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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 />

Table 8: Satellite c<strong>on</strong>stellati<strong>on</strong> main types and features<br />

Other c<strong>on</strong>stellati<strong>on</strong> type not menti<strong>on</strong>ed in the above table is HEO (Highly Elliptical Orbit). This specific<br />

satellite c<strong>on</strong>stellati<strong>on</strong> is ideal <strong>for</strong> fixed and mobile applicati<strong>on</strong>s within high latitudes <strong>of</strong> Northern and<br />

Southern Hemisphere including both Polar Regi<strong>on</strong>s. The <strong>on</strong>ly problem is that the user terminal needs<br />

reliable antenna tracking systems and numerous Gateway Earth Stati<strong>on</strong>s (GES). The essential<br />

employment possibility <strong>of</strong> this orbit is to be in hybrid c<strong>on</strong>stellati<strong>on</strong> with GEO or Medium Earth Orbit<br />

(MEO) satellite systems to provide worldwide coverage.<br />

SATELLITE BEAMS<br />

All satellites generate beams, which focuses microwaves signals <strong>on</strong>to the specified porti<strong>on</strong>s <strong>of</strong> the<br />

earth‘s surface to most effectively use the limited power <strong>of</strong> their transp<strong>on</strong>ders. These focused signals<br />

create unique beam patterns called ―footprints.‖ The most typical footprints types are:<br />

<br />

<br />

<br />

Global beam footprint,<br />

Mobile (or regi<strong>on</strong>al) beam footprint or<br />

Spot beams<br />

Satellites do not always support perfectly spherical coverage areas. There<strong>for</strong>e, shaped spot beams let<br />

the operator c<strong>on</strong>centrate coverage and power where required. In additi<strong>on</strong>, movable antennas also let<br />

the satellite operator provide more support (traffic) to a regi<strong>on</strong> <strong>on</strong> demand.<br />

An example <strong>of</strong> typical <strong>SATCOM</strong> architecture is shown in the next figure:<br />

Forward Link<br />

Return Link<br />

Terrestrial Link<br />

SATELLITE SYSTEM<br />

SPACE<br />

SEGMENT<br />

Traffic<br />

C<strong>on</strong>trol<br />

Centre<br />

GROUND<br />

SEGMENT<br />

USER<br />

SEGMENT<br />

Train<br />

Stati<strong>on</strong>s<br />

WAN<br />

GES/NCC<br />

GAP FILLERS<br />

RBCs<br />

Figure 11: Satcom baseline system architecture (<strong>railway</strong> oriented)<br />

Above figure identifies the main comp<strong>on</strong>ents <strong>of</strong> each <strong>on</strong>e <strong>of</strong> the segments (i.e. user, ground and<br />

space) and their relati<strong>on</strong>ships through the satellite communicati<strong>on</strong> payload.<br />

Doc.Nº: SRAIL-FNR-010-IND<br />

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

Date: 16/02/2017<br />

Page 47 <strong>of</strong> 285

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