Chapter I
Introduction
The first chapter is devoted to simple and explicit examples of dynamical systems
that illustrate some concepts and help to ask the appropriate questions. For sim-
plicity, the systems under consideration are discrete and hence given by mappings
acting on sets. The aim is to study the behavior of points under all iterates of a map
(orbits of the points) and also to see what happens under perturbation of a map.
A dynamical system consisting of a continuous map acting on a topological space
is called transitive, if it possesses a dense orbit. The transitivity of a system will
be guaranteed by the criterion of G. Birkhoff. An example of such a system is the
rigid irrational rotation of the unit circle where every orbit of the system is dense
on the circle. This example will lead us to the equidistribution (mod 1) theorem of
H. Weyl. In sharp contrast to the stable systems of rigid rotations, a simple expan-
sive map on the circle shows already a quite chaotic behavior described by the shift
map in a sequence space. In this example, orbits of completely different behavior
over a long-time interval (many iterates) coexist side by side. In the language of
physics, the system shows a sensitive dependence on the initial conditions. It is a
typical phenomenon that such an unstable behavior survives under a perturbation of
the system, as will be demonstrated by a special case of the so-called structural sta-
bility theorem. Measure preserving mappings acting on a measure space will show
strong recurrence properties and the question arises, how an orbit of such a system
is distributed statistically in the space. As an answer we shall prove the individual
ergodic theorem of G. Birkhoff following the strategy designed by A. M. Garsia.
The origin of the field of dynamical systems lies in the deep mathematical
problems of celestial mechanics. That is why we shall first recall the N -body
system whose dynamics is determined by the Newton equations.
I.1 N -body problem of celestial mechanics
In the N -body problem of celestial mechanics one studies N points x
k
2 R
3
in the
3-dimensional Euclidean space having masses m
k
>0. The evolution in time of
these mass points,
x
k
.t/; 1 k N;
is determined by the Newton equations
m
k
Rx
k
D
X
j ¤k
m
k
m
j
x
j
x
k
jx
j
x
k
j
3
;1 k N;