4 Final Report - Emits - ESA
4 Final Report - Emits - ESA
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