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The Global
Positioning System (GPS) is the only fully functional
Global Navigation Satellite System (GNSS). Utilizing a
constellation of at least 24 Medium Earth Orbit
satellites that transmit precise microwave signals, the
system enables a GPS receiver to determine its location,
speed, direction, and time. Other similar systems are
the Russian GLONASS (incomplete as of 2007), the
upcoming European Galileo positioning system, the
proposed COMPASS navigation system of China, and IRNSS
of India.
Developed by the United States Department of Defense,
GPS is officially named NAVSTAR GPS (Contrary to popular
belief, NAVSTAR is not an acronym, but simply a name
given by John Walsh, a key decision maker when it came
to the budget for the GPS program). The satellite
constellation is managed by the United States Air Force
50th Space Wing. The cost of maintaining the system is
approximately US$750 million per year, including the
replacement of aging satellites, and research and
development.
Following the shootdown of Korean Air Lines Flight 007
in 1983, President Ronald Reagan issued a directive
making the system available for free for civilian use as
a common good. Since then, GPS has become a widely used
aid to navigation worldwide, and a useful tool for
map-making, land surveying, commerce, and scientific
uses. GPS also provides a precise time reference used in
many applications including scientific study of
earthquakes, and synchronization of telecommunications
networks.
A typical
GPS receiver calculates its position using the signals
from four or more GPS satellites. Four satellites are
needed since the process needs a very accurate local
time, more accurate than any normal clock can provide,
so the receiver internally solves for time as well as
position. In other words, the receiver uses four
measurements to solve for 4 variables - x, y, z, and t.
These values are then turned into more user-friendly
forms, such as latitude/longitude or location on a map,
then displayed to the user.
Each GPS satellite has an atomic clock, and continually
transmits messages containing the current time at the
start of the message, parameters to calculate the
location of the satellite (the ephemeris), and the
general system health (the almanac). The signals travel
at a known speed - the speed of light through outer
space, and slightly slower through the atmosphere. The
receiver uses the arrival time to compute the distance
to each satellite, from which it determines the position
of the receiver using geometry and trigonometry.
Although
four satellites are required for normal operation, fewer
may be needed in some special cases. For example, if one
variable is already known (for example, a sea-going ship
knows its altitude is 0), a receiver can determine its
position using only three satellites. Also, in practice,
receivers use additional clues (doppler shift of
satellite signals, last known position, dead reckoning,
inertial navigation, and so on) to give degraded answers
when fewer than four satellites are visible.
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