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Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis Programs Stennis Space Center ASPRS 2004 Annual Conference and Technology Exhibition Denver, CO, May 23-28, 2004 USGS & NASA Digital Imagery USGS & NASA Digital Imagery Product Characterization Product Characterization
58

Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

Jan 13, 2016

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Page 1: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

Vicki ZanoniNASA Earth Science Applications Directorate

Stennis Space Center

Charles Smith, Slawomir BlonskiLockheed Martin Space Operations – Stennis Programs

Stennis Space Center

ASPRS 2004 Annual Conference and Technology ExhibitionDenver, CO, May 23-28, 2004

USGS & NASA Digital Imagery USGS & NASA Digital Imagery Product CharacterizationProduct Characterization

Page 2: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

2ASPRS, Denver, May 2004

Partnership Overview

• USGS and NASA are jointly developing an airborne digital imagery characterization capability– Supports USGS future procurement and cooperative partnerships

for digital imagery acquisition– Enables digital data providers the ability to sell products to a larger

market– Provides NASA with access to high spatial resolution imagery for

development of new characterization techniques

• NASA - USGS Space Act Agreement signed January 2003– USGS Role: Define characterization requirements, interface with

industry, provide certification– NASA Role: Perform product characterization using Stennis test

range

Page 3: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

3ASPRS, Denver, May 2004

USGS-NASA Product Characterization Approach

• Vendors acquire data over Stennis characterization range

• Vendors provide common data package to Stennis

• Stennis personnel perform geopositional and spatial response characterization analyses– Radiometric characterization to be performed in the future

• Document results in report and delivery to USGS

Page 4: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

4ASPRS, Denver, May 2004

Stennis Characterization Range

• The Stennis characterization range is built within the Stennis “Fee Area” – Approximately 5 mi. x 5 mi. in size– Relatively flat terrain

• ~14 meter change in elevation across site

– Land cover:• Buildings• Roads• Canals• Pine Forests• Wetlands• Open grass

– Characterization Targets• Geodetic network• Concrete edge targets• Radiometric targets and atmospheric instrumentation

Page 5: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

5ASPRS, Denver, May 2004

Stennis Geodetic Targets

• Currently 45 targets located throughout Stennis Space Center (SSC) “Fee Area”

• Targets are 2.44 m in diameter painted white with a 0.6 m red center

• Target centers have been geolocated by Global Positioning System (GPS) to <3 cm accuracy

Page 6: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

6ASPRS, Denver, May 2004

Stennis Manhole Covers

• 136 painted/surveyed man-hole covers located throughout SSC fee area

• Paint reflectance nominally 50% • Manhole cover diameters range between 0.6 and 2.9

meters• Manhole cover centers have been geolocated by GPS to

<3 cm horizontal accuracy

Page 7: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

7ASPRS, Denver, May 2004

Stennis Edge Target

4 deg

~50% reflective

~5%reflective

10 m

20 m

10 m

20 m

Lat/lon:30 23 10.1N89 37 43.6W

N

Page 8: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

8ASPRS, Denver, May 2004

Stennis Characterization Site

Page 9: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

9ASPRS, Denver, May 2004

Delivered Data

• Vendors provide common data package to Stennis– Panchromatic and/or multispectral (RGB) imagery– Smallest ground sample distance (GSD) that vendor

plans to sell to USGS, and no greater than 1-meter GSD

– Orthorectified and mosaicked imagery• Standard USGS National Elevation Dataset (NED)

digital elevation model (DEM)• Ground Control

– Five ground control point locations are provided to the vendors

– Locations of points are approximately in each corner and the center of the Fee Area

– Uncompressed or lossless compression– NAD83 datum– Federal Geographic Data Committee (FGDC)

compliant metadata format– UTM Zone 16– Compatible with common RS software packages

Temporary Tarp TargetUsed for GCPs provided to vendors

0.91m diameter<3 cm survey accuracy

Page 10: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

10ASPRS, Denver, May 2004

Other Data Considerations

• Radiometric Response

– Dynamic range must be such that objects with reflectance of 5% and 50% are imaged without saturation.

– Radiometric response cannot differ by more than 1% over a uniform area for pixels separated by less than 20 meters.

• Image Registration

– Images resampled using the cubic-convolution or bilinear interpolation can be used directly for spatial resolution characterization.

– Images resampled with the nearest-neighbor method can be used only when the resampling results in a uniform shift of the entire image or when precise data on the original geolocation of each pixel is available.

– Otherwise, non-resampled images must be provided for the analysis.

To perform spatial response assessments, delivered data products must have the following characteristics:

Page 11: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

11ASPRS, Denver, May 2004

Status

• EarthData Technologies– Acquired Leica ADS40 data in November 2002– Geopositional and spatial assessment completed

• Emerge– Acquired Digital Sensor System (DSS) data in January 2003 – Geopositional assessment completed and presented at 2003

ASPRS conference– Spatial assessment could not be performed because of data

saturation over edge target

• Northwest Geomatics – Acquired Leica ADS40 data in October 2003 – Awaiting data delivery

Page 12: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

12ASPRS, Denver, May 2004

Status (cont’d.)

• Space Imaging– Acquired Digital Airborne Imagery System (DAIS) data in

November 2003– Geopositional and spatial assessments completed

• Space Imaging– Acquired IKONOS satellite image on December 5, 2003– Geopositional and spatial assessments completed

• Aerometric– Acquired Zeiss DMC data in February 2004– Awaiting data delivery

Page 13: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

13ASPRS, Denver, May 2004

Geopositional Assessment Approach

• Locations of geodetic targets and manhole covers identified in the imagery are compared to “true” locations of the targets

• Positional differences are calculated from the ground truth data to the same points in the image being evaluated

• From these differences statistics are calculated• The following equations should be used if there is no bias present in

the dataset.

These equations may be found in FGDC-STD-007.3-1998

2y

2xnet

2

y

2

x

RMSERMSE RMSE

)( RMSE

)( RMSE

zation Characteri Imagefor UsedTargetsInput ofNumber

Y Delta Northing

Delta Easting

n

Y

n

X

n

YY

XXX

controlinput

controlinput

yx95

yx90

RMSERMSE2

4477.2 CE

RMSERMSE2

1460.2 CE

Page 14: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

14ASPRS, Denver, May 2004

Geopositional AssessmentApproach (cont’d.)

• To calculate bias:

These equations may be found in FGDC-STD-007.3-1998, (Greenwalt, C.R. and M.E. Shultz, 1962), (Shultz, M.E., 1963), and (Ager, T.P., 2004).

• To calculate standard deviation (random error):

Page 15: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

15ASPRS, Denver, May 2004

• If

– then there is a bias present in the data and the previous FGDC equations should not be used

• The following equations should be used if there is a bias present in the dataset.

Geopositional AssessmentApproach (cont’d.)

1.0/ CH

These equations may be found in, (Greenwalt, C.R. and M.E. Shultz, 1962), (Shultz, M.E., 1963), and (Ager, T.P., 2004).

RCE

RCE

YXR

%95 Empirical

%90 Empirical

Delta Total

95

90

22

Page 16: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

16ASPRS, Denver, May 2004

Spatial Assessment Approach

Relative Edge Response (RER) is estimated using Stennis edge target and a tilted edge technique

• RER is one of the engineering parameters used in the General Image Quality Equation (GIQE) to provide predictions of imaging system performance expressed in terms of the National Imagery Interpretability Rating Scale (NIIRS).

• RER is a geometric mean of normalized edge response differences measured in two directions of image pixels (X and Y) at points distanced from the edge by -0.5 and 0.5 GSD.

Page 17: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

17ASPRS, Denver, May 2004

Spatial Assessment Approach

)]5.0()5.0()][5.0()5.0([ YYXX ERERERERRER

RER estimates effective slope of the imaging system’s edge response because distance between the points for which the differences are calculated is equal to the GSD.

Page 18: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

18ASPRS, Denver, May 2004

Spatial Assessment Approach

• Edge responses are measured using a tilted-edge technique in which the response functions were approximated with a linear combination of an odd number of sigmoidal functions (chosen between 3 and 15 for the best fit).

• In the tilted-edge method, the edge target is intentionally oriented such that on an image, the edge is aligned slightly off-perpendicular to a pixel grid direction.

• Use of the tilted edge overcomes the main difficulty in applying the edge response method to digital images inherently based on limited, discrete spatial sampling.

• A small edge tilt causes pixels from adjacent lines to have their distance from the edge shifted by a fraction of the sampling distance.

• When shifted pixels from different lines are superimposed during the edge response analysis, the effective sampling distance of the derived edge response is smaller then that of the original image.

Page 19: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

19ASPRS, Denver, May 2004

Edge Response

Problem: Digital cameras undersample edge target

Solution: Image tilted edge to improve sampling

Superposition of 24 edge responses shifted to compensate for the tilt

3 examples of undersampled

edge responses measured across

the tilted edge

– edge tilt angle

– pixel index

x – pixel’s distance from edge (in GSD)

Page 20: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

Results to Date

Page 21: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

21ASPRS, Denver, May 2004

EarthDataADS40 Sensor and Data

• ADS40 Sensor System– System manufacturer: Leica– Array Size: 12000 x 1 pixels– GSD: 0.15–0.6 m (typical, platform, and altitude dependent) – Spectral bands: 0.47–0.68 µm (Pan), 0.43–0.49 µm (Blue),

0.54–0.59 µm (Green), 0.61–0.66 µm (Red), 0.84–0.89 µm (NIR) – Direct Georeferencing System: ADS40 internal– Platform: Piper Navajo Chieftain

• Delivered dataset: Pan, NIR, and RGB orthorectified imagery acquired November 2002– 0.25-meter GSD– GeoTIFF format– NED DEM– No ground control provided

Page 22: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

22ASPRS, Denver, May 2004

EarthData ADS40 Sample Data

Very small portion of one ADS40 data tile showing an SSC geodetic target

0.25m (~10 in) GSD

Geodetic Target

Page 23: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

23ASPRS, Denver, May 2004

EarthData ADS40Geopositional Assessment Results

RGB 0.25 m GSD datasetused in analysis

Evaluated against SSC test control• 183 ground targets located

Bias is present in the data:• μH = 0.20 m• σC = 0.15 m• μH / σC = 1.36

Must use empirical calculations:CE90: 0.43 m (~16.9 in)CE95: 0.49 m (~19.3 in)

Page 24: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

24ASPRS, Denver, May 2004

EarthData ADS40Geopositional Assessment Results

Geodetic target residuals (manholes not included).Vectors have been enlarged for visibility purposes. Vector magnitudes are

not absolute.

Page 25: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

25ASPRS, Denver, May 2004

EarthData ADS40Spatial Assessment Results

8-bit, 0.25-meter GSD panchromatic images used in analysis

Image area selected for spatial responsemeasurement in Easting direction

Image area selected for spatial responsemeasurement in Northing direction

Page 26: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

26ASPRS, Denver, May 2004

EarthData ADS40Spatial Assessment Results

Edge responses measured for the panchromatic image

Easting direction

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.47

Distance / GSD

Norm

aliz

ed E

dge R

esp

onse

06_BW_TARGET.tif

Northing direction

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

ER(0.5) - ER(-0.5)= 0.51

Distance / GSDN

orm

aliz

ed E

dge R

esp

onse

06_BW_TARGET.tif

Page 27: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

27ASPRS, Denver, May 2004

EarthData ADS40Spatial Assessment Results

EastingDirection

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

ER(0.5) - ER(-0.5)= 0.58

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_IR_TARGET.tif

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.60

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_RGB_TARGET.tif : Band 1

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.53

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_RGB_TARGET.tif : Band 2

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

ER(0.5) - ER(-0.5)= 0.37

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_RGB_TARGET.tif : Band 3

NIR band

Blue bandGreen band

Red band

Page 28: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

28ASPRS, Denver, May 2004

EarthData ADS40Spatial Assessment Results

NorthingDirection

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.65

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_IR_TARGET.tif

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.48

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_RGB_TARGET.tif : Band 1

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.57

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_RGB_TARGET.tif : Band 2

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.41

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

06_RGB_TARGET.tif : Band 3

NIR band

Blue bandGreen band

Red band

Page 29: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

29ASPRS, Denver, May 2004

EarthData ADS40Spatial Assessment Results

• The mean RER for all bands is approximately 0.5.• Uncertainty of spatial resolution characterization results was increased

by the higher level of noise present in images of the dark panels of the edge targets, in comparison to images of the bright panels.

• This does not follow usual performance of detector-noise-limited imaging systems (equal noise) or photon-noise-limited systems (noise higher for the bright panels).

• It may be an indication of a non-linear (e.g., logarithmic-like) radiometric response of the EarthData’s ADS40 system.

Band REREasting Direction Northing Direction

Pan 0.47 0.51 0.5NIR 0.58 0.65 0.6Red 0.60 0.48 0.5

Green 0.53 0.57 0.6Blue 0.37 0.41 0.4

ER(0.5) - ER(-0.5)

Page 30: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

30ASPRS, Denver, May 2004

Space ImagingDAIS Sensor and Data

• DAIS Sensor System– System Manufacturer: Dalsa– Lens Manufacturer: Nikon– Array Size: 1024 x 1024 pixels– GSD: 0.5–2 m (platform and altitude dependent) – Spectral bands: 0.45–0.53 µm (Blue), 0.52–0.61 µm (Green), 0.64–0.72 µm (Red),

0.77–0.88 µm (NIR)– Direct Georeferencing System: Applanix POS AV– Platform: Cessna 421C

• Delivered dataset: RGB orthorectified imagery acquired November 2003– 1-meter GSD 12-bit and 8-bit multispectral (4 separate bands)– 1-meter GSD 8-bit true color and false color composites– 0.5-meter GSD 8-bit and 16-bit multispectral (4 separate bands)– 0.5-meter GSD 8-bit true color and false color composites– GeoTIFF and ERDAS IMAGINE formats– NED DEM

Page 31: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

31ASPRS, Denver, May 2004

DAIS Sample Data

Very small portion of one DAIS data tile showing an SSC geodetic target

0.5m (~20 in.) GSD

Geodetic Target

Page 32: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

32ASPRS, Denver, May 2004

Space Imaging DAISGeopositional Assessment Results

RGB true color 0.5 m GSD, 8-bit dataset was used for this assessment

Evaluated against SSC testcontrol•158 ground targets located

Slight bias is present in the data:•μH = 0.04 m•σC = 0.34 m•μH / σC = 0.12

Must use empirical calculations•CE90: 0.74 m (~29.1 in)•CE95: 0.81 m (~31.9 in)

Page 33: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

33ASPRS, Denver, May 2004

Space Imaging DAISGeopositional Assessment Results

Geodetic target residuals (manholes not included).Vectors have been enlarged for visibility purposes. Vector magnitudes are

not absolute.

Page 34: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

34ASPRS, Denver, May 2004

Space Imaging DAISSpatial Assessment Results

16-bit, 0.5-meter GSD multispectral imagery used in analysis

Blue band is shown

Image area selected for spatial response measurement in Easting direction

Page 35: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

35ASPRS, Denver, May 2004

Space Imaging DAISSpatial Assessment Results

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.89

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b1.tif

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.88

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b2.tif

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.49

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b3.tif

EastingDirection

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.64

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b4.tif

Blue band

NIR band

Green band

Red band

Page 36: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

36ASPRS, Denver, May 2004

Space Imaging DAISSpatial Assessment Results

16-bit, 0.5-meter GSD multispectral imagery used in analysis

Blue band is shown

Image area selected for spatial response measurement in Northing direction

Page 37: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

37ASPRS, Denver, May 2004

Space Imaging DAISSpatial Assessment Results

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.83

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b4.tif

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

1.4

ER(0.5) - ER(-0.5)= 0.80

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b1.tif

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.63

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b2.tif

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.44

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

3282003e_trm_TARGET_b3.tif

NorthingDirection Blue band

NIR band

Green band

Red band

Page 38: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

38ASPRS, Denver, May 2004

Space Imaging DAISSpatial Assessment Results

• The mean RER for all bands is approximately 0.7.• RER for the red band differs from the other bands.

– This may negatively affect comparisons of the red band image with the other bands such as with the NIR band in calculations of the Normalized Difference Vegetation Index (NDVI).

• Uncertainty of spatial resolution characterization results were increased by using nearest-neighbor resampling in processing of the provided DAIS image products.

• The uncertainty was also enlarged by small (~3%) non-uniformity of radiometric response (“banding”) observed in the images (mainly for the blue band).

Band REREasting Direction Northing Direction

blue 0.89 0.80 0.8green 0.88 0.63 0.7

red 0.49 0.44 0.5NIR 0.64 0.83 0.7

ER(0.5) - ER(-0.5)

Page 39: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

39ASPRS, Denver, May 2004

IKONOS Sensor and Data

• IKONOS Sensor System– System manufacturer: Eastman Kodak– Lens Manufacturer: Eastman Kodak– Array Size: 11300 x 1 pixels– GSD: 1 m (Pan), 4 m (Multispectral)– Spectral bands: 0.45–0.90 µm (Pan), 0.45–0.52 µm (Blue),

0.51–0.60 µm (Green), 0.63–0.70 µm (Red), 0.76–0.85 µm (NIR)– Platform: IKONOS Satellite

• Delivered dataset: Pan and RGB “Precision” imagery acquired on December 5, 2003– 1.0-meter GSD (Pan), and 4.0-meter GSD (MSi)– GeoTIFF format– NED DEM

Page 40: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

40ASPRS, Denver, May 2004

Space Imaging IKONOS Sample Data

Very small portion of the IKONOS panchromatic image showing an SSC geodetic target

~1 m GSD

Geodetic Target

Page 41: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

41ASPRS, Denver, May 2004

Space Imaging IKONOSGeopositional Assessment Results

Pan 1.0 m GSD dataset used in analysis

Evaluated against SSC testcontrol• 42 ground targets located

Bias is present in the data:• μH = 0.61 m• σC = 0.51 m• μH / σC = 1.20

Must use empirical calculations:CE90: 1.44 m (~56.7 in)CE95: 1.54 m (~60.6 in)

Page 42: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

42ASPRS, Denver, May 2004

Space Imaging IKONOSGeopositional Assessment Results

Geodetic target residuals (manholes not included).Vectors have been enlarged for visibility purposes. Vector magnitudes are

not absolute.

Page 43: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

43ASPRS, Denver, May 2004

Space Imaging IKONOSSpatial Assessment Results

11-bit, 1.0-meter GSD panchromatic images with MTFC used in analysis

Image area selected for spatial responsemeasurement in Easting direction

Image area selected for spatial responsemeasurement in Northing direction

Page 44: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

44ASPRS, Denver, May 2004

Space Imaging IKONOSSpatial Assessment Results

Edge responses measured for the panchromatic image

Easting direction

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.85

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

po_142257_pan_0000000_TARGET.tif

Northing direction

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2-0.2

0

0.2

0.4

0.6

0.8

1

1.2

ER(0.5) - ER(-0.5)= 0.65

Distance / GSD

Nor

mal

ized

Edg

e R

espo

nse

po_142257_pan_0000000_TARGET.tif

Page 45: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

45ASPRS, Denver, May 2004

Space Imaging IKONOSSpatial Assessment Results

Band REREasting Direction Northing Direction

pan 0.85 0.65 0.7

ER(0.5) - ER(-0.5)

Only the panchromatic image product was evaluated because of limitations imposed by size of the edge targets

Page 46: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

46ASPRS, Denver, May 2004

Next Steps

• Perform geopositional and spatial assessments for the following systems, upon data delivery:– NW Geomatics (ADS40)– Aerometric (DMC)

• Perform absolute radiometric assessments– Coordinate acquisition window that can accommodate multiple

systems in order to minimize costs of analysis

• Perform geopositional assessment of 3001, Inc., LIDAR data

Page 47: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

Questions???

Page 48: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

Backup

Page 49: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

49ASPRS, Denver, May 2004

Points of Contact

Greg StensaasUSGS Eros Data Center

Sioux Falls, SCPh: [email protected]

George LeeUSGS National Mapping Program

Menlo Park, CAPh: [email protected]

Vicki ZanoniNASA Earth Science Applications Directorate

Stennis Space Center, MSPh: 228-688-2305

[email protected]

Page 50: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

50ASPRS, Denver, May 2004

Significance of RER

RER also characterizes applicability of digital camera image products in quantitative remote sensing such as thematic mapping based on image classification.• For such tasks, a digital raster image of Earth’s surface is thought to divide the surface

into a grid of square pixels with size of each pixel being equal to GSD.• Radiance measured for each pixel is assumed to come from the Earth’s surface area

represented by that pixel. • However, due to many factors, actual measurements integrate radiance from the

entire surface with a weighting function provided by a system’s point spread function (PSF).

• It can be shown that the Relative Edge Response squared (RER2) may be used to assess the percentage of the measured pixel radiance which actually originates from the Earth’s surface area represented by the pixel.

Page 51: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

51ASPRS, Denver, May 2004

RER References

• J.C. Leachtenauer, W. Malila, J.M. Irvine, L.P. Colburn, and N.L. Salvaggio, “General Image-Quality Equation: GIQE,” Applied Optics, 36 (1997) 8322.

• “Multispectral Imagery Reference Guide,” LOGICON Geodynamics, Fairfax, Virginia, 1997.

• See also: – http://www.fas.org/irp/imint/niirs_c/index.html – http://www.fas.org/irp/imint/niirs_ms/index.html

Page 52: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

52ASPRS, Denver, May 2004

Geolocational Accuracy References

• Ager, T.P., 2004. An Analysis of Metric Accuracy Definitions and Methods of Computation, an internal report of InnoVision in support of the National Geospatiol-Intelligence Agency. 13 pp.

• Federal Geographic Data Committee, Geospatial Positioning Accuracy Standards Part 3: National Standard for Spatial Data Accuracy (FGDC-STD-007.3-1998, 1998).

• Greenwalt, C.R. and M.E. Shultz, 1962. Principles of Error Theory and Cartographic Applications (ACIC Technical Report No. 96, 1962).

• Leachtenauer, J.C., W. Malila, J.M. Irvine, L.P. Colburn, and N.L. Salvaggio, “General Image-Quality Equation: GIQE,” Applied Optics, 36 (1997) 8322.

• “Multispectral Imagery Reference Guide”, LOGICON Geodynamics, Fairfax, Virginia, 1997.

• Schowengerdt, R.A., “Remote Sensing: Models and Methods for Image Processing,” 2nd Ed., Academic Press, San Diego, California, 1997, Chapter 3.

• Shultz, M.E, 1963. Circular Error Probability of a Quantity Affected by a Bias, an internal report of the Geophysical Studies Section, Geo-Sciences Branch of the United States Air Force Aeronautical and Chart Information Center, St. Louis, Missouri, 25 pp.

• See also: • http://www.fas.org/irp/imint/niirs_c/index.html • http://www.fas.org/irp/imint/niirs_ms/index.html

Page 53: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

53ASPRS, Denver, May 2004

Emerge Sensor and Data

• Digital Sensor System (DSS)– System Manufacturer: Emerge– Lens Manufacturer: Zeiss– Array Size: 4092 x 4079 pixels– GSD: 0.10–1 m (platform and altitude dependent) – Spectral bands:

• Color mode: 0.4–0.5 µm (Blue), 0.5–0.6 µm (Green), 0.6–0.68 µm (Red)• Color Infrared mode: 0.51–0.6 µm (Green), 0.6–0.7 µm (Red), 0.8–0.9 µm (NIR)

– Direct Georeferencing System: Applanix POS AV– Platform: Cessna 172

• Delivered dataset– RGB orthorectified imagery acquired January 2003

• 0.3-meter nominal GSD (~11.8 in)• GeoTIFF format (28 scenes to create mosaic)• No control used• NED DEM

Page 54: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

54ASPRS, Denver, May 2004

Emerge DSSSample Product Tile

Very small portion of one Emerge data tile showing an SSC geodetic target

~I ft. GSD

Geodetic Target

Page 55: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

55ASPRS, Denver, May 2004

Emerge DSSGeopositional Assessment Results

Evaluated against SSC testcontrol• 150 targets located

Bias is present in the data:• μH = 0.03 m• σC = 0.22 m• μH / σC = 0.14

Must use empirical calculations:

• CE90: 0.45 m (~17.7 in)• CE95: 0.54 m (~21.3 in)

Page 56: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

56ASPRS, Denver, May 2004

Emerge DSSGeopositional Assessment Results

Geodetic target residuals (manholes not included).Vectors have been enlarged for visibility purposes. Vector magnitudes are

not absolute.

Page 57: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

57ASPRS, Denver, May 2004

Sigma_c versus Sigma_h

sigma_x sigma_y sigma_C sigma_H1 1 1 11 0.95 0.975 0.975321 0.9 0.95 0.9513151 0.85 0.925 0.9280361 0.8 0.9 0.9055391 0.75 0.875 0.8838831 0.7 0.85 0.8631341 0.65 0.825 0.8433561 0.6 0.8 0.8246211 0.55 0.775 0.8070011 0.5 0.75 0.7905691 0.45 0.725 0.7754031 0.4 0.7 0.7615771 0.35 0.675 0.7491661 0.3 0.65 0.7382411 0.25 0.625 0.7288691 0.2 0.6 0.721111 0.15 0.575 0.7150171 0.1 0.55 0.7106341 0.05 0.525 0.70799

0.4

0.5

0.6

0.7

0.8

0.9

1.0

0 0.2 0.4 0.6 0.8 1

sigma_y

sig

ma

_to

tal

sigma_C

sigma_H

Page 58: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.

58ASPRS, Denver, May 2004

General Imagery Quality Equation

• The GIQE mathematically relates NIIRS to several parameters as a means of quantifying image quality

SNR

GHRERbGSDaNIIRS GMGMGM

344.0656.0loglog251.10 1010

where

GSDGM is the geometric mean of the ground sampled distance,

RERGM is the geometric mean of the relative edge response,

HGM is the geometric mean-height overshoot caused by MTFC (Leachtenauer et al., 1997), and

G is the noise gain associated with MTFC. In the current form of the GIQE,

SNR is estimated for differential radiance levels from Lambertian scenes with reflectances of 7% and 15% with the noise estimated from photon, detector, and uniformity noise terms.

If the RER exceeds 0.9, then a equals 3.32 and b equals 1.559; otherwise, a equals 3.16 and b equals 2.817.