GSC Sentinel-2 PDGS OCD - Emits - ESA
GSC Sentinel-2 PDGS OCD - Emits - ESA
GSC Sentinel-2 PDGS OCD - Emits - ESA
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<strong>GSC</strong> <strong>Sentinel</strong>-2 <strong>PDGS</strong> <strong>OCD</strong><br />
Issue 1 Revision 2 (draft) - 25.07.2010<br />
GMES-GSEG-EOPG-TN-09-0008<br />
page 161 of 350<br />
○ Support problem investigations during OSV, Phase-E1 and Phase-E2 of the<br />
spacecrafts as required by the corrective-maintenance activity;<br />
○ Support the qualification phase of all <strong>PDGS</strong> system upgrades before deployment as<br />
required by maintenance or evolution activities;<br />
○ Support the <strong>PDGS</strong> deployment phases of the initial and upgraded versions in<br />
configuring and assembling the deployed-configuration elements to be deployed.<br />
As holding a true functional role including during the entire <strong>PDGS</strong> operational phase, the<br />
<strong>PDGS</strong> RP is intended as a specific functional item of the <strong>PDGS</strong> with a dedicated associated<br />
operations concept.<br />
4.6.2 SYSTEM STATES AND CONFIGURATIONS<br />
Throughout its lifetime, the <strong>PDGS</strong> will evolve between several configurations and states as<br />
required by its development and maintenance activities and by the gradual phase-in of the<br />
<strong>Sentinel</strong>-2 constellation spacecrafts it will serve.<br />
As regarding the successive phase-in of the <strong>Sentinel</strong>-2 units with their respective mission<br />
phases, and while it is assumed that a single and unique <strong>PDGS</strong> system will be shared to<br />
serve the constellation, a distinction has to be made between the <strong>PDGS</strong> instance and the<br />
specific state in which it is operating.<br />
The instance of the <strong>PDGS</strong> refers to its specific existence as an integrated system. As such,<br />
there will be a single physically deployed <strong>PDGS</strong> instance. In complement, a localised (in a<br />
single location) reference instance of the <strong>PDGS</strong> called the Reference-Platform (RP) will be<br />
used for testing, simulation and long-term maintenance purposes (cf. previous section).<br />
In counterpart, the state of the <strong>PDGS</strong> refers to its capability in serving a specific spacecraft<br />
mission. Hence, it is assumed that a single <strong>PDGS</strong> instance can operate in 2 distinct states<br />
simultaneously, one per <strong>Sentinel</strong>-2 unit. E.g. the <strong>PDGS</strong> may operate operationally for<br />
<strong>Sentinel</strong>-2A at the time <strong>Sentinel</strong>-2B is launched for which it operates in pre-operational state<br />
until the end of its commissioning phase.<br />
Finally the configuration of the <strong>PDGS</strong> applies to a particular <strong>PDGS</strong> instance and is configured<br />
to operate on one or both missions each one in their respective states.<br />
The following paragraphs describe those concepts in more details.<br />
4.6.2.1 System States<br />
As driven by the successive phases of the <strong>Sentinel</strong>-2A and <strong>Sentinel</strong>-2B missions described in<br />
section 1.3 leading to a fully operational system supporting the <strong>Sentinel</strong>-2 constellation, as<br />
well as beyond this point, the following states of the <strong>PDGS</strong> are identified:<br />
○ Development state: In this state, the <strong>PDGS</strong> is being built and pre-assembled as a<br />
system on the RP for testing purposes. It is assumed it embeds at this point some but<br />
not necessarily all of its intended functionality and as such may support only partial<br />
services limited to testing activities in a reduced configuration e.g. external interfaces<br />
compatibility testing, etc;<br />
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