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Tectonics through geodesy (GPS)

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Title: Tectonics through geodesy (GPS)


1
Tectonics through geodesy (GPS)
Wednesday 1600-1730
Rocco Malservisi e-mail rocco_at_geophysik.lmu.d
e phone 21804202
Class Web page www.geophysik.lmu.de/malservisi/
TectGPS.html
2
COMPARISON OF DIFFERENT TECHNIQUES
3
The Global Positioning System
  • The Global Positioning System (GPS) is a
    satellite-based navigation system.
  • GPS was originally intended for military
    applications, but in the 1980s, the government
    made the system available for civilian use.
  • GPS works in any weather conditions, anywhere in
    the world, 24 hours a day. There are no
    subscription fees or setup charges to use GPS
  • Some civilian uses
  • Navigation on land, sea, air
  • and space
  • Geophysics research
  • Guidance systems
  • Geodetic network densification
  • Hydrographic surveys

4
HOW GPS WORKS
GPS is based on a 3 segment system
SATELLITE VEICLES
CONTROL SEGMENT
USERS SEGMENT (Receivers, data analysis)
5
HOW GPS WORKS
SATELLITE VEICLES (Space segment)
  • The GPS satellite constellation includes 28
    satellites in 6 orbits (55 inclination).
  • Satellite orbital path is near to circular, with
    a semi-major axis of about 26,600 km (20000 km
    hight) (1158 hr orbits).
  • The satellites travel at speed of 3 km/s, and are
    built to last 10 years.

6
HOW GPS WORKS
SATELLITE VEICLES (Space segment)
  • Time kept by Cesium or Rubidium Clocks (3)
  • SVs broadcast on 2 wavelenght L1 (1.5GHz, 19cm)
    L2 (1.2 GHz 24cm)
  • Signals modulated by a code (discussed later)
  • Message with satellite personal code,
    ephemerides and satellite health

7
GPS SIGNAL
  • Each satellite transmits low-power radio signals
    in 2 carrier frequencies
  • L1 1575.42 MHz 154 time base oscillator
  • L2 1227.6 MHz 120 time base oscillator
  • The signal contains two complex patterns of
    digital signals Precise (P) code and
    Coarse/Acquisition (C/A) code
  • A long period modulation broadcast
    data as SV or
    ephemerides.

Wavelength(m) Frequency (MHz)
293 1.023 C/A code
29.3 10.23 P-code
0.19 1574.42 L1
0.24 1227.6 L2
30 sec data
8
HOW GPS WORKS
CONTROL SEGMENT
  • ground-based facilities are used to monitor and
    control the satellites.
  • Checking and reporting the satellites operational
    health.
  • Checking their exact position in space.
  • The master ground station transmits
  • Corrections for the satellite's ephemeris
    constants.
  • Clock offsets.
  • The GPS signal is updated
    every 2 hours.
  • The satellites can then incorporate
    these updates in
    the signals they
    send to GPS receivers.

9
HOW GPS WORKS
USERS SEGMENT (Receivers, data analysis)
  • Receivers generate the same code as transmitted
    by satellites.
  • The time delay (Dt) between a received signal and
    the receivers generated code enables a receiver
    to estimate its Range to a satellite.

Range (receiver-satellite) DT x c
errors Pseudorange DT x c
  • main error source - receiver clock (d t)

10
THE BASIC IDEA
11
FIND YOUR TIME
Using an extra satellite
Perfect clock
Slow clock
12
HOW TO COMPUTE DISTANCE FROM SVCODE PSEUDORANGE
13
NOISES
  • IONOSPHERE
  • TROPOSPHERE
  • MULTIPATH
  • SATELLITE CONFIGURATION/GEOMETRY (DOP)
  • CLOCKS
  • MONUMENTS
  • ORBITS
  • ANTI SPOOFING (AS)
  • SELECTIVE AVAILABILITY (S/A)

14
NOISES
IONOSPHERE and TROPOSPHERE
15
NOISES
Ionospheric Tropospheric Effects
  • Delay of GPS signal - code modulation and carrier
    phases
  • Carrier phases are greatly effected by the free
    electrons in the Ionosphere.
  • The Ionospheric effect increase as the Total
    Electron Content (TEC) increase.
  • The Ionosphere is a dispersive medium its
    effect is frequency dependent.
  • Troposphere is non-dispersive medium effecting
    both code modulation and carrier phases the same
    way.

For more See Leick (1995)
16
Atmospheric Effects
Solutions for Ionospheric Effect
  • The GPS message contains Ionospheric model
    data.This allow the computation of the
    approximate group delay.
  • Dual-Frequency Ionospheric-free Solution by
    using dual-frequency (L1 L2) receivers
    (Expensive).

17
Atmospheric Effects
Solutions for Tropospheric Effect
  • The Tropospheric delay can vary from 2.0-2.5m in
    the zenith, to 20-28m at a 5o angle.
  • The delay depends on the temperature, humidity
    and pressure
  • The dry atmosphere can be accurately modeled to
    about 2-5 based on the laws of ideal gases
  • The wet component is more difficult to quantify,
    but its contribution is only about 10 of the
    total effect
  • The wet delay is about 5-30 cm. In continental
    midlatitudes.

18
NOISES
MULTIPATH
19
NOISES
SATELLITE CONFIGURATION/GEOMETRY GDOP Geometric
Dilution of Precision
20
HOW TO COMPUTE DISTANCE FROM SVPHASE PSEUDORANGE
21
Precise relative positioning
Single Difference
  • Single Difference phase observable cancels most
    common SV errors, such as SV clock error.
  • Other errors decrease as the length of the
    Baseline is shorter.

Illustration IGS/JPL/NASA
22
Precise relative positioning
Double Difference
  • Uses the L1 and L2 Carrier frequencies
    (wavelength 19-24 cm) to calculate precise
    positioning between 2 GPS stations.
  • Double differencing received signals at both
    stations cancels out most systematic errors
    (station and satellite clock offsets).

Illustration IGS/JPL/NASA
23
Relative positioning (DGPS)
  • For precise positioning we use a GPS receiver at
    known location.
  • Since we know this receivers exact location, we
    can determine the errors in the satellite
    signals.
  • Corrections are transmitted from the base-station
    to various users.
  • Positioning accuracy is 1-2 m (Pseudorange
    wavelength 300 m).

Illustration garmin.com
24
GPS METHODS COMPARISON
Lecture 3 May 10th 2005
25
Permanent sites examples
www.pbo.unavco.org
Lecture 3 May 10th 2005
26
GPS Data Analysis
  • GIPSY-OASIS 2.5 Zumberge et al. 1997
  • JPL Precise Orbits
  • ITRF-97
  • Atmospheric ionospheric models
  • Error Analysis Mao et al. 1999
  • Position Uncertainties (mean) 3, 6 12 mm
  • Rate Uncertainties (mean) 1.0, 1.3 2.5 mm/a

27
Co-Seismic Offsets (Model from InSAR local GPS)
Pedersen et al., 2003
28
Co-Seismic Corrected
  • June 17 21, 2000 SISZ earthquakes
  • Distributed slip model Pedersen et al., 2003
  • Correct positions for offsets, recalculate time
    series
  • Residual Feb. 28 March 6, 2000 Hekla eruption

29
Hekla Deformation
30
Co-Seismic Corrected
  • June 17 21, 2000 SISZ earthquakes
  • Distributed slip model Pedersen et al., 2003
  • Correct positions for offsets, recalculate time
    series
  • Residual Feb. 28 March 6, 2000 Hekla eruption

31
Co-Seismic Corrected
32
Velocity Field Relative to Stable North America
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