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GROUP MEMBERS Rajnish Kumar Jha & Rishabh Gandhi B.Tech 2 nd Year , 4 th Semester Computer Science “B”
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Page 1: Gps ppt

GROUP MEMBERS

Rajnish Kumar Jha

&Rishabh Gandhi

B.Tech 2nd Year , 4th SemesterComputer Science “B”

Page 2: Gps ppt
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G LOBALPS

OSITIONINGYSTEM

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WHAT IS GPS?• Satellite based

navigation system.

• Based on a constellation of about 24 satellites

• Developed by the United States Department of Defense (DOD)

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WHAT IS GPS?

• Can provide accurate positioning 24 hours a day, anywhere in the world.

• No subscription fees or setup charges to use GPS.

• GPS satellites also called NAVSTAR, the official U.S. DOD name for GPS

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STRUCTURE

Space Segment Control Segment

User Segment

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HOW GPS DETERMINES A LOCATION

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HOW GPS DETERMINES A LOCATIONThings which need to be determined: • Current Locations of GPS Satellites

• The Distance Between Receiver’s Position and the GPS Satellites

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CURRENT LOCATIONS OF GPS SATELLITES

• GPS satellites are orbiting the earth at an altitude of 11,000 miles.

• The orbits, and the locations of the satellites, are known in advance.

• GPS receivers store this orbit information for all of the GPS satellites in an ALMANAC*.

* THE ALMANAC IS A FILE WHICH CONTAINS POSITIONAL INFORMATION FOR ALL OF THE GPS SATELLITES

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• All 24 satellites are divided into 6 parts.

• There are 4 satellites in each part.

• A definite orbit is defined for each part.

• Each of these 3,000- to 4,000-pound solar-powered satellites.

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DISTANCE BETWEEN RECEIVER’S POSITION & THE GPS SATELLITES• By measuring the amount of time taken by

radio signal (the GPS signal) to travel from the satellite to the receiver.

• Radio waves travel at the speed of light, i.e. about 186,000 miles per second.

• The distance from the satellite to the receiver can be determined by the formula “distance = speed x time”.

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GPS ERROR BUDGET

Different errors can cause a deviation of +/- 50 -100 meters from the actual GPS receiver position which are :

ATMOSPHERIC CONDITIONS:

• Speed of GPS signal is affected by ionosphere & troposphere.

• Which cause a deviation of 0 to 30 m. from the actual position of receiver.

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EPHEMERIS ERRORS:

• The predicted changes in the orbit of a satellite.

• Which cause a deviation of 0 to 5 m. from the actual position of receiver

CLOCK DRIFT:

• Due to different code generations in satellite and receiver simultaneously.

• Which cause a deviation of 0 to 1.5 m. from the actual position of receiver

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MULTIPATH:

• Bouncing of GPS signal due to a reflecting surface before reaching to receiver antenna.

• Which cause a deviation of 0 to 1 m. from the actual position of receiver

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MEASURING GPS ACCURACY

The geometry of the constellation is evaluated by Dilution Of Precision, or DOP.

DOP

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INCREASING ACCURACY OF GPS

• Differential correction provides accuracy within 1-5 m.

• Coarse Acquisition receiver provides accuracy within 1-5m.

• Carrier Phase receivers provides accuracy within 10-30 cm.

• Dual-Frequency receivers are capable of providing sub-centimeter GPS position accuracy.

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APPLICATIONS

AVIATION AGRICULTURE

MARINE TIMING

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SPACE RAILWAYS

ROADWAYS DISASTER RELIEF

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Name Launch Date

NAVSTAR 64 (USA 206) August 17, 2009

NAVSTAR 63 (USA 203) March 24, 2009

NAVSTAR 62 (USA 201) March 15, 2008

NAVSTAR 61 (USA 199) December 20, 2007

NAVSTAR 60 (USA 196) October 17, 2007

NAVSTAR 59 (USA 192) November 17, 2006

NAVSTAR 58 (USA 190) September 25, 2006

NAVSTAR 57 (USA 183) September 26, 2005

NAVSTAR 56 (USA 180) November 6, 2004

NAVSTAR 55 (USA 178) June 23, 2004

NAVSTAR 54 (USA 177) March 20, 2004

NAVSTAR 53 (USA 175) December 21, 2003

NAVSTAR 52 (USA 168) March 31, 2003

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ANY QUESTIONS ?