1 / 30

Level 2 Scatterometer Processing

Level 2 Scatterometer Processing. Alex Fore Julian Chaubell Adam Freedman Simon Yueh. L2 Processing Flow. L1B geolocated, calibrated TOI σ 0. Average over block; filter by L1B Qual. Flags. L2 (lon, lat) L2 σ TOI + KPC. Ancillary Data: ρ HHVV, f HHHV , f VVHV Θ F (from rad or IONEX).

quant
Télécharger la présentation

Level 2 Scatterometer Processing

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Level 2 Scatterometer Processing Alex Fore Julian Chaubell Adam Freedman Simon Yueh

  2. L2 Processing Flow L1B geolocated, calibrated TOI σ0 Average over block; filter by L1B Qual. Flags L2 (lon, lat) L2 σTOI + KPC • Ancillary Data: • ρHHVV, fHHHV, fVVHV • ΘF (from rad or IONEX) L2 σTOA + KPC Cross-Talk + Faraday Rotation Wind Retrieval L2 wind + σwind • Ancillary Data: • -PALS HIGHWINDS 2009 data • Ancillary Data: • NCEP wind dir. ΔTB retrieval L2 ΔTB+ σΔTB

  3. Level 2 Scatterometer Cross-Talk and Faraday Rotation Mitigation Strategy Alex Fore Adam Freedman Simon Yueh

  4. Forward Beam Integration • We use Mueller matrix formalism • Mtot gives transformation from transmitted signal to received signal. • Model Srx for transmit H (SrxH) and transmit V (SrxV). • Received power for (H or V) is modeled as appropriate element of SrxH + that fromSrxV times instrument gain + noise.

  5. Simulated Total σ0 Performance • Total σ0 performance is independent of any Faraday rotation corrections or cross-talk removal. • De-biased RMSE will be below 0.1 dB for high σ0 for all beams. • Total L2 σ0 as compared to a area-weighted 3 dB footprint model function σ0 computed in forward simulation. • Total is σ0 wind retrieval is our baseline algorithm. • In future we may use the area-gain weighted model function σ0

  6. L2 Faraday and Cross-Talk Mitigation Process Flow TOI: (σHH, σHV, σVV) Explicit fit trained on scale -model antenna patterns Cross-Talk Correction Cross-Talk Corrected: (σHH, σHV, σVV) 2d non-linear minimization problem Ancillary Inputs: Faraday rotation angle -radiometer -IONEX TOA: (σHH, σHV, σVV) Faraday Rotation Correction Assumptions: (ρHHVV, fHHHV, fVVHV ) per beam. PALS HIGHWINDS data

  7. Cross-Talk Correction • Training data: • Forward simulated data with nominal antenna model. • Forward simulated data where cross-talk explicitly set to zero in beam integration. (This was done in a way to conserve total σ0 at level 2). • Computing the Fit: • Perform a least-squares fit of the HV σ0 in the absence of cross-talk to a simple distortion model. • Perform a second least-squares fit to determine how to distribute the remaining σ0 into the co-polarized channels. • Yields an explicit 3 parameter (α, β, γ) fit for each beam Simplified Distortion Model:

  8. Cross-Talk Correction - Beam 1 No cross-talk correction With cross-talk correction nesz≈-26.5

  9. Cross-Talk Correction – Beam 2 With correction No correction nesz≈-25.5

  10. Cross-Talk Correction - Beam 3 No correction With correction nesz≈-24

  11. Faraday Rotation Correction • Inputs: • Faraday rotation angle. • Observed HH, HV, VV σ0. (symmetrized cross-pol) • HH-VV correlation; ratio of HV to both HH and VV channels. This factor may need to be tuned depending on if cross-talk removal is or is not performed before Faraday rotation correction. • Method: • Non-linear measurement model. • Minimize cost function to solve for Faraday rotation corrected σ0 HH and σ0 VV. (called sigma true below). • Obtain σ0 HV via conservation of total σ0. Measurement Model: Cost Function

  12. Faraday Rotation Correction – Beam 1 No correction With correction No correction With correction

  13. Faraday Rotation Correction – Beam 2 With correction No correction With correction No correction

  14. Faraday Rotation Correction – Beam 3 No correction With correction No correction With correction

  15. Open Issues / Future Work • Antenna patterns: • The cross-talk from the theory and scale-model antenna patterns seems to be significantly different. • Will the cross-talk in the as-flown configuration differ from both the theory and scale-model patterns? • The error estimate for Faraday rotation correction needs to be analyzed for nominal ionospheric TEC, not worst case. • We need to develop a strategy to determine antenna patterns post-launch.

  16. Level 2 Scatterometer Wind Retrieval Alex Fore Julian Chaubell Adam Freedman Simon Yueh

  17. L2 Wind Retrieval Process Flow Baseline algorithm: -total σ0 approach. -Faraday rotation and cross-talk has no effect on total σ0 approach. Ancillary Inputs: -NCEP wind direction Inputs: -Total σ0 -antenna azimuth -Kpc estimate L2 Scat wind speed + error Solve for wind speed Newton’s Method: 1d root-finding problem Newton’s Method Wind Model Function -input: wind speed, relative azimuth angle, incidence angle (or beam #) -output: total sigma-0

  18. L2 Wind Retrieval • We also compute a wind speed error due to the uncertainty in the scatterometer σ0,tot. • From the estimated kpc we have the variance of the observed σ0,tot. • We numerically compute dw/dσ0tot and propagate the error to a variance for wind.

  19. Simulated Total σ0 Wind Retrieval Performance • Total σ0 performance is independent of any Faraday rotation corrections or cross-talk removal. • As compared to beam-center NCEP wind speed: • B1 total std: 0.205 m/s • B2 total std: 0.186 m/s • B3 total std: 0.226 m/s • By construction, when we derive the model function from the data there will be no bias.

  20. Wind Speed Retrievals

  21. Open Issues / Future Work • Derivation of model function from the data. • Re-perform the analysis using averaged wind over 3-dB footprint as the truth for training • Comparison of predicted σwind to observed RMSE of retrieved wind as compared to beam center wind. • Use individual polarizations to retrieve winds after calibration of individual channels.

  22. Level 2 Scatterometer Delta TB Estimation Alex Fore Adam Freedman Simon Yueh

  23. PALS HIGHWINDS 2009 Campaign • NASA/JPL conducted HIGHWINDS 2009 campaign with following instruments: • POLSCAT, a Ku band scatterometer. • PALS, a L-band scatterometer and radiometer. • From POLSCAT we determine the wind speed, and then we consider the relationship to the observed L-band active and passive observations • From this data we can show the high correlation between radar σ0 and excess TB due to wind speed. • We also can derive the wind speed - radar σ0 model function as well as the wind speed – ΔTB model function.

  24. PALS HIGHWINDS Results • We find very high correlation between wind speed and TB( > 0.95 ). • We also find a similarly high correlation between radar backscatter and TB. • Suggests radar σ0 is a very good indicator of excess TB due to wind speed. • Caveat: we need ancillary wind direction information for Aquarius: PALS results show a significant dependence on relative angle between the wind and antenna azimuth.

  25. PALS HIGHWINDS Results (2)

  26. PALS HIGHWINDS Results (3) • From all of the data we derived a fit of the excess TB wind speed slope as a function of Θinc.

  27. L2 ΔTB • L2 ΔTB will be the scatterometer wind speed times the PALS dTB/dw. (Note: not included in v1 delivery) • We estimate the ΔTB errors due to the wind RMSE numbers on previous slide. PALS Tb relation:

  28. Comparison with Previous Measurements • Horizontal polarization has very good agreement with the measurements from WISE ground-based campaign. • Large discrepancy for vertical polarization • Cause is uncertain • Wave effects? • WISE – Camps et al., TGRS 2004 • Hollinger – TGE, 1971 • Swift – Swift, Radio Science, 1974

  29. L2 ΔTB

  30. Open Issues / Future Work • The wind speed - ΔTB coefficients will be updated with Aquarius data after launch.

More Related