System Characterization Report on Resourcesat-2 Linear Imaging Self Scanning-3 (LISS–3) Sensor

Open-File Report 2021-1030-H
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Executive Summary

This report addresses system characterization of the Indian Space Research Organisation Resourcesat-2 Linear Imaging Self Scanning-3 (LISS–3) sensor and is part of a series of system characterization reports produced and delivered by the U.S. Geological Survey Earth Resources Observation and Science Cal/Val Center of Excellence in 2021. These reports present and detail the methodology and procedures for characterization; present technical and operational information about the specific sensing system being evaluated; and provide a summary of test measurements, data retention practices, data analysis results, and conclusions.

Resourcesat-2 is a medium-resolution satellite launched in 2011 on the Polar Satellite Launch Vehicle-C16 launch vehicle. Resourcesat-2 carries the same sensing elements as Resourcesat-1 (launched in October 2003) and provides continuity for the mission. The objectives of the Resourcesat mission are to provide remote sensing data services to global users, focusing on data for integrated land and water resources management.

Resourcesat-2A is identical to Resourcesat-2 and was launched in 2016 on the Polar Satellite Launch Vehicle-C36 launch vehicle for continuity of data and improved temporal resolution. The two satellites operating in tandem improved the revisit capability from 5 days to 2–3 days. The Resourcesat-2 platform is of Indian Remote Sensing Satellites-1C/1D–P3 heritage and was built by the Indian Space Research Organisation. Resourcesat-2 and Resourcesat-2A carry the Advanced Wide Field Sensor and LISS–3, as well as the Linear Imaging Self Scanning-4 for medium-resolution imaging. More information on Indian Space Research Organisation satellites and sensors is available in the “2020 Joint Agency Commercial Imagery Evaluation—Remote Sensing Satellite Compendium” and from the manufacturer at https://www.isro.gov.in/.

The Earth Resources Observation and Science Cal/Val Center of Excellence system characterization team completed data analyses to characterize the geometric (interior and exterior), radiometric, and spatial performances. Results of these analyses indicate that LISS–3 has an interior geometric performance in the range of −4.620 (−0.154 pixel) to 13.230 meters (m; 0.441 pixel) in easting and −12.360 (−0.412 pixel) to 1.500 m (0.050 pixel) in northing in band-to-band registration, an exterior geometric error of −27.805 (−0.927 pixel) to 26.578 m (0.886 pixel) in easting and −35.341 (−1.178 pixel) to −6.286 m (−0.210 pixel) in northing offset in comparison to the Landsat 8 Operational Land Imager, a radiometric performance in the range of −0.096 to 0.036 in offset and 0.585–0.946 in slope, and a spatial performance in the range of 1.87–1.95 pixels for full width at half maximum, with a modulation transfer function at a Nyquist frequency in the range of 0.045–0.070.

Introduction

The Linear Imaging Self Scanning-3 (LISS–3) sensor onboard the Indian Space Research Organisation Resourcesat-2 satellite is a high-resolution land observation instrument consisting of four bands: green, red, near infrared, and shortwave infrared. Resourcesat-2 was launched in 2011, and an identical mission, Resourcesat-2A, was launched in 2016. The primary objectives for data acquired by LISS–3 include monitoring biomass, vegetation, land cover, leaf area index, and normalized difference vegetation index.

The data analysis results provided within this report have been derived from approved Joint Agency Commercial Imagery Evaluation (JACIE) processes and procedures. JACIE was formed to leverage resources from several Federal agencies for the characterization of remote sensing data and to share those results across the remote sensing community. More information about JACIE is available at https://www.usgs.gov/core-science-systems/eros/calval/jacie?qt-science_support_page_related_con=3#qt-science_support_page_related_con.

Purpose and Scope

The purpose of this report is to describe the specific sensor or sensing system, test its performance in three categories, complete related data analyses to quantify these performances, and report the results in a standardized document. In this chapter, the LISS–3 sensor is described. The performance of the system is limited to geometric, radiometric, and spatial analyses. The scope of the geometric assessment is limited to testing the interior alignments of spectral bands against each other and testing the exterior alignment in reference to the Landsat 8 Operational Land Imager (OLI).

The U.S. Geological Survey (USGS) Earth Resources Observation and Science (EROS) Cal/Val Center of Excellence (ECCOE) project, and the associated system characterization process used for this assessment, follows the USGS Fundamental Science Practices, which include maintaining data, information, and documentation needed to reproduce and validate the scientific analysis documented in this report. Additional information and guidance about Fundamental Science Practices and related resource information of interest to the public are available at https://www.usgs.gov/about/organization/science-support/office-science-quality-and-integrity/fundamental-science-practices. For additional information related to the report, please contact ECCOE at eccoe@usgs.gov.

System Description

This section describes the satellite and operational details for Resourcesat-2 and provides information about the LISS–3 sensor.

Satellite and Operational Details

The satellite and operational details of Resourcesat-2 are listed in table 1.

Table 1.    

Satellite and operational details for Resourcesat-2 Linear Imaging Self Scanning-3.

[kg, kilogram; NIR, near infrared; SWIR, shortwave infrared; W, watt; AH, amp hour; Ni-Cd, nickel-cadmium; Mbps, megabit per second; ~, about; km, kilometer; °, degree; min, minute; ±, plus or minus; lat., latitude; N/A, not applicable; m, meter; USGS, U.S. Geological Survey]

Product information Resourcesat-2 Linear Imaging Self Scanning-3 data
Product name Level 1T
Satellite name Resourcesat-2
Sensor name(s) Linear Imaging Self Scanning-3
Lift-off mass 1,206 kg
Instrument mass 106 kg
Sensor type Multispectral, visible, and infrared (green, red, NIR, SWIR)
Scanning technique Pushbroom; 6,000 detectors array
Power Solar array generating 1,250 W at end of life; two 24 AH Ni-Cd batteries
Data rate 52.5 Mbps
Mission type Global land-monitoring mission
Launch date April 20, 2011
Number of satellites 2
Expected lifetime ~5 years
Operator Indian Space Research Organisation
Operating orbit Circular polar Sun synchronous
Orbital altitude range 817 km
Sensor angle altitude 98.7° inclination
Altitude and orbit control Three-axis body stabilized using reaction wheels, magnetic torquers, and hydrazine thrusters
Orbit period 101.35 min
Imaging time 10:30 descending node
Geographic coverage Land imaging ± 81.3° lat.
Temporal resolution 24 days
Temporal coverage 2011 to present
Imaging angles N/A
Ground sample distance(s) 23.5 m
Data licensing Free through USGS for the United States only
Data pricing Free through USGS for the United States only
Product abstract https://www.isro.gov.in/RESOURCESAT_2.html
Product locator https://earthexplorer.usgs.gov/
Table 1.    Satellite and operational details for Resourcesat-2 Linear Imaging Self Scanning-3.

Sensor Information

The spectral characteristics and the relative spectral response are listed in table 2 and figure 1, respectively.

Table 2.    

Imaging sensor details for Resourcesat-2 Linear Imaging Self Scanning-3.

[The Resourcesat-2 Linear Imaging Self Scanning-3 (LISS–3) sensor has a swath width of 140 kilometers; μm, micrometer; m, meter; NIR, near infrared; SWIR, shortwave infrared]

Spectral band(s) details Resourcesat-2 LISS–3
Lower band (µm) Upper band (µm) Radiometric resolution (bits) Ground sample distance (m)
Band 2—green 0.52 0.59 10 23.5
Band 3—red 0.62 0.68 10 23.5
Band 4—NIR 0.77 0.86 10 23.5
Band 5—SWIR 1.55 1.70 10 23.5
Table 2.    Imaging sensor details for Resourcesat-2 Linear Imaging Self Scanning-3.
Spectral responses range from 0 to about 100 and wavelengths range from about 500
                        to 1,730 nanometers.
Figure 1.

Resourcesat-2 Linear Imaging Self Scanning-3 relative spectral response.

Procedures

ECCOE has established standard processes to identify Earth observing systems of interest and to assess the geometric, radiometric, and spatial qualities of data products from these systems.

The assessment steps are as follows:

  • system identification and investigation to learn the general specifications of the satellite and its sensor(s);

  • data receipt and initial inspection to understand the characteristics and any overt flaws in the data product so that it may be further analyzed;

  • geometry characterization, including interior geometric orientation measuring the relative alignment of spectral bands and exterior geometric orientation measuring how well the georeferenced pixels within the image are aligned to a known reference;

  • radiometry characterization, including assessing how well the data product correlates with a known reference and, when possible, assessing the signal-to-noise ratio; and

  • spatial characterization, assessing the two-dimensional fidelity of the image pixels to their projected ground sample distance (GSD).

Data analysis and test results are maintained at the USGS EROS Center by the ECCOE project.

Measurements

The observed USGS measurements are listed in table 3. The mean of interior (band-to-band) and exterior (image-to-image) mean errors, standard deviation (STDDEV), and root mean square errors (RMSEs) are listed in meters (pixels). Details about the methodologies used are outlined in the “Analysis” section.

Table 3.    

U.S. Geological Survey measurement results.

[USGS, U.S. Geological Survey; m, meter; RMSE, root mean square error; NIR, near infrared; SWIR, shortwave infrared; LISS–3, Resourcesat-2 Linear Imaging Self Scanning-3; L8 OLI, Landsat 8 Operational Land Imager; FWHM, full width at half maximum; MTF, modulation transfer function]

Description of product Top of Atmosphere reflectance
Interior (band to band) Band 2 (green)
Mean: −4.620 to 13.230 m (−0.154 to 0.441), −12.360 to 0.510 m (−0.412 to 0.017)
RMSE: 1.170 to 13.410 m (0.039 to 0.447), 1.530 to 12.450 m (0.051 to 0.415)
Band 3 (red)
Mean: −4.620 to 11.970 m (−0.154 to 0.399), −8.940 to 0.930 m (−0.298 to 0.031)
RMSE: 1.170 to 12.390 m (0.039 to 0.413), 1.860 to 9.120 m (0.062 to 0.304)
Band 4 (NIR)
Mean: −4.080 to 13.230 m (−0.136 to 0.441), −9.660 to 1.500 m (−0.322 to 0.050)
RMSE: 1.290 to 13.410 m (0.043 to 0.447), 1.530 to 9.810 m (0.051 to 0.327)
Band 5 (SWIR)
Mean: −4.620 to 11.970 m (−0.154 to 0.399), −12.360 to 1.500 m (−0.412 to 0.050)
RMSE: 3.810 to 12.150 m (0.127 to 0.405), 3.990 to 12.450 m (0.133 to 0.415)
Exterior (geometric location accuracy) Mean: −27.805 to 26.578 m (−0.927 to 0.886), −35.341 to −6.286 m (−1.178 to −0.210)
RMSE: 0.348 to 0.939 m (10.434 to 28.177), 0.218 to 1.239 m (6.546 to 37.158)
Radiometric evaluation (linear regression—LISS–3 versus L8 OLI reflectance) Band 2—Green (offset, slope): (0.022 to 0.029, 0.610 to 0.696)
Band 3—Red (offset, slope): (0.015 to 0.025, 0.656 to 0.696)
Band 4—NIR (offset, slope): (0.021 to 0.029, 0.590 to 0.658)
Band 5—SWIR (offset, slope): (−0.096 to 0.036, 0.585 to 0.946)
Spatial performance measurement Band 2—Green: FWHM = 1.96 pixels; MTF at Nyquist = 0.070
Band 3—Red: FWHM = 1.88 pixels; MTF at Nyquist = 0.045
Band 4—NIR: FWHM = 1.87 pixels; MTF at Nyquist = 0.050
Band 5—SWIR: FWHM = 1.95 pixels; MTF at Nyquist = 0.045
Table 3.    U.S. Geological Survey measurement results.

Analysis

This section describes the geometric, radiometric, and spatial performance of LISS–3.

Geometric Performance

This geometric performance for LISS–3 is characterized in terms of the interior (band-to-band alignment) and exterior (geometric location accuracy) geometric analysis results.

Interior (Band to Band)

The band-to-band alignment analysis was completed using the EROS System Characterization (EROSSC) software on three separate images over the United States. Band combinations were registered against each other to determine the mean error, STDDEV, and RMSE, as listed in table 4 with results represented in pixels at a 30-meter (m) GSD (the LISS–3 image was resampled to 30 m). Geometric error maps for each assessed band combination over the New Mexico image, as well as the corresponding histogram graphs, are shown in figures 25. The geometric error maps indicate the directional shift and relative magnitude of the shift, and the histogram and error distribution indicate frequency of observed mean error measurements within the image. Together, the interior and exterior geometric analysis results, as reported in the “Interior (Band to Band)” and “Exterior (Geometric Location Accuracy)” sections, provide a comprehensive assessment of geometric accuracy.

Table 4.    

Band-to-band registration error (in pixels).

[ID, identifier; STDDEV, standard deviation; RMSE, root mean square error]

Scene ID (location) Band combination Mean error (easting) Mean error (northing) STDDEV (easting) STDDEV (northing) RMSE (easting) RMSE (northing)
R2LS310212018267036_L1T (Fargo, North Dakota) Band 2–band 3 0.003 0.001 0.039 0.062 0.039 0.062
Band 2–band 4 −0.000 −0.001 0.043 0.051 0.043 0.051
Band 2–band 5 −0.139 −0.293 0.053 0.078 0.149 0.303
Band 3–band 4 −0.004 −0.009 0.057 0.065 0.057 0.065
Band 3–band 5 −0.0153 −0.298 0.078 0.060 0.172 0.304
Band 4–band 5 −0.136 −0.322 0.039 0.056 0.141 0.327
R2LS305022018295036_L1T (Maine) Band 2–band 3 0.017 −0.015 0.049 0.084 0.052 0.085
Band 2–band 4 −0.049 0.017 0.118 0.146 0.128 0.146
Band 2–band 5 −0.154 −0.051 0.130 0.123 0.201 0.133
Band 3–band 4 −0.065 0.031 0.118 0.175 0.134 0.177
Band 3–band 5 −0.154 −0.098 0.142 0.117 0.209 0.152
Band 4–band 5 0.000 0.050 0.173 0.186 0.173 0.192
R2LS305152019264046_L1T (New Mexico) Band 2–band 3 −0.021 −0.194 0.053 0.068 0.057 0.205
Band 2–band 4 0.441 −0.241 0.071 0.104 0.447 0.262
Band 2–band 5 0.367 −0.412 0.054 0.055 0.371 0.415
Band 3–band 4 0.395 0.003 0.123 0.073 0.413 0.071
Band 3–band 5 0.399 −0.212 0.073 0.083 0.405 0.228
Band 4–band 5 −0.122 −0.285 0.037 0.057 0.127 0.291
Table 4.    Band-to-band registration error (in pixels).
The easting and northing errors are distributed evenly throughout the map grid.
Figure 2.

Band 2 (green) to band 3 (red) geometric error map for New Mexico.

The frequency of observed error is highest at about −0.1 pixel (easting) and −0.2
                           pixel (northing).
Figure 3.

Band 2 (green) to band 3 (red) geometric error histogram (upper) and error distribution (lower) for New Mexico.

The easting and northing errors are shown throughout the map grid but are most dense
                           in the central and western parts.
Figure 4.

Band 3 (red) to band 5 (shortwave infrared) geometric error map for New Mexico.

The frequency of observed error is highest at about 0.5 pixel (easting) and −0.3 pixel
                           (northing).
Figure 5.

Band 3 (red) to band 5 (shortwave infrared) geometric error histogram (upper) and error distribution (lower) for New Mexico.

Exterior (Geometric Location Accuracy)

For this analysis, band 2 (green) of the LISS–3 data was compared against the corresponding band from three Landsat 8 OLI images over sites in the United States using the EROSSC software. Conjugate points in the reference and search images were identified automatically and refined using similarity measures such as normalized cross-correlation metrics, and the mean error, STDDEV, and RMSE results are listed in table 5 with results represented in pixels (and meters) at a 30-m GSD (LISS–3 was resampled to 30 m). For each of the three images, geometric error maps showing the directional shift and relative magnitude of the shift, when compared with the Landsat 8 OLI, along with the corresponding histogram and error distribution, are provided in figures 611. The Landsat 8 OLI imagery had a control uncertainty of about 8 m.

Table 5.    

Geometric error of Resourcesat-2 Linear Imaging Self Scanning-3 relative to Landsat 8 Operational Land Imager.

[ID, identifier; STDDEV, standard deviation; RMSE, root mean square error; m, meter]

Scene ID (location) Mean error (easting) Mean error (northing) STDDEV (easting) STDDEV (northing) RMSE (easting) RMSE (northing)
R2LS310212018267036_L1TLC08_L1TP_030027_20181021_20200830_02_T1
(Fargo, North Dakota)
−0.311 pixel
(−9.342 m)
−0.209 pixel
(−6.286 m)
0.156 pixel
(4.667 m)
0.061 pixel
(1.833 m)
0.348 pixel
(10.434 m)
0.218 pixel
(6.546 m)
R2LS305022018295036_L1TLC08_L1TP_010028_20180502_20200901_02_T1
(Maine)
0.885 pixel
(26.578 m)
−1.178 pixels
(−35.341 m)
0.254 pixel
(7.615 m)
0.383 pixel
(11.489 m)
0.921 pixel
(27.646 m)
1.238 pixels
(37.158 m)
R2LS305152019264046_L1TLC08_L1TP_032036_20190515_20200828_02_T1
(New Mexico)
−0.926 pixel
(−27.805 m)
−0.567 pixel
(−17.014 m)
0.152 pixel
(4.569 m)
0.288 pixel
(8.652 m)
0.939 pixel
(28.177 m)
0.636 pixel
(19.082 m)
Table 5.    Geometric error of Resourcesat-2 Linear Imaging Self Scanning-3 relative to Landsat 8 Operational Land Imager.
The easting and northing errors are distributed evenly throughout the map grid.
Figure 6.

Relative geometric error for Landsat 8 Operational Land Imager and Resourcesat-2 Linear Imaging Self Scanning-3 for Fargo, North Dakota.

The frequency of observed error is highest at about −11 pixels (easting) and −7 pixels
                           (northing).
Figure 7.

Relative geometric error histogram (upper) and error distribution (lower) for Fargo, North Dakota.

The easting and northing errors are shown throughout the map grid but not in the western,
                           northern, and northeastern edges.
Figure 8.

Relative geometric error for Landsat 8 Operational Land Imager and Resourcesat-2 Linear Imaging Self Scanning-3 for Maine.

The frequency of observed error is highest at about 30 meters (easting) and −40 meters
                           (northing).
Figure 9.

Relative geometric error histogram (upper) and error distribution (lower) for Maine.

The easting and northing errors are distributed evenly throughout the map grid with
                           blank cells in the west and north.
Figure 10.

Relative geometric error for Landsat 8 Operational Land Imager and Resourcesat-2 Linear Imaging Self Scanning-3 for New Mexico.

The frequency of observed error is highest at about −30 meters (easting) and −15 meters
                           (northing).
Figure 11.

Relative geometric error histogram (upper) and error distribution (lower) for New Mexico.

Radiometric Performance

For this analysis, cloud-free regions of interest were selected within three near-coincident LISS–3 and Landsat 8 OLI scene pairs using the EROSSC software. Once the relative georeferencing error between Landsat 8 OLI and Resourcesat-2 LISS–3 has been corrected, Top of Atmosphere reflectance values from the two sensors are extracted. The scatterplot (fig. 12) is drawn in a way that the x-axis is the reference sensor and the y-axis is the comparison sensor. The linear regression, thus, represents Top of Atmosphere reflectance relative to that of the reference sensor. Ideally, the slope should be near unity and the offset should be near zero. For instance, if the slope is greater than unity, that means the comparison sensor has a tendency to overestimate Top of Atmosphere reflectance compared to the reference sensor.

Reflectance mostly follows the 1:1 line for the green, red, and shortwave infrared
                        bands but deviates for near infrared.
Figure 12.

Top of Atmosphere reflectance comparison for Landsat 8 Operational Land Imager (OLI) and Resourcesat-2 Linear Imaging Self Scanning-3 (LISS–3; Maine).

Top of Atmosphere reflectance comparison results are listed in table 6. A band-by-band graphical comparison between the LISS–3 image over Maine, when compared with the corresponding Landsat 8 OLI band, is shown in figure 12.

Table 6.    

Top of Atmosphere reflectance comparison of Resourcesat-2 Linear Imaging Self Scanning-3 against Landsat 8 Operational Land Imager.

[ID, identifier; NIR, near infrared; SWIR, shortwave infrared; %, percent; R2, coefficient of determination]

Scene ID (location) Statistics Band 2—Green Band 3—Red Band 4—NIR Band 5—SWIR
R2LS310212018267036_L1TLC08_L1TP_030027_20181021_20200830_02_T1
(Fargo, North Dakota)
Uncertainty (%) 8.750 11.220 15.020 13.410
R2 0.926 0.939 0.937 0.631
Radical offset −0.027 0.017 0.027 −0.072
Radical slope 0.610 0.655 0.589 0.904
R2LS305022018295036_L1TLC08_L1TP_010028_20180502_20200901_02_T1
(Maine)
Uncertainty (%) 13.340 17.470 12.700 24.170
R2 0.793 0.852 0.836 0.877
Radical offset 0.022 0.015 0.021 0.036
Radical slope 0.695 0.575 0.635 0.584
R2LS305152019264046_L1TLC08_L1TP_032036_20190515_20200828_02_T1
(New Mexico)
Uncertainty (%) 4.49 6.48 5.33 5.46
R2 0.904 0.908 0.894 0.665
Radical offset 0.029 0.025 0.030 −0.096
Radical slope 0.648 0.687 0.658 0.946
Table 6.    Top of Atmosphere reflectance comparison of Resourcesat-2 Linear Imaging Self Scanning-3 against Landsat 8 Operational Land Imager.

Spatial Performance

For this analysis, spatial analysis based on Helder and others (2004), was used to determine the full width at half maximum and modulation transfer function at Nyquist frequency, as listed in table 7.

Table 7.    

Spatial performance of Resourcesat-2 Linear Imaging Self Scanning-3.

[RER, relative edge response; FWHM, full width at half maximum; MTF, modulation transfer function; NIR, near infrared; SWIR, shortwave infrared]

Spatial analysis RER FWHM (pixels) MTF at Nyquist
Band 2—green 0.452 1.96 0.070
Band 3—red 0.460 1.88 0.045
Band 4—NIR 0.455 1.87 0.050
Band 5—SWIR 0.444 1.95 0.045
Table 7.    Spatial performance of Resourcesat-2 Linear Imaging Self Scanning-3.

Summary and Conclusions

This report summarizes the sensor performance of the Resourcesat-2 Linear Imaging Self Scanning-3 (LISS–3) sensor based on the U.S. Geological Survey Earth Resources Observation and Science Cal/Val Center of Excellence (ECCOE) system characterization process. In summary, we have determined that this sensor provides an interior geometric performance in the range of −4.620 (−0.154 pixel) to 13.230 m (0.441 pixel) in easting and −12.360 (−0.412 pixel) to 1.500 m (0.050 pixel) in northing in band-to-band registration, an exterior geometric error of −27.805 (−0.927 pixel) to 26.578 m (0.886 pixel) in easting and −35.341 (−1.178 pixel) to −6.286 m (−0.210 pixel) in northing offset in comparison to the Landsat 8 Operational Land Imager, a radiometric performance in the range of −0.096 to 0.035 in offset and 0.585–0.946 in slope, and a spatial performance in the range of 1.87–1.95 pixels for full width at half maximum, with a modulation transfer function at a Nyquist frequency in the range of 0.045–0.070.

In conclusion, the team has completed an ECCOE standardized system characterization of the Resourcesat-2 LISS–3 sensing system. Although the team followed characterization procedures that are standardized across the many sensors and sensing systems under evaluation, these procedures are customized to fit the individual sensor as was done with LISS–3. The team has acquired the data, defined proper testing methodologies, carried out comparative tests against specific references, recorded measurements, completed data analyses, and quantified sensor performance accordingly. The team also endeavored to retain all data, measurements, and methods. This is key to ensure that all data and measurements are archived and accessible and that the performance results are reproducible.

The ECCOE project and associated Joint Agency Commercial Imagery Evaluation partners are always interested in reviewing sensor and remote sensing application assessments and would like to see and discuss information on similar data and product assessments and reviews. If you would like to discuss system characterization with the U.S. Geological Survey ECCOE and (or) the Joint Agency Commercial Imagery Evaluation team, please email us at eccoe@usgs.gov.

Selected References

Helder, D., Choi, T., and Rangaswamy, M., 2004, In-flight characterization of spatial quality using point spread functions, in Morain, S.A., and Budge, A.M., eds., Post-launch calibration of satellite sensors: CRC Press, p. 151‒170.

Indian Space Research Organisation, 2021, Resourcesat-2: Indian Space Research Organisation web page, accessed June 2021 at https://www.isro.gov.in/Spacecraft/resourcesat-2.

Ramaseri Chandra, S.N., Christopherson, J.B., and Casey, K.A., 2020, 2020 Joint Agency Commercial Imagery Evaluation—Remote sensing satellite compendium: U.S. Geological Survey Circular 1468 (ver. 1.1, October 2020), 253 p. [Also available at https://doi.org/10.3133/cir1468.] [Supersedes USGS Circular 1455.]

U.S. Geological Survey, 2020a, EROS CalVal Center of Excellence (ECCOE): U.S. Geological Survey web page, accessed June 2021 https://www.usgs.gov/core-science-systems/eros/calval.

U.S. Geological Survey, 2020b, EROS CalVal Center of Excellence (ECCOE)—JACIE: U.S. Geological Survey web page, accessed June 2021 at https://www.usgs.gov/core-science-systems/eros/calval/jacie?qt-science_support_page_related_con=3#qt-science_support_page_related_con.

U.S. Geological Survey, 2020c, Landsat missions—Glossary and acronyms: U.S. Geological Survey web page, accessed June 2021 at https://www.usgs.gov/core-science-systems/nli/landsat/glossary-and-acronyms.

Conversion Factors

International System of Units to U.S. customary units

Multiply By To obtain
meter (m) 3.281 foot (ft)
meter (m) 1.094 yard (yd)

Abbreviations

ECCOE

EROS Cal/Val Center of Excellence

EROS

Earth Resources Observation and Science

EROSSC

EROS System Characterization

GSD

ground sample distance

JACIE

Joint Agency Commercial Imagery Evaluation

LISS–3

Linear Imaging Self Scanning-3

OLI

Operational Land Imager

RMSE

root mean square error

STDDEV

standard deviation

USGS

U.S. Geological Survey

For more information about this publication, contact:

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47914 252nd Street

Sioux Falls, SD 57198

605–594–6151

For additional information, visit: https://www.usgs.gov/centers/eros

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Any use of trade, firm, or product names is for descriptive purposes only and does not imply endorsement by the U.S. Government.

Although this information product, for the most part, is in the public domain, it also may contain copyrighted materials as noted in the text. Permission to reproduce copyrighted items must be secured from the copyright owner.

Suggested Citation

Ramaseri Chandra, S.N., Christopherson, J., Anderson, C., Stensaas, G.L., and Kim, M., 2021, System characterization report on Resourcesat-2 Linear Imaging Self Scanning-3 (LISS–3) sensor (ver. 1.2, December 2024), chap. H of Ramaseri Chandra, S.N., comp., System characterization of Earth observation sensors: U.S. Geological Survey Open-File Report 2021–1030, 20 p., https://doi.org/10.3133/ofr20211030H.

ISSN: 2331-1258 (online)

Publication type Report
Publication Subtype USGS Numbered Series
Title System characterization report on Resourcesat-2 Linear Imaging Self Scanning-3 (LISS–3) sensor
Series title Open-File Report
Series number 2021-1030
Chapter H
DOI 10.3133/ofr20211030H
Edition Version 1.0: October 21, 2021; Version 1.1: August 29, 2024; Version 1.2: December 2, 2024
Year Published 2021
Language English
Publisher U.S. Geological Survey
Publisher location Reston, VA
Contributing office(s) Earth Resources Observation and Science (EROS) Center
Description iv, 20 p.
Online Only (Y/N) Y
Additional Online Files (Y/N) Y
Google Analytic Metrics Metrics page
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