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GLOBAL POSITIONING SYSTEM 
Presented by 
PRANAY MONDAL 
M.Tech. (Communication System Engg.) 
ROLL - 1351015
CONTENTS :- 
 Introduction 
 What is GPS? 
 Basic principal of GPS 
 Information in a GPS signal 
 GPS segments 
 Errors in GPS 
 DGPS 
 GPS application 
 Conclusion
INTRODUCTION :- 
 Radio-based navigation system developed by U.S. Department of 
Defense (DOD) 
 Initial operation in 1993 
 Fully operational Capability in 1995 
 System is called NAVSTAR 
 NAVigation with Satellite Timing And Ranging 
 Referred to as GPS 
 Provides specially coded radio signals that can be processed in a 
GPS receiver. 
– position 
– velocity 
– time
 What is GPS? :- 
• Based on a constellation of about 24 
satellites. 
• Transmit coded radio signals that can be 
processed in a GPS receiver by position, 
velocity and time. 
 The system measures the time delay 
between the signal transmission and 
signal reception of the GPS signal. 
 The signals carry information about 
the satellite’s location. 
 Determines the position of, and 
distance to, at least three satellites, to 
reduce error. 
 The receiver computes position using 
trilateration.
BASIC PRINCIPAL OF GPS :- 
Trilateration :
Trilateration (cont.) :- 
2D & 3D Positioning by Satelites
INFORMATION IN A GPS SIGNAL :- 
The GPS signal contains 2 types of data. 
 Ephemeris data – 
 status of the satellite 
 current date 
 time 
 Almanac data - 
 orbital information for that satellite and for every other 
satellite
GPS SEGMENTS :- 
 Space segment 
 Control Segment 
 User Segment
SPACE SEGMENT :- 
 24 satellites that orbit the 
earth at about 11,000 
nautical miles, once every 
12 hours. 
 Each planes has about 55° 
tilt relative to Earth's 
equator in order to cover 
the polar regions. 
 Each satellite is identified 
by number and broadcasts 
a unique signal.
SPACE SEGMENT (CONT.) :- 
 Satellite Signals-Code-Phasing Ranging 
 Each satellite has a unique no & unique signal. 
 It continuously broadcasts its signal and also sends out a 
time signal every time it starts. 
 The receiver has a copy of each satellite signal and 
determines the distance by recording the time between when 
the satellite says it starts its signal and when the signal 
reaches the receiver.
SPACE SEGMENT (CONT.) :- 
 Satellite Signals-Code-Phasing Ranging (cont.) 
 Distance is calculated using the velocity equation. 
Velocity = Distance/time 
 Rearranging the equation for distance 
Distance= velocity * time 
 If the system knows the velocity of a signal and the 
time it takes for the signal to travel from the sender to 
the receiver, the distance between the sender and the 
receiver can be determined.
CONTROL SEGMENT :- 
The CS consists of 3 entities: 
i) Master Control Station , ii) Monitor Stations , 
iii) Ground Antennas
CONTROL SEGMENT (CONT.) :- 
 Master Control Station : 
 responsible for overall management of the remote monitoring and 
transmission sites. 
 Monitor Stations : 
 Each of the monitor stations checks the exact altitude, position, 
speed, and overall health of the orbiting satellites. 
 uses measurements collected by the monitor stations to predict 
the behavior of each satellite's orbit and clock. 
 The prediction data is up-linked, or transmitted, to the satellites 
for transmission back to the users. 
 ensures that the GPS satellite orbits and clocks remain within 
acceptable limits. 
 Ground Antennas : 
 Ground antennas monitor and track the satellites from horizon 
to horizon. 
 They also transmit correction information to individual 
satellites.
USER SEGMENT :- 
 GPS receivers are generally 
composed of an antenna, tuned to 
the frequencies transmitted by the 
satellites, receiver-processors, and 
a highly-stable clock. 
 They can also include a display 
for showing location and speed 
information to the user.
USER SEGMENT (CONT.) :- 
 GPS receiver has to know two things: 
 The location of atleast three satellites above one’s. 
 The distance between us and each of those satellites 
 A standard GPS receiver can give you several 
information- 
 How far you've travelled (odometer) 
 How long you've been travelling 
 Our current speed (speedometer) 
 Our average speed 
 A "bread crumb" trail showing us 
exactly where we have travelled on 
the map 
 The estimated time of arrival at 
our destination if you maintain 
our current speed.
ERRORS IN GPS :- 
 Selective Availability or SA – 
hamper very precise positioning accuracy 
 Ionosphere and troposphere delays- 
Signal delayed upon going through the ionosphere and 
troposphere. 
 Receiver clock errors – 
the receiver timing references will have some small error. 
 Orbital errors - 
Also known as ‘ephemeris errors’, these are inaccuracies in the 
satellite’s reported position.
ERRORS IN GPS (CONT.) :- 
 Multipath error – can produce large location errors. 
 Signal attenuation - 
Non-restricted GPS signals (1.575 GHz) are blocked by 
steel and concrete structures .
DGPS :- 
 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.
GPS APPLICATIONS :- 
 GPS in the air 
 GPS on land 
 GPS in sea 
 Military Uses for GPS 
 GPS in scientific research 
 Applications for your business 
 Monitor Nuclear Explosions 
 Every Day Life 
 Set Your Watch!
CONCLUSION :- 
 GPS will find more civilian uses 
 The applications using GPS are constantly growing. 
The cost of the receivers is dropping while at the same 
time the accuracy of the system is improving. 
 DOD has promised to eliminate Selective Availability
Global Positing System

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Global Positing System

  • 1. GLOBAL POSITIONING SYSTEM Presented by PRANAY MONDAL M.Tech. (Communication System Engg.) ROLL - 1351015
  • 2. CONTENTS :-  Introduction  What is GPS?  Basic principal of GPS  Information in a GPS signal  GPS segments  Errors in GPS  DGPS  GPS application  Conclusion
  • 3. INTRODUCTION :-  Radio-based navigation system developed by U.S. Department of Defense (DOD)  Initial operation in 1993  Fully operational Capability in 1995  System is called NAVSTAR  NAVigation with Satellite Timing And Ranging  Referred to as GPS  Provides specially coded radio signals that can be processed in a GPS receiver. – position – velocity – time
  • 4.  What is GPS? :- • Based on a constellation of about 24 satellites. • Transmit coded radio signals that can be processed in a GPS receiver by position, velocity and time.  The system measures the time delay between the signal transmission and signal reception of the GPS signal.  The signals carry information about the satellite’s location.  Determines the position of, and distance to, at least three satellites, to reduce error.  The receiver computes position using trilateration.
  • 5. BASIC PRINCIPAL OF GPS :- Trilateration :
  • 6. Trilateration (cont.) :- 2D & 3D Positioning by Satelites
  • 7. INFORMATION IN A GPS SIGNAL :- The GPS signal contains 2 types of data.  Ephemeris data –  status of the satellite  current date  time  Almanac data -  orbital information for that satellite and for every other satellite
  • 8. GPS SEGMENTS :-  Space segment  Control Segment  User Segment
  • 9. SPACE SEGMENT :-  24 satellites that orbit the earth at about 11,000 nautical miles, once every 12 hours.  Each planes has about 55° tilt relative to Earth's equator in order to cover the polar regions.  Each satellite is identified by number and broadcasts a unique signal.
  • 10. SPACE SEGMENT (CONT.) :-  Satellite Signals-Code-Phasing Ranging  Each satellite has a unique no & unique signal.  It continuously broadcasts its signal and also sends out a time signal every time it starts.  The receiver has a copy of each satellite signal and determines the distance by recording the time between when the satellite says it starts its signal and when the signal reaches the receiver.
  • 11. SPACE SEGMENT (CONT.) :-  Satellite Signals-Code-Phasing Ranging (cont.)  Distance is calculated using the velocity equation. Velocity = Distance/time  Rearranging the equation for distance Distance= velocity * time  If the system knows the velocity of a signal and the time it takes for the signal to travel from the sender to the receiver, the distance between the sender and the receiver can be determined.
  • 12. CONTROL SEGMENT :- The CS consists of 3 entities: i) Master Control Station , ii) Monitor Stations , iii) Ground Antennas
  • 13. CONTROL SEGMENT (CONT.) :-  Master Control Station :  responsible for overall management of the remote monitoring and transmission sites.  Monitor Stations :  Each of the monitor stations checks the exact altitude, position, speed, and overall health of the orbiting satellites.  uses measurements collected by the monitor stations to predict the behavior of each satellite's orbit and clock.  The prediction data is up-linked, or transmitted, to the satellites for transmission back to the users.  ensures that the GPS satellite orbits and clocks remain within acceptable limits.  Ground Antennas :  Ground antennas monitor and track the satellites from horizon to horizon.  They also transmit correction information to individual satellites.
  • 14. USER SEGMENT :-  GPS receivers are generally composed of an antenna, tuned to the frequencies transmitted by the satellites, receiver-processors, and a highly-stable clock.  They can also include a display for showing location and speed information to the user.
  • 15. USER SEGMENT (CONT.) :-  GPS receiver has to know two things:  The location of atleast three satellites above one’s.  The distance between us and each of those satellites  A standard GPS receiver can give you several information-  How far you've travelled (odometer)  How long you've been travelling  Our current speed (speedometer)  Our average speed  A "bread crumb" trail showing us exactly where we have travelled on the map  The estimated time of arrival at our destination if you maintain our current speed.
  • 16. ERRORS IN GPS :-  Selective Availability or SA – hamper very precise positioning accuracy  Ionosphere and troposphere delays- Signal delayed upon going through the ionosphere and troposphere.  Receiver clock errors – the receiver timing references will have some small error.  Orbital errors - Also known as ‘ephemeris errors’, these are inaccuracies in the satellite’s reported position.
  • 17. ERRORS IN GPS (CONT.) :-  Multipath error – can produce large location errors.  Signal attenuation - Non-restricted GPS signals (1.575 GHz) are blocked by steel and concrete structures .
  • 18. DGPS :-  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.
  • 19. 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.
  • 20. GPS APPLICATIONS :-  GPS in the air  GPS on land  GPS in sea  Military Uses for GPS  GPS in scientific research  Applications for your business  Monitor Nuclear Explosions  Every Day Life  Set Your Watch!
  • 21. CONCLUSION :-  GPS will find more civilian uses  The applications using GPS are constantly growing. The cost of the receivers is dropping while at the same time the accuracy of the system is improving.  DOD has promised to eliminate Selective Availability