using satellite observations to assess high resolution ocean...
TRANSCRIPT
1 JHRCP WS 13-15 April 2016
HRCP workshop 2016
Hans Bonekamp
EUMETSAT
Using satellite observations to assess high resolution ocean models
2 JHRCP WS 13-15 April 2016
Should I have reversed the title of this talk?
<=
Using high resolution ocean
models to assess satellite
observations
=>
Using satellite observations to
assess high resolution ocean
models
I did not !
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Session 2: Development of coherent designs and
collaborations for experiments
• Coordination at high level
CGMS (<= atmosphere) CEOS (<= Ocean)
( In-situ: GOOS, EUROGOOS, other regional alliances)
• Coherency in time
Sustainability (Essential Climate Variables, Essential Ocean
Variables)
CEOS Virtual constellations and associated science teams
• “Higher resolution models need higher resolution observations “
will give some important examples with individual missins
• Collaborations for experiments
GODAE ocean view
In addition
• EUMET in service and user requirements
Sentinel-3 and Jason-3 services Marine Data stream
user requirements
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Space
-based
baseli
ne
GOS
2015
2020
Increasing importance for Ocean
Uncertain
FY-3E in early morning orbitz
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WMO / CGMS <-> CEOS
CGMS Ocean Considerations
• Several coordination areas are well catered for outside CGMS, in particular by CEOS Virtual Constellations
• Encourage the CEOS Virtual Constellations to submit papers to CGMS on relevant operational matters with appropriate recommendations to CGMS
• Strengthen the link to JCOMM, in particular the Cross Cutting Task team on Satellite Data Requirements.
• Ocean is considered explicitly in climate activities and handled by the CEOS-CGMS Joint Working Group, and the increased capabilities of the next generation GEO satellites for ocean applications will also be addressed in this context.
CGMS-42 meeting, 19-23 May 2014, Guangzhou
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www.CEOS.org
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What can you expect from a CEOS VC?
• Provision of a coordination mechanism to harmonize systems, payloads, data
processing and calibration/validation infrastructures;
• Serving as a programmatic PoC for the global geophysical variable measurement system as a whole, addressing issues which go beyond the individual mission programmes, such as orbit optimisation;
• Establishing and maintaining an international consensus on the structure of the (minimum) constellation that fulfils user needs;
• Supporting and engaging the active user community, structured through the International Science Teams (GHRSST, OSTST, IOCS, IOVWST) assuming that these sciences teams also address the key applications areas.
Generally, VC work is done on “Best Effort” basis.
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GOVST-V Beijing 2014
CEOS Ocean Virtual Constellations
Sea Surface Height:
• CEOS Ocean Surface Topography Virtual Constellation (OST-VC)
• Ocean Surface Topography Science Team (OSTST)
Sea Surface Temperature:
• CEOS SST Virtual Constellation (SST-VC)
• Group for High Resolution SST (GHRSST)
Ocean Surface Vector Winds:
• CEOS Ocean Surface Vector Winds Virtual Constellation (OSVW-VC)
• International Ocean Vector Winds Science Team (IOVWST)
Ocean Colour:
• CEOS Ocean Colour Radiometry Virtual Constellation (OCR-VC)
• International Ocean Colour Coordination Group (IOCCG), IOCS meetings
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Altimetry over the years
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15 16 17 18 19 20 21 22 23 24 25 26 27
CRYOSAT-2 EU
Complementary Nadir Missions
Broad-Coverage Mission
HY-2B CN
HY-2A CN
14 13
Reference Nadir Missions (Non Sun-Synchronous) Jason-2 FR/EU/USA
Launch Date
02/13
Operating Proposed Development
Sentinel-3C EU
Sentinel-3B EU
SWOT USA/FR
Jason-CS-A/Sentine-6-A EU/USA
Feb 2016
Missions Now-Future
Saral/AltiKa FR/Ind
20/08
JCS-B EU/USA
04/10
08/11
HY-2D CN
HY-2C CN
Jason-3 FR/EU/USA
Sentinel-3A EU
Sentinel-3D EU
Compira jp
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04 05 06 07 08 09 10 11
12 13 14 15 16
CRYOSAT-2 EU
Complementary Nadir Missions
HY-2A CN
03 02
Reference Nadir Missions (Non Sun-Synchronous)
Jason-2 FR/EU/USA
Launch Date
Operating Past Feb 2016
Missions Past-Now
Saral/AltiKa FR/Ind
Jason-1 FR/EU/USA
TOPEX/POSEIDON FR/USA 08/92
ENVISAT EU
ERS-2 EU 04/95
GEOSAT FO USA 02/98
J3 FR/EU/USA
S3A eu
Today’s Alongtrack altimetry technology
Conventional
Low
Resolution
Mode (LRM)
Signal & noise
averaged over
5-7 km radius
footprint
Synthetic
Aperture
Radar (SAR)
Mode –
delayed
doppler
300 m
alongtrack, 5-7
km crosstrack
radius
CR2-SAR
Sentinel-3 (2016)
J-CS (2020)
T/P – Jason
Envisat
SARAL
3
SWOT (Surface Water Ocean Topography) Mission
Mission Architecture
Nadir interf. channels
Main Interf. Left swath
Main Interf. Right swath
87
3 k
m
10-60 km 10-60 km
• Ka-band SAR interferometric (KaRIn) system with 2 swaths, 60 km wide
• Produces heights and co-registered all-weather SAR imagery
• Intrinsic resolution 2 m x 10-70 m grid
• Onboard processor gives 250 m2 grid over oceans
• Interferometry will reduce noise by 1 order of magnitude : 2.4 cm2/cycle/km2
• Use conventional Jason-class altimeter for nadir coverage, radiometer for wet-tropospheric delay, and GPS/Doris/Laser ranging for orbit determination.
• Partnered mission NASA, CNES & CSA & UKSA • Mission life of 3.5 years • 890 km Orbit, 78º Inclination, 21 day repeat • Launch: 2020 9
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• EKE calculated from mapped satellite altimetry
• – benchmark for validating HR ocean models
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GOVST-V Beijing 2014
Sentinel-6: Continuity of Service for Topography (1)
Global Sea Level Trends Over Past 21+ Years (1992 to 2013)
Promise of an unprecedented 40 years long systematic measurement Great boon for Climate, Sea Level Rise Monitoring
Prime mission objective: Continue high-precision global sea level time series with an error on sea level trend < 1 mm/year
Continuity with past altimeters in the reference series (all operated in LRM)
90 91 92 93 94 95 96 97 98 99 00 01 02 03 04 05 06 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 >
TOPEX/POSEIDON France/USA
Jason-1 France/USA
Jason-2 Europe/USA
Jason-3 Europe/USA
Jason-CS A Europe/USA
Jason-CS B Europe/USA
Past Operating Approved Proposed
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Interleaved Mode (INTM): LRM + SARM
Slide: 16
Figure 6: Sketch of the Interleaves Mode pulse timing over 12
ms. Red (green) stripes represent generated (received) pulses
(Courtesy NOAA).
LRM
SARM
SARM+LRM
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In orbit Approved Planned/Pending approval
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
GOES-R (ABI) US
Meteosat-9 (SEVIRI) EU
FY-4 0/A,B,C (China)
Sea Surface Temperature (Geostationary)
GOES-13 (Imager) US-West GOES-14(Imager) US-west
GOES-15 (Imager) US-East
GOES-S (ABI) US
MTSAT-1R (Japan) MTSAT-2 (Japan)
FY-2E FY-2F (China)
MTG-I1 EU MTG-I2 EU
Elektro-L N3 (Russia)
Elektro-L N1 (Russia)
COMS (Korea) COMS 2A/B (Korea)
MTG-S1 EU
Kaplana (India)
Meteosat-11 (SEVIRI) EU Meteosat-10 (SEVIRI) EU
Himawari-8 (Japan) Himawari-9 (Japan)
Elektro-L N2 (Russia)
INSAT-3A (India) INSAT-3D R/S (India)
INSAT-3D (India)
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Dual view capability
In orbit Approved Planned/Pending approval
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
ERS-2 ATSR-2
Sentinel-3A SLSTR Sentinel-3B SLSTR
POES AVHRR/3 (pm orbit)
AQUA & TERRA (MODIS)
FY-3A
METOP-A
S-NPP (VIIRS) JPSS-1 (VIIRS)
JPSS-2 (VIIRS)
Passive Microwave, Polar & non sun-synchronous Orbiting TRMM
GCOM-W1 (AMSR-2)
FY-3B,C,D (VIRR)
GCOM-W3 (AMSR-2)
FY-3B,C,D (VIRR)
GCOM-W2 (AMSR-2)
Sentinel-3C/D SLSTR
METEOR-M3
Optical (TIR) Polar Orbiting
Sea Surface Temperature (Polar orbiting)
OCEANSAT-3 (TIR) Aquarius SAC/D (NIRST)
ENVISAT AATSR
WindSat
AMSRE
METOP-B (AVHRR/3, IASI) (am orbit)
HY-2B,C,D HY-2A
METOP-C
METEOR-M2 MSU-MR METEOR-M1 MSU-MR
GPM-Core GMI
GCOM-C SGLI
Metop-SG A (METimage, IASI-NG)
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Key SST –VC issues
• Redundant capability of passive microwave
radiometers with 6GHz channel is needed (e.g.
continuation of GCOM-W)
• improved drifting buoys. towards high resolution
and higher accuracy SST drifter sensors
(HRSST-2) for satellite SST validation.
• Capacity building : SST dedicated capacity
building in consideration
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Surface Winds constellation status
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SCA specifications
• Scatterometer specifications: ASCAT
versus SCA
SCA
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Observation Principle
• DopSCAT transmits a dual chirp, that is a combination of an up-chirp, and a down-chirp.
• This waveform allows estimating not only the σº but also the Doppler shift of the ocean.
• The ambiguity functions of LFM pulses with opposite chirp rates are skewed in opposite direction, meaning that the introduced delay has an opposite sign.
22
)(rect 2
12exp
2
12exp
)()()(
22 ttτ
BtfπjAt
τ
BtfπjA
tststs
τcc
du
B
τfτ Ds
Ambiguity function up-chirp Ambiguity function down-chirp
Detected IRFs
Cross- correlation
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GNSS-Reflectometry: basics
• Signals of opportunity from Global Navigation Satellite Systems e.g GPS, Galileo…
• Global, ubiquitous signals Huge improvement in
space-time sampling
L-band (unaffected by rain) • Small low-cost receivers
Can be accommodated on small satellites or satellites of opportunity to build a constellation of GNSS-R receivers
Measurements of ocean height and ocean surface roughness
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Scatterometer constellation status
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Addition of RapidSCAT to the constellation – first opportunity to look into
the diurnal cycle, helping to refine the optimum constellation requirement: at
least three missions in sun-synchronous orbit (WMO driven), plus one in non
sun-synchronous orbit to resolve the diurnal cycle to improve inter-calibration
ScatSAT launch and validation expected early 2016 - work on facilitating
data access operationally already ongoing
Updated our CEOS web page
Progress on updating the IDN for ASCAT data sets
IOVWST working groups followed up and with VC participation:
On data formats and standards
On climate data sets – main focus being the integration of Ku- and C-
band winds
On high winds characterisation and validation - workshop coming up in
December 2015
Status and main topics since last VC day
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OCR-VC: Mission Overview
SIT Tech. Workshop 2015
EUMETSAT, Darmstadt, Germany
17th-18th September
27
• OCR-VC agencies are fully in support of the GEO Blue Planet Components
• "agency mapping" exercise. Mission planned. Consideration of available, and
planned, international agency assets and resources for OCR cal/val.
• Steps towards implementation of the International Network for Sensor Inter-
comparison and Uncertainty assessment for Ocean Colour Radiometry (INSITU-OCR)
o Vicarious calibration
NOAA continues to fund and sustain MOBY
NASA VCAL Instrument competitive tender
ESA/EUMETSAT studies
o In-situ data base. the format for submissions of in situ data to the agencies. For
example, it would be beneficial to have an interagency standard template.
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Copernicus Spce
component
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GOVST: Coupled Prediction Task Team
connected/supported by the other TTs
Intercomparison & Validation TT (IV-TT)
Observing System Evaluation TT (OSEval-TT)
Marine Ecosystem Analysis & Prediction TT (IV-TT)
Coupled Prediction TT (IV-TT)
Coastal Ocean & Shelf Sea TT (IV-TT)
Sample key issue: How to use Altimetry Data ?
Data Assimilation TT (DA-TT)
Sentinel3 Geographical Coverage
Image: ESA
Sentinel-3 Ground Track
Image: ESA
high inclination orbit (98.65°):
optimal coverage in high latitudes
Sentinel SRAL ground track patterns
Image: Landsat (Google Earth)
S3A = 104 km S3A + S3B = 52 km
Sentinel-3 Marine Core Products Distribution Product EUMETCa
st ODA Data Centre Timeliness Dissemination Unit size Size per orbit
(GB) (likely compressed sizes)
OLCI L1 EFR NRT Frame (3 min) 21.5
NTC idem idem
OLCI L1 ERR
NRT Full Orbit Daylight (2666 sec)
1.4
NTC idem idem
OLCI L2 WFR NRT, NTC Frame 14.2
OLCI L2 WRR NRT Full Orbit Daylight 0.95
NTC idem idem
SLSTR L1B NRT, NTC Frame (3 min) 29.0
SLSTR L2 WST
NRT Frame (3 min) 0.75
NTC Full orbit: South Pole to South Pole
Idem
SRAL L1B NRT, STC* Full orbit: dump 0.4
NTC *Half Orbit: Pole to Pole idem
SRAL L2 WAT NRT, STC* Full orbit: dump 0.2
NTC *Half Orbit: Pole to Pole idem
http://www.esa.int/Our_Activities/Observing_the_Earth/Copernicus/Sentinel-3
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3. Data Centre: Estimated Data Volume increase
0
20,000
40,000
60,000
80,000
100,000
120,000
Vo
lum
e i
n T
era
byte
Data Centre growth (prognosis) related to missions
EPS-SG
MTG-RPR
MTG
S3-RPR
S3
Jason
Metop
MSG
MTP Now:
1,500 TB
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Conmclusions and recommendations
• Next decade enhanced capabilities to support HR modelling
• For oceanography, the satellite observing community (under CEOS) becomes more user-driven and coordinated. Engage yourself also as a application science community;
user requirements should have an upward trace to the applications AND science. request detailed information and capability building Support and/or link with Godae Oceanview Support and/or link with Int Science teams