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PRESENTED BY-Akash Adwani
2008JE0303
GLOBAL POSITIONING SYSTEM
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Presentation OutlineI. Introduction
II. GPS History
III. GPS Forms
IV. Segments
V. How It Works
VI.Sources Of Error
VII.Applications
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What is GPS?The Global Positioning System (GPS)
A Constellation of Earth-OrbitingSatellites Maintained by the United
States Government for the Purpose ofDefining Geographic Positions On andAbove the Surface of the Earth. Itconsists of Three Segments:
Control Segment
Space Segment
User Segment
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GPS Satellites (Satellite Vehicles(SVs)) First GPS satellite launched in
1978
Full constellation achieved in 1994
Satellites built to last about 10years
Approximately 2,000 pounds,17
feet across
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GPS Lineage Phase 1: 1973-1979
CONCEPT VALIDATION
1978- First Launch of Block 1 SV
Phase 2: 1979-1985
FULL DEVELOPMENT AND TESTS
Phase 3: 1985-Present
PRODUCTION AND DEPLOYMENT
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Precise Positioning System (PPS) Authorized users ONLY
U. S. and Allied military
Requires cryptographicequipment, specially
equipped receivers
Accurate to 21 meters 95%of time
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Standard Positioning Service (SPS) Available to all users
Accuracy degraded bySelective Availability until 2May 2000 Horizontal Accuracy: 100m
Now has roughly sameaccuracy as PPS
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Space Segment 24+ satellites
6 planes with 55
inclination Each plane has 4
satellites
About 10 satellites are
visible Constellation has
spares
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Space Segment Very high orbit
20,200 km
1 revolution inapproximately 12 hrs
Travel approx. 7,000mph
Considerations
Accuracy
Survivability
Coverage
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Control Segment
Master Control Station
Monitor Station
Ground Antenna
Colorado
Springs
Hawaii Ascension
Islands
DiegoGarcia
Kwajalein
Monitor and Control
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Control Segment: Maintaining the System
(5) Monitor Stations
Correct Orbitand clockerrors Create newnavigation message
Observeephemerisand clock
MASTER CONTOLSTATION
Upload Station
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User Segment Over $19 Billion invested by DoD
Dual Use System Since 1985
(civil & military) Civilian community was quick to take
advantage of the system Hundreds of receivers on the market
3 billion in sales, double in 2 years DoD Executive Board sets GPS
policy
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How the system worksSpace Segment24+ Satellites
The CurrentEphemeris is
Transmitted toUsersMonitor
Stations Diego Garcia AscensionIsland
Kwajalein Hawaii ColoradoSprings
GPS ControlColorado Springs
EndUser
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TriangulationSatellite 1 Satellite 2
Satellite 3 Satellite 4
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Distance Measuring
Rate = 186,000 milesper second (Speed of
Light)
Time = time it takessignal to travel fromthe SV to GPS receiver
Distance = Rate xTime
Each satellite carriesaround four atomicclocks
Uses the oscillation of cesiumand rubidium atoms tomeasure time
Accuracy?
The whole systemrevolves around
time!!!
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SV and Receiver Clocks
SV Clocks 2 Cesium & 2 Rubidium in each SV $100,000-$500,000 each
Receiver Clocks Clocks similar to quartz watch Always an error between satellite and
receiver clocks ( t)
4 satellites required to solve for x, y,z, and t
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PROBLEM
Cant use atomic
clocks in receiver
SOLUTION
Receiver clocks
accurate over shortperiods of time
Reset often
4th
SV used torecalibrate receiverclock
Cesium Clock =$$$$$$$!!!
Size of PC
4
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Breaking the Code
Transmission Time
Receiver
The Carrier Signal...
combined with
The PRN code...
produces the
Modulated carrier signalwhich is transmitted...demodulated...
And detected by receiver,Locked-on, butWith a time delay...
Time delay
Satellite
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Accuracy and Precision in GPS
Accuracy
The nearness of a measurement to the
standard or true value Precision
The degree to which several
measurements provide answers very closeto each other.
What affects accuracy andprecision in GPS?
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Sources of Error
Selective Availability
Intentional degradation of GPSaccuracy
100m in horizontal and 160m invertical
Accounted for most error in
standard GPS Turned off May 2, 2000
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ESSC 541-542 Lecture 4.14.05
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Sources of Error
Geometric Dilution ofPrecision (GDOP)
Describes sensitivity of receiver tochanges in the geometricpositioning of the SVs
The higher the DOP value, thepoorer the measurement
QUALITY DOP
Very Good 1-3
Good 4-5
Fair 6
Suspect >6
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Sources of Error
Clock Error Differences between satellite
clock and receiver clock
Ionosphere Delays Delay of GPS signals as they
pass through the layer ofcharged ions and free electronsknown as the ionosphere.
Multipath Error Caused by local reflections ofthe GPS signal that mix withthe desired signal
Dire
ctSigna
l
Refl
ected
Sign
al
GPSAntenna
Reflected
Sign
al
Hard Surface
Satellite
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Differential GPS Method of removing errors that affect GPS
measurements
A base station receiver is set up on a locationwhere the coordinates are known
Signal time at reference location is compared totime at remote location
Time difference represents error in satellitessignal
Post-Processing DGPS involves correcting at alater time
Referencelocation
Remotelocation
= Error
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Common Applications of GPS
Military Applications Navigation
Target Tracking
Missile and Projectile Guidance Search and rescue
Civilian Application Local velocity and Orientation
Research work
Measuring Earthquakes
Gps tours
Map-Making
Recreational Uses
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Cont.
Recreational activities Hiking ,Tracking ,Fishing, Sailing, Treasure hunt,
car racing and many more
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Wide Area Augmentation System (WAAS)
System of satellites and ground stations thatprovide GPS signal corrections
25 ground reference stations across US
Master stations create GPS correctionmessage
Corrected differential message broadcastthrough geostationary satellites to receiver
5 Times the accuracy (3m) 95% of time
Only requires WAAS enabled GPS
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ESSC 541-542 Lecture 4.14.05
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Geodetic Latitude, Longitude
Prime Meridian and Equator are referenceplanes used to define latitude and longitude
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Mobile Mapping
Integrates GPS technologyand GIS software
Makes GIS data directlyaccessible in the field
Can be augmented withwireless technology
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Mobile Mapping Pros and Cons
Pros More efficient data entry
Ready access to GIS data
Less transcription error
Possible real-timeupload/download throughwireless
Cons Cost
Data storage limit
Digital data can be
lost/corrupted
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Hands on with GPS
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WORLD SCENARIO Developed by the united states department of defense , GPS is
officially named NAVSTAR GPS Other satellite navigation system in use or various states of
development include:
Beidou-Chinas regional system that China has proposed to expandinto a global system named Compass.
Galileo-A proposed global system being developed by the EuropeanUnion, joined by China, Israel, India, Morocco, Saudi Arabia, SouthKorea and Ukraine, planned to be operational by 2011-12.
Glonass-Russias global system which is being restored to to fullavailability in partnership with India.
Indian regional navigational Satellite System(IRNSS)- Indiasproposed regional system.
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IRNSS
The Indian Regional Navigational SatelliteSystem(IRNSS) is an autonomous regional satellitenavigation system being developed by Indian Spaceresearch organization which would be under totalcontrol of Indian Government.
Development
The government approved the project in May, 2006,with the intention it be implemented within six toseven years. The first satellite of the proposed
constellation, developed at a cost of Rupees 1,600crores(1.6 billion rupees) is expected to be launchedin 2009.
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THANK YOU
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