Full text: Proceedings, XXth congress (Part 4)

ınbul 2004 
5. The X. 
the three 
owns and 
1ean point 
Y, and Z 
n, 6.8 km, 
ts located 
tion 
refer 
wed us to 
)oor point 
ering only 
scribed by 
squares fits 
d a 3-axial 
[ errors as 
ned a RMS 
it a sphère 
and that it 
er models. 
1ined to be 
MS=5 km) 
  
  
1880 
International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B4. Istanbul 2004 
  
  
  
  
  
T 
LM - 
T. ii 
^ * 
4 Y " 
i 
Hl + - ^ 
- ze 
= | E] 
Anm 
r 
Mio € 
Be 
Ht 
Nit 
À imma dis - 
Mx „| HN 
T 
de 
DI 
: Horizontal error ellipses of the control points, with th 
largest ellipse has a size of 13.6 km. Compare the 
  
  
  
  
T TT T T T 1 
i 
1 . i 
| i 
N | 4 
Í 
> 
^t 
adm 
E 
e lengths of the ellipse axes proportional to the errors. The 
sizes of the error ellipses with the image resolutions (Fig. 1)! 
  
  
   
  
  
  
  
  
BHD Y 
1 
| 
575 T 
^w k 
| I 
4H , Í i 
dr. sil 7 | Li | 
= à se, à! | | Í 
X zh od, ui i! * | 1 I i 
- AMA Tle Li | 
i RM = ; ^ é - 
8 FELELCRANIAR EEA NT NASER CRATE EES «ued % id = ud Ex "uvautu TT L JE "4532.74 VERRS WA 
8 Iii [i H Mai 1 i d i 
"zn e le d € " E «il i > 
2 sáb ; | m 4d ¥ | { 
t T s | 
i CE | 
= it 4 
455 Là i 
© E. | 
| : 
à 
ang i 
4. ¥ = 
482 ****** Murfterer Radius 
seu - vi - - - - 
‚180 „120 a e él 126 180 
Länge [*] 
Fig. 3: Radial distances and errors for the control points of Dione 
3. DIGITAL IMAGE MOSAICS 
Image mosaics and maps were produced for the five largest 
Satellites (excluding the cloud-shrouded satellite Titan) 
Mimas, Enceladus, Tethys, Dione, and Rhea. The images were 
first reprojected to digital maps, using orbit and pointing 
data derived by Davies and Katayama (1983a,b,c; 1984). 
However, for Dione images, improved pointing data were 
taken from limb-fitting procedures mentioned above. 
For comparison and interpretation of the maps, a 3-axial 
ellipsoid was used for the calculation of the ray intersection 
point; however, the map projections were done on a sphere, 
with all satellite shape parameters taken from IAU 
recommendations (Seidelmann et al., 2003, see Table 1). A 
photometric correction using the Minnaert function was 
applied to every image during map projection. 
The final step of the image processing was the combination 
of all map-projected images (14, 9, 8. 13, and 37 Voyager-1 
images, for Mimas, Enceladus, Tethys, Dione, and Rhea, 
respectively) to a homogeneous mosaic. Special care had to 
be taken to the different ground resolution of the input 
881 
 
	        
Waiting...

Note to user

Dear user,

In response to current developments in the web technology used by the Goobi viewer, the software no longer supports your browser.

Please use one of the following browsers to display this page correctly.

Thank you.