Figure 1.
VIIRS horizontal sampling interval (HSI) for a VIIRS moderate band as a function of scan angle. The light blue and green lines show the unaggregated pixel growth along-scan for the scan and track directions, respectively. The dark blue line shows the pixel growth for the scan direction with the three aggregation zones.
Figure 1.
VIIRS horizontal sampling interval (HSI) for a VIIRS moderate band as a function of scan angle. The light blue and green lines show the unaggregated pixel growth along-scan for the scan and track directions, respectively. The dark blue line shows the pixel growth for the scan direction with the three aggregation zones.
Figure 2.
VIIRS scan section diagram illustrating the different collection regions and their angles during a single scan.
Figure 2.
VIIRS scan section diagram illustrating the different collection regions and their angles during a single scan.
Figure 3.
Diagram of the VIIRS solar diffuser calibration. This includes the VIIRS scanner that looks at the Earth and solar diffuser (SD) when illuminated by the Sun through an attenuation screen and the solar diffuser stability monitor (SDSM) that views the Sun through a screen and the SD while it is illuminated.
Figure 3.
Diagram of the VIIRS solar diffuser calibration. This includes the VIIRS scanner that looks at the Earth and solar diffuser (SD) when illuminated by the Sun through an attenuation screen and the solar diffuser stability monitor (SDSM) that views the Sun through a screen and the SD while it is illuminated.
Figure 4.
A cartoon of the VIIRS TVAC test chamber setup. The SV, TMCBB, and SIS100 sources are shown with respect to the instrument location within the chamber.
Figure 4.
A cartoon of the VIIRS TVAC test chamber setup. The SV, TMCBB, and SIS100 sources are shown with respect to the instrument location within the chamber.
Figure 5.
A comparison of the on-orbit solar spectral irradiance profile and the SIS100 radiance profile. The OOB RSR contributions are not weighted the same in on-orbit and prelaunch applications.
Figure 5.
A comparison of the on-orbit solar spectral irradiance profile and the SIS100 radiance profile. The OOB RSR contributions are not weighted the same in on-orbit and prelaunch applications.
Figure 6.
Band M4 dynamic range measurements for all detectors, legend in the upper right, for HAM side B. The points to the left of the first vertical line are high gain measurements. The band switches to low gain after a radiance of 40. The first and second vertical red lines are for high and low gain Lmax, respectively. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement.
Figure 6.
Band M4 dynamic range measurements for all detectors, legend in the upper right, for HAM side B. The points to the left of the first vertical line are high gain measurements. The band switches to low gain after a radiance of 40. The first and second vertical red lines are for high and low gain Lmax, respectively. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement.
Figure 7.
Band M8 dynamic range measurements for all detectors, legend in the upper right, for HAM side A. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement. The vertical red line corresponds to Lmax, and the saturation occurs before the line. The rollover in the response is due to saturation of the focal plane electronics. This causes two unique radiance levels to produce the same VIIRS digital number.
Figure 7.
Band M8 dynamic range measurements for all detectors, legend in the upper right, for HAM side A. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement. The vertical red line corresponds to Lmax, and the saturation occurs before the line. The rollover in the response is due to saturation of the focal plane electronics. This causes two unique radiance levels to produce the same VIIRS digital number.
Figure 8.
Band I3 dynamic range measurements for all detectors, legend on the right, for HAM side B. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement. The vertical red line corresponds to Lmax, and the saturation occurs before the line. The rollover in the response is due to saturation of the focal plane electronics. This causes two unique radiance levels to produce the same VIIRS digital number. The blue crosses are from detector 4 that is an out of family with degraded performance that has continued on orbit.
Figure 8.
Band I3 dynamic range measurements for all detectors, legend on the right, for HAM side B. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement. The vertical red line corresponds to Lmax, and the saturation occurs before the line. The rollover in the response is due to saturation of the focal plane electronics. This causes two unique radiance levels to produce the same VIIRS digital number. The blue crosses are from detector 4 that is an out of family with degraded performance that has continued on orbit.
Figure 9.
Band M6 dynamic range measurements for all detectors, legend in the upper right, for HAM side B. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement. The vertical red line corresponds to Lmax, and the saturation occurs before the line. The rollover in the response is due to saturation of the focal plane electronics. This causes two unique radiance levels to produce the same VIIRS digital number.
Figure 9.
Band M6 dynamic range measurements for all detectors, legend in the upper right, for HAM side B. The y-axis is offset subtracted VIIRS response, and the x-axis is the SIS100 radiance during the measurement. The vertical red line corresponds to Lmax, and the saturation occurs before the line. The rollover in the response is due to saturation of the focal plane electronics. This causes two unique radiance levels to produce the same VIIRS digital number.
Figure 10.
Band M7 digital numbers (DNs) as a function of scan during prelaunch testing (upper image). The pattern shows the detector’s response to the SIS100 profile as it scans across it in auto gain mode. The wings on the left and right are high gain DNs (blue line), where the detector is partially viewing the SIS100 aperture. When the DNs reach the gain switch point value, the detector switches to low gain and the DNs drop in the middle of the image (orange line). The M7 radiance is shown in the middle image and is the upper image DNs’ converted radiance using the prelaunch calibration coefficients. The lower image is a zoom-in of the gain transition point to show that it is continuous in radiance.
Figure 10.
Band M7 digital numbers (DNs) as a function of scan during prelaunch testing (upper image). The pattern shows the detector’s response to the SIS100 profile as it scans across it in auto gain mode. The wings on the left and right are high gain DNs (blue line), where the detector is partially viewing the SIS100 aperture. When the DNs reach the gain switch point value, the detector switches to low gain and the DNs drop in the middle of the image (orange line). The M7 radiance is shown in the middle image and is the upper image DNs’ converted radiance using the prelaunch calibration coefficients. The lower image is a zoom-in of the gain transition point to show that it is continuous in radiance.
Figure 11.
The signal-to-noise ratio (SNR) of band I3 for all detectors (colored symbols) as a function of SIS100 radiance (W/m2/µm/sr). The three vertical red lines are for Lmin (left), Ltyp (middle), and Lmax (right). The decrease in SNR at the Lmax line is due to partial saturation of the signal. This behavior is used help identify valid response data for characterization purposes.
Figure 11.
The signal-to-noise ratio (SNR) of band I3 for all detectors (colored symbols) as a function of SIS100 radiance (W/m2/µm/sr). The three vertical red lines are for Lmin (left), Ltyp (middle), and Lmax (right). The decrease in SNR at the Lmax line is due to partial saturation of the signal. This behavior is used help identify valid response data for characterization purposes.
Figure 12.
The signal-to-noise ratio (SNR) of band M10 for all detectors (colored symbols) as a function of SIS100 radiance (W/m2/µm/sr). The three vertical red lines are for Lmin (left), Ltyp (middle), and Lmax (right).
Figure 12.
The signal-to-noise ratio (SNR) of band M10 for all detectors (colored symbols) as a function of SIS100 radiance (W/m2/µm/sr). The three vertical red lines are for Lmin (left), Ltyp (middle), and Lmax (right).
Figure 13.
Band M1 high gain fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols). The columns are tau, , and . The rows are HAM A and B. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 13.
Band M1 high gain fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols). The columns are tau, , and . The rows are HAM A and B. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 14.
Band M1 low gain fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols). The columns are tau, , and . The rows are HAM A and B. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 14.
Band M1 low gain fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols). The columns are tau, , and . The rows are HAM A and B. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 15.
Band M1 high gain fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols) for HAM A. The columns are tau, , and . The rows are not fixed parameters, fixed at zero, fixed at zero, and the tau set to the detector average of each plateau. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 15.
Band M1 high gain fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols) for HAM A. The columns are tau, , and . The rows are not fixed parameters, fixed at zero, fixed at zero, and the tau set to the detector average of each plateau. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 16.
Band M7 low gain fit residuals as a function of SIS100 radiance within the Lmin and Lmax regions for all detectors (colors and symbols).
Figure 16.
Band M7 low gain fit residuals as a function of SIS100 radiance within the Lmin and Lmax regions for all detectors (colors and symbols).
Figure 17.
Band M8 fit residuals as a function of SIS100 radiance within the Lmin and Lmax regions for all detectors (colors and symbols) using a second-order polynomial fit.
Figure 17.
Band M8 fit residuals as a function of SIS100 radiance within the Lmin and Lmax regions for all detectors (colors and symbols) using a second-order polynomial fit.
Figure 18.
Band M8 fit residuals as a function of SIS100 radiance within the Lmin and Lmax regions for all detectors (colors and symbols) using a third-order polynomial fit.
Figure 18.
Band M8 fit residuals as a function of SIS100 radiance within the Lmin and Lmax regions for all detectors (colors and symbols) using a third-order polynomial fit.
Figure 19.
Band M8 fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols) for HAM A. The columns are tau, , , and . The rows are not fixed parameters, fixed at zero, fixed at zero, and the tau set to the detector average of each plateau. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 19.
Band M8 fit coefficients for all detectors (x-axis) and TVAC/electronics configurations (colors and symbols) for HAM A. The columns are tau, , , and . The rows are not fixed parameters, fixed at zero, fixed at zero, and the tau set to the detector average of each plateau. Cold, nominal, and hot plateaus and electronics sides A and B are shown here.
Figure 20.
Band M1 temperature sensitivity (dL) as a function of electronics module (EM) temperature change between nominal and hot plateau for each detector (colors and symbols).
Figure 20.
Band M1 temperature sensitivity (dL) as a function of electronics module (EM) temperature change between nominal and hot plateau for each detector (colors and symbols).
Figure 21.
Band M1 temperature sensitivity (dL) as a function of focal plane assembly (FPA) temperature change between nominal and hot plateau for each detector (colors and symbols).
Figure 21.
Band M1 temperature sensitivity (dL) as a function of focal plane assembly (FPA) temperature change between nominal and hot plateau for each detector (colors and symbols).
Figure 22.
VIIRS top-level radiometric calibration uncertainty tree.
Figure 22.
VIIRS top-level radiometric calibration uncertainty tree.
Table 1.
VIIRS spectral, dynamic range, and noise requirements for the reflective solar bands.
Table 1.
VIIRS spectral, dynamic range, and noise requirements for the reflective solar bands.
Band | Spectral Range (µm) | Band Gain | Ltyp | Lmax | SNR |
---|
VNIR |
DNB | 0.500–0.900 | VG | 0.00003 | 200 | 6 |
M1 | 0.402–0.422 | High | 44.9 | 135 | 352 |
Low | 155 | 615 | 316 |
M2 | 0.436–0.454 | High | 40 | 127 | 380 |
Low | 146 | 687 | 409 |
M3 | 0.478–0.498 | High | 32 | 107 | 416 |
Low | 123 | 702 | 414 |
M4 | 0.545–0.565 | High | 21 | 78 | 362 |
Low | 90 | 667 | 315 |
I1 | 0.600–0.680 | Single | 22 | 718 | 119 |
M5 | 0.662–0.682 | High | 10 | 59 | 242 |
Low | 68 | 651 | 360 |
M6 | 0.739–0.754 | Single | 9.6 | 41 | 199 |
I2 | 0.846–0.885 | Single | 25 | 349 | 150 |
M7 | 0.846–0.885 | High | 6.4 | 29 | 215 |
Low | 33.4 | 349 | 340 |
SWIR |
M8 | 1.230–1.250 | Single | 5.4 | 165 | 74 |
M9 | 1.371–1.386 | Single | 6 | 77.1 | 83 |
I3 | 1.580–1.640 | Single | 7.3 | 72.5 | 6 |
M10 | 1.580–1.640 | Single | 7.3 | 71.2 | 342 |
M11 | 2.225–2.275 | Single | 0.12 | 31.8 | 10 |
Table 2.
Measured dynamic range performance for the reflective solar bands. Bands I3 and M8 fail the sensor specification, and band M9 shows just below the requirements but has impacts of water absorption in the analysis and most likely passes the requirements.
Table 2.
Measured dynamic range performance for the reflective solar bands. Bands I3 and M8 fail the sensor specification, and band M9 shows just below the requirements but has impacts of water absorption in the analysis and most likely passes the requirements.
| Single Gain | High Gain | Low Gain |
---|
| L_sat | L_max | L_sat/L_max | L_sat | L_max | L_sat/L_max | L_sat | L_max | L_sat/L_max |
---|
I1 | 772 | 718 | 1.08 | -- | -- | -- | -- | -- | -- |
I2 | 401 | 349 | 1.15 | -- | -- | -- | -- | -- | -- |
I3 | 65.2 | 72.5 | 0.90 | -- | -- | -- | -- | -- | -- |
M1 | -- | -- | -- | 164 | 135 | 1.21 | 710 | 615 | 1.15 |
M2 | -- | -- | -- | 173 | 127 | 1.36 | 797 | 687 | 1.16 |
M3 | -- | -- | -- | 144 | 107 | 1.35 | 851 | 702 | 1.21 |
M4 | -- | -- | -- | 113 | 78.0 | 1.44 | 863 | 667 | 1.29 |
M5 | -- | -- | -- | 76.5 | 59.0 | 1.30 | 733 | 651 | 1.13 |
M6 | 46.8 | 41.0 | 1.14 | -- | -- | -- | -- | -- | -- |
M7 | -- | -- | -- | 38.1 | 29.0 | 1.31 | 414 | 349 | 1.19 |
M8 | 115 | 165 | 0.69 | -- | -- | -- | -- | -- | -- |
M9 | 72.1 | 77.1 | 0.93 | -- | -- | -- | -- | -- | -- |
M10 | 77.0 | 71.2 | 1.08 | -- | -- | -- | -- | -- | -- |
M11 | 33.5 | 31.8 | 1.05 | -- | -- | -- | -- | -- | -- |
Table 3.
VNIR dual gain switch point performance for each HAM and electronics side. The minimum (Lmin) and maximum (Lmax) switch point radiance levels are listed along with the measured transition radiance (L at Transition). The red shows the bands that exceeded the requirements.
Table 3.
VNIR dual gain switch point performance for each HAM and electronics side. The minimum (Lmin) and maximum (Lmax) switch point radiance levels are listed along with the measured transition radiance (L at Transition). The red shows the bands that exceeded the requirements.
Band | E Side | HAM | Lmin Switch Point | Lmax Switch Point | L at Transition | Ratio of Switch with Requirement |
---|
Temperature Plateau | Temperature Plateau |
---|
Cold | Nominal | Hot | Cold | Nominal | Hot |
---|
M1 | A | A | 135 | 202.5 | 167.2 | 155.5 | 158.9 | 1.24 | 1.15 | 1.18 |
M1 | A | B | 135 | 202.5 | 169.3 | 158.0 | 161.3 | 1.25 | 1.17 | 1.19 |
M2 | A | A | 127 | 190.5 | 161.5 | 153.0 | 156.3 | 1.27 | 1.21 | 1.23 |
M2 | A | B | 127 | 190.5 | 162.6 | 154.0 | 157.4 | 1.28 | 1.21 | 1.24 |
M3 | A | A | 107 | 160.5 | 122.2 | 115.3 | 118.4 | 1.14 | 1.08 | 1.11 |
M3 | A | B | 107 | 160.5 | 122.5 | 115.5 | 118.6 | 1.14 | 1.08 | 1.11 |
M4 | A | A | 78 | 117 | 98.3 | 92.5 | 95.4 | 1.26 | 1.19 | 1.22 |
M4 | A | B | 78 | 117 | 98.2 | 92.4 | 95.3 | 1.26 | 1.18 | 1.22 |
M5 | A | A | 59 | 88.5 | 66.9 | 62.3 | 65.1 | 1.13 | 1.06 | 1.10 |
M5 | A | B | 59 | 88.5 | 66.6 | 62.0 | 64.8 | 1.13 | 1.05 | 1.10 |
M7 | A | A | 29 | 43.5 | 33.4 | 30.7 | 32.5 | 1.15 | 1.06 | 1.12 |
M7 | A | B | 29 | 43.5 | 33.5 | 30.8 | 32.6 | 1.16 | 1.06 | 1.12 |
M1 | B | A | 135 | 202.5 | 169.3 | 157.8 | 165.8 | 1.25 | 1.17 | 1.23 |
M1 | B | B | 135 | 202.5 | 170.0 | 160.2 | 168.6 | 1.26 | 1.19 | 1.25 |
M2 | B | A | 127 | 190.5 | 163.7 | 155.0 | 160.7 | 1.29 | 1.22 | 1.27 |
M2 | B | B | 127 | 190.5 | 164.6 | 156.1 | 161.7 | 1.30 | 1.23 | 1.27 |
M3 | B | A | 107 | 160.5 | 123.9 | 117.0 | 121.1 | 1.16 | 1.09 | 1.13 |
M3 | B | B | 107 | 160.5 | 124.1 | 117.1 | 121.3 | 1.16 | 1.09 | 1.13 |
M4 | B | A | 78 | 117 | 99.5 | 93.8 | 97.1 | 1.28 | 1.20 | 1.25 |
M4 | B | B | 78 | 117 | 99.2 | 93.6 | 97.1 | 1.27 | 1.20 | 1.25 |
M5 | B | A | 59 | 88.5 | 67.9 | 63.9 | 66.3 | 1.15 | 1.08 | 1.12 |
M5 | B | B | 59 | 88.5 | 67.5 | 63.7 | 66.0 | 1.14 | 1.08 | 1.12 |
M7 | B | A | 29 | 43.5 | 33.7 | 32.0 | 33.1 | 1.16 | 1.10 | 1.14 |
M7 | B | B | 29 | 43.5 | 33.6 | 32.0 | 33.1 | 1.16 | 1.10 | 1.14 |
Table 4.
Signal-to-noise ratio (SNR) results for the VIIRS reflective solar bands. The SNR, SNR requirement, and ratio of the two are shown here. All bands pass the SNR requirements with out-of-family band I3 detector 4 (shown at the bottom) passing as well.
Table 4.
Signal-to-noise ratio (SNR) results for the VIIRS reflective solar bands. The SNR, SNR requirement, and ratio of the two are shown here. All bands pass the SNR requirements with out-of-family band I3 detector 4 (shown at the bottom) passing as well.
| Single Gain | High Gain | Low Gain |
---|
| SNR | Spec | SNR/Spec | SNR | Spec | SNR/Spec | SNR | Spec | SNR/Spec |
---|
I1 | 307.1 | 119.0 | 2.6 | -- | -- | -- | -- | -- | -- |
I2 | 278.4 | 150.0 | 1.9 | -- | -- | -- | -- | -- | -- |
I3 | 186.8 | 6.0 | 31.1 | -- | -- | -- | -- | -- | -- |
M1 | -- | -- | -- | 628.9 | 352.0 | 1.8 | 878.1 | 155.0 | 5.7 |
M2 | -- | -- | -- | 567.6 | 380.0 | 1.5 | 1009.3 | 146.0 | 6.9 |
M3 | -- | -- | -- | 692.1 | 416.0 | 1.7 | 1155.7 | 123.0 | 9.4 |
M4 | -- | -- | -- | 542.4 | 362.0 | 1.5 | 961.9 | 90.0 | 10.7 |
M5 | -- | -- | -- | 376.5 | 242.0 | 1.6 | 928.3 | 68.0 | 13.7 |
M6 | 424.4 | 41.0 | 10.4 | -- | -- | -- | -- | -- | -- |
M7 | -- | -- | -- | 542.7 | 215.0 | 2.5 | 1148.2 | 33.4 | 34.4 |
M8 | 390.4 | 164.9 | 2.4 | -- | -- | -- | -- | -- | -- |
M9 | 302.8 | 77.1 | 3.9 | -- | -- | -- | -- | -- | -- |
M10 | 826.7 | 71.2 | 11.6 | -- | -- | -- | -- | -- | -- |
M11 | 69.7 | 31.8 | 2.2 | -- | -- | -- | -- | -- | -- |
| SNR | Spec | SNR/Spec | | | | | | |
I3 D4 | 8.9 | 6.0 | 1.5 | | | | | | |
Table 5.
VIIRS radiometric sensitivity to temperature change of the instrument. Columns 2 and 3 are for electronics module and optomechanical module temperature sensitivities for the TVAC transition from cold to nominal plateaus and columns 4 and 5 are the corresponding sensitivities for the nominal-to-hot plateau transition.
Table 5.
VIIRS radiometric sensitivity to temperature change of the instrument. Columns 2 and 3 are for electronics module and optomechanical module temperature sensitivities for the TVAC transition from cold to nominal plateaus and columns 4 and 5 are the corresponding sensitivities for the nominal-to-hot plateau transition.
| Cold-to-Nominal | Nominal-to-Hot |
---|
| dL/dT EM | dL/dT OMM | dL/dT EM | dL/dT OMM |
---|
I1 | 0.0161 | 0.0762 | 0.0065 | 0.0291 |
I2 | −0.0014 | −0.0207 | −0.0057 | −0.0531 |
I3 | 0.0018 | −0.0052 | −0.0005 | −0.0155 |
M1 | −0.0007 | −0.0120 | −0.0002 | −0.0145 |
M2 | 0.0000 | −0.0074 | 0.0010 | −0.0111 |
M3 | −0.0006 | −0.0114 | 0.0007 | −0.0158 |
M4 | 0.0012 | −0.0159 | −0.0002 | −0.0197 |
M5 | −0.0008 | −0.0128 | −0.0010 | −0.0138 |
M6 | 0.0006 | −0.0041 | 0.0002 | −0.0075 |
M7 | −0.0011 | −0.0177 | −0.0012 | −0.0186 |
M8 | 0.0014 | −0.0221 | 0.0002 | −0.0263 |
M9 | 0.0046 | 0.0071 | −0.0181 | 0.0031 |
M10 | 0.0013 | −0.0063 | −0.0018 | −0.0182 |
M11 | 0.0015 | 0.0010 | 0.0000 | −0.0024 |
Table 6.
A breakout of the reflective solar band calibration uncertainty tree for each component and a total rollup (highlighted in green for pass and red for fail). Band M11 fails due to high uncertainty in the SD BRF characterization.
Table 6.
A breakout of the reflective solar band calibration uncertainty tree for each component and a total rollup (highlighted in green for pass and red for fail). Band M11 fails due to high uncertainty in the SD BRF characterization.
Description | Error Type | M1 | M2 | M3 | M4 | M5 | M6 | M7 | M8 | M9 | M10 | M11 | I1 | I2 | I3 |
---|
Low | High | Low | High | Low | High | Low | High | Low | High | | Low | High | | | | | | | |
---|
Reflectance Accuracy (RSS of Bias & Random Totals) | | 1.90 | 1.88 | 1.78 | 1.74 | 1.88 | 1.68 | 1.41 | 1.37 | 1.38 | 1.41 | 1.50 | 1.43 | 1.42 | 1.76 | 1.48 | 1.37 | 2.25 | 1.36 | 1.35 | 1.37 |
Characterization Uncertainty at Ltyp | Random | 0.24 | 0.05 | 0.46 | 0.31 | 0.85 | 0.19 | 0.45 | 0.31 | 0.32 | 0.43 | 0.67 | 0.49 | 0.49 | 1.14 | 0.36 | 0.21 | 0.59 | 0.23 | 0.18 | 0.13 |
Response Stability | Random | 0.140 | 0.140 | 0.120 | 0.120 | 0.110 | 0.110 | 0.120 | 0.120 | 0.130 | 0.130 | 0.120 | 0.120 | 0.130 | 0.130 | 0.220 | 0.200 | 0.120 | 0.130 | 0.120 | 0.190 |
Offset Knowledge & Stability | Random | 0.040 | 0.010 | 0.040 | 0.010 | 0.030 | 0.012 | 0.040 | 0.014 | 0.040 | 0.040 | 0.090 | 0.040 | 0.010 | 0.040 | 0.030 | 0.020 | 0.070 | 0.070 | 0.045 | 0.060 |
Spec Unc Alloc | Random | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
RVS Unc Alloc | | 0.71 | 0.71 | 0.25 | 0.25 | 0.06 | 0.06 | 0.07 | 0.07 | 0.1 | 0.1 | 0.06 | 0.06 | 0.06 | 0.13 | 0.49 | 0.1 | 0.09 | 0.09 | 0.06 | 0.08 |
Pre-Launch Char Uncer | Random | 0.10 | 0.10 | 0.06 | 0.06 | 0.05 | 0.05 | 0.06 | 0.06 | 0.08 | 0.08 | 0.04 | 0.05 | 0.05 | 0.12 | 0.48 | 0.07 | 0.08 | 0.07 | 0.05 | 0.04 |
Polarization Error | Random | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
RVS Change over Life | Random | 0.70 | 0.70 | 0.24 | 0.24 | 0.04 | 0.04 | 0.03 | 0.03 | 0.06 | 0.06 | 0.04 | 0.03 | 0.03 | 0.06 | 0.08 | 0.07 | 0.04 | 0.06 | 0.03 | 0.07 |
SD Uncertainty | | 1.74 | 1.74 | 1.69 | 1.69 | 1.67 | 1.66 | 1.33 | 1.33 | 1.33 | 1.33 | 1.33 | 1.33 | 1.33 | 1.33 | 1.33 | 1.33 | 2.16 | 1.33 | 1.33 | 1.34 |
Pre-Launch SD BRDF | Random | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 | 0.76 |
Straylight | Bias | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 | 0.63 |
M11 BRDF Extrapolation | Random | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 1.70 | 0.00 | 0.00 | 0.00 |
Other SD | | 1.43 | 1.43 | 1.38 | 1.37 | 1.34 | 1.34 | 0.89 | 0.89 | 0.89 | 0.89 | 0.89 | 0.89 | 0.89 | 0.89 | 0.9 | 0.89 | 0.9 | 0.89 | 0.89 | 0.91 |
SD Degradation over Life | Random | 0.12 | 0.07 | 0.13 | 0.07 | 0.10 | 0.04 | 0.10 | 0.04 | 0.10 | 0.04 | 0.04 | 0.09 | 0.03 | 0.09 | 0.13 | 0.09 | 0.16 | 0.08 | 0.10 | 0.20 |
SD - Sun Angle Uncertainty | Random | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 |
Post-Launch BRF Change | Random | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 | 0.50 |
SAS Error | Random | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 | 0.24 |
SDSM Error | | 0.79 | 0.79 | 0.68 | 0.68 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 |
Baseline SDSM Test | Random | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 | 0.61 |
Spectral OOB | Bias | 0.50 | 0.50 | 0.30 | 0.30 | 0.07 | 0.07 | 0.03 | 0.03 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
Lunar Cal Error | Random | 1.00 | 1.00 | 1.00 | 1.00 | 1.00 | 1.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |