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2 Interference between Satellite Circuits (B1 and B2 Modes) A satellite circuit may suffer the B1 and B2 modes of interference shown in Fig 131 from a number of neighboring satellite circuits, the resultant effect being termed aggregate interference Because of the difficulties of taking into account the range of variations expected in any practical aggregate, studies of aggregate interference have been quite limited, with most of the study effort going into what is termed singleentry interference studies (see Sharp, 1984a) As the name suggests, single-entry interference refers to the interference produced by a single interfering circuit on a neighboring circuit Interference may be considered as a form of noise, and as with noise, system performance is determined by the ratio of wanted to interfering powers, in this case the wanted carrier to the interfering carrier power or C/I ratio. rdlc pdf 417 PDF417 Barcode Creating Library for RDLC Reports | Generate ...
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NET web & IIS applications; Easy to draw & create 2D PDF - 417 barcode images in jpeg, gif, png and bitmap files; Able to generate & print PDF - 417 in RDLC ... The single most important factor controlling interference is the radiation pattern of the earth-station antenna Comparatively. large-diameter reflectors can be used with earth-station antennas, and hence narrow beamwidths can be achieved For example, a 10-m antenna at 14 GHz has a 3-dB beamwidth of about 015 This is very much narrower than the 2 to 4 orbital spacing allocated to satellites To relate the C/I ratio to the antenna radiation pattern, it is necessary first to define the geometry involved Figure 132 shows the angles subtended by two satellites in geostationary orbit The orbital separation is defined as the angle subtended at the center of the earth, known as the geocentric angle However, from an earth station at point P the satellites would appear to subtend an angle Angle is referred to as the topocentric angle. rdlc pdf 417 PDF - 417 Client Report RDLC Generator | Using free sample for PDF ...
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Free trial package available to insert PDF - 417 barcode image into Client Report RDLC . In all practical situations relating to satellite interference, the topocentric and geocentric angles may be assumed equal, and in fact, making this assumption leads to an overestimate of the interference (Sharp, 1983) Consider now S1 as the wanted satellite and S2 as the interfering satellite An antenna at P will have its main beam directed at S1 and an off-axis component at angle directed at S2 Angle is the same as the topocentric angle, which as already shown may be assumed equal to the geocentric or orbital spacing angle Therefore, when calculating the antenna sidelobe pattern, the orbital spacing angle may be used, as described in Sec 1324 Orbital spacing angles range from 2 to 4 in 05 intervals in the C band In Fig 133 the satellite circuit being interfered with is that from earth station A via satellite S1 to receiving station B. rdlc pdf 417 How to add Barcode to Local Reports ( RDLC ) before report ...
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Barcode Control SDK supports generating Data Matrix, QR Code, PDF - 417 barcodes in RDLC Local Report using VB and C# class library both in ASP.NET and ... The following example creates a torus based on user input: Public Sub TestAddTorus() Dim pntPick As Variant Dim pntRadius As Variant Dim dblRadius As Double Dim dblTube As Double Dim objEnt As Acad3DSolid Dim intI As Integer '' set the default viewpoint SetViewpoint '' get input from user With ThisDrawing.Utility .InitializeUserInput 1 pntPick = .GetPoint(, vbCr & "Pick the center point: ") .InitializeUserInput 1 pntRadius = .GetPoint(pntPick, vbCr & "Pick a radius point: ") .InitializeUserInput 1 + 2 + 4, "" dblTube = .GetDistance(pntRadius, vbCr & "Enter the tube radius: ") End With '' calculate radius from points For intI = 0 To 2 dblRadius = dblRadius + (pntPick(intI) - pntRadius(intI)) ^ 2 Next dblRadius = Sqr(dblRadius) '' draw the entity Set objEnt = ThisDrawing.ModelSpace.AddTorus(pntPick, dblRadius, dblTube) objEnt.Update ThisDrawing.SendCommand "_shade" & vbCr End Sub The B1 mode of interference can occur from satellite S2 into earth station B, and the B2 mode of interference can occur from earth station C into satellite S1 The total single-entry interference is the combined effect of these two modes Because the satellites cannot carry very large antenna reflectors, the beamwidth is relatively wide, even for the so-called spot beams For example, a 35-m antenna at 12 GHz has a beamwidth of about 05 ,. Resource Pricing Resource Demand Changes in Resource Demand True or False Questions Solved Problems and the equatorial arc subtended by this angle is about 314 km. In interference calculations, therefore, the earth stations will be assumed to be situated on the 3-dB contours of the satellite footprints, in which case the satellite antennas do not provide any gain discrimination between the wanted and the interfering carriers on either transmit or receive. Equation (12.13) may be used to calculate the wanted and interfering downlink carrier powers received by an earth station. The carrier power [C] in dBW received at station B is [C] [EIRP]1 3 [GB] [FSL] (13.1) Here, [EIRP]1 is the equivalent isotropic radiated power in dBW from satellite 1, the 3 dB accounts for the 3-dB contour of the satellite transmit antenna, GB is the boresight (on-axis) receiving antenna gain at B, and [FSL] is the free-space loss in decibels. A similar equation may be used for the interfering carrier [I], except an additional term [Y]D dB, allowing for polarization discrimination, must be included. Also, the receiving antenna gain at B is determined by the off-axis angle , giving [I ] [EIRP]2 3 [GB ( )] [FSL] [Y ]D (13.2)
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