EFSO and DFS diagnostics for JMA s global Data Assimilation System: their caveats and potential pitfalls

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EFSO and DFS diagnostics for JMA s global Data Assimilation System: their caveats and potential pitfalls Daisuke Hotta 1,2 and Yoichiro Ota 2 1 Meteorological Research Institute, Japan Meteorological Agency 2 Numerical Prediction Division, Japan Meteorological Agency Special thanks to: many colleagues at JMA Eugenia Kalnay (UMD) and Takemasa Miyoshi (UMD/RIKEN) for general advice 1

EFSO and DFS diagnostics for JMA s global Data Assimilation System: their caveats and potential pitfalls Daisuke Hotta 1,2 and Yoichiro Ota 2 1 Meteorological Research Institute, Japan Meteorological Agency 2 Numerical Prediction Division, Japan Meteorological Agency Special thanks to: many colleagues at JMA Eugenia Kalnay (UMD) and Takemasa Miyoshi (UMD/RIKEN) for general advice 2

1. Adjoint and Ensemble FSO FSO: Forecast Sensitivity to Observations!(#) = # & '#, e: vector of forecast error Δ! = # & & ) + '# ) + # ) -. '# ) -. 5 8 0 1-2& 34 + 34 ) + 3! 36 7 5 9 34 8 + 34 ) + < < (4 : ; =4: >? )/A = 0 1-2& B & C & ' # ) + + # ) -. Adjoint FSO (Langland and Baker 2004) 0 1-2& E F-E G-E H 5 8& + I ) + ' #) + + # ) -. Ensemble FSO (Kalnay et al. 2012) 3

2. FSOI inter-comparison project (c.f. Rahul Mahajan s talk this morning) Different global NWP centers computed FSOI data for the same period using the same error-norm metric. Data collected from GMAO, NRL, Met Office, JMA (adjoint) NCEP, JMA (ensemble) Note: JMA is the only center that provided both adjoint and ensemble FSO. 4

3. EFSO impact amplitude deviates from adjoint FSO Courtesy of T. Auligné and R. Mahajan Adjoint FSO from different centers have comparative amplitudes, whereas NCEP (EMC) s EFSO exhibits O(10) larger amplitude, and JMA s EFSO exhibits ~ 0.2 times smaller amplitude NCEP Why? 5

4. NCEP s EFSO Overestimation problem: Inconsistent use of K for mean update and covariance update Mean update: Compute P a first, then compute δx a by Kd=P a H T R -1 d No inflation applied to P a Covariance (perturbation) update: Compute P a, then applied posterior inflation (relaxation to prior) à To correctly estimate obs impact (how each obs improved ens mean), X f has to be initialized from uninflated X a. But the NCEP implementation of EFSO uses X f initialized from inflated X a (D. Groff., pers. comm.) 6

5. JMA s EFSO Underestimation problem: Estimated and actual forecast error reduction # EFSO Δ) * = 1 2. 23 / 14. 2 / 1 1 2. 23 2 / 674. / 67 # EFSO Δ) * JMA EFSO, lead time=24 hr EFSO successfully reproduces temporal variation of forecast error reductions (correlation coefficient as high as ~ 0.8), but Only ~ 20 % of the amplitude explained by EFSO. 7

6. A possible reason for impact underestimation (1/3) EFSO implemented for JMA s LETKF underestimates forecast error reduction. Why? Bug? à not found. Possible reason: forecast errors not well captured by the space spanned by the forecast perturbations 8

6. A possible reason for impact underestimation (2/3) EFSO formulation: Δ" #$% ' ($' )* + $',. / 0 #* 1(3 4 6 # # +34 $8 ) In evaluating @0 # A3 0 #* 1(3 4 6 # # +34 $8 ) = 1 '/< 0 # * [1 ' <(3 4 6 # # +34 $8 )] =: @0 #* A3 the portion of B3 that lies in the nullspace of @0 # does not contribute to @0 #* A3. Namely: Let B3 = B3 CDEF + B3 FGHH, B3 CDEF span @0 #, B3 FGHH null @0 # then @0 #* A3 = @0 #* B3 CDEF + B3 FGHH = @0 #* B3 CDEF N.B.: This issue does not arise in adjoint FSO. 9

6. A possible reason for impact underestimation (3/3) Does this hypothesis really explain the impact underestimation? à Verify the hypothesis by performing the following diagnostics: For each model grid, Restrict all state vectors (mean and ptb) into localization volume Decompose!" into!" #$%& and!" &'((. (detail in the backup slide) Compute the explained fraction!" )*+, -!" -. Compare this with the impact underestimation /012 34 -. If the two agrees, we conclude that the hypothesis is likely correct. 10

Diagnosed explained fraction Horizontal distribution (near tropopause level) "! #$%& ' "! ' Vertical Profile (global average) -+- Kinetic -x- Dry -*- Moist Fcst err well-captured by ensemble over the SH ocean, but not over the land. à Perhaps related to observation density: Data-sparse area: analysis (verification) and forecast both close to model s free+ run à "( * similar to Bred Vector à covered well by,+ Errors in moisture difficult to capture by the ensemble. Very good agreement between "! #$%& "! ' ' and 11./01 23 '! (both ~ 20%)

Explained fraction increases when ens covariance is given higher weight The 20 % explained fraction is obtained for EFSO within hybrid 4D-Var (LETKF anl mean recentered to Var anl) where B hyb =0.23B ens + 0.77B clim We observed that explained fraction increases monotonically with ens cov weight. Explained fraction for pure (stand-alone) LETKF was as high as 67% 12

7. Conclusion EFSO is successfully implemented on JMA s global DA system, but the total impact considerably underestimated. Explaiend fraction diagnostics has been proposed that decomposes fcst err into column- and null- spaces of the fcst ensemble! " The results suggests that significant portion of fcst err lies in the null-space of! ", which exposes the lack of the ensemble size used at JMA (currently only 50). 13

Questions? Suggestions? Questions from me to you: Have I addressed localization correctly? What does my conclusion imply about validity of EFSO diagnostics? 14

Backup slides

Hybrid 4DVar-LETKF DA developed in JMA Analysis resolution (outer / inner) T L 959L100 (~20km, top:0.01hpa) / T L 319L100 (~55km, top:0.01hpa) Assimilation window 6 hours (analysis time +/- 3 hours) Hybrid method Extended control variable method (Lorenc2003) Weights on B β stat2 = 0.77, β ens2 = 0.23 LETKF resolution T L 319L100 Ensemble size 50 Localization scale (4DVar) Horizontal: 800km Vertical: 0.8 scale heights Localization scale Horizontal: 400km, Vertical: 0.4 (LETKF) (0.8 for Ps) scale heights Covariance inflation Adaptive inflation (Miyoshi 2011) Deterministic part Deterministic forecast QC 4DVar Next analysis from Yoichiro Ota (2015, Adjoint Workshop) Deterministic analysis Observations Recentering B = b B + b 2 stat Operational global DA at JMA is 4DVar (not hybrid) stat Static (Climatological) background error covariance Ensemble part Ensemble forecast Perturbations Ensemble mean QC EnKF (LETKF) Ensemble analysis Next analysis 2 ens B ens Ensemble-based background error covariance 16

EFSO implementation at JMA DA system: hybrid LETKF/4D-Var coupled with JMA GSM Resolution: (outer) TL959L100 ; (inner and ensemble) T319L100 Window: 6 hours (analysis time +/- 3 hours) B weights: 77% from static, 23% from ensemble Member size: 50 Localization scales (e-folding): LETKF: Horizontal: 400km, Vertical: 0.4 scale heights 4D-Var: Horizontal: 800km, Vertical: 0.8 scale heights Covariance Inflation: Adaptive inflation of Miyoshi (2011) LETKF part initially coded by Dr. T. Miyoshi; maintained and updated by Y. Ota and T. Kadowaki. EFSO: Lead-times investigated: FT=0,6,12,24 Localization scales: same as LEKTF advection: moving localization scheme of Ota et al.(2013) with scaling factor of 0.5 for horizontal wind. Verification: high-resolution analysis from 4D-Var Error norm: KE, Dry TE and Moist TE by Yoichiro Ota (2015) Period: Jul. 10, 2013, 06UTC Jul. 15, 2013, 18UTC (5days, 20cases) 17

Decomposition of fcst error into column- and null- spaces of fcst ptbs Fix a grid and consider a local patch that would be used if an observation was located at the grid point in question. In the derivation below, all vectors/matrices are assumed to be restricted to this local patch. In EnKF, the sum of each column of = > is zero, so rank(= > )=D 1: span H= > = span H= > I,, H= > KLI, H= > K = span H= > I,, H= > KLI In light of this, we now denote by H= > the first D 1 columns of the original H= >. Now, suppose that NO Q R S (OT V > > +O T LX ) can be decomposed as NO = NO YZ[\ + NO \]^^, NO YZ[\ = `ab clb d e H= > = H= > f, ` f = d I, d KLI g Multiplying NO = NO YZ[\ + NO \]^^ with Q I/h = > g =: H= >g from left, NO \]^^ vanishes by definition, giving: H= >g NO = H= >g H= > f + NO \]^^ = H= >g H= > f f = H= >g H= > LI H= >g NO h Once f is determined, we can obtain NO YZ[\ and NO h \]^^ by h NO YZ[\ = H= > f h = H= > f g H= > f = f g H= >g H= > f = f g H= >g NO NO h \]^^ = NO h h NO YZ[\