GPS

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GPS:
Global Positioning System
Our next utility
How do we know where we are?
 Line
of sight
 Celestial Navigation
 LORAN
 DECCA
 Sat-Nav
What is GPS?

Developed by the Dept. of Defense
 $12 billion system
 Began construction in mid ’70s
 Developed for military operations, but with a
provision for civilian use
 Consists of 24 (28) high orbit satellites
sending out coded radio signals that are
picked up by receivers that calculate position
How does GPS work?

GPS is based on satellite ranging
 24+ satellites orbit 11,000 miles overhead
 Each satellite orbits the earth once every 12
hours
 Four satellites are required by the receiver for
an exact position
 Usually with 5 to 8 SVs visible at any time

(SVs= Space Vehicles)
Precision timing

Each satellite is equipped with an atomic
clock, accurate timing is key
 Receiver clocks don’t have to be perfect
because a trigonometry trick can cancel out
receiver clock errors
 In reality 3 satellites can give a position
(narrows it down to 2 points and the
erroneous point is discarded)
 The fourth satellite allows for correction of the
receiver’s clock
Knowing where the satellites are is key
 Satellites
have predictable orbits
 Minor variations in their orbits occur
 Base stations monitor satellite atomic
clocks and position
 Corrections are broadcast from the
satellites
GPS Satellites

NAVSTAR (NAVigation Satellite Timing And Ranging)
 Rockwell International
 Orbit is 10,900 nautical miles above Earth
 Satellites weigh 1900 lbs
 17 ft with solar panels extended
 12 hour orbital period
 Orbital plane is 55* to equatorial plane
 Six orbital planes with 4 SVs in each plane
 Life span 7.5 years
 24+ satellites at any given time (only 17 are
required)
Measuring the distance from a
satellite

Speed of light x time = distance
 Radio waves are electromagnetic waves, like
light, and travel at 186,000 miles per second
 A satellite overhead will transmit its signal to
us in 6/100ths of a second
 Most receivers measure in nanoseconds
(0.000000001 second)
 All satellites generate the same “psuedorandom” code every second
 These codes are compared by the receiver to
calculate position
GPS Errors (typical)

Satellite clock error
2 feet
 Ephemeris error
2 feet
 Receiver error
4 feet
 Atmospheric delay
12 feet
 Selective Availability (if on) 25 feet
 Multipath errors and obstructions*

Multiply by Geometric Dilution of Precision
 Error = 60 to 100 feet in most cases, up to
350 with selective availability implemented
Selective Availability

Turned off May 1, 2000
 Limits civilian accuracy while allowing military
to use GPS full potential
 Alters satellite’s atomic clocks according to a
specific code
 However the “civilians” got around this quickly
with Differential GPS
 Can get accuracy of less than a meter with
inexpensive equipment
 Specialized receivers can get within a
centimeter
So why have Selective Availability?
[It’s turned off now]

It was turned off during the Persian Gulf War
and the invasion of Haiti because the military
did not have enough classified equipment to
go around and bought off the shelf GPS units
by mail order.
 The Russians have their own GPS and it is
not encoded
 So why bother with selective availability when
it cost us millions of taxpayers money?
 Because the DOD is dithering on Earth and in
space
Differential GPS

A receiver placed at a known location
calculates the combined error in the satellite
range data
 That correction can be applied to all other
receivers in the same locale, to eliminate
virtually all error in their measurements.
 This can be done in “real time” or by “postprocessing” the data after collection
Selecting a GPS

Do you need an occasional position fix or
accurate steering?
 Do you need accurate velocity measurements?
 Is economy more important than accuracy?
 Is power consumption an important factor?
 Is size and weight a factor?
 Will the receiver operate in high dynamic
conditions (ex. open ocean)?

Two broad groups of receivers are those that
can track four or more satellites simultaneously
and those that sequence between satellites.
Satellite Health
Good GPS receivers will carry an “Almanac”
that they download from the satellites
 This means the GPS receiver is programmed
to know where in the sky each satellite will be
at a given moment
 An addition to the psuedo-random code each
satellite broadcast a “data message”
indicating the satellite’s health and will also
broadcast minor corrections.

GeoExplorer III
 12
Channels
 Post processing and real-time
differential collection
 Stores an Almanac
 Capable of receiving “Carrier Signals”
GeoExplorer II by Trimble
[The GeoExplorer III’s are simplier]
There are five GeoExplorer II settings:
 Logging
Interval
 Position Mode
 Elevation Mask
 Signal-To-Noise Ratio
 Position Dilution of Precision (PDOP)
Logging Interval

Logging interval defines the frequency at
which a position is stored.
 Point features – Set a 1 second
 Line/Area features – should match the base
station logging interval. Logging intervals
may also depend on speed of travel:


If walking – 5 seconds
If driving – 1 second
Position Mode
For the best accuracy with GEII avoid 2D
data collection
 Manual 2D: you must enter the altitude
value
 Auto 2D/3D: uses 3D unless only 3 SVs
available than 2D is collected
 Manual 3D: uses 4+ SVs
 Overdetmined 3D: uses 5+ SVs
Elevation Mask

Elevation masks restrict your receiver to
using only those satellites above a certain
elevation in the sky.
 This ensures that a base station can always
see all the satellites used by the rover.
 The default elevation mask for a rover is 15*
 Lowing masks increase # of satellites,
increases atmospheric delay and increases
effects of multipath.
Signal to Noise Ratio Mask
 As
the proportion between the signal
and the noise decreases, data is
distorted by the noise.
 The higher the value of the SNR, the
better.
 Quality is degraded if it falls below 6.0
 Typical SNRs range between 10 and 25
Position Dilution of Precision (PDOP)

Is a value that indicates when the satellite
geometry can provide the most accurate
results.
 The wider the angle between satellites the
better the measurement.
 It measures satellite’s location relative to
other satellites.
 A low PDOP, such as 3, indicates a higher
probability of accuracy, a high value of 7,
indicates a lower probability of accuracy.
Vertical Error

Depending on satellite geometry the vertical
error can be up to 3 times the horizontal error.
 It is difficult to calculate because SVs have a
limited perspective in which to measure
height.
 If the receiver could use signals form
underneath it would be much better but the
Earth blocks that
Autonomous GEII operation
 No
differential applied
 Errors now seem to be about 5 to 10
meters with atmospheric delay causing
the largest errors.
 In the past Selective Availability caused
the largest error.
 SA error can be up to 100 meters in the
horizontal and 156 meters in the vertical
Postprocessed Differential

Done with Pathfinder Office software
 You need 2 receivers to correct data
 One that operates as a base station at a
known location
 One that operates as a rover and collects
data at the same time as the base station
 The correction factor is applied to the rover
 Accuracy is 2-5 meters in the horizontal
Real-time Differential
 GPS
receiver is linked to the base
station by radio and corrections are
continuously broadcast
 Additional equipment is needed
 Can be less accurate than postprocessing but usually not by more than
5 meters
High Accuracy
In addition to determining a satellite’s range
by measuring code, the GEII can measure
carrier waves between the satellite and the
receiver.
 The carrier wave is a much finer measuring
tool
 High accuracy requires more rigorous data
collection
 Only point features can by collect in this
mode, best to collect data for 10 minutes
 Accuracies are submeter, will not work on the
water.

Where next?

Weather forecasting (atmospheric moisture)
 GPS in rental cars
 Land planes
 Emergency medical services
 Science
 Lead the blind
 Commercial applications far outnumber the
military
 Annual GPS services are worth about $1
billion in the US
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