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how to create barcode in ssrs report [BO]i in Software
[BO]i QR Code 2d Barcode Reader In None Using Barcode Control SDK for Software Control to generate, create, read, scan barcode image in Software applications. Encoding QR Code In None Using Barcode creation for Software Control to generate, create QR Code image in Software applications. G d T U
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Printing ANSI/AIM Code 39 In None Using Barcode creation for Software Control to generate, create Code 39 image in Software applications. EAN / UCC  13 Drawer In None Using Barcode encoder for Software Control to generate, create UCC128 image in Software applications. An uplink at 14 GHz requires a saturation flux density of 2 1 91.4 dBW/m and an input BO of 11 dB. The satellite [G/T] is 6.7 dBK , and receiver feeder losses amount to 0.6 dB. Calculate the carriertonoise density ratio. DataMatrix Printer In None Using Barcode maker for Software Control to generate, create Data Matrix ECC200 image in Software applications. UPC A Encoder In None Using Barcode drawer for Software Control to generate, create UPCA image in Software applications. Solution As in Example 12.9, the calculations are best carried out in tabular form. 44.37 dBm2 for a frequency of 14 GHz is calculated by using Eq. (12.44) [A0] as in Example 12.10. Encoding Industrial 2 Of 5 In None Using Barcode encoder for Software Control to generate, create 2 of 5 Standard image in Software applications. Paint Barcode In None Using Barcode printer for Microsoft Excel Control to generate, create bar code image in Excel applications. Quantity Saturation flux density [A0] at 14 GHz Input BO Satellite saturation [G/T ] [k] Receiver feeder loss Total Making Code39 In Java Using Barcode encoder for BIRT Control to generate, create Code 3/9 image in Eclipse BIRT applications. Code 128A Creation In Java Using Barcode creator for Java Control to generate, create ANSI/AIM Code 128 image in Java applications. Decilogs 91.4 44.4 11.0 6.7 228.6 0.6 74.5
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Bar Code Creation In Java Using Barcode creator for Android Control to generate, create barcode image in Android applications. UCC.EAN  128 Generator In None Using Barcode drawer for Font Control to generate, create USS128 image in Font applications. Note that [k] 228.6 dB, so [k] in Eq. (12.50) becomes 228.6 dB. Also, [RFL] and [BO]i are entered as negative numbers to take account of the minus signs attached to them in Eq. (12.50). The total gives the carriertonoise density ratio at the satellite receiver as 74.5 dBHz. Since fade margins have not been included at this stage, Eq. (12.50) applies for clearsky conditions. Usually, the most serious fading is caused by rainfall, as described in Sec. 12.9. 12.7.3 The earth station HPA
The earth station HPA has to supply the radiated power plus the transmit feeder losses, denoted here by TFL, or [TFL] dB. These include waveguide, filter, and coupler losses between the HPA output and the transmit antenna. Referring back to Eq. (12.3), the power output of the HPA is given by [PHPA] [EIRP] [GT] [TFL] (12.51) The [EIRP] is that given by Eq. (12.49) and thus includes any input BO that is required at the satellite. The earth station itself may have to transmit multiple carriers, and its output also will require back off, denoted by [BO]HPA. The earth station HPA must be rated for a saturation power output given by [PHPA,sat] [PHPA] [BO]HPA (12.52) Of course, the HPA will be operated at the backedoff power level so that it provides the required power output [PHPA]. To ensure operation well into the linear region, an HPA with a comparatively high saturation level can be used and a high degree of BO introduced. The large physical size and high power consumption associated with larger tubes do not carry the same penalties they would if used aboard the satellite. Again, it is emphasized that BO at the earth station may be required quite independently of any BO requirements at the satellite transponder. The power rating of the earthstation HPA should also be sufficient to provide a fade margin, as discussed in Sec. 12.9.1. 12.8 Downlink The downlink of a satellite circuit is the one in which the satellite is transmitting the signal and the earth station is receiving it. Equation (12.38) can be applied to the downlink, but subscript D will be used to denote specifically that the downlink is being considered. Thus Eq. (12.38) becomes c C d N0 D [EIRP]D c G d T D [LOSSES]D [k] (12.53) Twelve
In Eq. (12.53) the values to be used are the satellite EIRP, the earthstation receiver feeder losses, and the earthstation receiver G/T. The free space and other losses are calculated for the downlink frequency. The resulting carriertonoise density ratio given by Eq. (12.53) is that which appears at the detector of the earth station receiver. Where the carriertonoise ratio is the specified quantity rather than carriertonoise density ratio, Eq. (12.38) is used. This becomes, on assuming that the signal bandwidth B is equal to the noise bandwidth BN: c C d N D [EIRP]D c G d T D [LOSSES]D [k] [B] (12.54) Example 12.12 A satellite TV signal occupies the full transponder bandwidth of
36 MHz, and it must provide a C/N ratio at the destination earth station of 22 dB. Given that the total transmission losses are 200 dB and the destination earthstation G/T ratio is 31 dB/K, calculate the satellite EIRP required.

