Elana Fertig Jos Aravquia Hong Li Seung-Jong Baek Junjie Liu Brian - - PowerPoint PPT Presentation

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Elana Fertig Jos Aravquia Hong Li Seung-Jong Baek Junjie Liu Brian - - PowerPoint PPT Presentation

Elana Fertig Jos Aravquia Hong Li Seung-Jong Baek Junjie Liu Brian Hunt Edward Ott Eugenia Kalnay Istvan Szunyogh Eric Kostelich Ricardo Todling University of Maryland NASA Goddard Space Flight Center Arizona State University CPTEC, Brazil


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SLIDE 1

Elana Fertig

November 4, 2010

José Aravéquia Seung-Jong Baek Brian Hunt Eugenia Kalnay Eric Kostelich Hong Li Junjie Liu Edward Ott Istvan Szunyogh Ricardo Todling University of Maryland NASA Goddard Space Flight Center Arizona State University CPTEC, Brazil

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SLIDE 2

Overview

  • Ensemble-based assimilation schemes

– Utilize flow-dependent forecast uncertainties. – Provide superior estimates than operational schemes because they account for “errors of the day.”

  • Correcting forward model errors

– Bias correction of radiances in assimilation schemes – Ensemble schemes can correct for these biases

  • Assimilating satellite observations

– Radiance observations improve forecasts in temperature and winds

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SLIDE 3

Overview

  • Ensemble-based assimilation schemes

– Utilize flow-dependent forecast uncertainties. – Provide superior estimates than operational schemes because they account for “errors of the day.”

  • Correcting forward model errors

– Bias correction of radiances in assimilation schemes – Ensemble schemes can correct for these biases

  • Assimilating satellite observations

– Radiance observations improve forecasts in temperature and winds

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SLIDE 4

Forecast ~106 - 108 d.o.f. Observations ~105 - 107 d.o.f.

B R

Covariances in 3D and 4D-VAR

  • E. Kalnay
slide-5
SLIDE 5

Structure of Forecast Errors

  • E. Kalnay

Forecast ~106 - 108 d.o.f. Observations ~105 - 107 d.o.f.

slide-6
SLIDE 6

Ensemble Kalman Filter Schemes

  • E. Kalnay

Observations ~105 - 107 d.o.f. Forecast ~106 - 108 d.o.f.

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SLIDE 7

Local Ensemble Transform Kalman Filter (LETKF)

LETKF finds the best linear combination of the ensemble members fitting observations at the analysis time. time analysis at time t-1 analysis at time t

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SLIDE 8

Forecast Uncertainty

Operational Schemes:

  • Constant forecast

error covariance matrix.

  • Subject to “errors of

the day”. Ensemble Schemes:

  • Propagate the

forecast error covariance with an ensemble.

time t-1 time t

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SLIDE 9

Perform data assimilation in local patch (3D-window) The state estimate is updated at the central grid red dot All observations (purple diamonds) within the local region are assimilated

Localization

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SLIDE 10

Perform data assimilation in local patch (3D-window) The state estimate is updated at the central grid red dot All observations (purple diamonds) within the local region are assimilated

Localization

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SLIDE 11

Perform data assimilation in local patch (3D-window) The state estimate is updated at the central grid red dot All observations (purple diamonds) within the local region are assimilated

Localization

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SLIDE 12
  • LETKF is model independent and relatively simple to

implement.

  • Can parallelize the LETKF scheme.
  • Gain further efficiency because matrix computations are

performed in the space spanned by the ensemble.

  • LETKF takes only 5 minutes on a 20 node PC cluster,

which is comparable to the computational cost of

  • perational schemes.
  • LETKF should provide a more accurate analysis than
  • perational schemes because it utilizes an evolving

forecast error covariance.

  • LETKF can adjust for “errors of the day.”

Features of LETKF

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SLIDE 13

Comparing LETKF to NCEP’s 3D-VAR

  • Use NCEP’s 3D-VAR (SSI) and LETKF as the data assimilation scheme for

T62 NCEP GFS.

  • Assimilate all conventional observations for Jan-Feb, 2004.
  • Analyses and forecasts are verified against operational T254 analysis.
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SLIDE 14

Comparing LETKF to NCEP’s 3D-VAR

  • Use NCEP’s 3D-VAR (SSI) and LETKF as the data assimilation scheme for

T62 NCEP GFS.

  • Assimilate all conventional observations for Jan-Feb, 2004.
  • Analyses and forecasts are verified against operational T254 analysis.

In NH, the results are comparable

In SH, the LETKF results

are much better than SSI

Szunyogh, Kostelich, et al. (2007) Tellus A RMS error (K) RMS error (K)

NH SH

Pressure (hPa) Pressure (hPa) 48 hour temperature SSI LETKF

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SLIDE 15

Overview

  • Ensemble-based assimilation schemes

– Utilize flow-dependent forecast uncertainties. – Provide superior estimates than operational schemes because they account for “errors of the day.”

  • Correcting forward model errors

– Bias correction of radiances in assimilation schemes – Ensemble schemes can correct for these biases

  • Assimilating satellite observations

– Radiance observations improve forecasts in temperature and winds

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SLIDE 16

Form of Satellite Observations

  • Model for unbiased satellite observations is

y = h(xtrue) + η,

– h takes model state variables into observation space – xtrue is the true model state – η is unbiased random noise

  • Biased satellite observation are assumed to be of the

form

– β is a vector of bias parameters to be determined.

y = ˜ h xtrue,β

( ) + η

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SLIDE 17

Estimating Bias Parameters

  • Biased satellite observation are assumed to be of the form
  • β can be estimated online, during the data assimilation procedure

(Derber and Wu, 1998; Dee and DaSilva, 1998; Baek et al., 2006)

  • Ensemble-based schemes can incorporate a variety of bias

correction techniques for radiances, including

– Variational bias estimate and ensemble analysis (Miyoshi et al., 2010) – State space augmentation (Fertig et al., 2009)

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SLIDE 18

LETKF

time LEKF finds the best linear combination of the model state ensemble members fitting the observations at the analysis time analysis at time t-1 analysis at time t

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SLIDE 19

LETKF with state space augmentation bias correction

time analysis at time t-1 analysis at time t

Analysis  [Analysis; Bias]

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SLIDE 20

LETKF with state space augmentation bias correction

Finds the best linear combination of the ensemble of model states and bias parameters fitting the observations. time analysis at time t-1 analysis at time t

Analysis  [Analysis; Bias]

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SLIDE 21

Perfect model scenario: A “true” trajectory is generated by integrating the SPEEDY (low resolution, simplified GCM) model for two simulated months (Jan and Feb, 1982). Observations:

  • Rawinsonde observations (U, V, T, Ps)
  • Satellite observations

– Use pCRTM to simulate 15 AIRS channels. – Created at every model grid point. – Bias simulated by assuming there is a fractional error in the satellite absorption coefficient (Watts and McNally, 2004).

  • Satellite forward model uses raw pCRTM without

without the Watts and McNally term.

Perfect model experiments

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SLIDE 22

Typical Simulated Satellite Bias

Time averaged satellite observation bias

The simulated bias has a similar structure to the true bias.

0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 K

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SLIDE 23

Temperature Analysis RMS Error (global and Feb. average)

The bias correction improves the analysis.

RMS Error (K) Pressure (hPa)

100 200 300 400 500 600 700 800 900 0 0.5 1 1.5 2 2.5 3

  • Conventional
  • Biased satellite and conventional
  • Unbiased satellite and conventional
  • Constant correction
  • Constant and 850 to 300hPa thickness
  • Constant and surface skin temperature
  • All three predictors.
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SLIDE 24

Overview

  • Ensemble-based assimilation schemes

– Utilize flow-dependent forecast uncertainties. – Provide superior estimates than operational schemes because they account for “errors of the day.”

  • Correcting forward model errors

– Bias correction of radiances in assimilation schemes – Ensemble schemes can correct for these biases

  • Assimilating satellite observations

– Radiance observations improve forecasts in temperature and winds

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SLIDE 25

Assimilating radiances in NCEP GFS

  • Use LETKF as the data assimilation

scheme for T62 NCEP GFS.

  • Assimilate all conventional
  • bservations and AMSU radiances

for Jan-Feb, 2004.

  • Bias correction terms are (1)

constant, (2) scan angle, (3) skin temperature

  • Analyses and forecasts are verified

against operational T254 analysis. Conventional Observations Radiances without bias correction Radiances with bias correction Bias correction enables positive impacts from AMSU observations.

slide-26
SLIDE 26

Assimilating radiances in NCEP GFS

  • Use LETKF as the data assimilation

scheme for T62 NCEP GFS.

  • Assimilate all conventional
  • bservations and AMSU radiances

for Jan-Feb, 2004.

  • Bias correction terms are (1)

constant, (2) scan angle, (3) skin temperature

  • Analyses and forecasts are verified

against operational T254 analysis. Conventional Observations Radiances without bias correction Radiances with bias correction Bias correction enables positive impacts from AMSU observations.

slide-27
SLIDE 27

Assimilating radiances in NCEP GFS

  • Use LETKF as the data assimilation

scheme for T62 NCEP GFS.

  • Assimilate all conventional
  • bservations and AMSU radiances

for Jan-Feb, 2004.

  • Bias correction terms are (1)

constant, (2) scan angle, (3) skin temperature

  • Analyses and forecasts are verified

against operational T254 analysis. Conventional Observations Radiances without bias correction Radiances with bias correction Cross-correlations enable positive impacts in wind field from AMSU.

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SLIDE 28

Conclusions

  • Ensemble schemes efficiently incorporate flow-

dependent forecast uncertainties in a model independent way.

  • LETKF improves the analysis obtained from 3D-VAR.
  • LETKF can estimate radiance biases through forward

model errors online efficiently.

  • Bias correction improves analyses and forecasts in

simulations with “perfect model” and real radiances.

  • LETKF successfully uses cross-correlations between

dynamic variables to improve forecasts of unmeasured variables.

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SLIDE 29

Biased AIRS observations

  • Typical radiative transfer model:
  • Assume the error in the satellite observations is in the

absorption coefficient:

  • Watts and McNally (2004) find γ = 1.05 for AIRS.

h(x) = B(T(p))dτ ∫ τ = exp − κ(p)ρ(p)dp ∫

( )

κ →γκ τ → τ γ