Page 404 - Satellite Communications, Fourth Edition
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384  Chapter Twelve

                                The carrier-to-intermodulation-noise ratio is usually found experimen-
                              tally, or in some cases it may be determined by computer methods. Once
                              this ratio is known, it can be combined with the carrier-to-thermal-noise
                              ratio by the addition of the reciprocals in the manner described in Sec.
                              12.10. Denoting the intermodulation term by (C/N )  and bearing in mind
                                                                         0 IM
                              that the reciprocals of the C/N power ratios (and not the corresponding
                                                         0
                              dB values) must be added, Eq. (12.61) is extended to
                                               N 0    a N 0 b   a N 0 b   a N 0 b
                                               C      C  U     C  D     C  IM           (12.62)

                                A similar expression applies for noice-to-carrier (N/C) ratios.

                                Example 12.20 For a satellite circuit the carrier-to-noise ratios are uplink 23 dB,
                                downlink 20 dB, intermodulation 24 dB. Calculate the overall carrier- to-noise ratio
                                in decibels.
                                Solution From Eq. (12.62),

                                                N      2.4    2.3    2
                                                      10    10    10    0.0019
                                                 C
                                               c  C d   10 log(0.0019)
                                               N
                                                    17.2 dBHz

                                In order to reduce intermodulation noise, the TWT must be operated
                              in a BO condition as described previously. Figure 12.10 shows how the
                              [C/N ]  ratio improves as the input BO is increased for a typical TWT.
                                  0 IM
                              At the same time, increasing the BO decreases both [C/N ]    and
                                                                                       0 U
                              [C/N ] , as shown by Eqs. (12.50) and (12.55). The result is that there
                                  0 D
                              is an optimal point where the overall carrier-to-noise ratio is a maxi-
                              mum. The component [C/N ] ratios as functions of the TWT input are
                                                       0
                              sketched in Fig. 12.11. The TWT input in dB is [ ]   [BO] , and there-

                                                                                   i
                                                                            S
                              fore, Eq. (12.50) plots as a straight line. Equation (12.55) reflects the
                                                                                              ,
                              curvature in the TWT characteristic through the output BO, [BO] 0
                              which is not linearly related to the input BO, as shown in Fig. 12.7.
                              The intermodulation curve is not easily predictable, and only the
                              general trend is shown. The overall [C/N ], which is calculated from
                                                                    0
                              Eq. (12.62), is also sketched. The optimal operating point is defined
                              by the peak of this curve.
                              12.12 Inter-Satellite Links
                              Inter-satellite links (ISLs) are radio frequency or optical links that pro-
                              vide a connection between satellites without the need for intermediate
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