Satelite Coomm

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    CONTENTS : Whats mean by satellite ?

    History of Satellites :

    Layer Of Atmosphere :

    Generalized communication system :

    What are the components of a satellite?

    How Satellites Work ?

    How do satellite stay in orbit ?

    Why satellite are launched 36,000 Km from centre of earth ?

    Types of bands :

    Types of orbits :

    Global position system :

    Advantages And Disadvantages Of satellite :

    Uses of satellite :

    References :

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    whats mean by sateLLIte

    Passive Satellites Active satellites

    I. Natural satellites

    II. artificial satellites.

    A passive satellite only

    reflects received signals

    back to earth.

    Ex.moon is a natural

    Active satellites are

    complicated structureshaving a processing

    equipment called

    Transponder .

    An active satellite acts as aREPEATER

    A Satellite is a solid object which revolves around some body due

    to the effect of gravitational forces OR

    a satellite is an object which has been placed into orbit byhuman endeavour.

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    History of Satellites :

    First satellite that was used

    for communication purpose inINDIA was -

    ARYABHATTA (19 April1975)

    The first geostationary

    communication satellite -SYNCOM 3(19 Aug 1963).

    Father of geostationarycommunication satellite is

    -HAROLD ROSEN

    (Aircraft engineer)

    The world's first artificial satellite is the Sputnik 1

    was launched in 1957

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    Layer Of Atmosphere :

    TROPOSPHERE

    STRATOSPHERE

    MESOSPHERE

    THERMOSPHERE

    EXOSPHERE

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    What are the components ofa satellite?

    Many satellites are

    powered by

    rechargeable batteries.

    Small thrusters provide

    attitude i.e. stabilizethe satellite's position

    in space.

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    How Satellites Work :

    I. A Earth Station sendsmessage in GHz range(Uplink).

    II. Satellite Receive andretransmit signalsback. (Downlink)

    III. Difference betweenDownlink and Uplinkfrequency is

    2GHz.

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    Why geostationarysatellite are launched 36,000km from the center of theearth?

    1.Gravitational force=

    attraction between any twoobjects, given by

    2.Centrifugal force=an

    outward-directed force that

    normally balances the inward-

    directed centripital forceThere are two relevant

    forces involved in this problem

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    Equate that 2 eqn=

    i.e.

    The tangential

    velocity of the

    satellite (vs) is

    related to itsorbital period, T

    so,

    Eqating that 2

    eqn=

    As we know

    Then T=? and sqaring

    We know:

    G= 6.67 x 10-11Nm2kg-2

    me= 5.97 x 1024kg

    e= 7.29 x 10-5rad s-1

    Hence, substituting

    the above constants

    into

    gives:

    R = 35,786 km for center of

    earth

    Near about 36,000 km.

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    C-band : C-band is the most

    common frequencyspectrums used by

    todays satellite.

    C-band satellite

    transmissions occupy

    the 4 to 8 GHz

    frequency range.

    C-band antenna is

    approximately 2-3

    meters in diameter

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    Ku-band :

    Ku-band satellitetransmissions occupy the 13 to

    18 GHz frequency range.

    Ku-band antennas can be as

    small as 18 inches in diameter

    These very high frequency

    transmissions mean very small

    wavelengths and very small

    diameter receiving antennas.

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    TYPES OF ORBITSLow-Earth-Orbit LEOs)Medium-Earth-Orbit MEOs)Geostationary GEOs)

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    Low-Earth-Orbit LEO) Altitude (600-1000 KM)

    satellite gives it a better signal

    strength

    Advantages:

    Reduces transmission

    delay

    Disadvantages:

    Smaller coverage area.

    Shorter life span (5-8 yrs.)

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    Little LEOs Applications 0.8 GHz range

    Small, low-cost

    Used for short

    communications.

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    Middle-Earth-Orbiting MEO)MEOs orbits between the altitudes

    of 8,000 - 20,000 km above the earth.

    MEO satellites have a larger

    coverage.

    These orbits are primarily reserved

    for communications satellites that

    cover the North and South Pole.

    MEOs are placed in an elliptical (oval-shaped) orbit.

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    Geosynchronous-Earth-OrbitGEO)

    From the ground level the

    satellite appears fixed.

    GEO satellites have a 24

    hour view of a

    particular area.

    Coverage to 40% of area Of

    planet by this satellite

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    The Global Positioning

    System :

    EQUATORIAL ORBIT :

    POLAR CIRCULAR ORBIT :

    INCLINED ORBIT :

    EACH SATELLITE COVER 40AREASATELLITE MAKES AN ANGLEOF 120 WITH EACH OTHER.

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    ADVANTAGES ANDDISADVANTAGES OF SATELLITEADVANTAGES :

    DISADVANTAGES :

    Make repeatedobservations over a givenarea .

    At a time satellites observe alarger coverage

    Minimum Satellite lifetimeis about 10-15 years.

    Poor spatial resolution in

    the polar regions.

    Launching satellites into

    orbit is costly.

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    Uses of satellite: IT IS USED FOR LONG DISTANCE COMMUNICATION.

    IT IS SPEEDY AND RELIABLE.

    IT IS USED FOR WEATHER FORECASTING.

    (study of atmosphere ,rain ,sunshine at any placeat perticular time)

    IT IS USED FOR TRANSMIT T.V. SIGNAL OVER LARGE DISTANCECOMMUNICATION.

    POLAR SATELLITE IS USED FOR REMOTE SENSING.

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    REFERENCES : http://en.wikipedia.org/wiki/Geosynchronou

    s_satellie

    Geostationary Satellite(Author- Louis

    E.Frenzel)

    (Edition- Third)

    (Publication- Tata McGraw-Hill)

    http://web.mit.edu/invent/iow/rosen.html

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    >>BY SWAPNIL G. THAWARE