Assimilation and Impact of GPS Radio Occultation data - PowerPoint PPT Presentation

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Assimilation and Impact of GPS Radio Occultation data

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UCAR and JPL have agreed on a 'minumiuCurrently tracking in OL ... There appear to be no show-stoppers or insurmountable problems - just a lot of tough problems ... – PowerPoint PPT presentation

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Title: Assimilation and Impact of GPS Radio Occultation data


1
CDAAC Update
2
Issues
3
Open Loop Status at JPL
  • UCAR and JPL have agreed on a minumiuCurrently
    tracking in OL mode each day UT 10 - 16
  • Setting OL occultations working well
  • Rising OL occultations presently 15 per 6 hours
    that look good
  • Bug fix of scheduler should bring this to 50 /
    six hours
  • Transition to L1 phased-lock-loop (PLL) at -10 km
    line-of-sight altitude (LSA)
  • Transition to L2 PLL 3-4 seconds later (15-20 km
    tangent point height)
  • UCAR is expected to receive data by next week
  • JPL still needs to write the data translator
  • UCAR and JPL have agreed on a minimum
    requirement document for first flight software
    version (expected in a few weeks)
  • Things look positive - need to see the data

4
CDAAC Open Loop Data Processing Status
  • CDAAC processed some initial OL data from JPL
    (Aug. 04)
  • Format of OL data and content will change again
    in next release
  • Significant changes to the CDAAC software are
    expected including
  • Level 0 - Level 1 translator
  • Additional external data are needed (50 bps data
    stream)
  • Format of excess phase file may have to be
    changed to include OL model output
  • Interface to inversion software will have to be
    changed
  • Changes will be significant but it is not clear
    yet what is the best way to accomplish them
  • Work on this will hopefully start March 14 05

5
Receiver generated doppler (model) agrees
reasonably well with UCARs model. several Hz
6
Reasonable SNR can be observed for open loop data
(right of red line)
7
(No Transcript)
8
Refractivity profile from one of the early OL
profiles from SAC-C
9
OL starts at 3000, Data bit modulation cannot
be removed after 4000 samples
10
Bit Grab Receivers
  • COSMIC has to develop GPS receivers to collect
    and send to CDAAC all GPS data bits (50 bps data
    stream)
  • Contract with CU has been negotiated - FFP for
    25 k to design and build 10 such receivers
  • UCAR/COSMIC is purchasing all the hardware
    computers, special GPS receiver boards, etc
  • Receivers must be installed at global sites
    (Boulder, Kyoto, Potsdam, Sao Paulo, Wellington,
    Johannesburg, .) host sites must still be found
    and negotiated
  • Prototype is currently collecting data bits at CU
  • Establishing this network is challenging - but on
    track
  • Without this network OL data profiles degrade

11
Fiducial Network for COSMIC
  • Three COSMIC fiducial sites installed in TWP
  • Two COSMIC fiducial sites delivered to Brazil
    (just passed customs)
  • Eleven fiducial sites are regularily received in
    real-time from NRCan (IGS)
  • Six more sites will become available by March 11
    (this week)
  • 30 sites are received with 15 minutes latency
    from CDDIS
  • Presently we receive sufficient amount of
    fiducial data for the COSMIC mission goals (still
    we plan to add 20 more real-time sites for
    greater redundancy)

12
Revising CDAAC QC
  • Existing CDAAC QC has been reviewed based on
    feed-back from first assimilations at NCEP and
    comparison with ECMWF reanalysis
  • Generally the existing QC was found to work well
    by rejecting most bad occultations
  • However, some bad occultation still passes the QC
    with errors up to 40
  • By closely inspecting those profiles it was found
    that these outliers can be divided into five
    categories
  • Too late truncation of L1 when this signal is
    lost
  • Too late truncation of L2 when this signal is
    lost
  • Too low truncation of the radio holographic
    bending angle profile
  • Bad signals (tracking errors and 1 second spike
    (CHAMP))
  • Poor adjustment of climatology for statistical
    optimization

13
Improved CDAAC QC
  • Threshold for controlling the truncation of L1
    and L2 have been tightened to avoid big errors in
    the troposphere related to L1 and L2 truncation
    time
  • A new more conservative QC check has been
    introduced to control the truncation height of
    the radio holographic bending angle profile
  • A New QC check has been introduced to catch bad
    profiles based on relative deviations from the
    climatology bending angle and deviations between
    RO scale height and the scale height of the
    climatology
  • A more robust technique for adjusting the
    climatology for statistical optimization has been
    implemented
  • New QC criteria greatly reduces the number and
    magnitude of outliers

14
Result Improvements at UCAR
Old
New
15
BUFR and data distribution UCAR
16
Space Weather data analysis at CDAAC
  • Defining near-real-time ionospheric products and
    formats - draft to be sent out to the space
    weather community with a request for feedback
  • Absolute TEC to all GPS satellites in view at all
    times - automatic editing algorithm to delete
    outliers and correct for cycle slips -
    solving for differential code biases (one day
    averages) of COSMIC GPS receivers (POD antennae)
    - near-real-time calibration of TEC
  • TIP processing - conversion from raw TIP data
    to radiances (getting radiance code from Scott
    Budzien, NRL) - calculate pointing direction from
    orbit and attitude of spacecraft
  • Electron density profiles - derive orbit electron
    density from TEC observations to be used for
    initialization (upper boundary) of profile
    retrievals - use horizontal gradients from
    Global Ionospheric Maps (GIMs) for improved
    ionospheric profiling (getting GIMs either from
    JPL or from CODE)

17
Near Real-Time CHAMP Orbit Overlap Results (vs.
JPL) with Bernese v5.0
Arcs for every CHAMP data dump
Position
Velocity
18
COSMIC GPS Antenna Test at Ball Aerospace
19
Antenna Requirements
20
COSMIC GPS Limb Antenna GainSAD0deg
L2
L1
21
COSMIC GPS Limb AntennaL3 Phase (FOV7 X
40)SAD(0)
L3 Phase (mm)
Gradient Magnitude(mm/deg)
22
COSMIC GPS POD AntennaL3 Phase (FOV60)SAD(0)
L3 Phase (mm)
Gradient Magnitude(mm/deg)
23
POD Excess Phase Status
  • POD - To Do
  • - Analyze orbit quality for all missions,
    optimize reduced-dynamic tracking
  • - Investigate simultaneous use of data from 2
    POD antennas
  • - Additional real-time
  • Excess Phase
  • - Test single-difference and zero-difference
    (GRACE-USO) processing
  • - correct cycle slips in non-occulting links
  • - modify software to process data with short
    gaps in non-occulting links
  • - include antenna phase center corrections in
    processing
  • - Complete documentation and algorithm
    description

24
CDAAC Status Summary
  • A lot of work and exciting challenges remain
  • There appear to be no show-stoppers or
    insurmountable problems - just a lot of tough
    problems
  • CDAAC team is working hard and making progress
  • CDAAC will be completed for launch assuming that
  • No unexpected problems in OL data
  • Postpone or receive additional help to deal with
    RoadRunner
  • TBB network will be installed by NRL and NRL
    provides TIP software modules
  • No staffing changes (hired J. Johnson for Bit
    Grabber project, fiducial tasks and software
    support)
  • Minimize distractions of CDAAC staff between now
    launch
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