306
Greg
King
and
Ian
Stewart
signals produced by
a
continuous dynamical system. Broomhead and
King
[7]
explains how to apply these ideas
to
Poincar6 sections, that
is, to mappings, by local analysis. We describe only the technique
as
it applies to continuous dynamical systems.
As
in the Packard-Takens method, we form
a
‘moving window’
of length
N
from this time series, but the difference is that we then
apply principal component analysis to write the resulting vectors in
RN
as
linear combinations of eigenvectors
of
a
correlation matrix.
Intuitively, this process finds the most common patterns among the
vectors in
RN
and expresses each such vector
as
a
linear combination
of such patterns. The dominant patterns, having the largest eigen-
values, are retained: the remainder are considered to be ‘noise’ and
are ignored.
Specifically, define an N-column matrix
X
=
(z;j),
where
1
5
j
5
N
but
i
is arbitrary, by setting
x;,
=
y;+j-1.
Form the
N
x
N
correlation matrix
C
=
X
X
and let its eigenvectors be
~1,
. .
.
,
VN
and corresponding eigenvalues
01,.
.
.
,
UN.
These eigenvalues are
all
real, since
C
is symmetric, and can be arranged in decreasing order:
without loss of generality
01
2
. .
.
2
UN.
Typically these eigenvalues decrease rapidly and then level
off,
as
in Figure
28.
The point at which they level
off
is the noise
froor
for the observations.
Suppose this starts at
UM+~.
Let
V
=
span(v1,.
.
.
,
VM)
and let the projection of
v
E
RN
into
V
be
ij.
Then
the original time series is replaced by the series of M-dimensional
vectors
fi
where
z;
is the ith row
of
X.
What happens if we apply this method to
a
time series obtained
from an equivariant dynamical system?
As
a
numerical experiment,
we take the
Field-Golubitsky-Chossat
mapping
(3)
with parameters
a
=
l.8,/3
=
O,7
=
1.34164,X
=
-1.8,
which we know produces
the fully symmetric attractor of Figure 4(b). For simplicity we use
the Packard-Takens approach, though similar remarks apply to the
Broomhead-King refinement. We take
N
=
2
(knowing in advance
that the attractor is embedded in
R2),
and let the ‘experimental
measurement’ be the z-coordinate of the point on the attractor. Thus
we plot the pairs (z;,z;+l), for an orbit
(zt,
yt) defining the attractor.
The result is shown in Figure
29.
We can recognise this
as
a
T