Resonant motions in a substantially non-linear system with one degree of freedom in the critical case

Resonant motions in a substantially non-linear system with one degree of freedom in the critical case

RESONANT MOTIONS IN A SUBSTANTIALLY NON-LINEAR SYSTEM WITH ONE DEGREE OF FREEDOM IN THE CRITICAL CASE* L. D. AKULENKO Moscow (Received 1. The Con...

422KB Sizes 0 Downloads 19 Views

RESONANT MOTIONS IN A SUBSTANTIALLY NON-LINEAR SYSTEM WITH ONE DEGREE OF FREEDOM IN THE CRITICAL CASE* L. D.

AKULENKO Moscow

(Received

1.

The

Consider

problem.

solutions

of

the

set

of

the

1966)

November

29

stationary

periodic

or rotatory

resonant

equations

dE =‘Ef(t,

E, 4); e),

at

;

-

(1)

o(E)+ eF(t, E, +; e),

t 5 (-co, 00) Is the independent real where E > 6 is a small parameter, variable, E is the perturbed “energy”, v the perturbed phase, and f,w and F are smooth functions of their arguments, S- and 2a-periodic with The chief method of invest igatlng these respect to t and 01 respectively. solutions

is

by the

so-called

equation

of

phase

balance

[1 - 51

T Pt(r)=

‘2)

1 f(r, EO*, $0; 0)dt = 0, 0

where

Ea* is

the

real

root

of

the

equation

V

_=;

(3)

(v=2?),

o(E)

in which

T = mS,

and m and n are

(n/m)V(t

-

T.

*

Zh.

to)

uychisl.

+

Mat.

mat.

Fit.

7,

relatively

6,

221

prime

1379 - 1385,

Integers;

1967.

\vc =

222

L.D.

It was shown in [21 that the resonant solution of (1) exists a sense, and has the form

Akulenko

stationary (for for E sufficiently

all

t E small,

[to,

CO)) m/n-

Is unique

in

E = EC,*+ eu(t, e), (I; =

(IL / m)v(t

-

to) + T* + ev(t,

(4)

e),

where u and v are functions smooth with respect to t and E aud periodic in t, provided T* Is the real root of (2) and we have o’(Eo’)aP,/&* +o. The solution vided

(4)

is

asymptotically

Lyapunov-stable

and is unstable if one or both these assertions can be made for t L to.

inequalities

for

t ryto,

are reversed.

pro-

Similar

A very common practical case Is when PlCr)= 0, i.e. the phase balance equation Is satisfied independently of -f. We say in this case that motions of higher degrees (above the first) exist. The oscillations of the first. second and third degrees were examined in [41 for the close t 0 conservative system z+F(s) The possibility of such out in [51. The rotatory lar to (5) were studied The present degree

for

the

note

E==E0”+&i(t)

oscillations solutions in [Sl.

obtains

the

more general

2. The solution. of the first degree,

we seek +...,

e)+

(5)

for more general systems was pointed simiof higher degree of an equation

stationary

system

As in the

+e2&(t)

= ef(t,s;%

(1)

resonant

and examines

solutions their

ordinary case of rotations the solution as the series 1P =

(n/m)v(t--to)

of the second

stability. or oscillations

+T+E+)i(t)

+...,

(6)

of course, that the right -hand sides are analytic in the assuming, neighbourhood of E = EO*, li, = $0, e = 0, Substituting (6) In (1) and equatinfinite ing coefficients of like powers of E, we obtain the following set of equations for the unknown periodic functions Ei, vi Ci& 2):

Resonant

motions

in

a substantially

non-linear

223

system

In the case of motions of the first degree, all the coefficients can be found from this set independently of the form of the functions fi_1, of the second degree, we have to know the form of the Fi-1. For motions terms containing gi_2 and vi-gIn particular, the unknown phase constant T of the zero approximation of y is given by the condition for E2 to be periodic, i.e. by

(7)

where

Al(t)

is

a known function

iT

Ai=--

T

tained

from the

expressions

E,

=

&(r)+

for

El

1fodh

s 0

dt

t s

0

to

and ~1

(fo = tl.=o, E=E,*,+%)>

to t W1=B,(t)i-oi’d,(~)(t-t~)+~o’S

t1

dti

to

(1

fodfz+Fo)

=

B,(z)+

~(4 z),

to

in which B1 is a constant of integration, and ?I( t, T) is a T-periodic function. Hence, if -r* is the real root of (‘I), ye and EI will be completely determined. To find Eg and ~1, we use the periodicits conditions for y2 and- Eg. The first condition gives a connection between the as yet unknown constants of integration Bl and AS, namely,

(8) Substituting that

dkP1 / a+

(8) =

into 0 ik =

the 0,1,2,.

periodicity . .), we get

condition

for

Es,

and recalling

L.D.

294

Akulenko

where

It is relations

easily seen that the next coefficients of the form (6) and (9):

The following simgle real root

Ai+l are given

by

conclusion can be drawn from the above. If T* is a of (‘I), a solution of the required form (4) can be found

In the form of series parameter e, provided a simple real root of represent the required degree, unique in the periodic coefficients their index, the solution

Bi,

(6) in increasing integral powers of the small of course that o’(Eo*) # 6, i.e. that Eg. is also (3). If these series are uniformly convergent, they stationary m/n-resonant solution of the second region where f, o and F are analytic. The bounded Ei, vii (i 22 1) can be found, no matter how high

by the method described, in the explicit is, up to e2 for E and E for ly:

form.

In particular,

Resonant

motions

in

I= + Fo -;

a substantially

non-

225

system

linear

t

1 dt

sfo dt, - $

0

to

Our method can be extended to the nonanalytic case when f and w have second part ial derivatives in the neighbourhood of g = go*, v, = ~0, derivative. As before, we only require E = 0, and F has only the first continuity with respect to t. To summarize: Theorem

1

If 1) PI(T)

= 0;

31 equations

(3)

3) o’(BO*)aPg/;)r*

and (7)

have unique

Eo*,

T*;

= 0,

then the disturbed system (1) with E f, o and F are defined and smooth, a solution of the second degree of the ing E = go*, yl = (nlm)V(t - to) + 9 Note solution

roots

> 0 small has, in the region where unique stationary m/n-resonant form (41, reducing to the generatfor E = 0.

1. The uniqueness is understood in the sense corresponding to each fixed set of constant

As a rule, v* in the

(3) has one root go*, while interval (0, 2~) [21.

Note 2. As mentioned above, under more general assumptions

(7)

that there Is one m, n, Eo* and v*.

has a finite

the solution (4) exists regarding the smoothness

number of roots

and is of f,

Note 3. The case when (7) has multiple roots -r* presents difficulties and Involves an expansion in fractional powers parameters [3, 3, 6, 71.

unique o and F.

considerable of the small

Note 4. If o’@e*) # 0, but Pi = 0, the motions realizable In the system have degrees not less than 3. The corresponding solutions can be obtained by a similar method. Notes 1 - 3 also apply to these SOlUtiOns. 3. Stability

of

second

degree

motions.

The case

of multiple

zero

226

L.D.

Akulcnko

characteristic exponents is well known to present great difficulties in studying the stability of motions described by equations with a small parameter. In some simple cases, however, the characteristic equation can be found and the characteristic exponents written as series in lntein the case of the era1 [51 or fractional [2 - 61 powers of E.’ Clearly, set of two equations cl), the expansion will be in powers of 6 = JE [4, 51 . Recalling Lyapunov’ s familiar theorem, we form a system in variations in the Polncare form. I.e. we confine ourselves to the first approximation system:

If both characteristic exponents of (16) have negative real parts, the perturbed solution will be asymptotically Lyapunov-stable, and will be unstable if one or both have a positive real part [4, 51. The other critical cases require the consideration of the still neglected nonlinear terms. The aim of the present section is to find sufficient conditions for the asymptotic stability of our second-degree solution. The solution

of

(16) will

be sought E = z&e=‘,

as q = vest,

where u and v are T-periodic functions ponent. We have the expansions

Substituting

(12)

in (11).

then (11)

(11;

and a is the characteristic

in (lo),

and equating

ex-

coeffi-

cients of like powers of S, we obtain, in particular. from the system of the zero approximation: ue = 6, vu = bg = const. From the system of the first approximation, we have aI = al = const., ~1 = bl = const., where w’(&*)ai = a,bO, In view of this,

the system of the second au2 -=

bo,

dt

*vz

-= dt

(13) approximation

o’(Eo’)

u2 +

bo -

a&o -

sib,.

in 6 is

Resonant

motions

in

a substantially

non-linear

The ug perlodicity condition gives al = 3, which, al = 0, i.e. III = 0. The ~2 periodicits condition

The equations

of the next approximation

au3

-

dl

=

O’(Eg+)UQ +

3F -

227

system

by (131, is

leads

to

are

vi -

aA

-

a&O,

() ti0

whence

u3

a3 +

=

h

where

The perfodicity condition for the function ~4, obtained equation of the fourth approximation, namely,

from the

is (14)

co&P+ cio2 + cz = 0, in view of which: @pi / 8th = 0 (k = &g;.

. .), where

*T co=--;,

ci=~j[(~)o+(;)o] 00

It follows provfded

d4

c2-$.

0

obviously

from (14) that the solution

i[(%)o+(;)o]

dt
0

ghile the second of (15) is necessary sufficient. Notice that the vanishing

is asymptotically

oo’$
stable

(15)

for stability, it is by no means case is excluded from the theorem.

228

L.D.

Akulcnko

However, if the first expression is zero, the characteristic exponents in the calculated approximation are pure imaginary, and in order to find the sufficient conditions for stability, we have to evaluate a3 etc. As a result we have: Theorem

2

Relations (15) are the stability of our perturbed

sufficient resonant

conditions for solution of the

asymptotic Lyapunovsecond degree for

t > to. 4. Example. Take the problem of the resonant rotatory motions of a plane physical pendulum with moment of inertia I, the point of suspension of which executes small rectilinear oscillations of high frequency through an angle 6 to the vertical according to the law A cos at + (B/4) forces and the second cos 2 at. A simpler problem, In which friction harmonics of the oscillations are Ignored, Is considered in [51. The motion

of the

system

d2x

Iz+pagsinx=

can be described

approximately

by

--pao2sin(z-*)(Acosot+Bcos20t)-g~ dt



where x is the angle of deviation of the pendulum from the vertical, u a the distance from the centre of gravity to the mass of the pendulum, the axis of rotation, and q the constant coefficient of viscous friction We introduce the parameter acting on the axis of rotation. forces, e = g’lnl-%o-‘-=q 1, where 1 = I/us is the reduced length of the pendulum. We also denote A -= 1

The equation

eb,

-

B 1

of mot ion d2x -=-

=

ezbc,

9 = OZ

82).

(b, c, h -

11,

0 =

wt

is

s2sinr-ebsin(r-6)(;ose+eccos28)-e2h~.

d02

Introducing the phase ly and “energy” g in accordance with the usual [81, this equation can be reduced to a system with rotating formulae however, since the phase of the form (I). There is no need for this, equation is easily written directly in the forrll (1): dE -=

de

-

e2

sin Q - eb sin(g - 6) (cos 0 + ec cos 0)-

e%E,

motions

Resonant

The equation

of phase

in a substantially

non-linear

229

system

balance is 2mn

P, (7) = - b

Ze+T-8 m

!

cosOde=O

which is easily seen to define the nain resonant motion in the Rotations with m/n # 1 are obviously motions of higher degree. resonance l/2. Equation (7) then becomes P2c-r) = - abc sin(~ 4nh = 0, which, if h < bc/4. has two real roots in an interval 2r: 4h z, = 6 - arcsin -

43.

‘t2= 6+n+arcsin--,

hc’

system. the 6) of length

Take

bc

where 8Pz / ~3%~( 0 for -r* = T 1 and 8Pz / at* > 0 for “I* = 72. Since, for solution can be obtained by evaluA < bc/4, aP&* # 0, any approximate ating the coefficients of the series (6) or by successive approximations. This perturbed solution is asymptotically stable for h > 0 for T* = ~1, and unstable otherwise. Translated

by D.E.

Brown

REFERENCES 1.

BOGOLYUBOV,N.N. Theory

of

nelineinykh 2.

3.

kolebanil),

Oscillations

Yu.A. Asymptotic (Asimptoti~heskie

Moscow, Fizmatglz,

AKULENKO, L.D. On resonance in non-linear freedom. Zh. uychisl. Mat. mat. Fiz. 6, AKULENKO, L. D. and VOLOSOV, V.L. Vest.

4.

and MITROPOL’SKII,

Non- linear

Mosk.

Gas.

Univ.

Ser.

mekhan.,

in

metody

the

v teorii

1963. systems

with

6,

-

On resonance

mat.,

Methods

1126

one degree 1966.

in a rotatory 1,

KATS, A.M. Forced oscillations of near-conservative systems with one degree of freedom, Prikl. Mat. 32, 1955.

13

of

1130,

-

17,

system, 1667.

non-linear Mekh.,

19,

1,

13

5.

MALKIN, 1-G. Some problems of non-linear oscillation theory (Nekotorye zadachi teorii nellneinykh kolebanii). Moscow, Gostekhlzdat, 1956.

6.

AKULENKO, L.D.

and VOLOSOV, V.M. Resonant

rotations

of higher

-

230

L.D.

degrees, 1961. 7.

8.

Vest.

Mosk.

Gos.

Akulsnko

Univ.

Ser.

mat.,

mekhan.,

2,

10

-

14,

PROSKURYUAKOV. A.P. Periodic solutions of quasilinear aUtOnOmOUS systems with one degree of freedom, as series in integral and fractional Powers of a parameter, in hoc. Internat. Symposium Non-linear Oscillations, 1, 367 - 380, Kiev, AN USSR, 1963. voLOsOV, V.M. Averaging tions, Usp. mat. Nauk

in systems of ordinary 17,

6,

3

-

126,

1962.

differential

equa-

on