The document provides an overview of the GPS system, including its history from feasibility studies in the 1960s to becoming fully operational in 1995. It describes the three segments that make up the GPS system: the control segment, space segment, and user segment. It also discusses various sources of error in GPS positioning and methods to improve accuracy, such as differential and wide area augmentation systems.

1. Introduction to NAVSTAR GPS Charlie Leonard, 1999 (revised 2001, 2002)

3. How GPS Works

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

5. Control Segment Kwajalein Atoll US Space Command Hawaii Ascension Is. Diego Garcia Cape Canaveral Ground Antenna Master Control Station Monitor Station

6. Space Segment

9. 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”

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

11. What Time is It? 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 ahead of UTC by approximately 13 seconds

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

13. Signals From Two Satellites

14. Three Satellites (2D Positioning)

15. Triangulating Correct Position

16. Three Dimensional (3D) Positioning

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

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

21. Using GPS Receivers for Positioning and Navigation

22. GPS Navigation Terminology 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 Course Made Good (CMG) (CMG) (x º ) Active From Waypoint

23. GPS Navigation: On the Ground Active GOTO Waypoint Location Where GOTO Was Executed Bearing = Course Over Ground (COG) = Cross Track Error (XTE) = 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

26. Planning a Navigation Route Start = Waypoint

27. How A Receiver Sees Your Route

28. GPS Waypoint Circle of Error X

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

31. Ideal Satellite Geometry N S W E

32. Good Satellite Geometry

33. Good Satellite Geometry

34. Poor Satellite Geometry N S W E

35. Poor Satellite Geometry

36. Poor Satellite Geometry

37. Differential GPS

38. Real Time Differential GPS 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 DGPS Site x +30, y +60 x +5, y -3 x -5, y +3 DGPS Receiver Receiver

39. 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.

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

42. How good is WAAS? 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. + - 3 meters +-15 meters