Öland Test Field 1965 and 1966
Öland Test Field 1965 and 1966
dr'micron Aviogon 29
Fig. 3.11: 7. Empirical radial distortion curves of aerial photo
graphs from partial calibrations in 1965 and 1966. Flying alti
tude 1300 meters, polyester base. Corrections applied for the
influences of atmospheric refraction and earth’s curvature. The
number of independent tests is indicated by the figures within
parentheses. In 1965 the grid (circle) method was used and in
1966 the radial distortion was determined with a fifth-order
polynomial. In the latter case all image coordinates were re
garded to be of equal weight. The dotted lines indicate the stan
dard errors of the radial distortion amounts. The dashed lines
indicate the radial distortion of the lenses, according to labora
tory calibrations. Ref. 3: 2 and A. Morén.
dr'micron Universal Aviogon 281
Fig. 3.11: 9. Empirical radial distortion curves of aerial photo
graphs from partial calibrations in 1965 and 1966 under condi
tions similar to those described in Fig. 3.11: 7.
Partial calibration
Radial distortion curves
Otand test field 1966
Pleogon
dr'jjm
Camera 2108
Öland Test Field 1965 and 1966
dr'micron Aviogon 41
Fig. 3.11: 8. Empirical radial distortion curves of aerial photo
graphs from partial calibrations in 1965 and 1966 under condi
tions similar to those described in Fig. 3.11: 7.
dr',um Camera 2118
+ Radial distortion according to the grid method.
S'q Standard error of unit weight according to
the grid method
Fig. 3.11: 10. Empirical radial distortion curves of aerial photo
graphs from partial calibrations. Aerial photography by Geo-
dfetisk Institut in Copenhagen with Zeiss RMK Pleogon c =
153 mm from the flying altitude 1500 meters on Cronar film.
The calculations were performed with
a) The grid (circle) method. The crosses indicate the radial
distortion amounts and a' 0 indicates the standard error of unit
weight of each circle combination.
b) The polynomial method for the determination of the radial
distortion. The fully drawn lines indicate the radial distortion
according to this method. The standard errors of unit weight
according to this method are 4.4 ¡um for camera 2108 and 4.7
¡um for the camera 2118. The root mean square values of the
standard errors of unit weight according to the method a) were
found to be 4.0 and 4.5 ¡um respectively. The agreement between
the two methods is consequently very good. When the method
b) is applied all image coordinates are assumed to be of equal
weight.
t
Fig.
unit
tion
error
coor<
Fig
photo
18