Fabrizio Battazza, ASI – Osservazione della Terra GMES ... · ASI – Osservazione della Terra....

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Rome – 27.06.2012 GMES: III Workshop di FP7 1 Earth Observation ASI EO Missions Fabrizio Battazza, ASI – Osservazione della Terra GMES: III WS di FP7 Rome, 27.06.12

Transcript of Fabrizio Battazza, ASI – Osservazione della Terra GMES ... · ASI – Osservazione della Terra....

Rome – 27.06.2012 GMES: III Workshop di FP7 1

Earth Observation

ASI EO Missions

Fabrizio Battazza,ASI – Osservazione della TerraGMES: III WS di FP7Rome, 27.06.12

Rome – 27.06.2012 GMES: III Workshop di FP7 2

Earth Observation

ASI EO ASI EO MissionsMissions

MICROWAVESMICROWAVES VISIBLEVISIBLEINFRAREDINFRARED

SAR MISSIONSSAR MISSIONS

MULTIFREQUENCY APPROACH MULTIFREQUENCY APPROACH

ASI CENTRE FOR SPACE GEODESY

OPTICAL MISSIONSOPTICAL MISSIONS

HYPERSPECTRAL MISSION

HYPERSPECTRAL MISSION

Rome – 27.06.2012 GMES: III Workshop di FP7 3

Earth Observation

ASI Current Missions

- COSMO-SkyMed- ROSA (on board on OCEANSAT-2,

Aquarius/SAC-D, Megha-Tropiques)

ASI EO ASI EO MissionsMissions

ASI Future Missions

- PRISMA (2014)- COSMO-SkyMed Second Generation (2015)

ASI Contributions to ESA Missions

Rome – 27.06.2012 GMES: III Workshop di FP7 4

Earth Observation

• Orbit and lifetime:– LEO SSO, 620km, 6.00 LTAN– 5+2 years lifetime

• System elements:– 4 Satellites

• Platform• X-band SAR• PDHT

– Ground Segment• Mission & Control Center: Fucino• I-CUGS: Matera

– Launch Segment• BOEING Delta II

COSMOCOSMO--SkyMed SkyMed ConstellationConstellation

COSMO-SkyMedCOSMO-SkyMed

THE LARGEST ITALIAN INVESTMENT

IN SPACE SYSTEM FOR EO

4 X-BAND SAR SATELLITES

COSMO-1

COSMO-2

67.5°

COSMO-3

COSMO-4

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Earth Observation

MULTI-MODE ACQUISITION CAPABILITY

PINGPONG15x15 m Res.

(30 km X 30 km)

HIMAGE3x3 – 5x5 m Res.(40 km X 40 km)

HUGEREGION100X100 m Res.

(200 km X 200 km)

WIDEREGION30X30 m Res.

(100 km X 100 km)

SPOTLIGHT1 m Res.

(10 km X 10 km)

450 IMAGES/DAY

EACH SAR SATELLITE CAN ACQUIRE UP TO

560 PRODUCTS/DAYARCHIVING

200 PRODUCTS/DAYPROCESSING

COSMOCOSMO--SkyMed: SkyMed: MainMain E2E PerformanceE2E Performance

REVISIT TIME4 Satellites

MAX < 12h (worst case)

REVISIT TIME4 Satellites

MAX < 12h (worst case)

18 h18 h

36 h36 h

72 h72 h

4 SATELLITES (worst case)4 SATELLITES (worst case)

VERY URGENT

VERY URGENT

CRISISCRISIS

ROUTINEROUTINE

RESPONSE TIMERESPONSE TIME

Rome – 27.06.2012 GMES: III Workshop di FP7 6

Earth ObservationThe instrument uses the Radio Occultation technique to retrieve the vertical profile of

atmospheric temperature, pressure and humidity

from the ground up to 100 km as well as the profiles of the electron content in the ionosphere.

The first ROSA instrument is performing the operational phase on

board of OCEANSAT-2, the Indian mission for the oceanography and meteorology study launched in September 2009, in June 2011

a second instrument was launched with the Aquarius/SAC-D

a NASA-CONAE mission and in October 2011

the third one on CNES-ISRO Megha-Tropiques

mission.

The ROSA instrument is able to measure the atmospheric vertical profiles with high resolution (~200 m in the troposphere and ~1000 m in the stratosphere) and high thermal accuracy

(<1K).

ROSA (Radio ROSA (Radio OccultationOccultation for for SoundingSounding the Atmosphere)the Atmosphere)

OCEANSAT-2 [Courtesy of ISRO]

Aquarius/SAC-D [Courtesy of NASA/CONAE]Megha-Tropiques [Courtesy of CNES-ISRO]

Rome – 27.06.2012 GMES: III Workshop di FP7 7

Earth Observation

• Mission Objectives:– Pre-operational and technology

demonstrator nature– Focus on

• Space qualification of Hyperspectral (HYP) and panchromatic (PAN) payloads

• Development and production of PAN/HYP products/ applications

• Program Highlights:– National program – Fully funded by ASI– B2/C/D/E1 contract running– Launch schedule: 2014

Applications:Vegetation monitoringGeological mappingAgricultural diagnostics, agricultural indicatorsLand cover maps and crop inventories Urban and functional areas mapping and monitoringCoastal and inland productivity assessment of aquatic ecosystemsMonitoring of carbon sources and sinks on land (Kyoto Protocol)Land surface hydrology and water management, Risk Management Support (fires, landslides, volcanic and seismic hazard).Atmosphere characterization

PRISMA = PRecursore IperSpettrale della Missione Applicativa

PRISMA PRISMA MissionMission

Rome – 27.06.2012 GMES: III Workshop di FP7 8

Earth Observation

Hyperspectral• Swath:

– 30 km

• Spatial GSD:– <30 m

• Spectral ranges (contiguous spectrum):

– VNIR: 400-1010 nm– SWIR: 920-2500 nm

• Spectral resolution: – 10 nm

Panchromatic• Swath:

– 30 km• Spatial GSD:

– <5 m• Spectral ranges: 400-700 nm

PRISMA: PRISMA: characteristicscharacteristics

Orbit and lifetime:– LEO SSO, 620km, 10.30 LTDN– 5 years lifetime

Coverage:– World-wide

The Satellite– Mass: ≈700kg– Power: ≈1000 W (generated)

Rome – 27.06.2012 GMES: III Workshop di FP7 9

Earth Observation

COSMOCOSMO--SkyMed SkyMed SecondSecond GenerationGeneration

• COSMO 2nd Gen. system is conceived as the follow-on to COSMO-SkyMed first generation (COSMO 1st Gen.) with main goals of assuring performance improvement and operational continuity.

Improved operational profiles• CSK = 450 products/day/satellite• CSG = 1000 ca. products/day/satellite

(equivalent to. CSK products)

Main improvements in terms of :• SAR Antenna• PDHT (higher data volume)

Rome – 27.06.2012 GMES: III Workshop di FP7 10

Earth Observation

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Earth Observation

4 OPERATIONAL SATELLITES

2011 …2007

COSMO‐SkyMed 2nd GENERATION

2015Launch

of

COSMO‐SkyMed 1

>2023COSMO‐SkyMed 4

operative

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Earth Observation

ConclusionsConclusions

ASI is developing COSMO-SkyMed SG and PRISMA

To provide the user with a new dataset to be potentially exploited in the GMES framework