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Nonlinear vibrations produced by unbalanced motors

Abstract

The present thesis is concerned with the nonlinear dynamics of vibrating systems excited by unbalanced motors. The main focus is the reciprocal (nonideal) interaction which in general exists between the dynamics of the exciter –the unbalanced motor– and that of the vibrating system. Two models were analytically and numerically studied. First, a 2DoF model of a general structure with a cubic nonlinearity, excited by a nonideal motor, was analysed in detail. The second model is a 3DoF simplified representation of the process of vibrocompaction of quartz agglomerates. The first model requires different treatments depending on the order of magnitude of the slope of the motor characteristics. Then, two cases were considered separately: large and small slope. For the first scenario, a new analytical approach was developed, which combines two well – known perturbation techniques: the Averaging Method and the Singular Perturbation Theory. This scheme allows uncovering the system dynamics as composed of three consecutive stages of time. The first two ones occur in a short time scale and can be considered as a fast transient regime. During the third stage, the system dynamics was shown to be well – represented by a reduced 2D system. A detailed analysis of this reduced system allowed obtaining its fixed points and their stability. As a very relevant outcome of the stability analysis, conditions were found for the existence of a Hopf bifurcation, which had not been addressed before in the literature, to the author’s knowledge. This result is particularly significant, for it shows that the stability region of a stationary motion of the system can be smaller than predicted by usual theories. Thus, not taking the Hopf bifurcation into account may lead to unexpected instabilities in real applications. The Hopf bifurcations were analytically investigated and very simple conditions were derived to characterize them as subcritical and supercritical. Moreover, by using the Poincaré – Béndixson theorem, conditions were found under which all trajectories of the reduced system are attracted towards a limit cycle. This kind of motion in the reduced system corresponds to a quasiperiodic oscillation in the original one. The global bifurcations whereby the found limit cycles disappear were numerically analysed, finding homoclinic and saddle – node homoclinic bifurcations. All these results were validated by comparing numerical solutions of the original and reduced systems, which exhibited a remarkable accordance. The case of small slope was also analytically studied in detail. Having found the existence of a resonance manifold in the phase space, the regions far (outer) and close (inner) to the resonance manifold were separately investigated through averaging techniques. Under certain conditions, the inner region contains two fixed points, whose stability was analysed. As an apparent limitation of the procedure, it was addressed that the time of attraction of one the fixed points was much longer than the time of validity of the averaged system. Consequently, it is not obvious whether or not the stability of that fixed point in the averaged system is necessarily the same as in the original system. The main contribution of this part of the thesis consists in having proved, by using attraction arguments, that solutions of the averaged system near the fixed point of interest are actually valid for all time, thereby solving the above difficulty. The existence of a stable fixed point in the resonance region justifies the possibility of resonance capture. As in the case of large slope, numerical simulations were conducted in order to compare solutions of the original and averaged systems. A good agreement was also found in all the considered scenarios. The final part of the thesis considered a real industrial process, where a mixture of granulated quartz and polyester resin is compacted by using a piston with unbalanced electric motors. A simplified 3DoF model of the process was built, including the nonideal coupling between the motor and the vibrating system, impacts and separation between the piston and the quartz slab and a nonlinear constitutive law for the mixture which models the compaction itself. Although the model is not complex enough to give reliable quantitative results, it is a first step towards the construction of more sophisticated models which are able to predict the behaviour of actual compacting machines. Interestingly, it has been shown that the torque – speed curves obtained in the first chapters of the thesis can also be applied, in an approximate way, to the vibrocompaction model. These curves allow predicting whether a particular set of parameters for the process will give an efficient compaction of the mixture. Several simulations have been conducted, illustrating how such a model could be used to understand the effect of each parameter in the final result of the process.

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Nonlinear vibrations produced by unbalanced motors

Author: González-Carbajal, Javier
Year: 2017
Source: https://idus.us.es/bitstreams/375d7923-0226-47b1-bcce-4e12bfb46954/download
Nonlinea Vib a ions P oduced by
Unbalanced Mo o s
Doc o al Thesis
Ja ie González Ca bajal
Supe ised by
P o . Jaime Domínguez and P o . Daniel Ga cía
Depa men o Mechanical and Manu ac u ing Enginee ing
Facul y o Enginee ing
Uni e si y o Se ille
Ma ch 2017
i
Con en s
1 In oduc ion 1
1.1 S a e o he A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
1.2 Mo i a ion and Objec i es . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
1.3 O ganiza ion o he Documen . . . . . . . . . . . . . . . . . . . . . . . . . . 8
2 Ma hema ical Me hods 13
2.1 Fi s O de A e aging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
2.2 Second O de A e aging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
2.3 Singula Pe u ba ion Theo y . . . . . . . . . . . . . . . . . . . . . . . . . . 19
2.4 Hop Bi u ca ions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22
2.5 The Poinca é-Béndixson Theo em . . . . . . . . . . . . . . . . . . . . . 25
3 The Case o La ge Slope o he Mo o Cha ac e is ic: Analy ical
App oach 27
3.1 P oblem S a emen and Assump ions . . . . . . . . . . . . . . . . . . . . 28
3.2 Al e na i e Fi s O de A e aging . . . . . . . . . . . . . . . . . . . . . . 33
3.3 Pe u ba ion App oach: De i a ion o he Reduced Sys em . . . 36
3.4 Analysis o he Reduced Sys em . . . . . . . . . . . . . . . . . . . . . . . 45
3.5 Classi ica ion o he Hop bi u ca ions . . . . . . . . . . . . . . . . . . 55
ii
3.6 Condi ions unde which all Sys em T ajec o ies a e A ac ed
owa ds a Limi Cycle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63
3.7 Discussion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 66
4 The Case o La ge Slope o he Mo o Cha ac e is ic: Nume ical
Simula ions 71
4.1 Global Bi u ca ions o he Limi Cycles . . . . . . . . . . . . . . . . . 72
4.2 Nume ical Valida ion o Analy ical Resul s . . . . . . . . . . . . . . . 80
5 The Case o Small Slope o he Mo o Cha ac e is ic: Analy ical
App oach 89
5.1 Ou e Region . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92
5.2 Inne Region . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 94
6 The Case o Small Slope o he Mo o Cha ac e is ic: Nume ical
Simula ions 113
7 To que-Speed Cu es o he Whole F equency Range 127
7.1 Compu a ion o he To que-Speed Cu es . . . . . . . . . . . . . . . 128
7.2 A Global Pe spec i e o he Cases o La ge and Small Slope 136
8 Modelling and Simula ion o he Vib ocompac ion P ocess 141
8.1 Some No es on he Real P ocess . . . . . . . . . . . . . . . . . . . . . . 142
8.2 Full Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 144
8.3 Simpli ied Model and To que-Speed Cu es . . . . . . . . . . . . . 156
8.4 Analy ical In es iga ion o a Quasis a ic Vib ocompac ion
P ocess . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 161
8.5 Nume ical Resul s and Discussion . . . . . . . . . . . . . . . . . . . . . 171
9 Summa y and Conclusions 203
Appendix 211
iii
Acknowledgemen s
T as es os cua o años de esis, es oy en deuda con muchas pe sonas y me gus a ía
pode inclui las a odas en es e ag adecimien o. Con ío en que sepan disculpa me
las que, po al a de espacio o po mi despis e exis encial, no apa ezcan
exp esamen e nomb adas.
En p ime luga , quie o ag adece a mis di ec o es, Jaime y Dani, odos sus
buenos consejos y el clima de libe ad que han p opiciado desde el p incipio de
es e abajo. Es oy con encido de que no pod ía habe enido mejo es maes os.
G acias ambién al p o eso Emilio F ei e, po o ien a me sabiamen e cuando me
aden aba en e enos ma emá icos pan anosos.
I would like o exp ess my g a i ude o P o esso Gaë an Ke schen o my s ay a
he Uni e si y o Liège. Wo king wi h his g oup was a wonde ul esea ch
expe ience, in an en i onmen which could no ha e been iendlie . Thanks o
Peppe, who kindly con ibu ed o co ec ypos in he hesis, Lionel, Thibau ,
Chia a, Edoua d, Vincen , I án, Mi co and many mo e good iends ha I hope o
keep o many yea s and made my s ay in Liège wa m and enjoyable.
Thanks o P o esso Jan A. Sande s, who was e y willing o ad ise me abou he
a ac ion p ope ies o a e aged sys ems. His keen e-mail esponses we e uly
help ul o he de elopmen o Chap e 5 in he hesis.
G acias a Joselu, compañe o de a igas desde los mí icos iempos en que
in en amos la osca cuad ada, a Acei uno, Jo ge Julio, Se gio, Me che, Juan,
Da id y al es o de compañe os del depa amen o, po que ha sido una aleg ía
pode abaja odeado de buenos amigos. Ex iendo con gus o es e ag adecimien o
al g an Guido, pese a su obsesión posesi a con el espacio de abajo y con las
papas i as.
A Cha ly, Me chan e, Diego, O ega, Bill, Angeli o, And és, Miguel, Yoshua,
Koc el, Nacho, De ey, Vale a y muchos más, po los buenos a os y ce ezas que
una esis necesi a, aunque sigan pensando que la mía a a de o nillos.

i
A Ma a, mi equipo alpha pa icula , que ha sabido anima me como nadie y
hace lo odo muy lle ade o es os úl imos meses.
Muchas g acias a mis pad es, que son el mejo ejemplo que engo, y a Pablo y Ana,
po su apoyo y su ca iño dia ios. También al es o de mi g an amilia, desde mis
abuelas y abuelos has a Julia y Ra illa. Es e abajo hab ía sido mucho más du o si
no hubie a es ado an bien odeado.
Y p incipalmen e g acias a Dios, a quien le debo odo.
1 INTRODUCTION
The linea heo y o ib a ions is one o he mos use ul ools in he handbook o a
mechanical enginee . I u nishes a solid and well-es ablished ma hema ical
amewo k o concep s such us esonance and linea modes o ib a ion, which a e
cen al o he modal analysis o s uc u es and mechanical sys ems.
A mos appealing quali y o his linea heo y is i s ela i e simplici y. Linea
models exhibi special a ibu es which make hem pa icula ly use ul om a
p ac ical poin o iew, such us he p inciple o supe posi ion –whe eby he
esponse o a linea combina ion o exci a ions can be ob ained as he linea
combina ion o indi idual esponses– o he ac ha se e al a ac o s ne e coexis
– he s a iona y mo ion o a o ced, damped, linea sys em, is independen o he
ini ial condi ions–. I is hanks o hese p ope ies, oge he wi h he ac ha many
eal s uc u es a e well ep esen ed by linea models in hei anges o ope a ion,
2 1 In oduc ion
ha linea ib a ion analysis has become a chie ool in he design o mechanical
sys ems and s uc u es in indus y.
Howe e , linea i y is clea ly an idealiza ion. Na u e is no linea in gene al,
al hough i can be app oxima ely ep esen ed by linea models in some cases. Fo
ins ance, he linea heo y o elas ici y is known o gi e good esul s o s uc u es
unde going small displacemen s and small s ains. Howe e , as soon as
displacemen s become signi ican , nonlinea e ec s need o be conside ed (Luongo,
Rega, & Ves oni, 1986). Some o he possible sou ces o nonlinea i y in mechanical
sys ems a e (Thomsen, 2003)
- Ma e ial nonlinea i ies due o a nonlinea ela ion be ween s esses and
s ains in some ma e ials.
- Nonlinea body o ces, such as magne ic o ae odynamic in e ac ions.
- Nonlinea i ies due o he physical con igu a ion, such as hose associa ed o
discon inuous couplings, clea ances o s ops.
Nonlinea i y plays a key ole in he dynamic beha iou o nume ous eal-wo ld
applica ions. Some examples a e he mo ion o la ge wind u bines, he
c ashwo hiness o ehicles o he ib ocompac ion o g anula ma e ials. The
ae onau ical indus y, wi h g ea in e es in minimizing weigh , is inc easingly
p oducing e y ligh and slende s uc u es, wi h he subsequen ac i a ion o
geome ical nonlinea i ies. The use o ma e ials such as ca bon- ibe composi es in
ae ospace applica ions can also p oduce a signi ican de ia ion om linea i y. I is
e iden ha , in all hese si ua ions, a linea ized model would no be able o cap u e
he eal sys em dynamics. Thus, in o de o ha e eliable p edic ions, nonlinea i y
would need o be included in he model, which in u n implies en e ing he complex
ield o nonlinea dynamics.
Nonlinea dynamics is he b anch o ma hema ics which in ends o unco e he
empo al e olu ion o nonlinea dynamical sys ems. Unlike i s linea coun e pa ,
nonlinea dynamics is no a closed subjec –no e en a ma u e one–. The main
eason is ha , while all linea sys ems a e essen ially he same, each nonlinea
1 In oduc ion 3
sys em is nonlinea in i s own way. This means ha , in gene al, conclusions abou
he beha iou o a pa icula nonlinea sys em canno be gene alized o any o he .
Besides, he dynamics o nonlinea sys ems is ex emely ich, exhibi ing a wide
ange o phenomena which canno occu in linea sys ems, such as mul is abili y,
chaos o limi cycles. All his complexi y ende s i ex emely ha d o ob ain
analy ical solu ions o he nonlinea di e en ial equa ions go e ning he sys em
dynamics. In gene al, i is necessa y o eso o nume ical compu a ions in o de o
ge some insigh in o he sys em beha iou .
F om he abo e conside a ions, i is clea ha a signi ican esea ch e o needs o
be o ien ed o a be e comp ehension o he dynamic beha iou o nonlinea
mechanical sys ems. This will hope ully lead o e icien p edic ions abou he
pe o mance o sys ems whe e nonlinea i y has a signi ican e ec , and will also
mo i a e he design and de elopmen o new nonlinea componen s which a e able
o ou pe o m hei linea coun e pa s. I is he aim o his hesis o con ibu e o
his gene al objec i e, by analysing in de ail a pa icula class o nonlinea sys ems,
namely hose exci ed by unbalanced mo o s.
The mo ion o unbalanced o o s cons i u es one o he mos common ib a ion
sou ces in mechanical enginee ing (Boyaci, Lu, & Schweize , 2015; Yang e al.,
2016). Vib a ions due o unbalance may occu in any kind o o a ing sys ems, such
as u bines, lywheels, blowe s o ans (Shabana, 1996). Ac ually, in p ac ice, o o s
can ne e be comple ely balanced because o manu ac u ing e o s such as po osi y
in cas ing, non-uni o m densi y o he ma e ial, manu ac u ing ole ances, e c. (Xu
& Ma angoni, 1994). E en a subsequen balancing p ocess will ne e be pe ec
due o he ole ances o he balancing machines. Mo eo e , some amoun o
unbalance gene ally appea s du ing he ope a ion o he machine, as a consequence
o une en wea , co osion o unequal build-up o deposi s (di , lime, e c.).
Usually, o o unbalance has a ha m ul e ec on o a ing machine y, since ib a ion
may damage c i ical pa s o he machine, such as bea ings, seals, gea s and
couplings (Xu & Ma angoni, 1994). Howe e , he e a e applica ions whe e
10 1 In oduc ion
ixed poin s o bo h a e aged sys ems a e ob ained and hei s abili y is analysed.
Admi edly, some o he de elopmen s o his Chap e a e no o ally new, bu a
e o mula ion o al eady published ea men s o he p oblem. Howe e , he
s abili y o he s a iona y mo ions o he sys em nea esonance was no o ally
sol ed hi he o. By using a ac ion a gumen s, a de ailed s abili y analysis o hese
solu ions is conduc ed.
Chap e 6 p esen s nume ical esul s which alida e he esul s and conclusions o
Chap e 5.
In Chap e 7, an al e na i e app oxima e me hod is used o ob ain he s a iona y
solu ions o he sys em s udied in p e ious chap e s. This app oach is based on he
Me hod o Di ec Sepa a ion o Mo ions, p oposed by Blekhman (Blekhman, 2000)
and has he ad an age o p o iding a g aphical ep esen a ion o he s a iona y
mo ions which is highly con enien wi h a iew o he ib ocompac ion analysis o
he nex chap e . Fu he mo e, his al e na i e p ocedu e p o ides a e y clea
g aphical compa ison be ween he cases o la ge and small slope conside ed in
p eceding chap e s.
A new model is in oduced in Chap e 8, mo e complex han he one analysed in
p e ious chap e s. This sys em is a i s a emp o model he ib ocompac ion
p ocess, which has no been done be o e, o he au ho ’s knowledge. In addi ion o
he nonlinea i y in insically associa ed o nonideali y, he model includes con ac
and impac s be ween he mix u e and he pla o m suppo ing he unbalanced
mo o , and also be ween he mix u e and he mould whe e i is con ained.
Fu he mo e, a nonlinea cons i u i e law o he mix u e, which allows modelling
he compac ion i sel , is p oposed. I is shown ha , unde some condi ions, his
model can be ans o med in o he simple sys em analysed in Chap e s 3-7, which
makes he p eceding analy ical de elopmen s use ul o he ib ocompac ion
analysis. Se e al nume ical simula ions illus a e how he p oposed model can be
used o in es iga e he e ec o di e en pa ame e s on he inal le el o
compac ion achie ed.

1.3 O ganiza ion o he Documen 11
Finally, Chap e 9 summa ises he conclusions o his wo k and p oposes possible
u he in es iga ions.
2 MATHEMATICAL
METHODS
Be o e he analysis o he p oblem unde s udy, a b ie desc ip ion o he
ma hema ical me hods used wi hin he hesis is p esen ed.
2.1 Fi s O de A e aging
Pe u ba ion me hods cons i u e a b oad class o ma hema ical echniques aimed a
inding app oxima e solu ions o a p oblem, based on he solu ion o a simple
ela ed p oblem. In pa icula , a e aging p ocedu es a e among he mos widely
used pe u ba ion me hods, p esen ing wo ele an s eng hs (Sande s e al., 2007):
- They a e suppo ed by igo ously p o ed heo ems.
- They can be sys ema ically ex ended o any o de o accu acy.
In o de o unde s and he basic idea behind a e aging, conside a sys em o he
o m 󰇗 ( ), whe e is a small pa ame e and is -pe iodic in . The
14 2 Ma hema ical Me hods
dynamics o such sys ems con ains wo di e en ime scales: a as scale, associa ed
o he ac ha depends on , and a slow scale, associa ed o he ac ha is a
slow a iable ( 󰇗 ( )). Then, i can be shown ha he essen ial ea u es o he
sys em a e main ained when i is eplaced by i s co esponding a e aged sys em
󰇗 ∫ ( )
( ). The idea is o ake in o accoun he mean e ec o
he as oscilla o y dynamics h ough a e aging, so ha he second sys em e ains
he long e m beha iou o he i s one. This ans o ma ion is use ul because he
a e aged sys em is au onomous and, he e o e, conside ably easie o analyse han
he non-au onomous o iginal sys em.
Al hough he abo e desc ip ion has been gi en o a e aging o e ime, i is
some imes use ul o a e age o e as o a ing angles, which play essen ially he
same ole as ime. Once he in ui i e idea has been explained, some mo e igo ous
esul s a e now gi en, which will be used h oughou he hesis.
Then, conside an ini ial alue p oblem o he o m
{ 󰇗 ( )
󰇗 ( ) ( )} ( )
( )
(2.1)
whe e is a ec o o slow a iables, is a as o a ing phase and is a
su icien ly small, posi i e, dimensionless pa ame e , . No e ha
ep esen s he ci cum e ence. Hence o say ha me ely means ha ,
wi h unc ions and being -pe iodic in .
Le be he solu ion o
󰇗 ( ) ( )
(2.2)
whe e
2.1 Fi s O de A e aging 15
( )
∫ ( )
(2.3)
Then, i ( ) emains in ,
( ) ( ) ( ) (
⁄)
(2.4)
The p oo can be ound in (Sande s e al., 2007).
This is he s anda d e sion o he heo em o i s o de a e aging o e angles.
No e ha , hanks o his heo em, an asymp o ic app oxima ion o he solu ion ( )
can be ob ained by eplacing he o iginal sys em (2.1) wi h he app oxima e sys em
(2.2). In o he wo ds, i is possible o educe he sys em dimension, om o
, upon a e aging o e he as o a ing phase.
No e also ha , as explici ly s a ed in (2.4), he app oxima ion ob ained h ough
a e aging is only alid du ing a limi ed ime scale. This is a gene al ea u e o
pe u ba ion app oaches, which can be o e come in some si ua ions (e.g. when
a ac ion exis s, as desc ibed la e on in his sec ion). The limi a ion in he ime
scale whe e he app oxima ion is alid will p o e o be c ucial in Sec ion 5.2.
Gene aliza ion o mul i- equency sys ems
The gene aliza ion o his heo em o mul i- equency sys ems is s aigh o wa d
(Sande s e al., 2007). The only ca ea ha needs o be aken in o accoun is ha
unc ion mus be w i en as a sum o unc ions, each o one depending on only
one o he as angles. Thus, conside he mul i- equency sys em gi en by
{ 󰇗 ( )
󰇗 ( ) ( )} ( )
( )
(2.5)
whe e ep esen s he - o us. Then, assuming ha unc ion can be w i en as

16 2 Ma hema ical Me hods
( ) ∑ ( )
(2.6)
he i s o de a e aged sys em can be ob ained as
󰇗 ∑  ( )
( )
(2.7)
wi h  de ined as in (2.3). Then, he e o es ima e is gi en by
( ) ( ) ( ) (
⁄)
(2.8)
This mul i- equency e sion o he heo em will be used in Sec ion 5.1.
The concep o ‘Resonance Mani old’
A c ucial poin o his a e aging p ocess is ha , o he app oxima ion o be alid,
each equency ( ) mus be bounded away om ze o. The eason is ha , when
any ( ) app oaches ze o, a anishing denomina o appea s in he highe o de
e ms o eqs. (2.4) and (2.8). (This will be seen clea ly in equa ion (2.12) o Sec ion
2.2.)
The se s o o which one o mo e unc ions ( ) anish a e called ‘ esonance
mani olds’. The ailu e o a e aging in he icini y o esonances can be easily
unde s ood by no icing ha , nea a esonance mani old, one o mo e angles a e
no as and, consequen ly, we canno a e age o e hem.
The main consequence is he ollowing: away om esonances, i is possible o
a e age o e all angles. Howe e , in he icini y o a esonance mani old, we can
only a e age o e pa icula angles, namely hose whose equencies emain
bounded away om ze o. This dis inc ion will be necessa y in Chap e 5.
2.1 Fi s O de A e aging 17
A e aging wi h A ac ion
Asymp o ic app oxima ions ob ained by a e aging a e, in gene al, alid on a ime
scale
⁄. Howe e , his ime scale can be enla ged i he e exis s a ac ion in he
a e aged sys em (Sande s e al., 2007).
Conside again a sys em o he o m (2.1), wi h a e aged sys em (2.2).
Suppose is an asymp o ically s able ixed poin o sys em (2.2), wi h domain
o a ac ion . Then, o all , i can be shown ha
( ) ( ) ( ) , )
(2.9)
Thus, he app oxima ion is uni o mly alid –i.e. alid o all ime– o solu ions o
he a e aged sys em which a e a ac ed by an asymp o ically s able ixed poin .
Two di e en p oo s o his heo em ha e been gi en by Sánchez-Palencia
(Sanchez-Palencia, 1975) and Eckhaus (Wik o Eckhaus, 1975).
A simila esul holds o ajec o ies o he a e aged sys em which a e a ac ed by
an asymp o ically s able limi cycle. In his case, he app oxima e solu ion is alid
on , ) o all a iables excep he angula one, i.e. he a iable which
measu es he low on he closed o bi (Sande s e al., 2007). This is equi alen o
say ha he closeness o he limi cycle can be uni o mly app oxima ed, ye no he
posi ion on i . The eason is ha any small de ia ion on he equency is
accumula ed o e he cycles, gi ing ise o la ge e o s a e a su icien numbe o
pe iods.
2.2 Second O de A e aging
In some si ua ions, mo e accu a e app oxima ions han hose p o ided by a i s
o de a e aging (Sec ion 2.1) a e equi ed, as will be he case in Chap e 5 o his
18 2 Ma hema ical Me hods
hesis. Fo una ely, he e exis gene al esul s o o de a e aging which allow
inc easing he p ecision o he app oxima ion as much as needed. He e we only
show some esul s o o de 2, which is enough o he pu pose o his hesis. Hence
conside a sys em o he o m
8 󰇗 ( ) ( ) , -( )
󰇗 ( )9 ( )
( )
(2.10)
whe e, ollowing he no a ion in (Sande s e al., 2007), b acke s a e used in , - o
s ess ha his e m is a emainde o an expansion in powe s o . This is also
no ed by he ac ha , - depends on , while and do no .
Le * ( ) ( )+ be he solu ion o
8 󰇗  ( )  ( )
󰇗 ( )9 ( ) ( )
( )
(2.11)
whe e  is de ined as in (2.3) and
( )
∫[ ( )  ( )]
(2.12)
 ( )
∫[ ( ) ( ) ( )]
(2.13)
Cons an in (2.12) is chosen in such a way ha
∫ ( )
(2.14)
2.2 Second O de A e aging 19
while symbol in (2.13) ep esen s di e en ia ion wi h espec o . Then, he
e o es ima e is
( ) ( ) ( ( ) ( )) ( ) (
⁄)
(2.15)
This esul will be used in Chap e 5. The p oo can be ound in (Sande s e al.,
2007).
No e he p esence o in he denomina o o exp ession (2.12), in connec ion wi h
he concep o ‘ esonance mani old’ explained in Sec ion 2.1. A anishing
equency would make unbounded and, acco ding o (2.15), he
app oxima ion would no be alid anymo e. In o he wo ds, he a e aging
ans o ma ion becomes singula when app oaches ze o.
2.3 Singula Pe u ba ion Theo y
The Singula Pe u ba ion Theo y (SPT) explains he beha iou o a pa icula class
o as -slow sys ems (Hun e , 2004; Lesne, 2006; Ve huls & Bak i, 2006). As has
been done wi h a e aging, an in ui i e desc ip ion o he heo y is i s gi en,
ollowed by he exposi ion o some mo e igo ous esul s which will be used la e
on in he hesis.
Sys ems whe e he SPT is applicable a e hose exhibi ing a singula limi . This
means ha he sys em depends on a pa ame e in such a way ha , when he
pa ame e app oaches some limi ing alue, he gene al solu ion o he p oblem is
quali a i ely di e en o he solu ion o he limi ing p oblem. Typically, sys ems o
his ype exhibi wo sepa a e ime scales –o space scales– wi h e y di e en
beha iou s. A well-known example is he bounda y laye heo y in luid mechanics,
whe e he e ec s o iscosi y a e ele an in a e y hin laye o luid, close o a
bounding su ace, while being negligible o he es o he domain.
26 2 Ma hema ical Me hods
is o ien ed inwa ds, as depic ed in Fig. 2.3. Then, all ajec o ies which s a inside
a e es ic ed o emain inside.
Fig. 2.3 Phase po ai showing a closed, bounded egion wi h he low di ec ed
inwa ds a he bounda ies. I con ains no ixed poin s, hen i con ains a leas one
s able limi cycle.
R

3 THE CASE OF LARGE
SLOPE OF THE MOTOR
CHARACTERISTIC:
ANALYTICAL
APPROACH
This Chap e in es iga es he dynamics o a 2-DOF sys em consis ing in an
unbalanced mo o a ached o he ixed ame by a nonlinea sp ing and a linea
dampe . As commen ed in he in oduc ion, wo di e en scena ios need o be
conside ed sepa a ely, depending on he o de o magni ude o he slope o he
mo o cha ac e is ic. The Case o a La ge Slope is conside ed in his Chap e and
he ollowing, while he al e na i e si ua ion will be s udied in Chap e s 5 and 6.
28 3 The Case o La ge Slope: Analy ical App oach
3.1 P oblem S a emen and Assump ions
Conside he sys em depic ed in Fig. 3.1. I consis s in an unbalanced mo o
a ached o a ixed ame by a nonlinea sp ing –whose o ce has linea and cubic
componen s– and a linea dampe . The cubic componen o he sp ing gi es he
possibili y o model a nonlinea beha io o he s uc u e suppo ing he mo o
(Me le , 1962). The e ec o g a i y can be shown o ha e no ele ance
(Dimen be g e al., 1997) and, he e o e, i will no be included in he model.
Fig. 3.1 Model
Va iable s ands o he linea mo ion, is he angle o he o o , is he
unbalanced mass wi h eccen ici y , is he es o he ib a ing mass, is he
o o ine ia (wi hou including he unbalance), is he iscous damping coe icien
and and a e, espec i ely, he linea and cubic coe icien s o he sp ing. The
equa ions o mo ion o he coupled 2-DOF sys em a e (El-Badawy, 2007)
󰇘 󰇗 ( 󰇗 󰇘 )
󰇘 ( 󰇗) 󰇘
(3.1)
whe e , and an o e do ep esen s di e en ia ion wi h
espec o ime, .
Func ion ( 󰇗) is he d i ing o que p oduced by he mo o –gi en by i s o que-
speed cu e, also known as s a ic cha ac e is ic– minus he losses o que due o
0
I
0
m
1
m
b
x

,
k

3.1 P oblem S a emen and Assump ions 29
ic ion a he bea ings, windage, e c. We assume his ne o que o be a linea
unc ion o he o o speed:
( 󰇗) 󰇗
(3.2)
Al hough ( 󰇗) includes he damping o o a ional mo ion, we will usually e e o
i sho ly as ‘ he mo o cha ac e is ic’.
As will be seen la e , i is con enien o he pu pose o his chap e o w i e he
d i ing o que in an al e na i e way. Then, deno ing by he linea na u al
equency o he oscilla o , gi en by √
⁄, he mo o o que can be w i en
as
( 󰇗) ( 󰇗 )
(3.3)
whe e ep esen s he d i ing o que a esonance ( ( ) ). F om equa ions
(3.2) and (3.3), he ela ion be ween cons an s and can be di ec ly deduced:
(3.4)
Along he whole hesis, he mo o cha ac e is ic will be w i en as (3.2) o (3.3),
depending on he si ua ion. I should be kep in mind ha hese wo exp essions a e
o ally equi alen . The impo an poin is ha he d i ing o que is assumed o
ollow a linea ela ion wi h he o o speed. I is u he assumed ha – he
d i ing o que dec eases wi h he o o speed–, as is usual o mos kinds o mo o .
This assump ion will p o e o be o majo impo ance.
30 3 The Case o La ge Slope: Analy ical App oach
Fig. 3.2 Typical s a ic cha ac e is ic o an asynch onous mo o
Fig. 3.3 S a ic cha ac e is ic co esponding o equa ion (3.3)
As an example, he s a ic cha ac e is ic o an induc ion mo o is depic ed in Fig. 3.2.
No e ha such a mo o is usually designed o wo k on he egion 󰇗 , whe e
he cu e could be easonably app oxima ed by a s aigh line wi h nega i e slope.
The simpli ied mo o cha ac e is ic gi en a (3.3) is ep esen ed in Fig. 3.3.
m
L

m
L
n

C
1
D
peak


3.1 P oblem S a emen and Assump ions 31
In he second o equa ions (3.1), which imposes he equilib ium o he o o , he las
e m is o g ea signi icance, since i accoun s o he o que on he o o caused by
linea mo ion o he sys em. I s physical in e p e a ion can be eadily unde s ood
wi h he aid o Fig. 3.4. Due o displacemen ( ), a ho izon al ine ial o ce ac s on
he unbalanced mass and gene a es a o que wi h espec o he o o axis. This
pa icula e m o he equa ions o mo ion is wha makes he exci a ion nonideal, o
i akes in o accoun how ib a ion in luences o a ion. I his o que due o
ib a ion did no exis –o i i was negligible–, he o o equilib ium equa ion
would educe o 󰇘 ( 󰇗), and i could be sol ed o ( ) ega dless o he
linea mo ion. Then, his solu ion ( ) could be in oduced in he i s o equa ions
(3.1) as a p esc ibed exci a ion.
Fig. 3.4 To que on he o o due o ib a ion
By de ining
⁄
⁄
√
(
)
(3.5)
he equa ions o mo ion can be w i en in a mo e con enien dimensionless o m
󰇘 󰇗 ( 󰇗 󰇘 )
󰇘 ( 󰇗 ) 󰇘
(3.6)
1
mx
sin


x
1
m

32 3 The Case o La ge Slope: Analy ical App oach
whe e a do now ep esen s di e en ia ion wi h espec o dimensionless ime, .
In o de o apply pe u ba ion echniques o sys em (3.6), some assump ions on he
o de o magni ude o he sys em pa ame e s ha e o be made. Thus, we assume he
damping, he unbalance and he nonlinea i y o be small. This is exp essed by
making he co esponding coe icien s p opo ional o a su icien ly small, posi i e
and dimensionless pa ame e :
(3.7)
whe e pa ame e s wi h subsc ip a e -independen . I is also assumed ha he
o que gene a ed by he mo o a esonance ( 󰇗 ) is su icien ly small:
(3.8)
Finally, he slope o he mo o cha ac e is ic is assumed o be o he o de o uni y,
i.e. independen o :
(3.9)
This assump ion co esponds o wha we ha e called ‘la ge slope cha ac e is ic’.
The case o small slope, wi h p opo ional o , is ea ed in Chap e s 5 and 6.
Taking he p oposed scaling (3.7)-(3.9) in o accoun and d opping he subsc ip ‘ ’
o con enience, sys em (3.1) akes he o m
󰇘 [ 󰇗 ( 󰇗 󰇘 )]
󰇘 ( 󰇗 ) , 󰇘 -
(3.10)
3.2 Al e na i e Fi s O de A e aging 33
3.2 Al e na i e Fi s O de A e aging
Be o e u ning o he ea men o sys em (3.10) h ough some pe u ba ion
echniques, an al e na i e a e aging p ocedu e is de eloped in his sec ion, which
will be use ul in wha ollows. In o de o make he p ocedu e as gene al as
possible, conside a sys em o he o m
{ 󰇗 , ( )- ( )
󰇗 ( ) ( )
󰇗 ( )}
(3.11)
whe e and a e ma ices o cons an coe icien s and is a scala cons an ,
bounded away om ze o. I will be shown in he nex sec ion ha sys em (3.10) can
be w i en in he o m (3.11).
Suppose ha we y o pe o m a i s o de a e aging on sys em (3.11) o e angle
. Acco ding o he esul s explained in Sec ion 2.1, such a echnique is no
applicable in his case, because he se o a iables is no slow. In o de o use he
heo em o Sec ion 2.1 we would need o ha e 󰇗 ( ) and 󰇗 ( ), which is
no he case. This jus i ies he in oduc ion o he modi ied echnique p esen ed
below.
Fi s , he a e aged a iables a e de ined as
( ) ∫ ( )
⁄
⁄ ( ) ∫ ( )
⁄
⁄
(3.12)
whe e
⁄. As illus a ed in Fig. 3.5, he e ec o he ope a o de ined in
(3.12) is o smoo h ou he sho - e m luc ua ions o each a iable, while e aining
he long- e m beha io .
34 3 The Case o La ge Slope: Analy ical App oach
Fig. 3.5 De ini ion o he a e aged a iables
Suppose we a e in e es ed in he e olu ion o he a e aged a iables ( ) and ( ).
Then, we can a e age he i s wo equa ions in (3.11), which yields
{
󰇗 [  ∫ ( ( ) ( ))
⁄
⁄] ( )
󰇗  ∫ ( ( ) ( ))
⁄
⁄ ( )
}
(3.13)
whe e i has been used ha he a e age, as de ined in (3.12), is a linea ope a o ( he
a e age o he sum is he sum o he a e ages).
The nex s ep consis s in ans o ming he in eg als in (3.13). Since he p ocess is
exac ly he same o bo h in eg als, we only ocus on he i s o hem.
Fi s , we can w i e
6.4 6.6 6.8 7 7.2
0
0.2
0.4
0.6
0.8
1
x
x
3.2 Al e na i e Fi s O de A e aging 35
∫ ( ( ) ( ))
⁄
⁄ ∫ ( ( ) ( ))
⁄
⁄ ( )
(3.14)
whe e i has been used he p ope y ha , in one pe iod , ( ) can only change by
( ), acco ding o (3.11). Thus, we can w i e ( ) ( ) ( ). Changing he
in eg a ion a iable om o yields
∫ ( ( ) ( ))
⁄
⁄ ( )
∫ ( ( ) )
(
⁄)
(
⁄) ( )
(3.15)
whe e he las o ela ions (3.11) has been used ( ( )). The
in eg a ion limi s can also be ans o med by using again 󰇗 ( ):
∫ ( ( ) )
(
⁄)
(
⁄) ( )
∫ ( ( ) )
( )
( ) ( )
(3.16)
Finally, as unc ion is -pe iodic in , we can w i e
∫ ( ( ) )
( )
( ) ( )
∫ ( ( ) )
( )
(3.17)
By compa ing his las exp ession o de ini ion (2.3), sys em (3.13) can be ew i en
as
8 󰇗 ,  ( )- ( )
󰇗  ( ) ( )9
(3.18)
42 3 The Case o La ge Slope: Analy ical App oach
can be w i en as
( )
(3.41)
which is he exp ession o he Slow Mani old: a 2D su ace in he 3D phase
space. Thus, he i s condi ion is sa is ied.
2. Fo ixed alues o and , i is ound ha ( ) is a globally
asymp o ically s able ixed poin o he 1D sys em
󰇗
(3.42)
p o ided ha assump ion holds. The e o e, he second condi ion is
also ul illed.
Once bo h equi emen s ha e been e i ied, i can be s a ed ha sys em (3.38)
displays wo quali a i ely di e en beha io s a wo sequen ial ime scales –see
Sec ion 2.3–, which co espond o he second and hi d s ages o he o iginal sys em
(3.26). Using he esul s o Sec ion 2.3, we ha e ha , a he i s o hese s ages –
second s age o (3.26)–, he sys em can be w i en as
( )
( )
󰇗 ( )
(3.43)
whe e i has been aken in o accoun ha , a he beginning o s age 2,
( ) and ( ). Then, a his s age, he sys em is a ac ed owa ds he
Slow Mani old, wi h he slow a iables emaining nea ly cons an :
( )
(3.44)

3.3 Pe u ba ion App oach: De i a ion o he Reduced Sys em 43
Summing up, he second s age co esponds o a ime leng h ( ), jus as he
i s one. I ends once a iable has eached an ( )–dis ance o ( ).
Du ing his phase o he mo ion, and do no change signi ican ly.
Thi d s age
The hi d s age o he o iginal sys em (3.26) –which is he second s age o he
a e aged sys em (3.38)– occu s a a ime scale (
⁄). This can be easily
unde s ood by no icing ha , once he sys em is nea he slow mani old, a iable
becomes slow (in oducing (3.41) in (3.38) leads o 󰇗 ( )). The e o e, nea he
slow mani old, all a iables a e slow and, as a consequence, he sys em na u al ime
scale is (
⁄).
By in oducing he exp ession o he slow mani old in (3.38), he equa ions
co esponding o he hi d phase o he mo ion a e ob ained:
{
󰇗 ( ) ( )
󰇗 ( ( )
) ( )
( ) ( )
}
(3.45)
As usual, highe o de e ms in (3.45) can be elimina ed, gi ing ise o an ( )
app oxima ion o a ime leng h (
⁄):
{ 󰇗 ( )
󰇗 ( ( )
)
( ) }
(3.46)
I is con enien o obse e ha , al hough (3.46) con ains h ee equa ions, only wo
o hem a e di e en ial equa ions. Thus, (3.46) ep esen s a 2D au onomous
dynamical sys em. The e olu ion o and no longe depends on , once is
w i en as a unc ion o and . The las equa ion is w i en wi h he only pu pose
o acking he e olu ion o a iable .
44 3 The Case o La ge Slope: Analy ical App oach
In summa y, he hi d s age co esponds o a ime leng h (
⁄). A his phase
o he mo ion, he a e aged sys em e ol es along he slow mani old gi en by
(3.41). Va iables , and obey equa ions (3.46), wi h ( ) p ecision.
Fig. 3.6 shows a schema ic ep esen a ion o he h ee di e en s ages o he sys em
dynamics, summing up he esul s ob ained in he p esen sec ion. No e ha , in Fig.
3.6, he use o o e ba s o he a e aged a iables is eco e ed. The mos ele an
esul is ha , once he ini ial ansien co esponding o he i s wo s ages has
inished, he e olu ion o a iables and is go e ned by equa ions (3.46) –wi hin
an ( ) e o –.
F om Fig. 3.6, i is clea ha sui able ini ial condi ions o sys em (3.46) a e
* +. Recalling de ini ion (3.31), his can be w i en as * ( )
⁄+,
whe e * + is he se o ini ial condi ions o sys em (3.26)
Fig. 3.6 O e iew o he sys em dynamics, wi h * + being he solu ion o
sys em (3.46) wi h app op ia e ini ial condi ions.
S age 3
S age 2
S age 1
0
0
0
a


0
0
1
()
()
()
*
aa O
O
O

  







00
0
0
()
()
( ) ( )
*
*
*,
aa
a
O
O
O

  
   






0


0
0
1
()
*
aa O






00
0
0
()
()
()
*
**,
aa
a
O
O

  
  





()
()
( ) ( )
*,
RR
R
R
aa
a
O
O
O

  
   







(1)O


(1)O


()
1
O


3.3 Pe u ba ion App oach: De i a ion o he Reduced Sys em 45
Howe e , we may be in e es ed in a pa icula se o ini ial condi ions o sys em
(3.10), gi en as { 󰇗 󰇗 }. I is, hen, con enien , o exp ess he ini ial
condi ions o (3.46) as unc ions o he ini ial condi ions o (3.10):
√ 󰇗
( 󰇗
) 󰇗
(3.47)
as can be eadily deduced om ela ions (3.20), (3.25) and (3.31).
Recapi ula ing, we ha e been able o elimina e om he o mula ion a iable by
A e aging, and a iable by applying he Singula Pe u ba ion Theo y.
3.4 Analysis o he Reduced Sys em
This sec ion ocuses on he beha iou o sys em (3.46), once i has been shown o
cap u e, wi h ( ) p ecision, he dynamics o he o iginal sys em (3.10) du ing he
hi d s age o he mo ion.
Fi s ly, i is use ul o make a compa ison be ween he sys em unde s udy and i s
ideal coun e pa , whe e he o o speed is cons an . Clea ly, o his ideal case, he
equa ion o mo ion o he sys em shown in Fig. 3.1 is gi en by
󰇘 󰇗 󰇗
(3.48)
wi h 󰇗 ixed. Equa ion (3.48) desc ibes a Du ing oscilla o , subjec ed o ha monic
exci a ion. This is a e y well-known p oblem, which has been widely s udied in he
li e a u e (B ennan, Ko acic, Ca ella, & Wa e s, 2008; Fidlin, 2006; Nay eh &
Mook, 1995; Thomsen, 2003). Unde he assump ions o small damping, small
46 3 The Case o La ge Slope: Analy ical App oach
nonlinea i y, small unbalance and nea - esonan exci a ion ( 󰇗 ), he
A e aging Me hod can be applied o sys em (3.48), leading o
{ 󰇗 ( )
󰇗 (
)}
(3.49)
whe e all he pa ame e s and a iables a e de ined as in Sec ions 3.1 and 3.3. I is
easy o e i y ha sys em (3.49) is exac ly he same as (3.46), wi h he only
di e ence o eplacing ( ) by he cons an alue . This is a clea illus a ion
o he concep o nonideal exci a ion. In he ideal case, he o o speed appea s in
equa ions (3.49) as a cons an alue , ex e nally imposed by he mo o . Howe e ,
in he nonideal case, he o o speed en e s equa ions (3.46) as a unc ion o he
sys em ib a o y mo ion, ( ).
I is also impo an o obse e ha an ideal mo o displays a e ical s a ic
cha ac e is ic, co esponding o he limi case . The mo o is, hen, able o
gene a e any o que o he same o o speed. This sugges s he idea ha a eal
mo o wi h a s a ic cha ac e is ic o e y la ge slope (in absolu e alue) is mo e
likely o beha e in an ideal manne han ano he one wi h a smalle slope.
Fixed poin s
Going back o he objec i e o analyzing sys em (3.46), i is i s con enien o look
o i s ixed poin s, { }:
( )
( )
(3.50)
F om he i s o equa ions (3.50), we ha e
3.4 Analysis o he Reduced Sys em 47
√
(3.51)
Combining (3.41), (3.50) and (3.51) yields
√
(3.52)
Solu ions o (3.52), o bo h alues o , gi e o all he ixed poin s o (3.46).
This can be done analy ically, bu he exp essions become cumbe some and
di icul o in e p e . An al e na i e p ocedu e is p oposed, which leads o he ixed
poin s o (3.46) in a g aphical way. To his end, he las o equa ions (3.46) can be
ew i en as
(3.53)
whe e de ini ion (3.41) has been used. Now, ecall he las o equa ions (3.38),
which go e ns he e olu ion o he o o speed o he a e aged sys em:
󰇗 ( )
(3.54)
In he ligh o (3.54), (3.53) can be in e p e ed as an equilib ium be ween wo
o ques on he o o . The le hand e m in (3.53) ep esen s he d i ing o que
p oduced by he mo o , while he igh hand e m ep esen s he esis ing o que due
o ib a ion. Thus, he ac ha he a e aged sys em is on he slow mani old –which
is exp essed in equa ion (3.53)– can be unde s ood as a o que equilib ium
condi ion.
Equa ion (3.53), pa icula ized o he ixed poin { }, akes he o m

48 3 The Case o La ge Slope: Analy ical App oach
(3.55)
whe e (3.50) has been used. We now de ine he ollowing unc ions:
( )
( )
(3.56)
Clea ly, acco ding o he commen s below equa ion (3.54), ep esen s he
d i ing o que p oduced by he mo o , while co esponds o he esis ing o que
due o ib a ion. Then, (3.55) can be ew i en as
( ) ( )
(3.57)
which is he o que equilib ium condi ion, pa icula ized o he ixed poin .
In o de o sol e (3.57) in a g aphical way, i would be desi able o w i e bo h
o ques explici ly in e ms o . Howe e , his would in u n need explici ly
w i ing in e ms o , which p oduces long and complica ed exp essions.
Thus, an implici p ocedu e o he g aphical ep esen a ion is p oposed. Combining
(3.50) and (3.51) esul s in
( )
(3.58)
whe e unc ion ( ) is de ined as
( ) √
(3.59)
The p oposed ep esen a ion can be cons uc ed as ollows: i s , g aph e sus
acco ding o (3.56). Then, g aph on he same plo he pa ame ic cu e gi en by
3.4 Analysis o he Reduced Sys em 49
* ( ) ( )+, o and ( -. The ac ha is s ic ly posi i e
comes om he de ini ion o as he adius o a pola coo dina e ans o ma ion –
see (3.20)–. On he o he hand canno be g ea e han 1, acco ding o he i s o
equa ions (3.50).
The abo e p ocedu e gi es ise o a plo like ha shown in Fig. 3.7. Conside ing
equa ion (3.57), he ixed poin s can be ound as he in e sec ions o he wo o que
cu es. In he pa icula case displayed in Fig. 3.7, he e a e h ee equilib ium
poin s, ma ked wi h ci cles. No e ha he cu e associa ed o he ib a ion o que is
composed o wo b anches, which collide a he maximum o he cu e. They
co espond o he wo possible alues o pa ame e , as speci ied in Fig. 3.7.
Fig. 3.7 Fixed poin s o sys em (3.46)
We no e ha he ‘Somme ed e ec ’, which was desc ibed in he in oduc ion, can
be eadily explained by using Fig. 3.7. Fo such an explana ion, he in e es ed
eade can e e o (Blekhman, 2000; Dimen be g e al., 1997; Kononenko, 1969;
Nay eh & Mook, 1995).
-2 0 2 4 6 8 10 12
0
0.5
1
1.5
2
2.5
1z

T
T
1z
m
T
50 3 The Case o La ge Slope: Analy ical App oach
S abili y Analysis
Once he ixed poin s o he educed sys em ha e been ob ained, i is con enien o
in es iga e hei s abili y. Fo a 2D sys em, his educes o calcula ing he ace and
de e minan o he jacobian ma ix, e alua ed a he equilib ium poin o in e es :
[
(
)
]
(3.60)
whe e s ands o √
.
The condi ions o a ixed poin o be asymp o ically s able a e
( )
(3.61)
( )
(3.62)
A e some algeb a, hese condi ions can be exp essed as
(3.63)
{
}
(3.64)
whe e deno es he slope o he cu e a he conside ed equilib ium poin (see
Fig. 3.8 and Fig. 3.9), and has he exp ession
3.4 Analysis o he Reduced Sys em 51
(3.65)
as can be deduced om (3.56), (3.59).
Condi ions (3.63) and (3.64) a e now applied o e alua e s abili y egions in
di e en scena ios. The p ocedu e is as ollows. Conside pa ame e s ixed,
so ha he cu e –see Fig. 3.7– is ixed oo. Conside a pai o alues ( )
which gi es a pa icula cu e ( ). The in e sec ions be ween he wo cu es
ep esen he equilib ium poin s o he sys em. Selec one o hem –i he e a e mo e
han one– and le pa ame e s ( ) a y in such a way ha he selec ed equilib ium
poin emains an equilib ium poin . In o he wo ds, le pa ame e s ( ) a y so as
o make he cu e ( ) o a e a ound he selec ed equilib ium poin , sa is ying
es ic ion . Finally, use condi ions (3.63) and (3.64) o analyze how he
s abili y o he ixed poin is a ec ed by he slope o he mo o cha ac e is ic.
Fig. 3.8 displays he ou come o applying he abo e p ocedu e o a ixed poin
loca ed a he le b anch o he ib a ion o que cu e ( ). Two scena ios a e
conside ed, depending on he sign o slope , e alua ed a he ixed poin unde
conside a ion. I is obse ed ha a change o s abili y occu s when bo h o que
cu es become angen ( ). This can be shown o co espond o a ansc i ical
bi u ca ion. No e ha , in Fig. 3.8, he mo o cu e co esponding o has been
di ec ly labeled as , ins ead o ( ). This sho ened no a ion will be
widely used in he igu es o he documen .
Fig. 3.9 shows analogous esul s o a ixed poin loca ed a he igh b anch o he
ib a ion o que cu e ( ). The sys em beha io is iche in his case, since
s abili y may change in wo di e en ways, depending on he compa ison
whe e is de ined below.
58 3 The Case o La ge Slope: Analy ical App oach
T ans o ma ion o he eal eigenbasis o ma ix
A new change o a iables, using he eal eigenbasis o ma ix , is de ined:
0 1 0
1
(3.76)
whe e he columns o ma ix a e he eal and imagina y pa s o he complex
conjuga e eigen ec o s o , deno ed by :
0
1 0
1 0
1
(3.77)
wi h
√4
5
(3.78)
Sys em (3.73), w i en in e ms o he new a iables, akes he o m
[ 󰇗 󰇗] ([
]0
1 [ ( )
( )])
(3.79)
whe e unc ions and , con aining he nonlinea e ms o he sys em, can be
w i en as Taylo se ies:

3.5 Classi ica ion o he Hop Bi u ca ions 59
( ) ∑
( ) ∑
(3.80)
Coe icien s and a e speci ied in he Appendix.
No e ha he sys em is inally w i en in he o m (2.21). Thus, he esul explained
in Sec ion 2.4 can be di ec ly applied.
T ans o ma ion o No mal Fo m
Sys em (3.79) can be ans o med o i s No mal Fo m by a s anda d p ocedu e
(Guckenheime & Holmes, 1983; Kuzne so , 1998), as desc ibed in Sec ion 2.4:
󰇗
(3.81)
whe e pa ame e is ob ained as
{
, ( ) ( ) -}
(3.82)
In summa y, i can be said ha , a e a la ge numbe o a iable ans o ma ions,
sys em (3.46) can be w i en as (3.81), om which i is concluded ha he
bi u ca ion is supe c i ical (subc i ical) i ( ).
Despi e he ac ha coe icien s and a e o a he complica ed o m, we ind
–wi h he aid o so wa e o symbolic compu a ion (Ma lab)– ha he condi ion o
supe c i icali y o subc i icali y can be exp essed in a su p isingly simple manne :
60 3 The Case o La ge Slope: Analy ical App oach
(3.83)
Fig. 3.11 De ini ion o slope
F om (3.83), i is clea ha a nonlinea i y o he so ening ype ( ) is needed o
ha e a supe c i ical bi u ca ion.
I is also wo h no ing ha condi ions (3.83) admi a e y clea g aphical
in e p e a ion. Conside a cu e which in e sec s a he equilib ium poin
unde conside a ion and also a he peak o cu e . Le deno e he slope o his
pa icula mo o cha ac e is ic, as depic ed in Fig. 3.11.
In o de o ob ain , he coo dina es o he wo poin s de ining he s aigh line a e
de ined below. Fi s , he highes peak o cu e can be shown o co espond o
. Subs i u ing his condi ion in (3.56) and (3.59) yields
(3.84)
T
T
P
d

3.5 Classi ica ion o he Hop Bi u ca ions 61
On he o he hand, he ( ) coo dina es o he equilib ium poin unde s udy a e
di ec ly gi en in (3.56) and (3.59):
(3.85)
Then, om (3.84) and (3.85), he exp ession o can be eadily ob ained:
(3.86)
By compa ing (3.86) and (3.66), condi ions (3.83) can be exp essed as
(3.87)
This las manne o cha ac e izing he bi u ca ion is ce ainly appealing om a
g aphical poin o iew, since he basic in o ma ion abou he bi u ca ion can be
di ec ly obse ed om he o que–speed cu es, as shown in Fig. 3.12 o wo
pa icula examples.
62 3 The Case o La ge Slope: Analy ical App oach
Fig. 3.12 Examples o (a) subc i ical and (b) supe c i ical bi u ca ions.
(a)
(b)
-4 -3 -2 -1 01234
0
0.1
0.2
0.3
0.4
0.5

T
-10 -5 0 5
0
0.1
0.2
0.3
0.4
0.5

T
(a)
(b)
T
P
d
H
d
T
P
d
H
d
3.6 Condi ions o he Sys em o be Always A ac ed by a Limi Cycle 63
3.6 Condi ions unde which all Sys em T ajec o ies a e
A ac ed owa ds a Limi Cycle
In Sec ion 3.5, a simple condi ion has been ob ained o asce ain whe he he Hop
bi u ca ion unde s udy is subc i ical o supe c i ical, which in u n allows
p edic ing he kind o limi cycle gene a ed by he bi u ca ion (see Fig. 3.10).
Al hough his dis inc ion is ele an , i is based on a local analysis and,
consequen ly, i only gi es local in o ma ion abou he sys em beha iou . This is so
in wo senses: he analysis o Sec ion 3.5 p o ides insigh in o he sys em dynamics
- o alues o close enough o ( esul s a e local in he pa ame e space)
and
- o ajec o ies close enough o he in es iga ed ixed poin ( esul s a e local
in he phase plane).
In iew o he a o emen ioned limi a ions, his sec ion add esses a new global esul
ha complemen s hose o Sec ion 3.5. I will be shown ha , unde ce ain
ci cums ances, he Poinca é-Bendixson (P-B) heo em can be used o p o e ha all
ajec o ies o he sys em unde s udy a e a ac ed owa ds a limi cycle. Fo a b ie
explana ion o he heo em, see Sec ion 2.5.
Fi s , i can be easily deduced om (3.46) ha
󰇗
(3.88)
Le and ep esen pola coo dina es on he phase plane, acco ding o (3.70), and
le deno e a ci cle cen ed a he o igin o he phase plane wi h a adius sligh ly
g ea e han , say . F om (3.88), i can be said ha e e y ajec o y s a ing
ou side egion will en e and emain inside o all subsequen ime. Ob iously,
ajec o ies s a ing inside will also emain inside o e e . This kind o beha io
would p esen as a sui able candida e o he ole o egion in he P-B heo em
–see Sec ion 2.5 –, i i we e no o he p esence o ixed poin s inside .

64 3 The Case o La ge Slope: Analy ical App oach
Conside now he ollowing pa icula si ua ion:
{
}
(3.89)
whose o que cu es a e depic ed in Fig. 3.13. We suppose ha he only ixed poin
o he sys em is on he igh b anch o cu e and unde goes a Hop bi u ca ion. I
is also assumed ha he ac ual slope o he mo o cha ac e is ic is and,
he e o e, he equilib ium is uns able.
Fi s , le us p o e ha he ixed poin is a epelle . Since he equilib ium is al eady
known o be uns able, we only need o p o e ha i is no a saddle. Le be he
jacobian ma ix o sys em (3.46), e alua ed a he equilib ium poin . Taking in o
accoun ha a saddle poin has wo eal eigen alues wi h di e en signs, we
can s a e
( )
(3.90)
Wi h some simple algeb a, i can be shown ha , o , condi ion ( )
can be w i en as . Then, i is clea ha , o a ixed poin sa is ying (3.89), we
ha e ( ) . Thus, he equilib ium is a epelle .
A new egion is now de ined as minus a ci cle o in ini esimal adius a ound
he equilib ium poin . F om he abo e conside a ions –all ajec o ies en e and
he ixed poin is a epelle –, i is clea ha he low on he bounda y o is
di ec ed inwa ds, as depic ed in Fig. 3.14.
In summa y, a closed, bounded egion o he phase plane has been ob ained,
which con ains no ixed poin s and such ha all ajec o ies o he sys em en e
and emain inside o e e . Then, all condi ions o he P-B heo em a e ul illed, and
i can be assu ed ha any ajec o y o he sys em is a ac ed owa ds a closed o bi
as , i i is no a closed o bi i sel .
3.6 Condi ions o he Sys em o be Always A ac ed by a Limi Cycle 65
Fig. 3.13 Schema ic iew o he o que cu es co esponding o condi ions (3.89)
Finally, i should be no ed ha , al hough he P-B heo em does no gua an ee ha
all ajec o ies end o he same closed o bi , all he nume ical expe imen s
conduc ed wi hin his hesis show he p esence o only one s able limi cycle,
namely ha c ea ed by he Hop bi u ca ion. This sugges s ha , o a sys em
e i ying (3.89), all he sys em dynamics is a ac ed owa ds a unique limi cycle.
-8 -6 -4 -2 0 2 4
0
0.1
0.2
0.3
0.4
0.5
T
T
d
H
d

66 3 The Case o La ge Slope: Analy ical App oach
Fig. 3.14 Flow on he bounda y o egion (dashed), unde condi ions (3.89)
3.7 Discussion
Time Validi y
A c ucial poin in any pe u ba ion analysis is he ime scale o which he ob ained
app oxima e solu ion is alid. I has been shown in Sec ion 3.3 ha he solu ion
gi en by he educed sys em is alid, a leas , o a ime scale (
⁄) –see Fig.
3.6–.
Howe e , he si ua ion is e en be e han ha . As desc ibed in Sec ion 2.1
(A e aging wi h A ac ion), he asymp o ic app oxima ions a ained h ough
a e aging a e alid o all ime, whene e hey a e a ac ed by a s able ixed poin
o a s able limi cycle. In he la e case, he uni o m alidi y holds o all a iables
excep he angula one, i.e. he a iable which measu es he low on he limi cycle.
As will be seen la e , all he nume ical solu ions ob ained in Chap e 4 ul ill he
abo e condi ion o a ac ion.
Region 𝑄
Fixed
Poin
101
.
a
x
y
3.7 Discussion 67
Compa ison wi h o he au ho s’ esul s
In his subsec ion, he p esen ed app oach and esul s a e compa ed o some
p oposed by o he au ho s.
Fi s o all, as a as he au ho s know, he e has been no a emp in he li e a u e o
use he SPT o he analysis o nonideally exci ed sys ems. Thus, he analy ical
p ocedu e add essed in his Chap e appea s o be a no el app oach o he p oblem.
On he o he hand, he possibili y o a Hop bi u ca ion on he igh b anch o he
ib a ion o que cu e (Fig. 3.9b.2) has been add essed. An impo an implica ion
o his esul is ha he s abili y o he s a iona y solu ions nea esonance does no
only depends on he compa ison be ween he slopes o he wo o que cu es
( ), as commonly s a ed in he li e a u e (Blekhman, 2000; Dimen be g e al.,
1997; Kononenko, 1969; Nay eh & Mook, 1995). Le us y o explain his
di e gence in he esul s.
Kononenko’s book (Kononenko, 1969) is one o he mos ele an e e ences in he
subjec . He conside ed se e al linea and nonlinea sys ems exci ed by nonideal
mo o s. By using he a e aging me hod, he was able o analy ically in es iga e he
s a iona y mo ions o he mo o and hei s abili y. His app oach was as ollows.
Conside ing he o o speed o be in he icini y o esonance, he expanded i as
󰇗
(3.91)
Thus, he ound equa ions o mo ion o he o m
{
󰇗 ( )
󰇗 ( )
󰇗 ( )
󰇗
}
(3.92)
74 4 The Case o La ge Slope: Nume ical Simula ions
Fig. 4.2 Phase po ai s co esponding o pa ame e s (4.1). The ixed poin s a e
ma ked wi h do s. The dashed loop ep esen s he uns able limi cycle
(a) , (b)
The dynamical mechanism whe eby he limi cycle is des oyed, which u ns ou o
be a homoclinic bi u ca ion (Kuzne so , 1998), is shown in Fig. 4.2 and Fig. 4.3.
Le us ollow he e olu ion o he phase po ai . F om Fig. 4.2 (a) o Fig. 4.2 (b),
he Hop bi u ca ion akes place: he ocus becomes s able, while an uns able limi
cycle is bo n a ound i . In Fig. 4.3(a), he cycle has swelled conside ably and passes
close o saddle poin . The homoclinic bi u ca ion occu s when he cycle ouches
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
-0.8
-0.6
-0.4
-0.2
0
0.2
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
-0.8
-0.6
-0.4
-0.2
0
0.2
x
y
x
y
(a)
(b)

4.1 Global Bi u ca ions o he Limi Cycles 75
he saddle poin ( ), becoming a homoclinic o bi . In Fig. 4.3(b), we ha e
and he loop has been des oyed.
Fig. 4.3 Phase po ai s co esponding o pa ame e s (4.1). The ixed poin s a e
ma ked wi h do s. The dashed loop ep esen s he uns able limi cycle
(a) , (b)
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
-0.8
-0.6
-0.4
-0.2
0
0.2
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
-0.8
-0.6
-0.4
-0.2
0
0.2
x
y
x
y
(a)
(b)
S
76 4 The Case o La ge Slope: Nume ical Simula ions
I is wo h no ing ha , when he uns able limi cycle exis s –namely, o
–, i ac s as a on ie be ween he domains o a ac ion o he wo s able
equilib ium poin s o he sys em –see Fig. 4.2(b) and Fig. 4.3(a)–.
Many o he cases exhibi ing a subc i ical bi u ca ion, which a e no shown he e,
ha e also been nume ically sol ed. In all o hem, he uns able limi cycle has been
ound o disappea h ough a homoclinic bi u ca ion.
The Supe c i ical Case
Conside he ollowing se o dimensionless pa ame e s:
(4.5)
which migh be associa ed o dimensional pa ame e s
{
⁄
⁄
⁄
}
(4.6)
wi h . Equa ions (3.66) and (3.86) yield he alues o slopes and ,
depic ed in Fig. 4.4.
(4.7)
C i e ion (3.87) allows cha ac e izing he bi u ca ion as supe c i ical. Then, as
ep esen ed in Fig. 3.10, i can be assu ed ha a s able limi cycle enci cles he
uns able equilib ium o , wi hin a ce ain neighbo hood o . As a ma e
o ac , he esul s o Sec ion 3.6 can be used he e o in es iga e he ange o slopes
o which he limi cycle exis s.
4.1 Global Bi u ca ions o he Limi Cycles 77
Conside he cu e which in e sec s a he ixed poin unde s udy and is
angen o cu e a ano he poin . Le s and o he slope o ha pa icula
o que cu e, as displayed in Fig. 4.4. Then, i is s aigh o wa d o show ha , o
, condi ions (3.89) a e ul illed and, consequen ly, i can be assu ed
ha all sys em ajec o ies end o a pe iodic o bi . In he case unde analysis, we
ha e
(4.8)
Fig. 4.4 To que cu es co esponding o pa ame e s (4.5)
No e ha he Poinca é-Bendixson Theo em gi es su icien , bu no necessa y,
condi ions o he exis ence o a s able pe iodic o bi . Thus, i canno be deduced
om he Theo em whe he he limi cycle su i es o no when . To he end
o answe ing his ques ion, we eso again o a nume ical esolu ion o sys em
(3.46), o inc easing alues o . The esul s a e displayed in Fig. 4.5 and Fig. 4.6.
-6 -4 -2 0 2
0
0.2
0.4
0.6
0.8
1

T
T
H
d
T
d
P
d
78 4 The Case o La ge Slope: Nume ical Simula ions
Fig. 4.5 Phase po ai s co esponding o pa ame e s (4.5). The ixed poin s a e
ma ked wi h do s. The solid loop ep esen s he s able limi cycle
( ) , (b)
Le us ack he e olu ion o he phase po ai . In Fig. 4.5(a) we ha e and
all sys em ajec o ies a e a ac ed owa ds he only ixed poin o he sys em. I
may seem om Fig. 4.5(a) ha ajec o ies a e ac ually a ac ed owa ds a limi
cycle su ounding he ixed poin . The eason o his alse imp ession is ha he
a ac ion o he ixed poin is e y weak, as i is close o becoming uns able ( is
-1 -0.5 0 0.5 1
-1
-0.5
0
0.5
1
-1 -0.5 0 0.5 1
-1
-0.5
0
0.5
1
x
y
x
y
(a)
(b)
4.1 Global Bi u ca ions o he Limi Cycles 79
close o ). Hence he equi ed ime o ajec o ies o app oach he equilib ium is
ex emely long.
Fig. 4.6 Phase po ai s co esponding o pa ame e s (4.5), o . The
ixed poin s a e ma ked wi h do s. The solid loop ep esen s he s able limi cycle
Fig. 4.5b co esponds o . The Hop bi u ca ion has occu ed and,
he e o e, he ocus has los i s s abili y a he same ime ha a s able limi cycle has
appea ed a ound i . No e ha , in Fig. 4.5(b), condi ions (3.89) hold. Consequen ly,
all sys em ajec o ies a e a ac ed owa ds a pe iodic o bi . Ac ually, Fig. 4.5b can
be obse ed as a pa icula example o he gene al pic u e shown in Fig. 3.14.
The nume ical esul s men ioned abo e a e only use ul o con i m he analy ical
de elopmen s o p e ious sec ions. By con as , Fig. 4.6 does p o ide new
in o ma ion abou he global dynamics o he sys em. I shows ha he s able limi
cycle is des oyed h ough a saddle-node homoclinic bi u ca ion (Kuzne so , 1998),
which occu s a . This means ha he cycle disappea s exac ly when
condi ions (3.89) a e no ul illed anymo e. The mechanism is as ollows. A
a new ixed poin , which immedia ely spli s in o a saddle and a node, is
c ea ed h ough a saddle-node bi u ca ion. This new equilib ium appea s p ecisely
on he limi cycle, ans o ming i in o a homoclinic o bi . Wha is ound a ,
-1 -0.5 0 0.5 1
-1
-0.5
0
0.5
1
x
y

80 4 The Case o La ge Slope: Nume ical Simula ions
as obse ed in Fig. 4.6, is ha he limi cycle has been eplaced by a couple o
he e oclinic o bi s connec ing he saddle and he node.
I has been shown ha , o he pa icula se o pa ame e s (4.5), condi ions (3.89)
a e necessa y and su icien o he exis ence o a s able limi cycle. Thus, he
pe iodic o bi ne e coexis s wi h any o he a ac o o he sys em. Ne e heless, i
should be s essed ha his is no always he case. In ac , cases ha e also been
ound whe e he s able limi cycle is des oyed h ough a homoclinic bi u ca ion,
jus like in he subc i ical case. In hese si ua ions, he global bi u ca ion occu s a
ce ain slope and, he e o e, he limi cycle coexis s wi h a s able
equilib ium o .
As an example, conside a case wi h sa is ying . Clea ly,
acco ding o (3.87), he Hop bi u ca ion is supe c i ical. Howe e , i is no possible
o he limi cycle o be des oyed h ough a saddle-node homoclinic bi u ca ion,
because he saddle and he node a e c ea ed be o e he limi cycle. In ac , in hese
cases, he closed o bi has been ound o die in he same way as he uns able limi
cycle shown in Fig. 4.3, i.e. h ough a homoclinic bi u ca ion due o he p esence o
a saddle poin .
In summa y, he simula ions ca ied ou sugges ha , while uns able limi cycles a e
des oyed by homoclinic bi u ca ions, he s able ones can disappea ei he h ough
homoclinic bi u ca ions o saddle-node homoclinic bi u ca ions.
4.2 Nume ical Valida ion o Analy ical Resul s
A Subc i ical Case
Conside again he se o pa ame e s gi en a (4.1), which gi es ise o a subc i ical
Hop bi u ca ion, as depic ed in Fig. 4.2 and Fig. 4.3. Two di e en scena ios a e
s udied, co esponding o he ollowing slopes o he mo o cha ac e is ic:
4.2 Nume ical Valida ion o Analy ical Resul s 81
(4.9)
By compa ing (4.9) wi h Fig. 4.2 and Fig. 4.3, i can be e i ied ha , o ,
he sys em has a s able ocus su ounded by an uns able limi cycle, while, a
, he ocus has become uns able h ough a Hop bi u ca ion. As poin ed ou
in Sec ion 4.1, he uns able limi cycle o is he bounda y which sepa a es
he basins o a ac ion o he wo a ac ing ixed poin s p esen in he sys em–see
Fig. 4.3(a)–.
Fo , wo se s o ini ial condi ions, I.C. (1) and I.C. (2), a e selec ed, ou side
and inside he limi cycle, espec i ely:
( ){
} ( ){
}
(4.10)
Then, by using ela ions (3.47), co esponding ini ial condi ions o he o iginal
sys em can be compu ed:
( )
{
󰇗
󰇗
}
( )
{
󰇗
󰇗
}
(4.11)
No e ha his s ep has no a unique solu ion, because di e en se s o o iginal ini ial
condi ions can p oduce he same educed ini ial condi ions.
The ob ained nume ical solu ions a e shown in Fig. 4.7, o . A good
ag eemen be ween solu ions o bo h sys ems is obse ed. Clea ly, he wo
conside ed se s o ini ial condi ions lead he sys em o di e en a ac o s.
82 4 The Case o La ge Slope: Nume ical Simula ions
Fig. 4.7 Compa ison o nume ical solu ions o he o iginal (solid line) and educed
(dashed line) sys ems o pa ame e s (4.1), and
(a) Displacemen s
(b) Ro o Speed
I is con enien o make he e an obse a ion abou he size o pa ame e . The
p ocedu e used in Chap e 3 o ans o m he o iginal sys em in o a simple educed
sys em is based on pe u ba ion me hods. These echniques a e use ul o dynamical
sys ems which con ain a small pa ame e , and hey explain how such sys ems
beha e o a su icien ly small . This means ha he smalle is, he mo e accu a e
0 0.5 1 1.5 2 2.5 3 3.5 4
x 104
-1
-0.5
0
0.5
1

u, a
0 1 2 3 4
x 104
0.998
1
1.002
1.004


I.C. (2)
I.C. (1)
I.C. (2)
I.C. (1)
(a)
(b)
4.2 Nume ical Valida ion o Analy ical Resul s 83
pe u ba ion p edic ions a e. Fig. 4.7 shows ha , o he case unde conside a ion, a
alue o gi es a ema kable acco dance be ween solu ions o he o iginal
and educed sys em. As an illus a i e example, he same nume ical compu a ion is
done, o ini ial condi ions I.C. (2) and . This la ge gi es ise o a less
accu a e p edic ion, as displayed in Fig. 4.8. The equi ed o ha e an accu a e
esul depends on he case unde s udy. Fo ins ance, in he ollowing simula ion
(Fig. 4.9), i was necessa y o ake o a good ma ching be ween solu ions
o he exac and app oxima e sys ems. Howe e , in he majo i y o simula ions
conduc ed wi hin his wo k, p o ed o be small enough.
Conside now he case whe e, acco ding o Fig. 4.2(a), he ocus is uns able
and he e is a unique a ac ing ixed poin in he sys em. Ini ial condi ions
( ){
}
(4.12)
a e selec ed o he educed sys em, om which co esponding ini ial condi ions o
he o iginal sys em can be ob ained:
( )
{
󰇗
󰇗
}
(4.13)
The o iginal and educed sys ems a e nume ically sol ed wi h and ini ial
condi ions (4.13) and (4.12), espec i ely. The esul s a e displayed in Fig. 4.9,
whe e i is clea ly obse ed how he sys em mo es away om he uns able ocus, as
he oscilla ion ampli ude inc eases, un il i is a ac ed o he s able node.
I.C. (1)
90 5 The Case o Small Slope: Analy ical App oach
o que a esonance–, and eplacing assump ion (3.9) –la ge slope o he mo o
cha ac e is ic– wi h
(5.1)
The assump ion is kep wi hin his chap e . Mo eo e , we assume ,
wi h de ined in (3.5).
Wi h hese new assump ions, he dimensionless equa ions o mo ion a e
󰇘 [ 󰇗 ( 󰇗 󰇘 )]
󰇘 [ ( 󰇗 ) 󰇘 ]
(5.2)
whe e subsc ip ‘0’ has been d opped o con enience.
I is use ul o ans o m sys em (5.2), acco ding o change o a iables
{ ( )
󰇗 ( )}
(5.3)
and de ine a new a iable o he o o speed:
󰇗
(5.4)
No ice ha he p ocedu e ollowed in Chap e 3 is being epea ed: a change o pola
coo dina es is pe o med by eplacing he pai o a iables * ( ) 󰇗( )+ wi h he
pai o ampli ude–phase a iables * ( ) ( )+. Thus, he in e media e s eps can be
skipped, since hey a e exac ly he same as in Chap e 3. The sys em, w i en in he
new a iables, akes he o m

5 The Case o Small Slope: Analy ical App oach 91
{
󰇗 ( ) ( ) ( )
󰇗 , ( ) ( )- ( )
󰇗 ( )
( ) ( )
󰇗
}
(5.5)
whe e
( ) ( )
(5.6)
Equa ions (5.5) and (5.6) a e analogous o (3.26) and (3.27).
A di ec inspec ion o sys em (5.5) e eals ha i con ains wo non-angula eal
a iables * + which a e slow – hey e ol e wi h a e ( )– and wo angula
a iables * + which a e, in p inciple, as – hey e ol e wi h a e ( ) unless
o –. Hence his is a sui able scena io o a e aging o e he as
angles. Howe e , in o de o a e age o e se e al angles, he sys em needs o be
w i en in he o m (2.5), (2.6), as explained in Sec ion 2.1. To his end, new
angula a iables a e de ined:
(5.7)
Then, by expanding he p oduc s o sines and cosines in (5.5), he sys em can be
w i en as
{
󰇗 [ ( ) ( ( ) ( ))] ( )
󰇗 0 ( ) 1 ( )
󰇗 ( )
󰇗 ( )
󰇗 ( )
}
(5.8)
92 5 The Case o Small Slope: Analy ical App oach
Now, assume a posi i e o o speed, . Then, he only esonance mani old
p esen in sys em (5.8) is gi en by condi ion
(5.9)
As explained in Sec ion 2.1, i is necessa y o dis inguish be ween wo scena ios,
depending on whe he o no he sys em is close o he esonance mani old.
5.1 Ou e Region
Suppose he o o speed is away om . Then, we can a e age sys em (5.8) o e
he h ee as angles , and . The esul ing a e aged sys em is
{ 󰇗
󰇗 ( )}
(5.10)
whe e
( ) ( )
(5.11)
Acco ding o he a e aging heo em s a ed in Sec ion 2.1, sys em (5.10) is alid on
a ime scale (
⁄), wi h ( ) p ecision.
A s aigh o wa d analysis o sys em (5.10) yields he conclusion ha i has one
only ixed poin , gi en by
{
( ) } 8
 9
(5.12)
which is globally asymp o ically s able as long as .
5.1 Ou e Region 93
No e ha , acco ding o assump ions , he equilib ium poin (5.12)
co esponds o a pos - esonan egime, . This solu ion has a e y clea
physical in e p e a ion. Fi s , no e by compa ing (5.11) o (3.3) ha unc ion ( )
is simply a dimensionless e sion o he mo o cha ac e is ic ( 󰇗):
( ) ( )
(5.13)
Clea ly,  is he only ze o o ( ), as ep esen ed in Fig. 5.1. Then, he ou e
ixed poin (5.14) co esponds o a pos - esonan mo ion whe e he oscilla ion
ampli ude is ze o and he o o speed akes he alue which makes he mo o o que
anish. No e ha his holds o he a e aged sys em (5.10), whose solu ions a e a
an ( ) dis ance o hose o he o iginal sys em (5.2). Then, ega ding he o iginal
sys em, i can be said ha he ou e ixed poin (5.14) ep esen s a pos - esonan
mo ion wi h small oscilla ion ampli udes ( ) and wi h he o o speed close o
he ze o o he mo o cha ac e is ic  ( ).
Fig. 5.1 Dimensionless mo o cha ac e is ic ( )
In physical e ms, i is consis en ha a non- esonan exci a ion p oduces a small
oscilla ion o he ib a ing sys em. No e ha , o such small oscilla ions, he o que


()
m
H
1
c
1
d
94 5 The Case o Small Slope: Analy ical App oach
on he o o due o ib a ion is e y small ( 󰇘 ( )). Then, du ing his
pos - esonan mo ion, he mo o does no ha e o p o ide any signi ican o que o
main ain he sys em ib a ion and, consequen ly, he o o speed akes such a alue
ha he d i ing o que is i ually ze o:  ( ) , ( )-
( ).
Two di e en scena ios can be conside ed:
- I ( ) , sys em (5.10) is exponen ially a ac ed owa ds equilib ium
(5.12) wi hou app oaching he esonance mani old. Then, acco ding o
Sec ion 2.1 (A e aging wi h A ac ion), he ou e a e aged sys em is alid
o all .
- I ( ) , sys em (5.10) is also exponen ially a ac ed by equilib ium
(5.12). Howe e , in i s way owa ds he equilib ium, he sys em will
necessa ily each he icini y o he esonance mani old, making sys em
(5.10) no longe alid. The e a e, in p inciple, wo op ions:
o The sys em emains close o he esonance mani old o all
subsequen ime ( esonan cap u e).
o The sys em s ays nea he esonance mani old o some ini e ime,
a e which i con inues i s e olu ion owa ds ixed poin (5.12)
(passage h ough esonance).
The nex Sec ion in es iga es he dynamics o (5.5) close o he esonance mani old.
5.2 Inne Region
In o de o s udy he sys em beha io in he icini y o he esonance mani old, he
o o speed is expanded as
√
(5.14)
5.2 Inne Region 95
No e ha he de ini ion o he de uning a iable is no he same as in he case o
la ge slope –compa e (5.14) o (3.35)–. The eason is ha , unde he assump ion o
small slope made in his chap e , he p oblem equi es a di e en pe u ba ion
app oach, which in u n equi es a di e en scaling o he o o speed. I can be
checked ha a scaling such as (3.35) would no yield any ele an esul in he
p esen case.
Replacing (5.14) in (5.5), (5.6) yields
{
󰇗 ( ) ( ) ( √ )
󰇗 √ ( )
( ) ( √ )
󰇗 √ , ( )- ( √ )
󰇗 √
}
(5.15)
wi h
( ) ( )
(5.16)
Clea ly, sys em (5.15) con ains h ee slow a iables * + and a as o a ing
phase . I is, hen, sui able o a second o de a e aging p ocedu e. Following he
p ocedu e desc ibed in Sec ion 2.2, we a i e a a e aged sys em
{
󰇗 (  )
󰇗 √  4  
 5
󰇗 √ 0  1 
󰇗 √ 
}
(5.17)
whe e, wi h an app op ia e ela ion be ween he ini ial condi ions o he o iginal
and a e aged sys ems, he e o es ima es a e

96 5 The Case o Small Slope: Analy ical App oach
{
 ( )
 ( )
 √  (  ) ( )
 (√ )
}
(
√ )
(5.18)
No e ha he (√ ) e ms in he i s wo o ela ions (5.18) u n ou o be ze o in
his pa icula case.
Despi e he ac ha he e olu ion {   } is independen o  –as is e iden , since
his is p ecisely he pu pose o a e aging–, sys em (5.17) includes  as a s a e
a iable. The eason is ha a iable ( ) is necessa y o cons uc he e o
es ima es in (5.18). Howe e , in o de o in es iga e he dynamics o he a e aged
sys em, i is con enien o ew i e i wi hou he as angle:
{
󰇗 (  )
󰇗 √  4  
 5
󰇗 √ 0  1 
}
(5.19)
A di ec analysis o (5.19) allows deducing ha , i
⁄, he e a e no ixed
poin s in he inne egion. On he o he hand, i
⁄, sys em (5.19) exhibi s wo
ixed poin s, gi en by
{ √ ( )
√ ( )
√ ( )}
(5.20)
wi h
5.2 Inne Region 97
{
√
(
)
}
(5.21)
whe e √ . The wo possible alues o co espond o he wo di e en
equilib ium poin s.
No e ha , unlike in he case o la ge slope –see (3.52)–, he analy ical exp essions
o he ixed poin s a e e y simple in he p esen scena io. Howe e , he o que-
speed plo s used in Sec ion 3.4 may also be illus a i e he e and will p o ide an
in e es ing compa ison wi h he case o la ge slope.
Thus, conside he equilib ium condi ion applied o a iable . F om he hi d o
equa ions (5.19) we ha e, a i s o de ,
(5.22)
On he o he hand, condi ion 󰇗 yields
(5.23)
which allows w i ing (5.22) as
(5.24)
Equa ion (5.24) can be clea ly in e p e ed as a o que equilib ium condi ion:
( )
(5.25)
wi h
98 5 The Case o Small Slope: Analy ical App oach
( )
(5.26)
ep esen s he d i ing o que p oduced by he mo o and co esponds o he
esis ing o que due o ib a ion. In o de o ob ain he usual o que-speed plo , we
would need o w i e and in e ms o . Ne e heless, his would in u n
equi e w i ing in e ms o , and hen subs i u e in (5.25). Since his
yields e y long and cumbe some exp essions, we eso o an al e na i e implici
p ocedu e o he g aphical ep esen a ion.
F om condi ion 󰇗 , we ha e
√
(5.27)
Then, we can w i e
( )
(5.28)
whe e unc ion ( ) is de ined as
( ) √
(5.29)
The p oposed ep esen a ion can be cons uc ed as ollows. Fi s , g aph e sus
(in his case, as , a cons an unc ion is ob ained). Then, ep esen he
pa ame ic cu e gi en by * ( ) ( )+ o and ( -. The ac ha
is s ic ly posi i e comes om i s de ini ion as he adius o a pola coo dina e
ans o ma ion –see (5.3)–, while condi ion (5.23) o bids o be g ea e han .
This p ocedu e gi es ise o a plo like ha shown in Fig. 5.2.
5.2 Inne Region 99
Fig. 5.2 Fixed poin s o sys em (5.19)
A di ec compa ison be ween Fig. 5.2 and Fig. 3.7 is qui e illus a i e as o he
di e ence be ween he wo scena ios conside ed in his hesis. In he case o la ge
(small) slope, he d i ing o que cu e exhibi s a slope which is compa able
(negligible) wi h espec o ha o he ib a ion o que cu e.
Fig. 5.2 shows he exis ence o wo ixed poin s, as long as
⁄. The s abili y
o hese equilib ia is now in es iga ed. To his end, he jacobian ma ix o sys em
(5.19) needs o be ob ained and e alua ed a he equilib ium poin o in e es :
√ ( √ )
(5.30)
wi h
[
] [
]
(5.31)
The eigen alues o ma ix a e now compu ed. A e some algeb a, we ind, o
he igh b anch o he o que cu e ( ),
-2 0 2 4 6 8 10 12
0
0.5
1
1.5
2
2.5
1z

T
T
1z
m
T
c
2

106 5 The Case o Small Slope: Analy ical App oach
whe e is a eal ma ix whose columns con ain he eal eigen ec o s o he
jacobian o (5.45), e alua ed a . In he case o complex conjuga e
eigen ec o s, he eal and imagina y pa s a e s o ed in di e en columns o .
Clea ly, change o a iables is composed o wo ans o ma ions. Fi s , he
coo dina e sys em is ansla ed so ha he o igin coincides wi h he ixed poin .
Then, a ans o ma ion o he eal eigenbasis o he jacobian is pe o med, by means
o ma ix .
Vec o con ains he s a e a iables o he sys em, exp essed wi h espec o he
basis o med by he eigen ec o s o he jacobian. Then, i is clea ha hese
eigen ec o s a e necessa ily o hogonal in he space o coo dina es .
Consequen ly, o wo solu ions s a ing in he Poinca é-Lyapuno domain, we ha e
‖ ( ) ( )‖ ‖ ( ) ( )‖
(5.53)
By conside ing a ime inc emen
⁄ in (5.53), we ha e
‖ ‖ ‖ ( ) ( )‖
(5.54)
whe e
( )
(5.55)
Thus, i has been shown ha ( ) exhibi s exponen ial con ac ion on he ime scale
⁄, e en hough his con ac ion is weak.
Now, a iable ( ) –solu ion o he o iginal sys em (5.35)– can also be ans o med
acco ding o (5.52):
(5.56)

5.2 Inne Region 107
Conside he ollowing pa i ion o ime in in e als o (
⁄):
[
] [
] [
] ( )
(5.57)
whe e cons an s a e chosen such ha
4 (
) (
)5
(5.58)
No e ha his choice o cons an s is always possible, because anishes a leas
once pe pe iod, acco ding o (5.44).
We de ine
(
) ( ) ( ( ) )
(5.59)
(
) ( ) ( ( ) )
(5.60)
( ) (
) (
)
(5.61)
Thus, ( ) ep esen s he alue o a he end o an in e al when, as an ini ial
condi ion, is imposed o be equal o a he beginning o he in e al.
Fi s , we ha e ha
‖ ( )‖
(5.62)
as is clea om (5.37),(5.49) and (5.56), using ha a he conside ed
ins an s.
108 5 The Case o Small Slope: Analy ical App oach
On he o he hand, by i ue o ela ion (5.54), we can w i e
‖ ( )‖ ‖ ‖
(5.63)
Combining (5.62) and (5.63), we ha e
‖ ‖ ‖ ‖
(5.64)
By using (5.64) ecu si ely, we a i e a
‖ ‖ ( ) ‖ ‖
(5.65)
No e ha , acco ding o (5.37), (5.49) and (5.56), we can w i e
‖ ‖
(5.66)
hanks o he ac ha ( (
⁄) (
⁄)) .
Finally, in oducing (5.66) in o (5.65) and aking he limi o yields
‖ ‖
(5.67)
whe e (5.55) has been used.
Al hough (5.67) only holds, in p inciple, o he pa icula ins an s
⁄, i can be
eadily gene alized o any . No e ha , as s a ed in (5.44), any is a ( )–
dis ance om an ins an whe e . Clea ly, could be aken as
⁄ and,
he e o e, (5.67) holds a . On he o he hand, and can only unde go ( )
a ia ions in an ( ) ime inc emen , which jus i ies he gene aliza ion o (5.67) o
any . Then, o , we can w i e
5.2 Inne Region 109
‖ ( ) ( )‖
(5.68)
Reco e ing he o iginal a iables, we ha e
‖ ( ) ( )‖ ‖ ‖‖( ( ) ( ))‖ , )
(5.69)
Finally, in oducing (5.68) in o (5.69) yields
‖ ( ) ( )‖ , )
(5.70)
whe e
‖ ‖
(5.71)
The conclusion is ha , o ini ial condi ions close enough o he conside ed
equilib ium, he solu ion o he a e aged sys em is a an ( ) dis ance om he
solu ion o he o iginal sys em, o all . Then, i he equilib ium is
asymp o ically s able in he a e aged sys em, i is asymp o ically s able as well o
he o iginal sys em.
Now, he ob ained esul is pa icula ized o he case o he mo o wi h small slope
cha ac e is ic. Equa ion (5.70) akes he o m
{  (√ )
 (√ )
 (√ )} , )
(5.72)
110 5 The Case o Small Slope: Analy ical App oach
o solu ions s a ing close enough o he ixed poin (5.20), (5.21), wi h .
By compa ing (5.70) wi h (5.18), i is clea ha he ime alidi y o he
app oxima ion has been ex ended, paying he p ice o a less accu a e solu ion.
Final Rema ks
In summa y, he sys em has been ound o exhibi wo equilib ium poin s in he
esonance egion as long as
⁄. Fig. 5.2 ep esen s bo h equilib ia on a
o que-speed plo , whe e he ixed poin on he igh b anch is uns able and he one
on he le b anch is s able. No e ha he exis ence o a s able ixed poin in he
inne egion jus i ies he possibili y o ‘ esonance cap u e’.
Recall ha he sys em eaches he esonance mani old whene e ( ) . Fo
some se s o ini ial condi ions, he ajec o y will en e he Poinca é-Lyapuno
domain o he s able ixed poin and, he e o e, i will emain nea esonance o all
subsequen ime – esonan cap u e–. Clea ly, he e may also be se s o ini ial
condi ions such ha he ajec o y does no each he Poinca é-Lyapuno domain o
he s able ixed poin . In hese cases, he sys em will p obably lea e he inne egion
and e ol e owa ds ixed poin (5.12) in he ou e egion –passing h ough
esonance–.
In p inciple, i would also be possible ha he sys em was a ac ed by a di e en
objec in he inne egion, such as a s able limi cycle o a chao ic a ac o . This
would ep esen ano he kind o esonance cap u e, no due o he p esence o he
s able ixed poin analysed in his sec ion. Howe e , he nume ical simula ions
ca ied ou ha e no e ealed he exis ence in he inne egion o any a ac o o he
han he analysed ixed poin .
No e also ha his chap e has coped wi h he inne and ou e app oxima ions
sepa a ely. We ha e no ied o cons uc a ‘composi e expansion’ by ma ching he
inne and ou e solu ions, which is a a he in ica e and complex subjec , ea ed,
o example, in (W. Eckhaus, 1979; Sande s e al., 2007).
5.2 Inne Region 111
Be o e showing nume ical esul s o con i m he analy ical de elopmen s o his
Chap e , i is con enien o commen some o he wo ks on he subjec .
Sande s, Ve huls and Mu dock conside ed he sys em s udied in his Sec ion as an
illus a i e example in Chap e s 7 and 8 o hei book (Sande s e al., 2007).
Rega ding he ou e egion o he phase space, hey conduc ed he same analysis as
in his Chap e , a e aging o e he h ee as angles in (5.8) and ob aining
equilib ium (5.12). Howe e , in he inne egion hey only ca ied ou a i s o de
a e aging in con as o he second o de a e aging add essed in his Chap e . This
p ocedu e did no allow hem o analyse he s abili y o he ixed poin s nea
esonance, since a i s o de a e aging is no accu a e enough o his pu pose.
In addi ion, Alexande Fidlin de o ed Chap e 5 o his book (Fidlin, 2006) o he
s udy o nonideal exci a ions, aking sys em (5.2) as a ele an example. He ocused
only on he esonance egion, a i ing a a sys em analogous o (5.19) a e a second
o de a e aging. Howe e , he e a e wo main di e ences be ween his esul s and
hose p esen ed in he p esen Chap e :
- Acco ding o he analysis p oposed in his hesis, he equilib ium poin o
is s able as long as . Howe e , Fidlin came o he conclusion
ha he condi ion o s abili y is . The eason o his di e ence is
a small e a um in he eigen alues compu a ion in (Fidlin, 2006), namely in
he s ep om equa ion (5.21) o (5.22) o he men ioned e e ence: whe e i
eads , i should ead .
- Fidlin add essed he sho ime scale whe e he inne a e aged sys em is
alid, ( √
⁄), as an impo an limi a ion o he analysis. He
p oposed a hie a chic a e aging p ocedu e as a way o enla ge he ime o
alidi y o he app oxima ion (Pechene , 1992). Howe e , his me hod ails
p ecisely in he icini y o he equilib ium poin o in e es , because he
equi ed a iable ans o ma ion becomes singula a ha poin . The e o e,
he hie a chic a e aging scheme canno be used o jus i y he asymp o ic
s abili y o he ixed poin .

112 5 The Case o Small Slope: Analy ical App oach
In conclusion, he chie con ibu ion o his Chap e wi h espec o p e ious
published wo ks is he igo ous jus i ica ion o he asymp o ic s abili y o one o he
s a iona y mo ions o he sys em nea esonance, which in u n gi es a solid
explana ion o he possibili y o esonan cap u e, o ‘locking in o esonance’.
6 THE CASE OF SMALL
SLOPE OF THE MOTOR
CHARACTERISTIC:
NUMERICAL
SIMULATIONS
This Chap e is in ended o e i y he esul s o Chap e 5 by means o nume ical
simula ion. Following an analogous scheme o ha in Chap e 4, pa icula alues
a e assigned o he sys em pa ame e s and bo h he o iginal and app oxima e
sys ems a e nume ically sol ed in o de o compa e he ob ained solu ions.
Thus, conside he ollowing pa ame e s
114 6 The Case o Small Slope: Nume ical Simula ions
(6.1)
which migh be associa ed o dimensional pa ame e s
{
⁄
⁄
⁄
}
(6.2)
wi h . This se o pa ame e s gi es ise o he o que-speed cu es
depic ed in Fig. 6.1. No e ha condi ion
⁄ is ul illed, which implies ha
he e exis wo ixed poin s in he inne egion o he phase space, co esponding o
he wo in e sec ions be ween and in Fig. 6.1.
Fig. 6.1 To que-speed cu es co esponding o pa ame e s (6.1).
S and U label he s able and uns able ixed poin s, espec i ely.
-6 -4 -2 0 2 4 6 8
0.5
1
1.5
2

T
m
T
T
S
U
6 The Case o Small Slope: Nume ical Simula ions 115
As discussed in Chap e 5, he equilib ium on he le b anch o cu e is s able,
while he one on he igh b anch is uns able. The ixed poin s can be eadily
compu ed by in oducing (6.1) in o (5.21):
{
}
(6.3)
{
}
(6.4)
The hi d equilib ium, in he ou e egion o he phase space, can be ob ained by
in oducing (6.1) in o (5.12):
2
3
(6.5)
The simula ions ha e been ca ied ou as ollows. A se o ini ial condi ions o he
o iginal sys em (5.2) is chosen wi h ( ) , i.e. in he p e- esonan egion o he
phase space. Then, he o iginal sys em o equa ions is nume ically sol ed o a ime
in e al [ ] which is long enough o asce ain whe he he sys em is cap u ed o
passes h ough esonance.
Suppose he sys em passes h ough esonance. Looking a he nume ical solu ion o
he o iginal equa ions, wo pa icula ins an s, and a e de ined, a which he
sys em en e s and lea es he esonance egion, espec i ely. Al hough he choice o
hese wo alues is somewha a bi a y, hey gi e an app oxima ion o he limi s
be ween he inne and ou e solu ions. Then, he ou e app oxima e sys em (5.10) is
sol ed o , - and [ ], wi h he ini ial condi ions ob ained as he
solu ion o he o iginal sys em e alua ed a and , espec i ely. The
inne app oxima e sys em (5.17) is sol ed o , -, wi h he ini ial condi ions
co esponding o he solu ion o he o iginal equa ions pa icula ized a .
Finally, he solu ions o he o iginal, ou e and inne sys ems a e ep esen ed
122 6 The Case o Small Slope: Nume ical Simula ions
app oxima e equa ions. Once he sys em has o e come he esonance egion, i
e ol es owa ds he ou e s able equilib ium gi en by (6.5).
I is also illus a i e o conside a di e en si ua ion. Suppose pa ame e is
inc eased un il he e a e no ixed poin s in he a e aged sys em nea esonance. The
condi ion o mee is
⁄ . Then, conside he ollowing se o pa ame e
alues:
(6.8)
which is exac ly he same as (6.1) excep o a la ge d i ing o que a esonance.
The o que-speed g aph o his scena io, ob ained h ough ela ions (5.26) and
(5.29), is depic ed in Fig. 6.6, exhibi ing no in e sec ions be ween he cu es.
Fig. 6.6 To que-speed cu es co esponding o pa ame e s (6.8)
Clea ly, esonance cap u e canno occu in his si ua ion, unless an a ac o o he
han a ixed poin exis ed in he inne egion. As s a ed be o e, no nume ical
e idence o such an a ac o has been ound. The conclusion is ha he sys em will
pass h ough esonance o any p e- esonan ini ial condi ion and will lead owa ds
he ou e s able equilib ium, which is now gi en by
-6 -4 -2 0 2 4 6 8
0
0.5
1
1.5
2

T
m
T
T

6 The Case o Small Slope: Nume ical Simula ions 123
2
3
(6.9)
as can be ob ained by in oducing (6.8) in o (5.12):
Despi e he esonance being no ac i e –i.e. he e a e no a ac o s in he esonance
egion–, i can be expec ed ha ajec o ies a e somehow dis o ed when passing
h ough he esonance mani old. To he end o obse ing his e ec , wo di e en
simula ions ha e been conduc ed wi h di e en ini ial condi ions:
{
󰇗
󰇗
}
(6.10)
{
󰇗
󰇗
}
(6.11)
The esul s a e displayed in Fig. 6.7-Fig. 6.9. No e ha , o ini ial condi ions (6.10),
he e olu ion o he o o speed is nea ly una ec ed by esonance, while he e is a
signi ican e ec on he ib a ion ampli ude. I is in e es ing ha exac ly he
opposi e case is encoun e ed o ini ial condi ions (6.11): whe eas he s uc u e
ib a ion is almos unal e ed by esonance, he o o speed unde goes signi ican
oscilla ions when he sys em passes h ough he esonance mani old. Thus, i is
clea ha he in luence o esonance on he sys em beha iou depends on he ini ial
condi ions. In gene al, we can s a e ha some ansien esonan e ec s can be
expec ed in he sys em, e en when he e a e no a ac o s in he esonance egion.
124 6 The Case o Small Slope: Nume ical Simula ions
Fig. 6.7 Nume ical solu ions o pa ame e s (6.1), ini ial condi ions (6.10) and
. Solid, dashed and do ed lines co espond o he o iginal, inne and ou e
sys ems, espec i ely
a) Displacemen
b) Ro o speed
0500 1000 1500 2000 2500
-0.1
-0.05
0
0.05
0.1

u, a
0500 1000 1500 2000 2500
0
1
2
3


(a)
(b)
1

2

1

2

6 The Case o Small Slope: Nume ical Simula ions 125
Fig. 6.8 Nume ical solu ions o pa ame e s (6.1), ini ial condi ions (6.11) and
. Solid, dashed and do ed lines co espond o he o iginal, inne and ou e
sys ems, espec i ely
a) Displacemen
b) Ro o speed
0500 1000 1500 2000 2500
-2
0
2

u, a
0500 1000 1500 2000 2500
0
1
2
3


1

2

1

2

(a)
(b)
126 6 The Case o Small Slope: Nume ical Simula ions
Fig. 6.9 Close-up a ound esonance o nume ical solu ions o pa ame e s (6.1),
ini ial condi ions (6.11) and . Solid, dashed and do ed lines co espond o
he o iginal, inne and ou e sys ems, espec i ely
a) Displacemen
b) Ro o speed
150 250 350 450
0.5
1
1.5


150 250 350 450
-3
-2
-1
0
1
2
3

u, a
1

2

1

2

(a)
(b)
7 TORQUE-SPEED CURVES
FOR THE WHOLE
FREQUENCY RANGE
This Chap e se es as a connec o be ween he analyses p esen ed in Chap e s 3-6
and he s udy o he ib ocompac ion p ocess expounded in Chap e 8. Recall ha
o que-speed cu es ha e al eady been success ully used o ob ain he s a iona y
mo ions o he ib a ing unbalanced mo o in Chap e s 3-6. Howe e , in hese
p e ious app oaches, he o que-speed plo is only ep esen ed o he esonance
egion, like in Fig. 3.7 and Fig. 5.2, o o he non- esonan egion, like in Fig. 5.1.
This necessa y dis inc ion be ween esonan and non- esonan egions o he phase

128 7 To que-Speed Cu es o he Whole F equency Range
space is a di ec consequence o he pe u ba ion app oaches ha ha e been u ilized
in p e ious chap e s.
The objec i e is now o gene alize he use o hese cu es, so ha he ib a ion
o que and he mo o o que can be plo ed oge he in a single g aph o he whole
equency ange, he eby ep esen ing he esonan and non- esonan s a iona y
mo ions o he mo o . This will u n ou o be e y use ul in he nex chap e , as will
be seen, and will also p o ide a clea global pe spec i e o he p oblem s udied in
Chap e s 3-6.
7.1 Compu a ion o he To que-Speed Cu es
Conside again he mechanical sys em shown in Fig. 3.1, whose equa ions o
mo ion (3.1) a e ew i en below.
󰇘 󰇗 ( 󰇗 󰇘 )
󰇘 ( 󰇗) 󰇘
(7.1)
No e ha he cubic nonlinea i y is now assumed o be ze o o simplici y. As usual,
he mo o cha ac e is ic is assumed o be a linea unc ion o he o o speed:
( 󰇗) 󰇗
(7.2)
wi h .
We no e ha he analysis shown in wha ollows is based on Blekhman’s app oach
o di ec sepa a ion o mo ions (Blekhman, 2000). In o de o app oxima ely ob ain
he s a iona y mo ions o he sys em, i is easonable o look o solu ions whe e he
o o speed has he o m
7.1 Compu a ion o he To que-Speed Cu es 129
󰇗( ) ( )
(7.3)
wi h cons an and ( ) a pe iodic unc ion o ime wi h ze o a e age. I is also
assumed ha he solu ion sa is ies
{ ( )
󰇗 ( ) }
(7.4)
Condi ions (7.4) will be e i ied a e wa ds. In oducing (7.3) in o he i s o
equa ions (7.1) yields
󰇘 󰇗 [( ) 󰇗 ]
(7.5)
By aking (7.4) in o accoun , equa ion (7.5) can be app oxima ed as
󰇘 󰇗 ( )
(7.6)
whe e ( ) has been assumed o simplici y. No e ha , o i s app oxima ion,
he small oscilla ion o he o o speed ( ) does no a ec he sys em ib a ion.
I may seem om (7.6) ha he p oblem has been ende ed linea wi h he p oposed
app oxima ion. In ac , equa ion (7.6) ep esen s a ha monically o ced linea
oscilla o . Howe e , he sys em as a whole is s ill nonlinea , due o he nonideal
in e ac ion wi h he exci e . This can be seen by no icing ha cons an in (7.6) is
no known a p io i. Hence he linea mo ion ( ) needs o be sol ed as a unc ion o
. Then, he o que p oduced by his ib a ion will be in oduced in he o o
equilib ium equa ion –second o equa ions (7.1)–, which will allow ob aining .
The e o e, he e is s ill a wo-way coupling be ween ib a ion and o a ion.
The s a iona y solu ion o (7.6) is e y well-known om linea ib a ion heo y:
130 7 To que-Speed Cu es o he Whole F equency Range
( ) ( )
(7.7)
wi h
.
/
√6.
/ 7 0
1
(
.
/
)
(7.8)
whe e √
⁄, ( )⁄ . The ib a ion ampli ude is ep esen ed
agains he a e age o o speed in Fig. 7.1, acco ding o (7.8).
Fig. 7.1 Ampli ude o he s a iona y ib a ion e sus a e aged o o speed,
co esponding o equa ion (7.8)
Once he linea mo ion has been ob ained, i can be in oduced in he o o
equilib ium equa ion in o de o compu e he s a iona y o o speed. Fi s , he
p oposed solu ion o he o o speed (7.3) is eplaced in he second o equa ions
(7.1):
0
xmax
n

7.1 Compu a ion o he To que-Speed Cu es 131
󰇗 ( ) 󰇘 ( )
(7.9)
whe e assump ion (7.4) has been used. Then, in oducing solu ion (7.7) in o (7.9)
yields
󰇗 ( ) ( ) ( )
(7.10)
I is con enien o ew i e he las e m in (7.10) as he sum o i s mean alue and an
oscilla ing componen :
󰇗 ( )
( )
(7.11)
No e ha (7.11) con ains cons an and oscilla ing e ms wi h ze o a e age. Clea ly,
i equa ion (7.11) is a e aged, only he cons an e ms emain:
( )
(7.12)
Subs ac ing (7.12) o (7.11) yields
󰇗 ( )
(7.13)
Equa ion (7.12) can be in e p e ed as an equilib ium condi ions be ween he a e age
o ques ac ing on he o o du ing he s a iona y mo ion. Ac ually, by inse ing (7.8)
in o (7.12), he ollowing ela ion is ob ained:
( ) ( )
(7.14)
138 7 To que-Speed Cu es o he Whole F equency Range
Fig. 7.4 To que-speed cu es co esponding o a case o small slope o he mo o
cha ac e is ic
(a) Resonan cap u e can occu
(b) Resonan cap u e does no occu
To que
To que
m
L
L
To que
n



n

m
L
L
(a)
(b)

7. 2 A Global Pe spec i e o he Cases o La ge and Small Slope 139
The nea - esonan s a iona y mo ions in Fig. 7.4(a) co espond o he ixed poin s
shown in Fig. 5.2. As was widely discussed in Sec ion 5.2, he i s o hese wo
ixed poin s is asymp o ically s able, whe eas he second one is uns able. The hi d
s a iona y mo ion ep esen ed in Fig. 7.4(a), which is ou side he esonance egion,
co esponds o he ixed poin o he ou e a e aged sys em, depic ed in Fig. 5.1.
This solu ion was shown o be s able in Sec ion 5.1.
Then, o he case o small slope –assuming he mo o o que a esonance o be
smalle han he esonance peak o he ib a ion o que cu e–, wo s able s a iona y
beha iou s exis , one o hem in he esonance egion, and he o he being a away
om esonance. Fo any p e- esonan ini ial s a e, he sys em can be a ac ed by
ei he he nea - esonan o he pos - esonan s able s a iona y mo ions. These wo
scena ios a e e e ed o as esonan cap u e and passage h ough esonance,
espec i ely. In he simple case ep esen ed in Fig. 7.4(b), whe e no s a iona y
mo ions close o esonance exis , he sys em always passes h ough esonance, and
e ol es owa ds i s only a ac o , away om he esonance egion.
Hope ully, i has been shown ha mos o he conclusions abou he sys em
beha iou ob ained in p e ious chap e s can be summed up and easily e ained by
using he o que-speed cu es desc ibed in his chap e . Howe e , he igo ous
pe u ba ion app oaches o Chap e s 3 and 5 a e necessa y o assess he s abili y o
he s a iona y mo ions.
8 MODELLING AND
SIMULATION OF THE
VIBROCOMPACTION
PROCESS
This Chap e ocuses on he ib ocompac ion p ocess which has mo i a ed he
whole hesis. A e desc ibing he eal indus ial p ocedu e, a 4-DOF nume ical
model o he ib ocompac ion sys em is p esen ed. Al hough his model is sui able
o nume ical in es iga ion o he p ocess, i is s ill oo complex o an analy ical
ea men which may e eal mo e gene al in o ma ion abou he sys em dynamics.
Then, a second model wi h 2 DOFs is de i ed, h ough some easonable
simpli ica ions, which u ns ou o be e y use ul in o de o analyse he p ocess and
e en une he pa ame e s o he compac ing machine. Finally, nume ical
simula ions on he i s model ( ull model) and compa ison wi h he p edic ions o

142 8 Modelling and Simula ion o he Vib ocompac ion P ocess
he second (simpli ied model) illus a e hei abili y o p edic he e ec o di e en
pa ame e s on he inal le el o compac ion achie ed.
8.1 Some No es on he Real P ocess
Qua z agglome a es, made o g anula ed qua z mixed wi h a polyes e esin, a e
widely used as an a i icial s one o coun e ops in ki chens o ba h ooms. The
manu ac u ing p ocess o a slab o his ma e ial s a s wi h he illing o a mould
wi h he mix u e o qua z and esin. Once he mould is ull, a con eyo bel ca ies
i o he ib ocompac ion zone, whe e he hickness o he slab is educed o nea ly
hal o i s ini ial alue, by elimina ing he ai ou o he ma e ial. Then, he mix u e
is cu ed in a kiln, du ing a speci ied ime in e al, a a sui able empe a u e o he
polyme iza ion o he esin. A e he esin is polyme ized, an ai s eam is used o
cool he slab be o e i en e s he mechanical inishing s age. Du ing his p ocess he
edges a e cu , p oducing a slab o p esc ibed dimensions, and he su aces a e
polished. Then, he p oduc is eady o he quali y con ol s age.
I is wo h gi ing some mo e insigh in o he ib ocompac ion s age o he p ocess,
which is he one o in e es o he pu pose o his s udy. Be o e he mix u e has
been compac ed, i is composed o h ee di e en phases: solid ( he qua z g ains),
liquid ( he esin) and gas (ai ). The ai is p esen in he ma e ial in wo di e en
ways: as bubbles wi hin he esin o as gaps be ween g ains o qua z ha he esin
has no been able o ill. The aim o he compac ion p ocess is o elimina e he ai
ou o he mix u e, since he p esence o po es a he su ace o he inal coun e op
is clea ly de imen al om a p ac ical poin o iew: he po es end o accumula e
di and a e a he di icul o clean.
The compac ion is conduc ed by means o se e al unbalanced elec ic mo o s,
moun ed on a pis on wi h he dimensions o he slab su ace. A he beginning o
he ib ocompac ion p ocess, he pis on descends on o he mix u e and exe s a
s a ic p essu e, due o i s weigh and o an ai p essu e applied on i . Then, he ai
8.1 Some No es on he Real P ocess 143
p essu e inside he mould is educed by using a acuum sys em, a e which he
mo o s a e swi ched on. The ib a ion p oduced by he unbalanced mo o s is he
main esponsible o he compac ion. Du ing he mo ion o he sys em, he e can be
sepa a ions and impac s be ween he pis on and he slab, which a e gene ally
bene icial o he compac ion, as hey p oduce e y high peaks o comp ession
o ces. In o de o educe ib a ions in he icini y o he compac ion machine,
elas ic elemen s a e placed be ween he ounda ion o he machine and he g ound,
ac ing as a ib a ion abso be and hus p o ec ing nea by equipmen . Fig. 8.1 shows
a pilo plan used o es ing pu poses, which p ese es he main ea u es o he
ac ual indus ial machine. I is in e es ing o no e ha he e a e wo mo o s moun ed
on he pis on, which o a e in opposi e di ec ions in o de o cancel he ho izon al
componen s o he cen i ugal o ces on he unbalanced masses. Hence he ne
e ec o he o a ion o bo h mo o s is an oscilla ing e ical o ce.
Fig. 8.1 Pilo plan o he analysis o he ib ocompac ion p ocess
144 8 Modelling and Simula ion o he Vib ocompac ion P ocess
F om he abo e commen s, i is clea ha he ib ocompac ion p ocess is ex emely
complex om a physical poin o iew. A la ge numbe o ac o s –some o hem
being in insically nonlinea – in luence he inal esul o he compac ion:
- The qua z g anulome y, he heological p ope ies o he esin and he
mass a io be ween qua z and esin a ec he mechanical beha iou o he
compac ing mix u e. This beha iou is necessa ily nonlinea , since he
mix u e su e s i e e sible de o ma ion du ing compac ion. Mo eo e , an
accu a e desc ip ion o his cons i u i e law would equi e modelling he
mo ion o he bubbles h ough he mix u e, he ic ion be ween qua z
pa icles, he in e ac ion be ween qua z and esin, e c. Some in es iga ions
abou he beha iou hese ypes o h ee-phase mix u es can be ound in
(Alonso, Gens, & Josa, 1990; Pie uszczak & Pande, 1996; S ickel &
Powell, 2005).
- The dynamic p ope ies o he di e en elemen s o he machine – he
pis on, he con eyo bel suppo ing he mould, he elas ome be ween he
ounda ion and he g ound, e c. – may in luence he ib ocompac ion as
well.
- The speed o he mo o s, hei a ailable powe and he amoun o unbalance
a e key pa ame e s o he p ocess.
- The inal esul o he compac ion may also depend on he du a ion o he
p ocess.
- The spa ial dis ibu ion o he acuum channels in luences he ex ac ion o
he ai ou o he mix u e, he eby a ec ing he compac ion.
8.2 Full Model
Building a eliable model o such a complex manu ac u ing p ocess, able o
accu a ely p edic he esul o he compac ion depending on he sys em pa ame e s,
is an ex emely ha d ask, which clea ly exceeds he scope o his hesis. I should
be no ed ha , as a as he au ho know, such a model is no a ailable ye .
8.2 Full Model 145
The aim o his Sec ion is o p esen an app oxima e model which, wi hou
in ending o gi e accu a e quan i a i e p edic ions, p o ides use ul quali a i e
esul s ega ding he ib ocompac ion p ocess. This may be seen as a i s s ep
owa ds he ambi ious goal o achie ing a mo e complex model which eliably
cap u es he dynamics o he eal sys em. No e ha he name ull model is used he e
only o dis inc ion om he simpli ied model p esen ed in he nex sec ion.
The simpli ica ion ca ied ou can be obse ed in Fig. 8.2 and Fig. 8.3. The o me
shows a schema ic pic u e o he eal machine, while he la e displays he
app oxima e 4-DOF model.
The qua z- esin mix u e is ep esen ed in he model by a couple o masses a ached
o each o he by a linea dampe and a nonlinea sp ing, which models he
compac ion i sel by allowing o pe manen de o ma ion when he sp ing is
comp essed. Then, he dis ance be ween bo h masses would ep esen he hickness
o he compac ing mix u e. The mould is modelled as a igid base, while he pis on
wi h he unbalanced mo o s is ep esen ed by a mass wi h a single unbalanced
mo o . The mix u e is in con ac –wi h sepa a ions and impac s allowed– wi h he
mould a he bo om and wi h he pis on a he op. The acuum sys em is no
included in he model.
I should be no ed ha he model assumes he ho izon al mo ion o he pis on o be
comple ely es ained, which makes unnecessa y o include a couple o mo o s
o a ing in opposi e di ec ions.
As ep esen ed in Fig. 8.3, he model has 4 DOFs: , , and , which
co espond, espec i ely, o posi ion o he bo om o he mix u e, posi ion o he
op o he mix u e, posi ion o he pis on and o a ion o he mo o .
The pa ame e s ep esen ed in Fig. 8.3 a e as ollows: s ands o he mass o
he mix u e, is he unbalanced mass, is he mass o he pis on and he mo o ,
is he eccen ici y o he unbalance, is he o o ine ia, is he damping