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Satellite-based positioning
R. Knippers
Application fields
Surveying
Military operations
Engineering
Vehicle tracking
Flight navigation
Car navigation
Ship navigation
Agriculture
Mapping
Topics for discussion
 The segments of a satellite-based
positioning system
 GPS, GLONASS and Galileo
 Principle of positioning
 Errors and their sources
 Positional accuracies
 Relative (differential) positioning
Three segments
 Space segment: the satellites that orbit
the Earth, and the radio signals that they
emit.
 Control segment: the ground stations that
monitor and maintain the space segment
components.
 User segment: the users with their hard-
and software to conduct positioning.
Space segment of GPS system
The space segment of GPS
consists of 24 satellites on 6
orbits (approx. 22,000 km
from the centre of the Earth):
 Each satellite carries a
clock.
 Each satellite completes 2
orbits/day.
 24 hour complete GPS
coverage anywhere on the
Earth.
 Accuracy: 21 meters 95% of
time
NAVSTAR GPS
Satellite
L2 Carrier
L1 Carrier
P-Code
P-Code
C/A Code
Navigation
Message
Navigation
Message
1227.60 MHz
1575.42 MHz
GPS Signal Structure
Control Segment of GPS
Space Segment
24+ Satellites
Current ephemeris is
transmitted to users
Monitor Stations
• Diego Garcia
• Ascension Island
• Kwajalein
• Hawaii
• Colorado Springs
GPS Control
Colorado Springs
End
User
Control Segment of GPS
Master Control Station
Monitor Station
Ground Antenna
Colorado
Springs
Hawaii
Ascension
Islands
Diego
Garcia
Kwajalein
User segment of GPS
Receivers and their users:
 (Military)
 Navigation in 3D-aircrafts,
 ships, ground vehicles and
hand-carried instruments
 Precise positioning -
Surveying
 (Time dissemination -
astronomy)
 (Research projects on
atmospheric distortions)
GPS-Receivers
Selection of a GPS receiver
 Application (boating, flying, driving,
mapping, surveying)
 Accuracy requirements
 Power consumption requirements
 Operational environment
 Signal processing requirements
 Cost
 Data exchange standards
Space segment of GLONASS system
Russian system
(Globalnaya Navigatsionnaya
Spunikova Sistema - GLONASS)
 24 satellites (21 operational and
3 spare).
 Three orbital planes at 65º
inclination.
 Two codes as GPS, but all
satellites broadcast identical
codes but using slightly
different carrier frequencies for
each satellite.
 The positioning principal is the
same as GPS
 Accuracy: 20 m horizontal and
~30 m vertical
GLONASS Satellite
http://www.glonass-ianc.rsa.ru
Space segment of Galileo system
Galileo is in the implementation
phase, first satellite to be
launched in 2006, planned
operation start 2008.
 Designed for civil purposes
 30 satellites
 3 orbits (23,222 km high)
 Network of ground stations, 2
control centresin Europe
 Accuracy of single receiver:
around 1 m
http://www.esa.int/esaNA/SEMY02FFWOE_galileo_0.html
Galileo Satellite
Principle of positioning
GPS-receiver
GPS-satellite
Distance =
(velocity of light) x (travel time)
The GPS-receiver computes the
distances (ranges) to the satellites
The GPS-receiver computes the
distances (ranges) to the satellites
How does the GPS-receiver
computes the travel time?
How does the GPS-receiver
computes the travel time?
L2 = 1227.60 MHz
L1 = 1575.42 MHz
GPS code on Carrier wave
(C/A or P code)
It receives GPS-codes and
Carrier waves from the satellite
It receives GPS-codes and
Carrier waves from the satellite
Code from Satellite
Code from Receiver
Time difference
between
Receiver and Satellite signal
∆t
Code comparison
Principle of positioning
GPS-receiver
GPS-satellite
Pseudo-range =
(velocity of light) x (travel time)
+ (receiver clock error) + (other errors)
The GPS-receiver measures in fact
pseudo distances (pseudo-ranges) to
the satellites
The GPS-receiver measures in fact
pseudo distances (pseudo-ranges) to
the satellites
Principle of positioning
(X,Y,Z)
1 2
3
distance 1
distance 2
distance 3
To determine a position in a
3 dimensional space it takes in theory
3 distance measurements from
3 satellites
To determine a position in a
3 dimensional space it takes in theory
3 distance measurements from
3 satellites
Pseudorange positioning
Three-satellite fix position
(trilateration)
Two-satellite fix position
One-satellite fix position
(X,Y,Z,∆
∆
∆
∆t)
1
2
3
4
pseudorange 1
pseudo-
range 2
pseudo-
range 3
pseudorange 4
Pseudorange =
velocity of light * travel time
+ receiver clock error + other errors
Accurate positioning requires
an extra distance measurement
from a fourth satellite to
eliminate the receiver clock error
Accurate positioning requires
an extra distance measurement
from a fourth satellite to
eliminate the receiver clock error
Principle of positioning
Synchronization bias of the receiver clock
Error sources in absolute positioning
 Selective availability
 Satellite clock and orbit errors
 Ionospheric and tropospheric delays
 Receiver’s environment (multi-path)
 Satellite constellation
Receiver’s environment errors
Magnitude of the error sources*
* Absolute, single-point positioning based on code measurements
*
Good satellite constellation
Low PDOP (1.5)
Good satellite constellation
Low PDOP (1.5)
Bad satellite constellation
High PDOP(5.7)
Bad satellite constellation
High PDOP(5.7)
Satellite constellation
positional error
Positional accuracy in absolute positioning
Absolute, single-point positioning based on
code measurements:
Typical error: 5-10 m (horizontal accuracy)
Typical error: 2-5 m (horizontal accuracy) when using a dual-
frequency receiver or the encrypted military signals (P-code)
Location errors: noise, bias and blunder
 Noise (random) errors:
noise in code and noise
in receiver, multi-path.
 Bias (systematic) errors:
clock, satellite position,
ionosphere, troposphere,
GDOP effects.
 Blunder: incorrect
geodetic datum,
software failures,
hardware problems etc.
Systematic errors (bias) removal is essential
to improve the positional accuracy!
(X,Y,Z) Reference point
Reference (or base) receiver
Target (or field) receiver
Differential (or relative)
positioning
Relative positioning
Positional accuracy in relative positioning
Relative, single-point positioning based on
code measurements:
Typical error: 0.5 - 5m (horizontal accuracy)
Positional accuracy in relative positioning
Relative, single-point positioning based on
carrier phase measurements:
Typical error: 2mm – 2cm (horizontal accuracy)
Carrier phase measurements
Carrier phase measurement is a technique to measure the range
(distance) of a satellite by determine the number of cycles of the
(sine-shaped) radio signal between sender and receiver.
The number of cycles is determined in a long observation session
from the change in carrier phase (Phase Shift Keying). This
change happens because the satellite is orbiting itself.
L1/L2 Carrier
Relative (differential) survey
techniques using carrier phase
measurements
 Static
 Stop and go kinematic
 Pseudo-kinematic
 Kinematic
 Rapid static
 On-the-fly (OTF)/real-time kinematic (RTK)
Real-time kinematic positioning
Network positioning
Network positioning
Relative positioning using a network of reference stations
NLR Globalcom
http://www.lnrglobalcom.nl
GlobalNET 2005
Network positioning
GlobalNET 2005: Reference Station at ITC
Satellite-Based Augmentation
Systems (SBAS)
(X,Y,Z) Reference point
Ground station
Field receiver
(X,Y,Z) Reference point
Ground station
Geostationary satellite
Satellite-based Augmentation
Systems
(X,Y,Z) Reference point
Ground station
(X,Y,Z) Reference point
Ground station
Geostationary satellite
Satellite-based Augmentation
Systems
Operational systems
 WAAS (Wide-Area Augmentation System)
for North America
 EGNOS (European Geostationary
Navigation Overlay Service) for Europe
 MSAS (Multi-functional Satellite
Augmentation System) for eastern Asia
WAAS, EGNOS, MSAS
Satellite Based Positioning.
Wide Area Augmentation System (WAAS)
Local Area Augmentation System (LAAS)
INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION
The end !
INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION
Mobile GIS applications
Data collection with a mobile computer
INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION
Location-Based Services (LBS)
Location-Based Services on a Mobile
computer or mobile phone.
INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION
Location-Based Services - Applications
1. Location based information services (e.g.
search for the nearest restaurant or the nearest
banking cash machine)
2. Location based emergency service (e.g.
pinpoint your location on dialing 9-1-1)
3. Location based billing service (e.g. preferential
billing for calling by establishing personal zones
such as a home zone or work zone).
4. Fleet applications (tracking a vehicle and/or
operator).
INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION
LBS application - Mobile phone tracking
http://geotracing.com/tland

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Satellite Based Positioning.

  • 2. Application fields Surveying Military operations Engineering Vehicle tracking Flight navigation Car navigation Ship navigation Agriculture Mapping
  • 3. Topics for discussion The segments of a satellite-based positioning system GPS, GLONASS and Galileo Principle of positioning Errors and their sources Positional accuracies Relative (differential) positioning
  • 4. Three segments Space segment: the satellites that orbit the Earth, and the radio signals that they emit. Control segment: the ground stations that monitor and maintain the space segment components. User segment: the users with their hard- and software to conduct positioning.
  • 5. Space segment of GPS system The space segment of GPS consists of 24 satellites on 6 orbits (approx. 22,000 km from the centre of the Earth): Each satellite carries a clock. Each satellite completes 2 orbits/day. 24 hour complete GPS coverage anywhere on the Earth. Accuracy: 21 meters 95% of time NAVSTAR GPS Satellite
  • 6. L2 Carrier L1 Carrier P-Code P-Code C/A Code Navigation Message Navigation Message 1227.60 MHz 1575.42 MHz GPS Signal Structure
  • 7. Control Segment of GPS Space Segment 24+ Satellites Current ephemeris is transmitted to users Monitor Stations • Diego Garcia • Ascension Island • Kwajalein • Hawaii • Colorado Springs GPS Control Colorado Springs End User
  • 8. Control Segment of GPS Master Control Station Monitor Station Ground Antenna Colorado Springs Hawaii Ascension Islands Diego Garcia Kwajalein
  • 9. User segment of GPS Receivers and their users: (Military) Navigation in 3D-aircrafts, ships, ground vehicles and hand-carried instruments Precise positioning - Surveying (Time dissemination - astronomy) (Research projects on atmospheric distortions) GPS-Receivers
  • 10. Selection of a GPS receiver Application (boating, flying, driving, mapping, surveying) Accuracy requirements Power consumption requirements Operational environment Signal processing requirements Cost Data exchange standards
  • 11. Space segment of GLONASS system Russian system (Globalnaya Navigatsionnaya Spunikova Sistema - GLONASS) 24 satellites (21 operational and 3 spare). Three orbital planes at 65º inclination. Two codes as GPS, but all satellites broadcast identical codes but using slightly different carrier frequencies for each satellite. The positioning principal is the same as GPS Accuracy: 20 m horizontal and ~30 m vertical GLONASS Satellite http://www.glonass-ianc.rsa.ru
  • 12. Space segment of Galileo system Galileo is in the implementation phase, first satellite to be launched in 2006, planned operation start 2008. Designed for civil purposes 30 satellites 3 orbits (23,222 km high) Network of ground stations, 2 control centresin Europe Accuracy of single receiver: around 1 m http://www.esa.int/esaNA/SEMY02FFWOE_galileo_0.html Galileo Satellite
  • 13. Principle of positioning GPS-receiver GPS-satellite Distance = (velocity of light) x (travel time) The GPS-receiver computes the distances (ranges) to the satellites The GPS-receiver computes the distances (ranges) to the satellites How does the GPS-receiver computes the travel time? How does the GPS-receiver computes the travel time?
  • 14. L2 = 1227.60 MHz L1 = 1575.42 MHz GPS code on Carrier wave (C/A or P code) It receives GPS-codes and Carrier waves from the satellite It receives GPS-codes and Carrier waves from the satellite
  • 15. Code from Satellite Code from Receiver Time difference between Receiver and Satellite signal ∆t Code comparison
  • 16. Principle of positioning GPS-receiver GPS-satellite Pseudo-range = (velocity of light) x (travel time) + (receiver clock error) + (other errors) The GPS-receiver measures in fact pseudo distances (pseudo-ranges) to the satellites The GPS-receiver measures in fact pseudo distances (pseudo-ranges) to the satellites
  • 17. Principle of positioning (X,Y,Z) 1 2 3 distance 1 distance 2 distance 3 To determine a position in a 3 dimensional space it takes in theory 3 distance measurements from 3 satellites To determine a position in a 3 dimensional space it takes in theory 3 distance measurements from 3 satellites
  • 18. Pseudorange positioning Three-satellite fix position (trilateration) Two-satellite fix position One-satellite fix position
  • 19. (X,Y,Z,∆ ∆ ∆ ∆t) 1 2 3 4 pseudorange 1 pseudo- range 2 pseudo- range 3 pseudorange 4 Pseudorange = velocity of light * travel time + receiver clock error + other errors Accurate positioning requires an extra distance measurement from a fourth satellite to eliminate the receiver clock error Accurate positioning requires an extra distance measurement from a fourth satellite to eliminate the receiver clock error Principle of positioning
  • 20. Synchronization bias of the receiver clock
  • 21. Error sources in absolute positioning Selective availability Satellite clock and orbit errors Ionospheric and tropospheric delays Receiver’s environment (multi-path) Satellite constellation
  • 23. Magnitude of the error sources* * Absolute, single-point positioning based on code measurements *
  • 24. Good satellite constellation Low PDOP (1.5) Good satellite constellation Low PDOP (1.5) Bad satellite constellation High PDOP(5.7) Bad satellite constellation High PDOP(5.7) Satellite constellation positional error
  • 25. Positional accuracy in absolute positioning Absolute, single-point positioning based on code measurements: Typical error: 5-10 m (horizontal accuracy) Typical error: 2-5 m (horizontal accuracy) when using a dual- frequency receiver or the encrypted military signals (P-code)
  • 26. Location errors: noise, bias and blunder Noise (random) errors: noise in code and noise in receiver, multi-path. Bias (systematic) errors: clock, satellite position, ionosphere, troposphere, GDOP effects. Blunder: incorrect geodetic datum, software failures, hardware problems etc. Systematic errors (bias) removal is essential to improve the positional accuracy!
  • 27. (X,Y,Z) Reference point Reference (or base) receiver Target (or field) receiver Differential (or relative) positioning Relative positioning
  • 28. Positional accuracy in relative positioning Relative, single-point positioning based on code measurements: Typical error: 0.5 - 5m (horizontal accuracy)
  • 29. Positional accuracy in relative positioning Relative, single-point positioning based on carrier phase measurements: Typical error: 2mm – 2cm (horizontal accuracy)
  • 30. Carrier phase measurements Carrier phase measurement is a technique to measure the range (distance) of a satellite by determine the number of cycles of the (sine-shaped) radio signal between sender and receiver. The number of cycles is determined in a long observation session from the change in carrier phase (Phase Shift Keying). This change happens because the satellite is orbiting itself. L1/L2 Carrier
  • 31. Relative (differential) survey techniques using carrier phase measurements Static Stop and go kinematic Pseudo-kinematic Kinematic Rapid static On-the-fly (OTF)/real-time kinematic (RTK)
  • 34. Network positioning Relative positioning using a network of reference stations NLR Globalcom http://www.lnrglobalcom.nl GlobalNET 2005
  • 35. Network positioning GlobalNET 2005: Reference Station at ITC
  • 37. (X,Y,Z) Reference point Ground station Field receiver (X,Y,Z) Reference point Ground station Geostationary satellite Satellite-based Augmentation Systems
  • 38. (X,Y,Z) Reference point Ground station (X,Y,Z) Reference point Ground station Geostationary satellite Satellite-based Augmentation Systems
  • 39. Operational systems WAAS (Wide-Area Augmentation System) for North America EGNOS (European Geostationary Navigation Overlay Service) for Europe MSAS (Multi-functional Satellite Augmentation System) for eastern Asia
  • 42. Wide Area Augmentation System (WAAS)
  • 43. Local Area Augmentation System (LAAS)
  • 44. INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION The end !
  • 45. INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION Mobile GIS applications Data collection with a mobile computer
  • 46. INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION Location-Based Services (LBS) Location-Based Services on a Mobile computer or mobile phone.
  • 47. INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION Location-Based Services - Applications 1. Location based information services (e.g. search for the nearest restaurant or the nearest banking cash machine) 2. Location based emergency service (e.g. pinpoint your location on dialing 9-1-1) 3. Location based billing service (e.g. preferential billing for calling by establishing personal zones such as a home zone or work zone). 4. Fleet applications (tracking a vehicle and/or operator).
  • 48. INTERNATIONAL INSTITUTE FOR GEO-INFORMATION SCIENCE AND EARTH OBSERVATION LBS application - Mobile phone tracking http://geotracing.com/tland