GPS Overview Edit this ex :paras  wadher
What is GPS? Radio-based navigation system developed by DoD Initial operation in 1993 Fully operational in 1995 System is called NAVSTAR NAV igation with  S atellite  T iming  A nd  R anging Referred to as GPS Series of 24 satellites, 6 orbital planes, 4 satellite vehicles (SV) on each plane  Works anywhere in the world, 24 hours a day, in all weather conditions and provides:  Location or positional fix Velocity Direction of travel Accurate time
Global Navigation Satellite Systems  (GNSS) NAVSTAR USA GLONASS Russians Galileo Europeans
Trilateration Intersection of spheres SV Ranging Determining distance from SV Timing Why consistent, accurate clocks are required Positioning Knowing where SV is in space Correction of errors Correcting for ionospheric and tropospheric delays GPS involves 5 Basic Steps
How GPS works? Range from each satellite calculated range = time delay X speed of light Technique called  trilateration  is used to determine you position or “fix”  Intersection of spheres At least 3 satellites required for 2D fix  However, 4 satellites should always be used The 4 th  satellite used to compensate for inaccurate clock in GPS receivers Yields much better accuracy and provides 3D fix
Determining Range Receiver and satellite use same code Synchronized code generation Compare incoming code with receiver generated code From satellite Measure time difference between the same part of code From receiver Series of ones  and zeroes repeating every 1023 bits.  So  Complicated alternation of bits that pattern looks random thus called “ pseudorandom code”.
Signal Structure Each satellite transmits its own unique code Two frequencies used L1 Carrier  1575.42 MHz  L2 Carrier  1227.60 MHz Codes CA Code use L1 (civilian code)  P (Y) Code use L1 & L2 (military code)
Three SV ranges known 20,000 Km radius 22,000 Km radius 21,000 Km radius Located at one of these 2 points.  However, one point can easily  be eliminated because it is either  not on earth or moving at impossible rate of speed.
Accurate Timing is the Key SVs have highly accurate atomic clocks Receivers have less accurate clocks Measurements made using “nanoseconds” 1 nanosecond = 1 billionth of a second 1/100 th  of a second error could introduce error of 1,860 miles  Discrepancy between satellite and receiver clocks must be resolved Fourth satellite is required to solve the 4 unknowns (X, Y, Z and receiver clock error)
Satellite Positioning Also required in the equation to solve the 4 unknowns is the actual location of the satellite. SV are in relatively stable orbits and constantly monitored on the ground SV position is broadcast in the “ephemeris” data streamed down to receiver
Sources of Errors Largest source is due to the atmosphere Atmospheric refraction Charged particles Water vapor Ionosphere (Charged Particles) Troposphere
Other Sources of Errors Geometry of satellite positions  Satellite clock errors SV position or “ephemeris” errors Quality of GPS receiver Multi-path errors
Dilution of Precision (DOP) Geometric location of the satellites as seen by the receiver The more spread out the satellites are in the sky, the better the satellite geometry PDOP (position dilution of precision) is a combination of VDOP and HDOP The lower the PDOP value, the better the geometric strength PDOP value less than 6 is recommended
Selective Availability The intentional introduction of errors for civilian users is called  Selective Availability  SA was terminated on May 2, 2000 When SA was on, civilian users accuracy was ~100 meters  Military has capability to degrade signal in certain “theaters of operation” – this is called  “spoofing”
Differential Correction Technique used to correct some of these errors Referred to as “differential GPS” or DGPS In DGPS, two GPS receivers are used One receiver is located at an accurately surveyed point referred to as the “base station” A correction is calculated by comparing the known location to the location determined by the GPS satellites The correction is then applied to the other receiver’s (known as the “rover”) calculated position
DGPS Methods Post-processing  Corrections performed  after the data is collected Special software required  Real-time  Corrections are performed  while the data is being collected Need special equipment to receive the DGPS signal
Wide Area Augmentation System - WAAS New “real-time” DGPS Satellite based  FAA initiative….now fully operational Series of ~25 ground reference stations relay info to master control station Master control station sends correction info to WAAS  satellite http:// gps.faa.gov/programs/waas/howitworks.htm
WAAS Satellites WAAS satellites are  geo-stationary   On east coast, WAAS satellite sits off coast of Brazil over equator at 53.96 ° West (#35 on Garmin) http://www.lyngsat.com/tracker/inmar3f4.shtm On west coast, WAAS satellite sits over Pacific ocean at  178.0° East (#47 on Garmin) http://www.lyngsat.com/tracker/inmar3f3.shtml Ability to get signal deteriorates in northern latitudes (satellite is lower on the horizon) If you can get WAAS satellite signal……..~3 meter accuracy However, cannot always get signal due to obstructions  More WAAS satellites becoming available in future Europeans (EGNOS) Japanese (MSAS)
GPS Accuracy Comparison Some common GPS devices used by FWS: Accuracy given in meters Sub-meter 1-3 ~3 ~ 10 Trimble - GeoXT NA 3 NA ~ 8 - 15 Rockwell – PLGR Federal Users Only 1 - 3 3 ~3 ~ 10 - 15 Garmin GPSMap 76s  Post-process  DGPS Real-time  DGPS WAAS DGPS Autonomous GPS Device
GPS Accuracy Issues  Ways to improve the accuracy of your GPS collected data Standardize data collection methods Establish protocols for your applications Employ averaging techniques Perform mission planning Utilize DGPS  Understand how the selection of datums and coordinate systems affect accuracy GPS data collected in wrong datum can introduce ~200 meters of error into your GIS!
Some issues to consider when purchasing GPS devices What is the accuracy level required for your application?  (10 meters or sub-meter)  How is unit going to be used in field? External antenna required, in heavy canopy, ease of use, durability, data dictionary capability,  waterproof… Cost…… from $100 to $12K Staff expertise..training..support network How well does unit interface with GIS?
Mobile mapping software for WindowsCE devices TerraSync (Trimble) ArcPad (ESRI) Multi-path rejection technology  Trimble GeoXT  Bluetooth Allows for cable free operation Latest Technology
ArcPad Software Bring GIS data into the field! Custom forms for data collection Integrate GPS with GIS
ArcPad Training NCTC 3 day course (TEC7133) Utilize ArcPad Tools for ArcGIS Geodatabase - “check out” & “check in” Design custom forms for data collection Applets & ArcPad Studio Utilize GPSCorrect extension Customize the ArcPad interface  Visit paraswadher.com & wadher.info for more
 

The Gps Technology Paras

  • 1.
    GPS Overview Editthis ex :paras wadher
  • 2.
    What is GPS?Radio-based navigation system developed by DoD Initial operation in 1993 Fully operational in 1995 System is called NAVSTAR NAV igation with S atellite T iming A nd R anging Referred to as GPS Series of 24 satellites, 6 orbital planes, 4 satellite vehicles (SV) on each plane Works anywhere in the world, 24 hours a day, in all weather conditions and provides: Location or positional fix Velocity Direction of travel Accurate time
  • 3.
    Global Navigation SatelliteSystems (GNSS) NAVSTAR USA GLONASS Russians Galileo Europeans
  • 4.
    Trilateration Intersection ofspheres SV Ranging Determining distance from SV Timing Why consistent, accurate clocks are required Positioning Knowing where SV is in space Correction of errors Correcting for ionospheric and tropospheric delays GPS involves 5 Basic Steps
  • 5.
    How GPS works?Range from each satellite calculated range = time delay X speed of light Technique called trilateration is used to determine you position or “fix” Intersection of spheres At least 3 satellites required for 2D fix However, 4 satellites should always be used The 4 th satellite used to compensate for inaccurate clock in GPS receivers Yields much better accuracy and provides 3D fix
  • 6.
    Determining Range Receiverand satellite use same code Synchronized code generation Compare incoming code with receiver generated code From satellite Measure time difference between the same part of code From receiver Series of ones and zeroes repeating every 1023 bits. So Complicated alternation of bits that pattern looks random thus called “ pseudorandom code”.
  • 7.
    Signal Structure Eachsatellite transmits its own unique code Two frequencies used L1 Carrier 1575.42 MHz L2 Carrier 1227.60 MHz Codes CA Code use L1 (civilian code) P (Y) Code use L1 & L2 (military code)
  • 8.
    Three SV rangesknown 20,000 Km radius 22,000 Km radius 21,000 Km radius Located at one of these 2 points. However, one point can easily be eliminated because it is either not on earth or moving at impossible rate of speed.
  • 9.
    Accurate Timing isthe Key SVs have highly accurate atomic clocks Receivers have less accurate clocks Measurements made using “nanoseconds” 1 nanosecond = 1 billionth of a second 1/100 th of a second error could introduce error of 1,860 miles Discrepancy between satellite and receiver clocks must be resolved Fourth satellite is required to solve the 4 unknowns (X, Y, Z and receiver clock error)
  • 10.
    Satellite Positioning Alsorequired in the equation to solve the 4 unknowns is the actual location of the satellite. SV are in relatively stable orbits and constantly monitored on the ground SV position is broadcast in the “ephemeris” data streamed down to receiver
  • 11.
    Sources of ErrorsLargest source is due to the atmosphere Atmospheric refraction Charged particles Water vapor Ionosphere (Charged Particles) Troposphere
  • 12.
    Other Sources ofErrors Geometry of satellite positions Satellite clock errors SV position or “ephemeris” errors Quality of GPS receiver Multi-path errors
  • 13.
    Dilution of Precision(DOP) Geometric location of the satellites as seen by the receiver The more spread out the satellites are in the sky, the better the satellite geometry PDOP (position dilution of precision) is a combination of VDOP and HDOP The lower the PDOP value, the better the geometric strength PDOP value less than 6 is recommended
  • 14.
    Selective Availability Theintentional introduction of errors for civilian users is called Selective Availability SA was terminated on May 2, 2000 When SA was on, civilian users accuracy was ~100 meters Military has capability to degrade signal in certain “theaters of operation” – this is called “spoofing”
  • 15.
    Differential Correction Techniqueused to correct some of these errors Referred to as “differential GPS” or DGPS In DGPS, two GPS receivers are used One receiver is located at an accurately surveyed point referred to as the “base station” A correction is calculated by comparing the known location to the location determined by the GPS satellites The correction is then applied to the other receiver’s (known as the “rover”) calculated position
  • 16.
    DGPS Methods Post-processing Corrections performed after the data is collected Special software required Real-time Corrections are performed while the data is being collected Need special equipment to receive the DGPS signal
  • 17.
    Wide Area AugmentationSystem - WAAS New “real-time” DGPS Satellite based FAA initiative….now fully operational Series of ~25 ground reference stations relay info to master control station Master control station sends correction info to WAAS satellite http:// gps.faa.gov/programs/waas/howitworks.htm
  • 18.
    WAAS Satellites WAASsatellites are geo-stationary On east coast, WAAS satellite sits off coast of Brazil over equator at 53.96 ° West (#35 on Garmin) http://www.lyngsat.com/tracker/inmar3f4.shtm On west coast, WAAS satellite sits over Pacific ocean at 178.0° East (#47 on Garmin) http://www.lyngsat.com/tracker/inmar3f3.shtml Ability to get signal deteriorates in northern latitudes (satellite is lower on the horizon) If you can get WAAS satellite signal……..~3 meter accuracy However, cannot always get signal due to obstructions More WAAS satellites becoming available in future Europeans (EGNOS) Japanese (MSAS)
  • 19.
    GPS Accuracy ComparisonSome common GPS devices used by FWS: Accuracy given in meters Sub-meter 1-3 ~3 ~ 10 Trimble - GeoXT NA 3 NA ~ 8 - 15 Rockwell – PLGR Federal Users Only 1 - 3 3 ~3 ~ 10 - 15 Garmin GPSMap 76s Post-process DGPS Real-time DGPS WAAS DGPS Autonomous GPS Device
  • 20.
    GPS Accuracy Issues Ways to improve the accuracy of your GPS collected data Standardize data collection methods Establish protocols for your applications Employ averaging techniques Perform mission planning Utilize DGPS Understand how the selection of datums and coordinate systems affect accuracy GPS data collected in wrong datum can introduce ~200 meters of error into your GIS!
  • 21.
    Some issues toconsider when purchasing GPS devices What is the accuracy level required for your application? (10 meters or sub-meter) How is unit going to be used in field? External antenna required, in heavy canopy, ease of use, durability, data dictionary capability, waterproof… Cost…… from $100 to $12K Staff expertise..training..support network How well does unit interface with GIS?
  • 22.
    Mobile mapping softwarefor WindowsCE devices TerraSync (Trimble) ArcPad (ESRI) Multi-path rejection technology Trimble GeoXT Bluetooth Allows for cable free operation Latest Technology
  • 23.
    ArcPad Software BringGIS data into the field! Custom forms for data collection Integrate GPS with GIS
  • 24.
    ArcPad Training NCTC3 day course (TEC7133) Utilize ArcPad Tools for ArcGIS Geodatabase - “check out” & “check in” Design custom forms for data collection Applets & ArcPad Studio Utilize GPSCorrect extension Customize the ArcPad interface Visit paraswadher.com & wadher.info for more
  • 25.