Microwave - the SMOS Mission

Prof. Bob Suprepared by Monday 29 June 2009, D1L3a

• SMOS - Soil Moisture Ocean Salinity

• MIRAS - Microwave Imaging Radiometer using Aperture Synthesis

• “Passive” microwave 2-D interferometric radiometer (L-Band, 1.4GHz, 21cm).

Part 1 SMOS – MIRAS

SMOS – MIRAS Movie

SMOS – MIRAS: to provide global & regional measurements of soil moisture, ocean salinity and ice

• One of the Earth Explorer’s missions (see also lecture D1L1)

• 1st space borne global measurement of salinity – currently only complex model output is available

• Launch scheduled for April to July 2009

Simulated seasonal (winter) sea-surface salinity map. The units are in practical salinity units (psu)

Simulated seasonal soil moisture map (winter) of Europe and Africa. The units are 'cubic metre of water per cubic metre of soil'

Measurement of Soil Moisture in the Surface Zone

• Soil moisture (SM) is a measure of the amount of water within a given volume of soil and is usually expressed as a percentage.

• Ground measurements• Networks (GEWEX)• SW, SWIR, ….• THIR….• Low frequency microwaves

– Active microwaves• Vegetation, roughness• Revisit• Sensitivity

– Passive microwaves antennaissue

How measured in the surface zone?

SMOS – MIRAS Soil Moisture Measurement Goals

• Multi-angular• Dual polarisation (H and V)• 4 % volume 3 day revisit• (Vegetation 7 day)• Better than 50 km resolution• Global products

• A new technique (2D interferometry) to provide global measurements from space of key variables (SSS and SM) for the first time

TB(40,V) 1st February 87 (K)

TB(40,V) 1

st February 87 (K)

TB(40,H) 1

st February 87 (K)

0 7200

300

TB(40,H) 1st February 87 (K)

TB(40,H) 1

st February 87 (K)

TB(40,H) 1

st February 87 (K)

0 7200

300

Pellarin et al.Le Traon et al.

How will the Measurement Goals be Achieved?

Constraining models by global soil moisture and ocean salinity observations estimated from dual-pol., multi-angular, L-band brightness temperature measurement acquired by a 2D interferometer.

Nadir path

Satellite

Spacecraftvelocity

d N

Swath1000 km

30°

θ = 55°

Local incidenceangle θ

Earth

ηm

Instrument as proposed:

2-D Y-shaped interferometer 4.5m arms

69 LICEF receivers will allow either H &V or full polarisation acquisition

Full polarisation. mode is experimental and utility will be reported as part of Cal/Val experiments

Use of full pol. mode impacts on data downlink volume (x2 compared to dual pol.)

Measuring Soil Moisture at L-band

• Negligible atmospheric attenuation (at L-Band 99% atmospheric transmission)

• Attenuation from vegetation small (for biomass < 5 kg m-2, which is 65% of the Earth’s land surface)

• Emission from the Earth shows a large contrast between water and land (signal-to-noise ratio from dry to wet soils) due to the large difference between the dielectric constant of water (ca 80) and dry soil (ca 3.5)

• Emissivity originates from deeper surface soil layer (at L-band ~5 cm) than for shorter wavelengths

Jackson and Schmugge, 1989

Aperture Interferometry

• Angular resolutionprovided by separatedantennas

• Correlation productss(1)*s(2) → VisibilityFunctions V(D/λ)

• Inverse F.T. on V → TB(θ)

Space sampling requirement : every λ/2 value at least one time ; hence "thinning" possibilities.

1

θ

DD '

Δθ

Δθ ≈ λ / D'

2

At L-band classic radiometers require large steerable antennae, MIRAS offers an alternative design that achieves the appropriate resolution through interferometric processing.

SMOS – MIRAS Hexagonal Foot Print

• From an altitude of 763 km, the antenna will view an area of almost 3000 km in diameter.

• However, due to the interferometryprinciple and the Y-shaped antenna, the field of view is limited to a hexagon-like shape about 1000 km across called the 'alias-free zone'.

• This area corresponds to observations where there is no ambiguity in the phase-difference.

• Due to orbit and foot print configuration the coverage will be global every 3 days

SMOS – MIRAS Payload

Launch: 2009

Mission duration: 3(+2) years

Orbit: sun-synchronous, dawn-dusk, 763km, Inclination 98.4

Mass: 683kg (incl. 28kg hydrazine, Platform 317kg – Payload 366kg)

Power: 900W (525 W max. payload consumption, 78 Ah Li-ion battery

Launcher: Rocket from Plesetsk, Russia

Mission Operation: CNES Proteus Control in Toulouse via S-band link in Kiruna

Data Acquisition & Processing: X-band downlink in Villafrance (User Service Villafranca /ESA-ESRIN)

Launch: 2009

Mission duration: 3(+2) years

Orbit: sun-synchronous, dawn-dusk, 763km, Inclination 98.4

Mass: 683kg (incl. 28kg hydrazine, Platform 317kg – Payload 366kg)

Power: 900W (525 W max. payload consumption, 78 Ah Li-ion battery

Launcher: Rocket from Plesetsk, Russia

Mission Operation: CNES Proteus Control in Toulouse via S-band link in Kiruna

Data Acquisition & Processing: X-band downlink in Villafrance (User Service Villafranca /ESA-ESRIN)

SMOS – MIRAS Interferometry

How Will Soil Moisture be Retrieved?

For vegetated surfacesThe retrieval of SM requires ancillary data to evaluate the effect caused by the vegetation. The vegetation optical depth can be related to the amount of water in vegetation which can be estimated from indices such as NDVI. BUT dual-polarised, multi-angle L-band data give the opportunity to retrieve both soil moisture and vegetation optical depth.

SMOS SM and vegetation characteristics will be produced by an operational SMOS Level 2 retrieval algorithm which is based on an iterative approach, minimizing a cost function computed from the sum of squared weighted differences between measured and modelled brightness temperature (TB) data, for a variety of incidence angles.

For bare soil surfacesSM* = a0 + a1 PR +a2 (TBv-TBh) ; SM* retrieved Surface Soil Moisture PR = (Tbv-TBh)/(TBv+TBh) ; Polarization ratio from MIRAS measurements

Sources of Uncertainty in SM measurement

Instrumental errors- Radiometric sensitivity, accuracy, calibration stability- Characterisation of system elements incomplete- Interferometric image reconstruction

Surface characteristics- Soil surface roughness (causes increase in backscatter)- Soil texture- Land cover & surface heterogeneity- Dew, intercept, snow- Topography- Litter effect- Surface water

Radiofrequency Interference

Pixel heterogeneity

global BT at SM OSantennas

Synthetic antenna directional gaindi

e1 e2 e3 e4 e5 e6 e7 e8 e9

G 2

G 5

type 1 emitter ⇒ CF1

type 2 emitter ⇒ CF2

type 3 emitter ⇒ CF3

antenna footprint

G 7

Due to area of footprint, many types of land use can be expected within a resolution cell, for each surface there will be a different model

Cover Dependent Models Relating Emissivity to SM

Accounting for Uncertainties due to Surface Characteristics

Pixel heterogeneity- SMOS pixels are highly heterogeneous- Processor distinguishes between three main types of pixels: land, sea/water and mixed- Land surfaces are classified into 12 categories, aggregated from the ECOCLIMAP land cover map (dry sand/desert, bare soils, natural low vegetation, cropland, dense forest, moderately dense forests, snow covered area, marshes, swamps, wetlands, rocky terrain, maintains, ice, urban)

ECOCLIMAP Land use map

Auxiliary data for static characteristics- Land/sea mask- Water bodies, rivers - Urban areas - Topography: DEM - Soil texture: FAO data set 5’x5’- Surface roughness

Auxilliary data for dynamic characteristics- Land use map (ECOCLIMAP)- Snow cover extent and status

(MODIS-MERIS, ECMWF)- Freezing (weather centres)- Land surface temperature (AVHRR, MODIS)- Atmospheric characteristics (weather centres)

How Homogeneous? Forest vs. Non Forest LC fractions

In ConclusionSM retrievals can be attempted in many areas with varying expected accuracy

SMOS Validation and Retrieval Team (SVRT) – Soil Moisture

• For SM several sites and dedicated teams worldwide• Supported by ground and airborne campaigns and Announcement of

Opportunity projects in 2005• There will also be SMOS validation for Sea Surface Salinity

SVRT – Airborne System (AMIRAS)

AMIRAS on aircraft in SMOS configuration, 24° from nadir

• Similar configuration but smaller version of MIRAS (three Y-shaped arms)

• Being flown to provide SMOS simulations and in support of CAL/VAL activities

• Like MIRAS, this airborne instrument is able to measure in horizontal as well as vertical polarisations in both dual- and full-polarisation modes.

• Only 4 LICEF like receivers per arm, MIRAS will carry a total of 69 receivers

AMIRAS Brightness temperature in the alias-free field-of-view during its maiden flight over Pensaariisland in the Lohja lake west of Helsinki. The brightness contrast between water and land is as expected.

Credits: UPC (Polytechnic University of Catalonia)

SVRT in China

• Workshop in 2008 in Beijing to bring SSS and SM teams together • In China Dragon 2 project id. 5252 will specifically address SMOS Soil

Moisture CAL/VAL– Area centred on Takla Makan Sand Desert. The specified site is selected

for its homogeneity, stability, relatively easy to access and significant accuracy from previous passive microwave studies.

– Area centred on Northwest of China will look at localisation of algorithms for China

– Lead investigators are Dr. Weiguo Zhang (in photo right) & Prof. Yann Kerr (centre of photo left)

SVRT Ice (Antartica) and Land Surfaces (Europe)

cour

tesy

Y. K

err,

CES

BIO

An L-band radiometer operated near Toulouse, France. Temporal measurements are used to determine the effect of vegetation growth and soil moisture on L-band emissivity.

Long-term observations of snow and ice-sheet surfaces will be used for external calibration of MIRAS as the ice sheets exhibit stable microwave emission at 1.4 GHz.

cour

tesy

PN

RA

Retrievals - Forward Modeling by Iterative Minimisation

Initial SM/OS ValueInitial SM/OS Value

Aux dataAux data

Instrument characteristicsInstrument characteristics

Decision Tree

Decision Tree

Field component

Forward Model

ΔTB

observed

modelled

Submodels/weighting factors

Initial SM/OS ValueInitial SM/OS Value

Aux dataAux data

Instrument characteristicsInstrument characteristics

Decision Tree

Decision Tree

Aux dataAux data

Instrument characteristicsInstrument characteristics

Decision Tree

Decision Tree

Field component

Forward Model

ΔTB

observed

modelled

Submodels/weighting factors

Field component

Forward Model

ΔTB

observed

modelled

Submodels/weighting factors

Neural Network or other (semi)empirical relationship

Output

TBh(0°) TBh(50°) TBv(50°) Land cover Soil-type

Soil Moisture τ Tsoil

SMOS Level-1 Products

Level 1A: SMOS reformatted and calibrated observation and housekeeping data in engineering units; physically consolidated in pole-to-pole time-based segments; “calibrated visibilities”

Level 1B: output of image reconstruction of SMOS observation measurements; consisting of geo-located vectors of Fourier Component of TB on antenna frame

Snapshot-wise information• Satellite position and attitude• TEC magnitude• IGRF magnetic vector• Sun illumination angle• Direct Sun corrected magnitude Snapshot Overall Radiometric Accuracy

Geo-located information• grid point information: latitude, longitude, altitude• Number of measured values in grid point• For each value:Flags (Polarization, Sun, position in the Field of View), BT value, radiometric accuracy, Incidence and Azimuth Angle, Snapshot ID, Footprint size

Level 1C: Brightness temperatures Swath; Magnitudes are expressed at Top of Atmosphere; Information is geo-located on a Discrete Global Grid (ISEA 4-9); L1c semi-orbit product (pole to pole) split by Land and Sea grid point Two sets of information available: pixel-wise and snapshot-wise

L1C Sea product dual polarization snapshot: Brightness temperature @ H-pol (ESA-ESRIN 2007)

Sea Surface Salinity (SSS) computed at each ISEA grid point for a semi orbit (ascending or descending)

Three SSS values (3 models, with uncertainties)Pseudo-dielectric constant retrievedWind Speed and Sea Surface Temperature used in the retrievalPolarized Tb at 42.5º incidence angle at surface and antenna frameFlags and confidence and science descriptors

Soil Moisture (SM) computed at each ISEA grid point for a semi orbit (ascending or descending):

SM values, optical thickness, physical temperature, Polarized TB (surface and antenna frame at 42.5º) , and dielectric constantsAll quantities have related uncertaintiesFlags to indicate presence/absence of features/events of interest such as rocks, topography, snow, RFIDescriptors to describe properties such as number of wild views and mean spatial resolution

SMOS L2 SM retrieved over North Africa (Cabot et al 2007)

SMOS Level-2 Products

Levels 3 & 4 Daily and Averaged Global SM &

SSS Maps

• Level 3– global, single instrument

• Level 4– global root zone SM,

multi-instrument retrieval with US missions 2010 on

– will be developed and available through French and Spanish national programmes

Simulated Seasonal Maps Winter at top

Soil MoistureSimulated Sea Surface Salinity

SMOS Ground Segment Acquisition and Products Distribution From Europe

CNES – ToulouseSatellite Operations

ESAC – VillafrancaData Processing Ground Segment &X-Band Acquisition Station

ESRIN – FrascatiUser Services/ Quality control/Facilities, Mission management

ESTEC – NoordwijkPost Launch Support Office

KirunaLong-term ArchiveReprocessing CentreS-Band Acquisition

SvalbardNRT Acquisition Station

+ Science users

+ Expert Support Laboratories

+ NRT users

SMOS Data Access

• SMOS data will be made available through the ESA category-1 procedure, either through dedicated AOs or registration service online (http://eopi.esa.int).

• SMOS calibration & validation data will be available via the SMOS Cal/Val portal: http://calvalportal.ceos.org/CalValPortal/welcome.do

• Near-real time products will be available either from the WMO-GTS network or the ESAC FTP server

• Soil Moisture in situ data will be made available via the SMOS Soil Moisture Network Data Hosting under development at the University of Lisbon

• ESA campaign data will be available via the campaign database http://earth.esa.int/campaigns and via the SMOS CalVal portal