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EPS/IJPS

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Title: EPS/IJPS


1
THE EUMETSAT POLAR SYSTEM (EPS) Presented by
Ken ASHWORTH EUMETSAT Representative
to NOAA EUMETSAT
(Ken.Ashworth_at_noaa.gov)
2
Presentation Outline
  • The EPS Programme within IJPS
  • EPS Services, System Architecture
  • Metop Payload, EPS Mission and Products
  • Programmatic Status

3
The EPS Programme within IJPS
4
A Major Cooperation Between Europe and the USA
  • IN THE MARGINS OF THE G7, EUROPE AGREED IN
    PRINCIPLE TO SHARE THE BURDEN OF THE
    METEOROLOGICAL POLAR SERVICE WITH THE USA
  • INITIAL JOINT POLAR SYSTEM (IJPS) TO BE
    IMPLEMENTED
  • In the context of the USA Convergence
  • Under a NOAA-EUMETSAT cooperation agreement
    signed in November 1998
  • Through integration coordination of the NOAA
    POES and the EUMETSAT EPS (EUMETSAT POLAR SYSTEM)
    Programmes
  • SCOPE OF COOPERATION
  • Afternoon early morning orbits covered by the
    USA (POES DMSP Satellites)
  • Morning orbit covered by Europe (Metop
    Satellites)
  • Exchange of instruments and data, coordinated
    development and operations

5
Initial Joint Polar System (IJPS)
Metop launches in 2005 and 2010 (9 Years of
Operation)
0930 LST Metop-1,2 - AVHRR/3 (US) - IASI
(CNES/EUM) - HIRS/4 (US) - AMSU-A (US) - MHS
(EUM) - ASCAT (ESA/EUM) - GOME-2 (ESA/EUM) - DCS
(CNES) - GRAS (ESA/ EUM) - SR (CNES/Canada) -
SEM (US)
0530 LST 0830 LST USAF - DMSP - OLS - SSM/I -
SSM/T - SSM/T-2
1330 LST NOAA-N,N' - AVHRR/3 (US) - HIRS/4
(US) - AMSU-A (US) - MHS (EUM) - DCS (CNES/US) -
SR (CNES/Canada) - SBUV (US) - SEM(US)
USAF (NOAA)
NOAA
EUMETSAT
6
EUMETSAT SATELLITE PROGRAMMES
13
15
16
17
14
96
97
98
99
00
01
02
03
04
05
06
07
08
09
10
11
12
METEOSAT
NominaI operation estimated lifetime
Over Indian Ocean since 7/98
Non nominal operation
  • Meteosat-5

IODC at 63E
Estimated fuel margin
Hot stand by at 10 W (since 6/98)
  • Meteosat-6

Approved
Available for launch
  • Meteosat-7

Planned
Operational S/C at 0(since 6/98)
Cal/val phase
MSG
  • MSG-1
  • MSG-2
  • MSG-3
  • MSG-4

EPS
  • Metop-1
  • Metop-2
  • Metop-3

JASON-2
7
The EPS Programme Within IJPS
  • The EUMETSAT Polar System (EPS) is the European
    contribution to the Initial Joint Polar System
    (IJPS) established with NOAA
  • The IJPS will provide global meteorological and
    climate data from a series of European and
    American sun-synchronous polar orbiting
    satellites, comprising NOAA NNand Metop 1 2.
  • EUMETSAT has established Co-operation Agreements
    with
  • ESA, for the development and procurement of the
    three Metop satellites
  • NOAA, for the exchange of instruments, data and
    operation cross-support
  • CNES, for the provision of IASI and ARGOS-DCS
    payloads

8
The EPS Programme Within IJPS
3 MetOp Satellites MetOp-1, 2, 3
Launcher
Ground Segment
14 years of operation
EPS Programme Elements
9
The EPS Program within the IJPS
IJPS
EPS
NOAA
system
system
WMO
EPS
NOAA
Community

Users
Users
through GTS/RMDCN
10
The EPS Programme Within IJPS
NOAA N N p.m.
METOP 1 2 a.m.
SAF
SAF
EUMETSAT POLAR SYSTEM
11
The EPS Programme Within IJPS
EPS CDA Station (Svalbard) Coverage for Metop.
Fairbanks/Wallops Stations coverage is also
indicated
12
EPS Services, System Architecture
13
EPS Services, System Architecture
The EPS Missions
Support to the space environment monitoring on
behalf of NOAA Part of the IJPS program in
partnership with NOAA
14
EPS HRPT and LRPT Services
Direct read-out services
Data source is the
satellite for the user
HRPT and LRPT
point of view.
Possible means of
controlling access
Encryption.
Data set limited to
the observation of
the instantaneous
sub satellite
observation.
15
EPS Services, System Architecture
EPS Offers the following operational services /
Data access
16
EPS Services, System Architecture
Data Distribution - Timeliness
Global Data Dump
LEGEND
NRT Data Circulation
GTS/RMDCN dissemination
117mn
U-MARF Data Access
Max. Data Age (up to Level 1)
117mn
Realtime
SAF (via NRT)
135 mn
135 mn
Other NRT User
GTS/RMDCN
7 hours
U-MARF Users
17
height 6.3 m transverse section 3.4 m x 3.4
m (launch configuration) solar panel 11.3
m power 2210 W (end of life, orbit
average) lifetime 5 years 13
instruments launch mass 4200 kg data flow
3500 kbps
The Metop Satellite
18
EPS Services, System Architecture
Metop Satellites
  • Customer Single Space Segment Team at ESTEC
  • EUMETSAT and ESA placed a contract with Astrium.
  • Metop Prime Contractor
  • ASCATGRAS development
  • Satellite Simulator
  • The Metop satellites design is based on the
    heritage of the SPOT-5 and ENVISAT programmes
  • Status of Metop Space segment
  • PDR held in June 1999
  • CDR held in September 2001
  • EUMETSAT and ESA placed a contract (Signed in
    March 2000) with Officine Galileo for the
    development of 3 GOME-2 instruments
  • IASI CDR held April 2002

19
Metop Payload, EPS Missions Products
20
Metop Payload, EPS Missions Products
  • MetOp-1, 2, 3 satellites embark the following
    sensor payload (except HIRS not planned to be
    flown on MetOp-3)
  • Infrared / Visible Imagery Advanced Very
    High Resolution Radiometer (AVHRR/3) 6 channel
    visible / infrared cross-track scanning
    radiometer.
  • Advanced Infrared Sounding Infrared
    Atmospheric Sounding Interferometer (IASI)
    Michelson interferometer covering 3.4 to 15 ?m
    range with
  • 0.25 cm-1 spectral resolution and integrated
    infrared imager.
  • Infrared Sounding High resolution
    Infra-Red Sounder (HIRS/4)
  • 20 channel visible / infrared cross-track
    sounder.

21
Metop Payload, EPS Missions Products
  • Microwave Sounding Advanced Microwave
    Sounding Unit - A (AMSU-A) Microwave Humidity
    Sounder (MHS) 20 channel microwave radiometer
    suite (cross-track scanning).
  • Ozone Profiling Global Ozone Monitoring
    Experiment - 2 (GOME-2) Ultraviolet /
    visible, nadir-viewing grating spectrometer.
  • Wind Scatterometry Advanced
    Scatterometer (ASCAT)
  • C-band, dual swath scatterometer with three
    independent views.
  • GPS Sounding GNSS Receiver for
    Atmospheric Sounding (GRAS)
  • 12 channel GPS receiver for navigation and
    occulation sounding.

22
Metop Payload, EPS Missions Products
The Metop meteorological Payload - Accomodation
AVHRR-3
GOME-2
GRAS
HIRS-4
IASI
ASCAT
AMSU-A1
AMSU-A2
MHS
23
EPS Product Services
  • PRODUCT SERVICES AVAILABLE FROM CORE GROUND
    SEGMENT
  • NETWORK OF SATELLITE APPLICATION
    FACILITIES
  • CGS BASELINE PRODUCTS INCLUDE
  • All level 1 Products from all NOAA Metop
    sensors
  • Selected Level 2 Products Temperature/Moisture
    Profiles, Cloud Products...
  • VARIETY OF SERVICES/LEVEL 2 PRODUCTS FROM 7
    SAFs
  • Ocean Sea Ice
  • Support to nowcasting VSRF (SW Packages)
  • Ozone Monitoring
  • GRAS Meteorology
  • Climate Monitoring
  • Land Surface Analysis
  • Numerical Weather Prediction (NWP)

24
Metop Payload, EPS Missions Products
The Metop System generates the following products
(all in near realtime, Global coverage) Level 0
products SEM, Level 1b products AVHRR,
AMSU, HIRS, IASI, MHS, ASCAT, GOME, GRAS Level 2
Products ATOVS, IASI, ASCAT, GOME,
GRAS Note Level 1b products are
radiometrically corrected, calibrated in physical
units and geolocation information
appended All Level 0, Level 1 and IASI/ATOVS
Level 2 products are generated within the Core
Ground Segment located at the EUMETSAT
headquarters Level 2 products for ASCAT,
GOME,GRAS are generated by decentralised
Satellite Application Facilities (SAF) Further
processing to Level 3 is entirely performed at
SAFs
25
EPS Data Circulation
  • Global data read-out through high latitude
    station
  • Exchange of global data with NOAA
  • Direct data read-out services HRPT and LRPT
  • High Resolution Picture Transmission
  • Low Resolution Picture Transmission
  • Digital version of NOAA APT
  • Level of commonality with MSG HRIT/LRIT
  • Coordinated with CGMS
  • Near Real Time delivery of CGS products (level 1
    and elected level 2) to Primary NRT Terminals
    within Member States
  • Near Real Time delivery of level 2 products
    through GTS/RMDCN

26
EPS Data Distribution and User Community
HRPT/LRPT
Key
Users
End Users
EPS System
to Space Segment Users
EPS Space Segment
to CGS NRT Users - Internal to OGS
EPS Overall Ground Segment (OGS)
to Primary NRT User Entities external to OGS
(level 1/2 products)
EPS Core
to EPS NRT End User (level 2 products, via
GTS/RMDCN)
IASI-TEC
CAL/VAL
Ground Segment
CGS
to off line OGS Users
Primary NRT User Entity
GTS
UMARF
SAFs
Gateway
GTS/RMDCN
ARGOS DATA
Network
WMO
EPS Offline
EPS NRT
National Met.
ARGOS Users
CLS-ARGOS
Community
Users
End Users
Services
EPS Users
27
Metop Payload, EPS Missions Products
EPS provides global soundings at high spectral
resolution with IASI
28
Metop Payload, EPS Missions Products
EPS provides global AVHRR imagery at full
resolution Multispectral image (Channels
2,3,4)
29
EPS Global AVHRR data is received processed
with 1 km sampling (nadir)
30
Metop Payload, EPS Missions Products
EPS provides operational services with
instruments in the heritage of European Earth
Observation missions
  • Global Ozone Monitoring Experiment (GOME-2)
  • Advanced Scatterometer (ASCAT)

Exemple of Ozone Products from the GOME mission
31
Example of ERS Wind Vector Field (500 Km Swath)
Metop Payload, EPS Missions Products
Source ESA
32
Example Wind prototype product from
ERS-2http//www.knmi.nl/onderzk/applied/scattmtr/
prescat/eng/
Metop Payload, EPS Missions Products
33
Metop Payload, EPS Missions Products
EPS provides additional sounding capabilities
(for the first time in an operational environment)
GNSS Radiooccultaion Atmospheric Sounder (GRAS)
Path of the ray perigee through the atmosphere
34
Metop Payload, EPS Missions Products
Climate monitoring capabilities
Mean Surface Temperature in K for April ,1987
Chédin et al., 1996
El Nino, 1986-1987, Surface Temperature Anomaly
for April 1987 compared to April 1988. Chédin
et al. 1996
Mean Surface Temperature in K for April ,1988
Chédin et al., 1996
35
Metop Payload, EPS Missions Products
EPS allows sea surface monitoring at global scale
36
Metop Payload, EPS Missions Products
GOME/ERS-2 15-16-17 July 1998 NO2 total column
concentration over USA. High concentration over
areas with dense population (East coast)
GOME/ERS-2 15-16-17 July 1998 NO2 total column
concentration over Europe. High concentration
over areas with dense population (Po valley, The
Netherland and England)
Source DLR
37
Metop Payload, EPS Missions Products
  • Conclusions EPS provides (1)
  • Continuity to the current system
  • High level sounding performances provide
    enhanced data streams needed to further improve
    the capabilities of advanced NWP systems
  • Multi-instrument capabilities assure service
    beyond operational meteorology, e.g. climate
    research and monitoring)
  • Instruments built on the heritage of Earth
    observation missions (GOME, ASCAT). These are
    introduced into an operational environment
  • Long mission duration (14 years). This will
    assure that users are provided with long-term
    near real-time and off-line data service for
    meteorological and climate applications

38
Programmatic Status
39
Programmatic Status
  • Basic Dates
  • EUMETSAT EPS Programme approval in 1998
  • ESA Metop-1 Programme approval in 1999
  • Metop industrial activities Signature of the
    Phase C/D Contract in 12/1999
  • Core Ground Segment Contract signature with
    Alcatel in 12/2000
  • Launch Service EUMETSAT signed the contract
    for the launch of the Metop satellites by Soyuz
    launchers from Baikonour with Starsem (a joint
    European Russian company) in 12/2000
  • Nominal MetOp-1 launch date is between July
    2005 (without margin) and
  • December 2005 (5 months margin included).

40
Programmatic Status
  • Current Status of Metop activities
  • PFM PLM integration at Astrium ED essentially
    completed
  • Final system testing started in September,
    including TV testing planned in November
  • In parallel integration (and test) of the FM2 PLM
    avionics successfully completed.
  • PFM SVM integrated and initial system reference
    testing has commenced
  • SVM will undergo TV and EMC testing at Intespace
    prior to satellite integration (with PLM) in
    March 03

41
Programmatic Status
Metop Satellite Integration Test
42
Programmatic Status
  • Ground Segment Status
  • The Core Ground Segment (CGS) CDR held from late
    May to early July 2002
  • Core Ground Segment Factory Acceptance Testing
    started for the Polar Station Facility (PSF),
    Front End Processor (FEP), Product Generation
    Facility (PGF), Flight Dynamics Facility (FDF)
    and the Dissemination Facility (DIF).
  • Polar Site Infrastructure Service in Svalbard
    successfully completed its Verification Review in
    May 2002
  • Transportation, assembly and erection of both EPS
    antennas and radomes was completed by early
    August, within the available weather window.
  • The RF, baseband and monitoring and control
    equipment shipped in autumn 2002
  • On-site Acceptance of the PSF planned for early
    2003.
  • Unified Archive Facility Detailed Design Review
    for the EPS extension took place in October 2002

43
Final stages of mechanical assembly of the CDA-1
antenna and radome (Svalbard).
Programmatic Status
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