358
because of
ding connected with the security against distortions,
aircraft orientation changings.
As ground system a compatible PC 386 with a high
grafic display is used to read the flight data, for
and first interpretations.
The processing contains the correction of aircraft
changes with the help of the recorded orientation
images in the visible range are also used for rectification
for cartographic calibration of the TIR-images. Therefore it
necessary to read the visible images into the computer,
photographic images of the airborne photocamera can be read
means of an A4-scanner and the camcorder-data can be read by
frame-grabber-board.
The rectificated TIR-images are then processed with image-
restauration-algorithms to improve the SNR in the images. This
means the use of filters for removal of systematical errors, edge
detection and smoothing algorithms.
Booth the rough images and the resulting images are transmitted
to the central VAX 11/785 station of the institute for archiving.
There the data access for other institutions is possible.
resolution
processing
orientation
data. The
and
is
The
by
a
6. Image data processing
During the forward movement of the aircraft there occur changes
of the platform attitude. They can be resolved into roll, pitch
and yaw. This leads to geometrical distortions in the scanned
images. These distortions may be corrected with the help of the
orientation data of the aircraft.
In ref./6/ a method is described , which permits to make the
geometrical corrections in real-time already on the aircraft. But
it will be used only in future flights. This method bases on a
variation of the cycle-time of the scanner which depends on the
angular velocity of the aircraft. A necessary precondition for
realisation of this method is a very fast signal processing. Cur
rent TIR-data are geometrically corrected on ground by means of
the recorded orientation data.
Fig. 7 shows, how the atmosphere influences the measured radia
tion compared with the original values on the earth.. There is the
self-radiation of the atmosphere and the radiation of the back
ground, which overlays the radiation of the source. On the other
side one part of the radiation of the source is scattered and
absorbed by' the atmosphere and so it cannot be measured by the
scanner. During the first flights the temperature was measured on
the earth and in the air and also the humidity of the air paral
lel to the line of the aircraft. The aircraft was also flying in
two different heights (500m and 1000m). With these comperative
values it is possible to correct the atmospheric distortions. In
the DLR (Deutsche Forschungs- und Versuchsanstalt fuer Luft- und
Raumfahrt) programs are developed, which allow more exactly
radiometric corrections /7/. These programs will be used in the
future to correct the TIR-data.