CP0461_19-Apr-2012_RM01 (1)

Embed Size (px)

Citation preview

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    1/43

    GPS Triangulation Procedure

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    2/43

    Triangulation Requirements

    To triangulate, a GPS receiver measures distanceusing the travel time of radio signals.

    To measure travel time, GPS receiver needs very

    accurate timing.

    Along with distance, receiver need accurate dataon where satellites are in space.

    System will also need to correct for any delaysthe signal experiences as it travels throughatmosphere.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    3/43

    Components of GPS System

    Control Segment: five ground stations located onearth.

    Space Segment: satellite constellation (24 activesatellites in space).

    User Segment: GPS receiver units that receivesatellite signals and determine receiver locationfrom them.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    4/43

    Ground Monitor Stations

    Falcon AFB

    Colorado Springs, CO

    Master Control Monitor Station

    Hawaii

    Monitor StationAscension Island

    Monitor Station

    Diego Garcia

    Monitor Station

    Kwajalein

    Monitor Station

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    5/43

    Basic Functions of Monitor Stations

    These stations are the eyes and ears of GPS,monitoring satellites as they pass overhead bymeasuring distances to them every 1.5 seconds

    This data is then smoothed using ionosphericand meteorological information and sent toMaster Control Station at Colorado Springs.

    The ionospheric and meteorological data isneeded to get more accurate delaymeasurements, which in turn improve locationestimation.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    6/43

    Functions of Monitor Stations (Contd)

    Master control station estimates parametersdescribing satellites' orbit and clockperformance,. It also assesses health status of

    the satellites and determines if any re-positioningmay be required.

    This information is then returned to three uplink

    stations (collocated at the Ascension Island,Diego Garcia and Kwajalein monitor stations)which transmit the information to satellites.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    7/43

    Space Segment

    Space segment is the satellite constellation.

    24 satellites with a minimum of 21 operating

    98% of the time 6 Orbital planes

    Circular orbits

    20-200 km above the Earth's surface

    11 hours 58 minute orbital period Visible for approximately 5 hours above the

    horizon

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    8/43

    GPS Satellite Orbits

    We can obtain updates of GPS satellites at

    http://www.ngs.noaa.gov/GPS/GPS.html

    http://www.ngs.noaa.gov/GPS/GPS.htmlhttp://www.ngs.noaa.gov/GPS/GPS.html
  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    9/43

    GPS Satellite Orbits (Contd)

    Orbits of GPS satellites need to be updatedevery once in a while because orbit does notstay circular without adjustments.

    Adjustments needed because: Other objects exert gravitational force on each

    satellite (e.g. sun, moon) Effect of gravity is non-uniform during orbit.

    Radiation pressure (due to solar radiation). Atmospheric drag Other effects

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    10/43

    Interesting Aside on GPS Orbits

    When GPS satellites are decommissioned,

    they are placed on a disposal orbit (outside

    the operating GPS orbit).

    Some studies show that satellites in disposal

    orbits can eventually, perhaps over 20-40

    years, encroach into operating constellation.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    11/43

    Aside (Contd)

    This is because disposal orbits, while circularinitially, become increasingly elliptical, mostlyas result of sun-moon gravitational

    perturbations.

    Besides intersecting GPS constellation, these

    satellites eventually could pose a threat tooperational satellites in low Earth andgeosynchronous orbits

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    12/43

    Aside (Contd)

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    13/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    14/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    15/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    16/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    17/43

    Third Component of GPS: User

    Segment

    User segment comprises receivers that have beendesigned to decode signals transmitted fromsatellites for purposes of determining position,

    velocity or time.

    Receiver must perform the following tasks:

    select one or more satellites in view

    acquire GPS signals

    measure and track signal

    recover navigational data

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    18/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    19/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    20/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    21/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    22/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    23/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    24/43

    Synchronizing Clocks

    In order to make this measurement, the

    receiver and satellite both need clocks that

    can be synchronized down to the nanosecond.

    Accurate time measurements are required. If

    we are off by a thousandth of a second, at the

    speed of light, that translates into almost 200

    miles of error.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    25/43

    Synchronizing Clocks (Contd)

    To make a satellite positioning system using onlysynchronized clocks, you would need to haveatomic clocks not only on all the satellites, butalso in the receiver itself.

    But atomic clocks cost somewhere between$50,000 and $100,000, which makes them a just abit too expensive for everyday consumer use.

    The Global Positioning System has a clever,

    solution to this problem. Every satellite containsan expensive atomic clock, but the receiver itselfuses an ordinary quartz clock, which it constantlyresets.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    26/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    27/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    28/43

    Synchronizing Clocks (Contd)

    The receiver can easily calculate the necessary

    adjustment that will cause the four spheres to

    intersect at one point.

    Based on this, it resets its clock to be in sync

    with the satellite's atomic clock.

    The receiver does this constantly whenever

    it's on, which means it is nearly as accurate as

    the ex ensive atomic clocks in the satellites.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    29/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    30/43

    Knowing Satellite Locations

    In order to properly synchronize clocks and

    figure out which PRC signal to listen to, the

    receiver has to know where the satellites

    actually are.

    This isn't particularly difficult because the

    satellites travel in very high and predictableorbits.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    31/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    32/43

    2 Types of Errors

    Errors can be categorized as intentional andunintentional.

    Intentional errors: government can and doesdegrade accuracy of GPS measurements. Thisis done to prevent hostile forces from usingGPS to full accuracy.

    Policy of inserting inaccuracies in GPS signalsis called Selective Ability (SA). SA was singlebiggest source of inaccuracy in GPS. SA was

    deactivated in 2000.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    33/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    34/43

    Typical Errors

    Source of Error Typical Error in Meters

    (per satellite)

    Satellite Clocks 1.5

    Orbit Errors 2.5

    Ionosphere 5.0

    Troposphere 0.5

    Receiver Noise 0.3Multipath 0.6

    SA 30

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    35/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    36/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    37/43

    Using GPS Data

    A GPS receiver essentially determines the receiver'sposition on Earth.

    Once the receiver makes this calculation, it can tell youthe latitude, longitude and altitude of its current

    position. To make thenavigation more user-

    friendly, most receivers

    plug this raw data into

    map files stored inmemory.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    38/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    39/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    40/43

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    41/43

    Using GPS Data (Contd)

    You can use maps stored in the receiver's memory,

    connect the receiver to a computer that can holdmore detailed maps in its memory, or

    simply buy a detailed map of your area and find yourway using the receiver's latitude and longitudereadouts.

    Some receivers let you download detailed mapsinto memory or supply detailed maps with plug-in map cartridges.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    42/43

    Using GPS Data (Contd)

    A standard GPS receiver will not only place youon a map at any particular location, but will alsotrace your path across a map as you move.

    If you leave your receiver on, it can stay inconstant communication with GPS satellites to

    see how your location is changing.

    This is what happens in cars equipped with GPS.

  • 7/29/2019 CP0461_19-Apr-2012_RM01 (1)

    43/43