WL ÜÜ i
«
n »smce:- : ;
*98*8(11)
'ocess for the
ormai camera
st in the form
cceptance test
t a series of
'ac MMS and
This section
suits for 8 of
luate the DSS
nes is flown,
lple Distance
own at either
ngth (60 mm
ire flown in a
ielap is 60%
15 cm GSD
imnarison on
the Extenor
The CalQC
the imagery,
ra model and
fits” against
dS accuracy
uality of the
each flight.
laerv due to
ough only 2
th such high
iple images,
The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences. Vol. XXXVII. Part B5. Beijing 2008
The SmartBase network used for the processing is comprised of
5 reference station; four from the Can-Net VRS network
(www.can-net.ca), and one CORS station. Figure 11 shows the
trajectory and layout of the network. Figure 12 shows a plot of
the distance to the nearest base station for one of the flights. As
indicated by the peaks and valleys, the turns are anywhere from
36 to 49 km from the nearest station.
SSHL.
f t*
Figure 11. Test Flight Trajectory and SmartBase Network
3© Ototzm* u Cl**-#*» Staösn fw?
Figure 12. Distance to Nearest Reference Station
Two of the DSS flight tests were flown with maximum bank
angles of 25 deg. The remaining 6 were flown with maximum
bank angles of 30 to 40 degrees. In all cases the Applanix IN-
Fusion technology was able to remain in fixed integer
ambiguity mode, even during the turns.
Figure 13 shows a plot of the roll for one of the flights that had
bank angles up to 40 deg, with the exposure times indicated by
the blue squares. Figure 14 shows the number of SV’s tracked
during the same flight. During the turns this drops to as low as 5.
Figure 15 shows the solution status for the same flight, which
always remains in fixed integer even as SV’s come in and out
of the solution. Table 1 provides a summary of the checkpoint
residuals for the 8 flights. In each case the RMS accuracy is
well within the DSS system accuracy specification of 1.2 X
W * - * i
effective GSD RMS horizontal and 3 X effective GSD RMS
vertical (approximately 20 cm and 50 cm RMS respectively).
The average RMS over the 8 flights is 11 cm and 12 cm
horizontal, and 13 cm vertical.
This indicates that the accuracy of the EO produced by the POS
AV 410 is well within its specification and completely
unaffected by flying sharp turns with distance to the nearest
base station as large as 49 km.
#
Lens
(mm
)
Max
Roll
(deg)
RMS E
(m)
RMS N
(m)
RMS H
(m)
#
GCP
1
60
25
0.17
0.19
0.07
8
2
60
25
0.16
0.17
0.15
7
3
60
40
0.06
0.14
0.09
3
4
60
30
0.13
0.12
0.23
4
5
60
40
0.12
0.13
0.15
4
6
40
30
0.07
0.09
0.19
2
7
60
30
0.08
0.08
0.07
2
8
60
35
0.12
0.07
0.07
2
Avg
0.11
0.12
0.13
Table 1. RMS Accuracy vs GCP, 15 cm GSD
833
№
WfwU ■
Mim i
gm
jr v . ; i
fist