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SAR Interferometry opportunities with the European Space Agency ERS-1, ERS-2, Envisat, Sentinel-1A /-1B ESA 3 rd Party Missions (ALOS) Prepared by ESA teams and ESA supporting companies Special thanks to S. Schmuck, A. Vollrath, N. Miranda and ARESYS
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  • SAR Interferometry opportunitieswith the European Space Agency

    ERS-1, ERS-2, Envisat, Sentinel-1A /-1B

    ESA 3rd Party Missions (ALOS)

    Prepared by ESA teams and ESA supporting companies

    Special thanks to S. Schmuck, A. Vollrath, N. Miranda and ARESYS

  • For the last 20 years, ESA has been constantly supporting the SAR

    Interferometry (InSAR) communities with:

    the provision of relevant InSAR data, through:

    the development and operations of SAR satellites (ERS-1, ERS-2, Envisat)

    a precise satellite orbital maintenance including InSAR tandem campaigns (ERS-1/ERS-2 tandem, ERS-2/Envisat tandem, Envisat 2010+)

    the development of a large and consistent InSAR data archive

    a constant effort in facilitating access to SAR data

    the development of InSAR science and InSAR applications,

    bringing together the InSAR communities through the Fringe workshop.

    ESA and SAR Interferometry

  • 20 years of ERS-1/2 SAR data in the archive

    The most complete and consistent

    SAR archive

    ERS-1 and ERS-2 missions

  • 20 years of ERS-1/2 SAR data in the archive

    ERS-1 and ERS-2 missions

    InSAR measurement of surface displacement of the Parkfield section of the San Andreas Fault over the decade before the last Mw 6.0 Parkfield earthquake (28 September 2004).

    from M. de Michele et al., 'Spatiotemporal evolution of surface creep in the Parkfield region of the San Andreas Fault (1993–2004) from SAR', June 2011, Earth and Planetary Science Letters

    Based on a set of 51 ERS1-2 images combined to calculate 341 differential interferograms with a perpendicular baseline of less than 250 meters.

    Parkfield section of San Andreas FaultCalifornia (USA)

  • 2007 2008 2009 2010 2011 2012 2013 2014

    ERS-21995

    2006

    ERS-11991

    ERS

    SA

    RTa

    ndem

    1991

    2000

    30 m < baseline < 100 m

    100 m < baseline < 200 mERS SAR Tandem data allowed identifying the acceleration of Greenland glaciers flow (Rignot, 2006)

    ERS SAR 1-day tandem:

    a unique dataset !

    ERS-1 / ERS-2 SAR 1-day tandem

  • ERS-2 reached 16 years of operations ERS-2 was designed for 3 years nominal lifetime ! no gyroscopes since 2001: gyro-less operations

    gyro-less data was Doppler screened removing the attitude uncertainty

    the SAR instrument worked satisfactorily until its last day of operations on 4 July 2011

    ERS-2 mission

    ERS-2 : a veteran just retired

    The decision to terminate the ERS-2 satellite operations is motivated by: no more synergy with Envisat (i.e. different orbits), end of operations budget, need to de-orbit the satellite (space debris mitigation)

    Rome, 4 July 2011

  • DOSTAG meeting 2nd February 2011

    Space debris is becoming a major issue in the altitude range 700-900 km

    Two collisions of space objects have contributed to increase the overall collision risk:

    Space Debris evolution (1)

    Iridium / Cosmos 2251 collision in Feb.

    2009

    Chinese anti-missile test in Jan. 2007

  • 0

    10

    20

    30

    40

    50

    60

    2002 2003 2004 2005 2006 2007 2008 2009 2010

    DOSTAG meeting 2nd February 2011

    Space Debris evolution (2)

    ==> old satellites shall be moved out the crowded orbit before losing them (when technically feasible) !

    ==> hence the de-orbitation of ERS-2 after 16 years of operations (ERS-2 altitude has been lowered from 800 km to 570 km, allowing the satellite to re-enter and burn in the atmosphere well within the required maximum of 25 years)

    Yearly number of Envisat collision warnings

    Envisat collision avoidance manoeuvres

    2 1

    2

    4

    Example of increased risk of collisions with Envisat

  • The most complete and consistent

    SAR archive

    ERS-2 Ice Phase

    Fringe’09 recommendation: consider moving ERS-2 to a 3-day repeat orbit for tracking grounding lines – a unique opportunity to assess advance and retreat of ice sheets.

    Done

    Before its “retirement”, ERS-2 was moved on a 3-days repeat cycle orbit

    [March to June 2011]

    Same orbital parameters as for ERS-1 Ice Phase in 1992 and 1994

    Targets: Antarctica, Greenland, glaciers and some tectonic areas

    Archive: more than 5200 segments

  • Kangerdlugssuaq Ice Stream (East Greenland)

    ERS-2 Ice-Phase• 3-day repeat cycle (March - June 2011)• animation over 1.5. months using 13 scenes between 11 March and 1st May

    Calving front advances ~1.8km

    Ice Stream Tracking with SAR

    ERS-2 Ice Phase

  • 2007 2008 2009 2010 2011 2012 2013

    ERS-21995

    2002

    ERS-11991

    1991 2000

    Extension

    2002

    Envisat 1stTa

    ndem

    2nd

    Tand

    em

    Three ERS-2 / Envisat SAR tandem campaigns, exploiting the synergy between the 2 missions (30 min. time interval on the same orbit) until Envisat orbital change at end 2010.

    Ice phase

    Extension

    ERS-2 / Envisat SAR Tandem 2 Feb. 2008, Bperp : 2210 m

    Mohave (USA)

    ERS-2 / Envisat SAR 30-min. tandemFringe’09 recommendation: More ERS-Envisat cross-InSAR campaigns needed, repeats observations would minimise topographic effects. Done

    3rd

    Tand

    em

    South / Northhemisphere

  • 60 to 81 deg South Latitude, descending arc (only within O’Higgins station mask)

    Archive: 129 interferometric pairs

    Antarctic Tandem Campaign

    ERS-2 / Envisat SAR 30-min. tandem

    14 Feb 2010 to 26 April 2010

  • ERS-2 / Envisat SAR 30-min. tandem

    06 July 2010 to 22 Oct 2010

    Last Tandem Campaign

    North hemisphere

  • Envisat has reached 9.5 years of operations:

    Envisat was designed for 5 years nominal lifetime

    Satellite:

    good overall status will platform and payload ASAR instrument works satisfactorily

    Ground segment:

    about 270 min. of ASAR (high rate) data acquired every day, equivalent to 270 ScanSAR products or 1080 stripmap products per day

    Envisat mission

  • A large archive dedicated to InSAR

    ASAR archive: Image Mode, Swath 2, VV (i.e. ERS-like)

    Envisat data archive

  • Envisat data archiveE. Sansosti et al., Geophysical Research Letters, 2010, “Space-borne radar interferometry techniques for the generation of deformation time series: An advanced tool for Earth's surface displacement analysis"

    Envisat archi

    ve compatible

    with ERS arc

    hive

  • A large archive dedicated to InSAR

    Image Mode, Swath 2, HH Image Mode, Swath 6, VV

    Wide Swath Mode, HHWide Swath Mode, VV

    Envisat data archive

  • ASAR Wide Swath Mode data used together with Image Mode data to analyse the Lazufre volcanic system (Central Andes)

    Jan Anderssohn et al. (GFZ), in Remote Sensing of Environment , Volume 113, Issue 10, October 2009

    Envisat data archive

  • 73 ASAR Image Mode IS6 , HH ascending segments

    Greenland Campaign [08 Dec 2009 to 30 Jan 2010]

    Envisat data archive

  • 2007 2008 2009 2010 2011 2012 2013 2014

    ERS-21995

    2002

    Envisat

    2006

    ERS-11991

    1991

    2000Funding to

    be confirmed

    Envisat mission extension

    • Altitude change: -17.4 km • Repeat cycle: 30 days / 431 orbits• Orbit control: only altitude, inclination drift• Mean Local Solar Time variation: +/- 10 min.

    The Envisat operations extension requested a modification of the orbital parameters in 2010.

    The new orbital parameters allow: 1. to extend the mission well beyond 2010, for about 3.5 years2. to operate all Envisat instruments with no degradation of their measurements, and

    minor impact on data quality, excepted for InSAR

  • Envisat Nominal Phase35 days cycle, nominal control

    Envisat Extension Phase 30 days cycle, inclination drift

    799.8 Km

    782.4 Km

    Altitude

    22:00

    22:07

    Mean Local Solar Time

    Orbit inclination

    21:50

    mid 2

    014

    22 Oc

    t 201

    0

    May 2

    012

    -17.4 Km

    26 Oc

    t 201

    0

    no inclination control

    altitude control

    inclination control

    altitude control

    Envisat mission extensionhow does it work ?

    Cycle nCycle n+1

    Equator

    Cycle nCycle n+1

  • Cycle nCycle n+1

    Lat. 38 N

    Since November 2010, Envisat orbit inclination is not maintained, i.e. there are no more out-of-plane manoeuvres (high saving of hydrazine) the orbit inclination is drifting slowly no impact on Envisat data quality, except for ASAR data:

    orbit baselines become loo large for allowing SAR Interferometry (InSAR) applications, except where the orbits cross (for the same track)

    Trick for limiting the impact on InSAR applications:“Naturally” orbits of the same track would cross at Equator, however Equator is not the most interesting geographical area for InSAR applications.

    The crossing node was moved to 38 deg. latitude, allowing covering the most interesting geographical areas for tectonics (and volcanology)• crossing at latitude 38 deg. North on descending pass

    • crossing at latitude 38 deg. South on ascending pass

    Envisat new orbit and SAR Interferometry

  • 6 November/ 6 December 2010Bperp 120m

    Envisat new orbit and SAR Interferometry

    F. Guglielmino & G. Puglisi, INGV

    E. Fielding, NASA/JPL

    San FranciscoEtna

  • Baselines suitable only between 2

    consecutive cycles

    Baselines suitable only between 2

    consecutive cycles

    38 deg NDescending pass

    38 deg SAscending pass

    South Italy

    Greece Turkey

    San Francisco

    North Iran

    Baselines suitable only between 2

    consecutive cycles

    +/- 4 deg.for beam 6 desc. pass

    Baselines suitable for differential interferometry from 2011 to 2013

    +/- 4 deg.for beam 6 asc. pass

    Baselines suitable for differential interferometry from 2011 to 2013

    A new ASAR background data acquisition scheme was put in place with the new Envisat orbit, including coverage of tectonic/volcanic areas around 38 deg. latitude for InSAR.

    Envisat new orbit and SAR Interferometry

    As a consequence, there was an excellent and recent archive of ASAR data over Japan at time of the major earthquake of 11 March 2011.

  • Co-seismic (30 days) displacement

    Courtesy JPL/Caltech

    Colour cycle = 50 cm

    Thanks to the background data acquisitions (pre- seismic acquisitions in February 2011), it was possible to generate a mosaic derived from many Envisat ASAR interferograms (combining with post-seismic acquisitions in March 2011).

    The mosaic provides a detailed estimation of the terrain movement on a very large scale.Courtesy

    INGV

    Displacement map

    (line of sight)

    Japan earthquake (March 2011)

  • Importance of providing scientists with easy access not only to EO datasets but also to in-situ datasets:

    GeoHazard Supersites initiative

    NorthGround motion in three directions derived from integration of Envisat data with GPS data. Both types of data are available through GeoHazard Supersites.Courtesy INGV (S. Stramondo et al.) See GeoHazard Supersites for more details.

    Japan earthquake (March 2011)

  • Envisat new orbit and SAR Interferometry

    Fringe’09 recommendation: The post-2010 Envisat acquisition mode should be IS6 to increase the geographical extent of the zone where InSAR can be done.

    Done

    Fringe’09 recommendation: ESA should redefine a background mission to ensure systematic acquisitions over sensitive regions (Tibet, California, Mediterranean, South America etc…). This will allow incremental time series construction and coverage in the case of a major seismic event.

    Done

  • Since Oct. 2010, Envisat orbit inclination is no more maintained:

    InSAR baselines gradually increase with respect to their initial values, except around 38 deg. latitude

    some opportunities of better baseline values between consecutive acquisitions during (boreal) spring

    Envisat new orbit and SAR Interferometry

    1-cycle-step (30-days) normal baseline evolution since Nov. 2010

    Nor

    mal

    bas

    elin

    e (m

    ) Latitude

    38 deg.Equator

    80 deg.

    80

    38

    0

    60

    20

  • 2 4 6 8 10 12 14-8

    -6

    -4

    -2

    0

    2

    4

    6

    8

    cycles

    Bas

    elin

    e ev

    olut

    ion

    vers

    us ti

    me

    [km

    ]

    0° N desc20° N desc38° N desc60° N desc80° N desc

    Envisat new orbit and SAR Interferometry

    Since Oct. 2010, Envisat orbit inclination is no more maintained:

    InSAR baselines gradually increase with respect to their initial values, except around 38 deg. latitude

    some opportunities of better baseline values between consecutive acquisitions during (boreal) spring cumulative normal baseline

    evolution since Nov. 2010

    Bold: Actual values

    Predicted values

  • 2007 2008 2009 2010 2011 2012 2013 2014

    ERS-21995

    2002

    Envisat

    2006

    ERS-11991

    1991

    2000

    ESA 3rd party mission: ALOS

    ALOS (ESA 3rd party mission)

    ALOS mission has ceased its operations due to a satellite malfunction in early 2011 ESA operated the ALOS Data European Node (ADEN) ESA intends to continue providing the archived ALOS data

    1stTa

    ndem

    2nd

    Tand

    emER

    S S

    AR

    Tand

    em

    3rd

    Tand

    em

  • Ice Flow of the Antarctic Ice SheetE. Rignot et al., Science, September 2011

    => A result of the coordination between SAR satellite operators (CSA, ESA, JAXA)

    during the International Polar Year 2007-2008

    The coordination with other agencies

  • 2007 2008 2009 2010 2011 2012 2013 2014

    ERS-21995

    2002

    Envisat

    2006

    ERS-11991

    1991

    2000

    GMES and Sentinel-1 mission

    ALOS (ESA 3rd party mission)1s

    tTa

    ndem

    2nd

    Tand

    emER

    S S

    AR

    Tand

    em

    3rd

    Tand

    em

    Sentinel-1B

    + national SAR missions (Radarsat, TerraSAR-X, COSMO, …)

    GMES Space Component – led by ESA :• Sentinel missions: developed specifically for GMES• Contributing missions: EO missions built for

    purposes other than GMES but offering part of their capacity to GMES (EU/ESA Member States, EUMETSAT, commercial, international)

    GMES Space Component – led by ESA :• Sentinel missions: developed specifically for GMES• Contributing missions: EO missions built for

    purposes other than GMES but offering part of their capacity to GMES (EU/ESA Member States, EUMETSAT, commercial, international)

    Sentinel-1A

  • 07 08 09 10 11 12 13 14 15 16 171995

    2002

    The future ESA missions

    Extension

    GOCE

    Extension

    Extension

    SMOS

    CryoSat

    Note: data management (e.g. access, reprocessing) shall be ensured beyond mission active lifetime

    ADM-Aeolus

    1998

    ERS-2

    Envisat

    Sentinel-1A, -1BSentinel-2A, -2BSentinel-3A, -3B

    Sentinel-5P

    EarthCARE

    SWARM

    More information on ESA Earth Observation:

    http://www.esa.int/esaEO

    Funding requested to ESA Ministerial

    Council 2012

  • ERS and Envisat New ESA data policy [approved in 2010]:• Open and Free datasets (for all data available on Internet)• Some restrictions in case of technical constraints (e.g. SAR instrument tasking, large SAR data production)

    Data Policy of individual data providers

    Third Party Missions & Contributing Missions (to GMES)

    Earth Explorers

    Sentinel missions

    Earth Observation data policy

    Full and open access to all users [Joint Principles for a Sentinel Data Policy, approved by ESA]

    Fringe’09 recommendation: ESA should extend the Sentinel data policy to the existing ERS and ENVISAT archive.

    Done

  • A constant objective: ease access to Earth Observation data

    Common objective for all missions data handled by ESA:Envisat, ERS, Earth Explorers, and Third Party Missions

    New ESA EO data policy

    Development of alternative ways to provide data (e.g. processing on demand, toolboxes)

    Maintain effort in improving quality of products (algorithms, validation)

    Maintain effort in supporting data exploitation by scientists and by value adding industry

    Facilitating access to Earth Observation data

    see following presentation on GeoHazard Supersites (W. Lengert)

  • Industrial Sectors• Mining• Oil & Gas• Civil Engineering• Utility operators• Transport• Insurance • CO2 Capture &

    Storage (emerging)

    Supporting value adding industry Precision Land Motion Services

    • Unique, Specialist Service Providers

    • Growing commercial Business,

    • European leadership in services

    Long-Term ESA support (15+ years) from R&D to commercial exploitation

  • As for the last 20 years, ESA is committed to continue its support to the InSAR user communities:

    maintaining the effort in facilitating access to SAR data,

    strengthening the exploitation of its large InSAR archive,

    developing and operating the Sentinel-1 mission (2 satellites),

    seeking reinforced partnerships with other SAR operators.

    Conclusions

    Slide Number 1Slide Number 2Slide Number 3Slide Number 4Slide Number 5Slide Number 6Slide Number 7Slide Number 8Slide Number 9Slide Number 10Slide Number 11Slide Number 12Slide Number 13Slide Number 14Slide Number 15Slide Number 16Slide Number 17Slide Number 18Slide Number 19Slide Number 20Slide Number 21Slide Number 22Slide Number 23Slide Number 24Slide Number 25Slide Number 26Slide Number 271-cycle-step (30-days) normal baseline evolution since Nov. 2010Slide Number 29Slide Number 30Slide Number 31Slide Number 32Slide Number 33Slide Number 34Slide Number 35Slide Number 36Slide Number 37


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