R ENDICONTI
del
S EMINARIO M ATEMATICO
della
U NIVERSITÀ DI P ADOVA
F RANCO C ARDIN
A generalized theory of classical mechanics for the two body problem
Rendiconti del Seminario Matematico della Università di Padova, tome 69 (1983), p. 135-151
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Theory
for the Two Body Problem.
FRANCO CARDIN
(*)
1. Introduction.
A well known result of Classical Mechanics consists of the
following
assertion about the Two
Body (1)
Problem in the reduced mass frame:(a) if P2
issubject
to agravity field
with centre atPI,
and theorbits
of
itspossible
motions relative toPI
are conic sections with af ocus
at
Pi ,
thenP2 fulfils
Newton’s law: U== -rig.
Because of the
large
range ofvalidity
for Newton’slaw,
it may asked whether it ispossible
to build a mechanicaltheory
in whichthis
law,
or aphysically
relevantgeneralization
ofit,
can be deducedfrom
hypotheses
weaker than these in(a).
In the
present
paper Itry
togive
aclassical,
thatis,
nonrelativistic,
answer to the above
question.
The basicchange
withrespect
to theusual Classical Mechanics consists of a
generalization
of Mach’s axiom for mass.Moreover,
in[4]
it is shown that a naturalapplication
ofthis
theory
leads to aphysically acceptable description
of theperi-
helion’s
precession
ofplanets.
The last result is very similar to the well knownapproximation
of the motion of aparticle
under Schwarz- schild’s solution for the metric tensor within GeneralRelativity.
In connection with the Two
Body Problem,
thepresent theory
isinteresting especially
because(*)
Address: Seminario Matematico, Università di Padova, via Belzoni 7, 35100 Padova. This paper has been worked out within thesphere
ofactivity
of the research group no. 3 for Mathematical
Physics
of C.N.R.(Consiglio
Nazionale delle
Ricerche).
(1)
Materialpoints Pi
andP2.
(i)
its results are obtained within a classicalconception
of thephysical world,
hence(ii)
the critical reviews of theconcepts
of space,time,
andmatter,
which are essential for General
Relativity,
are not necessary in thepresent theory. Therefore,
the latter is muchsimpler
than GeneralRelativity.
In sections
2,
3 the axioms of atheory
T of ClassicalMechanics,
restricted for shortness of treatment to the Two
Body Problem,
arepresented
in a wayslightly
different from[2]
but inconceptual
agree- ment with that paper. In theorems Tl to T4 some well known resultsare deduced from
hypotheses
moregeneral
than the usual ones.In section 4 we formulate a weaker
version, A2*,
of axiom A2 formass in section 2. This
generalization
issuggested by
ageneral
the-orem of
representation, T2,
for the force in 17. Westudy
theresulting theory 5"*
and someimportant
consequences of it. Indetail,
in(4.15)
and
(4.16),
we offer the mostgeneral expression
for the forceand,
in section
5,
in the mass reduced frame we show that the orbitbelongs
to a certain conic surface(T2*).
As consequence,assuming
that
Pl
coincides with theorigin
of a framef!Jl:T84,
we prove that the motionof P2
isplane if
andonly
it its orbit is a conic section.In section 6 we show that within 5"* any
plane
motion isgenerated only by
a forceW
of aquasi-Newtonian kind,
thatis, by
a Newtoniancentral force to which we add a force of little
magnitude, depending
on the
velocity
also. The force ~ reduces to Newton’s when(in
con-nection with
plane motions)
5"* reduces to 5".Thus in v* the
following
alternative assertion to(a)
holds in themass reduced frame:
(a*) if P2
issubject
to aforce field
which admits ageneralized potential
and describes aplane orbit,
then this orbit is a eonic section and thequasi-Newtonian force
law( 6.8 )
holds.2. Classical axioms for the Two
Body
Problem.We consider classical
physics
andregard
the motions of inertial spaces and inertialf rames
as known. Let such a frame. We as- sume thatonly
theparticles P1
andP2 exist,
so thatthey
constitutean isolated
system.
Before
listing
the axioms of ClassicalMechanics,
here enunciatedbriefly only
forour aystem,
we state in advance an axiom ofphysical possibility
whose use is essential in severalproofs.
Al
(of Phys. Poss.).
Let be anarbitrary
inertialf rame.
T hen( i ) if
Xl’ X2’ VI and V2 arefour
vectorsof
11~3 with X2, it isphys.
pOSSe(2)
that at some instant t E l!~ the twoparticles Pl
andP2
have in
RJ
thepositions
x, and X2 and velocities VI and V2respectively, (ii)
it isphys.
poss.for P,
andP2
to havenon-vanishing
accelera-tions
parallel
with X2 - x1, inf!ae J
and hence in any other inertialf rame,
at some instant t.
A2
( mass existence).
T here are Ill, l~+for which, calling
ai theacceleration
of Pi (i
=1, 2)
withrespect
to~,~
at the instantt,
wenecessarily
haveThis axiom is in
harmony
with Mach’s paper[6]
and with morerecent axiomatization of classical
particle
mechanics-cf.[2].
If(2.1)
holds
necessarily,
then i ~ is called a mass distribution. If also i- p§
is a massdistribution,
then for some b EIt’
=blzi (i
=1, 2)
as is easy to prove on the basis of
Al(ii).
Thus we have oo1 massdistributions
mutually
connectedby changes
of the unit mass.A3
(dynamic Zaw) .
In connection with anarbitrary
choiceof f?ae J
there is ac
function (force) f
such that
if
i r--7>- f-li is a mass distribution and withrespect
toIf,
atthe instant
t, Pi
has theposition
xi andvelocity
v i(i
=1, 2),
then(2)
Physically
Possible meansideally
realizable, i.e.technically possible
for ideal
experimenters-cf.
[3].The function
f
that fulfils the condition above is called force func-tion,
anddepends only
on the choice of units in the well known way.Further on
by f
such a function will be understood.By Al(i)
and A2 we have thefollowing
theorem:T1
(Action
and Reactionprinciple for
theresultant). If
XI’ X2’Vl, V2 E l~3 and x2 , then
Usually
one also assumes thefollowing
Action and Reactionprin- ciple for
the moment : Under theassumptions
in A2 wenecessarily
have that
This
principle
is not included in thepresent theory. Instead,
in sect.
3, (2.5)
will be deduced from theassumption
that ageneralized
energy
integral
holds for thesystem P2~.
Well known
homogeneity
andisotropy properties
of inertial spaces -cf.[1], § 2-restrict
the form off according
to thefollowing
axiomA4. T here is a
f unction
F:[R3n(0)]
x R3 - R3for
whichand, for
all u, w E R3 with u 0 0 and all properorthogonal
matricesQ (QQP
=1,
detQ == 1).
By
a theorem ofCauchy -
cf.[7],
p. 60 -, one has thefollowing representation
theorem for the above function F.T 2. Let F
fulfil (2.7).
T hen there are threemappings ~, ØI,
and Vof
~8+ >C X ll~ intofor
whichThrough
the weak Action and Reaction theoremTl,
the massaxiom A2
implies
a further restriction on the form of F. Under the definitionsthe
following
theorem can beeasily proved:
T3. T he most
general function F,
that has thef orm (2.8)
and under condition(2.6) fulfils ( 2 .4 ) ,
isgiven by
3.
Assumption
that a certaingeneralized
energyintegral
exists.From the
physical point
ofview,
it appears natural to assume thatgeneralized
energyintegral
exists for our isolatedsystem-cf.
axiom A5below. As a
preliminary
let us note that the mass axiomA2,
andhence the Action and Reaction
principle
for theresultant,
yimplies
the
following theorem, proved
in textbooks afterhaving
stated the full Action and Reactionprinciple-cf.
also[5],
p. 352-butusing only
the
part
Tl of it.In the
reference f rame
whoseorigin
is(always)
inPl,
and isrotationless with
respect
to inertial spaces, thedynamic equations of P2
reads-cf.
(2.3)
If a function
V(q, q), exists,
y for whichthen
(since 0)
Tr has thefollowing
form(linear
inq) :
where
For the kinetic
energies
we have the
identity
The
Lagrangian
functions ofP2~
in and arerespectively,
so that theircorresponding
Hamiltonian functions readAxiom A2
implies
=0,
hence = const. Then -V’ is afirst integral of
the motionof P2~ iff
is such anintegral.
Since
by (3.6) aL/ at =
0 = in our case arefirst integrals.
It is clear that if A2 is excluded from the
theory
ffbeing
con-sidered,
both(3.1)
and the aboveequivalence
assertion on andare no
longer
theorems. With a view toweakening
A2 andconsidering
the material reference frames which e.g. the motions of
planets
arereferred
to,
not to be inertial but choices of9,,_v
with theorigin
inthe sun, I propose the
following
version of the afore-mentioned exist-ence
assumption
for ageneralized
energyintegral.
A5.
If has
theorigin
inPI
and has the same orthonormal basis{eh}h=1,2,3
asf!ae-F’
thef unction 97(g, q) for
which the motiono f P2
neces-sarily fulfils
theequation p* 4 = ~ (q, q),
isafforded by
ageneralized
potential V(q, q),
V EC(2) ([R3BA] x R3; R), for
some set A without in- ternalpoints,
such that thefunctions
have continuous extensions onto
On the basis of some
preceding
considerations-cf.(3.1)-A2 implies .
From
(3.2)
and(3.3)
we deduceNow we are
going
to characterize(the
formof)
the functions ~ and 4. AxiomAl(I)
ofphys.
poss. tells us that for all 0 and alltj,
some motion of ispossible
forwhich,
at someinstant t,
q and
q represent
theposition
andvelocity
ofP2
inf!Jt:TØ6.
Then(2.10)
and
(3.10) imply
thatSince
hence
By (3.11 ), equation (3.10)
becomesThe term
rot a(q)
in(3.14)
isisotropic
iff for some function-9(q),,
!Ø: R+ -¿.
R,
By (3.14), (3.15),
and(2.10)
(see Al(i));
it is true iffCalling
~l’ thetheory
based on axioms A1 toA5,
let us summarizethe
preceding
resultsby
thefollowing
theoremT4.
(i)
The mostgeneral force
F in !T ispositional
and admits a(universaZ) potential U(q) :
(ii)
also the Action and .Reactionprinciple for
the moment holds(iii)
in the abovesystem
the motionof P2
is central(with respect
to theorigin P,)
and henceplane.
A natural
specialization
ofer, through
a suitable choice ofU,
leads to Newton’s
theory
ofgravitation.
Thevalidity
of this choicecan be
proved
when e.g. new facts arepostulated,
e.g. that the pos- sible orbits ofP2
inPÃ/TfJI
are conic. In theremaining
sections atheory
~"*is
studied,
which can be obtained from erby replacing
the mass ax-iom A2 with a weaker
axiom,
A2*. Under the additionalassumption
that the motion of
P2
in should beplane-see
axiom A6 below-(which
is a theoremin V, T4(iii)),
9-* will be shown to admit New- toniangravitation
as a limittheory
and to foresee(in
aslightly
ap-proximated version)
aprecession
of theapsidal points
ofquasi
conicorbits,
in substantialagreement
with thecorresponding
results of GeneralRelativity.
4. A
theory
~ * with a mass axiom A2 ~ weaker than A2.The
general
form(2.8)
for F(together
with thedynamical
axiomA3)
.suggests
to weaken the mass axiom A2 into thefollowing
A2*. For some
!l1,!l2ER+, if
xi[ai]
is theposition [acceleration], of Pi
in the inertialf rame f1i oF
at some instant t(i
=1, 2),
then we neces-sarily
haveLet Al and A3 to A5
keep holding. Then,
as iseasily checked,
theorem T2
keeps holding
unlike theoremsTl, T3,
and T4. Inspite
of this the
theory -q-*,
based onAl, A2*,
and A3 toA5,
appears tosubstantially belong
to classical mechanicsby
the notions of space,time,
and mass. In fact it is easy to prove also with an essentialuse of the axiom
A1(ii) (of phys. poss.),
that ool mass distributions i ~ ,ui exist.The
replacement
of axiom A2 with A2*enlarges
the classof the motions of
P,l compatible
with the axioms of thetheory being
considered. In order to deal withgravitation,
let us restrictthis class
by
means of some conditions on the motionsphys.
poss.for The
following
axiom on the orbits ofP2
in9,,_q
isreached
by qualitative observations,
it is atheorem, T4(iii),
in I andcertainly
weaker than therequirement that,
forexemple,
these orbits should be conic.A6. In
~,~-~,
which has itsorigin
inPI,
the motionof P2
isplane.
This axiom will be
exploited only
from section 6 on.Let
5r(q7 q )
theforce,
relative toabove,
extertedby
theparticle P1
of mass ,u1 on theparticle P2
of mass ,u2. Hence(4.2),
below holds
By
A5(4.2)2
holds for some functionsa(q)
andU(q).
Let
F(q, q)
be the effective force exertedby P1
onP2,
thatis,
the one relative to an inertial frame
having
the same orthonormal.basis
{e,}
as Thenhence
by (4.2)1, (2.9)1,
and(3.1)2,
Therefore the
analogue
of(2.7)
holds for4),
so that the samecan be said of the consequence
(2.8)
of(2.7). q)
has the formIn order to characterize
.91, f!4
and W on the basis of(4.2),
let usnow reason like in the
proof
of theorem T4 in section 3.By
an es-sential use of axiom
Al(i) (of phys. poss.),
from(4.2)
and(4.5)
with4
= 0 we deduce thatFurthermore let us note that the term rot
a(q)
in(4.2)
isisotropic
iff for some function
9(q)
9 ~: R+ -118,
Under the definition
(4.8)
equality (4.7)
becomesThe
general
solution of(4.9)2
isso that
(4.9)1
becomes.Some solutions of
(4.11)
can be foundeasily
inspherical
co-ordinatesr,
8, g~ (r
---q).
In fact thesystem
is
solved,
foresample, by
and in cartesian co-ordinates we have that
where A =
Meg.
Then for some functionU(q)
of class W2> and somethe force function
(4.2)
has the formso that it
obviously
has a continuous extension ontoI
hence it is
compatible
with A5.By (4.4)
so that
by (4.15)
weeasily
obtainwhere
Remark that the presence of the factor
(#1 - #2)-1
in(4.16)
doesnot
imply
asingularity
for = ,u2. In fact theintegration
con-stant K can
depend
on pi and ,u2. Theassumptions
thaton
(4.16),,,,-are
natural andimply
thatwhere h E R is a universal constant.
Note that the force law
(4.16)
iscompatible
with axiomA2*,
inthat
(4.16) yields
5. Orbits of
P 2 in
theThe
dynamical equation
of.P2
in~~-~
isLet us call Reduced Moment
o f
.Momentum ofP2
the vector L* :Then
(5.3)
so that
Tl*. In the
theory ff*, I
is afirst integral of
the motionof P,
with
respect
toLet
9#,
be agenerally
non-inertial frameJ1, J2 , J~)
in whosemotion with
respect
to~~-~,
to beregarded
as thedragging motion,
the
plane
isrolling
onP2’s trajectory
inffl.rg¡
withoutsliding.
The index will be used forquantities
referred to(and regarded
therefore as absolute[relative]).
ForP2
we have(oc)
Determinationof
wD. Since isrotating
withrespect
tof!Jl:rfJï
around an axisthrough Pl ,
we have thatand
by (5.6)~,, Furthermore, by (5.2)
L* isorthogonal
to theplane (P,, Jl, J2),
so that for suitable orientation ofJ,, J2
and forq A q # 0
Poisson’s
equation
forJ3
readsand
by (5.8), (5.5),
and(5.3)
we also have thathence, by (5.4)4’
=0,
i.e. wD - S2 = for some X E R.Furthermore
Henee Z
= 0 and(B) Determination of
theangular velocity of
theplane
(Pl, J3, qlq)
withrespect
to SinceP2
=Pl -~--
qalways
belongs
to theplane (PI, II, J2 ) ,
we have HenceFurthermore by (5.2)
and(5.5),
the vector L* is constant in!?lip¿,
the area
swept
out in unit time isconstant,
andby (5.12)
we have that isBy
thecomposition
theorem forangular
velocitiesHence
(y) Expression of
the time derivativeof
w withrespect
toBy (5.15), (5.11)
and(5.16)
9--v
hence
Thence we
lastly
obtain thatSome results obtained in this section within J"* are summarized in the
following
theoremT2*. According
to thetheory
based on axiomsAl, A2*,
and A3to
A5, ( i )
the mostgeneral force function q ) [F( q, q ) ]
relative toexpressed by (4.15) [(4.16)], ( ii )
the motionsof P2 compatible
with these
forces
havetrajectories
inlying (each)
on acf ixed
conicsurface
inthat
has the vertex atPI,
the axisparallel
withwÅ,
andsemi-aperture 6
whereAs was
expected,
for K - 0 we i.e. the conicsurface
reduces to a
plane.
It can be asserted that T is thespecial
case of 17-*obtained for .K = 0-cf.
(4.16).
It is evident that
P2’s plane
orbits in A6-arenecessarily conics;
however it must be remarked that theplane through P2’s trajectory Z2
can containP1 only when Z2 belongs
to astraight
line.6. On the
theory !!7* +
A6. Onplane
motions.We want to determine the most
general expression
of~(q, q)
-cf.
(4.15)-in
thetheory /*+A6
obtained from F*by
the addi-tion of A6 as an axiom. It suffices to
require
thefollowing identity
i.e. that the about vector
b,
which isorthogonal
to theosculatory plane
fortrajectory,
should have an invariant direction.By (4.15)
and the
following
definition of A =A ( q )
we have that
Remembering
that andwriting
A’ fordA/dq,
wehave that
that
is,
For
q/~ q ~
0 the vectors q,q,
and4A q
arelinearly independent.
Hence
(6.1)
holds iff thecorresponding components
of the vectors band
b, put
in evidenceby (6.3)4
and(6.4),
areproportional,
i.e.While
(6.5 )~
holdsidentically, ( 6.5 ) 2
isequivalent
withequation
in the unknown A. The
general
solution of(6.6)
isAs a consequence,
by (6.2)
and(4.15)
Now the
validity
of the theorem below is evident.T3. In
( i ) P2’S trajectory
inrJl9"’ffl
is aconic, ( ii )
the centralcomponent o f q) (i.e. Ilq)
isquasi-Newtonian-cf. (6.8)2
.( yq-3 -J-
where y and K areindependent constants,
and(iii)
in the case g =0,
which occursiff
thefull
Action and Reactionprinciple
issatisfied,
the Newtoniangravitation
lawholds,
i. e. theforce
q)
isindependent of q
and admits thepotential U
= -y/q.
The limit behaviour of the theories 9-* can be ex-
pressed symbolically by
REFERENCES
[1] V. I. ARNOLD, Mathematical Methods
of
Classical Mechanics,Springer- Verlag,
New York - Berlin, 1978.[2] A. BRESSAN, Metodo di assiomatizzazione in senso stretto della Meccanica
Classica. Applicazione
di esso ad alcuniproblemi
di assiomatizzazione non ancoracompletamente
risolti, Rend. Sem. Mat. Univ. di Padova, 32 (1962), pp. 55-212.[3] A. BRESSAN, On
Physical Possibility,
Italian Studies in thePhilosophy of Science,
pp. 197-210, ReidelPublishing Company,
1980.[4]
F. CARDIN, Precessionof
theperihelion
within ageneralized theory for
theTwo
Body problem,
to appear on Rend. Acc. Naz. dei Lincei.[5] G. GRIOLI, Lezioni di Meccanica Razionale, Libreria Cortina, Padova, 1977.
[6] E. MACH, Die Mechanik in ihrer
Entwickelung
historisch-kritischdarge-
stellt, 1883.[7] C. TRUESDELL, Six Lectures on Modern Natural
Philosophy, Springer,
1966.Manoscritto pervenuto in redazione il 9 dicembre 1981.