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4 Final Report - Emits - ESA

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4 <strong>Final</strong><br />

<strong>Report</strong><br />

• one or several deployable Payload Data Reception and Processing facilities.<br />

The Figure below depicts the Ground Segment Architecture. It also identifies the main internal and<br />

external interfaces. The external interfaces comprise the interfaces to the users and additional data<br />

sources, which provide auxiliary data for processing and meteorological forecast data supporting the<br />

scheduling of observations.<br />

EGSE<br />

Instrument Raw Data<br />

LEOP<br />

Network X-Band<br />

TMTC<br />

TMTC<br />

station<br />

S-Band<br />

S-Band<br />

Flight Operations<br />

Control Centre<br />

FOS PDGS<br />

Receiving<br />

Station(s)<br />

Backup<br />

Payload Data<br />

Reception<br />

Decryption, Processing,<br />

Archiving &<br />

Dissemination<br />

Users Services<br />

Coordination & Control<br />

Payload Mission<br />

Planning<br />

User<br />

Requests<br />

External<br />

Auxiliary Data<br />

Sensor<br />

Performance,<br />

Products and<br />

Algorithms<br />

Meteo Forecast Data<br />

+ MTG real time data<br />

Users<br />

Figure 4.6-2: Preliminary Architecture of the Geo-Oculus Ground Segment<br />

External<br />

External<br />

Data<br />

Data<br />

Sources<br />

Sources<br />

Basic Products<br />

User Reception<br />

and Processing<br />

Terminal<br />

Service<br />

Segment<br />

Customised<br />

Services<br />

Payload Data<br />

Reception<br />

Decryption,<br />

Processing,<br />

Archiving &<br />

Dissemination<br />

Basic Products<br />

The concept for the GEO-Oculus Ground Segment takes into account the particular principles of<br />

operations and technical constraints resulting from a spacecraft on a geostationary orbit. Moreover,<br />

the ground segment architecture is adapted to the needs of its customers for the different targeted<br />

applications, in terms of revisit time, flexibility in satellite observations programming and latency from<br />

observation to end of product delivery. In addition, the Ground Segment concept for the Sentinel<br />

missions, which will be operated by <strong>ESA</strong> in the GMES era, has been considered as a "loose" design<br />

guideline.<br />

The mission for an optical high spatial resolution satellite operating from a GEO orbit must be<br />

regarded as the conjunction of routine monitoring missions (sometimes termed “background” mission)<br />

and of one or several emergency monitoring missions, which are by nature less schedulable than the<br />

routine ones. An example of routine monitoring mission is the monitoring of coastal areas for which the<br />

revisit times and the response times are comparatively long. Emergency monitoring missions are e.g.<br />

fire or disaster monitoring. In this case, the revisit time as well as the response time need to be much<br />

Doc. No: GOC-ASG-RP-002 Page 4-79<br />

Issue: 2<br />

Date: 13.05.2009 Astrium GmbH

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