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    Globalpositioning system

    ABSTRACT

    The Global Positioning System is a navigation system developed

    by United states Department of Defense. Earlier time it was developed

    for military uses only. Nowadays it is open for common people also.

    Navigation in Global Positioning System is done with the help of

    satellites. A total of 32 satellites are now on service.

    Besides the military uses GPS service can be used for lost and stolen

    things recovery, root mapping etc. Other nations are also trying to build

    up their on satellite navigation systems IRNSS of India is a proposed

    project on satellite navigation system.

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    Globalpositioning system

    ACKNOWLEDGEMENT

    The constant encouragement of all sources has gone a long way in the

    accomplishment of this seminar. It is our pleasant duty to thank all those

    who have been helpful in various ways towards successful completion of

    this seminar. This seminar was completed in due time as we were

    constantly supported by our teachers and friends.

    I wish to express my deep sense of acknowledgement and

    respect to my guide Mr. Syed Aftab Ahmed , lecturer, Department of

    IS&E and Mrs. Sunitha G P , Asst. professor, for their encouragement

    throughout the completion of our seminar. I am very much grateful toour respected HOD Dr.S N Jagadeesha for his encouragement.

    I sincerely thank the whole teaching and non-teaching staff of

    Information Science and Engineering department.

    MANOJ KUMAR

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    CONTENTS

    1 Before GPS.1

    2 Introduction to GPS3

    3 Technical Description5

    4 How GPS Works 8

    5 Accuracy and Error Sources.13

    6 Application15

    Conclusion

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    Refererence

    1. BEFORE GPS:

    For thousands of years, speed to a walking pace and

    landmark were used to find locations. At sea, early navigators limited

    their voyages to coastal routes to avoid becoming lost. New methods for

    determining position arose as trade between distant ports increased.

    Polaris, the North Star, was used to determine north-south distance

    (latitude) in the hemisphere. But mariners also had to find latitude when

    sailing in the southern hemisphere, and they lacked a method for

    determining east-west position (longitude). The solution, celestial

    navigation, required accurate time. In the late 18th century this led to the

    development of the marine chronometer, an accurate sea-going

    timepiece. Beginning in the 19th century the U.S Naval Observatory, the

    nations official timekeeper, provided accurate time for navigators from

    an array of chronometers.

    1. a. Electronic Innovations:

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    Electronic navigation introduced all-weather capability,

    ease of use, and eventually, increased accuracy. In the 1930s radio

    beacons were used to provide bearings from airfields.

    During World War II radio navigation system were developed, the

    best-known being LORAN, or LONG RANGE AID TONAVIGATION. Positions were determined by the timing of signals

    received from different LORAN transmitter stations. In the 1960s the

    OMEGA SYSTEM provided worldwide electronic navigation coverage

    for the first time.

    In the mid- 1960s the U.S Navys Navigation system (NAVSAT), also

    known as TRANSIT, was developed to provide positions for ships and

    submarine.

    1.b. TRANSITE

    Satellite:

    Fig 1: The first

    Electronic navigation

    TRANSIT Satellite

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    TRANSIT was the first operational satellite positioning system. Six

    satellites gave worldwide coverage every 90 minutes and provided

    positions that were accurate to within 200 meters (660 feet). Position

    Were obtained by measuring the Doppler shift of the satellite signal.

    TRANSIT was effective, but it was limited by low accuracy and lack of

    24-hour availability. The TRANSIT system operated until 1996.

    2. INTRODUCTION TO GPS:

    The Global Positioning System (GPS) is the only fully

    functional Global Navigation Satellite System (GNSS). The GPS uses a

    constellation of at least 24 (32 by March 2008) Medium Earth Orbit

    satellites that transmit precise microwave signals, that enable GPS

    receivers to determine their location, speed, direction, and time. GPS

    was developed by the United States Department of Defense. Its official

    name is NAVSTAR-GPS. Although NAVSTAR-GPS is not an

    acronym, a few acronyms have been created for it. The GPS satellite

    constellation is managed by the United States Air Force 50th space wing.

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    Similar satellite navigation systems include the Russian GLONASS

    (incomplete as of 2008), the upcoming European Galileo positioning

    system, the proposed COMPASS navigation system of China, and

    IRNSS of India. Following the shooting down of Korean Air Lines

    Flight 007 in 1983, President Ronald Reagan issued a directive making

    the system available 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, scientific uses,

    and hobbies such as geocaching. GPS also provides a precise time

    reference used in many applications including scientific study of

    Earthquakes and synchronization of telecommunications network.

    A GPS receiver calculates its position by carefully timing the

    signals sent by the constellation of GPS satellites high above the Earth.

    Each satellite continually transmits messages containing the time the

    message was sent, a precise orbit for the satellite sending the message

    (the ephemeris), and the general system health and rough orbits of allGPS satellites (the almanac). These signals travel at the speed of light

    through outer space, and slightly slower through the atmosphere. The

    receiver uses the arrival time of each message to measure the distance to

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    each satellite, from which it determines the position of the receiver using

    geometry and trigonometry. The resulting coordinates are converted to

    more user-friendly forms such as latitude and longitude, or location on a

    map, and then displayed to the user.

    It might seem that three satellites would be enough to

    solve for a position, since space has three dimensions. However, a three

    satellite solution requires the time be known to a nanosecond or so, far

    better than any non-laboratory clock can provide. Using four or more

    satellites allows the receiver to solve for time as well as geographical

    position, eliminating the need for a super accurate clock. In other words,the receiver uses four measurements to solve for four variables: x, y, z,

    and t. While many GPS applications have no particular use for the

    computed time, it is used in some GPS applications such as time

    transfer.

    3. TECHNICAL DESCRIPTION

    The Global Positioning System consists of 3 segments:

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    Space Segment: It is a constellation of 24 satellites, which orbit the

    earth every 12 hours.

    Control Segment: The Control Segment comprises a series of

    monitoring stations at different locations around

    the world, with the master control facility located

    at Schriever Air Force Base in Colorado USA.

    User Segment: The User Segment is made up of all the GPS

    receivers in the worlds aircraft, ships, cars, and

    handheld units.

    3. a. Space Segment:

    The space segment comprises the orbiting GPS satellites or

    Space Vehicles in GPS parlance. The GPS design originally called for

    24 SVs, eight each in three circular orbital planes but this was modified

    to six planes with four satellites each. The orbital planes are centered on

    the Earth, not rotating with respect to the distant stars. The six planes

    have approximately 55 inclination (tilt relative to Earth's equator) and

    are separated by 60 right ascension of the ascending node. (angle along

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    the equator from a reference point to the orbit's intersection). The orbits

    are arranged so that at least six satellites are always within line of sight

    from almost everywhere on Earth's surface.

    Fig 2: Orbital planes indicating constellations

    Orbiting at an altitude of approximately 20,200 kilometers

    (12,600 miles or 10,900 nautical miles; orbital radius of 26,600 km

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    (16,500 mi or 14,400 NM)), each SV makes two complete orbits each

    sidereal day.The ground track of each satellite therefore repeats each

    (sidereal) day. This was very helpful during development, since even

    with just four satellites, correct alignment means all four are visible from

    one spot for a few hours each day. For military operations, the ground

    track repeats can be used to ensure good coverage in combat zones.

    As of September 2007, there are 31 actively broadcasting satellites

    in the GPS constellation. The additional satellites improve the precision

    of GPS receiver calculations by providing redundant measurements.

    With the increased number of satellites, the constellation was changed to

    a no uniform arrangement. Such an arrangement was shown to improve

    reliability and availability of the system, relative to a uniform system,

    when multiple satellites fail.

    3. b. Control segment:

    The flight paths of the satellites are tracked by US Air Force

    monitoring stations in Hawaii, Kwajalein, Ascension Island, Diego

    Garcia, and Colorado Springs, Colorado, along with monitor stations

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    operated by the National Geospatial-Intelligence Agency (NGA). The

    tracking information is sent to the Air Force Space Commands master

    control station at Schriever Air Force Base in Colorado Springs, which

    is operated by the 2nd Space Operations Squadron (2 SOPS) of the

    United States Air Force (USAF). Then 2 SOPS contacts each GPS

    satellite regularly with a navigational update (using the ground antennas

    at Ascension Island, Diego Garcia, Kwajalein, and Colorado Springs).

    These updates synchronize the atomic clocks on board the satellites to

    within a few nanoseconds of each other, and adjust the ephemeris of

    each satellite's internal orbital model. The updates are created by a

    Kalman filter which uses inputs from the ground monitoring stations,

    space weather information and various other inputs.

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    Fig 3: GPS Master Control and Monitor Station Network

    3. c. User Segment:

    The GPS User Segment consists of the GPS receiver and the

    user community.

    GPS receiver converts SV (satellite vehicle) signals into position,

    velocity, and time estimates. Four satellites are required to compute the

    four dimensions of X, Y, Z (position) and time.

    GPS receivers are used for navigation, positioning, time dissemination,

    and other research. The receiver must perform the following task:

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    Selecting one or more satellite in view

    Acquiring GPS signals

    Recovering navigational data

    Measuring and tracking

    Fig 4: GPS Receivers (User Segment)

    4. HOW GPS WORKS:

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    As weve said, the complete GPS space system includes 24

    satellites, 11,000 nautical (speed unit) miles above the Earth, which take

    12 hours each to go around the earth once (one orbit). They are

    positioned so that we can receive signals from six of them nearly 100

    percent of the time at any point on earth. You need that many signals to

    Get the best position information. Satellites are equipped with very

    precise clocks that keep accurate time to within three nanoseconds-thats

    0.000000003, or three billionths, of a second. This precision timing is

    important because the receiver must determine exactly how long it takes

    for signals to travel from each GPS satellite. The receiver uses this

    information to calculate its position.

    The principle behind GPS is the measurement of distance

    (or range) between the receiver and the satellites. The satellites also

    tell us exactly where they are in their orbits above the earth. It works

    something like this: If we know our exact distance from a satellite in

    space, we know we are somewhere on the surface of an imaginary

    sphere with radius equal to the distance to the satellite radius. If we

    know our exact distance from two satellites, we know that we are

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    located somewhere on the line where two spheres intersect.

    Fig 5: Two sphere surface intersecting in a circle

    And, if we take a third measurement, there are only two possible points

    where we could be located. One of these is usually impossible, and the

    GPS receivers have mathematical methods of eliminating the impossible

    location.

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    Fig 6: surface of sphere intersecting a circle at two points

    Trilateration is used to determine the two points of intersection of three

    sphere surfaces corresponding to three satellites. The surface of thesphere corresponding to the fourth satellite or the surface of the earth is

    used to determine which of the two intersections provides a valid

    estimate of GPS receiver position.

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    4. a. Positioning with GPS:

    There are essentially two broad categories of GPS

    positioning which can be described as a real-time navigation and high

    precision carrier phase positioning. Navigation uses a minimum of

    four pesudorange measurements to four satellites, which are used to

    solve for the three-dimensional coordinates of the receiver and the clock

    offset between the receiver and the clock offset between the receiver

    oscillator and GPS system time.

    Carrier phase observations are used to compute baselines

    between two locations. Since the two carriers have short wavelength (19

    and 24 cm for L1 and L2 respectively), they cannot be used in the same

    manner as the pseudo range. Positions are determined by intersecting

    distances between the GPS satellites and the receiver.

    Traditionally, the technique is called trilateration.

    Distances between the GPS satellites and the receiver are not measured

    directly and therefore must be derived.

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    5. Accuracy and error sources:

    Sources of User Equivalent Range Errors (UERE)

    Source Effect

    Ionospheric effect 5 m

    Ephemeris errors 2.5 m

    Satellite clock errors 2 m

    Multipath distortion 1 m

    Tropospheric effects 0.5 m

    Numerical errors 1 m

    Table 1.1: Error sources

    The position calculated by a GPS receiver requires the

    current time, the position of the satellite and the measured delay of the

    received signal. The position accuracy is primarily dependent on the

    satellite position and signal delay.

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    5.1 Atmospheric effects:

    Inconsistencies of atmospheric conditions affect the speed of

    the GPS signals as they pass through the Earth's atmosphere, especially

    the ionosphere. Correcting these errors is a significant challenge to

    improving GPS position accuracy. These effects are smallest when the

    satellite is directly overhead and become greater for satellites nearer the

    horizon since the path through the atmosphere is longer (see air mass).

    Once the receiver's approximate location is known, a mathematical

    model can be used to estimate and compensate for these errors.

    5.2 Multipath effects:

    GPS signals can also be affected by multi path issues,

    where the radio signals reflect off surrounding terrain; buildings, canyon

    walls, hard ground, etc. These delayed signals can cause inaccuracy. A

    variety of techniques, most notably narrow correlate spacing, have been

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    developed to mitigate multipath errors. For long delay multipath, the

    receiver itself can recognize the wayward signal and discard it.

    To address shorter delay multipath from the signal reflecting off the

    ground, specialized antennas (e.g. a choke ring antenna) may be used to

    reduce the signal power as received by the antenna. Short delayreflections are harder to filter out because they interfere with the true

    signal, causing effects almost indistinguishable from routine fluctuations

    in atmospheric delay.Multipath effects are much less severe in moving

    vehicles. When the GPS antenna is moving, the false solutions using

    reflected signals quickly fail to converge and only the direct signals

    result in stable solutions.

    5.3 Ephemeris and clock errors:

    While the ephemeris data is transmitted every 30 seconds,

    the information itself may be up to two hours old. Data up to four hours

    old is considered valid for calculating positions, but may not indicate the

    satellites actual position. If a fast TTFF is needed, it is possible to upload

    valid ephemeris to a receiver, and in addition to setting the time, a

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    position fix can be obtained in under ten seconds. It is feasible to put

    such ephemeris data on the web so it can be loaded into mobile GPS

    devices.

    The satellite's atomic clocks experience noise and clock drift errors. The

    navigation message contains corrections for these errors and estimates of

    the accuracy of the atomic clock. However, they are based on

    observations and may not indicate the clock's current state. These

    problems tend to be very small, but may add up to a few meters (10s of

    feet) of inaccuracy.

    6. Applications

    The Global Positioning System, while originally a military project is

    considered a dual-use technology, meaning it has significant

    applications for both the military and the civilian industry.

    6.1 Military:

    The military applications of GPS span many purposes: -

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    Navigation: GPS allows soldiers to find objectives in the dark or in

    unfamiliar territory, and to coordinate the movement of troops and

    supplies. The GPS-receivers commanders and soldiers use are

    respectively called the Commanders Digital Assistant and the Soldier

    Digital Assistant.

    Target tracking: Various military weapons systems use GPS to track

    potential ground and air targets before they are flagged as hostile. These

    weapon systems pass GPS co-ordinates of targets to precision-guided

    munitions to allow them to engage the targets accurately.

    Missile and projectile guidance: GPS allows accurate targeting of

    various military weapons including cruise missiles and precision-guided

    munitions. Artillery projectiles with embedded GPS receivers able to

    withstand accelerations of 12,000G have been developed for use in 155

    mm howitzers.

    Search and Rescue: Downed pilots can be located faster if they

    have a GPS receiver.

    Reconnaissance and Map Creation:The military use GPS

    extensively to aid mapping and reconnaissance.

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    6.2 Civilian:

    Many civilian applications benefit from GPS signals,

    using one or more of three basic components of the GPS: absolute

    location, relative movement, and time transfer.

    The ability to determine the receiver's absolute location allows GPSreceivers to perform as a surveying tool or as an aid to navigation. The

    capacity to determine relative movement enables a receiver to calculate

    local velocity and orientation, useful in vessels or observations of the

    Earth.

    GPS functionality has now started to move into mobile phones en masse.

    The first handsets with integrated GPS were launched already in the late

    1990s, and were available for broader consumer availability on

    networks.

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    7. CONCLUSION

    GPS continues to perform as the world's premier space-based

    positioning, navigation, and timing service. Endeavors such as mapping,

    aerial refueling, rendezvous operations, geodetic surveying, and search

    and rescue operations have all benefited greatly from GPS's accuracy.

    GPS capabilities are integrated into nearly all facets of US military

    operations. GPS receivers are incorporated into nearly every type of

    system used by aircraft, spacecraft, ground vehicles and ships. In

    addition, GPS-guided munitions have showcased their increased

    accuracy in recent conflicts with unprecedented precision, thus

    improving military capability while decreasing the number of weapons

    required achieving military objectives.

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    REFERENCES

    [1].Steven R. Strom. "Charting a Course Toward Global Navigation".

    The Aerospace Corporation.2002.

    [2].Noe, P.S.; Myers, K.A. "A Position Fixing Algorithm for the Low-

    Cost GPS Receiver".IEEE Transactions on Aerospace and Electronic

    Systems, 2006.

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