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View File - University of Engineering and Technology, Taxila

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e lf cf lghh 0kk ek slmm km snn cn chn ppðxÞpðyÞpðxj yÞqrr br cr rt dt et pt svw saa HbDD aDf chDf ueElectrical losses <strong>of</strong> solar cellsIncoming signal frequencyLocal oscillator frequencyAcceleration due to gravity at the surface <strong>of</strong> the earthNumber <strong>of</strong> octets in the headerAltitude above the subsatellite point on the earth terminalBoltzmann’s constantConstant used to emphasise the type <strong>of</strong> apertureSolar constantNumber <strong>of</strong> accesses or usersReference burstsLength <strong>of</strong> shift registerSatellite massBlock lengthNumber <strong>of</strong> cells in a designated radio cell areaNumber <strong>of</strong> radio channels in a cellNumber <strong>of</strong> bursts, accesses, or traffic stations to the frameProbability <strong>of</strong> xProbability <strong>of</strong> yProbability <strong>of</strong> transmitting x given that y was receivedLength <strong>of</strong> burst errorsRadius distance focus to the orbit pathInput digital bit rate <strong>of</strong> the user (bit=sec)Average radius <strong>of</strong> a radio cellRain rateTransmission delay between an earth terminal <strong>and</strong> satelliteRotation period <strong>of</strong> the earthAmount <strong>of</strong> time an earth station is required to communicate withan orbiting satellite as it passes overheadOrbit periodVelocity <strong>of</strong> the satellite with respect to the atmosphereSwath widthApex angle for global coverageMagnetic heading <strong>of</strong> the antennaState probabilityDifference in longitude between the earth station <strong>and</strong> the satelliteDeviation angle between true North <strong>and</strong> North magnetic polesTotal b<strong>and</strong>width assigned to the serviceB<strong>and</strong>width allocated to each userError vectorCopyright © 2002 by Marcel Dekker, Inc. All Rights Reserved.

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