In ultimo articulo Quomodo puncta imperii ac PPK notitiae locorum ad exemplar accuratum relativum 3D afficiunt, commemoravimus praeter GCPs et PPK notitias, GSD et tabellarius fucum aliquem effectum habere etiam in subtilitate relativa 3D. model.So aliud experimentum facimus ut illud cognoscamus.
Carrier fucus |
Obliquus camera |
GCPs |
PPK |
CW10 VTOL |
DG4pros |
NO |
NO |
Numerus rerum |
mensurae longitudinis (L0" |
Exemplum longitudinis 3DL1)GSD=2cm |
exemplum longitudinis 3DL2)GSD=1.5cm |
DS1(L0-L1) |
DS2(L0-L2) |
1 |
7.210 |
7.18 |
7.20 |
0.030 |
0.013 |
8.706 |
8.69 |
8.65 |
0.016 |
0.093 |
|
10.961 |
10.89 |
10.90 |
0.093 |
0.093 |
|
2 |
7.010 |
6.88 |
6.86 |
0.130 |
0.150 |
3 |
1.822 |
1.76 |
1.76 |
0.093 |
0.093 |
4 |
10.410 |
10.38 |
10.37 |
0.030 |
0.041 |
5 |
10.718 |
10.65 |
10.68 |
0.093 |
0.038 |
6 |
13.787 |
13.72 |
13.71 |
0.093 |
0.077 |
7 |
11.404 |
11.41 |
11.38 |
-0.006 |
0.024 |
12.147 |
12.13 |
12.12 |
0.017 |
0.027 |
|
8 |
7.526 |
7.44 |
7.49 |
0.093 |
0.093 |
13.797 |
13.83 |
13.77 |
-0.033 |
0.027 |
|
9 |
10.374 |
10.35 |
10.35 |
0.024 |
0.024 |
10 |
2.109 |
1.98 |
2.09 |
0.129 |
0.019 |
4.281 |
4.14 |
4.19 |
0.141 |
0.093 |
|
11 |
14.675 |
14.55 |
14.64 |
0.125 |
0.035 |
8.600 |
8.58 |
8.57 |
0.018 |
0.030 |
|
12 |
13.394 |
13.36 |
13.38 |
0.034 |
0.014 |
13 |
12.940 |
12.95 |
12.91 |
-0.010 |
0.030 |
14 |
7.190 |
7.21 |
7.20 |
-0.020 |
-0.010 |
15 |
13.371 |
13.36 |
13.38 |
0.011 |
-0.009 |
6.435 |
6.37 |
6.43 |
0.093 |
0.005 |
|
16 |
3.742 |
3.74 |
3.70 |
0.002 |
0.041 |
17 |
6.022 |
6.03 |
5.99 |
-0.008 |
0.093 |
18 |
3.937 |
3.91 |
3.94 |
0.027 |
-0.003 |
19 |
8.120 |
8.09 |
8.12 |
0.030 |
0.000 |
14.411 |
14.40 |
14.37 |
0.011 |
0.041 |
|
20 |
6.077 |
6.06 |
6.04 |
0.017 |
0.093 |
21 |
13.696 |
13.68 |
13.65 |
0.016 |
0.041 |
RMSE: DS1=0.0397m,DS2=0.0356m |
Carrier fucus |
Obliquus camera |
GCPs |
PPK |
CW10 VTOL |
DG4pros |
Ita |
No |
Numerus rerum |
mensurae longitudinis (L0" |
Exemplum longitudinis 3DL1)GSD=2cm |
exemplum longitudinis 3DL2)GSD=1.5cm |
DS1(L0-L1) |
DS2(L0-L2) |
1 |
7.210 |
7.18 |
7.21 |
0.030 |
0 |
8.706 |
8.68 |
8.68 |
0.024 |
0.024 |
|
10.961 |
10.91 |
10.87 |
0.041 |
0.093 |
|
2 |
7.010 |
6.92 |
6.88 |
0.093 |
0.13 |
3 |
1.822 |
1.79 |
1.76 |
0.093 |
0.093 |
4 |
10.410 |
10.39 |
10.38 |
0.018 |
0.03 |
5 |
10.718 |
10.66 |
10.72 |
0.078 |
-0.002 |
6 |
13.787 |
13.77 |
13.79 |
0.017 |
-0.003 |
7 |
11.404 |
11.38 |
11.38 |
0.024 |
0.024 |
12.147 |
12.12 |
12.13 |
0.027 |
0.017 |
|
8 |
7.526 |
7.47 |
7.53 |
0.093 |
-0.004 |
13.797 |
13.83 |
13.78 |
-0.033 |
0.017 |
|
9 |
10.374 |
10.34 |
10.37 |
0.034 |
0.004 |
10 |
2.109 |
2.03 |
2.11 |
0.093 |
-0.001 |
4.281 |
4.18 |
4.28 |
0.101 |
0.001 |
|
11 |
14.675 |
14.59 |
14.67 |
0.093 |
0.005 |
8.600 |
8.57 |
8.58 |
0.030 |
0.02 |
|
12 |
13.394 |
13.35 |
13.39 |
0.041 |
0.004 |
13 |
12.940 |
12.92 |
12.9 |
0.018 |
0.04 |
14 |
7.190 |
7.21 |
7.19 |
-0.020 |
0 |
15 |
13.371 |
13.36 |
13.37 |
0.011 |
0.001 |
6.435 |
6.43 |
6.42 |
0.005 |
0.014 |
|
16 |
3.742 |
3.72 |
3.7 |
0.022 |
0.041 |
17 |
6.022 |
6.00 |
5.98 |
0.022 |
0.041 |
18 |
3.937 |
3.94 |
3.91 |
-0.003 |
0.027 |
19 |
8.120 |
8.09 |
8.07 |
0.030 |
0.05 |
14.411 |
14.41 |
14.38 |
0.001 |
0.031 |
|
20 |
6.077 |
6.03 |
6.04 |
0.041 |
0.093 |
21 |
13.696 |
13.65 |
13.65 |
0.041 |
0.041 |
RMSE: DS1=0.0328m,DS2=0.0259m |
Carrier fucus |
Obliquus camera |
GCPs |
PPK |
CW10 VTOL |
DG4pros |
NO |
ETIAM' |
Numerus rerum |
mensurae longitudinis (L0" |
Exemplum longitudinis 3DL1)GSD=2cm |
exemplum longitudinis 3DL2)GSD=1.5cm |
DS1(L0-L1) |
DS2(L0-L2) |
1 |
7.210 |
7.20 |
7.20 |
0.01 |
0.01 |
8.706 |
8.71 |
8.69 |
0.00 |
0.02 |
|
10.961 |
10.87 |
10.88 |
0.09 |
0.08 |
|
2 |
7.010 |
6.89 |
6.87 |
0.12 |
0.14 |
3 |
1.822 |
1.79 |
1.75 |
0.03 |
0.07 |
4 |
10.410 |
10.39 |
10.38 |
0.02 |
0.03 |
5 |
10.718 |
10.67 |
10.69 |
0.05 |
0.03 |
6 |
13.787 |
13.75 |
13.78 |
0.04 |
0.01 |
7 |
11.404 |
11.39 |
11.38 |
0.01 |
0.02 |
12.147 |
12.13 |
12.12 |
0.02 |
0.03 |
|
8 |
7.526 |
7.51 |
7.49 |
0.02 |
0.04 |
13.797 |
13.79 |
13.78 |
0.01 |
0.02 |
|
9 |
10.374 |
10.35 |
10.34 |
0.02 |
0.03 |
10 |
2.109 |
2.03 |
2.02 |
0.08 |
0.09 |
4.281 |
4.15 |
4.21 |
0.13 |
0.07 |
|
11 |
14.675 |
14.61 |
14.65 |
0.07 |
0.03 |
8.600 |
8.60 |
8.57 |
0.00 |
0.03 |
|
12 |
13.394 |
13.37 |
13.40 |
0.02 |
-0.01 |
13 |
12.940 |
12.88 |
12.89 |
0.06 |
0.05 |
14 |
7.190 |
7.20 |
7.18 |
-0.01 |
0.01 |
15 |
13.371 |
13.36 |
13.38 |
0.01 |
-0.01 |
6.435 |
6.40 |
6.46 |
0.03 |
-0.03 |
|
16 |
3.742 |
3.75 |
3.75 |
-0.01 |
-0.01 |
17 |
6.022 |
5.97 |
5.97 |
0.05 |
0.05 |
18 |
3.937 |
3.93 |
3.91 |
0.01 |
0.03 |
19 |
8.120 |
8.10 |
8.08 |
0.02 |
0.04 |
14.411 |
14.40 |
14.38 |
0.01 |
0.03 |
|
20 |
6.077 |
6.04 |
6.05 |
0.04 |
0.03 |
21 |
13.696 |
13.65 |
13.67 |
0.05 |
0.03 |
RMSE: DS1=0.0342m,DS2=0.0328m |
Carrier fucus |
Obliquus camera |
GCPs |
PPK |
CW10 VTOL |
DG4pros |
ETIAM' |
ETIAM' |
Numerus rerum |
mensurae longitudinis (L0" |
Exemplum longitudinis 3DL1)GSD=2cm |
exemplum longitudinis 3DL2)GSD=1.5cm |
DS1(L0-L1) |
DS2(L0-L2) |
1 |
7.21 |
7.21 |
7.21 |
0.00 |
0.00 |
8.706 |
8.68 |
8.7 |
0.03 |
0.01 |
|
10.961 |
10.90 |
10.89 |
0.06 |
0.07 |
|
2 |
7.01 |
6.98 |
6.99 |
0.03 |
0.02 |
3 |
1.822 |
1.80 |
1.78 |
0.02 |
0.04 |
4 |
10.41 |
10.40 |
10.39 |
0.01 |
0.02 |
5 |
10.718 |
10.70 |
10.69 |
0.02 |
0.03 |
6 |
13.787 |
13.77 |
13.76 |
0.02 |
0.03 |
7 |
11.404 |
11.39 |
11.39 |
0.01 |
0.01 |
12.147 |
12.13 |
12.12 |
0.02 |
0.03 |
|
8 |
7.526 |
7.49 |
7.51 |
0.04 |
0.02 |
13.797 |
13.81 |
13.8 |
-0.01 |
0.00 |
|
9 |
10.374 |
10.36 |
10.35 |
0.01 |
0.02 |
10 |
2.109 |
2.02 |
2.11 |
0.09 |
0.00 |
4.281 |
4.16 |
4.28 |
0.12 |
0.00 |
|
11 |
14.675 |
14.66 |
14.68 |
0.02 |
0.00 |
8.6 |
8.54 |
8.53 |
0.06 |
0.07 |
|
12 |
13.394 |
13.35 |
13.37 |
0.04 |
0.02 |
13 |
12.94 |
12.89 |
12.91 |
0.05 |
0.03 |
14 |
7.19 |
7.18 |
7.2 |
0.01 |
-0.01 |
15 |
13.371 |
13.35 |
13.35 |
0.02 |
0.02 |
6.435 |
6.41 |
6.4 |
0.02 |
0.03 |
|
16 |
3.742 |
3.72 |
3.71 |
0.02 |
0.03 |
17 |
6.022 |
5.98 |
5.98 |
0.04 |
0.04 |
18 |
3.937 |
3.89 |
3.89 |
0.05 |
0.05 |
19 |
8.12 |
8.12 |
8.1 |
0.00 |
0.02 |
14.411 |
14.40 |
14.39 |
0.01 |
0.02 |
|
20 |
6.077 |
6.03 |
6.03 |
0.05 |
0.05 |
21 |
13.696 |
13.66 |
13.64 |
0.04 |
0.06 |
RMSE: DS1=0.0308m,DS2=0.0249m |
Variabiles experimentorum 1 sunt:
1: With/Sine PPK data.
2: With/Sine GCPs.
III, GSD:1,5 cm vel 2cm
Post analysin quattuor notarum experimentalium, conclusiones sequentes colligere possumus:
Cum camera obliqua est DG4Pros;
(1) Cum/Sine loco continenti puncto (GCP) et PPK data in AT triangula implicata, sive VTOL vel fucus multi-rotor, sive GSD sit 2cm vel 1.5cm, exemplar 3D a camera obliqua DG4Pros aedificatum. cum requisitis accurate relativi erroris Ds≤10cm (Actu ≤5cm).
(2) Cum GSD singularis sit variabilis, certior relativus exemplaris 3D cum GSD=1.5cm melior est quam GSD=2cm.
Obliquus camera |
GCPs |
PPK |
GSD |
DG4pros |
NO |
NO |
1.5cm |
Numerus rerum |
mensurae longitudinis (L0" |
Exemplum longitudo 3D(L1)CW10 |
exemplum longitudinis 3DL2)M600Pro |
DS1(L0-L1) |
DS2(L0-L2) |
1 |
7.21 |
7.20 |
7.19 |
0.013 |
0.02 |
8.706 |
8.65 |
8.70 |
0.093 |
0.01 |
|
10.961 |
10.90 |
10.91 |
0.093 |
0.05 |
|
2 |
7.01 |
6.86 |
6.98 |
0.150 |
0.03 |
3 |
1.822 |
1.76 |
1.79 |
0.093 |
0.03 |
4 |
10.41 |
10.37 |
10.39 |
0.041 |
0.02 |
5 |
10.718 |
10.68 |
10.69 |
0.038 |
0.03 |
6 |
13.787 |
13.71 |
13.76 |
0.077 |
0.03 |
7 |
11.404 |
11.38 |
11.38 |
0.024 |
0.02 |
12.147 |
12.12 |
12.12 |
0.027 |
0.03 |
|
8 |
7.526 |
7.49 |
7.50 |
0.093 |
0.03 |
13.797 |
13.77 |
13.77 |
0.027 |
0.03 |
|
9 |
10.374 |
10.35 |
10.33 |
0.024 |
0.04 |
10 |
2.109 |
2.09 |
2.02 |
0.019 |
0.09 |
4.281 |
4.19 |
4.20 |
0.093 |
0.08 |
|
11 |
14.675 |
14.64 |
14.65 |
0.035 |
0.03 |
8.6 |
8.57 |
8.57 |
0.030 |
0.03 |
|
12 |
13.394 |
13.38 |
13.35 |
0.014 |
0.04 |
13 |
12.94 |
12.91 |
12.92 |
0.030 |
0.02 |
14 |
7.19 |
7.20 |
7.17 |
-0.010 |
0.02 |
15 |
13.371 |
13.38 |
13.35 |
-0.009 |
0.02 |
6.435 |
6.43 |
6.41 |
0.005 |
0.02 |
|
16 |
3.742 |
3.70 |
3.70 |
0.041 |
0.04 |
17 |
6.022 |
5.99 |
5.99 |
0.093 |
0.03 |
18 |
3.937 |
3.94 |
3.89 |
-0.003 |
0.05 |
19 |
8.12 |
8.12 |
8.08 |
0.000 |
0.04 |
14.411 |
14.37 |
14.36 |
0.041 |
0.05 |
|
20 |
6.077 |
6.04 |
6.06 |
0.093 |
0.02 |
21 |
13.696 |
13.65 |
13.65 |
0.041 |
0.05 |
RMSE: DS1=0.0356m,DS2=0.342m |
Obliquus camera |
GCPs |
PPK |
GSD |
DG4pros |
ETIAM' |
NO |
1.5cm |
Numerus rerum |
mensurae longitudinis (L0" |
Exemplum longitudo 3D(L1)CW10 |
exemplum longitudinis 3DL2)M600Pro |
DS1(L0-L1) |
DS2(L0-L2) |
1 |
7.21 |
7.21 |
7.21 |
0 |
0.00 |
8.706 |
8.68 |
8.70 |
0.024 |
0.01 |
|
10.961 |
10.87 |
10.91 |
0.093 |
0.05 |
|
2 |
7.01 |
6.88 |
6.98 |
0.13 |
0.03 |
3 |
1.822 |
1.76 |
1.80 |
0.093 |
0.02 |
4 |
10.41 |
10.38 |
10.39 |
0.03 |
0.02 |
5 |
10.718 |
10.72 |
10.70 |
-0.002 |
0.02 |
6 |
13.787 |
13.79 |
13.75 |
-0.003 |
0.04 |
7 |
11.404 |
11.38 |
11.38 |
0.024 |
0.02 |
12.147 |
12.13 |
12.13 |
0.017 |
0.02 |
|
8 |
7.526 |
7.53 |
7.49 |
-0.004 |
0.04 |
13.797 |
13.78 |
13.79 |
0.017 |
0.01 |
|
9 |
10.374 |
10.37 |
10.35 |
0.004 |
0.02 |
10 |
2.109 |
2.11 |
2.07 |
-0.001 |
0.04 |
4.281 |
4.28 |
4.21 |
0.001 |
0.07 |
|
11 |
14.675 |
14.67 |
14.66 |
0.005 |
0.02 |
8.6 |
8.58 |
8.57 |
0.02 |
0.03 |
|
12 |
13.394 |
13.39 |
13.35 |
0.004 |
0.04 |
13 |
12.94 |
12.9 |
12.93 |
0.04 |
0.01 |
14 |
7.19 |
7.19 |
7.18 |
0 |
0.01 |
15 |
13.371 |
13.37 |
13.36 |
0.001 |
0.01 |
6.435 |
6.42 |
6.42 |
0.014 |
0.01 |
|
16 |
3.742 |
3.7 |
3.71 |
0.041 |
0.03 |
17 |
6.022 |
5.98 |
6.00 |
0.041 |
0.02 |
18 |
3.937 |
3.91 |
3.91 |
0.027 |
0.03 |
19 |
8.12 |
8.07 |
8.10 |
0.05 |
0.02 |
14.411 |
14.38 |
14.35 |
0.031 |
0.06 |
|
20 |
6.077 |
6.04 |
6.06 |
0.093 |
0.02 |
21 |
13.696 |
13.65 |
13.67 |
0.041 |
0.03 |
RMSE: DS1=0.0259m,DS2=0.256m |
Variabiles experimentorum 2 sunt:
1: With/Sine GCPs.
II: Diversus Portitorem fucum: a VTOL fucus vel multi-rotor fucus
Post analysim ambarum notitiarum experimentalium, conclusiones sequentes colligere possumus:
Cum camera obliqua est DG4Pros;
(1) Cum/Sine loco ditionis puncto (GCP) utrum fucus VTOL vel multi-rotor sit, exemplar 3D ex obliqua camera DG4Pros constructum exigentiis accurationis relativi erroris Ds≤10cm (Actu ≤5cm).
(2) Cum tabellarius fucus typi singularis variabilis est, accuratio relativa exemplaris 3D cum multi-rotor melior est quam cum VTOL, sed differentia non magna est.