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GPS by Akash Adwani

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    PRESENTED BY-Akash Adwani

    2008JE0303

    GLOBAL POSITIONING SYSTEM

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    Presentation OutlineI. Introduction

    II. GPS History

    III. GPS Forms

    IV. Segments

    V. How It Works

    VI.Sources Of Error

    VII.Applications

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    What is GPS?The Global Positioning System (GPS)

    A Constellation of Earth-OrbitingSatellites Maintained by the United

    States Government for the Purpose ofDefining Geographic Positions On andAbove the Surface of the Earth. Itconsists of Three Segments:

    Control Segment

    Space Segment

    User Segment

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    GPS Satellites (Satellite Vehicles(SVs)) First GPS satellite launched in

    1978

    Full constellation achieved in 1994

    Satellites built to last about 10years

    Approximately 2,000 pounds,17

    feet across

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    GPS Lineage Phase 1: 1973-1979

    CONCEPT VALIDATION

    1978- First Launch of Block 1 SV

    Phase 2: 1979-1985

    FULL DEVELOPMENT AND TESTS

    Phase 3: 1985-Present

    PRODUCTION AND DEPLOYMENT

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    Precise Positioning System (PPS) Authorized users ONLY

    U. S. and Allied military

    Requires cryptographicequipment, specially

    equipped receivers

    Accurate to 21 meters 95%of time

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    Standard Positioning Service (SPS) Available to all users

    Accuracy degraded bySelective Availability until 2May 2000 Horizontal Accuracy: 100m

    Now has roughly sameaccuracy as PPS

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    Space Segment 24+ satellites

    6 planes with 55

    inclination Each plane has 4

    satellites

    About 10 satellites are

    visible Constellation has

    spares

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    Space Segment Very high orbit

    20,200 km

    1 revolution inapproximately 12 hrs

    Travel approx. 7,000mph

    Considerations

    Accuracy

    Survivability

    Coverage

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    Control Segment

    Master Control Station

    Monitor Station

    Ground Antenna

    Colorado

    Springs

    Hawaii Ascension

    Islands

    DiegoGarcia

    Kwajalein

    Monitor and Control

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    Control Segment: Maintaining the System

    (5) Monitor Stations

    Correct Orbitand clockerrors Create newnavigation message

    Observeephemerisand clock

    MASTER CONTOLSTATION

    Upload Station

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    User Segment Over $19 Billion invested by DoD

    Dual Use System Since 1985

    (civil & military) Civilian community was quick to take

    advantage of the system Hundreds of receivers on the market

    3 billion in sales, double in 2 years DoD Executive Board sets GPS

    policy

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    How the system worksSpace Segment24+ Satellites

    The CurrentEphemeris is

    Transmitted toUsersMonitor

    Stations Diego Garcia AscensionIsland

    Kwajalein Hawaii ColoradoSprings

    GPS ControlColorado Springs

    EndUser

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    TriangulationSatellite 1 Satellite 2

    Satellite 3 Satellite 4

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    Distance Measuring

    Rate = 186,000 milesper second (Speed of

    Light)

    Time = time it takessignal to travel fromthe SV to GPS receiver

    Distance = Rate xTime

    Each satellite carriesaround four atomicclocks

    Uses the oscillation of cesiumand rubidium atoms tomeasure time

    Accuracy?

    The whole systemrevolves around

    time!!!

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    SV and Receiver Clocks

    SV Clocks 2 Cesium & 2 Rubidium in each SV $100,000-$500,000 each

    Receiver Clocks Clocks similar to quartz watch Always an error between satellite and

    receiver clocks ( t)

    4 satellites required to solve for x, y,z, and t

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    PROBLEM

    Cant use atomic

    clocks in receiver

    SOLUTION

    Receiver clocks

    accurate over shortperiods of time

    Reset often

    4th

    SV used torecalibrate receiverclock

    Cesium Clock =$$$$$$$!!!

    Size of PC

    4

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    Breaking the Code

    Transmission Time

    Receiver

    The Carrier Signal...

    combined with

    The PRN code...

    produces the

    Modulated carrier signalwhich is transmitted...demodulated...

    And detected by receiver,Locked-on, butWith a time delay...

    Time delay

    Satellite

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    Accuracy and Precision in GPS

    Accuracy

    The nearness of a measurement to the

    standard or true value Precision

    The degree to which several

    measurements provide answers very closeto each other.

    What affects accuracy andprecision in GPS?

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    Sources of Error

    Selective Availability

    Intentional degradation of GPSaccuracy

    100m in horizontal and 160m invertical

    Accounted for most error in

    standard GPS Turned off May 2, 2000

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    ESSC 541-542 Lecture 4.14.05

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    Sources of Error

    Geometric Dilution ofPrecision (GDOP)

    Describes sensitivity of receiver tochanges in the geometricpositioning of the SVs

    The higher the DOP value, thepoorer the measurement

    QUALITY DOP

    Very Good 1-3

    Good 4-5

    Fair 6

    Suspect >6

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    Sources of Error

    Clock Error Differences between satellite

    clock and receiver clock

    Ionosphere Delays Delay of GPS signals as they

    pass through the layer ofcharged ions and free electronsknown as the ionosphere.

    Multipath Error Caused by local reflections ofthe GPS signal that mix withthe desired signal

    Dire

    ctSigna

    l

    Refl

    ected

    Sign

    al

    GPSAntenna

    Reflected

    Sign

    al

    Hard Surface

    Satellite

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    Differential GPS Method of removing errors that affect GPS

    measurements

    A base station receiver is set up on a locationwhere the coordinates are known

    Signal time at reference location is compared totime at remote location

    Time difference represents error in satellitessignal

    Post-Processing DGPS involves correcting at alater time

    Referencelocation

    Remotelocation

    = Error

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    Common Applications of GPS

    Military Applications Navigation

    Target Tracking

    Missile and Projectile Guidance Search and rescue

    Civilian Application Local velocity and Orientation

    Research work

    Measuring Earthquakes

    Gps tours

    Map-Making

    Recreational Uses

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    Cont.

    Recreational activities Hiking ,Tracking ,Fishing, Sailing, Treasure hunt,

    car racing and many more

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    Wide Area Augmentation System (WAAS)

    System of satellites and ground stations thatprovide GPS signal corrections

    25 ground reference stations across US

    Master stations create GPS correctionmessage

    Corrected differential message broadcastthrough geostationary satellites to receiver

    5 Times the accuracy (3m) 95% of time

    Only requires WAAS enabled GPS

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    ESSC 541-542 Lecture 4.14.05

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    Geodetic Latitude, Longitude

    Prime Meridian and Equator are referenceplanes used to define latitude and longitude

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    Mobile Mapping

    Integrates GPS technologyand GIS software

    Makes GIS data directlyaccessible in the field

    Can be augmented withwireless technology

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    Mobile Mapping Pros and Cons

    Pros More efficient data entry

    Ready access to GIS data

    Less transcription error

    Possible real-timeupload/download throughwireless

    Cons Cost

    Data storage limit

    Digital data can be

    lost/corrupted

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    Hands on with GPS

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    WORLD SCENARIO Developed by the united states department of defense , GPS is

    officially named NAVSTAR GPS Other satellite navigation system in use or various states of

    development include:

    Beidou-Chinas regional system that China has proposed to expandinto a global system named Compass.

    Galileo-A proposed global system being developed by the EuropeanUnion, joined by China, Israel, India, Morocco, Saudi Arabia, SouthKorea and Ukraine, planned to be operational by 2011-12.

    Glonass-Russias global system which is being restored to to fullavailability in partnership with India.

    Indian regional navigational Satellite System(IRNSS)- Indiasproposed regional system.

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    IRNSS

    The Indian Regional Navigational SatelliteSystem(IRNSS) is an autonomous regional satellitenavigation system being developed by Indian Spaceresearch organization which would be under totalcontrol of Indian Government.

    Development

    The government approved the project in May, 2006,with the intention it be implemented within six toseven years. The first satellite of the proposed

    constellation, developed at a cost of Rupees 1,600crores(1.6 billion rupees) is expected to be launchedin 2009.

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    THANK YOU

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