can be attributed to the mutual orientation of
communication is in practice constrained to
the antennas, which are not normally co-
`touch' range and hence limits its usefulness.
polarized and in the boresight direction of each
PAN systems, in which user touch or
other. Occasionally this leads to very large (up
handshake,  is used  for  low data  rate
to 25 dB) discrepancies between the data and
communication and has been demonstrated, [4],
the free space curve. The complexity of
at 10MHz. At higher frequencies, propagation
determining the relative orientation of the
has been characterised at ISM and other bands,
antennas along the on-body propagation path
for example, 400, 900 and 2450MHz, [5], to
renders it impractical to attempt a more
produce  simple  analytical  models  for
accurate theoretical prediction model, as the
stationary bodies. The measurements were
radiation pattern contribution and polarization
taken with dipoles oriented vertically to the
mismatch could not be measured sufficiently
body surface, and were taken over an angle of
accurately.
180º around the body. The propagation mode
is assumed to be a creeping wave which
The data points represented by circles in Fig. 4
exhibits an exponential decay of power, [6].
correspond to the scenarios when there was no
The expressions are of two slope form with a
LOS between the antennas, and the dominant
breakpoint part way around the body. Beyond
propagation path corresponded to a creeping
the breakpoint angle, the two rays are assumed
wave propagating around the body. Generally
to interfere, resulting in smaller decay but
speaking, the distance variation of such a wave
increased variability. The decay coefficient at
is fairly complex and depends on a number of
2.4 GHz corresponds approximately to 2
parameters. For example, the distance variation
dB/cm, assuming that the body radius is 20 cm.
is different on the free space sections of the
Significant interference takes place beyond the
propagation  path  and  on  the  sections
breakpoint at 400 and 900 MHz, indicating the
conformal to the body. However, because the
presence  of  multipath  effects,  although
human body has a complex geometry, which is
multipath is seen to be much smaller at 2.4
highly variable between individuals, tracing
GHz.
propagation paths around it is difficult and
often inaccurate. Nevertheless, the non-LOS
Measurements of channel loss, for many body
data points do appear to follow a trend shown
postures and antenna positions, have recently
as a straight line in Fig. 4. This trend
been made at 2.45GHz, [7, 8]. Fig 1 shows the
corresponds to an exponential attenuation
results collated to allow separation into classes
according to the following linear regression
of on-body propagation path gain - distance
formula:
variation. Two types of path gain variation
with the distance can be roughly distinguished
G  P [dB]  0.36d[cm] 35
(2)
based on the propagation scenario, namely,
variation in the illuminated region and in the
where d is the antenna separation distance
shadow region. The data points for the
propagation scenarios in which a line of sight
represented in centimeters and GP is the path
(LOS) was present, (receiver in the illuminated
gain in dB. The actual data points are spread
region), are shown in Fig. 4 by `+' signs. The
around this line with a standard deviation of
path gain of the antennas in free space in the
5.6 dB.
ground plane direction relative to each other,
given by the Friis formula, is also shown for
A number of propagation scenarios could not
comparison as a solid line. Fig. 4 shows that
be clearly identified as either LOS or non-LOS
most of the LOS data points follow the free
because the receiving antenna was very close
space curve but are generally below it with the
to the shadow boundary. Therefore, with a
mean difference between the measured and
slight change of body posture it could become
theoretical values of 5.1 dB. Thus, the path
either obstructed (completely or partially) or
gain in the illuminated region at 2.45 GHz is
unobstructed by a body part such as the trunk
given by the formula:
or an arm. These transition data points are
shown in Fig. 4 as x marks. Some of them
seem to follow the same trend as the LOS data
G  P [dB]  5.33 20 log  10 d [cm]
(1)
while others are clustered together with the
non-LOS data points.
The standard deviation of the difference
between the measured LOS values and those
given by this formula is 4.2 dB. This deviation