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CERES Flight Model 5 on NPP : Pre-Launch Performance  and  Sensor Data Record Validation Kory Priestley 1 G. Louis Smith 1 , Susan Thomas 1 , Herbert Bitting 2 1 NASA Langley Research Center,  2 Northrop Grumman Aerospace Systems IGARSS 2011 Vancouver, British Columbia July 29, 2011
Discussion Topics ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Earth Radiation Budget Components Kiehl & Trenberth 1997 CERES CERES TSIS Top of Atmosphere
Primary CERES Climate Data Records Reflected Solar Energy Emitted Thermal Energy
CERES FM-5 on NPP ,[object Object],[object Object],[object Object],[object Object]
CERES Instrument ,[object Object],[object Object],[object Object],[object Object],[object Object],Orbits 705 km altitude, 10:30 a.m. descending node (Terra) or 1:30 p.m. ascending node (PM-1), sun-synchronous, near-polar; 350 km altitude, 35 o  inclination (TRMM) Spectral Channels Solar Reflected Radiation (Shortwave): 0.3 - 5.0 μm Window: 8 - 12 μm Total: 0.3 to > 100 μm Swath Dimensions Limb to limb Angular Sampling Cross-track scan and 360 o  azimuth biaxial scan Spatial Resolution 20 km at nadir (10 km for TRMM) Mass 45 kg Duty Cycle 100% Power 45 W Data Rate 10 kbps Size 60 x 60 x 70 cm (deployed) Design Life 6 years Base Pedestal MAM Baffles Sensors Total, Longwave, Shortwave Azimuth Axis Elevation Axis Main Electronics Alignment Cube
Enabling Climate Data Record Continuity
[object Object],[object Object],Radiometric Performance Requirements CERES is defined as a class ‘B’ Mission  5-year design Lifetime Spectral Regions Solar Terrestrial Atmospheric Window Wavelengths 0.3 - 5.0   m 5.0 - 200   m 8 - 12   m Scene levels <100 w/m 2 -sr >100 w/m 2 -sr <100 w/m 2 -sr >100 w/m 2 -sr All Levels Accuracy Requirements 0.8 w/m 2 -sr 1.0 % 0.8 w/m 2 -sr 0.5 % 0.3 w/m 2 -sr SOW Stability Requirements < 0.14%/yr < 0.1%/yr Climate Stability Goals < 0.6 w/m 2 /dec < 0.03 %/yr < 0.2 w/m 2 /dec < 0.02%/yr
Why is CERES Climate Quality  Calibration so difficult? A question of time scales, experience and balancing accuracy  with providing data products to the community. - Calibrated Radiances have been released on ~6 month centers - 6 months is just a blink of an eye when analyzing decadal trends… Same time scale as phenomena which influence instrument response - Beta Angle - Earth Sun Distance - Orbital shifts - Instrument Operational modes (e.g. RAPS vs. Xtrack) Design weaknesses and anticipated failures in onboard calibration hardware - full spectral range of observations not covered by cal subsystems Complicates separation of instrument ‘artifacts’ from natural variability.
Cal-Val Approach ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Cal-Val Approach ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
CERES Ground Calibration ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Radiometric Calibration Facility
CERES FM-5 Pre-Launch Calibration Pre-launch Calibrations were performed with TRW’s Radiometric Calibration Facility (RCF). Four separate pre-launch calibration campaigns have been performed on the CERES FM5 instrument after it was fabricated. March 1999 February 2000 October 2006 Sept. –Oct. 2008 Completed hot acceptance tests.  During cold acceptance testing, calibration was stopped due to carousel problems. Tests done in hot and cold acceptance temperatures. Calibration tests done only in hot acceptance temperatures. Full calibration tests in hot and cold acceptance temperatures.  14 days 9 days 11 days 33 days
NPP Thermal Vacuum Summary   CERES TVAC Test Report:  CERES-FM5-I&T-012 ,[object Object],[object Object],[object Object],[object Object],[object Object],CERES goal temperatures over the duration of the test
Calibration Results from TVAC Testing  ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],CERES FM-5 Observatory TVAC Internal Calibration Test Results
Cal-Val Approach ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
CERES Integrated Mission Timeline ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
CERES Flight Radiometric Validation Activities Product Spatial Scale Temporal  Scale Metric Spectral Band Internal BB Filtered Radiance N/A N/A Absolute Stability TOT, WN On-Board Internal Lamp Filtered Radiance N/A N/A Absolute Stability SW Solar Filtered Radiance N/A N/A Relative Stability TOT, SW Theoretical Line-by-Line Filtered Radiance > 20 Km Instantaneous Inter-Channel Theoretical Agreement TOT, WN Unfiltering Algorithm Theoretical Validation N/A N/A N/A N/A TOT, SW, WN Inter-satellite  (Direct Comparison) Unfiltered Radiance 1-deg Grid 1 per crossing Inter-Instrument Agreement, Stability TOT, SW, WN Vicarious Globally Matched Pixels (Direct Comparison) Unfiltered Radiance Pixel to Pixel Daily Inter-Instrument Agreement TOT, SW, WN Tropical Mean (Geographical Average) Unfiltered Radiance 20N – 20S Monthly Inter-Channel Agreement, Stability TOT, WN DCC Albedo Unfiltered Radiance >40 Km Monthly Inter-Instrument agreement, Stability SW DCC 3-channel Unfiltered Radiance >100 Km Monthly Inter-Channel consistency, stability TOT, SW TIme Space Averaging Fluxes Global Monthly Inter-Instrument Agreement LW, SW Lunar Radiance Measurements Filtered Radiance Sub Pixel Quarterly Inter-Instrument Agreement LW, SW, WN
Cal-Val Approach ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
NPP CERES Operational Data Flow SD3E Land PEATE Archive and Distribution Segment (ADS-CLASS) Interface Data Processing Segment (IDPS) Science  Data  Segment (SDS) Science Data Data Records xDRs CERES RDRs,  Sub-sampled VIIRS & aerosols Command, Control and Communication Segment (C3S) Commands, Loads  and requests Raw DRs Sensor DRs Envi. DRs IPs CERES  Instrument Ops Team Ground  Station Svalbard Command  & Telemetry Mission  Data Existing data, agreements Ancillary  Data  Providers Mission Notices  and Data RDRs to PST ERB CARS Data and  Science  Operations Mission Notices  and Data requests Data  Distribution Data  Users  ,[object Object],[object Object],NPP Systems NOAA Systems CERES Systems JPSS Systems
SDR Product Release Strategy Edition1_CV - Static Algorithms and coefficients - baseline product used in    cal/val protocol (L+6 Months, continuous throughout mission) Edition2 - Utilizes temporally varying coefficients to correct for traceable    radiometric drift. All spectral changes are broadband and ‘gray’.  (L+1 yrs to ~5 yrs) Edition3 - Will incorporate temporally varying spectral artifacts in the SW  measurements. A complete re-analysis of Ground Calibration with  additional component characterization measurements. (L+5 yrs) User Applied Revisions - Advance capabilities to the users prior to the  release of the next Edition. Edition2 products lag Edition1_CV by a minimum of 4 months
Data Quality Summary Provided to User’s ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Summary ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
CERES Instrument Working Group Homepage http://asd-www.larc.nasa.gov/Instrument

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IGARSS 2011_Priestley.ppt

  • 1. CERES Flight Model 5 on NPP : Pre-Launch Performance and Sensor Data Record Validation Kory Priestley 1 G. Louis Smith 1 , Susan Thomas 1 , Herbert Bitting 2 1 NASA Langley Research Center, 2 Northrop Grumman Aerospace Systems IGARSS 2011 Vancouver, British Columbia July 29, 2011
  • 2.
  • 3. Earth Radiation Budget Components Kiehl & Trenberth 1997 CERES CERES TSIS Top of Atmosphere
  • 4. Primary CERES Climate Data Records Reflected Solar Energy Emitted Thermal Energy
  • 5.
  • 6.
  • 7. Enabling Climate Data Record Continuity
  • 8.
  • 9. Why is CERES Climate Quality Calibration so difficult? A question of time scales, experience and balancing accuracy with providing data products to the community. - Calibrated Radiances have been released on ~6 month centers - 6 months is just a blink of an eye when analyzing decadal trends… Same time scale as phenomena which influence instrument response - Beta Angle - Earth Sun Distance - Orbital shifts - Instrument Operational modes (e.g. RAPS vs. Xtrack) Design weaknesses and anticipated failures in onboard calibration hardware - full spectral range of observations not covered by cal subsystems Complicates separation of instrument ‘artifacts’ from natural variability.
  • 10.
  • 11.
  • 12.
  • 13. CERES FM-5 Pre-Launch Calibration Pre-launch Calibrations were performed with TRW’s Radiometric Calibration Facility (RCF). Four separate pre-launch calibration campaigns have been performed on the CERES FM5 instrument after it was fabricated. March 1999 February 2000 October 2006 Sept. –Oct. 2008 Completed hot acceptance tests. During cold acceptance testing, calibration was stopped due to carousel problems. Tests done in hot and cold acceptance temperatures. Calibration tests done only in hot acceptance temperatures. Full calibration tests in hot and cold acceptance temperatures. 14 days 9 days 11 days 33 days
  • 14.
  • 15.
  • 16.
  • 17.
  • 18. CERES Flight Radiometric Validation Activities Product Spatial Scale Temporal Scale Metric Spectral Band Internal BB Filtered Radiance N/A N/A Absolute Stability TOT, WN On-Board Internal Lamp Filtered Radiance N/A N/A Absolute Stability SW Solar Filtered Radiance N/A N/A Relative Stability TOT, SW Theoretical Line-by-Line Filtered Radiance > 20 Km Instantaneous Inter-Channel Theoretical Agreement TOT, WN Unfiltering Algorithm Theoretical Validation N/A N/A N/A N/A TOT, SW, WN Inter-satellite (Direct Comparison) Unfiltered Radiance 1-deg Grid 1 per crossing Inter-Instrument Agreement, Stability TOT, SW, WN Vicarious Globally Matched Pixels (Direct Comparison) Unfiltered Radiance Pixel to Pixel Daily Inter-Instrument Agreement TOT, SW, WN Tropical Mean (Geographical Average) Unfiltered Radiance 20N – 20S Monthly Inter-Channel Agreement, Stability TOT, WN DCC Albedo Unfiltered Radiance >40 Km Monthly Inter-Instrument agreement, Stability SW DCC 3-channel Unfiltered Radiance >100 Km Monthly Inter-Channel consistency, stability TOT, SW TIme Space Averaging Fluxes Global Monthly Inter-Instrument Agreement LW, SW Lunar Radiance Measurements Filtered Radiance Sub Pixel Quarterly Inter-Instrument Agreement LW, SW, WN
  • 19.
  • 20.
  • 21. SDR Product Release Strategy Edition1_CV - Static Algorithms and coefficients - baseline product used in cal/val protocol (L+6 Months, continuous throughout mission) Edition2 - Utilizes temporally varying coefficients to correct for traceable radiometric drift. All spectral changes are broadband and ‘gray’. (L+1 yrs to ~5 yrs) Edition3 - Will incorporate temporally varying spectral artifacts in the SW measurements. A complete re-analysis of Ground Calibration with additional component characterization measurements. (L+5 yrs) User Applied Revisions - Advance capabilities to the users prior to the release of the next Edition. Edition2 products lag Edition1_CV by a minimum of 4 months
  • 22.
  • 23.
  • 24. CERES Instrument Working Group Homepage http://asd-www.larc.nasa.gov/Instrument

Editor's Notes

  1. Global maps of the energy leaving the earth system on various temporal and spatial scales.
  2. Data coming from the satellite is retrieved by C3S and is run the IDPS who then sends to the SDS. Note SDS is not an NPOESS feature. Provide Land PEATE sub-sampling software for aggregated VIIRS SDRs (Science) Acknowledge data from SDS Land PEATE (ASDC) Ingest data from SDS Land PEATE &amp; other sources (ASDC) Produce, archive, distribute data products (ASDC) Report status of collection (ASDC) Support user access to collection (ASDC)