1

Global Positioning SystemTheory and Practice

Matthew J. Gray

College of Agricultural Sciences and Natural Resources

University of Tennessee-Knoxville

Lecture Outline

• GPS Operation• Trilateration and GPS Errors• Differential Correction• Trimble Planning Software and Topozone.com

Reading Assignment:

1) Chapter 15: pp. 429-433 and 421-429:

• “Using Global Positioning Systems”

• “Using GIS in the Wildlife Profession”

• “Data Documentation”

What is GPS?

Worldwide Space-based Navigation System

•Determine position of all military forces continuously worldwide.

•Accurately deploy nuclear missiles from subs.

Funded, Controlled, and Maintained by

U.S. Department of Defense

Operated by U.S. Air Force

Original Objective

2

Components of GPS

1.

2.

3.

Components of GPS(1: Space Segment)

• 28 satellites in 6 nearly-circular orbits (4-5).• Orbital paths are 20,200 km MSL with a 55o angle of

inclination and 60o horizontal separation (360).• Global coverage 4-10 observable satellites

simultaneously w/ 15o elevational mask.

X 4 345 mihr

vel = ,Circle Earth

Twice Daily

12-hour Orbit Time

Components of GPS(2: Control Segment)

•Master Control Station•5 Monitor Stations

•3 Ground-based Uplink Antennas

Monitor Errors in Satellite Position

& Clocks

Transmit Corrections

3

Components of GPS(3: User)

GPS Receivers

Computes

3-Dimensional Location

3-4 Satellites

GPS Receivers

Five Steps of GPS (3-Dimensional Location)

• Geometric positioning (trilateration) of satellites• Measure satellite-specific distance

• Correct clock errors • Correct ephemeris (orbit) errors

• Correct atmospheric errors Remove

3 SVs

4 SVs

Trilateration: Satellites 1 and 2

(18,000 km)

Located within the Intersection of 2 Spheres

(19,000 km)

We’re somewhere on this sphere

18,000 km

1

4

Trilateration: Satellites 1-4

(18,000 km) (19,000 km)

(20,000 km) Usually Can Reject 1 of 2 Locations; however, 4th Satellite Needed for Time Correction

2 Possible Locations at Intersection of 3 Spheres

(21,000 km)

1

Geometric Configuration of Satellites (Geometric Dilution of Precision)

P Position Dilution of Precision (PDOP)< Horizontal Dilution of Precision (HDOP)< Vertical Dilution of Precision (VDOP)

PDOP < 6

1 per quadrant, >15o Elevation

60o

15o

SatView Demonstration: DOP(http://www.trimble.com/planningsoftware.html)

02/25/99: Lubbock, TX1400-1800 hrs: CDT1400-2300 hrs: CDT

Sample when satellites are positioned optimally!!

Their locations are known.

Free Trimble Software

5

2 Measuring Accurate Time(Atomic vs. Quartz Clocks)

Accuracy: 10-10 seconds(10 nanoseconds)

$100,000 each (4/satellite)

Satellite and Receiver Codes Must beGenerated Simulataneously

Accuracy: 10-3 seconds(300 km error)

$50 each (1/receiver)

4-Channel Receiver

4th Satellite

Receiver Calculates Time Correction andCalibrates Itself to Universal Time

and Perfect Synchrony

Determining Satellite Position(Ephemeris: Satellite Orbit)

3

High Altitude Orbits

Orbit ErrorsP Gravitational Pull (Moon & Sun)P Pressure from Solar Radiation

P Extremely StableP No Atmospheric DragP Maximize Coverage of EarthP Enhance Satellite Survivability

Monitored by Ground Control

& Errors Transmitted

4 Determining Satellite Position(Correcting Orbit Errors)

Monitor StationsGround

Antennas

Master Control P Colorado SpringsP HawaiiP AscensionP Diego GarciaP Kwajalein

P Pseudo-random CodeP Navigation Message

GPS Signal

6

Correcting Atmospheric Delays(Ionospheric and Tropospheric Errors)

5

IonosphereRegion of the atmosphere (50-300 km MSL) containing

ionized particles that reflects radio waves.

Ionospheric errors can be modeled and are incorporated as temporal-specific algorithms in GPS receivers.

Correcting Atmospheric Delays(Ionospheric and Tropospheric Errors)

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TroposphereRegion of the atmosphere (0-20 km MSL) containing water

vapor, various gases, and temperature decrease with altitude.

Errors are minimal; nonetheless, tropospheric errors are modeled with ionospheric errors for “typical” meteorological conditions.

Additional Non-Intentional Errors

Receiver Noise

P Innate Receiver Error (i.e., technological limitations)

Multipath

P Signal Bounce or Reflection (i.e., same signal arrives >1 path)P Signal Rejection Techniquess

Expensive Receivers

7

Government-Induced Error(Selective Availability)

Error intentionally introduced randomly into satellite-specific clock data by the

U.S. Department of DefenseIntention of DOD is to limit accuracy of

non-U.S. military and government users for national security

SA can increase error in location by 20x (100 m)

No Longer Activated!

Differentially Corrected GPS (DGPS)

Real-time DGPSCorrections Transmitted via FM Radio Link

U.S Coast Guard

OmniStar, Inc.

•150 Broadcast Antennas

•FM Receiver & Antenna

•<100 km from Antenna

http://www.omnistar.com/

$300

Not good for mountainous

sites

Roving/Field UnitReceive Same

ErrorsReference/Base Station Unit< 300 km

apart

Differentially Corrected GPS (DGPS)

Post-processing DGPS

X

YZ

X

YZ

Error

Base Station

X

YZ

Rover

PathFinder Office Software

•http://www.rlageosystems.com/dgps.htm

Correction

8

Regional Community Base Stations

PSCC: Pellissippi State CollegeFRKN: Franklin, NC

White = 100 km

Tan = 200 km

Use Pathfinder Software

http://www.ngs.noaa.gov/CORS/cors-data.html

Accuracy and Cost of GPS ReceiversGeoExplorer XM PathFinder Pro XRGarmin Rino

10 m $250

2-5 m $2500

< 1 m $10000

SGPS

DGPS

Ephemeris Ionosphere Troposphere Noise Multipath Clock

2.5 0.60.55 0.3 1.5

3D

10.4

0 0.60.20.4 0.3 0 1.5

Good PDOP! http://users.erols.com/dlwilson/gps.htm

Helpful GPS Websites & ReferencesGPS Overview

http://www.trimble.com

GPS Products

http://www.magellandis.com

Community Base Stations

WAAS Enabled

http://www.garmin.com

Understanding GPS

E. D. Kaplan, editor

Artech House, Inc.

1996

GPS:Theory and PracticeHoffman-Wellenhof,

Lichtenegger, & Collins

Springer-Verlag1997

http://www.ngs.noaa.gov/CORS/Maps.html

http://www.trimble.com/gps/

http://gpsinformation.net/exe/waas.html

(7 m accuracy)