R ENDICONTI
del
S EMINARIO M ATEMATICO
della
U NIVERSITÀ DI P ADOVA
E UGENE L EIMANIS
On integration of the differential equation of central motion, I
Rendiconti del Seminario Matematico della Università di Padova, tome 68 (1982), p. 49-61
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Integration Equation
of Central Motion, I.
EUGENE LEIMANIS
SUMMARY -
Assuming
that the forceacting
on aparticle
is of the formthe
theory
of infinitesimal transformations isapplied
to determine the forms off (r)
and for which the differentialequation
of central motion isintegrable by quadratures
or reducible to a first order differentialequation.
1. It is well known that the
problem
of motion under central forces isalways
solvableby quadratures
when the forcef (r)
is a func-tion of the distance r
only [13].
If we ask the furtherquestion,
y inwhich cases the
integration
can be effected in terms of known func-tions,
then Newton[10]
showed that if the central force varies as somepositive
ornegative integral
power of thedistance,
say then-th,
the
problem
is solvableby
circular functions in the cases n =1, - 2
and - 3. The case n = - 3 was studied in detail
by
R. Cotes[3].
Next
Legendre [5]
showed that theintegration
can be effectedby
means of
elliptic
functions forn = 0, 3, 5, - 4, - 5
and - 7. After- wards Stader[12] investigated
ingreat
detail the cases n = -3, -4, -5, -6, -7, Karger [4]
the case n = - 4 and Macmillan[9]
thecase n = - 5.
Finally
Nobile[11]
discussed theintegration
in thecases when n is a
negative integer,
and inparticular
the cases n = -2, - 3, - 4, - ~,
and when n is a rationalfraction,
inparticular
the casesn
= - 3/2 and - 5/2.
(*)
Indirizzo dell’A.: 3839 Selkirk Street, Vancouver, B.C. V6H 2Z2, Ca- nada.In what follows we shall assume that the force
depends
on bothvariables r and 0,
and that it can be written in the form of aproduct Here r,
0 are thepolar
coordinates of theparticle
P withrespect
to the center of force 0. Our aim is to determine the forms off (r)
andg(6)
for which theequation (1)
isintegrable by quadratures
or for which the
integration
can be reduced to someparticular type
of differential
equations.
The method used is that of infinitesimal transformations which Iapplied [6, 7, 8]
some 35 years ago to theparticle problem
of exterior ballistics. It is a well knownfact,
thatthe
knowledge
of an infinitesimal transformation under which thegiven system
of differentialequations
remainsinvariant,
can be usedto lower the order of the
system.
In ourproblem
theintegration
ofthe second order differential
equation
of the central motion will be reduced to theintegration
of a first order differentialequation,
satisfiedby
the invariants of the infinitesimal transformationused,
and anadditional
quadrature
for the time.2. Consider the motion of a
particle
P of mass one acted onby
a central force of the form
Q(r, 0)
= Then the differentialequation
of thetrajectory
can be written in the form[13]
where =
I/r,
c2=1/h2 (h
is a constant whichrepresents
theangular
momentum of P about
0)
andF(u) _
Let
be an infinitesimal transformation which leaves the
system
which is
equivalent
toequation (1),
invariant. Letbe the trivial transformation. where ~. is an arbi-
trary
functionof u, v, 0,
is also an infinitesimal transformation which leavessystem (3)
invariant. If weput
!l. _ -O,
then to any trans- formation(2)
therecorresponds
a transformationwhere
If u, v
and ui, v, are the coordinates of twoneighboring points
in
the u, v-plane,
then theequations
represent explicitly
the infinitesimal transformation(4),
and the con-ditions to be satisfied in order that
(4)
leavessystem (3)
invariant areIn order to
integrate system (6),
let us rewrite the firstequation
in the form
or
(7)
where
Here the
subscripts
denotepartial
derivatives of U withrespect
tothe variables
represented by
the indices. Ifby
means of(7)
we cal-culate substitute its
expression
into the secondequation
ofsystem (6)
and arrange thatequation according
to the powers ofc2,
then we obtain the
equation
In order that the infinitesimal transformations
(2)
and(4)
beindependent
ofc2,
the functionsU, TT,
O and U must beindependent
of c2. This
implies
that thequadratic equation (8)
in c2 must vanishidentically.
In otherwords,
the coefficients ofc4,
c2 and c° mustvanish
separately.
Hence we must have,
Consequently U"
=99(u, 0)
andwhere 99 and
are two functions to be determined later.2)
The coefhcient ofc2, put equal
to zero,gives
theequation
or, interms
and
and theirderivatives,
theequation
Since 99 and V
areindependent of v,
then we must haveand
consequently 99 _ ~ ( 8 ) ,
yand
3)
The coefficient ofc°, equated
to zero, leads to theequation
Since and y
areindependent of v,
then in the lastequation
the coefficients of thequadratic equation
in v must vanishseparately.
Hence first we must have
consequently
and
Second,
we must haveand hence
(k
is a constant ofintegration) . Third,
theequation
must be satisfied. This
implies
thatIf we eliminate
ga’(8)
fromequations (14)
and(15),
then we obtainfor the differential
equation
the
general
solution of which iswhere C and a are two constants of
integration.
Sinceand
q(0)
satisfies the same differentialequation
as y thenFinally equation (10)
can be rewritten in the formIn order that the variables u and 0 be
separable
in(20),
or1fJ2(O)
must vanish
identically.
Ifyi(0)
=0,
then alsoq’(0)
=q(0)
= 0(since
C = 1~ =0)
andequation (20)
reduces to = 0. Hence1) F’(u)
=0,
or2) g(O)
= 0. The second case is of no interest. In the first caseF(u)
=const.,
sayequal
to one,f(r) =1 /r2
andg(O)
remains
arbitrary.
This is the case discoveredby Armeflini [2].
If1fJ2(O)
= 0 whichrepresents
the trivial solution of(16),
thenwhere m is an
arbitrary
constant. Hence(D
is a constant which without any loss ofgenerality
can be assumedequal
toone), (23)
and
or
Accordingly
U assumes theexpression
and
Then from formulas
(5)
and(7)
it follows thatHence, by comparison
of the coefficients we obtain thatand
Since
by (5)
U =U - vl9,
thenHence we have determined the three coefficient functions
U,
Vand 0 of the infinitesimal transformation
(2). They
contain threearbitrary
constantsC, a
and 1~. If weput
C = a =0,
k =1 ork = a = 0, C =1,
then we obtain two infinitesimal transformations which leavesystem (3)
invariant. A fourtharbitrary
constant menters formulas
(23)
and(24)
whichgive
the functionsf(r)
andg(O).
Let us consider now the two
special
casesjust
mentioned.3. Case
I: 1~=a=0,
C=1.In this case we have
and the invariants and Y of the infinitesimal
transformation,
de-termined
by
theequations
are
is
given by (22)
and from(24)
it follows thatThe derivatives of the invariants with
respect
to0, taking
into ac-count formulas
(3), (22)
and(30), satisfy
theequations
Hence
by
division we obtain theequation
or, if ’we
put
Y2 =Z,
theequation
The
general
solution of(32)
is( C1
is a constant ofintegration)
and henceFrom the first
equation
of(31)
it then follows thatand after
integration ~=~(0).
Thenby (33)
alsoand the first formula of
(29) gives
usIn order that the
integral
I on the left of(34)
could be evaluated in terms of circularfunctions,
must be apolynomial
of at mostthe second
degree.
This condition is fulfilled in thefollowing
threecases:
In
fact,
in the first two casesG(X)
is apolynomial
ofdegree
twoin X and in the third case
Gl(Xl)
isquadratic
inXi
= X2 andI =
(1/2) f dXl/Ý Gl(Xl).
Hence theintegrability
in terms of circularfunctions,
first consideredby
Newton f or n=1, - 2, - 3,
can be ex-tended to the above first two more
general
cases.Next,
let us list the cases in which theintegration
on the lef tof
(34)
can be effectedby
means ofelliptic integrals.
For this it is necessary thatG(X)
be of the third or fourthdegree
in ~. This con-dition is fulfilled in the
following
six cases:In
fact,
it is easy toverify
that in the above six cases theintegral
Iis of the form
where is a
polynomial
ofdegree
three orfour,
or of the formwhere
G(X)
is apolynomial
ofdegree
four inX,
or it can be reducedto one of the
integrals 11 or I2
in terms ofXi
= X2.Hence the
integrability
in terms ofelliptic functions,
first con-sidered
by Legendre
forn = 5, 3, 0, - 4, - 5, - 7,
can also be ex-tended to the above six more
general
cases.4. Case II:
As before
F(u)
isgiven by (22)
andg(O)
is definedby (24). By
in-tegration
we obtain thatFurther we have
and the invariants of the infinitesimal
transformation
y determinedby
the
equations
are
Their derivatives with
respect
to 8satisfy
theequations
and
hence, by
division we obtain theequation
If we
put r==2013~/2-2013~
thenequation (38)
becomeswhere
If m =
0,
thenand
equations (37)
can beeasily integrated.
Theirintegrals
arewhere A and B are two constants of
integration.
From the first for- mula of(36)
it then follows thatThis is the
general
solution ofequation (1)
forF(u)
=1. Sincein this
particular
caseequation (1)
islinear,
its solution(41)
can alsobe obtained
by
directintegration.
For m
= I,
we haveF(u)
= u,f (r) = 1/r3, g(o)
and thegeneral
solution of(38)
isOn the other hand for m == 1 we have
by (40)
forP(X)
theexpression
It is
interesting
to note that for thisparticular
case Abel[1]
hasgiven
an
integrating
factor forequation (39).
Ingeneral, however,
thisequation
cannot be solvedby quadratures.
REFERENCES
[1]
N. H.ABEL,
Oeuvrescomplètes
de Niels Henrik Abel, Nouvelle édition,publiée
par L.Sylow
et S. Lie, tome II, Christiania (1881), p. 35.[2]
G. ARMELLINI, see [13]WHITTAKER,
p. 81.[3] R. COTES, Harmonia mensurarum, 1722.
[4] E. KÄRGER,
Untersuchung
der Bahn eines Punktes welcher mit derKraft k/r4
angezogen oderabgestossen
wird, Archiv d. Mathematik u.Physik,
58 (1876), pp. 225-277.
[5]
A. M. LEGENDRE, Traité desfonctions elliptiques
et desintégrales eulériennes,
tome I, Paris, 1825.
[6]
E. LEIMANIS, Surl’intégration
parquadratures
deséquations
du mouvementdu centre de
gravité
d’unprojectile
dans un milieu de densité variable, C.R. Acad. Sci. Paris, 224 (1947), pp. 1618-1620.[7] E. LEIMANIS, Sur
l’intégration
parquadratures
deséquations
du mouvementdu centre de
gravité
d’unprojectile
dans un milieu de densité ettempérature
variables, C.R. Acad. Sci. Paris, 224 (1947), pp. 1752-1754.[8] E. LEIMANIS, The
application of infinitesimal transformations
to the in-tegration of differential equations of
exterior batlisticsby quadratures,
Proc.Second Canadian Math.
Congress,
Vancouver, 1949; Univ. of Toronto Press, Toronto, 1951, pp. 206-217.[9]
W. MACMILLAN, The motionof
aparticle
attracted towards afixed
centerby
aforce varying
as thefifth
powerof
the distance, Amer. J. of Math., 30 (1908), pp. 282-306.[10] I. NEWTON,
Philosophiae
NaturalisPrincipia
Mathematica, London, 1687.[11] V. NOBILE, Sulla
integrazione
delleequazioni
del movimento relativo dei duecorpi
che si attraggono secondo unalegge
espressa da una certaparti-
colare
funzione
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J. STADER, De orbitis et motibuspuncti
cuiusdamcorporei
circa centrum attractivum allis, quam Newtoniana, attractionistegibus
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[13]
E. T. WHITTAKER, A Treatise on theAnalytical Dynamies of
Particles andRigid
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