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Study on feasibility of SATCOM for railway communication

SRAIL-FNR-010-IND%20-%20FinalReport_v1.1_20170216

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Final Report<br />

C.4 <strong>SATCOM</strong> SOLUTION 4: GEO / L-BAND BASED ON ANTARES CS (IRIS FOC)<br />

GEO / L-band + ANTARES CS (IRIS FOC)<br />

Criteri<strong>on</strong> ID Criteri<strong>on</strong> Evaluati<strong>on</strong> Justificati<strong>on</strong><br />

CRT-TECH-1<br />

The “link availability” <strong>of</strong> the proposed satcom system shall be<br />

High.<br />

C (Low)<br />

Unlike the Inmarsat 4 system, it is an "open" soluti<strong>on</strong> where a high link availability<br />

<strong>for</strong> safety applicati<strong>on</strong>s can be c<strong>on</strong>sidered, since the use <strong>of</strong> a low frequency band<br />

(L-band) helps to this demanding requirement.<br />

Anyway, it is also worth to menti<strong>on</strong> that being compliant with the high link<br />

availability required may imply the impossibility to provide some types <strong>of</strong> terminals<br />

(basically handhelds). Regarding this issue, it is true that Inmarsat 4 (also a<br />

GEO/L-band soluti<strong>on</strong>) enables the use <strong>of</strong> handhelds, but not being compliant with<br />

the high link availability criteri<strong>on</strong>.<br />

CRT-TECH-2 The “reliability” <strong>of</strong> the proposed satcom system shall be High. C (High)<br />

With the aim <strong>of</strong> increasing reliability and comply with the safety applicati<strong>on</strong>s<br />

requirements, this future (hypothetical) satcom system can be designed with<br />

redundancy in both ground and space segments.<br />

In additi<strong>on</strong>, <strong>railway</strong> terminals shall be designed to provide the required MTBF and<br />

MTTR figures.<br />

CRT-TECH-3<br />

The end-to-end error ratio <strong>of</strong> the proposed satcom system shall<br />

be Low.<br />

Note: Since this criteri<strong>on</strong> <strong>on</strong>ly c<strong>on</strong>siders the satellite system,<br />

the error ratio shall be measured after the last satellite<br />

communicati<strong>on</strong><br />

C<br />

The end-to-end error ratio depends mainly <strong>on</strong> the FEC used. Current satcom<br />

systems have implemented powerful FECs based mainly <strong>on</strong> turbo codes (e.g.<br />

TCC, TPC, LDPC, etc.) that enable the use <strong>of</strong> low Eb/No to assure the minimum<br />

required BER and/or PER.<br />

ANTARES CS also provides powerful FEC codes, such as TCC and LDPC, and<br />

also ARQ techniques to improve c<strong>on</strong>tinuity.<br />

Doc.Nº: SRAIL-FNR-010-IND<br />

Edit./Rev.: 1/1<br />

Date: 16/02/2017<br />

Page 239 <strong>of</strong> 285

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