Bodey Beat
Transcript of Bodey Beat
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INTRODUCTION
The Russians kept the Doppler-effect in mind with
the launch of Sputnik I in 1957 .To keep radio
contact with a moving object, you have to
keep changing your frequency.
The Americans discovered how to invert this in 1959
with the start of the TRANSIT navigation
system.(Navy Navigational satellite system). If youknow the position of the satellite, you can
determine your relative position to it
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The Transit navigation system could only stay
for 2 years after it conception because it had
its limitations. Listed below are few of itslimitations.
Low orbit + few satellites = bad coverage
Receiver needs a continuous signal
Receiver has to wait for satellite to pass
overhead
Only up to 500/25 meter accuracy
Assumes sea level altitude
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NAVSTAR GPS(navigation satellite and
timing and ranging)
The concept of Navistar was to improve the
inaccuracies of transit navigation system.
Concept
Six orbital planes
(plane = orbit containing multiple satellites)
21 active satellites, plus 3 sparesFour per plane
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How it works
A receiver receives a signal from a GPS
satellite
It calculates the difference from the current
time and the time sent by the satellite
It now knows how far away the satellite is
Because we know that radio signals travel atthe speed of light, we can calculate this
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How it works(cont)
There are two possible locations
One is practically impossible, so it can be ruled
out
Too far away from Earth (too high)
Velocity is not realistic
Still, we need a fourth satellite
Confirm this location
Improve accuracy
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NAVSTAR GPS
Accuracy improved with the forth satellite
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THE GPS
The Global positioning system is a marvel of
satellites, a system of supporting ground
stations and coded radio transmissions all to
do one simple thing, tell you exactly where
you are. It was designed, built, operated and
maintained by Department of Defense which
serves the initial purpose of trackingsubmarines carrying nuclear missiles.
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THE GPS (CONT)
The development of the GPS first came about
in the year 1973 with the first four satellites
launched in 1978.However full operational
capacity was reached on 17 July 1995 which
cost the U.S Defense about 12 million dollars.
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HOW GPS WORKS
The GPS receivers collect the signals transmittedfrom the system of 31 satellites. The GPS worksunder five(5) conditions;
Satellite triangulation set basis of the system
Satellites ranging measures distance from asatellite
Satellite positioning locate where a satellite is inspace
Correcting errors does correction forionosphere and troposphere delays
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COMPONENTS OF GPS
The GPS comprises of three (3) segments.
The space segment
The ground segment(the ground controllednetwork)
The user segment(GPS receivers and their
users)
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GPS SPACE SEGMENT
GPS Constellation 31 satellites (Space Vehicles or SVs)
With three on standby
20,200km altitude (12 hour orbitperiod)
6 orbital planes (55
inclination) 4 satellites in each plane
GPS Satellite Details Manufactured by Rockwell
International, later by LockheedM&S
7000 miles per hour 2.2m body, 7m with solar panels
Average of 21 years expectedlifetime
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GPS CONTROL SEGMENT
The control segment consist of five
monitoring stations
Diego Garcia
Ascension Island
Hawaii
Kwajalein Island andColorado
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GPS CONTROL SEGMENT(CONT)
The control segment performs three main
tasks
Monitoring the health of the satellites
Determine their orbits and the behavior of
their atomic clocks
Inject the broadcast message into the
satellites
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GPS USER SEGMENT
The user segment consist ofthe user and all earth basedGPS receivers. The typicalreceiver is composed of,
Antenna Preamplifier
Radio signal microprocessor
Control and display device
Data recording unit and Power supply
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GPS RECEIVER RF FRONT END
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GPS SIGNAL
GPS SIGNAL
C/A code and P(Y) code
All SVs transmit at1575.42MHz
Each SV modulates using aunique 1023-bitpseudorandom (PRN) codesent at 1.023Mcps (chips persecond)
PRN allows spread-spectrumCDMA management of GPStransmit frequency
Receivers distance to the SVcan be determined bymeasuring the PRN time skew
between the transmitted andreceived signals
GPS system data (ephemeris,clock, and atmosphericparameters) are transmittedby further modulating the PRN
code at 50bps
1023 chips (1ms)
PRN
cod
e
PRN PRN PRN PRN PRN
0
01 10 0Data
Bits*
50bps (20ms/bit)
*PRN code inverts to signify bit transition (0/1)
1 chip
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ERRORS IN GPS
Errors in GPS takes place because of the
following reasons
Atmospheric delays
Satellite clock
Orbital
Multipath andReceiver measurement noise
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ERROR CORRECTION
DGPS is Differential GPS is used to correct thevarious inaccuracies in the GPS system, pushingits inaccuracies ever further.
Error is reduced by determining the error at aknown location, then subtracting that error fromthe solution at an unknown location.
DGPS consist of two receivers,
Stationary and a
Moving around making position measurements.
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GPS APPLICATIONS
GPS can be applied in the following areas:Agriculture
Marine
AviationRoad and Highways
Environment
Rail
Surveying and Mapping
Public Safety and Disaster Relief
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LIMITATION OF GPS
Solar activities can distort the GPS signals asthey pass through the earths ionospherecausing accuracy error.
The solar storm that occurred in early March2012 disrupted satellite communication andforce airline to reroute some flights.
More solar storm are likely to occur through2013-2014 as the sun reaches its solar maxperiod.
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RECOMMENDATION
We recommend that Africa should come up
with its own system for the interest of the
continent.
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CONCLUSION
Programs such as Earthscope is planning to
inculcate GPS to help understand why earth
quake and volcanic eruption occurs.
The GPS is without doubt the most successful
dual use(civilian and military) system
developed by US.
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REFERENCES
http://www.gpsy.com/gpsinfo/
Robert Sweet, GPS for mariners,
International Marine Publishing co., 2nd
Edition.
Alison.M.Smith,Law Enforcement use of GPS
device to monitor motor vehicle,
congressional research service, February 28,
2011.
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REFRENCES (CONT)
WWW.gps.gov/applications/
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THANK YOU
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