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==EGNOS Space Segment==
==EGNOS Space Segment==


The EGNOS Space Segment comprises 3 GEO satellites broadcasting corrections and integrity information for GPS satellites in the L1 frequency band (1575,42 MHz). At the
The [[EGNOS Space Segment | EGNOS Space Segment]]comprises 3 GEO satellites broadcasting corrections and integrity information for GPS satellites in the L1 frequency band (1575,42 MHz). At the
date of publication the 3 GEOs used by EGNOS are:<ref name=" THE EGNOS SYSTEM ARCHITECTURE EXPLAINED"/>
date of publication the 3 GEOs used by EGNOS are:<ref name=" THE EGNOS SYSTEM ARCHITECTURE EXPLAINED"/>



Revision as of 10:27, 4 May 2011


EGNOSEGNOS
Title EGNOS Architecture
Author(s) GMV.
Level Basic
Year of Publication 2011
Logo GMV.png


The goal of EGNOS (European Geostationary Navigation Overlay Service) is to augment the [GPS Introduction|GPS]] in order to improve the navigation performances in terms of accuracy and integrity (with the required levels of availability and continuity of service) over the European Civil Aviation Conference (ECAC) Region and to be expandable over neighbouring regions.

These augmentations are obtained by providing a GPS-like Geostationary Ranging service (R-GEO), by broadcasting precise Wide Area Differential corrections to correct for GPS, GLONASS and GEO orbit and clock errors and also to correct the ionospheric delays affecting the signal paths to the users. The complex message broadcast by EGNOS GEOs also include Integrity data which allow to bound the remaining errors with a high level of confidence. EGNOS has deployed its Advanced Operational Capability (AOC) using two existing INMARSAT-III navigation transponders (AOR-E and IOR-W) plus a navigation transponder on board of Artemis satellite.[1]

The EGNOS architecture is very complex and highly redundant. It is composed by 47 elements deployed onto 41 sites in 22 Countries. EGNOS has been designed to meet the international SBAS standards and performs the following tasks:

  • Collect GPS/GLONASS/GEO signals and data.
  • Estimate the integrity data and WAD corrections for the service area.
  • Transmit to the users, via the GEO satellites, a GPS-like signal, augmented with integrity and correction messages.
  • Verify the correctness of these integrity and correction messages.

Architecture Overview

The EGNOS system is directly decomposed in its four segments, a Ground Segment, a Space Segment, a User segment and a Support Segment:[2]

EGNOS functional architecture
  • The Ground Segment is the real-time part of EGNOS. It computes precise differential corrections as well as the GEO ranging and makes all these information available to users through a broadcast by the Space Segment.
  • The Space segment, using three GEO satellites, provides redundant data transmission channel to broadcast toward EGNOS users messages containing differential corrections with the associated integrity information. The GEO satellites additionally provide GPS-like ranging signal that is permanently steered and synchronised by the ground segment.
  • The User Segment is made of EGNOS receivers that enable EGNOS users to accurately compute their position.
  • The Support segment contains off-line facilities listed hereafter:
    • PACF: Performance Assessment and Check-out Facility, provides support to EGNOS management in such area as performances analysis, troubleshooting, operational procedures as well as upgrade specification and validation, support to maintenance.
    • ASQF: Application specific qualification facility provides civil aviation and aeronautical certification authorities with the tools to qualify validate and certify the different EGNOS applications.
    • DVP: Development & Verification platform is used to validate and verify EGNOS requirements during the design phase. It contains simulation facilities, a real-time testbed and an assembly, integration and verification platform. The DVP is incorporated in PACF.

EGNOS Space Segment

The EGNOS Space Segmentcomprises 3 GEO satellites broadcasting corrections and integrity information for GPS satellites in the L1 frequency band (1575,42 MHz). At the date of publication the 3 GEOs used by EGNOS are:[1]

GEO Name PRN Number ID(NMEA) Orbital Slot
ARTEMIS 124 37 21.5E
INMARSAT AOR-E 120 33 15.5W
INMARSAT IOR-W 126 39 25E

This space segment confi guration provides a high level of redundancy over the whole service area in case of a geostationary satellite link failure. The EGNOS operations are handled in such a way that, at any point in time, typically two of the three GEOs broadcast an operational signal. Since it is only necessary to track a single GEO satellite link to benefi t from the EGNOS SoL, this secures a switching capability in case of interruption and ensures a high level of continuity of service.

It is intended that the EGNOS space segment will be replenished over time in order to maintain a similar level of redundancy. The exact orbital location of future satellites may vary, though this will not impact the service offered to users. Similarly, different PRN code numbers may be assigned to future GEOs. However, all SBAS user receivers are designed to automatically detect and use any code in a pre-allocated set reserved for SBAS. Such evolutions will therefore be transparent for end users and will not necessitate any human intervention or change of receiving equipment.

EGNOS Ground Segment

The EGNOS Ground Segment comprises a network of Ranging Integrity Monitoring Stations (RIMS), four Mission Control Centres (MCC), six Navigation Land Earth Stations (NLES), and the EGNOS Wide Area Network (EWAN) which provides the communication network for all the components of the ground segment. Two additional facilities are also deployed as part of the ground segment to support system operations and service provision, namely the Performance Assessment and Checkout Facility (PACF) and the Application Specific Qualification Facility (ASQF), which are operated by the EGNOS Service Provider (ESSP SAS).

The EGNOS system is a widely distributed and redundant system. Data flows from one subsystem to another subsystem have different level of criticality.

EGNOS Data flow

The main EGNOS functions are carried out by the Ground Segment through the following critical subsystems: the RIMS stations, the CPF units and the NLES stations. The Ground Segment is a periodic synchronous and pipelined system. The synchronisation of subsystems located in widely separated geographic places is referred to the GPS time by means of GPS receivers providing a 1 PPS (one Pulse Per Second) synchronisation pulse to the associated subsystem.

Another feature of the EGNOS Ground Segment is that all Monitoring and Control (M&C) functions performed by humans (non automatic functions) are centralised and implemented in the CCF subsystems, which is outside of the critical data flow . Operators on duty in another CCF (hot backup) are ready to take over the system monitoring and control if the master CCF fails. Remaining two CCF (cold backup) can be reactivated if the master one fails.

In the EGNOS data flow representation, the real time critical data flow is indicated in red whereas the non-critical data flow is indicated in green.

The sub-systems involved in the processing of the critical data are responsible for the achievement of the main EGNOS system performance (accuracy, integrity, continuity, time to alarm, and service coverage) while the sub-systems involved in the management of non-critical data perform the Monitoring and Control (M&C) and archive functions.

EGNOS User Segment

The EGNOS User Segment segment consists of the GPS receivers. It is important to bear in mind that a GPS receiver only monitors signals sent by the satellites and does not establish any contact with them. Therefore, a GPS receiver cannot be used by a third party to find out a user’s position without his knowledge.[3]

To receive EGNOS signals an EGNOS compatible receiver is required There are many receivers now already on the market from a variety of manufacturers. An EGNOS receiver is like a GPS receiver but with special software inside that allows the receiver to lock onto the code used by the EGNOS satellites and compute the EGNOS corrections to the GPS signals. Apart from this, an EGNOS receiver is just like a GPS receiver. This means that it can pick up GPS signals as well. An EGNOS receiver is the same size as a GPS receiver and uses the same type of antenna.[4]

To test the EGNOS receiver, special prototypes have been developed with extensive capabilities to log and analyze data.

Notes

References

  1. ^ a b THE EGNOS SYSTEM ARCHITECTURE EXPLAINED; Didier Flament, Jean Poumailloux, Jean-Louis Damidaux, Stéphane Lannelongue Alcatel Alenia Space, France ; Javier Ventura-Traveset, P. Michel and C. Montefusco ; European Space Agency, EGNOS Project Office;
  2. ^ EGNOS Safety of Life (SoL) Service Definition Document (SDD)
  3. ^ USER GUIDE FOR EGNOS APPLICATION DEVELOPERS
  4. ^ ESA Navigation Site on EGNOS User Segment