STAR Calibration Support for GOES Post Launch Test (PLT) PowerPoint PPT Presentation

presentation player overlay
About This Presentation
Transcript and Presenter's Notes

Title: STAR Calibration Support for GOES Post Launch Test (PLT)


1
STAR Calibration Support forGOES Post Launch
Test (PLT)
  • X. Wu F. Yu
  • NOAA/NESDIS/STAR/SPB ERT _at_ NOAA

2
PLT Overview
  • GOES PLT is similar to POES OV in many ways
  • Longer, more complicated spacecraft maneuver
  • Engineering Test
  • Functionality of component and system
    (instrument)
  • Science Test
  • Products generation from instrument measurements
  • Radiance quality can be part of either, but has
    been primarily part of the Science Test.

3
PLT History (Science Test)
  • GOES-8 (1994)
  • 1st of its kind learn to make the best use of
    the data
  • Radiance is validated (quite substantially), but
    little beyond
  • GOES-9 (1995)
  • Still not formal, if any.
  • GOES-10 (1997)
  • Solar panel deployment led to yaw flip
  • Science Test in April 1998 to make sure its
    compatible with GOES-8/9
  • 1st 1-min rapid scan.
  • Goes-11/12 (2000/2001)
  • Formal and routine
  • GOES-13 (2006)
  • Significant change in hardware more
    sophisticated Science Test

4
PLT Structure
  • Engineering test has always been led by NASA
  • Science Test was earlier led by CIMSS and later
    co-led with OPDB or CIRA.
  • Calibration support
  • STAR personnel detailed at SOCC
  • With contractor support at SOCC
  • Engineering Test
  • Oversee the Implementation of CPIDS (examples).
  • Supply certain tests (example)
  • Science Test
  • Diagnose and correct for operational and
    calibration anomalies (examples)

5
Calibration Database Before/During PLT
  • Specify and verify
  • Coefficients and limits
  • Changes (e.g., BB dwell)
  • Generate some, e.g., band correction, scan mirror
    emissivity
  • OGE Compatibility Test
  • Unlike POES, GVAR is not Level 1b (in its
    traditional definition)
  • Need to test calibration and geo-location

6
Test Description for PLT
  • TEST NUMBER IC115
  • TEST NAME Benefits of Imager Extended Blackbody
    Dwell
  • TEST ENGINEER Angel Butts
  • TEST TYPE Characterization
  • TEST DURATION N/A
  • SPECIFICATION REFERENCES
  • GOES-NOPQ CCR 4233 Rev. (8/22/00) Increase SN08
    Imager Black Body Dwell Time.
  • GOES-NOPQ CCR 4233 Rev. B (2/27/01) Imager
    Blackbody Dwell Modifications and Miscellaneous
    Cleanup of the GOES NOPQ Imager and Sounder ICDs.
  • OBJECTIVES
  • To quantify the reduction in the variability in
    the means of the blackbody counts, the
    calibration slopes, and the frame-mean striping
    resulting from the increase in blackbody dwell
    time from 0.2s to 2.0s.
  • DESCRIPTION
  • 1. Data collected during 24 hours of successive
    blackbody events will be processed in parallel in
    two MSPSs. At each blackbody event, each MSPS
    routinely computes the means and standard
    deviations (in units of 10-bit digital counts) of
    the sequence of blackbody samples in each IR
    channel. In these computations, at each event one
    MSPS will use only the first 1000 blackbody
    samples, while the second MSPS will use the
    entire nominally 10,000 samples. We will use
    the means and standard deviations of the
    blackbody count levels, routinely produced by the
    MSPSs, to compute the standard errors of the
    means for each channel for each blackbody event.
    The standard errors from the two MSPSs will be
    compared. (If the distribution of blackbody data
    were close to normal, their ratio would be
    approximately ?10.) Also, the standard
    deviations (in counts) will be converted, through
    the calibration, to units of temperature and
    compared with the noises computed from
    thermal/vacuum tests and the noises computed in
    PLT IS004--Imager IR Channel Noise Equivalent
    Temperature Differences. The S.D.s from the 1000
    and the 10,000 samples should be nearly the same,
    both of them should be about the same as the
    S.D.s from the other tests, and all of them
    should meet spec.

7
Calibration Support During/After PLT
  • Operational anomalies confirm and diagnose
  • GOES-13 Sounder visible channel boost
  • GOES-14 cal/nav coeff., buffer overflow, Imager
    Ch6 det ID
  • Calibration Anomalies things were more or less
    complicated
  • Scan mirror emissivity
  • Midnight Blackbody Calibration Correction
  • Imager visible channel normalization
  • Radiance validation accuracy precision
    GEO-GEO GEO-LEO vis IR, imgr sndr
  • Co-registration
  • Stray light
  • Sounder striping

8
Preliminary http//www.star.nesdis.noaa.gov/smcd/
spb/fwu/homepage/GSICS_GOES14_AIRS_IASI.php
9
Issues
  • Need data during PLT
  • Both in real time and archived
  • Better for GOES-14, but far from ideal
  • Even available, GVAR is not Level 1b
  • Often a limiting factor for detailed
    investigations
  • Need more dedication
Write a Comment
User Comments (0)
About PowerShow.com