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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/1.jpg)
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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/3.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/4.jpg)
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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/6.jpg)
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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/8.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/9.jpg)
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
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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:
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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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/13.jpg)
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
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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):
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/16.jpg)
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.
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/18.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/19.jpg)
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)
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Results to Date
![Page 21: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/21.jpg)
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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/23.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/24.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/25.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/26.jpg)
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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/28.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/29.jpg)
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)
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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
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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
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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)
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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.
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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
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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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/37.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/38.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/39.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/40.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/41.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/42.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/43.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/44.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/45.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/46.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/47.jpg)
Questions???
![Page 48: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/48.jpg)
Backup
![Page 49: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/49.jpg)
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
![Page 50: Vicki Zanoni NASA Earth Science Applications Directorate Stennis Space Center Charles Smith, Slawomir Blonski Lockheed Martin Space Operations – Stennis.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/50.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/51.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/52.jpg)
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
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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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/54.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/55.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/56.jpg)
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.](https://reader035.fdocuments.us/reader035/viewer/2022081420/56649eb05503460f94bb64e3/html5/thumbnails/57.jpg)
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
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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.