The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences. Vol. XXXVII. Part Bl. Beijing 2008
1251
^Orttiophato^
c
№bI murid flKÿKt mmfUfrMMbfts
3
Oafcaritl eqturtiorts
►nag« distortion
c
Medusa Imme ooonünates
3
C
8ynth«öc Medusa kmga
J
Figure 9: Medusa simulator concept
Effect of changing focal length due to temp. diff. on direct georeferencing
Figure 10: Effect of changing focal length on direct
georeferencing.
This indicates that a thorough self-calibration approach is
necessary when metrically correct products need to be derived
from the Medusa instrument.
The in-flight calibration will be based on self-calibration by
means of block bundle adjustment. The DGAP block bundle
adjustment software (http://www.ifp.uni-stuttgart.de/
publications/software/openbundle/index.en.html) will be used
for this. A predefined flight pattern will be flown over a fixed
study area with sub centimetre accurately measured GCPs.
Figure 11 illustrates a minimally required flight pattern
resulting in maximally overlapping imagery with flight over the
same area in opposite directions.
Because of the expected temperature effects, a specific flight
pattern, oriented relative to the sun’s positions is needed. The
data will be processed in three independent blocks, illustrated as
numbered arrows in Figure 11. During the flights within block
one, the temperature gradient within the instrument will remain
relatively constant. For flights in block two and three,
temperature gradients will change direction. The proposed
flight pattern will allow to examine if the foreseen temperature
gradients will have a significant effect on the optical
characteristics of the system.
Figure 11: Minimal required flight pattern for Medusa
instrument calibration
Parameters that will be estimated by block bundle adjustment
are:
• Physical models
o Exterior orientation (6 parameters)
o Interior orientation
■ Principal point offset (2
parameters)
■ Focal length offset (1 parameter)
o Radial-symmetric distortions (3 parameters)
o Radial-asymmetric and tangential
distortions (2 parameters)
o Affinity and shear in the image plane (2
parameters)
• Mathematical models
o Ebner (12 parameters)
o Griin (44 parameters)
Because of the correlations that may exist between some
parameters (e.g. Platform altitude versus focal length offset),
the adjustment will be run piecewise.
For modem geometric frame cameras, it can be expected that
the parameters of the mathematical models are not significant:
these parameters are not correlated with the interior and exterior
orientation of the imaging system and are used to correct
distortions in the plane caused by for example deformations of
analog film products. However, usage of an optical mirror in
the Medusa instrument might introduce similar deformations
and will therefore be examined with care.
5. CONCLUSION AND OUTLOOK
A specific calibration strategy is proposed for the Medusa
instrument. Because of the technical constraints of the
instrument and its specific operation environment, in-flight
calibration was selected. On the one hand, the instrument
comprises an optical mirror, which could introduce planar