Chengdu Rainpoo Technology Co., Ltd.

Chengdu Rainpoo Technology Co., Ltd.

Chengdu Rainpoo Technology Co., Ltd.

Corporate News

articuli

articuli
Quam GSD carrier et pabula fucus exemplum 3D types afficit sensu respectivo subtiliter

In novissimis articulum Quam terram imperium puncta et PPK data afficit sensu respectivo accurate de 3D exemplum, siquidem hi quos diximus, ut praeter GCPs et PPK datas, ad GSD et carrier pabula fucus item in tali gradu effectus, in relative accurate de 3D test cognoscere illam ad se model.So faciemus.

Experimentum I: De GSD ad effectum respectu ad exemplar diligenter de 3D;

I conditione,

carrier pabula fucus

Medium Oblique camera

GCPs

PPK

 CW10 VTOL

DG4pros

NON

NON

Consequuntur Tabula I:

Secundum numerum objectorum,

longitudinis mensura (i0)

Longitudo exemplum 3D (L1) = GSD 2cm

Longitudo exemplum 3D (L2) = GSD 1.5cm

DS1 (L0-L1)

DS2 (L2, i0)

1

7,210

7,18

7.20

0.030

0.010

 

8,706

8-69

8.65

0.016

0.056

 

10,961

10.89

10.90

0.071

0.061

2

7,010

6.88

6.86

0.130

0.150

3

1,822

1,76

1,76

0.062

0.062

4

10,410

10,38

10,37

0.030

0.040

5

10,718

10.65

10.68

0.068

0.038

6

13,787

13.72

13.71

0.067

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

0.086

0.036

 

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

0.091

11

14,675

14.55

14.64

0.125

0.035

 

8,600

8.58

8.57

0.020

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

0.065

0.005

16

3,742

3.74

3,70

0.002

0.042

17

6,022

6.03

5.99

-0,008

0.032

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

0.037

21

13,696

13.68

13.65

0.016

0.046

RMSE: DS1 = 0.0397m, DS2 0.0356m =

II conditione,

carrier pabula fucus

Medium Oblique camera

GCPs

PPK

CW10 VTOL

DG4pros

Ita

nullum

Tabula II consequuntur:

Secundum numerum objectorum,

longitudinis mensura (i0)

Longitudo exemplum 3D (L1) = GSD 2cm

Longitudo exemplum 3D (L2) = GSD 1.5cm

DS1 (L0-L1)

DS2 (L2, i0)

1

7,210

7,18

7,21

0.030

0

 

8,706

8-68

8-68

0.026

0.026

 

10,961

10.91

10.87

0.051

0.091

2

7,010

6.92

6.88

0.090

0,13

3

1,822

1,79

1,76

0.032

0.062

4

10,410

10,39

10,38

0.020

0,03

5

10,718

10.66

10.72

0.058

-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

0.056

-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

0.079

-0.001

 

4,281

4,18

4.28

0.101

0.001

11

14,675

14,59

14.67

0.085

0.005

 

8,600

8.57

8.58

0.030

0.02

12

13,394

13.35

13.39

0.044

0.004

13

12,940

12.92

12,9

0.020

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

0.015

16

3,742

3,72

3,7

0.022

0.042

17

6,022

6.00

5.98

0.022

0.042

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

0.047

0.037

21

13,696

13.65

13.65

0.046

0.046

RMSE: DS1 = 0.0328m, DS2 0.0259m =

III conditione,

carrier pabula fucus

Medium Oblique camera

GCPs

PPK

CW10 VTOL

DG4pros

NON

ETIAM

 

Tabula III consequuntur:

Secundum numerum objectorum,

longitudinis mensura (i0)

Longitudo exemplum 3D (L1) = GSD 2cm

Longitudo exemplum 3D (L2) = GSD 1.5cm

DS1 (L0-L1)

DS2 (L2, i0)

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 =

IV conditione,

carrier pabula fucus

Medium Oblique camera

GCPs

PPK

CW10 VTOL

DG4pros

ETIAM

ETIAM

Tabula IV consequuntur:

Secundum numerum objectorum,

longitudinis mensura (i0)

Longitudo exemplum 3D (L1) = GSD 2cm

Longitudo exemplum 3D (L2) = GSD 1.5cm

DS1 (L0-L1)

DS2 (L2, i0)

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

In experimentum de I variables sunt:

I: With / PPK sine notitia.

II: Cum / Sine GCPs.

III: GSD alium: et 1.5 cm 2cm

Post quattuor analysi experimentalis notitia, possumus sic concludit:

 

Cum camera est DG4Pros obliquo;

(I), et / terram sine potestate punctum (GCP) et ad AT triangulation PPK involved in notitia, sive est a multi-rotor vel VTOL pabula fucus, utrum sit in 2cm GSD et 1.5cm, in exemplum 3D built obliquis figurationibus camera DG4Pros secundum quod exigit ratio videre possimus error accuracy Ds≤10cm (Quippe ≤5cm).

(II) cum GSD sit variabilis unius sustinetur, respectu ad exemplar diligenter de 3D = GSD 1.5cm melius quam GSD = 2cm.

Experimentum II: de generibus pabula fucus carrier effectus est in relative subtiliter exemplum 3D

I conditione,

Medium Oblique camera

GCPs

PPK

GSD

DG4pros

NON

NON

1.5cm

Consequuntur Tabula I:

Secundum numerum objectorum,

longitudinis mensura (i0)

Longitudo exemplum 3D (L1) CW10

Longitudo exemplum 3D (L2) M600Pro

DS1 (L0-L1)

DS2 (L2, i0)

1

7,21

7.20

7,19

0.010

0.02

 

8,706

8.65

8.70

0.056

0.01

 

10,961

10.90

10.91

0.061

0,05

2

7.01

6.86

6.98

0.150

0,03

3

1,822

1,76

1,79

0.062

0,03

4

10.41

10,37

10,39

0.040

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

0.036

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

0.091

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

0.042

0,04

17

6,022

5.99

5.99

0.032

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

0.037

0.02

21

13,696

13.65

13.65

0.046

0,05

RMSE: DS1 = 0.0356m, DS2 0.342m =

II conditione,

Medium Oblique camera

GCPs

PPK

GSD

DG4pros

ETIAM

NON

1.5cm

 

Tabula II consequuntur:

Secundum numerum objectorum,

longitudinis mensura (i0)

Longitudo exemplum 3D (L1) CW10

Longitudo exemplum 3D (L2) M600Pro

DS1 (L0-L1)

DS2 (L2, i0)

1

7,21

7,21

7,21

0

0.00

 

8,706

8-68

8.70

0.026

0.01

 

10,961

10.87

10.91

0.091

0,05

2

7.01

6.88

6.98

0,13

0,03

3

1,822

1,76

1,80

0.062

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

0.015

0.01

16

3,742

3,7

3,71

0.042

0,03

17

6,022

5.98

6.00

0.042

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

0.037

0.02

21

13,696

13.65

13.67

0.046

0,03

RMSE: DS1 = 0.0259m, DS2 0.256m =

Conclusiones

II In experimentum de variables sunt:

I: With / Sine GCPs.

II diversi Portitorem pabula fucus; VTOL ad pabula fucus aut multi-rotor pabula fucus

Postquam duobus experimentis analysi data possumus ita concludit:

 

Cum camera est DG4Pros obliquo;

(I), et / terram sine potestate punctum (GCP) vel est a multi-rotor vel VTOL pabula fucus, in exemplum 3D built DG4Pros camera potest obliquis figurationibus cum praesenti rerum incerti omnino error accuracy Ds≤10cm (Quippe ≤5cm).

(II) cum carrier types pabula fucus, est variabilis unius sustinetur, respectu subtiliter exemplum 3D cum multi-rotor cum ea VTOL melius est, manet tamen differentia non magni admodum.