cfosat wind and wave observations from space: a french … · 2009. 6. 5. · α=cotθ−4tgθ− 1...

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CFOSAT Wind and wave observations from space: A French-Chinese mission Scientific Pis: Danièle Hauser (France): CNRS/Univ. Versailles Liu Jianqiang (China): NSOA and the Mission and Technical Team Globwave Workshop, Brest, September 2007

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Page 1: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

CFOSAT

Wind and wave observations from space:

A French-Chinese mission

Scientific Pis:

Danièle Hauser (France): CNRS/Univ. Versailles

Liu Jianqiang (China): NSOA

and the Mission and Technical Team

Globwave Workshop, Brest, September 2007

Page 2: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

The Chinese French Oceanographic Satelllite CFOSAT

Two payloads

- Directional wave spectrum form SWIM (France)

- Wind scatterometer SCAT (China)

- Dedicated to ocean wind and waves obervation

- SWIM: ≈similar to the former SWIMSAT proposal to ESA in 2002

Page 3: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Outline• Mission objectives

• Overall mission description

• Wave measurements

- Scientific requirements- Scientific requirements

- Proposed instrument (SWIM)

- Principle of measurements

- Preparation studies

• CFOSAT in the context of GLOBWAVE

Page 4: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

CFOSAT Objectives

1) Monitor at the global scale the wind and waves at the ocean

surface

⇒Improve wind and wave prediction and sea-state monitoring

=> improve knowledge and modeling of sea-surface processes

• sea-state evolution

• role of waves in the atmosphere and ocean,

• sea-ice properties and evolution in marginal ice zones,• sea-ice properties and evolution in marginal ice zones,

• coastal processes

• determination of ocean surface parameters by remote

sensing.

2) Opportunity for additional estimates of land surface

parameters (in particular soil moisture and soil roughness)

3) Opportunity for studying polar ice sheet characteristics

Page 5: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Overall mission characteristics

-Recently agreed between China and France

-Launch planned in 2012-2013

-Platform and launcher under Chinese responsibility

-Ground segment shared between China and France

-SWIM designed and built by France

-SCAT designed and built by China

-Polar orbit (inclination ≈ 97°)

-Altitude 500 km approximately

-Near Real time transmission of data (within 3 hours)

Page 6: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

-Ku-Band

-Almost global coverage in one day

Two alternatives under study

Scatterometer on CFOSAT (Chinese part):

- Quickscat type (2 rotating pencil beams, with

incidence around 50°)

- intermediate between Quickscat and ERS (or

Ascat): rotating fan-beam with incidence from

about 20 to about 55°.

Page 7: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

•Measurement of directional wave spectrum at global scale with a

70x70 km spatial resolution

• Revisit better than 10 to 13 days (TBC) for latitudes > 35°

• Wavelengths to be measured : � ~ [70 - 500] m

• Variation of backscattering coefficient from 0 to 10° incidence

SWIM Scientific requirements

with absolute accuracy < 1dB

• Sea surface parameters to be derived :

- Significant Wave Height

- Wind speed

- Radial wave spectrum every 15° in azimuth

- Directional wave spectrum over scales of about 70 x 70 km

- Mean square slope of short waves and tentatively other

parameters of the slope pdf

Page 8: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Instrument SWIM

Ku-Band radar(13.6 GHz)

–1 nadir beam (altimeter-type)

–5 off-nadir beams (2 to 10°), rotating over 360°, real-aperture

Altitude : 500 km

Incidences : 0-2-4-6-8-10°°°°3dB beamwidth: 2°°°°x2°°°°

Sequential in time

3dB beamwidth: 2°°°°x2°°°°

88km

17.7 x17.7km²

6 tr.min-1

Nadir :

-Hs

-Normalized Radar Cross-Section σ0

Off-nadir :

- Each 15° in azimuth, wave slope

spectrum from the modulation spectrum of

σ0

- σ0 for each incidence θ. σ0(θ) => pdf of

surface slopes

Expected products

Page 9: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Principle for estimating wave spectra => similar to

STORM/RESSAC

Φ

θ

X(elevation)x

y

zZ

Y (azimuth)

m(X,Φ)

βθ

• In each azimuth direction, the normalized

radar cross-section σ0 is modulated by the tilt of

the long waves

=> Measurement of these modulations m(x,φ),

calculation of their spectrum Pm(k,φ)σ

Waves with

wave-number k

X(elevation)

Look direction

σ0

R

(θ)

Swath covering 2° incidence range

Page 10: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Pm(k,φ) =2π

Lyα2k2F(k,φ )

• Linear relationship between modulation spectrum

Pm(k,φ) and wave slope spectrum k2F(k,φ)

Ly: azimuth footprint dimension

• Complete directional information using the 360° scans

α = cotθ − 4tgθ −1

cos2θ

∂ ln p

∂(tanθ),

where p is the slope pdf

Page 11: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

H= 500 km, Rotation= 6 rpm, incidences 6, 8, 10°

100

Surface patterns for incidence beam 6, 8 10°

track distance

Scale at which directional spectra will be retrieved

70 x 70 km by combining 3 incidences

90 x 90 km for 10° incidence

-100

-80

-60

-40

-20

0

20

40

60

80

-200 -100 0 100 200 300 400 500 600

Along-track distance (km)

Tour 2, 6°

Tour 3, 6°

Tour 4, 6°

Tour 5, 6°"

Tour 1, 6°

Tour 1, 8°

Tour 2, 8°

Tour 3, 8°

tour 4, 8°

Tour 5, 8°

tour 1, 10°

Tour 2, 10°

tour 3, 10°

Tour 4, 10°

Tour 5, 10°

Along-track distance

Across-track distance

Zone

1

Zone

2

Page 12: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

0,02

0,025

0,03

0,035

backscatter modulation radial spectrum in the direction of wave propagation (averaged over 15°)

Swell case, Hs=2mU=13 m/s

Spectral density of backscatter modulation

Direct simulation, without_noise

, λ, λ, λ, λpeak≈200m

0,02

0,025

0,03

0,035

backscatter modulation radial spectrum in the direction of wave propagation (averaged over 15°)

Swell case, Hs=2mU=13 m/s

Spectral density of backscatter modulation

Direct simulation, without_noise

Inversion, after correction from speckle and thermal noise

0,02

0,025

0,03

0,035

Spectral density of backscatter modulation

Direct simulation, without_noise

Inversion, after correction from speckle and thermal noise

Preparation studies (1): simulations of observations and inversions

Objectives : - extraction of directional wave

spectrum

- instrument performance &

optimization

Example of simulated wave field (4x4 km ; res 1m)

wind waves + swell

Simulator developed through a CNES/CETP

cooperation

-0,005

0

0,005

0,01

0,015

0,02

0 0,05 0,1 0,15 0,2

Spectral density of backscatter modulation

Wave number (rad/m)

-0,005

0

0,005

0,01

0,015

0,02

0 0,05 0,1 0,15 0,2

Spectral density of backscatter modulation

Wave number (rad/m)

-0,005

0

0,005

0,01

0,015

0,02

0 0,05 0,1 0,15 0,2

Spectral density of backscatter modulation

Wave number (rad/m)

Speckle level

Page 13: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Other illustration: 2D plot mixed sea case with swell Hs=4m, )peak=200 m,wind sea with U = 3 m/s, 90°°°° angle between swell and wind seapropagation

Direct simulation

of the 2D modulation spectrum

2D modulation spectrum

after inversion

Page 14: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Preparation studies (2): development of

assimilation schemes, study of assimilation impact

Two kind of studies (Meteo-France, CETP, BOOST, SHOM,

IFREMER):

- simulation of SWIM-like data (observations simulated

with perturbed analyzed fields)

- assimilation of data from the ENVISAT SAR wave

modemode

Spectral data: assimilation of main parameters (significant

wave height, mean direction, mean frequency) of partitions of

the 2D spectrum

Model: WAM, cycle 4, global (1 x 1 °), 25 frequencies (0.04-0.41 Hz), 24/36 directions, 6 hourly analyzed ECMWF wind-

fields

Assimilation scheme: Optimal Interpolation

Page 15: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Description of the assimilation scheme

• Decomposition in partitions of the wave spectrum

(first guess and observation)

frequency [Hz]

0.19779

0.29668

0.39557

30

60300

330

0

15

20

Partition 2

frequency [Hz]

direction [degrees]

0.098894

210

240

90270

120

150

180

5

10

15

Partition 3Partition 1

Each partition is describedby Its mean parameters

Page 16: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

SWIMSAT synthetic caseSee also Aouf et al, JAOTech, 2006

-Simulation of a reference case (forecast without assimilation for a

period of 8 days )

-Simulation of synthetic “noisy” SWIM observations along the

orbit, including noise

-First guess perturbed wave field

-Assimilation for a period of 4 days, every 3 hours, then forecast

without assimilation

-Comparison between runs with and without assimilation

Page 17: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Main results of the simulations

1 day after

beginning of

assimilation

1 day of forecast after

end of assimilation

Difference in Hs between runs with and without assimilation of

SWIMSAT synthetic data

2 days after end of

assimilation

Page 18: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

1 day after

beginning of

assimilation

1 day of forecast after

end of assimilation

Difference in mean wave period between runs with and without

assimilation of SWIMSAT synthetic data

2 days after end of

assimilation

Page 19: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Comparison to assimilation of Hs only (case of an altimeter)

Difference of Hs , 2 days after end of assimilation, between runs

with and without assimilation of:

Spectral data

(SWIMSAT case)Non spectral data

(altimeter case)

Page 20: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Summary on efficiency of assimilation

- On H10 (waves with periods longer than 10 s): 6% 1 day after assimilation) ,

larger than on Hs and larger for spectral data (SWIM) than for non spectral

data

- On mean wave frequency and mean direction: larger for spectral data (about

- Use of the assimilation index: quantifies the reduction due to assimilation,

of rms error between model and observations

Spectral data (SWIMSAT case) brings more information in

the assimilation than standard altimeter data (Hs), efficiency

of assimilation larger than for SAR data (less cutoff effect)

- On mean wave frequency and mean direction: larger for spectral data (about

9% and 4%, respectively) than for non-spectral (5% and 2% respectively)

- Efficiency decreases significantly when the cutoff is larger than 150 m (case

of a SAR)

Page 21: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Impact of the assimilation of upgraded ASAR wave

spectra (cut-off de 244 m) in forecast mode

Mean wave periodWave height H10 (for

waves with period > 10 s)

28 November 2005 at 18:00 (UTC)

1-day forecast

Page 22: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Impact of the assimilation of upgraded ASAR wave

spectra (cut-off de 244 m) in the forecast mode

Wave height H10 (for

waves with period > 10 s)Mean wave period

November 29 2005, 18:00 (UTC)

2-day forecast

Page 23: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Using Jason-1 and GFO altimeter data as independent

verification data set at crossovers points

JASON-1 GFO

Sep-Oct-Nov-Dec 2005

���� Significant reduction of RMS error (AI) by 10.2 % and 7.6%

1

44

10

49

0

20

40

60

BIAS RMS

ASAR-SAR-NEW NOASSI

0

45

11

49

0

2040

60

BIAS RMS

ASAR-SAR-NEW NOASSI

Nb crossovers: 4421 Nb crossovers: 7806

in centimeters

in centimeters

Page 24: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Effect of combined assimilation (ASAR+RA2)

in the forecast period

Comparison of Significant wave heights at Jason-1 orbit tracks

After two months of

assimilation

(Jan et Féb 2004)

forecast period of8

10

12

14

Assim

ilation index for SWH(%

)

comparison with Jason-1 in forecast period

ASAR-200-RA2RA2onlyASAR-240-RA2

forecast period of

three days

� The spectral information induces a longer impact in the

period of forecast

-18 -12 -6 0 6 12 24 36 48 600

2

4

6

8

Time in forecast (hours)

Assim

ilation index for SWH(%

)

Page 25: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Concluding remarks on assimilation studies

� SWIM simulation : positive impact for H10, mean

period, direction; larger impact than in case of non-

spectral assimilation (Hs from altimeter)

�WAM with ASAR : positive impact for significant wave

height as shown by comparison with independent wave

data (Jason-1, GFO and NDBC buoys)

�Need for long term studies combining assimilation of

ASAR wave spectra and altimeter Ra-2 in WAM model

data (Jason-1, GFO and NDBC buoys)

�Need for better knowledge of correlation functions of

spectral parameters

�Need for independent data for validation, scores,…

Page 26: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

-CFOSAT will provide ocean winds and spectral characteristics

of surface waves (starting 2012-2013)

- coverage for wind should be global almost daily

- coverage for waves will be global over 10 to 13 days (to be

confirmed)

⇒CFOSAT must be used as one element of a « virtual »

CFOSAT in the context of a “Globwave system”

⇒CFOSAT must be used as one element of a « virtual »

constellation, with complementary characteristics :

•other altimeter missions (Sentinelle 3, Jason3,

SARAL/AltiKa,…)

• SAR missions (Sentinelle 1) with wave mode or image

mode over the ocean, Radarsat2, …

• Scat missions (METOP/ASCAT, Chinese HY2B??,

other missions of Quickscat type??)

Page 27: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

CFOSAT in the context of a “Globwave system”, (2)

-Real-time aspects will be under space agencies responsibility

-In addition: need for easy data access for science and

applications (not real-time)

-Need for in situ observations (wind, spectral characteristics of

waves) for validation of retrieval algorithms, assimilation

scores,..

-Need for models as observation integrating systems

(assimilation), as tool for open ocean forecast, as boundary

conditions and tool for coastal processes forecast and

analysis.

Page 28: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Personal recommandation

Wind and waves from various sources (satellites, buoy,

ships,..) in the same data base or via same interface

For remote sensing: radar cross-sections also archived

Ancillary useful data: rain, current, SST,…

Need for more in situ observations of spectral properties

of waves.

Even wit the present 1D buoy network : access to

the 1D spectrum rather than to the parameters of a

the spectra would be useful

Need for more 2D spectra

Page 29: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

First option (pencil-beam, Quickscat type)

Page 30: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Second option: rotating fan-beam

Overlap between adjacent scans

for large number of azimuth view

for each pixel

Nadir Point

footprint

Sub-satellite track

Resolution pixel

Resolution pixel

Page 31: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Radio-Frequency part

Frequency 13.575 GHz

Peak RF power (TWTA) 120-150 Watt

Waveform Chirp (frequency modulated)

Bandwidth 200 to 320 MHz depending on incidence

Pulse duration 50 µs

PRF 2 to 6.5 kHz, depending on incidence

Antenna part

Incidence 0, 2, 4, 6, 8, and 101

Polarisation HH (TBC)

3 dB beamwidth 21 x 21

Rotation 6 rotations/minute (TBC)

Design 80 cm diameter passive offset parabole with six

Tentative design of the antenna part

Offset antenna (80 cm)

for the 5 offset beams +

small antenna (40 cm)

for nadir beam

Tentative specifications (to be confirmed)

Design

80 cm diameter passive offset parabole with six rotating feeding horns

On-board Processing Unit

Range Compression Deramp technique (TBC)

Range resolution after compression 0.47 to 0.75 m depending on incidence

Time integration 17 to 48 ms (depending on incidence

with correction of the advection using tracking-loop)

Real time processing

- nadir beam: distance, radar cross-section and significant wave height - off-nadir beams: backscatter power versus distance, time integration accounting for migration due to satellite displacement

Data transmission

Data rate/data Link 8 Mbits, X-Band

Page 32: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

α = cotθ −4tgθ −1

cos2θ

∂lnp

∂(tanθ)

∂lnp

∂(tanθ)relatedto

1

σ0

∂σ0

∂ tanθ,

α is wind dependent

Pm(k,φ) =2π

Lyα2k2F(k,φ )

σ0(θ) for different wind speeds

(from Chapron- and TRMM data)

Page 33: CFOSAT Wind and wave observations from space: A French … · 2009. 6. 5. · α=cotθ−4tgθ− 1 cos2θ ∂lnp. ∂(tanθ) , wherepistheslopepdf. H= 500 km, Rotation= 6 rpm, incidences

Observation locations for 4 days assimilation of SWIMSAT synthetic

Coverage for 4 days of assimilation (preliminary specification)