ITU-R SA 2079-0-2015 Frequency sharing between SRS and FSS (space-to-Earth) systems in the 37 5-38 GHz band《音响还原电路和卫星固定业务的在37 5-38千兆赫频段的系统的频率共享(空间到地球)》.pdf

《ITU-R SA 2079-0-2015 Frequency sharing between SRS and FSS (space-to-Earth) systems in the 37 5-38 GHz band《音响还原电路和卫星固定业务的在37 5-38千兆赫频段的系统的频率共享(空间到地球)》.pdf》由会员分享，可在线阅读，更多相关《ITU-R SA 2079-0-2015 Frequency sharing between SRS and FSS (space-to-Earth) systems in the 37 5-38 GHz band《音响还原电路和卫星固定业务的在37 5-38千兆赫频段的系统的频率共享(空间到地球)》.pdf（9页珍藏版）》请在麦多课文档分享上搜索。

1、 Recommendation ITU-R SA.2079-0 (08/2015) Frequency sharing between SRS and FSS (space-to-Earth) systems in the 37.5-38 GHz band SA Series Space applications and meteorology ii Rec. ITU-R SA.2079-0 Foreword The role of the Radiocommunication Sector is to ensure the rational, equitable, efficient and

2、 economical use of the radio-frequency spectrum by all radiocommunication services, including satellite services, and carry out studies without limit of frequency range on the basis of which Recommendations are adopted. The regulatory and policy functions of the Radiocommunication Sector are perform

3、ed by World and Regional Radiocommunication Conferences and Radiocommunication Assemblies supported by Study Groups. Policy on Intellectual Property Right (IPR) ITU-R policy on IPR is described in the Common Patent Policy for ITU-T/ITU-R/ISO/IEC referenced in Annex 1 of Resolution ITU-R 1. Forms to

4、be used for the submission of patent statements and licensing declarations by patent holders are available from http:/www.itu.int/ITU-R/go/patents/en where the Guidelines for Implementation of the Common Patent Policy for ITU-T/ITU-R/ISO/IEC and the ITU-R patent information database can also be foun

5、d. Series of ITU-R Recommendations (Also available online at http:/www.itu.int/publ/R-REC/en) Series Title BO Satellite delivery BR Recording for production, archival and play-out; film for television BS Broadcasting service (sound) BT Broadcasting service (television) F Fixed service M Mobile, radi

6、odetermination, amateur and related satellite services P Radiowave propagation RA Radio astronomy RS Remote sensing systems S Fixed-satellite service SA Space applications and meteorology SF Frequency sharing and coordination between fixed-satellite and fixed service systems SM Spectrum management S

7、NG Satellite news gathering TF Time signals and frequency standards emissions V Vocabulary and related subjects Note: This ITU-R Recommendation was approved in English under the procedure detailed in Resolution ITU-R 1. Electronic Publication Geneva, 2015 ITU 2015 All rights reserved. No part of thi

8、s publication may be reproduced, by any means whatsoever, without written permission of ITU. Rec. ITU-R SA.2079-0 1 RECOMMENDATION ITU-R SA.2079-0 Frequency sharing between SRS and FSS (space-to-Earth) systems in the 37.5-38 GHz band (2015) Scope This Recommendation covers the frequency sharing betw

9、een the space research service (SRS) and the fixed satellite service (FSS) in the 37.5-38 GHz band (space-to-Earth). It gives e.i.r.p. and pfd limits for the space-VLBI (SVLBI) and lunar systems of SRS, and the geostationary orbit (GSO) and highly inclined elliptical Orbit (HEO) systems of FSS. Keyw

10、ords SRS near-Earth systems, FSS GSO and HEO systems, e.i.r.p. and p.f.d. limits, frequency sharing, 37.5-38 GHz The ITU Radiocommunication Assembly, considering a) that the space research service (SRS) (s-E) has a primary allocation in the 37-38 GHz band and the fixed-satellite service (FSS) (s-E)

11、has a primary allocation in the 37.5-42.5 GHz band, and these allocations overlap in the 37.5-38 GHz band; b) that the protection criteria for the SRS downlinks in the 37-38 GHz band are given in Recommendation ITU-R SA.1396; c) that calculation of interference to an SRS earth station that may resul

12、t from atmospheric and precipitation effects should be based on weather statistics for 0.001% of the time for manned missions and for 0.1% of time for unmanned missions; d) that deep space SRS downlinks often carry data of unique science events that are not repeatable; e) that the emissions from dee

13、p space downlinks typically have a power flux-density (pfd) on the surface of the Earth that is much lower than any other satellite signal and is therefore extremely vulnerable to interference from satellites operating in the same frequency band; f) that space-based very long baseline interferometry

14、 (SVLBI) SRS downlinks have interference criteria as given in Report ITU-R SA.2065, and that these links may be able to tolerate higher interference levels than indicated in Recommendation ITU-R SA.1396; g) that protection of SRS and FSS systems sharing the 37.5-38 GHz band has been studied in Repor

15、t ITU-R SA.2307 whose results are summarized in the Annex; h) that transmissions from the SRS SVLBI and lunar systems with e.i.r.p. levels below the limits given in Report ITU-R SA.2307 meet the protection criteria of the FSS GSO and HEO systems; i) that transmissions from the FSS GSO and HEO system

16、s with e.i.r.p. levels below the limits given in Recommendation ITU-R S.1328 meet the protection criteria of SRS SVLBI and unmanned lunar systems, but FSS GSO transmissions require a lower e.i.r.p limit to meet the protection criterion of SRS manned lunar missions; 2 Rec. ITU-R SA.2079-0 j) that tra

17、nsmissions from the FSS HEO systems operating at pfd limits given in ITU Radio Regulations Article 21, Table 21-4 meet the protection criteria of the SRS SVLBI and lunar missions; k) that other non-SVLBI near-Earth SRS systems, such as Lagrange L1/L2 missions, with low system noise temperature (abou

18、t 60 K) may be about 8 dB more sensitive to interference than the lunar systems with background noise temperature from the Moon (about 353 K); l) that for a small percentage of time, when propagation impairments in the 37 GHz band are severe during the fading conditions, the satellite systems in thi

19、s band could increase their e.i.r.p. spectral density to overcome the fading conditions, recognizing a) that FSS satellite systems may use the 37.5-38 GHz band for very small aperture terminal applications (the VSAT mode), or for gateway applications that use large antennas (the gateway mode); b) th

20、at FSS systems operating in the VSAT mode may use the 37.5-38 GHz band when operating in areas away from the SRS earth stations, and a different frequency band above 38 GHz when operating in areas near the SRS earth stations; c) that, for FSS systems using the gateway mode, the gateway stations may

21、be located away from the SRS earth stations, recommends 1 that the SRS deep-space missions should use the 37-37.5 GHz band as much as possible to be fully protected in accordance with Recommendation ITU-R SA.1396; 2 that SRS manned lunar missions in the 37.5-38 GHz band should use 0.1% exceedance pr

22、otection criterion from FSS systems rather than 0.001%; 3 that, to meet the FSS protection criterion, the SRS SVLBI and lunar systems transmitting in the 37.5-38 GHz band should operate below the maximum e.i.r.p. spectral density levels or below the pfd levels, under clear sky conditions, at the FSS

23、 earth stations shown in the Table below (Note 1); SRS systems Maximum e.i.r.p. spectral density (dBW/MHz) Pfd limit on Earths surface (dBW/MHz/m2) SVLBI 32 127 Lunar 56 128 4 that, to meet the SRS SVLBI systems and lunar mission interference criteria, the FSS systems in the 37.5-38 GHz band should

24、operate below the maximum e.i.r.p. spectral density levels or the pfd levels, under clear sky conditions, at the SRS earth stations given in the Table below (Note 1); Rec. ITU-R SA.2079-0 3 FSS systems Maximum e.i.r.p. spectral density (dBW/MHz) Pfd limit on Earths surface (dBW/MHz/m2) GSO 42 121 HE

25、O 48 105 (RR Table 21-4 limit) 5 that the FSS systems operating in the VSAT mode should use frequency bands above 38 GHz in geographical areas near the SRS earth stations; 6 that the pfd at the Earths surface for SRS and FSS systems transmitting in the 37.5-38 GHz band should be no greater than the

26、level(s) required to meet their link availability and performance objectives of the subject applications; 7 that other near-Earth SRS systems, such as Lagrange L1/L2 missions, should consider designing their downlink with an additional link margin of about 8 dB to achieve compatibility with FSS syst

27、ems, similar to a lunar SRS system. NOTE 1 During excessive fading conditions, the e.i.r.p. spectral density in Tables above can be exceeded by the amount needed to maintain link availability while meeting the pfd limits. Annex Frequency sharing between SRS near-Earth and FSS systems in the 37.5-38

28、GHz band 1 Introduction This Annex summarizes the results of the Report ITU-R SA.2307, which gives the frequency sharing analysis between the SVLBI and lunar systems of SRS and the GSO and HEO systems of FSS. The interference between these systems is simulated for two cases. In Case 1, the systems a

29、re assumed to operate using the parameters and e.i.r.p. density levels as given in the following sections. In Case 2, the systems are assumed to operate with higher transmit powers generating the maximum pfd spectral density levels on the Earths surface as given by Radio Regulation Article 21, Table

30、 21-4. 2 SRS systems The planned parameters for the SVLBI and lunar SRS systems are summarized in Table 2.1 below. These parameters are used in calculating the interference levels between these SRS systems and the GSO and HEO FSS systems for Case 1. 4 Rec. ITU-R SA.2079-0 TABLE 2.1 Planned SRS SVLBI

31、 and lunar system parameters (Case 1) Parameters Units SVLBI Lunar Space station parameters Orbital inclination degrees 20, 31, 65 Moon Transmit power dBW 3 14.5 Antenna gain dBi 48.1 64 Data rate Mb/s 500 250 Max transmit e.i.r.p. density dBW/MHz 24.1 54.5 Earth station parameters Antenna diameter

32、M 15, 34 6 Gain pattern RR AP8-10 RR AP8-10 Lowest elevation degrees 10 10 Noise temperature K 150 353 Protection criterion Io/No dB 6 6 Interference protection dBW/MHz 153 149.1 Exceedance percentage p 2% 0.1% (unmanned) 0.001% (manned) For Case 2, it is assumed that the transmissions from SRS SVLB

33、I and lunar systems satisfy the pfd limits specified in RR Table 21-4 on the surface of the Earth for the 37.5-38 GHz band. In the results section, the SVLBI systems with different orbital inclinations will be identified as SVLBI-20, SVLBI-31, and SVLBI-65. 3 FSS systems The planned parameters for t

34、he FSS GSO and HEO systems are summarized in Table 3.1 below. These parameters are used in calculating the interference levels between these FSS systems and the SVLBI and lunar SRS systems for Case 1. Rec. ITU-R SA.2079-0 5 TABLE 3.1 Planned FSS GSO and HEO system parameters (Case 1) Parameters Unit

35、s GSO HEO Space station parameters Number of satellites 2 3 Transmit power dBW 11 11 Antenna gain dBi 53 53 Occupied bandwidth MHz 500 500 Max transmit e.i.r.p. density dBW/MHz 37 37 Earth station parameters Antenna gain dB 58.9 58.9 Gain pattern Recommendation ITU-R S.465 Recommendation ITU-R S.465

36、 Lowest elevation degrees 10 10 Noise temperature K 343 340 Protection criterion Io/No dB 0 0 Interference protection dBW/MHz 143 143 Exceedance percentage p 0.005% 0.005% For Case 2, it is assumed that the transmissions from FSS GSO and HEO systems satisfy the pfd limits specified in RR Table 21-4

37、on the surface of the Earth for the 37.5-38 GHz band. 4 Results For Case 1, Table 4.1 below summarizes interference level exceedance observed at the SRS and FSS earth stations. 6 Rec. ITU-R SA.2079-0 TABLE 4.1 Exceedance of protection criteria for SRS and FSS systems using planned e.i.r.p. density l

38、evels in the 37.5-38 GHz band (Case 1) (Case 1) e.i.r.p. Interfering systems (Victim systems) Exceedance of protection criteria (dB) Max. exceedance (dB) SRS FSS SVLBI-20 SVLBI-31 SVLBI-65 Lunar (unmanned) Lunar (manned) GSO HEO SRS SVLBI-20 SVLBI-31 SVLBI-65 6 Note, however, that the SRS and FSS sy

39、stems do not intend to use these high e.i.r.p. density levels 100% of the time, but only when the weather is bad and atmospheric attenuation is excessive. In this case, if the SRS and FSS earth stations are close to each other such that they have the same weather conditions, the interference will be

40、 much smaller than expected due to atmospheric losses, and will probably be below the protection criteria. If, however, the SRS and FSS earth stations are separated by large distance, then they might experience different weather conditions. If the interference goes through clear sky, the atmospheric

41、 attenuation might be small. In this case, however, the transmitting antenna will have a smaller off-boresight gain, and the spectral e.i.r.p. density towards the victim earth station will be reduced. For example, for an FSS GSO system, if the SRS and FSS earth stations are separated by 100 km, the

42、interference e.i.r.p. density seen by the victim earth station would be reduced by 3 dB, and if they are separated by 200 km, the reduction would be 10 dB. If the FSS systems cannot satisfy the specified pfd spectral density limits, then they should choose to use frequency bands above 38 GHz when op

43、erating near the SRS earth station locations, and only use the 37.5-38 GHz band when operating far from the SRS earth stations. FSS systems with spot beams should be able to satisfy this condition easily. The SRS systems without spot beams will have to operate at the specified e.i.r.p. density level

44、s to avoid interfering with the FSS. Above results indicate that, in the 37.5-38 GHz band, sharing between SRS (SVLBI and unmanned lunar) and FSS (GSO and HEO) is feasible using the planned system parameters. If interference exceeds the protection criteria of SRS or FSS systems, then mitigation methods exist to reduce the interference to an acceptable level. _