1. Field Methods in Geospatial Science I: GPS and GIS tools (BOT 4810/5810, Section 200)

2. Introduction to Global Positioning System Segments of the GPS how does GPS works Problems with the GPS Advancements in the GPSOverview Part 1: Global Positing System Part 2: GIS Integration Hardware and Software Integration of GPS data with GIS systems

3. The History of GPS1973Decision to develop a satellite navigation system 1974 - 1979 System tests 1977First receiver tests. Transmitters are installed on the earth’s surface called Pseudolites (Pseudo satellites) 1978 - 1985 A total of 11 Block I satellites are launched in this period. 1979Decision to expand the GPS system. At first only 18 satellites should be operated. 1980Launching of the first Block I satellite carrying sensors to detect atomic explosions. 1982The critical financial, usefulness of the system is questioned again and again by the sponsors. 1983decided to allow the civilian use of the GPS system. 1986Delta rockets intended for the transportation in the first place. 1989The first Block II satellite was installed and activated. 1991 Temporal deactivation of the selective availability (SA) during the Gulf war. On July 01, 1991 SA is activated again. 1993 The Initial Operational Capability (IOC) is announced. In the same year it is also definitely decided to authorize the world wide civilian use free of charge. 1994The last Block II satellite completes the satellite constellation. 1995Full Operational Capability (FOC) is announced. 2000 Final deactivation of the selective availability and therefore improvement of the accuracy for civilian users from about 100 m to 20 m. 2004Launching of the 50 st GPS satellite. 2005 Launch of the first IIR-M GPS-satellite. This new type supports the new military M-signal and the second civil signal L2C. 2007mainframe-based Ground Segment Control System was transitioned to the new Architecture Evolution Plan 2008The most recent launch was on March 15, 2008, Transition of GPS Fleet to Upgraded Control System

4. 24+ satellites 20,200 km altitude 55 degrees inclination 12 hour orbital period 5 ground control stations Each satellite passes over a ground monitoring station every 12 hours How Does GPS Work ?

5. GPS satellite in orbit

6. Control Segment Space Segment User Segment Monitor Stations Ground Antennas Master Station Three Segments of the GPS

7. Space Segment

8. Kwajalein Atoll US Space Command Control SegmentHawaii Ascension Is. Diego Garcia Cape Canaveral Ground Antenna Master Control Station Monitor Station

9.  Military.  Search and rescue.  Disaster relief.  Surveying.  Marine, aeronautical and terrestrial navigation.  Remote controlled vehicle and robot guidance.  Satellite positioning and tracking.  Shipping.  Geographic Information Systems (GIS).  Recreation. User Segment

10.  Position and coordinates.  The distance and direction between any two waypoints, or a position and a waypoint.  Travel progress reports.  Accurate time measurement. Four Primary Functions of GPS

11. Position is Based on Time T + 3 Distance between satellite and receiver = “3 times the speed of light” T Signal leaves satellite at time “T” Signal is picked up by the receiver at time “T + 3”

12. Pseudo Random Noise Code Receiver PRN Satellite PRN Time Difference

13. What Time is it Anyway? Zulu Time Military Time (local time on a 24 hour clock) Universal Coordinated Time Greenwich Mean Time Local Time: AM and PM (adjusted for local time zone) GPS Time - 13* * GPS Time is currently ahead of UTC by 13 seconds.

14. Signal From One Satellite The receiver is somewhere on this sphere.

15. Signals From Two Satellites

16. Three Satellites (2D Positioning)

17. Triangulating Correct Position

18. Three Dimensional (3D) Positioning

19. Selective Availability (S/A)  The Defense Department dithered the satellite time message, reducing position accuracy to some GPS users.  S/A was designed to prevent America’s enemies from using GPS against us and our allies.  In May 2000 the Pentagon reduced S/A to zero meters error.  S/A could be reactivated at any time by the Pentagon.

21. Sources of GPS Error Standard Positioning Service (SPS ): Civilian Users SourceAmount of Error  Satellite clocks:1.5 to 3.6 meters  Orbital errors:< 1 meter  Ionosphere:5.0 to 7.0 meters  Troposphere:0.5 to 0.7 meters  Receiver noise:0.3 to 1.5 meters  Multipath:0.6 to 1.2 meters  Selective Availability(see notes)  User error:Up to a kilometer or more Errors are cumulative and increased by PDOP.

22. Sources of Signal Interference Earth’s Atmosphere Solid Structures Metal Electro-magnetic Fields

23. Receiver Errors are Cumulative! User error = +- 1 km System and other flaws = < 9 meters

24. Using GPS Receivers for Positioning and Navigation

25. XTE (CDI) N (000 0 ) (0 0 ) N Desired Track (DTK) (x º ) Active Leg Distance to Waypoint Bearing (X 0 ) Present Location Speed Over Ground (SOG) Tracking (TRK) (x º ) Active GOTO Waypoint GPS Navigation Terminology Course Made Good (CMG) (CMG) (x º ) Active From Waypoint

26. Active GOTO Waypoint Bearing = Course Over Ground (COG) = Cross Track Error (XTE) = Location Where GOTO Was Executed Bearing = 65 0 COG = 5 0 XTE = 1/2 mi. Bearing = 78 0 COG = 350 0 XTE = 1/3 mi. Bearing = 40 0 COG = 104 0 XTE = 1/4 mi. Active Leg N GPS Navigation: On the Ground

27. Position Fix  A position is based on real-time satellite tracking.  It’s defined by a set of coordinates.  It has no name.  A position represents only an approximation of the receiver’s true location.  A position is not static. It changes constantly as the GPS receiver moves (or wanders due to random errors).  A receiver must be in 2D or 3D mode (at least 3 or 4 satellites acquired) in order to provide a position fix.  3D mode dramatically improves position accuracy.

28. Waypoint  A waypoint is based on coordinates entered into a GPS receiver’s memory.  It can be either a saved position fix, or user entered coordinates.  It can be created for any remote point on earth.  It must have a receiver designated code or number, or a user supplied name.  Once entered and saved, a waypoint remains unchanged in the receiver’s memory until edited or deleted.

29. Planning a Navigation Route Start = Waypoints

30. How A Receiver “Sees” Your Route Yellow stars: where you want to go. Green stars: where the GPS receiver may take you. Blue circles: the potential circle of GPS error at each waypoint.

31. GPS Waypoint Circle of Error X

32. GPS Dilution of Precision and Its Affects On GPS Accuracy

33. GPS Satellite Geometry  Satellite geometry can affect the quality of GPS signals and accuracy of receiver trilateration.  Dilution of Precision (DOP) reflects each satellite’s position relative to the other satellites being accessed by a receiver.  There are five distinct kinds of DOP.  Position Dilution of Precision (PDOP) is the DOP value used most commonly in GPS to determine the quality of a receiver’s position.  It’s usually up to the GPS receiver to pick satellites which provide the best position triangulation.  More advanced GPS receivers can filter out poor DOP values.

34. Ideal Satellite Geometry N S W E

35. Good Satellite Geometry

36. Poor Satellite Geometry N S W E

38. Differential GPS  Realtime  Post process

39. DGPS Site x+30, y+60 x+5, y-3 True coordinates = x+0, y+0 Correction = x-5, y+3 DGPS correction = x+(30-5) and y+(60+3) True coordinates = x+25, y+63 x-5, y+3 Real Time Differential GPS DGPS Receiver Receiver

40. USCG NDGPS Ground Stations National Differential Global Positioning System Yellow areas show overlap between NDGPS stations. Green areas are little to no coverage. Topography may also limit some areas of coverage depicted here.

41. USCG NDGPS Ground Stations National Differential Global Positioning System Yellow areas show overlap between NDGPS stations. Green areas are little to no coverage. Topography may also limit some areas of coverage depicted here.

42. Wide Area Augmentation System Geostationary WAAS satellites GPS Constellation WAAS Control Station (West Coast) Local Area System (LAAS) WAAS Control Station (East Coast)

43. How good is WAAS? + - 3 meters +-15 meters With Selective Availability set to zero, and under ideal conditions, a GPS receiver without WAAS can achieve fifteen meter accuracy most of the time.* Under ideal conditions a WAAS equipped GPS receiver can achieve three meter accuracy 95% of the time.* * Precision depends on good satellite geometry, open sky view, and no user induced errors.

44. Accuracy of +/- 10 m (30 ft) error (horizontal) +/- 15 m (45 ft) error (vertical) Your location is: xx o xx.xxx’ N xx o xx.xxx’ W Instantaneous positioning with GPS

45. High-precision GPS  N D -Use the carrier phase, not pseudorange -Dual-frequency receivers ( to remove ionosphere ) -High-precision orbital information -Good monuments -Multiple stations ( to remove satellite clock variations ) -Sophisticated processing software -Collect lots of data

46. Timing Roads & Highways Space Aviation Agriculture Marine Rail Environment Public Safety & Disaster Relief Surveying & Mapping Recreation GPS Applications

47. Further Reading Elementary http://www8.garmin.com/gpsacademy/ http://www8.garmin.com/gpsacademy/ http://www.trimble.com/gps/index.html Novice http://www.colorado.edu/geography/gcraft/notes/gps/gps_f.html Expert http://www.gmat.unsw.edu.au/snap/gps/gps_survey/principles_gps.htm Source materials: Wikipedia, Charlie Leonard, IIRS….

48. Part 2: GIS Integration Hardware and Software Integration of GPS data with GIS systems