)
where (1)tτ ω= .
3.3 Second-order approximation
Based on the first-order approximations, the periodic solution and the frequency
of Eq. (12) can be further expressed as
0 1 2( ) ( ) ( ) ( )u u u puτ τ τ τ= + + , 2 20 1 2.pω ω ω ω= + + (26)
and
2 32 52( ) (cos cos3 ) (cos cos5 ),u a aτ τ τ τ τ= − + − (27)
where 32a , 52a and the former parameter 2ω are unknown constants that will be
determined later.
Substituting Eq. (26) into Eq. (12) and taking the coefficients of the p , we obtain
the function 2 32 52 2( , , , )F a aτ ω . Substituting Eq. (24) and Eq. (25) into Eq. (12) it
results the residual error function 1( )R τ . Taking the two functions into following
equation
2 32 52 2 1( , , , ) ( ) 0.F a a Rτ ω τ+ = (28)
Equating the coefficients of cos( )τ , cos(3 )τ and cos(5 )τ to zero in Eq. (28),
we obtain
21
2 2 4
4,
(39 10 32)
A X
A Aω = −
+ + ∆
232 2 4
4,
9(39 10 32)
AXa
A A= −
+ + ∆
352
2,
3
AXa =
∆ (29)
where the values ( 1,2,3)i
X i = and ∆ are presented in Appendix.
The second-order approximate periodic solution is
(2) 0 1 2 31 32 52 31 32 52( ) ( ) ( ) ( ) ( )cos( ) ( )cos(3 ) cos(5 ),u u u u A a a a a a aτ τ τ τ τ τ τ= + + = + + + − + −
2 2(2) 0 1 2 ,ω ω ω ω= + + (30)
where (2)tτ ω= .
It should be clear how the procedure works for constructing further higher-order
approximations.
4 Result and discussion
In order to illustrate the applicability, accuracy and effectiveness of the proposed
approach, we compare the analytical approximate frequency and periodic solution
with the exact ones.
The exact frequency can be obtained from the following complicated relation
that is given in [5].
12
2 202 2
2
cos( )
2 coscos ln[1 ]
1
e
A tdt
A tA t
A
ππ
ω −=
+ −+
∫ (31)
We denote 100( )i i e e
E ω ω ω= − as the relative error of the i th-order
approximation for Duffing-harmonic oscillator.
Table 1 shows the comparison between the present and existing solutions,
namely the second-order approximations obtained with GRHBM, the first-order
approximation to the frequency of oscillation obtained by Guo et al., by means of an
iterative homotopy harmonic balance method (IHHBM) [6] , frequency obtained by
He’s energy balance method (HEBM) [10] and max-min approach (MMA) [21].
Table 1 Comparison of approximations and exact frequencies for Duffing-harmonic oscillator.
The results presented in Table 1 clearly show that the methods GRHBM and
IHHBM achieved more excellent agreement than HEBM and MMA. The GRHBM
result is more (respectively, slightly less) accurate than that of IHHBM for 1A ≤
(respectively, 5A ≥ ) . For example, when 0.5A = the relative error of the
second-order frequency is -0.0012%, the former result obtained by Guo et al., is
-0.4967% [6].
A e
ω GRHBM IHHBM HEBM MMA
0.01
0.05
0.1
0.5
1.0
5.0
10
50
100
0.00847
0.04232
0.08439
0.38737
0.63678
0.96698
0.99092
0.99961
0.99990
0.008472(0.0283%)
0.042322(0.0043%)
0.084394(0.0049%)
0.38737(-0.0012%)
0.636795(0.0023%)
0.968107(0.1165%)
0.991591(0.0677%)
0.999657(0.0047%)
0.999914(0.0014%)
0.008478(0.0945%)
0.042344(0.0567%)
0.084418(0.0332%)
0.38545(-0.4967%)
0.63136(-0.851%)
0.96667(-0.0319%)
0.99090(-0.0024%)
0.99961(-0.0002%)
0.999901(0.0001%)
0.00866(2.2432%)
0.04326(2.2212%)
0.08627(2.2278%)
0.39638(2.3259%)
0.65164(2.3336%)
0.97343(0.6670%)
0.99314(0. 2240%)
0.99973(0.0120%)
0.99999(0.0090%)
0.00866(2.2432%)
0.04326(2.2212%)
0.08627(2.2278%)
0.39736(2.5789%)
0.65465(2.8063%)
0.97435(0.6691%)
0.99340(0.2503%)
0.99973(0.0120%)
0.99993(0.0030%)
It is worth noting that, for the maximal absolute value of the relative errors, the
approximate frequency obtained in this paper, combining IHHBM, is slightly more
accurate (0.2895%( 1E ) and 0.1165% ( 2E ) versus 0.851%[6]) than the first-order
approximate frequency obtained by Guo et al. [6].
The periodic solution achieved by numerical integration of Eq. (12) using
Runge-Kutta scheme and the second-order approximate periodic solution given by Eq.
(30) are plotted in Figs1-4. These figures represent, respectively, four different
amplitudes 0.01A = , 0.5, 5 and 50. They show that the approximate periodic solution
provides excellent approximation comparing to the exact periodic solution for small
as well as for large amplitude of oscillation.
5. Conclusion
A global residue harmonic balance method (GRHBM) has been used to obtain
three approximate frequencies and periodic solutions for the Duffing-harmonic
oscillator. We obtain an excellent agreement for all the residual error is used to
proceeding with harmonic balancing. The results will be helpful in study other
strongly nonlinear oscillators. Recently, some new methods were proposed by Y.
Khan et al. in [22-24] which are easy to use and friendly methods. A future work is to
compare GRHBM with these new methods.
Fig. 1 Comparison between analytical approximate solutions and exact solution for 0.01A =
Fig. 2 Comparison between analytical approximate solutions and exact solution for 0.5A =
Fig. 3 Comparison between analytical approximate solutions and exact solution for 5A =
Fig 4 Comparison between analytical approximate solutions and exact solution for 50A =
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Appendix
The values ( 1, 2,3)i
X i = and ∆ in Eq. (29) are presented as below
1X =(1749600000000 6A +51379920000000 4A +698057352000000 2A +5827905547200000) 28A
+(33501446346240000 4A +140840415446832000 2A +449008725898404000) 22A
+(1110938790236693040 4A +2164791346739164872 2A +3349676218711307796) 16A
+(4124299437382437900 4A +4020561823848634167 2A +3059478252685316576) 10A
+(1768736508843204096 4A +741310535886624768 2A +207616456123678720) 4A
+33188673240170496 2A +2028721749884928,
2X =(5904900000000 6A +189022410000000 4A +2820893202000000 2A +26080808976000000)
30A +(167438166962940000 4A +792861943102488000 2A +2870799782408657100) 24A
+(8130057620217126030 4A +18262949906675678562 2A +32796531300124106163) 18A
+(47207173907726830701 4A +54339065166680506062 2A +49637428874998281144) 12A
+(35472746687173366800 4A +19372704358011629184 2A +7786374240783392768) 6A
+2162332794660438016 4A +368560237035651072 2A +28812435901120512,
3X =(218700000000 6A +6215454000000 4A +81545648400000 2A +654185388420000) 26A
+(3581997701040000 6A +14144492109310200 4A +41465266496357400 2A +91407280917881286
) 18A +(151432124231541141 4A +185469101630190189 2A +160640096015382210) 12A
+(86882476987596360 4A +14380666515959808 2A -18021998043072512) 6A
-15882568932057088 4A -5645816199905280 2A -803408235724800,
∆ =(6123600000000 6A +211205880000000 4A +3404341548000000 2A +34028121546000000) 28A
+(236059546632120000 6A +1205418822799968000 4A +4689648931579491600 2A
+14193355896848141280) 20A +(33822874705790864268 6A +63813346845672803868 4A
+95309456481644416311 2A +112041973038923497908) 12A +(102396952803640001008 4A
+71229035343489706624 2A +36422203401630900224) 6A +12901760886549168128 4A
+2827110614223028224 2A +288586791747846144.