ITU-R F 760-1-1994 Protection of Terrestrial Line-of-Sight Radio-Relay Systems Against Interference from the Broadcasting-Satellite Service in the Bands Near 20 GHz《陆地视距无线中继系统对来自20.pdf

1、 XTU-R RECMN*F* 760-3 94 D 4855232 0523747 249 = Rec. ITU-R F.760-1 377 RECOMMENDATION ITU-R F.760- 1 * PROTECTION OF TERRESTRIAL LINE-OF-SIGHT RADIO-RELAY SYSTEMS AGAINST INTERFERENCE FROM THE BROADCASTING-SATELLITE SERVICE IN THE BANDS NEAR 20 GHz (Question ITU-R 11 119) (1 992- 1994) The ITU Radi

2、ocommunication Assembly, considering a) that according to the Radio Regulations, the fixed service (FS) and the broadcasting-satellite service (BSS) share the bands 17.7-17.8 GHz in Region 2 and 21.4-22 GHz in Regions 1 and 3; b) that the FS uses these bands extensively for line-of-sight radio-relay

3、 systems, particularly in urban areas; c that, because of this use, it is necessary to ensure that emissions from satellites do not exceed permissible levels of interference to line-of-sight radio-relay systems; d) that radio-relay systems can be protected from the satellite emissions by determining

4、 suitable values of power i-lux-density, set up at the surface of the Earth, in a reference bandwidth; e that the degree of correlation between the fading of the unwanted signal on the space-Earth interference path with the fading of the wanted signal on the radio-relay system is an important factor

5、 to consider when determining acceptable satellite power flux-density values; 0 that in cases where fading on the wantedunwanted signal path is highly correlated, the appropriate power flux-density limit will be more dependent on the FS receive antenna characteristics and the normal received carrier

6、 level, recommends 1. that in the frequency bands near 20 GHz, shared between systems in the BSS and the line-of-sight radio-relay systems, the maximum power flux-density produced at the surface of the Earth by emissions from a satellite, for all conditions and methods of modulation, in any 1 MHz ba

7、nd, required for the protection of the FS is: -1 15 dB(W/m2) for O“ I 0 I 5“ -1 i5 + 0.5 (0 - 5) dB(W/m2) for 5“ 0 I 25“ -105 dB(W/m2) for 25“ 0 I 90“ where 0 is the angle of arrival of the radio-frequency wave (degrees above the horizontal); 2. under free-space conditions; 3. radio-relay systems fo

8、r any further studies of sharing in the bands near 20 GHz. that the aforementioned values relate to the power flux-density and angles of arrival which would be obtained that the model, and the considerations of this model, given in Annex 1 be used to represent the line-of-sight * This Recommendation

9、 should be brought to the attention of Radiocommunication Study Groups 10 and 11 (Working Party 10-1 IS). COPYRIGHT International Telecommunications Union/ITU RadiocommunicationsLicensed by Information Handling ServicesITU-R RECMN*F. 760-3 94 E 4855232 0523748 385 E 378 Rec. ITU-R F.760-1 ANNEX 1 Pe

10、rmissible levels of interference into a radio-relay system from transmitting stations of the BSS where the FS and BSS share on an equal primary basis This Annex describes the interference model from which the power flux-density limits for low and high angles of elevation are derived. 1. Characterist

11、ics of the model As a basis for the calculations a model 64-QAM digital link operating at 22 GHz is assumed, the parameters of which are listed below: - transmitter power output: power output into antenna is -7 dBW (200 mW), - - - - - receiver bandwidth: 40 MHz, - receiver feededwaveguide loss: feed

12、erlwaveguide loss is 3 dB, antenna gain: antenna gain for a 46 cm microwave antenna with radome is 38 dBi, effective antenna area: 0.09 m2 (55% efficiency), free space loss: 139 dB for a 10 km path length, receiver noise figure: 5 dB. With the above model parameters, the standard receive carrier pow

13、er, C, is -73 dBW and the receiver noise floor, N, is -123 dBW. The model does not consider satellites in low-Earth orbits, which may be expected to be users of this band. The interference effects of low-Earth orbit satellites may be considerably different from the effects of satellites in geostatio

14、nary orbit. In the following calculations it is assumed that the interference power is uniformly distributed across the receiver passband. 2. Maximum power flux-density First, the in-beam interference which determines the maximum power tlux-density at low angles of elevation is considered. The error

15、 performance curves for a 64-QAM receiver determines the CIN and C/I ratios required to maintain a le3 BER in the presence of maximum permissible interference power (see Recommendation ITU-R SF.766). The interference, I, is given as: where: Pfd : A, : BW : L, : power flux-density (dB(W(m2/MHz) effec

16、tive receive antenna aperture (m2) = 0.09 m2 bandwidth (MHz) = 40 MHz receiver feededwaveguide loss (dB) = 3 dB. Thus the maximum pfd = I, - 3 (dB(W(m%fHz). COPYRIGHT International Telecommunications Union/ITU RadiocommunicationsLicensed by Information Handling ServicesRec. ITU-R F.760-1 379 Conside

17、ring rain fading with perfect correlation of wanted and interfering signals, a rain fade of 25 dB will produce outage with no interference. Using the rain attenuation expression from Recommendation ITU-R PN.530, one finds that the probability of outage at the 0.005% level would increase by 10% for 0

18、.8 dB reduction in fade margin (again with no interference). Using, for instance, Fig. 4 from Recommendation ITU-R SF.766, one finds that the CIN is degraded by about 0.8 dB where the C/1 is 8 dB more than the CIN, .e. 33 dB. The unfaded interference power is I, = C, - 33 = -106dBW. This corresponds

19、 to a pfd of -109 dB(W(m*/MHz) with no differential fading. Differential fading in this Recommendation implies that the fading of the wanted signal and the interfering signal does not occur at the same time, Le. the statistics of the two signals are not perfectly correlated. The power tlux-density n

20、oted above may need further reduction to allow for differential fading caused by rain and/or multipath. Propagation measurements of differential fading suggest that an allowance of 6 dB (see Note) for differential fiiding would be required to protect the fixed service receiver from interference in t

21、he presence of precipitation or clear- air fading. Next, off-beam interference is considered. The aggregate of interference from all sources is mitigated by the receive antenna discrimination. A similar relationship between angle of arrival and angle of elevation is assumed as in setting the pfd lim

22、its for sharing with the fixed-satellite service in lower frequency bands. As a result the pfd limit will increase by 0.5 dB per degree up to 25“ elevation and will remain at that value for higher elevation angles. A similar curve is generally applicable to space stations in other than low-Earth orb

23、it, transmitting at frequencies above about 15 GHz. In frequency bands shared between the fixed service and low-Earth orbit satellites, different power flux-density limits may be applicable. Note from the Director, BR - For information, the derivation of this allowance is given in: ALLEN, K.C., PAPA

24、ZIAN, L.B. and DEBOLT, R. 24-28 June, 19911 Presentation at N.A. Radio Science Meeting in London, Ontario, Canada. COVER, D.A. and RUMMLER, W.D. 19921 Conference Digest, IEEE 1992 International Conference on Communications, Chicago, IL, United States of America. COPYRIGHT International Telecommunications Union/ITU RadiocommunicationsLicensed by Information Handling Services