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The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences. Vol. XXXVII. Part Bl. Beijing 2008
GSD*n
pa (1—£-)
100
(1)
The minimum exposure interval of the digital medium format
cameras is somewhere between 2 - 3 s.
Figure 2 provides an overview which minimum GSD for a
photogrammetric aerial survey with an endlap of 60 % applies
at what speed over ground.
30 35 40 45 50 55 60 65 70 75 80 85 90 95 100 [m/s]
58 68 78 87 97 107 117 126 136 146 156 165 175 185 194 [kn/h]
Speed over Ground
Figure 2: Exposure interval of medium format cameras related to GSD
and ground speed
3.3 Image motion
image noise levels. The aperture is also a limiting factor,
because a wide aperture may cause or enhance vignetting and
optical aberrations. To sum up: the image motion limits the
GSD of medium format cameras and the short exposure interval
necessary limits the flying operation times under poor lightning
conditions when compared to large format cameras.
4. GEOMETRIC AND RADIOMETRC CALIBRATION
The calibration of digital cameras includes geometric and
radiometric issues. From the viewpoint of a photogrammetrist,
geometric issues are the more important. For large format
cameras detailed tests within the frame of OEEPE and
EuroSDR were conducted, e.g. Cramer, 2007. The special
geometric problems of multi head cameras are discussed quite
extensively in the literature, e.g., Jakobsen, 2007. Research in
the calibration of large format cameras systems is an ongoing
process with the aim to develop a calibration procedure of the
whole camera system and its subsystems, including GPS/INS,
radiometric and geometric issues and the whole
photogrammetric processing chain, EuroDAC 2 (2008).
4.1 Geometric calibration
Due to the compactness and the low weight of medium format
cameras, laboratory calibration of the interior is relatively easy
to obtain. As mentioned in section 3.1.1 the interior orientation
of medium format cameras may change under airborne
conditions. Therefore the geometric calibration of the medium
format camera system should be done in four different levels:
Airborne images are acquired from moving platforms such as
aircrafts or helicopters. The movement of the sensors during the
exposure influences the quality and the sharpness of the
acquired imagery. For analogue airborne cameras this image
motion is taken care by forward motion compensation (FMC).
For large frame digital airborne sensors the translation effect of
the FMC is solved digitally by moving the charges on the
matrix area itself (time delayed integration, TDI). Additional
rotational movements are compensated from the stabilised
mount. For medium format sensors an active mount is typically
not available - exemptions are the DSS and cameras which are
used as a sub-system e.g. in combination with laser scanners
mounted on a common platform which is then stabilised. Also
TDI is not available for the medium format digital sensors due
to the Bayer pattern of the CCD-chip. The image motion u is
related to the aircraft velocity over ground v g , the exposure time
t e , the focal length c, the flying height above ground h g and the
size of the pixel s p see formula 2.
2
GSD
(2)
where only 50% of the theoretical image motion u th is valid in
the images. For digital imagery the smear due to image motion
should not exceed 0.5 pixel. Since aircraft velocity and GSD are
typically given by default for a certain project, exposure time is
the only variable to minimise effects of image motion, if
suitable light conditions are available. Exposure time on the
other hand is coupled with lens aperture and the sensitivity of
the digital sensor given by the ISO value. However a higher
sensitivity (ISO number) is always associated with higher
1. Laboratory calibration with a 2-D or 3-D test field.
2. In flight calibration over a calibration range.
3. Simultaneous in flight calibration on the job to adjust for
project specific circumstances
4. Long term camera stability analysis to determine the
necessary calibration intervals.
4.2 Radiometric accuracy and calibration
An increasingly important task is the “radiometric accuracy”
and the radiometric calibration of aerial cameras. The first goal
of such a radiometric calibration is to eliminate the influence of
the optics and the sensor and make sure that the resulting
images will have the same sensitivity throughout the image.
The radiometric calibration is also split in two main parts. The
first part of the radiometric camera calibration is done by the
manufacturer to eliminate radiometric dysfunctions of the
sensor such as:
• Defect pixels
• Dark Signal Non Uniformity (DSNU)
• Individual sensitivity of each single CCD pixel
• Vignetting (partly)
• Influence of aperture (partly)
However, the manufacturer radiometric calibration effort differs
between medium format cameras. White balance calibration
procedure or more general the Look-Up-Table (LUT)
generation is the second step. For each project the user performs
this type of calibration individually. After post processing the
user can set the white balance for the project using some
example images which cover the typical surface,. With suitable