Full text: Proceedings, XXth congress (Part 2)

  
International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B2. Istanbul 2004 
  
are then geometrically corrected for lens distortion based on a 
calibration of the individual camera heads and are subsequently 
combined to form the image composite (see Dórstel et al. 2003 
and below for details). The final output images are written to 
the output RAID storage designated for the final images on the 
postprocessing server. The final output image data can then be 
transferred to a data management and distribution system, such 
as Z/l's TerraShare, where it can be archived or distributed to 
the destination defined by the operator. 
  
  
  
  
  
Processin | Processing Details In Step 
g Site Step 
Office Preprocess- | Mission planning 
ing 
Airplane | Photo Flight | Navigation and flight manage- 
ment system 
Camera software control 
module 
Quickview (inflight quality 
check) 
Data storage 
Office Postprocess- | Connection of flight data 
ing Storage (FDS) or Copy Station 
disks 
Postprocessing 
e Radiometric correction 
e Geometric correction 
e  Mosaicking (generation 
of virtual images) 
Color image generation 
Data distribution 
Office Data Data processing via 
Exploitation | photogrammetric and/or GIS 
tools 
  
  
  
  
  
Table 1. Typical DMC Workflow 
2. IMAGE COMPOSITE GENERATION 
The aim of generating image composites from the different raw 
panchromatic and multispectral images is to generate a central 
perspective image in such a way that, in subsequent processing 
steps, standard photogrammetric procedures and software can 
be used. 
First of all, each of the four camera heads needs a precise 
geometric calibration. This step is also known as ‘single-head- 
camera geometric calibration’ and applied at manufacturing 
site. The information generated during this procedure is 
delivered on a calibration CD to the customer together with the 
complete DMC System. During system installation the 
calibration data is stored at the postprocessing workstation. 
When the aircraft lands, the mission data is transferred to the 
postprocessing workstation. 
Within one exposure, the raw images are captured from slightly 
different positions (Figure 4, upper part). Relative to the tilted 
panchromatic images, the image composite is placed in an 
average position and can be thought of as a perfectly nadir- 
looking image. In Figure 4 the relation between two individual 
camera heads is depicted. In order to generate the image 
composite, the geometric relations between the four individual 
398 
images and the image composite must be given. Assuming 
known values for this relative orientation, e.g. from a prior 
calibration, the individual images are merged together and 
projected to a horizontal reference plane (see Figure 4) to form 
one perspective image (see Tang et al. 2000 for the related 
equations). In this step, the focal length of the image composite 
can be chosen freely. In order to avoid under- or over-sampling, 
a value close to the actual focal length of the individual camera 
heads should be used. Also, lens distortions of the individual 
camera heads can be respected in this step. It should be noted, 
however, that the image positions need to be corrected prior to 
the merge. 
       
     
projection center 
p n er * projection center 
ackward view 
forward view 
| 
| reference plane 
for composition 
CAOW X Ge 3 RR REDEN MN Gl aan EM N N NN 
  
  
Figure 4. Principle of the combination of convergent sub- 
images to an image composite 
Above: cross-section Below: 3-D situation 
3. ERROR ANALYSIS OF IMAGE COMPOSITE 
GENERATION | 
In terms of geometric accuracy of the image composite, there 
are three issues which need to be discussed: (a) all raw images 
must be acquired synchronously in time, (b) the systematic 
effect resulting from the different perspective centres must be 
negligible, and (c) the relative orientation of the camera heads 
must be stable. 
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