Galileo Concept of Operations, First
IOV LEOP and Initial Operations
Marco LISI
Senior Member AIAA
European Space Agency
SpaceOps 2012, Stockholm, June 11-15 2012
Navigation solutions powered by Europe
Table of Contents








Introduction
Galileo System Overview
Galileo Concept of Operations
Galileo IOV System Configuration
Launch, LEOP and Early Operations
Conclusions
Summary
EGNOS and Galileo are the key elements of the
European navigation “system of systems”, a
strategic and critical infrastructure of EU;
The Galileo global navigation satellite system,
joint initiative by the European Union and the
European Space Agency, is one of most
ambitious and technologically advanced service
oriented system being developed in Europe, by
European industries and with European
resources;
The first two satellites of the Galileo constellation
were successfully launched on 21st October
2011, after an integrated effort at systems
engineering, operations and ILS level.
GALILEO Program essentials
Galileo is Europe's initiative for a state-of-the-art
global navigation satellite system, providing a
highly accurate, guaranteed global positioning
service under civilian control
While providing autonomous navigation and
positioning services, Galileo will at the same
time be interoperable with GPS and GLONASS,
the two other global satellite navigation systems
The fully deployed Galileo system will consist of
30 satellites and the associated ground
infrastructure.
4
The Galileo System
Galileo Incremental Deployment
Galileo Services
Open Service

Free to air; Mass market; Simple
positioning

Commercial Service

Encrypted; High accuracy;
Guaranteed service

Safety of Life Service

Open Service + Integrity of
signal

Public Regulated
Service

Encrypted; Continuous
availability

Search and Rescue
Service

Near real-time; Precise; Return
link feasible
Galileo Concept of Operations
Galileo Key Operational Processes

9
Galileo KPI’s Dashboard

1st level
maintenance

2nd level
maintenance

Downtime of
Control Centers

Spare parts
availability

Preventive
maintenance

Respect of
procedures
In Orbit Validation Objectives
Constellation
Signal in Space

Users
Sensor Stations
Estaciones de
Referencia

TT&C
Stations

Control Centres

Mission
U/L
Stations
Galileo IOV System Architecture
IOV-1 Satellites
Galileo Constellation
Walker 27/3/1 constellation
plus 3 in-orbit spares
Semi-major axis
29600.318 km
Inclination 56 deg
Period: 14h 4m 42s
Ground track
repeat cycle
10 days / 17 orbits

Overall Spacecraft
Mass at Launch (incl. Propellant)
Power Consumption
Dimensions:
Lifetime
Orbit Injection
Attitude Profile

~700 kg
1420 W
2.74 x 14.5 x 1.59 m
12 years
Direct into MEO orbit
Yaw Steered
Galileo IOV – Ground Control Centres
2 Complementary Control Centres:
• Ground Mission Segment (GMS)
in Fucino has the responsibility
for the mission aspects ,
• Ground Control Segment (GCS)
in Oberpfaffenhofen, to control
and monitor the constellation.
Both centres will be completed
to become fully redundant.

© Axel Schultes Architekten
GCC-D at DLR - Oberpfaffenhofen
GCC-I at Telespazio - Fucino
Soyuz Launch Site at Centre Spatial Guyanais
(Kourou)
Kiruna TT&C Site
Redu IOT Station

IOT Measurement System Online Area

Redu IOT Station L-Band 21mt dish

Redu C-band antenna
Galileo IOV Operations Overview

Initial in-orbit operations (LEOP) are conducted from the LEOP Control
Centre (LOCC) in CNES Toulouse (F)
Following the start of the orbit drift phase, C&C of each S/C is handedover to the Galileo Control Centre (GCC-D) in DLR Oberpfaffenhofen
(D), in charge of all following PF/PL operations
PL IOT activities are conducted from the Galileo IOT Station in Redu (B),
with the S/C controlled by GCC-D
Specific PL IOT tests cases are executed from the Galileo Control Centre
(GCC-I) in TPZ Fucino (I), in charge of all mission operations activities
IOV-1 Launch Campaign (1/3)

FM2 arrival 
08/09

PFM arrival
15/09

Autonomous Operations
08‐30/09
IOV-1 Launch Campaign (2/3)

FM2 & PFM fuelling
26 & 30/09

Dispense Integration
04‐05/10

Fregat Integration
10/10
IOV-1 Launch Campaign (3/3)
Soyuz Rollout
14/10

Fairing Encapsulation and transport
12‐14/10

Upper Composite 
integrated in Soyuz 14/10
October 21st 2011: First IOV Launch
IOV-1 Launch Sequence
Galileo IOV LEOP (1/2)
After S/C separation from
Soyuz/Fregat, LOCC monitors
the automatic INIT sequence
TT&C TM transmitter ON
AOC units ON
Rate damping
Initial sun acquisition
Solar arrays deployment

After initial verification of the
Platform S/S status, the S/C is
commanded to Earth
acquisition
Galileo IOV LEOP (2/2)
Initial orbit maneuvers are then performed for:
Correcting the orbit injection errors and
Reaching the initial target orbit with the required accuracy
Positioning the S/C in its allocated orbital slot

After completion of the drift start man oeuvres, the S/C is
commanded to Normal Mode (which is the nominal
satellite operational mode)
Yaw steering control ensures that the solar arrays are tracking
the Sun and the navigation antenna is pointed towards Earth

Control of each spacecraft is then handed-over to the
GCC-D for all following operations
This constitutes the end of LEOP controlled activities
C&C Handover to GCC-D
•

•

Handover from LOCC to
GCC-D is performed after
completion of the
manoeuvres to start the
drift phase
It is carried during
combined visibility from
the LEOP GS and the
TTCF

The Handover process checks the status of each S/C
for:
Orbital elements of the satellite
Estimation of drift rate
Fuel consumption from operation until C&C hand-over
Status of each S/S
Operations from GCC-D
•
•

GCC-D is in charge of
operations of the Galileo
constellation
In IOV, the Ground
Control Segment (GCS)
facilities are deployed in
the GCC-D for command
and control of the space,
GCS, and GCC hosting
infrastructure

The main components of the GCS infrastructure covers:
Spacecraft Constellation Control Facility (SCCF) based on ESA
SCOS 5
Key Management Facilities (KMF) for S-Band TM/TC encryption
Tracking, Telemetry and Control Facility (TTCF) in Kourou and
Kiruna
IOT Operations from Redu
•

Following the navigation
payload switch on from GCC-D,
In Orbit Tests are conducted to
• verify the performances of the L-

•
•

•

Band navigation signals and
messages, and to receive the SAR
payload test downlink
transmit navigation test messages
towards GALILEO satellites
transmit test signals to the
GALILEO Search And Rescue
(SAR) payload

The IOT Measurement System
controls the whole system to
• track the GALILEO satellites
• perform the measurements
• produce the test reports
• connect to the GCC-D to retrieve
satellite telemetry and flight
dynamics data.
First Galileo IOV Signal Received
Operations from GCC-I

After completion of IOT Campaign, routine operations
are jointly conducted from GCC-D (PF/PL control) and
GCC-I (navigation mission control)
The GCC-I Ground Mission Segment (GMS)
infrastructure processes the L-Band data received from
the remote stations, and uplinks the C-Band navigation
messages
The Global Navigation Satellite SoS
GNSoS

ATM
GEOSS
Conclusions
Galileo is one of the most challenging and
rewarding initiatives of the European Union, with
numerous fall-outs in terms of technological,
industrial and operational know-how and
capabilities
Galileo is a service-oriented system of systems,
aiming at delivering services through a dynamic
configuration of people, organizational networks
and shared information (processes, metrics,
policies, regulations)
Service systems, such as Galileo, need the
adoption of specific systems engineering methods
and special attention to operational, governance
and Integrated Logistic Support aspects
Tack själv !

Traditional
Chinese

Thai

Gracias

Thank
You

Russian

Spanish

Obrigado
Brazilian
Portuguese

English
Arabic

Danke

Grazie
Korean

Italian

Simplified
Chinese

Japanese

Merci

German

French

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Galileo concept of operations, first iov leop and initial operations

  • 1. Galileo Concept of Operations, First IOV LEOP and Initial Operations Marco LISI Senior Member AIAA European Space Agency SpaceOps 2012, Stockholm, June 11-15 2012 Navigation solutions powered by Europe
  • 2. Table of Contents       Introduction Galileo System Overview Galileo Concept of Operations Galileo IOV System Configuration Launch, LEOP and Early Operations Conclusions
  • 3. Summary EGNOS and Galileo are the key elements of the European navigation “system of systems”, a strategic and critical infrastructure of EU; The Galileo global navigation satellite system, joint initiative by the European Union and the European Space Agency, is one of most ambitious and technologically advanced service oriented system being developed in Europe, by European industries and with European resources; The first two satellites of the Galileo constellation were successfully launched on 21st October 2011, after an integrated effort at systems engineering, operations and ILS level.
  • 4. GALILEO Program essentials Galileo is Europe's initiative for a state-of-the-art global navigation satellite system, providing a highly accurate, guaranteed global positioning service under civilian control While providing autonomous navigation and positioning services, Galileo will at the same time be interoperable with GPS and GLONASS, the two other global satellite navigation systems The fully deployed Galileo system will consist of 30 satellites and the associated ground infrastructure. 4
  • 7. Galileo Services Open Service Free to air; Mass market; Simple positioning Commercial Service Encrypted; High accuracy; Guaranteed service Safety of Life Service Open Service + Integrity of signal Public Regulated Service Encrypted; Continuous availability Search and Rescue Service Near real-time; Precise; Return link feasible
  • 8. Galileo Concept of Operations
  • 10. Galileo KPI’s Dashboard 1st level maintenance 2nd level maintenance Downtime of Control Centers Spare parts availability Preventive maintenance Respect of procedures
  • 11. In Orbit Validation Objectives Constellation Signal in Space Users Sensor Stations Estaciones de Referencia TT&C Stations Control Centres Mission U/L Stations
  • 12. Galileo IOV System Architecture
  • 13. IOV-1 Satellites Galileo Constellation Walker 27/3/1 constellation plus 3 in-orbit spares Semi-major axis 29600.318 km Inclination 56 deg Period: 14h 4m 42s Ground track repeat cycle 10 days / 17 orbits Overall Spacecraft Mass at Launch (incl. Propellant) Power Consumption Dimensions: Lifetime Orbit Injection Attitude Profile ~700 kg 1420 W 2.74 x 14.5 x 1.59 m 12 years Direct into MEO orbit Yaw Steered
  • 14. Galileo IOV – Ground Control Centres 2 Complementary Control Centres: • Ground Mission Segment (GMS) in Fucino has the responsibility for the mission aspects , • Ground Control Segment (GCS) in Oberpfaffenhofen, to control and monitor the constellation. Both centres will be completed to become fully redundant. © Axel Schultes Architekten
  • 15. GCC-D at DLR - Oberpfaffenhofen
  • 17. Soyuz Launch Site at Centre Spatial Guyanais (Kourou)
  • 19. Redu IOT Station IOT Measurement System Online Area Redu IOT Station L-Band 21mt dish Redu C-band antenna
  • 20. Galileo IOV Operations Overview Initial in-orbit operations (LEOP) are conducted from the LEOP Control Centre (LOCC) in CNES Toulouse (F) Following the start of the orbit drift phase, C&C of each S/C is handedover to the Galileo Control Centre (GCC-D) in DLR Oberpfaffenhofen (D), in charge of all following PF/PL operations PL IOT activities are conducted from the Galileo IOT Station in Redu (B), with the S/C controlled by GCC-D Specific PL IOT tests cases are executed from the Galileo Control Centre (GCC-I) in TPZ Fucino (I), in charge of all mission operations activities
  • 21. IOV-1 Launch Campaign (1/3) FM2 arrival  08/09 PFM arrival 15/09 Autonomous Operations 08‐30/09
  • 22. IOV-1 Launch Campaign (2/3) FM2 & PFM fuelling 26 & 30/09 Dispense Integration 04‐05/10 Fregat Integration 10/10
  • 23. IOV-1 Launch Campaign (3/3) Soyuz Rollout 14/10 Fairing Encapsulation and transport 12‐14/10 Upper Composite  integrated in Soyuz 14/10
  • 24. October 21st 2011: First IOV Launch
  • 26. Galileo IOV LEOP (1/2) After S/C separation from Soyuz/Fregat, LOCC monitors the automatic INIT sequence TT&C TM transmitter ON AOC units ON Rate damping Initial sun acquisition Solar arrays deployment After initial verification of the Platform S/S status, the S/C is commanded to Earth acquisition
  • 27. Galileo IOV LEOP (2/2) Initial orbit maneuvers are then performed for: Correcting the orbit injection errors and Reaching the initial target orbit with the required accuracy Positioning the S/C in its allocated orbital slot After completion of the drift start man oeuvres, the S/C is commanded to Normal Mode (which is the nominal satellite operational mode) Yaw steering control ensures that the solar arrays are tracking the Sun and the navigation antenna is pointed towards Earth Control of each spacecraft is then handed-over to the GCC-D for all following operations This constitutes the end of LEOP controlled activities
  • 28. C&C Handover to GCC-D • • Handover from LOCC to GCC-D is performed after completion of the manoeuvres to start the drift phase It is carried during combined visibility from the LEOP GS and the TTCF The Handover process checks the status of each S/C for: Orbital elements of the satellite Estimation of drift rate Fuel consumption from operation until C&C hand-over Status of each S/S
  • 29. Operations from GCC-D • • GCC-D is in charge of operations of the Galileo constellation In IOV, the Ground Control Segment (GCS) facilities are deployed in the GCC-D for command and control of the space, GCS, and GCC hosting infrastructure The main components of the GCS infrastructure covers: Spacecraft Constellation Control Facility (SCCF) based on ESA SCOS 5 Key Management Facilities (KMF) for S-Band TM/TC encryption Tracking, Telemetry and Control Facility (TTCF) in Kourou and Kiruna
  • 30. IOT Operations from Redu • Following the navigation payload switch on from GCC-D, In Orbit Tests are conducted to • verify the performances of the L- • • • Band navigation signals and messages, and to receive the SAR payload test downlink transmit navigation test messages towards GALILEO satellites transmit test signals to the GALILEO Search And Rescue (SAR) payload The IOT Measurement System controls the whole system to • track the GALILEO satellites • perform the measurements • produce the test reports • connect to the GCC-D to retrieve satellite telemetry and flight dynamics data.
  • 31. First Galileo IOV Signal Received
  • 32. Operations from GCC-I After completion of IOT Campaign, routine operations are jointly conducted from GCC-D (PF/PL control) and GCC-I (navigation mission control) The GCC-I Ground Mission Segment (GMS) infrastructure processes the L-Band data received from the remote stations, and uplinks the C-Band navigation messages
  • 33. The Global Navigation Satellite SoS GNSoS ATM GEOSS
  • 34. Conclusions Galileo is one of the most challenging and rewarding initiatives of the European Union, with numerous fall-outs in terms of technological, industrial and operational know-how and capabilities Galileo is a service-oriented system of systems, aiming at delivering services through a dynamic configuration of people, organizational networks and shared information (processes, metrics, policies, regulations) Service systems, such as Galileo, need the adoption of specific systems engineering methods and special attention to operational, governance and Integrated Logistic Support aspects