Iridium Satellite Systems

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    by,

    B.Amala

    H.Phanindra

    CVSR college of engineering.

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    The Iridium System is asatellite-based, wirelesspersonal communicationsnetwork to permit a wide range

    of mobile telephone servicesincluding voice, data andnetworking.

    Each satellite is cross-linked tofour other satellites; two

    satellites in the same orbitalplane and two in an adjacentplane.

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    Each satellite is equippedwith 3 L-band antennasforming a honeycombpattern that consists of 48

    individual spot beams witha total of 1628 cells aimeddirectly below the satellite.

    Each cell has 174 fullduplex voice channels for atotal of 283,272 channelsworldwide.

    3

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    o The polar constellation isformed by 6 orbital planeswith 11 satellites per plane.

    o The orbital planes are co-axial at the polar axis,separated from each other

    at an angle of nearly 30degrees.o Iridium uses 66 operational

    satellites configured at aattitude of 780km(spare at648) above the earth in sixnearly polar orbital times of

    100 min 28 sec

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    5

    66

    Ope

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    Iridium basedCommunicatio

    n unit

    Existingaircraft

    communication systems

    iridiumgatew

    ay

    PSTN

    phone

    Aircraft cockpit communication system

    Air to Ground-Voice:

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    Iridium basedCommunicatio

    n unit

    Existingaircraft

    communication systems

    iridiumgatew

    ay

    Iridium basedCommunicatio

    n unit

    Existingaircraft

    communication systems

    callsetup

    Aircraft cockpit communication system Aircraft cockpit communication system

    Air to Air-Voice:

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    The space segment which includes theLEO satellites and related control facilities.

    System control segment

    Gateway segmentThe subscriber segment (phones and

    pagers) which provide mobile access to thesatellite system and terrestrial wireless

    systems.

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    Three Principal Elements Of SV:

    Payload Provides All Command, Control and Communications FunctionsMain Mission Antennas (MMAs) Provide L-Band Telephony Functions Bus Platform For SV Operations, Provides Power, Pointing, Propulsion

    9

    Solar Array Panels (2)

    Battery &Radiator

    Ka-Band Cross-Link Antenna (4)

    Ka-Band FeederLink Antenna (4)

    L-BandMMA (3)

    PayloadElectroncis

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    The frequency bands are as follows: L-band subscriber to satellite voice

    links=1.616GHZ to 1.6265GHZ

    Ka-band gateway downlinks=19.4 GHZ to

    19.6GHZ. Ka-band gateway up-links=29.1GHZ to

    29.3GHZ

    Ka-band inter-satellite cross-links

    =23.18GHZ to23.38GHZ

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    Using satellite cross links is the unique key to theiridium system and the primary differentiationbetween iridium and the traditional satellite bentpipe system where all transmissions follow a pathfrom earth to satellite to earth.

    Iridium is the first mobile satellite to incorporatesophisticated, onboard digital processing on eachsatellite.

    Entire global coverage by a single wirelessnetwork systems.

    With this system the subscriber will never listen amessage called OUT OF COVERAGE AREA

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    Less reliance on wire-line networksContinuous talk timeFewer outagesDont need to be in the in the same footprint as the gatewa

    High risk associated with designing, building, and launchingsatellites.

    High cost for the terrestrial-based networking and interfaceinfrastructure.

    low power, dual mode transceivers are more cumbersome aexpensive

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    Commercial point of view: Availability of services and early subscriber take-up will

    be the key to survival for operators. Lower infrastructure costs will further help in early break-

    even and profitability for network operators.

    Economic point of view: Since the satellites has already been launched it is

    important that this system is applied as much as

    possible. Innovative Applications like seismic alert ofearthquakes and tsunami should be brought.

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