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  • 8/10/2019 Weakly Non-Linear Time Delay Systems With Modified Parameters

    1/7

    International Journal of Scientific Research and Engineering Studies (IJSRES)

    Volume 1 Issue 4, October 2014

    ISSN: 2349-8862

    www.ijsres.com Page 1

    Weakly Non-Linear Time Delay Systems With Modified Parameters

    Abstract: Delay in a gi ven system makes the dimension

    of the phase space high. I n th is paper, it i s shown that the

    modif icati on of parameters method can be appli ed to weakly

    non- li near systems with delay. For systems with order one

    delay, the method leads to reduced systems without delay.

    For systems with l arger delay, the method is extended and

    the appli cation of the extended method l eads to reduced

    systems with delay. The extended method can also be applied

    to systems with order one delay; the resultant reduced

    equations are dif ferent f rom those obtained by the use of the

    conventional r enormalization method. A time delay term of a

    given system makes the dimension of the phase space hi gh.

    Even in such a case, this method can lead to reduced

    equations.

    Keywords: Parameters; Weakly non-Linear Systems;

    Pertu rbation; Renormalization.

    I. INTRODUCTION

    Many non-linear dynamical systems in various scientificdisciplines are influenced by the finite propagation time ofsignals in feedback loops. A typical physical system is

    provided by a laser system where the output light is reflectedand fed back to the cavity. Time delays also occur in othersituations; for example, in traffic flow model including adrivers reaction time, in Biology due to physiological controlmechanisms, or in economy where the finite velocity ofinformation processing has to be taken into account.Moreover, realistic models in population dynamics or inecology include the duration for the replacement of resources.

    In some situations, such as lasers and electromechanicalsystems, systems with large-delay appear. It is with this reasonthat there is need for a Mathematical tool to study them,especially for weakly non-linear systems.

    If a perturbation term were added to a given system, thesystem will not be guaranteed to be structurally stable. So the

    perturbation result is plagued with singularities. It has beenrecognised that these singularities in the result of the

    perturbation method can be renormalized away by themodification of parameters associated with the unperturbedsystem. The modified parameters are governed by therenormalization equations that turn out to be reducedequations. To obtain a more useful and sophisticated tool to

    study weakly non-linear systems, reformulated versions of theoriginal method have been used. There are a variety ofapplications of renormalization method to physical systems,

    such as plasma physics, general relativity and quantum optics,in addition to studies in standard non-linear dynamicalsystems.

    II. CONVENTIONAL RENORMALIZATION METHOD

    A.

    LINEAR SYSTEMS

    Consider the following system,2

    2

    2

    ( )( ) ( ) 0

    d x tx t x t

    dt (2.1)

    where is a parameter, represents the time

    delay, and is a small parameter where 1 . In this

    system there is an oscillatory solution that is can be expressedanalytically without any approximation. The exact solution isgiven by;

    2

    ( ) exp( ) .x t A it c c (2.2)under the condition that;

    2.

    (2.3)

    Here c.c represents the complex conjugate terms of the

    proceeding expression, A is the integration constant. Inthe perturbation analysis, the exact solution (2.2) is not used.As in the case of a differential equation without delay, the

    perturbation solution,(0) (1) 2 (2) 3( ) ( ) ( ) ( ) ( )x t x t x t x t is found.

    This perturbation solution is obtained by solving the

    equations;(0) ( ) 0;Lx t ( ) ( 1)( ) ( ),j jLx t x t

    ( 1,2,....)j , where2

    2

    2( ) ( )

    dLx t x t

    dt

    We obtain;

    (0) .i tx t Ae c c , (1) ( ) .2

    i tiAx t te c c

    ,

    (2) 2 ( 2 )2

    2 . .,8

    i tA ix t t t t e c c

    where A

    is the integration constant of the solutionof the unperturbed system,

    0 ( )x t . The solutions

    Okwoyo, M. JamesSchool of Mathematics, University of Nairobi, Nairobi,

    Kenya

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    International Journal of Scientific Research and Engineering Studies (IJSRES)

    Volume 1 Issue 4, October 2014

    ISSN: 2349-8862

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    ( ) ( ),jx t 1j contain the terms const.exp ( )i t and

    const.exp ( )i t . These terms are included in

    exp( )A i t and its complex conjugate term in (0) ( )x t .

    Apparently the validity of the perturbation is invalid in theregime

    1( )t

    due to the terms 2 2( , )t t etc

    Define the normalized variable as;

    2 2 2

    2 2

    2 8

    i iiA A iA A te t t t e

    (2.4)

    This definition is a form of near identity transformation atthe constant A and the perturbation solution is expressed interms of the normalized variable;

    3( ) ( ) exp( ) . ( )x t A t i t c c (2.5)

    The equation which ( )A t should satisfy perturbatively is

    then constructed and such an equation is the renormalizedequation. From equation (2.4), the following two relations can

    be obtained

    2 2 2 3

    2( ) 2 2 ( )

    2 8

    i iiA A iA t A e t e

    (2.6)

    and

    2( )( ) ( )2

    iiA tA A t te

    (2.7)

    where is a parameter. Substituting equation (2.7)into equation (2.6), we have the approximate closed relation;

    2 2 3

    2 3

    ( ) ( ) ( )( ) ( , )

    2 4 8

    i iA t A t iA t ie A t e

    The renormalization equation can then be obtained as the

    limit 0 ;

    2 2

    2 3

    ( ) ( )( )( )

    2 4 8

    i idA t iA t ie A t edt

    (2.8)

    The solution of equation (2.8) is given by;( )( ) (0) tA t A e , where

    2 2

    2 3( ) ( )2 4 8

    i ii i

    t t e e

    (2.9)

    To compare the solution of the renormalization methodwith the exact solution (2.2), it is restricted to the approximatesolution imposed on the condition (2.3). Using equation (2.3),equation (2.9) can be written as;

    2 3

    3( ) (0) exp( ( )

    2 8

    it it A t A

    (2.10)

    In terms ofx (t),we obtain the approximate solution usingequation (2.5) and (2.10) as;

    23 3

    3( ) (0)exp ( ( )) . ( )

    2 8x t A it c c

    (2.11)

    In fact, due to the

    relation 2

    2

    32 8

    3( ) , equation

    (2.11) same as equation (2.2) up to the second term,2( )

    B. NON-LINEAR SINGLE OSCILLATOR

    Consider the non-linear equation;

    31 3( )

    ( ) ( ) ( ) ( )dx t

    x t x t x t x tdt

    (2.12)

    where 1, , and 3 are parameters. The

    value of represents the time delay, and is thesmall parameter. The unperturbed system has analyticallyexpressible oscillatory solution when the following conditionis satisfied;

    1

    2 2

    cos ( )

    ;2 2 (2.13)

    The oscillatory solution of the unperturbed system is

    given by;(0) ( ) .i tx t Ae c c

    where, 2 2 ,A is the integration

    constant, and the relation exp( )i i issatisfied. The exact solution can be expressed analytically

    though it is difficult in the case where. 0 Therenormalization equation is constructed to investigate theeffect of the perturbation term. The perturbation solution

    (0) (1) 2( ) ( ) ( ) ( )x t x t x t is obtained by solving thefollowing equations;

    (0) ( ) 0L x t (1) (0) (0)3

    1 3( ) ( ) ( )L x t x t x t , where

    ( )( ) ( ) ( )

    dx tL x t x t x t

    dt

    The solutions are given by;

    (0) ( ) .i tx t Ae c c .,2

    1 3(1) 3

    ( ) .1 ( )

    i tA A A

    x t t e c ci

    .,

    By defining the renormalization variable ( )A t by;2

    1 33

    ( )1 ( )

    A A AA t A t

    i

    ,the renormalization

    equation is thus obtained as;2

    1 3( ) 3 ( ) ( )( )

    1 ( )

    A t A t A tdA t

    dt i

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    This system can be split into two parts; dynamicsdescribed by its amplitude and phase;

    22 2 1

    3

    3

    3 ( )3

    dRQR R

    dt

    (2.14)

    23 1

    2 2

    3

    3

    (1 ) ( ) 3

    dR

    dt

    (2.15)

    Here;( )( ) ( ) i tA t R t e and

    2 2

    2 (1 )

    (1 ) ( )Q

    . From

    Equations (2.14) and (2.15), R R ,1

    33

    R

    is a

    stable fixed point when 1

    3

    0

    and 3 0Q . Thus the limit-

    cycle oscillation appears when the conditions are satisfied.

    C. LANG-KOBAYASHI PHASE EQUATION

    Consider the equation;

    1''' '' ' cos ( ) ( ) 0S S (2.16)where 1, , are parameters, is the small

    parameter, and the prime denotes differentiation with respectto S. A reduced equation is derived from equation (2.16) andthe result is compared with that obtained using the multiple-scale method [12] First the perturbation solution

    (0) (1) 2( ) ( ) ( ) ( )S S S is obtained bysolving the following equations;

    (0) ( )L S (2.17)

    (1) (0) (0) (0)

    1( ) ( ) cos ( ) ( )L S S S S (2.18)

    where;3

    3( ) ( )

    d dL S S

    dS dS

    The solution to the unperturbed system (2.17)(0) ( )S is

    obtained as;

    (0) ( )( ) . ,2

    i S vAS e c c S B (2.19)

    where ,A v and B are integration constants.Substituting equation (2.19) into equation (2.18), thefollowing equation is obtained;

    (1)

    1( ) cos( ) ( ) cos( )oL S A S v j D

    ( )2( )

    2

    2,4,... 1,3,...

    cos( ) ( ) sin( ) ( ) .

    inS vin

    S vn n

    n n

    eJ D e J D c c

    i

    (2.20)

    Here D is defined by 2 sin( )2

    D A

    , nJ denotes the

    nthorder Bessel functions, and the following relation has been

    used in deriving equation (2.20);

    sin

    0

    1,3,... 2,4,...

    ( ) 2 ( )sin( ) 2 ( ) cos( )iz

    n n

    n n

    e J z i J z n J z n

    The solution of equation (18) is given by;

    (1)

    1 0( ) cos( ) ( ) cos( )

    2

    ASS S v j D S

    1 1( )sin( ) sin( )

    2S j D S v

    ( )2

    1 22,4,...

    cos( ) ( )(1 )

    inS ve

    n

    n

    ej Din n

    ( )2

    23,5,...

    sin( ) ( ) .(1 )

    inS v

    n

    n

    ej D c c

    n n

    (2.21)

    This perturbation solution includes the terms ( , , )S .

    Next these terms are removed using the renormalization

    method. Define the renormalization variables ( )C S and

    ( )B S as follows;

    21 1

    ( ) 2 ( ( )) sin( ) ,2

    iSC S A A i j D A e

    1 0( ) ( ( )) cos( )B S B S j D A

    The set of the renormalization equations up to ( ) is

    obtained as;

    21 1

    ( )( ) ( ( ( ) ))sin( ) ,

    2

    iC S

    C S i j D C S edS

    (2.22)

    1 0

    ( )( ( ( ) )) cos( ),

    B Sj D C S

    dS

    (2.23)

    Now, comparison of the renormalization equations (2.22)and (2.23) with the reduced ones obtained by the multi-scalemethod is necessary. Using the decomposition

    ( )( ) ( ) iv SC S A S e where, ( ( ) , ( ) )A S iv S , youobtain;

    1 1

    ( )( ) sin( ) ( ( ( )))sin( )

    2 2

    dA SA S j D A S

    dS

    (2.24)

    11

    ( )sin( ) ( ( ( ))) cos( )

    2( )

    dv Sj D A S

    dS A S

    (2.25)

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    When the reduced variable is introduced, the renormalizationequations (2.23), (2.24), and (2.25) become the reducedequations derived in [12].

    D. WEAKLY NON-LINEAR SYSTEM

    Here, the method leads to a discrete complex Ginzburg-Landauequation from a weakly non-linear lattice with delay.In this lattice system, the finite propagation time of motionfrom the nearest oscillators is taken into account. The stabilityof the trivial solution is predicted by studying the derivedreduced equation.The weakly non-linear oscillator is given by;

    ( )( )

    j

    j

    dx tp t

    dt (2.26)

    2 31 1( )

    ( ) ( ) ( ) 2 ( ) ( ) ,j

    j j j j j

    dp tx t x t x t x t x t

    dt

    (2.27)

    where , are parameters, is the small

    parameter, and represents the time delay. Thevariables ( )jx t and ( )jp t denote the displacement

    and momentum of a single oscillator located at lattice site

    j respectively. This system becomes Hamiltonian

    system where 0 .Firstly the perturbation solutions

    (0) (1) 2( ) ( ) ( ) ( )j j jx t x t x t are obtained as;

    2

    1 1( ) ( ) 2 3 . .2

    i ti t i

    j j j j j j j

    te

    x t A e e A A A A A c ci

    (2.28)

    Here jA are the integration constants, and the higher

    harmonic terms in (1) ( )

    jx t are omitted.

    Secondly from equation (2.28), the renormalized variables aredefined as;

    2

    1 1( ) ( ) 2 32

    i

    j j j j j j j

    tA t A e A A A A A

    i

    From the definitions, we have the relation

    ( ) . .,i tj jx t A e c c and the renormalization equations as;

    2

    1 1

    ( )( ( ) ( )) 2 ( ) 3 ( ) ( )

    2

    j i r

    j j j j j

    dA te A t A t A t A t A t

    dt i

    (2.29)

    The system (2.29) becomes the discrete Schrdinger

    equation and Hamiltonian system, in the case 0 .When 0 , equation (2.29) becomes the discrete Ginzburg-

    Landauequation.Using the renormalization equations, the behaviour of

    motion of the original system is predicted and confirmed

    numerically, on restriction to the conditions ( ) ( )j N jx t x t ,

    withNbeing the number of oscillators, this conditions lead to

    ( ) ( )j N jA t A t . There is the trivial solution ( ) 0jA t inequation (2.29). The uniform solution, expressed as

    ( ) ( )j

    A t A t (for any j), can be viewed as one of the local

    stable manifolds of the fixed point 0j

    A when a certain

    condition is satisfied and this has to be shown. To do this, we

    study the linear stability for 0jA . Substituting the equation

    ( ) ( )j jA t a t where ( ( ) 1)ja t into equation (2.29) we

    have the linearized equation of motion in Fourier space;

    ( ) 21 cos( ) ( ),k

    k

    db t i ke i b t

    dt N

    (2.30)

    where;

    21

    ( )

    0

    1( ) j

    i kjN

    Na t

    k

    j

    b t eN

    and2

    1

    ( )

    0

    1( ) ki kj

    N

    Nb tj

    k

    a t eN

    with (0,......, 1)k N . From equation (2.30) we canpredict which modes increase or decrease in time. The

    absolute value of ( )k

    b t decreases to zero as time evolves

    when;

    2sin( ) cos( ) 0

    k

    N

    (2.31)

    and this condition with 0k , gives that the uniformsolution can be viewed as the local stable manifold of

    0jA .

    E.

    SPATIALLY EXTENDED SYSTEM

    In the case that a spatially extended system modelled byincluding unperturbed terms with delayed arguments, thefollowing system is considered;

    23

    2

    ( , ) ( , )( , ) ( , )

    2

    u t x u t xu t x u t x

    t x

    (2.32)

    where , are parameters, is the small

    parameter, and r represents the time delay. Although thesystem is described by a delay partial differential equation, themethod is not changed.

    First the perturbation solution(0) (1) 2( , ) ( , ) ( , ) ( )u t x u t x u t x is obtained by

    solving the following equations;(0) ( , ) 0L u t x ,

    2 ( 0)(1) (0)3

    2

    ( , )( , ) ( , )

    u t xL u t x u t x

    x

    where

    ( , ) ( , )( , )

    2

    u t x u t xL u t x

    t

    The solutions are given by;

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    (0 ) (2 )( , ) ( ) . .,

    i t

    u t x A x e c c

    and2

    2

    2(1) (2 )

    ( )3 ( ) ( )

    ( , )1

    2

    i tA x

    A x A xx

    u t x tei

    where ( , )A t x is an arbitrary differentiable functionof x. Next with the introduction of the renormalized variable

    ( , )A t x we have;

    22

    2

    ( )( , ) ( ) 3 ( ) ( )

    12

    t A xA t x A x A x A x

    xi

    Finally, the renormalized equation which should besatisfied is derived as;

    22

    2

    ( , ) ( )3 ( , ) ( , )

    12

    A t x A xA t x A t x

    t xi

    which is the well known complex Ginzburg-Landauequation

    III. EXTENDED RENORMALIZATION METHOD

    An extended renormalization method can lead to areduced equation with delay from a given system with large ororder-one delay. Large delay means that the delayed

    arguments are of order1

    ( 0)

    with being the small

    parameter associated with the given weakly non-linear system.

    A. LINEAR SYSTEM

    The model which is studied here is given by the equation;2

    2

    2

    ( )

    ( ) 0

    d x t

    x t x tdt

    (3.1)

    where

    represents large delay with being a

    small parameter and 0 is a parameter. When 1 and1 the system was analysed using the multiple-scale

    method as in Ref 23. This system will be analysed using theextended renormalization method and the result comparedwith that of the previous work.

    Firstly the perturbation solution,(0) (0) 2 (0) 3( ) ( ) ( ) ( ) ( )x t x t x t x t is obtained

    by solving the following equations;

    (0) ( ) 0Lx t , (3.2)

    (1) (0)( )Lx t x t

    (3.3)

    (2) (1)( )Lx t x t

    , where;

    22

    2( ) ( ).

    dLx t x t

    dt

    When deriving these equations, the magnitude of1

    in

    the delayed argument is treated as a large value, this treatmentcorresponds to the non-standard expansion in the previousstudy23

    The solution of equation (3.2) is given by;(0) ( ) (0) exp( ) . .,x t A i t c c (3.4)

    where (0)A represents the contribution to thesolution

    (0) ( )x t except for the first motion exp( )i t . We

    assume that the solution(0)

    x att

    is expressed as;

    (0) exp( ) . ..

    i

    x t A e i t c c

    Here,A

    represents the contribution to

    (0)

    x t

    , except for exp( )

    i

    e i t

    .This implies that

    the argument of ( )A t is only affected by a large time shift. At

    this stage the functional form of ( )A t is not known. The

    existence of ( )A t is the most fundamental assumption in this

    extended method. It is noted that the equation which

    ( )A t should perturbatively satisfy is the extended

    renormalization equation. This extended reduced equation isconstructed by removing the secular behaviour coming fromthe resonance between the frequency in the operator L and

    exp( )i t in the forcing terms. When the delay becomes

    zero, the extended method corresponds to the conventionalmethod. Substituting this solution

    (0) ( )x t into equation (3.3),

    the following equation is obtained;

    (1) ( ) exp( ) . ..

    i

    Lx t A e i t c c

    Whose solution is given by;

    (1) ( ) exp( ) . .2

    iit

    x t A e i t c c

    At the next order in , we obtain;

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    22(2 )

    3 3

    2( ) exp( ) . .

    8 8 4

    rt i r r

    x t t A e i t c c

    At this stage, the secular behaviour, as already seen in thecase with delay, is not large.Define the extended renormalized variable as;

    ( ) (0)2

    itA t A A e

    22

    2

    3 3

    2

    8 8 4

    t it A e

    (3.5)

    This definition is a form of a near-identity transformation

    at the function (0)A , instead of the constantA in the

    conventional renormalization method. From this definition of

    ( )A t , we obtain;

    ( ) ( )

    2

    A t A iA e

    2

    2 3

    3 3

    2 2( ) ( , )

    8 8 4

    t iA e

    (3.6)

    where, is a parameter whose value is smaller than

    . The inverse of equation (3.5) is given by;

    2(0) ( ) ( , )2

    itA A t A t e

    Using the above expression, the following relation can beobtained

    2

    ( )

    ( , )2

    im

    i t

    A m A t m A t m e

    (3.7)

    with m . Substituting equation (3.7) into equation(3.6) and taking the limit as 0, the extended

    renormalization method which ( )A t should perturbativelysatisfy is obtained, that is;

    2

    2

    3

    ( )2

    2 8

    i idA t i i

    e A t e A t dt

    (3.8)

    There are delay terms in equation (3.8), and this

    renormalization equation in the case of 1 and 1 isequivalent to reduced equations derived in [13], wherenumerical simulation and some analysis have shown that thereduced system reproduces the behaviour of slow motion in

    the original system. In the case that 0 and is given byequation (2.3), it can be shown that one of the solutions to

    equation (3.8) up to2( ) is given by equation (2.10).

    By comparing this extended renormalization method withthe conventional method discussed in section two above, whenusing the conventional method one cannot obtain a reducedequation.

    The perturbation solutions are;

    (0) ( ) .i tx t Ae c c , (1)( ) . .2

    i

    i titx t Ae e c c

    22(2 )

    3 3( ) . .

    8 8 4

    i

    i tt ix t t Ae e c c

    The renormalized variable is defined as;

    222

    3 3( ) .

    2 8 8 4

    i iit t i

    A t A Ae t Ae

    The renormalization equation up to ( ) becomes;

    ( )( ).

    2

    idA t i

    e A tdt

    (3.9)

    and up to2( ) becomes;

    2

    2

    3

    ( )( ) ( ).

    2 4 8

    i iA t i i

    e A t e A t dt

    (3.10)

    Since the magnitudes of the terms calculated as higher-

    order correction in equation (3.10) are2( ) and 2( ) ,

    this approximation is in contradiction with equation (3.9)

    except for the case of 0 . When 0 , equation (3.10)becomes equation (2.8), and there is no contradiction only inthe case. For systems with large-delay, the extendedrenormalization method can easily be used.

    B. NON-LINEAR OSCILLAOR

    Here, a weakly nonlinear system with large delay, whichusually appears in Optics, is considered. In [14] a system withoptoelectronic feedback is analyzed, and the system isdescribed as;

    2 2

    2

    ( ) 2( ) ( ) 1 ( ) 1 ( )

    1 2

    dx s P y s x s y s C y s

    ds P

    ( ) 1 ( ) ( ),dy s y s x sds

    where s is the scaled time, , ,C P are parameters

    and is the small parameter. The solution of great focusis the small amplitude regime, described by the followingassumptions;

    (1) 2 (2) 3 (3) 4

    ( ) ( ) ( ) ( ) ( )x s x s x s x s

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    (1) 2 (2) 3 (3) 4( ) ( ) ( ) ( ) ( )y s y s y s y s The reduced equation is constructed using the extended

    method, and the result is compared with that reported in [14].

    First the perturbation equations are;

    (1)(1)( )

    ( ),dx s

    y sds

    (1)(1)( )

    ( ),dy s

    x sds

    (2 )(2 )( )

    ( ) ,dx s

    y s Cds

    (2 )(2) (1) (1)( )

    ( ) ( ) ( ),dy s

    x s x s y sds

    (3)

    (3) (1) (1)( ) ( ) ( ) ( ),dx s y s x s Cy sds

    (3)(3) (2) (1) (1) (2)( ) ( ) ( ) ( ) ( ) ( ),

    dy sx s y s x s y s x s

    ds

    where2

    . The solutions (1) ( )x s , (2 ) ( )x s and

    (3) ( )x s are given by;(1)( )x s (0) . .,ise c c

    (2 ) ( )x s

    3

    i(0)

    2

    2 . .,ise c c

    (3) ( )x s 2

    s ( iC(0)

    3

    i | (0)|

    2

    (0) (0) iC ( ) ) . .ise c c higher harmonics.The definition of the renormalized variable is;

    (t) = (0) 22

    s ( iC(0)

    3

    i

    |(0)|2(0) (0) iC(-)). (3.11)

    The renormalization equation is given by;

    d(s) ds =2

    2

    s( iC(s)

    3

    i| (s) |

    2(s) (s)

    iC(s-)). (3.12)

    Equation (3.12) is the reduced equation derived in [14].The extended method gives the same results given by the useof multiple-scale method.

    C. DISCUSSION

    For both the renormalization methods, terms in thereduced equation arise from the terms appearing in the

    perturbation analysis. This implies that higher harmonics inthe perturbation analysis does not contribute to the reducedequation in the first order approximation. In this sense, thereduced equation can be obtained from a wide class includingthe original system.

    In this paper, it has been shown that the renormalizationmethod can be extended to study systems with delay, and themethod gives reduced systems successfully. The application ofthe renormalization method can help elucidate the behaviourof time delayed systems in a non-chaotic regime.

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