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State space model of precipitation rate (Tamre Cardoso, PhD UW 2004) Updating wave height forecasts using satellite data (Anders Malmberg, PhD U. Lund.

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Presentation on theme: "State space model of precipitation rate (Tamre Cardoso, PhD UW 2004) Updating wave height forecasts using satellite data (Anders Malmberg, PhD U. Lund."— Presentation transcript:

1 State space model of precipitation rate (Tamre Cardoso, PhD UW 2004) Updating wave height forecasts using satellite data (Anders Malmberg, PhD U. Lund 2005) Model emulators (O’Hagan and co- workers )

2 Rainfall measurement Rain gauge (1 hr) High wind, low rain rate (evaporation) Spatially localized, temporally moderate Radar reflectivity (6 min) Attenuation, not ground measure Spatially integrated, temporally fine Cloud top temp. (satellite, ca 12 hrs) Not directly related to precipitation Spatially integrated, temporally sparse Distrometer (drop sizes, 1 min) Expensive measurement Spatially localized, temporally fine

3 Radar image

4

5 Drop size distribution

6 Basic relations Rainfall rate: v(D) terminal velocity for drop size D N(t) number of drops at time t f(D) pdf for drop size distribution Gauge data: g(w) gauge type correction factor w(t) meteorological variables such as wind speed

7 Basic relations, cont. Radar reflectivity: Observed radar reflectivity:

8 Structure of model Data: [G|N(D),  G ] [Z|N(D),  Z ] Processes: [N|  N,  N ] [D|  t,  D ] log GARCH LN Temporal dynamics: [  N(t) |   ] AR(1) Model parameters: [  G,  Z,  N,  ,  D |  H ] Hyperparameters:  H

9 MCMC approach

10 Observed and predicted rain rate

11 Observed and calculated radar reflectivity

12 Wave height prediction

13 Misalignment in time and space

14 The Kalman filter Gauss (1795) least squares Kolmogorov (1941)-Wiener (1942) dynamic prediction Follin (1955) Swerling (1958) Kalman (1960) recursive formulation prediction depends on how far current state is from average Extensions

15 A state-space model Write the forecast anomalies as a weighted average of EOFs (computed from the empirical covariance) plus small-scale noise. The average develops as a vector autoregressive model:

16 EOFs of wind forecasts

17 Kalman filter forecast emulates forecast model

18 The effect of satellite data

19 Model assessment Difference from current forecast of Previous forecast Kalman filter Satellite data assimilated

20 Statistical analysis of computer code output Often the process model is expensive to run (in time, at least), especially if different runs needed for MCMC Need to develop real-time approximation to process model Kalman filter is a dynamic linear model approximation SACCO is an alternative Bayesian approach

21 Basic framework An emulator is a random (Gaussian) process  (x) approximating the process model for input x in R m. Prior mean m(x) = h(x) T  Prior covariance Run the model at n input values to get n output values, so

22 The emulator Integrating out  and  2 we get where q = dim(  ) and where t(x) T = (c(x,x 1 ),…,c(x,x n )) m** is the emulator, and we can also calculate its variance

23 An example y=7+x+cos(2x) q=1, h T (x)=(1 x) n=5

24 Conclusions Model assessment constraints: amount of data data quality ease of producing model runs degree of misalignment Ideally the model should have similar first and second order properties to the data similar peaks and troughs to data (or simulations based on the data)


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