PHI, OMEGA, KAPPA etc. however, are not real but simulated as ex- 
plained in the preceding paragraph. 
RESIDUALS AT CONTROL POINTS AFTER ABSORIENT 
I POINT DXG DYGC D7G 
1 3001 070 - 921 -.008 
2 3004 056 -.024 0 900 
3 3035 045 - 0680 - 0047 
4 3036 - 632 995 -.002 
S 3005 - 003 .987 - 500 
b 3006 - 439 - 057 00.4 
2 3008 - 005 = 903 909 
3 3038 043 .081 .009 
» 3919 - 004 ‚026 9.000 
10 3012 - 054 .079 004 
11 3010 - 077 = 050 000 
i3 3037 - 007 .060 003 
13 3019 - 052 -.041 - 303 
14 3021 091 059 .002 
15 3033 035 - 819 -.000 
16 3002 - 004 .033 - 002 
17 3023 = 015 - Obi - 004 
13 3024 946 = 978 - 283 
19 3926 - 088 082 .091 
20 39030 - 086 002 9007 
2i 3034 017 -.098 804 
29 : 3817 082 .088 - 915 
AAN 093 .056 .006 
Table 2 : Residuals 0XG, DYG, DZG in km units at ground control 
points after absolute orientation. 
Table 2 shows the residuals at the 22 control points after the 
absolute orientation, Fig. 2 the corresponding vector diagram: 
  
  
  
d FORMER 
  
N Sa3 | 
» ani? eo 
\ Suid 
x, 3034 
S 
oO 
* € 
\ 3C3C 
i 
| 3017 \ 
QM 
2025 
sor en ny 
: S 
301837 a Y 
e Ss 
x 3633 
et ^ 302 
Ph 
Î mx x 
i ^ JW 
X 
^Um UNIT i 
42412 UNITS 
  
Fig. 2 : Residual vectors at ground control points after absolute 
orientation (DZ 7 plotting) 
4 100m as vector 
3500 m on the ground