International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B1. Istanbul 2004
line of sight of the satellite and obtained from Figure 4 by
expression (1) (Hanssen, R.F., 2001).
Sat.orbit. North
Azimuth Look
Direction
> East
Satel. line
of sieht.
3 € = ws
Azimuth
ceri Look
» East
Br
Figure-4. Projection of the three components of the deformation
p ; :
vector d -(d,,d,,d,) onto satellite LOS. (Hanssen, R.F.,
2001)
d. -d cos, )-sinQ, Jd, cos, —3/2)*-d,sin&, -3z/2] (1)
Here a, is the azimuth angle of the satellite orbit and is ~190
degrees for the ERS satellite, 0, is the incidence angle of the
satellite and is ~23 degrees for ERS. If we consider the fact that
the North Anatolian Fault is a strike slip fault, the incidence
angle of the satellite is ~23 for ERS, the vertical deformation is
very small and we can assume d, =0.
The amount of deformation in the line of sight of the satellite at
such a point may be calculated with the formula below,
d, =-0.0678d, + 0.3848d, (2)
The GPS values collected before and after the Marmara
Earthquake of 1999 by two continuous data collecting
GPS stations, namely DUMT and TUBI erected in this
region by TUBITAK-MRC EMSRI are given in Table-2.
Deformation
d, (sn) d, (sn)
DUMT {0.010 0.013
TUBI 0.010 0.025
Table-2. Coordinate values obtained by two GPS stations
collecting continuous data.
Substituting d, and d, deformation values obtained from
Table-2 into expression [2], d, component of the
specified point is calculated 0.0043244sn for DUMT
station and 0.008942sn for TUBI station. If the earth's
radius is assumed R=6361236m, then we compute
d, puyn-13.34cm, d,rugy- 27.59cm. Taking these values
into consideration, definite deformation values for each
fringe digitized from Figure 3 are entered into the
database to obtain the absolute deformation map by linear
interpolation in the sight of the satellite as shown in
Figure 5. However, fringes on and in the vicinity of the
fault line were not explicitly obtained because of the
insufficiency of the wavelength here. These regions are
therefore masked in the deformation map.
“ligth
Directick
10 cm
Figure-5. Ground deformation in the satellite LOS
4. CONCLUSIONS
Until almost fifteen years ago, the scientists were experiencing
significant difficulties in application of SAR interferometry
potentially in various areas either because the technique is
difficult to comprehend in theoretic basis or unavailability of
suitable data sets. Although contemporarily significant progress
has been made on alleviation of these problems still some
problems exist with regard to phase unwrapping. Therefore, the
interferogram obtained in this study was visually interpreted
and the fringes were manually digitized in order to obtain more
correct results. Since LOS deformations obtained from digitized
Internatioi
fringes arc
computatic
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pp.763.
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Reilinger,
Lenk, A.
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Wright, |
2001. Tri,
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Lett., 28,
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