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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 />

<strong>ESA</strong> UNCLASSIFIED – For Official Use<br />

© <strong>ESA</strong><br />

The copyright of this document is the property of <strong>ESA</strong>. It is supplied in confidence and shall not be reproduced, copied or<br />

communicated to any third party without written permission from <strong>ESA</strong>.

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