Over all steps of its development celestial mechanics has played a key role in solar system researches and verification of the physical theories of gravitation, space and time. This is particularly characteristic for celestial mechanics of the second half of the 20th century with its various physical applications and sophisticated mathematical techniques. This paper is attempted to analyze, in a simple form (without mathematical formulas), the celestial mechanics problems already solved, the problems that can be and should be solved more completely, and the problems still waiting to be solved.
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ISSN 00380946, Solar System Research, 2013, Vol. 47, No. 5, pp. 347–358. © Pleiades Publishing, Inc., 2013.
Published in Russian in Astronomicheskii Vestnik, 2013, Vol. 47, No. 5, pp. 376–389.
347
1
1. INTRODUCTION
The domain of astronomy discussed below is not
too popular nowadays. Modern astronomy, with its
prevailing astrophysical topics, answers mainly the
questions about the structure of celestial bodies and
their evolution. Here, we consider more applied prob
lems related to the motion of celestial bodies in the
solar system and accurate determination of their posi
tion in space and time. Historically, these problems
were the subjects of celestial mechanics and astrome
try, which once covered the contents of astronomy as a
whole. Now the situation has been changed so drasti
cally that one may seriously ask if the people of the
notsodistant future will be able themselves to com
pute the motion of the planets, the Moon, planetary
satellites, etc., and to determine their positions, or if it
will simply be just a routine procedure of specialized
computer specialized software? The theoretical base of
modern celestial mechanics and astrometry is the gen
eral relativity theory (GRT). Therefore, this essay
concerns also the applied aspects of GRT demonstrat
ing the use of GRT for constructing highly accurate
theories of the motion of celestial bodies and discuss
ing very precise observations.
2. CELESTIAL MECHANICS
2.1. Methodology of Celestial Mechanics
In very brief terms, celestial mechanics is a science
of studying the motion of celestial bodies. This laconic
and nevertheless very broad definition involves many
ambiguities. What is to be meant by celestial bodies?
Does this term include both the actually existing nat
ural bodies as well as model mathematical objects? In
the case of artificial celestial bodies (satellites, space
probes, etc.), do the problems of guidance motion lie
in the scope of celestial mechanics? Celestial mechan
1
The article was translated by the author.
ics is, without a doubt, one of the most ancient sci
ences, but from the antique times until the Newtonian
epoch, it managed to describe only the kinematical
aspects of the motion of celestial bodies (Ptolemaeus’
theory of the motion of planets, the Sun and the
Moon, Kepler’s laws). Only since the Newtonian
epoch have the dynamical aspects of motion begun to
prevail in celestial mechanics. Actually, celestial
mechanics became a science about the motion of the
solar system bodies under Newton’s law of gravitation.
In the 18th–19th centuries, celestial mechanics was
advancing with permanent success in developing
highlyaccurate theories of the motion of the planets
and the Moon. This advance resulted in the triumphal
discovery of Neptune based on the analysis of pertur
bations caused by Neptune in the motion of Uranus.
In the end of 19th century, Poincaré, who contributed
so much to the development of celestial mechanics,
formulated the aim of celestial mechanics to be the
solution of the question whether Newton’s law of
gravitation alone is sufficient to explain all of the
observed motions of celestial bodies. Poincaré has
indeed received general recognition in pure mathe
matics and theoretical physics; however, this formula
tion of the aim of celestial mechanics demonstrates
that Poincaré has contributed a crucial part to the
agreement of astronomical observations with the
results of mathematical and physical theories.
The first half of the 20th century was a period of
comparative stagnation for celestial mechanics. The
only brilliant exclusion was Sundman’s finding of the
general solution of the threebody problem in 1912.
Even the development of the general relativity theory
by Einstein (1915) had no essential influence on celes
tial mechanics of that period. Drastic changes began in
the middle of the 20th century. The new advances of
celestial mechanics were stimulated by new techniques of
highprecision observations, computer generation,
development of spatial dynamics, and progress in mathe
matics and theoretical physics. Celestial mechanics
Celestial Mechanics: Past, Present, Future
1
V. A. Brumberg
Institute of Applied Astronomy, Russian Academy of Sciences, nab. Kutuzova 10, St. Petersburg, 191187 Russia
Received December 20, 2012
Abstract
—Over all steps of its development celestial mechanics has played a key role in solar system
researches and verification of the physical theories of gravitation, space and time. This is particularly charac
teristic for celestial mechanics of the second half of the 20th century with its various physical applications and
sophisticated mathematical techniques. This paper is attempted to analyze, in a simple form (without math
ematical formulas), the celestial mechanics problems already solved, the problems that can be and should be
solved more completely, and the problems still waiting to be solved.
DOI:
10.1134/S0038094613040011
348
SOLAR SYSTEM RESEARCH Vol. 47 No. 5 2013
BRUMBERG
became much more versatile than before. It lost the
title of theoretical astronomy (historical title when
astronomy was restricted only by astrometry and celes
tial mechanics representing its observational and the
oretical parts, respectively) but became related much
closer to physics and mathematics. Actually, celestial
mechanics of the second half of the 20th century dealt
with four interrelated groups of topics, as follows:
(1) Physics of motion, i.e., investigation of the
physical nature of forces affecting the motion of celes
tial bodies and formulation of a physical model for a
specific celestial mechanics problem. The final aim in
this domain is to derive the differential equations of
motion of celestial bodies and of light propagation.
The global physical model underlying contemporary
celestial mechanics is Einstein’s general relativity the
ory (GRT). Within presentday physics, Newtonian
celestial mechanics is regarded as a completed science
since the equations of motion for any Newtonian
problem are known and the problem is reduced to the
mathematical investigation of these equations. As it
was already stated above, preNewtonian celestial
mechanics was in fact a purely empirical science. Even
nowadays it is practically possible to develop purely
empirical theories of the motion of celestial bodies
based only on observations (e.g., such theories are suf
ficient to predict lunar–solar eclipses). But the poor
accuracy of such theories and the rather short time
interval of their validity make them noncompetitive as
compared with the dynamical theories of motion that
have arisen since the development of Newtonian
mechanics combined with Newton’s gravitation law.
Newtonian theories of motion of the major planets
and the Moon were purely dynamic with the exception
of some empirical terms introduced for better agree
ment with observations. At the same time, the physical
substance of the gravitation law remained unknown.
The essence of gravitation was explained only by Ein
stein’s general relativity theory. Since then, celestial
mechanics in its broad meaning became relativistic.
Presently, relativistic theories of motion of the major
planets and the Moon without any additive empirical
terms are in complete agreement with observational
data. By updating the abovementioned question by
Poincaré, the aim of relativistic celestial mechanics
can be formulated as the solution of the question
whether the Einstein general relativity theory alone is
sufficient to explain all observed motions of celestial
bodies;
(2) Mathematics of motion, i.e., investigation of
the mathematical characteristics of the solutions of
the differential equations of motion of celestial bodies
(various forms of solution representation, asymptotic
behavior, stability, convergence, etc.). Within this
domain a problem of celestial mechanics is considered
solved if the general solution form and qualitative pic
ture of motion are known. Celestial mechanics of the
18th and 19th centuries has developed in close relation
with the classical branches of mathematics (mathe
matical analysis, higher algebra, differential equa
tions, special functions, and so on). Many results were
obtained at first in solving specific celestial mechanics
problems to be generalized later as purely mathemati
cal results. Many mathematicians of that period made
remarkable contributions to celestial mechanics. No
doubt, celestial mechanics of the 18th–19th centuries
was the most mathematized amongst all natural sci
ences. But along with the evident merits, such early
mathematization had its drawbacks. In particular, due
to the highly developed techniques based on classical
mathematics, new mathematical trends of the
20th century were implemented in celestial mechanics
less efficiently as was done earlier;
(3) Computation of motion, i.e., the actual deter
mination of the quantitative characteristics of motion.
In many natural sciences this subject presents no diffi
culty and is not treated separately. This is not so in
celestial mechanics. For instance, if it is known that
some problem may be solved in the form of a
power/trigonometric series of many variables, then the
actual determination of the necessary number of the
terms of such a series and its summation is not a trivial
problem when the number of terms ranges to hundreds
or even thousands. Numerical integration of the equa
tions of motion of celestial bodies over a long interval
of time is also not a trivial problem. Analytical and
numerical techniques of celestial mechanics have been
permanently improved over the history of celestial
mechanics. In its turn, it was a stimulatory for many
branches of mathematics (the theory of special func
tions, linear algebra, differential equations, theory of
approximation, etc.). Representation of analytical or
numerical solutions of the celestial mechanics equa
tions in the form suitable for actual computation has
always been an independent and complicated task.
Indeed, demands for the accuracy of the celestial
mechanics solutions were always ahead of the time of
the existing technical computational possibilities.
That is why it is no wonder that the first sufficiently
accurate methods of numerical integration of the ordi
nary differential equations have been elaborated just
for application in celestial mechanics problems (high
accuracy integration over very long timeintervals).
The advent of computer facilities in the second half of
the 20th century has resulted in revolutionary changes
both in numerical and analytical techniques of celes
tial mechanics. It is to be noted that the first (special
ized) systems to perform symbolic (analytical) opera
tions by computer were developed in celestial
mechanics. Later on there appeared the universal
methods of numerical integration of the ordinary dif
ferential equations and universal computer algebra
systems (CAS) for symbolic operations. The actual
task became to combine this general software with spe
cific features of celestial mechanics problems. How
ever, these facilities may have negative influences if the
modern supercomputers with their practically unlim
SOLAR SYSTEM RESEARCH Vol. 47 No. 5 2013
CELESTIAL MECHANICS: PAST, PRESENT, FUTURE 349
ited memory and processing speed are used for a too
straightforward approach to solve a problem;
(4) Astronomy of motion, i.e., application of the
mathematical solution to a problem of a specific celes
tial body, comparison with the results of observations,
determination of initial values and parameters of
motion, and precomputation of motion for the
future. By comparing the theoretical (computed) and
observational results, one may make conclusions
about the adequacy of physical and mathematical
models to the observed picture of motion. If this ade
quacy is not satisfactory, the investigation of the prob
lem returns to one of the previous steps (improvement
of the physical model and mathematical solution).
The increase in precision of astronomical observations
is doubtless the main factor stimulating the advance of
celestial mechanics. The use of the highprecision
observations enables one to improve the accuracy of
the computation of the motion of natural and artificial
celestial bodies, increasing the applied role of celestial
mechanics. On the other hand, the comparison
between the computed and the observed characteris
tics of motion permits one to estimate the validity of
the physical model used far beyond the scope of celes
tial mechanics. Over the whole period of its develop
ment there was talk about the completeness of celestial
mechanics. But each time the further increases of the
observational precision have opened new challenges
for celestial mechanics.
In the first three items, celestial mechanics acts as
a fundamental science. The fourth section character
izes celestial mechanics as an applied science,
although eventually just the results of the fourth sec
tion’s investigations (agreement or disagreement with
observations) are crucial for the development of celes
tial mechanics as a whole. Needless to say, this classi
fication of the philosophy of celestial mechanics is
rather conventional, but in general it is a characteristic
for celestial mechanics of the second half of the
20th century.
2.2. Components of Newtonian Celestial Mechanics
As stated above, contemporary celestial mechanics
is relativistic both for its physical basis and highaccu
racy applications. However, in no way does it diminish
the value of Newtonian celestial mechanics as the
mathematical foundation of relativistic celestial
mechanics. Mutually independent components of
Newtonian celestial mechanics are based on the fol
lowing concepts:
(1) Absolute time, i.e., one and the same time inde
pendent of the reference system of its actual measure
ment. A reference system can be intuitively meant as a
laboratory equipped by clocks and some devices to
measure linear spatial quantities (a local physical ref
erence system) or angular quantities at the background
of distant reference celestial objects (a global astro
nomical reference system). Within this concept the
time interval between two events has the same value in
any reference system (invariance of time). More sim
ply, the clock rate does not depend on the velocity of
motion of a clock and its location in the gravitational
field of the celestial bodies;
(2) Absolute space described by the threedimen
sional Euclidean geometry. This space has maximal
homogeneity (no distinguished privileged points) and
maximal isotropy (no distinguished privileged direc
tions). In particular, the distance between two points
has the same value (invariance of length) independent
of the reference system of its actual measurement.
More simply, the linear sizes of a body and the dis
tances between bodies do not depend on the velocity of
motion of bodies and the gravitational field at their
location;
(3) Newtonian mechanics. The first of three basic
laws of Newtonian mechanics is the law of inertia. A
reference system providing its validity is called an iner
tial system. Any reference system moving uniformly
and rectilinearly relative to a given inertial system is
also inertial as well. The laws of Newtonian mechanics
are valid in any inertial system in accordance with
Galileo’s principle of relativity. Mathematically, this
principle manifests itself as the invariance of the equa
tions of Newtonian mechanics (ordinary differential
equations) under the Galilean transformation describ
ing the relationship between two inertial systems in
threedimensional Euclidean space. The abovemen
tioned features of absolute time (homogeneity) and
absolute space (both homogeneity and isotropy)
reflect the characteristics of the inertial systems;
(4) Newton’s law of universal gravitation. Mathe
matically, this law is formulated as the solution of the
linear equation in partial derivatives (Poisson equa
tion) describing the gravitational field of material bod
ies (Newtonian potential). Newtonian equations of
body motion (ordinary differential equations) and
equations of gravitational fields (linear equations in
partial derivatives) are absolutely independent.
The combination of Newton’s law of universal
gravitation and the laws of motion of Newtonian
mechanics within the concepts of absolute time and
absolute space defines the essence of Newtonian
celestial mechanics.
2.3. Classical Problems of Celestial Mechanics
Ranging in increasing order of complexity, the typ
ical problems of Newtonian celestial mechanics are
the twobody problem, the problem of two fixed cen
ters, the restricted threebody problem, the three
body problem and the problem of
n
(
n
> 3) bodies.
(1) The twobody problem is usually treated as the
problem of the motion of two material points mutually
attracted in accordance with Newton’s gravitation law.
Mathematically, this problem is reduced to the one
body problem, i.e., the problem of the motion of a test
particle (a particle of zero mass) in the Newtonian
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SOLAR SYSTEM RESEARCH Vol. 47 No. 5 2013
BRUMBERG
gravitation field of a central body with mass equal to
the sum of the masses of the two original bodies.
Depending on the initial conditions (initial position
and velocity), the test particle can move on an ellipse,
parabola or hyperbola, the central body being located
at the focus of this conic section. Particular (degener
ated) cases are circular motion and rectilinear motion
(this last case involves collision with the central body).
Elliptic motion presents the most important case for
practical applications. The solution of the elliptical
twobody problem is presented most often in one of
the following forms:
(a) the closed form, where the coordinates and
velocity components of the particle are expressed by
the closed expressions in terms of the auxiliary variable
(of the type of arc length), called anomaly and related
with the physical time by the transcendent equation
(in addition to true and eccentric anomalies of classi
cal celestial mechanics, the socalled elliptic anomaly
has recently come into use);
(b) infinite trigonometric series in terms of the
mean anomaly (representing some linear function of
time);
(c) series in powers of time (contrary to the first two
forms the solution in this form is valid generally only
for limited time intervals and just this form is used in
many numerical integration techniques).
Since in the solar system the mass of the Sun
exceeds by three orders of magnitude the total mass of
all of the planets, the twobody problem is an adequate
initial approximation in constructing the theories of
motion of many bodies of the Solar System.
(2) The problem of two fixed centers represents a
purely mathematical model problem of the motion of
a test particle in the gravitational field of two motion
less mutually nonattracting bodies (material points).
This problem admitting the solution in a closed form
(with the aid of elliptic functions) has played an
important role in the development of celestial
mechanics. In the second half of the 20th century, this
problem turned out to be useful in constructing some
theories of the motion of Earth’s artificial satellites.
(3) The restricted threebody problem deals with
the motion of a test particle in the gravitational field of
two mutually attracting bodies (material points). Of
the most interest are the restricted circular threebody
problem with finite mass bodies moving on circular
orbits and the restricted elliptical threebody problem
with finite mass bodies moving on elliptical orbits.
Next to the twobody problem, the restricted circular
threebody problem is the most investigated problem
of celestial mechanics. This problem is incapable of
being solved in the closed form and has always been an
object of application of various techniques of celestial
mechanics. In particular, just this problem stimulated
the development of qualitative techniques of celestial
mechanics (and mathematics generally) aimed to
investigate the features of the solutions without explic
itly obtaining the solutions themselves. In astronomy,
the restricted threebody problem is of great practical
importance in studying the motion of the natural sat
ellites of the planets (in the first instance the motion of
the Moon under the attraction of the Earth and the
Sun), minor planets (motion of asteroids in the field of
the Sun and the Jupiter) and comets. Each of these
cases, i.e., satellite, asteroid and comet, demands its
own specific techniques. Applicability of the restricted
threebody problem goes beyond the solar system,
e.g., to the problem of the existence of the planets
around the massive binary systems.
(4) The threebody problem is mathematically the
best known celestial mechanics problem to study the
motion of three material points under the action of
Newton’s law of gravitation. Many outstanding spe
cialists in celestial mechanics and mathematics have
contributed to its investigation. But the question of
whether or not this problem has been solved may be
both positive and negative. One knows the general
solution of this problem potentially permitting com
putation with known initial values (the positions and
velocities of the bodies at the initial epoch) the posi
tions and velocities of the bodies at any arbitrarily far
moment of time in the past or future (excepting initial
values making possible the triple collision of the bod
ies). But this solution found in 1912 by Finnish math
ematician Sundman in form of the power series in
terms of some auxiliary variable (of the type of an
anomaly of the twobody problem) turned out to be
extremely inefficient for real applications. Contrary to
widespread opinion, the matter does not consist of
only the astronomical number of terms of the Sund
man series required to obtain the result within any
acceptable accuracy. This drawback can be overcome
purely mathematically by replacing the power series by
a more effective series of polynomials. The actual
problem is that this power series form of solution, like
as all numerical integration solutions of the equations
of celestial mechanics, does not permit to have any
insight into the features of the solution. Other tech
niques not claiming to be a general solution of the
threebody problem are more effective in different
particular cases of this problem that are important in
the astronomical respect (the Sun and two planets, the
Sun–Earth–Moon problem, the stellar threebody
problem, etc.). In general, the character of motion in
the threebody problem can be regarded as known suf
ficiently well, enabling one to speak about its solution
rather optimistically. At the same time this problem, as
a purely mathematical problem, continues to be a
challenge to mathematicians and remains open for
further research.
(5) The problem of many bodies, i.e., the problem
of motion of
n
(
n
> 3) material points under the action
of Newton’s law of gravitation. No doubt this is a cen
tral problem of celestial mechanics. One knows in this
problem some rigorous particular solutions, as well as
the main types of motion and a set of theorems of gen
SOLAR SYSTEM RESEARCH Vol. 47 No. 5 2013
CELESTIAL MECHANICS: PAST, PRESENT, FUTURE 351
eral character. When applied to the motion in the
Solar System, this problem is treated as a problem of
motion of (
n
– 1) bodies of small masses and one body
of large mass (the Sun). With such a statement, the
solution of this problem is developed by different tech
niques of subsequent approximations. The
n
body
problem, when all masses are of the same order, is an
example of an unsolved problem of Newtonian celes
tial mechanics.
From the viewpoint of astronomers, the role of
celestial mechanics has been estimated not so much by
its advances in the problem of three or
n
bodies (these
researches have been regarded as more related to
mathematics), as by its efficiency in constructing the
theories of motion of the specific bodies of the Solar
System. One may note several interesting features in
this “astronomical” part of celestial mechanics.
First, there were also a variety of techniques used to
solve a specific problem. Many of these different tech
niques, which are rather sophisticated mathematically,
remained practically unrealized. The fact is that the
construction of a theory of the motion of a specific
celestial body generally demands a great number of
repetitive onetype operations and, consequently, is
very laborintensive of human time. For various rea
sons such a work has not been available for all special
ists in celestial mechanics.
Secondly, throughout the entire period of contem
porary celestial mechanics there has been a competi
tion between analytical and numerical solution tech
niques (between analytical and numerical theories of
motion speaking in terms of final results). This com
petition has often resulted into implacable antagonism
between supporters of these two trends. However,
there should not be any contrast between these trends.
The either/or decision should be replaced by the
option of both. Indeed, the analytical solution of a
celestial mechanics problem retaining all or a part of
the initial values and problem parameters in the literal
form acts as a general solution of the mathematical
problem. A numerical solution where all initial condi
tions and parameters have specific numerical values
represents a particular solution of the mathematical
problem. Both of these types of solutions are used in
contemporary celestial mechanics. They complement
each other and have different purposes. Analytical
theories are necessary in investigating the dependence
of a solution on the change of the initial values and
parameters, in using a given theory in other problems and
in studying the general characteristics of the solution.
Numerical theories are generally more effective in
obtaining the solution of maximum accuracy with spe
cific values for the initial conditions and parameters.
The third feature of the historical development of
celestial mechanics is the permanent search for a com
promise between the form of an analytical solution
and the time interval of the validity of this solution.
Purely theoretically, it was supposed that an ideal con
figuration of an analytical solution is provided by the
trigonometric form with the coordinates and compo
nents of velocity of celestial bodies represented by a
trigonometric series in some linear functions of time.
With application to the problem of the motion of the
major planets of the Solar System, the theory ensuring
such a form that is also valid, at least formally, for an
the infinite time interval has been called the general
planetary theory.
Laplace was the first to propose solving the equa
tions of planetary motion in a trigonometric form, but
technical difficulties of such a solution forced him to
develop another form of planetary theory, which has
since become classic and admits secular and mixed
terms (with respect to time) as well. For the major
planets of the Solar System, the classical theories are
valid for the intervals of the order of several hundred
years. The next attempt to find efficient methods for
constructing the general planetary theory was under
taken by Le Verrier. Not being successful in this direc
tion, Le Verrier developed his famous theories of
motion of the major planets in the form indicated by
Laplace. A mathematical form of the general plane
tary theory was rigorously proved for the first time by
Newcomb in 1876. It is of interest that Newcomb con
sidered his technique to be only an existence theorem
for such a solution, but he actually used the Newton
type quadratic convergence iterations underlying the
contemporary KAM theory (Kolmogorov–Arnold–
Moser theory) concerning the existence and construc
tion of quasiperiodic solutions of the celestial
mechanics equations. At the end of the 19th century
and the beginning of the 20th century, the general
planetary theory was advanced by Dziobek, Poincaré
and Charlier. Gyldén most closely approached the
practical construction of the general planetary theory.
He created therewith his own world of the art of celes
tial mechanics (the theory of periplegmatic orbits).
Finally, Hill, who created several firstclass classic
type planetary theories, considered them as only a
temporary compromise solution until the develop
ment of more efficient methods for constructing the
general planetary theory.
The development of the general planetary theory
continued in the second half of the 20th century. By
this time it became evident that the trigonometric
form of the solution is not efficient because of the great
number of trigonometric terms with practically identi
cal periods (the slow motions of the perihelia and
nodes of the planetary orbits have a small influence on
the periods due to the fast angular variables, i.e., the
mean longitudes of the planets). An alternative form of
the general planetary theory is provided by a normal
izing transformation of the planetary coordinates by
means of the trigonometric series in fast angular vari
ables with the coefficients dependent on slowly chang
ing variables. These slow variables satisfy an autono
mous system of differential equations (the secular sys
tem). With dependence on the analytical form of the
solution of the secular system (including the trigono
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SOLAR SYSTEM RESEARCH Vol. 47 No. 5 2013
BRUMBERG
metric form only as a particular case) one can obtain
different explicit expressions of the final series for the
planetary coordinates. The solution of the secular sys
tem can be found numerically as well, underlying once
again the possibility and feasibility of the combination
of analytical and numerical techniques.
General planetary theory in this form can be
expanded for the rotation of the planets, also resulting
into a unified general theory of the motion and rota
tion of the planets of the Solar System. This theory
avoids the fictitious secular terms inherent in classical
theories of the planetary motion and rotation enabling
one to use it for the time intervals of the order of many
thousands of years at least.
Actual construction of the general planetary theory
being performed in the 70s of the 20th century in the
Institute of Theoretical Astronomy (Leningrad) and
Bureau des Longitudes (Paris) was not developed to
the stage of comparison with observations. Within the
level of the available computation facilities of that time
it was necessary to solve purely technical problems
related to inadequate computer memory, insufficient
processing speed, etc. Today, the solution of this prob
lem that once was a challenge for celestial mechanics
is technically quite feasible. However, there is no
longer any interest in this problem. Even the contem
porary analytical theories of major planets’ motion
and the Earth’s rotation elaborated in the Bureau des
Longitudes by Bretagnon in advancing the theories by
Laplace and Le Verrier give way to numerical theories,
when it comes to practical needs in highaccuracy
ephemerides. In this competition of efficiency
between classical analytical theories and numerical
integration over time intervals of the order of hundreds
of years the general planetary theory is the oddman
out. But for intervals of the order of thousands of years,
the general planetary theory is beyond any competi
tion and thanks to it, one may still hope for its eventual
completion.
Generally speaking, in spite of its completeness
from the viewpoint of physicists, Newtonian celestial
mechanics, even in its classical form, still has many
unsolved and interesting problems. First of all, one
may note that the investigation of the evolution of
motion in the
n
body problem, most particularly in
the general case of comparable masses. Even in the
case of one dominant mass (the case of the Solar Sys
tem), the problem of the presentation of a solution
valid for long time intervals still remains timely. Inter
esting possibilities for compact presentation of the
analytical solutions (e.g., using the compact expan
sions for the elliptic functions) also remain unex
plored. Finally, beyond the model of point masses, the
motion of the nonrigid bodies, taking into account
their proper rotation, represents an immense field of
research. It is true that celestial mechanics nowadays
has lost its former relevance, but this is the general fate
of each science and does not signal the completeness
of the mathematical and astronomical content of
celestial mechanics. It should be noted therewith that
the wellknown expression “the new is the wellfor
gotten old” fully concerns contemporary celestial
mechanics because, very regretfully, many of the tech
niques and results of classical celestial mechanics
obtained still by Laplace, Le Verrier and its other
founders, turned out to be forgotten and are only now
being rediscovered again (sometimes in a worse ver
sion).
2.4. Trends of Contemporary Celestial Mechanics
At present, Newtonian celestial mechanics is char
acterized by two features making it cardinally different
from classical celestial mechanics, i.e., new objects of
research and new types of motion. New objects are
provided by exoplanets (planets beyond the Solar Sys
tem), new families of satellites of the major planets,
and minor planets of the Solar System with orbits
located outside the Neptune orbit (Kuiper belt). The
new types of motion are primarily embrace the chaotic
motions. Some people believe that celestial mechanics
has discovered new horizons, becoming much more
extensive than classical celestial mechanics with its
narrow class of objects (mainly major planets and their
satellites) and deterministic motions. But one forgets
therewith that “new” celestial mechanics takes on the
risk of losing its chief distinguished merit as compared
with all other sciences, i.e., highprecision observa
tions and the high accuracy of its mathematical theo
ries. As a result, celestial mechanics may lose its mean
ing for physics as a tool to verify the physical gravita
tion theories and its stimulating influence for applied
and computational mathematics. Indeed, along with
the exclusive interest of exoplanets for astronomy, it is
unlikely that someday their motion will be observed
and computed with the accuracy characteristic for the
Solar System bodies. Statistical techniques applied in
investigating the motion of exoplanets and Kuiper belt
asteroids have very little in common with classical
celestial mechanics methods. As far as presently pop
ular chaotic celestial mechanics is concerned, it deals
with cosmogony time intervals where there is no case
of observations at all. In terms of deterministic (pre
dictable) and nondeterministic (unpredictable)
motions one may separate three time zones as follows:
(1) predictable near zone (small time intervals of
the order of hundreds of years for the planetary prob
lems) available for using classical planetary theories
with the secular and mixed terms;
(2) predictable intermediate zone (large time inter
vals of the order of thousands of years for the planetary
problems) suitable for using general planetary theory
with separation of the shortperiod and longperiod
terms (with the potential possibility of the purely trig
onometric form);
(3) unpredictable far zone (overlarge time intervals of
the order of millions of years for the planetary problems)
with chaotic motions (in virtue of the KAM theory this
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does not exclude the existence of the deterministic solu
tions of the type of general planetary theory).
Chaotic behavior in dynamical systems is of great
interest in its mathematical arespect. The supporters
of the chaos theory speak about the chaotic state of the
Solar System in the infinite past and infinite future.
Their opponents argue that the very existence of the
mankind enables one to hope for the evolution of the
Solar System within the KAM theory. In any case,
there is no relation to any astronomical observations.
Moreover, this model has little to do with physics. Any
sophistication of the model, e.g., by replacing the
material points with more complicated objects in
Newtonian theory or by replacing the Newtonian
gravitation theory with the general relativity theory, all
the results of the chaos theory may be radically
changed. Therefore, “old” celestial mechanics as an
organic part of mathematics, physics and astronomy
should not be regarded as a science of the past.
The development of any science has been always
accompanied by a conflict of opinions. From the
viewpoint of some physicists, a physical theory that
cannot be confirmed or refuted by experiment (obser
vations) has no interest and cannot be regarded as a
physical theory at all. On the other hand, there are
mathematicians claiming that any mathematical
model is of interest for the natural sciences with no
relation to any experiments. These are two polar view
points. With application to celestial mechanics these
two viewpoints represent not the mutually exclusive
directions, but just different aspects of its methodology
mentioned above.
3. RELATIVISTIC CELESTIAL MECHANICS
3.1. Special Relativity Theory (SRT)
One of the greatest scientific achievements to open
the 20th century was the creation of the special relativ
ity theory by Albert Einstein in 1905. Nowadays, it is
even difficult to imagine the astonishment and admi
ration of the intellectual’s mankind caused by the SRT.
In its further development the 20th century generated
so much novelty into human life (both positively and
negatively), that people seemed to have lost the capa
bility to be surprised by anything. But, in the beginning
of the 20th century, the SRT and the resulting revolu
tionary change of the physical description of the world
was met by mankind in a quite adequate manner.
Indeed, for two preceding centuries, Newtonian
mechanics and the Newtonian gravitation theory had
successfully advanced in the description of the
observed world phenomena and the prediction of
observable effects. Therefore, the concepts of Newto
nian physics seemed to be absolutely true. As it was
mentioned above, these concepts include absolute
time, absolute space, the laws of Newtonian mechan
ics and Newton’s law of universal gravitation.
Newton’s law of universal gravitation and Newto
nian mechanics, within the concepts of absolute time
and absolute space, were fully consistent with to satisfy
the scientific and technical demands of human society
during these two centuries. The difficulties that arose
in the middle of the 19th century resulted in the crisis
of Newtonian physics at the beginning of the 20th cen
tury in attempting to explain the observed data in elec
trodynamics and optics of the moving bodies (Max
well’s electromagnetic theory and wave light theory).
These experimental data have led to the four position
statements:
(1) all points of space and all moments of time are
alike (homogeneity of space and time);
(2) all directions in space are alike (isotropy of
space);
(3) all laws of nature are the same in all inertial ref
erence systems (special principle of relativity);
(4) the velocity of light in a vacuum is the same
constant in all inertial reference systems (postulate of
the constancy of the velocity of light).
The first two statements are common both for
Newtonian mechanics and SRT. The latter two state
ments specific for SRT were formulated in the famous
paper by Einstein “On the electrodynamics of moving
bodies” published in September 1905, in the journal
“Annalen der Physik”.
The adoption of the special principle of relativity
and the postulate of the light velocity constancy dras
tically changed the Newtonian conceptions of space
and time. Instead of threedimensional space and
onedimensional time, SRT deals with a single four
dimensional space–time. The usual Euclidean geom
etry is valid in such a space provided that complemen
tary to three spatial coordinates, a quantity
ict
is added
as a fourth coordinate,
t
being the physical time and
i
being the imaginary unit whose square is equal to –1.
The transformations between two inertial fourdimen
sional reference systems of SRT are called Lorentz
transformations. These transformations generalizing
the Galileo transformations of Newtonian mechanics
reflect mathematically the special principle of relativ
ity. If the Galileo transformations retain invariant a
time interval and a spatial length measured in some
inertial system, then the Lorentz transformations
retain invariant a fourdimensional interval calculated
by Euclidean geometry with the condition indicated
above.
Lorentz transformations involve a set of kinemati
cal consequences that demonstrate the relativity of the
space–time observational data, in dependentce of a
reference system of actual measurements. One should
remember that Lorentz transformations imply that
inertial systems are to be considered as a special class
of all possible systems (justifying the name of SRT).
SRT is now not only a theory experimentally veri
fied in all of its aspects; it represents also a working
theory used in many domains of applied science and
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technology from astronavigation (by means of naviga
tion satellites) to the physics of elementary particles.
In the distant future, described now in science fiction,
SRT might play a major role as a scientific base for
interstellar flights with the use of photon rockets.
Nowadays, there are no explicit opponents of SRT
(although at the present time with the broad activity of
pseudoscience, one can often hear, from time to time,
about sensational “discoveries” claiming to argue
against the postulate of the light velocity constancy).
For Einstein, SRT was of importance not only as a
theory of space and time in the absence of gravitation
but, also, as a starting point to elaborate a theory of
space, time and gravitation. This new theory, com
pleted in 1915 and called general relativity theory, is
the physical foundation for contemporary celestial
mechanics. From a purely operational point of view
general relativity theory extends SRT demonstrating
that all space–time characteristics at the point of
observation in some reference system depend not only
on the velocity of this point but also on the value of the
gravitational potential (and its higher moments) at this
point.
3.2. General Relativity Theory (GRT)
The decade after 1905, when the SRT was created,
was significant. While a large part of Europe was living
in anticipation of the first world war and related social
changes, the scientists (physicists mainly) mastered
the SRT. Einstein, who considered the SRT as the first
step towards a more universal physical theory, tried to
generalize it to include gravitation. In 1915 Einstein
managed to formulate the general relativity theory. His
final summing paper on the foundations of the GRT
was published in 1916.
Some physicists believe that it might currently be
possible to develop the main idea of the GRT just from
experimental results. Yet Einstein derived the basic
statements of the GRT by purely logical consider
ations proceeding from the SRT and the fundamental
law of equality of gravitational and inertial mass.
Having completed the SRT, Einstein successfully
put forward the principle of equivalence and the prin
ciple of general covariance. According to the principle
of equivalence, all physical processes follow the same
pattern both in an inertial system under the action of
the homogeneous gravitational field and in a non
inertial uniformly accelerated system in the absence of
gravitation. The principle of equivalence is strictly
local in contrast to the law of identity of the gravita
tional and inertial mass underlying it. The principle of
general covariance, being of a purely mathematical
character, implies that equations of physics should
have the same form in all reference systems, i.e., all
systems should be equivalent. Combination of these
two principles enabled Einstein to formulate the prin
ciple of general relativity as a generalization of the spe
cial principle of relativity.
Following this, Einstein came to the conclusion
that in the presence of gravitation, the space–time
relations correspond not to the flat (Euclidean) four
dimensional space of events of the SRT, but to a curved
(Riemannian) space. The curvature of the space is
caused by the presence of the gravitatingional masses.
The most important characteristic of the Riemannian
space is its metric, i.e., the square of the infinitely
small fourdimensional distance between two points of
this space. According to the basic idea of the GRT, the
properties of space and time, i.e., the space–time met
ric, are determined by the motion and distribution of
masses and, conversely, the motion and distribution of
masses are governed by the field metric. This interrela
tion is revealed in the field equations for determining
the metric coefficients in terms of the gravitating
masses. The equations for the motion of mass and the
light propagation of light follow from the field equa
tions.
The GRT is distinguished by its logical simplicity
and perfection. Newton’s gravitation theory consists
of four mutually independent parts with their own
postulates (absolute time, absolute space, Newtonian
mechanics laws, Newton’s law of universal gravita
tion) giving therewith no physical explanation of grav
itation. GRT is based on the field equations written in
the covariant form valid for any reference systems. The
SRT permits one, if desirable, to write all equations in
the covariant form and to use any reference systems.
But the space–time of the SRT represents the flat
Euclidean space (without curvature) admitting the
existence of privileged distinguished systems (inertial
systems) defined up to the Lorentz transformation.
The corresponding mathematical coordinates of these
systems are called Galilean. Physically, they are ade
quate for time and three spatial coordinates. There are
no Galilean coordinates in the GRT. But the GRT
admits the quasiGalilean coordinates. In terms of
these coordinates, the Riemannian metric of the GRT
differs little from the Euclidean metric of the SRT.
However, this distinction caused by the gravitating
masses looks different for each reference system.
Moreover, at every point of the GRT space–time, one
may introduce the socalled local geodesic coordi
nates such that in the infinitesimal region of the given
point one has (in neglecting by the small quantities of
at least of second order) the SRT space–time. All SRT
relations will be valid in this infinitesimal region. This
possibility of introducing the local geodesic coordi
nates is due to the principle of equivalence valid only
locally.
The most amazing fact in the history of the creation
of the GRT creation is the absence of any experimen
tal reasons. A new physical theory often arises when an
old theory comes into contradiction with the corre
sponding experimental data. There was nothing of the
kind in the case of the GRT. Indeed, even since the
second half of the 19th century, one knew the disagree
ment between the observed value of the secular
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advance of the perihelion of the orbit of Mercury and
its theoretical value calculated by the Newtonian the
ory of its motion. But it has not bothered physicists,
especially as there were some other (less significant)
disagreements in the problem of the major planets
motion, e.g., in the motion of the perihelion of Mars
and in the motion of the node of Venus (only in the
middle of the 20th century a more rigorous analysis of
observations removed these disagreements). There
fore, when in 1916, Schwarzschild derived a rigorous
solution for the GRT motion of Mercury in the gravi
tational field of the Sun and obtained the missing cor
rection contribution to the Newtonian value, this first
experimental confirmation of GRT seemed rather
unexpected. On the other hand, the test of the effect of
the deflection of light in the Sun’s gravitational field,
predicted by Einstein, was greatly anticipated. The
observation performed during the total solar eclipse on
May 29, 1919, confirmed this effect. Quite reasonably,
it was regarded as a triumph for the GRT.
Not stopping at the laboratory experiments on
measuring the GRT effect in spectroscopy (mainly
the Mössbauer effect), let’s consider the “global”
applications of the GRT in astronomy. In fact, the
origin of the GRT has led to three new domains of
astronomy, i.e.,
(1) relativistic cosmology;
(2) relativistic astrophysics;
(3) relativistic celestial mechanics.
The most significant astronomical prediction of
GRT is doubtless the theory of the expanding universe
developed by A.A. Friedmann on the basis of the solu
tion of the Einstein equations. The phenomenon of
the expanding universe was discovered from observa
tions in 1929. Relativistic cosmology nowadays pre
sents an intensively developing branch of astronomy
based on the GRT, on the one hand, and on the vast
quantities of observational data, on the other hand.
As far as astrophysics is concerned, the GRT
enables one to analyze phenomena completely incon
sistent with Newtonian theory. Two examples are
characteristic. The GRT predicts the existence of
qualitatively new objects, e.g., the black holes with
such a strong gravitational field that no emission can
escape into the external space. The GRT has permit
ted the accurate computation of the binary pulsar
motion (as a problem of relativistic celestial mechan
ics). Binary pulsar observations confirmed the GRT
conclusion about the loss of binary system energy due
to gravitational radiation. The coincidence of the the
oretical and observational results relative to the binary
pulsar systems demonstrates implicitly the existence of
the gravitational waves predicted by the GRT,
although so far there are no direct results from the
gravitational wave detectors.
In general, the GRT plays quite an extraordinary
role for celestial mechanics. Relativistic celestial
mechanics does not deal with such impressive and
unusual events as intrinsic to cosmology and astro
physics. However, relativistic celestial mechanics has
one irrefutable merit, i.e., its exceptionally high preci
sion of observations absolutely unattainable in cos
mology and astrophysics. Just this feature makes
celestial mechanics and the related astrometry so
important in verifying the effects of the GRT. Para
phrasing the wellknown saying by Poincaré concern
ing Newtonian celestial mechanics, the final goal of
relativistic celestial mechanics is to answer the ques
tion whether GRT alone is capable of explaining all
observed motions of celestial bodies and the propaga
tion of light. Currently, celestial mechanics answers
this question positively. GRT is used therewith not
only as a theoretical basis of celestial mechanics, but
also as a working framework for increasing the accu
racy of celestial mechanics and astrometry solutions.
The problem of the comparison of the theoretical and
observational data is here of fundamentally new prin
cipal novelty as compared with Newtonian astronomy.
In Newtonian astronomy this problem is simply solved
by introducing the inertial systems with all quantities
having physical meaning. In relativistic astronomy the
solution of the equations of the motion of bodies and
the light propagation depends on the employed four
dimensional quasiGalilean coordinates close to the
SRT Galilean coordinates (only the most significant
secular effects such as the Mercury perihelion advance
of Mercury and the angle of the light deflection near
the solar limb do not depend on these coordinate con
ditions). Comparison of theoretical and experimental
data is based on the description of the observational
procedure (by means of the equations of the light
propagation) in the same space–time as is used for the
presentation of the motion of the bodies, enabling one
to exclude eventually all nonphysical immeasurable
quantities characteristic of Newtonian mechanics
(distances, coordinates, etc.). The contemporary the
ories of motion of the major planets of the Solar Sys
tem, lunar motion and the Earth’s rotation have been
developed in the GRT framework. The space astron
omy projects planned for the first quarter of the
21th century and designed for the observational preci
sion of one microarcsecond in the mutual angular dis
tances between celestial objects demand the intensive
use of the GRT analysis of observations.
3.3. Relativistic Celestial Mechanics and Astrometry
As indicated above, relativistic celestial mechanics
represents a science to study the motion of celestial
bodies within the framework of the GRT. Just this
change of the physical basis (GRT instead of Newto
nian mechanics and Newton’s gravitation law) speci
fies the qualitative difference between relativistic and
Newtonian celestial mechanics. But from purely the
operational point of view, i.e., in obtaining the practi
cal results to be compared with observational data
(within the domain “astronomy of motion” according
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to our classification) the difference between relativis
tic and Newtonian treatment of the problem of celes
tial bodies’ motion is revealed in two aspects, as fol
lows:
(1) mathematically, i.e., the difference in the equa
tions of the gravitational field and in the equations of
motion of bodies resulting in the differences in the
solutions of these equations (this is the object of rela
tivistic celestial mechanics in the narrow meaning of
the phrase);
(2) physically, i.e., the difference in the manners to
compare the calculated and observed data and in the
reduction itself of the calculated data to the measur
able quantities (the object of relativistic astrometry as
a part of relativistic celestial mechanics in the broad
sense).
The mathematical distinction is not essentially new
for celestial mechanics. Even in Newtonian celestial
mechanics all actually important problems beyond the
scope of the twobody problem cannot be solved in the
closed form, which demands the application of the
method of consecutive approximations (iterations) for
their approximate solution. Indeed, in Newtonian
celestial mechanics, the equations of motion of the
bodies can be formulated rigorously and only their
solution is to be found by approximations. In relativis
tic celestial mechanics only the equations of the one
body problem can be formulated rigorously. A good
example is provided by the Schwarzschild problem
dealing with the motion of a test particle in the spher
ically symmetrical gravitational field of one body. In
all more complicated cases, even for the problem of
the motion of two bodies of finite mass, the equations
of motion may be derived only in an approximate
form. It does not signify a significant obstruction in
practical work since, in any case, these equations can
be solved only by iterations, but this distinction is of
importance for theoretical studies. The theoretical
distinction between the solutions of the Newtonian
problem and its relativistic counterpart can be seen
even in the simplest case of the onebody problem. In
the Newtonian case (Kepler problem) the solution is
described by means of three linear parameters charac
terizing the size of the orbit (semimajor axis), its form
(eccentricity) and its positions in the space (inclina
tion), as well as by means of three angular parameters
determining the position of a moving particle in orbit
(anomaly or longitude), orientation of the orbit in the
plane of motion (longitude of the pericenter) and in
space (longitude of the node). Only the first of these
angular parameters varies in time whereas the two
other parameters remain constant (degenerate case).
In the relativistic case (Schwarzschild problem), not
only the first angular parameter, but also the second
one varies in time (this feature is used in the relativistic
discussion of observations of binary pulsars). In more
complicated problems, this distinction is not signifi
cant because all three angular quantities generalizing
the angular parameters of the onebody problem vary
in time. In the practical case of the motion of the Solar
System bodies, the smallness of the relativistic terms
with respect to the Newtonian terms is characterized
by a small parameter of the order
v
2
/
c
2
. With
v
being
the characteristic velocity of the motion of the bodies
(30 km/s in case of the motion of the Earth around the
Sun) and
c
being the velocity of light in vacuum
(300000 km/s) it gives the order 10
–8
for this parame
ter. For Solar System dynamics, it is generally suffi
cient to know these relativistic equations of motion
and their solutions with taking into account only the
firstorder terms with respect to this parameter (post
Newtonian approximation). Even within the second
order of accuracy with respect to this parameter (post
postNewtonian approximation) the solution of the
actual problems in the GRT framework is certainly
more complicated than in the Newtonian case, but
there are no qualitative distinctions. The significant
difference between Newtonian problems of motion
and the GRT problems of motion is revealed when the
terms of the order
v
5
/
c
5
are taken into account (an
approximation following the postpostNewtonian
one). This approximation involves the gravitational
radiation from the system of bodies resulting in the loss
of the energy in the system. The evolution of the sys
tem in this case qualitatively differs from the Newto
nian case. This approximation is not needed for the
Solar System dynamics. But, as mentioned above, just
this approximation applied to the binary pulsar
motion has enabled one to prove indirectly the exist
ence of the gravitational waves.
Any solution of the GRT equations of motion of
celestial bodies by itself has nothing to do with the real
relativistic effects valid for comparison with observa
tions. Contrary to the inertial coordinates of Newto
nian mechanics and SRT, no GRT coordinates for
finite (noninfinitesimal) domain of the space–time
have physical meaning and can be directly compared
with observational data. The solutions of the equations
of motion in different coordinates are inevitably dif
ferent from each other. This is in no way a drawback of
the GRT, as was sometimes believed by its opponents.
It is simply a demonstration that relativistic four
dimensional coordinates are nothing more than a con
venient mathematical tool to obtain a purely mathe
matical solution. That is why the problem of compar
ing the theoretical and observed data is so important
for contemporary relativistic astronomy. There is no
such problem in Newtonian mechanics or SRT since
the introduction of the inertial coordinates from the
very start or at the final step (if a solution was derived
in some curvilinear coordinates) immediately results
into the solution in terms of the measurable quantities.
In principle, there are three main possibilities for
solving the problem to compare the theoretical and
observed data:
(1) Eliminate coordinates completely by con
structing the solutions for motion of Solar System
bodies motion in terms of measurable quantities;
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(2) to use any welldefined coordinates mathemat
ically suitable for a specific problem potentially solv
ing the equations of the light propagation in the same
coordinates, enabling one to combine the solution of
the dynamical problem (body motion) and the solu
tion of the kinematic problem (light propagation) to
obtain the coordinateindependent quantities;
(3) for treating the actual problems directly or indi
rectly related with observations to use one specific type
of coordinate conditions adopted by some conven
tional agreements.
The first approach that might be tentatively consid
ered physical is often used in physical studies on local
GRT effects (in a sufficiently small space–time
region). Theoretical physicists have developed the
techniques potentially adequate for global astronomi
cal problems as well, but so far they have not found
application in astronomical practice. Nevertheless, it
should be noted that the antique (purely kinematical)
planetary theory by Ptolemaeus was constructed just
in terms of measurable quantities (mutual angular dis
tances between celestial bodies).
The second approach is rather mathematical, giv
ing primary consideration to how well different coor
dinates are suitable for the mathematical solution of
dynamical problems. Very regretfully, within this
approach one sometimes forgets the necessity of
reducing the employed coordinates to measurable
quantities. However, for the study of theoretical prob
lems of relativistic celestial mechanics, this approach
is the most flexible.
The third approach, widely used nowadays in prac
tical astronomy, is to avoid deliberately the GRT arbi
trariness in coordinate conditions for the sake of prag
matic simplicity. Positional astronomy deals with a set
of observational results obtained by different observers
at different moments of time rather than with a single
result at one space–time point. In discussing the
observations one has to use also the theoretical results
relating to the body motion (dynamical problem) and
light propagation (kinematic problem). For astronom
ical applications, there is no difference, which coordi
nates are used in these problems. However, it is very
important that both problems be treated in the same
coordinates. For the sake of actual convenience, the
specific coordinate option is used by the resolutions of
the International Astronomical Union (IAU). But in
so doing there is a danger of the too straightforward
“engineering” application of GRT in celestial
mechanics. The immense theoretical potentialities of
GRT are substituted therewith by a narrow set of prac
tical recipes adopted by IAU.
The coordinate method in relativistic celestial
mechanics is realized by means of fourdimensional
reference systems (three spatial coordinates and one
time coordinate). A reference system (RS) represents
a purely mathematical construction to facilitate math
ematical solution of astronomical problems. The rela
tionship between the fourdimensional coordinates
and the coordinateindependent measurable quanti
ti es ( int erval s of the proper tim e of an o bse rver, an gul ar
distances between celestial bodies reduced to the infi
nitely far distance, etc.) is determined by formulating
an observational procedure with the aid of the light
propagation solution found in the same RS. For exam
ple, as already mentioned, in the Solar System bary
centric RS, the relativistic terms in the equations of
body motion are of the order 10
–8
with respect to the
Newtonian terms. In introducing a relativistic geocen
tric RS where the Earth is the main attracting body
and the action of all other celestial bodies (the Sun, the
Moon, the major planets) is revealed only in the form
of the tidal force terms, then the ratio of the GRT
terms to the Newtonian ones will be less by two orders
of magnitude. Moreover, all parameters characterizing
the Earth (nonspherical figure of the Earth, angular
velocity of the axial rotation of the Earth, and so on),
will be, in the geocentric RS, in much better corre
spondence with the measurable quantities than in the
barycentric RS. Therefore, the problems such as the
motion of the Earth’s artificial satellites or the rotation
of the Earth are better examined in a more adequate
geocentric RS. Similarly, in investigating the motion
of a celestial body in the vicinity of any planet it is rea
sonable to use the corresponding planetocentric RS.
The fourth coordinate of such relativistic systems rep
resents the scale of the corresponding coordinate time
(barycentric or geocentric or planetocentric time),
used as an argument in the corresponding theories of
motion or rotation. Relativistic transformations gen
eralizing the Lorentz transformations of the SRT
enable one to reduce the fourdimensional coordi
nates of these systems (including the coordinate time)
to measurable quantities.
Practical realization of RSs (“materialization”) is
realized in astronomy by attributing the coordinate
values to some reference astronomical objects. In such
a way, the RS as mathematical construction is trans
formed to an astronomical reference frame (RF). In
modern positional astronomy two RFs are constantly
maintained, International Celestial Reference Frame
(ICRF) and International Terrestrial Reference
Frame (ITRF). The first RF is given by the positions
of quasars in the International Celestial Reference
System (ICRS), representing a specific barycentric
RS. The second RF is given by the positions of the
ground reference stations in the International Terres
trial Reference System (ITRS), representing a specific
geocentric RS rotating with the Earth. The relation
ship between these systems is derived theoretically
from solving the GRT Earth’s rotation equations, on
the one hand, and is determined from observations, on
the other hand. The absence of any discrepancies
between these data can be regarded presently as one more
convincing verification of the GRT in astronomy.
The present highlyaccurate theories of motion of
the major planets and the Moon, as well as the Earth’s
rotation theory have been constructed with account
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ing for the main relativistic terms (postNewtonian
approximation). The agreement of these theories with
observations enables one to conclude that currently
the GRT completely satisfies the available observa
tional data. It should be noted that the discussion of
observations performed now in many institutions
involves also the determination of the parameters of
the alternate gravitation theories competing with GRT
(postNewtonian formalism). This discussion demon
strates that there are no data now demanding for
inclusion of any empirical parameters to the GRT
framework as a physical basis of relativistic celestial
mechanics.
Relativistic celestial mechanics is a rather young
science with many problems waiting to be solved. In
addition to the problems of Newtonian celestial
mechanics requiring a relativistic generalization in a
postNewtonian approximation (sufficient for the
most actual applications), there are specific problems
of great theoretical interest, such as the investigation
of the general form of the GRT equations of motion,
orbital evolution under the gravitational radiation, the
general relativistic treatment of the body rotation, the
motion of bodies in the background of the expanding
universe (combination of the solar system dynamics
and cosmology problem), and many other problems.
Relativistic celestial mechanics is awaiting its new
researchers.
One should not forget therewith that being based
physically on the GRT, relativistic celestial mechanics
mathematically is based on Newtonian celestial
mechanics with its extensive abundance of mathemat
ical techniques. Disregarding this inheritance and the
present trend of some physicists, astronomers and
space dynamics specialists to treat relativistic celestial
mechanics aside from Newtonian celestial mechanics
may negatively affect the whole level of celestial
mechanics.
4. CONCLUSION
Investigation of the Solar System has been always,
and hopefully will be long further in the focus of celes
tial mechanics for a long time. Just in this investigation
one has the synthesis of highprecision observations,
the most sophisticated mathematical techniques
(numerical and analytical ones), and physical theories
of gravitation, space and time. The performed analysis
of the tendencies and problems of celestial mechanics
(already solved or still waiting to be solved) is aimed at
attracting the attention to the present goals of celestial
mechanics. For the first time in the author’s practice
this paper contains no formulas. In mathematical lan
guage, much of the above can be found in the latest
papers of the author indicated in the References.
REFERENCES
Brumberg, V.A., Relativistic celestial mechanics on the
verge of its 100 year anniversary (Brouwer Award lec
ture),
Celest. Mech. Dyn. Astron.,
2010, vol. 106,
pp. 209–234.
Brumberg, V.A. and Ivanova, T.V., On constructing the gen
eral Earth’s rotation theory,
Celest. Mech. Dyn. Astron.
,
2011, vol. 109, pp. 385–408.
... This means that the principle of equivalence flowing of all the physical processes that apply to any inertial system in the space of events in the SRT, in the space of events in the GRT is valid only locally. Therefore, the solutions of the equations in the space of events in the GRT inevitably differ from each other in different coordinate systems, and, therefore, no GRT coordinates for finite (not infinitesimal) regions of space-time have no physical meaning and, in such a way, can not be compared with observational data [1]. In the special theory of relativity, as in Newtonian mechanics, this problem of comparison the observational and theoretical data does not exist, since the use of inertial coordinate systems from the beginning as a baseline, or go to him in the final stage of processing observational data obtained in GR coordinates, automatically gives a solution to the equations of time-space directly in terms of the measured quantities. ...
... Although the framework of general relativity all the CS equivalent, to solve a specific problem, there are astronomical more preferred or less preferred CS. For example, if from the barycentric CS with the beginning of the spatial axes in the center of mass of the Solar System go to the relativistic geocentric CS with the beginning of the spatial axes in the center of mass of the Earth, where the main attracting body is the Earth, while the effect of all other heavenly bodies (Sun, Moon, planets) appears only in the form of tidal forces, so the contribution of the relativistic components is two orders of less [1]. Earth parameters, which are determined by the ratio 22 / Vc (non-spherical shape of the Earth, Earth's angular velocity, etc.), in the geocentric CS are closer to the measured values than in the barycentric CS. ...
... The basis of the choice of coordinate methods for constructing theories of the motion of celestial bodies in GRT puts the mathematical approach, taking into account the convenience of the various coordinates for purely mathematical solving of dynamic task, adopted, for example, in the calculation of the coordinates in the equations of planetary ephemeris of the Solar System [2]. The subsequent transition from ephemeris coordinates to the coordinate-independent physically measured values is achieved by combination of solutions of the dynamic task (the motion of bodies) and the kinematic task (propagation of light) in the same coordinates [1]. To comply with the principle of equivalence is only important that both tasks have to be solved in the same coordinates. ...
We obtain the es – as series of simultaneous and joint rotational motions of the planets. Copernicus (1473-1543 analytical coordinate-independent pulsar time scales, which are determined by the observed rotation parameters of pulsar. The scales extent into barycentric and any topocentric coordinate systems, providing simultaneity of the observed physical phenomena, including the periodic radiation of a pulsar as well, in any point of the three-dimensional space.
... We are interesting in discovering the way that past, present, and future can be studied via mathematical models. Compare with [4]. Hence we proposed the following question. ...
... Since w ′′ (t) = L(w) and L(0) = 0, we conclude that w (2) j (0) = 0 for 1 ≤ j ≤ n. We use (66) and (71) to deduce that w (4) j (0) = 0 for 1 ≤ j ≤ n. Then (67) implies that w (6) j (0) = 0 for 1 ≤ j ≤ n. ...
Newton’s equations of celestial mechanics for the N-body problem possess a continuum of solutions in which the future trajectories are a perfect reflection of their past. These solutions evolve from zero initial velocities of the N bodies. Consequently, the future gravitational forces acting on the N bodies are also a perfect reflection of their past. The proof is carried out via Taylor series expansions.
... In the very accurate review paper in Ref. [44], the author stresses that relativistic celestial mechanics has one irrefutable merit, i.e., its exceptionally high precision of observations absolutely unattainable in cosmology and astrophysics. In his opinion, with which we agree, the final goal of relativistic celestial mechanics is to answer the question whether general relativity alone is able of accounting for all observed motions of celestial bodies and the propagation of light. ...
... In his opinion, with which we agree, the final goal of relativistic celestial mechanics is to answer the question whether general relativity alone is able of accounting for all observed motions of celestial bodies and the propagation of light. The work in Ref. [44] lists eventually the following major tasks of relativistic celestial mechanics in the years to come: the investigation of general relativistic equations of motion, orbital evolution with emission of gravitational radiation, general relativistic treatment of body rotation, and the motion of bodies in the background of the expanding universe. ...
Towards the end of nineteenth century, Celestial Mechanics provided the most powerful tools to test Newtonian gravity in the solar system, and led also to the discovery of chaos in modern science. Nowadays, in light of general relativity, Celestial Mechanics leads to a new perspective on the motion of satellites and planets. The reader is here introduced to the modern formulation of the problem of motion, following what the leaders in the field have been teaching since the nineties. In particular, the use of a global chart for the overall dynamics of N bodies and N local charts describing the internal dynamics of each body. The next logical step studies in detail how to split the N-body problem into two sub-problems concerning the internal and external dynamics, how to achieve the effacement properties that would allow a decoupling of the two sub-problems, how to define external-potential-effacing coordinates and how to generalize the Newtonian multipole and tidal moments. The review paper ends with an assessment of the nonlocal equations of motion obtained within such a framework, a description of the modifications induced by general relativity of the theoretical analysis of the Newtonian three-body problem, and a mention of the potentialities of the analysis of solar-system metric data carried out with the Planetary Ephemeris Program.
... In the very accurate review paper in Ref. [44], the author stresses that relativistic celestial mechanics has one irrefutable merit, i.e., its exceptionally high precision of observations absolutely unattainable in cosmology and astrophysics. In his opinion, with which we agree, the final goal of relativistic celestial mechanics is to answer the question whether general relativity alone is able of accounting for all observed motions of celestial bodies and the propagation of light. ...
... In his opinion, with which we agree, the final goal of relativistic celestial mechanics is to answer the question whether general relativity alone is able of accounting for all observed motions of celestial bodies and the propagation of light. The work in Ref. [44] lists eventually the following major tasks of relativistic celestial mechanics in the years to come: the investigation of general relativistic equations of motion, orbital evolution with emission of gravitational radiation, general relativistic treatment of body rotation, and the motion of bodies in the background of the expanding universe. ...
Towards the end of nineteenth century, Celestial Mechanics provided the most powerful tools to test Newtonian gravity in the solar system and also led to the discovery of chaos in modern science. Nowadays, in light of general relativity, Celestial Mechanics leads to a new perspective on the motion of satellites and planets. The reader is here introduced to the modern formulation of the problem of motion, following what the leaders in the field have been teaching since the nineties, in particular, the use of a global chart for the overall dynamics of N bodies and N local charts describing the internal dynamics of each body. The next logical step studies in detail how to split the N-body problem into two sub-problems concerning the internal and external dynamics, how to achieve the effacement properties that would allow a decoupling of the two sub-problems, how to define external-potential-effacing coordinates and how to generalize the Newtonian multipole and tidal moments. The review paper ends with an assessment of the nonlocal equations of motion obtained within such a framework, a description of the modifications induced by general relativity on the theoretical analysis of the Newtonian three-body problem, and a mention of the potentialities of the analysis of solar-system metric data carried out with the Planetary Ephemeris Program.
... This work is also a contribution to our interest in past present and future of the universe. Compare with [4] . A perturbed system of equations of the N body problem is also considered. ...
Newton's equations of celestial mechanics are shown to possess a continuum of solutions in which the future trajectories of the N bodies are a perfect reflection of their past. These solutions evolve from zero initial velocities of the N bodies. Consequently, the future gravitational forces acting on the N bodies are also a perfect reflection of their past. The proof is carried out via Taylor series expansions. A perturbed system of equations of the N body problem is also considered. All real valued solutions of this perturbed system have no singularities on the real line. The perturbed system is shown to have a continuum of solutions that possess symmetry where the future velocities of the N bodies are a perfect reflection of their past. The positions and accelerations of the N bodies are then odd functions of the time. All N bodies then evolve from one location in space.
... Were applied, and studied the influence of their disturbances on the satellite orbital elements of multiple periods of prograde and retrograde satellite orbits Movement of orbital elements toward and against the Earth's rotation (Cornish 2008). Celestial Mechanics transaction with the orbital and rotational movement of celestial bodies (Brumberg 2013) The dynamics of stellar systems, the movement of stars within galaxies, the dynamics of planetary systems. This study will concentrate on the orbital movement of artificial satellites around the Earth (Beutler 2005). ...
Researching and modeling perturbations is essential in astrodynamics because it gives information on the deviations from the satellite's normal, idealized, or unperturbed motion. Examined the impact of non-conservative atmospheric drag and orbital elements of low-earth-orbit satellites under low solar activity. The study is consisting of parts, the first looks at the effects of atmospheric drag on LEO satellites different area to mass ratios, and the second looks at different inclination values. Modeling the impacts of perturbation is included in each section, and the final portion determines the effects of atmospheric drag at various node values. The simulation was run using the Celestial Mechanics software system's SATORB module (Beutler, 2005), which solves the perturbation equations via numerical integration. The findings were examined using Matlab 2012. Conclusion that the impacts are stronger for retrograde orbits, which is due to the fact that the satellite moves in the opposite direction. The atmospheric drag effects for all orbital elements were increased by increasing the area to mass ratio. When the node value rises, the size parameter changes slightly, but the other orbital elements change. At varying inclinations, it is found that the changes in orbital elements due to atmospheric drug.
... The subsequent transition from ephemeris coordinates to the coordinate-independent physically measured values is achieved by combination of solutions of the dynamic task (the motion of bodies) and the kinematic task (propagation of light) in the same coordinates. To comply with the principle of equivalence is only important that both tasks have to be solved in the same coordinates [12]. ...
... But this solution is so complicated and the series obtained converge so slowly that it is useless for real applications. In case of four and more interacting particles the problem is even more complicated and this stimulates development of different approximate analytical and numerical methods for its investigation (see [4,5]). ...
We discuss here the problem of solving the system of two nonlinear algebraic equations determining the relative equilibrium positions in the planar circular restricted four-body problem formulated on the basis of the Euler collinear solution of the three-body problem. The system contains two parameters , and all its solutions coincide with the corresponding solutions in the three-body problem if one of the parameters equals to zero. For small values of one parameter the solutions are found in the form of power series in terms of this parameter, and they are used for separation of different solutions and choosing the starting point in the numerical procedure for the search of equilibria. Combining symbolic and numerical computation, we found all the equilibrium positions and proved that there are 18 different equilibrium configurations of the system for any reasonable values of the two system parameters , . All relevant symbolic and numerical calculations are performed with the aid of the computer algebra system Wolfram Mathematica.
... Before proceeding further, it is advisable to briefly review some basic features of the confrontation between theory and observations in Relativistic Celestial Mechanics (RCM; Brumberg 2010b, 2010a; Kopeikin, Efroimsky & Kaplan 2011;Brumberg 2013). Such a task implies solving not only the dynamics of the specific problem at hand, i.e. the equations of motion of the massive bodies involved, but also the equations of propagation of the electromagnetic waves and the description of the observational procedures (the kinematical part of RCM). ...
We analytically calculate the time series for the perturbations induced by a general disturbing acceleration on the mutual range ρ and range-rate of two test particles A, B orbiting the same spinning body. We apply it to the general relativistic Lense-Thirring effect, due to the primary’s spin , and the classical perturbation arising from its quadrupole mass moment J2 for arbitrary orbital geometries and orientation of the source’s symmetry axis . The Earth-Mercury range and range-rate are nominally affected by the Sun’s gravitomagnetic field to the 10 m, 10⁻³ cm s⁻¹ level, respectively, during the extended phase (2026-2028) of the forthcoming BepiColombo mission to Mercury whose expected tracking accuracy is of the order of ≃ 0.1 m, 2 × 10⁻⁴ cm s⁻¹. The competing signatures due to the solar quadrupole , if modelled at the level of the latest planetary ephemerides INPOP17a, are nearly 10 times smaller than the relativistic gravitomagnetic effects. The position and velocity vectors of Mercury and Earth are changed by the solar Lense-Thirring effect by about 10 m, 1.5 m and 10⁻³ cm s⁻¹, 10⁻⁵ cm s⁻¹, respectively, over 2 yr; neglecting such shifts may have an impact on long-term integrations of the inner solar system dynamics over ∼Gyr timescales.
As we are now approaching 2015, both the General Relativity Theory (GRT) and the relativistic Celestial Mechanics based on it will soon arrive at their 100 year anniversaries. There is no border between Newtonian and relativistic Celestial Mechanics. The five-decade period of intensive development of Celestial Mechanics in the second half of the 20th century left many interesting techniques and problems uncompleted. This lecture reviews some problems of Newtonian and relativistic Celestial Mechanics worthy of further investigation. Concerning Newtonian mechanics, these problems include general solution of the three-body problem by means of the series of polynomials, construction of the short-term and long-term theories of motion using the fast converging elliptic function expansions, and representation of the rotation of the planets in the form compatible with the General Planetary Theory reducing the problem to the combined secular system for translatory motion and rotation. Relativistic problems considered here include the determination of the main relativistic effects in the motion of a satellite, e.g. the Moon, and in the rotation of the primary planet using the Newtonian theories of motion and rotation combined with the relativistic transformation of the reference systems, the use of the linearized weak-field GRT metric as a basis of relativistic Celestial Mechanics in the post-Newtonian approximation, and the motion of the Solar System bodies at the cosmological background in the framework of the basic cosmological models. The exposition of the chosen relativistic problems is preceded by reminding the basic features of relativistic Celestial Mechanics with discussing some present tendencies concerning the Parametrized Post-Newtonian formalism, International Astronomical Union resolutions, and standardization of the GRT routines.
In the present paper the equations of the orbital motion of the major planets and the Moon and the equations of the three–axial rigid Earth’s rotation in Euler parameters are reduced to the secular system describing the evolution of the planetary and lunar orbits (independent of the Earth’s rotation) and the evolution of the Earth’s rotation (depending on the planetary and lunar evolution). Hence, the theory of the Earth’s rotation can be presented by means of the series in powers of the evolutionary variables with quasi-periodic coefficients with respect to the planetary–lunar mean longitudes. This form of the Earth’s rotation problem is compatible with the general planetary theory involving the separation of the short–period and long–period variables and avoiding the appearance of the non–physical secular terms. KeywordsEarth’s rotation theory–Euler parameters–Secular system–General planetary theory

