Full text: Proceedings, XXth congress (Part 4)

stanbul 2004 
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1 must be lin- 
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control infor- 
vestigates the 
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| information 
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hlhof, 1994), 
1ssical GCPs, 
International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B4. Istanbul 2004 
too. Here, as control information they use irregular arranged ter- 
rain points which don't have to be identified in the images. Trans- 
ferred to case of Mars Express (Spiegel et al., 2003), the role of 
terrain points corresponds to the role of the MOLA track points. 
However, the HRSC tie points must be acquired in such a way, 
that at least HRSC points are arranged in the surrounding of each 
MOLA track point. The HRSC object points would define small 
surface patches, each containing a MOLA track point. 
In principle, these are two viable alternative ways to combine 
HRSC points and MOLA points. The first approach is to use the 
terrain surface derived by MOLA DTM points and fit the matched 
HRSC points into the MOLA surface. The second approach is to 
use a terrain surface defined by HRSC points and adapt this sur- 
face to the MOLA track points which serve as control informa- 
tion. The first alternative is suited better if there are more MOLA 
points than HRSC points. The second is more reasonable if there 
are more HRSC points than MOLA points. 
The comparison of the matched HRSC tie points and the MOLA 
data shows that in all investigated areas more MOLA points than 
matched HRSC tie points are available. Therefore, in the fol- 
lowing investigations the first approach will be applied. This 
approach will be described more in detail now. It uses a least 
squares adjustment with additional conditions to get a relation 
between a DTM and the HRSC points. As already mentioned, 
the HRSC points have to lie on a bilinear surface defined by four 
neighboring MOLA DTM points, which enclose the HRSC point 
(see Fig. 6). This condition can be formulated as a constraint on 
the vertical distance d from the HRSC point to the bilinear sur- 
face. Furthermore, this constraint can be substituted by a fictive 
observation, used as additional observation in the bundle adjust- 
ment. 
d 
  
M4.4: MOLA DTM mesh derived 
from MOLA points 
H: HRSC point 
d: distance between HRSC point 
and MOLA DTM-surface 
Figure 6: Fitting HRSC point in bilinear surface defined by 
MOLA DTM 
The mathematical model for this observation equation is given in 
(Equation (2)). 
da + d = f(Xn,Yn, Zn, X mis Ym,> ZM;) @) 
For each equation the number of unknowns is three 
(XH, Yu, Zu). lt contains one observation (d = 0) and 
twelve constants (Xu, Yu, ZM;, i — 1..4) The standard 
deviation c4 will be determined by the standard deviations of 
four MOLA DTM points M;, My, Ma, and Ma. Thus, the 
implementation of the least squares adjustment with observation 
equations only is quite easy. 
With this approach an improvement of the height (Z) can be ex- 
pected, of course. An improvement in planimetry (X, Y) can only 
be determined, if there are different local terrain slopes at the dif- 
ferent MOLA surfaces. 
UA 
4 PROCESSING OF HRSC IMAGERY 
This section is divided in two parts. Section 4.1 describes the 
results of bundle adjustment without control information. The 
results of bundle adjustment with the MOLA DTM as control in- 
formation is presented in Section 4.2. In both cases the a priori 
accuracy has been introduced into the bundle adjustment with a 
value of 1000 m for the position and 28 mgon for the attitude. 
One whole trajectory of the orbiter is considered to be very sta- 
ble. Therefore, only a bias over the whole trajectory will be 
improved. The MOLA DTM is introduced with an accuracy of 
100 m instead of 10 m in order to cope with differences between 
HRSC object points and MOLA track points due to the limited 
spatial resolution of MOLA. As mentioned before, the resolution 
on ground of HRSC is up to 12 m compared to the MOLA surface 
spot size of about 168 m. Regarding local areas, the MOLA data 
describe the surface less detailed as HRSC object points. The 
orbits 18, 22, and 68 will be analysed. 
4.4 Bundle adjustment without DTM 
In order to evaluate the quality of the matched image coordinates, 
the ray intersections of the tie points are analysed. First the ob- 
served values of the exterior orientation are fixed in the bundle 
adjustment, i.e., they are regarded as error free, and no DTM as 
control information is introduced. This can be considered as a 
forward intersection. The obtained values are then compared to 
the results calculated by the bundle adjustment improving ¢ and 
&. More precisely, a constant bias is modelled for both angles 
along the entire orbit. In all orbits the number of HRSC points is 
very high. Thus, it is possible to use only 3-ray points in the bun- 
dle adjustment. With 3-ray points the redundancy for each HRSC 
object point is high and gross errors of image coordinates are vis- 
ible. These errors can be eliminated by a robust adjustment. 
In Table 2 the accuracies of the object coordinates derived from 
the ray intersections are shown for the selected orbits. The left 
value is the accuracy of the ray intersections keeping the observed 
exterior orientation fixed. The right value shows the achieved 
accuracy of the ray intersections after improving « and «, i.e., 
after estimating the bias in ¢ and &. 
  
  
  
  
orbit | altitude [km] | cx [m] | ev [m] | ez [m] 
18 275 - 347 11/59 | 13/66 | 34/18 
22 311 - 941 13/78 | 18/92 | 427/22 
68 269 - 505 30/10 | 27/11 | 49/18 
  
  
  
  
  
  
  
Table 2: Object point accuracies of ray intersections 
The accuracies of the object points for all processed orbits are in 
a range of about 6 to 11 m in X and Y, depending on different 
imaging altitudes. Z accuracies for all orbits are about 18 - 22 m. 
The standard deviations of the ray intersections are improved by 
a factor of 2 and a final accuracy of about 0.4 pixel on the ground 
in X and Y and 0.8 pixel in Z is achieved. The generated tie 
points are evenly distributed over the whole image block except 
for areas with a lack of texture (see Fig. 7). Black points are 2-ray 
points and gray points are 3-ray points. White areas are without 
tie points. 
4.2 Bundle adjustment with DTM 
The second part of the results shows the evaluation after HRSC 
object points have been fitted to the MOLA DTM. Here, all six 
parameters of the exterior orientation (Xo, Yo, Zo, ¢,w, kK) have 
been improved along the trajectory. The reliability is very high 
because the coordinates of one point is determined on two ways. 
 
	        
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