go
e
with different
thods, one is
aximum and
ows that the
of the results
this visual
give the best
ilter but the o
ense of more
ected, in the
ie eigenvalue
'ferent filters.
nimum errors
npared to the
error is very
, o linear, B
1e most effect
is small. It
h to further
ler detection
nid.
roduced after
FILTER Mean Standard Max.
error error error
None 2.7 29.6 171
Lee 1.6 29.0 141
Kuan 21 30.4 176
Frost 1.1 29.7 202
Mod. Frost 0.8 20.7 201
o linear 22 29.7 135
MAP 0.9 29.2 162
B 19 29.0 143
y 22 29.6 201
Li 29 30.0 166
LVN 1.2 28.6 122
Crimmins 1:8 29.3 169
log-linear 17 29.2 190
Table 2. Statistics relating DEM with disparity model.
6. RESULTS FROM DEM PRODUCTION
The final stage of DEM production is the
transformation of the image disparities into three
dimensional co-ordinates. This requires a geometric
model as discused in section 2. Chen (1993) has
developed the model described by Clark (1991) and
has produced 3D co-ordinates without the use of
ground control points from opposite side and same
side stereoscopic pairs using roll-tilt mode data, of he
area of Provence, France, to the North of Marseilles.
The accuracy of the results has been tested with 38
ground check points. The method makes no use of
ground control points but requires accurate orbit data.
To date there have been difficulties in determining the
accuracy of the orbit data and this may contribute to
the errors in the results. Table 2 shows the statistics
for the 38 points used to check the transformation.
It is apparent that there are systematic errors in both
sets of data but that they apply to X and Z co-
ordinates derived from same side data and only in Z
with opposite side data. An analysis of errors
indicates that these results are consistent with theory
and that improved timing data and use of ground
control points would give better results.
Leberl (1990) has reported results from stereoscopic
SAR as shown in table 4. The current results indicate
that the method with ERS-1 data needs improvement
to give comparable accuracy.
Sensor Easting Northing Ht
(m) (m) (m)
Seasat 59 34 28
SIR A 48 84 93
SIR A 56 77 72
STAR* 13 26 28
*These results are from an airbourne system with GPS
Table 4. Results from stereo SAR systems quoted
by Leberl (1990).
7. CONCLUSIONS
Geocoding of SAR is now carried out at a routine
process. Experience has shown that processors
developed for ERS-1 can also handle JERS SAR data
but thet there can be problems in obtaining the correct
timing and orbit data. These may be ovcercome with
the use of tie points. It is important to include a
system for validation into the geocoding process and
this includes operator interaction. The production of
auxilliaty products such as layover, shadow and
energy maps is also important.
The work at UCL indicates that the use of
stereoscopic SAR data can produce DEMs which can
be used for geocoding. A SAR post proessing system
which had provision for stereoscopic height
determination and segmentation of the image into
Same side pair Opposite side pair
X(m) Y (m) Z(m) X(m) Y (m) Z(m)
Minimum -48 -91 -116 -85 -64 -103
residual
Maximum 137 93 8 72 45 28
residual
Mean 51 6 -42 4 -7 -51
Standard 70 35 S2 37 23 64
deviation
Table 3. Statistics from 38 ground check points.
441