GEOMETRIC CORRECTION OF LINEAR ARRAY SENSOR DATA
Shunji Murai and Ryosuke Shibasaki
Institute of Industrial Science
University of Tokyo
7-22, Roppongi, Minatoku
Tokyo, Japan
ABSTRACT
The Study deals with the following items:
1) Production of simulated stereo images which
will be obtained from linear array sensor, by
using the digital terrain model (DTM) and the
corresponding scene corrected LANDSAT MSS data.
2) Determination of exterior orientation parameters
given as the function of time, by using ground
control points.
3) Automated three dimensional measurement by
applying auto-correlation to the stereo imagery.
Computer simulation was done for the test area
where the national elevation data bank and scene
corrected LANDSAT data are available. The test
area was selected in the mountaneous area includ-
ing high mountaines covered with snow, flat plane,
rivers, reservoirs and so on.
Simulated stereo images were generated by
computer with a given exterior orientation para-
meters. Two different stereo angles of 30? and
45? were compared.
A mathematical model to determine the orienta-
tion parameters was developed with use of ground
control points which were selected in the imagery.
Accuracy of exterior orientation was compared
for two different stereo angles. Standard devia-
tion of residuals ranges 0.3 to 0.5 pixel around
the control points, while 0.3 to 1.0 pixel for
unobservel points.
Three auto-correlation methods to recognize
the conjugated points in the stereo imagery, were
compared with respect to the accuracy and comput-
ing time. As the result of comparison, minimum
alsolute sum method were selected as the optimum
method.
SIMULATED STEREO IMAGERY
Computer simulation was done for the following
variables.
. Stereo angle
. Satellite orbit
. satellite attitude
Following data are given as known input data.
configuration of earth surface
. ————— given by national elevation data bank
23
. allocation of elements of array sensor
. radiance value which will be reflected the
earth surface
-—---- given by LANDSAT MSS data
Simulated imagery for linear array sensor was
obtained as follows:
1) Input those data of satellite orbit ( X, (L),
Yo (1), Zo (L), and satellite attitude (uXL),
¢ (L), x (L)) as the function of line number.
2) Generate a beam connecting each element and
and the projection center.
3) Determine the cross point of the beam and the
earth surface.
4) Interpolate the radiance value from the geogra-
phically corrected LANDSAT MSS data.
Fig. 1 shows the schematic geometry of linear
array sensor and DTM.
Fig. 2 show the topographic map in the test
area.
Fig. 3 shows the computer simulated imagery.
EXTERIOR ORIENTATION
Exterior orientation parameters are given as
the function of time or line number, as follows.
satellite orbit:
Xo = Xoo + X, .L
Yo = Yoo t Y, .L
Zo = Zoo + 21 .L
satellite attitude:
Q =wo +w3.L Ha Le +03. L°
$ 7$o *$i.L +62.L° +63.L
K =K9 +K;.L 4K2.L? H3. L?
where L : line number
( Xo , Yo , Zo ) : projection center
(0. , à, K ) : attitude (roll,pitch
and yaw)