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Articulus

Articulus
Quomodo GSD et tabellarius fucum genera afficiunt accurate relativum exemplar 3D?

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.

Experimentum 1: effectus GSD in accuratione relativa exemplar 3D;

Conditio 1

Carrier fucus

Obliquus camera

GCPs

PPK

 CW10 VTOL

DG4pros

NO

NO

Proventus Table 1:

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

Conditio 2

Carrier fucus

Obliquus camera

GCPs

PPK

CW10 VTOL

DG4pros

Ita

No

Proventus Tabula 2:

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

Conditio 3

Carrier fucus

Obliquus camera

GCPs

PPK

CW10 VTOL

DG4pros

NO

ETIAM'

 

Proventus Table 3

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

Conditio 4

Carrier fucus

Obliquus camera

GCPs

PPK

CW10 VTOL

DG4pros

ETIAM'

ETIAM'

Proventus Tabula 4:

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

conclusiones

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.

Experimentum 2: effectus tabellarii fuci typi in accuratione relativi exemplaris 3D

Conditio 1

Obliquus camera

GCPs

PPK

GSD

DG4pros

NO

NO

1.5cm

Proventus Table 1:

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

Conditio 2

Obliquus camera

GCPs

PPK

GSD

DG4pros

ETIAM'

NO

1.5cm

 

Proventus Tabula 2:

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

conclusiones

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.