igarss2011_lion.pptx

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MODELING AND APPLICATIONS OF SWOT SATELLITE DATA C. Lion 1 , K.M. Andreadis 2 , R. Fjørtoft 3 , F. Lyard 4 , N. Pourthie 3 , J.-F. Crétaux 1 1 LEGOS/CNES, 2 Ohio State University/JPL 3 CNES, 4 LEGOS/CNRS

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Page 1: igarss2011_lion.pptx

MODELING AND APPLICATIONS OF SWOT SATELLITE DATA

C. Lion1, K.M. Andreadis2, R. Fjørtoft3,F. Lyard4, N. Pourthie3, J.-F. Crétaux1

1LEGOS/CNES, 2Ohio State University/JPL3CNES, 4LEGOS/CNRS

Page 2: igarss2011_lion.pptx

970

km

SWOT mission

• NASA and CNES, launch in 2019• 970km orbit, 78°inclination, 22 days repeat• KaRIN: InSAR Ka band• Wide swath altimeter

• Ocean: “Low resolution” meso-scale and submeso-scalephenomena (10km and greater)

• Hydrology: “High resolution”surface area above (250m)² rivers above 100m

1

Page 3: igarss2011_lion.pptx

Preparing the mission for hydrology

2. SAR amplitude image: Rhone river, France CNES/ Altamira information simulator

1. Radar cross section CNES/ CAP Gemini simulator

Modelisation and simulation for technical use

2

Page 4: igarss2011_lion.pptx

Goals

• Need for a simulator for scientific users (hydrology)– “Fast”: 3 months 3min– Easy to use: no need for heavy preparation of input data– Portable– Relatively realistic errors

• Targets: deltas, rivers, lakes…

• Output: water elevation

3

Simulator output: water heightThe Amazon river, Brazil

Page 5: igarss2011_lion.pptx

Simulator principle

• Based on works of:S. Biancamaria and M. Durand: swath calculation, principleV. Enjolras: residual error calculation

4

Page 6: igarss2011_lion.pptx

Simulator principle

• Based on works of:S. Biancamaria and M. Durand: swath calculation, principleV. Enjolras: residual error calculation

5

Page 7: igarss2011_lion.pptx

Simulator principle

• Based on works of:S. Biancamaria and M. Durand: swath calculation, principleV. Enjolras: residual error calculation

6

Page 8: igarss2011_lion.pptx

Residual height errors

Taken into account• Roll• Baseline variation• Thermal noise• Geometric

decorrelation• BAQ noise• Satellite position

Not taken into account yet• Troposphere• Layover• Shadow• Processing (classification…)• ….

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Page 9: igarss2011_lion.pptx

Residual height errors: Roll

• Roll

8

H

h

B a

ir1r2

R

Page 10: igarss2011_lion.pptx

Residual height errors

• Baseline

9

H

h

B

ir1

r2

R

E_b

Page 11: igarss2011_lion.pptx

Residual height errors

• Coherence loss

= g gSNR + gSQRN + gg

N number of looks

10

H

h

B

ir1r2

R

Page 12: igarss2011_lion.pptx

Simulator principle

• Based on works of:S. Biancamaria and M. Durand: swath calculation, principleV. Enjolras: residual error calculation

11

Page 13: igarss2011_lion.pptx

Simulator principle

• Based on works of:S. Biancamaria and M. Durand: swath calculation, principleV. Enjolras: residual error calculation

12

m

Page 14: igarss2011_lion.pptx

Simulator principle

• Based on works of:S. Biancamaria and M. Durand: swath calculation, principleV. Enjolras: residual error calculation

13

Page 15: igarss2011_lion.pptx

Simulation: Ohio River

Input: Model LisFLOODReference water height (m)

Output: Water height observed by SWOT (m)

3 months modelization courtesy: K. Andreadis

40.5

40

39.5

39

38.5

40.5

40

39.5

39

38.5

Latit

ude

Latit

ude

275 276 277 278 279 275 276 277 278 279Longitude Longitude

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Page 16: igarss2011_lion.pptx

Assimilation methodology• Assimilating SWOT

observations in a identical twin synthetic experiment

• Ohio River study domain (only main stem)

• LISFLOOD hydraulic model• Ensemble Kalman filter• Errors introduced to boundary inflows, channel

width, depth and roughness• Observation errors from a Gaussian distribution

N(0,5cm)

15

courtesy: K. Andreadis

Page 17: igarss2011_lion.pptx

Assimilation results• Water surface elevation along the river channel at two SWOT

overpass times

208 Hours 280 Hours

• Information is not always propagated down/up stream• Small ensemble size could partly be the reason

16

courtesy: K. Andreadis

Page 18: igarss2011_lion.pptx

Conclusions

• Simulation of SWOT data with more representative errors

• The simulator is more user friendly: output format as input format, GUI, can be used with several models

• Can be used for assimilations studies (estimate indirect valuables)

• Need to improve the simulator: layover, decorrelation due to vegetation, troposphere …

17

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Thank for your attention