how to create barcode in ssrs report [BO]i in Software

Generating Denso QR Bar Code in Software [BO]i

[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
QR Scanner In None
Using Barcode decoder for Software Control to read, scan read, scan image in Software applications.
Encoding Quick Response Code In Visual C#.NET
Using Barcode generation for .NET framework Control to generate, create QR Code image in .NET applications.
[RFL]
Creating Denso QR Bar Code In .NET
Using Barcode drawer for ASP.NET Control to generate, create QR Code JIS X 0510 image in ASP.NET applications.
QR Code Maker In Visual Studio .NET
Using Barcode printer for .NET framework Control to generate, create QR Code image in .NET applications.
(12.50)
QR Code ISO/IEC18004 Maker In Visual Basic .NET
Using Barcode generation for .NET Control to generate, create QR Code image in Visual Studio .NET applications.
Paint European Article Number 13 In None
Using Barcode drawer for Software Control to generate, create EAN 13 image in Software applications.
Example 12.11
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 UCC-128 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 carrier-to-noise 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 UPC-A 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 Code-39 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
Data Matrix Drawer In VB.NET
Using Barcode printer for VS .NET Control to generate, create Data Matrix image in VS .NET applications.
Make ECC200 In Java
Using Barcode generator for Android Control to generate, create Data Matrix image in Android applications.
The Space Link
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 USS-128 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 carrier-to-noise 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 clear-sky 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 backed-off 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 earth-station 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 earth-station receiver G/T. The free space and other losses are calculated for the downlink frequency. The resulting carrier-to-noise density ratio given by Eq. (12.53) is that which appears at the detector of the earth station receiver. Where the carrier-to-noise ratio is the specified quantity rather than carrier-to-noise 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.
Copyright © OnBarcode.com . All rights reserved.