ITU-R M 1799-2007 Sharing between the mobile service and the mobile-satellite service in the band 1 668 4-1 675 MHz《1 668 4-1 675 MHz波段中移动业务和移动卫星业务的共享》.pdf

《ITU-R M 1799-2007 Sharing between the mobile service and the mobile-satellite service in the band 1 668 4-1 675 MHz《1 668 4-1 675 MHz波段中移动业务和移动卫星业务的共享》.pdf》由会员分享，可在线阅读，更多相关《ITU-R M 1799-2007 Sharing between the mobile service and the mobile-satellite service in the band 1 668 4-1 675 MHz《1 668 4-1 675 MHz波段中移动业务和移动卫星业务的共享》.pdf（7页珍藏版）》请在麦多课文档分享上搜索。

1、 Rec. ITU-R M.1799 1 RECOMMENDATION ITU-R M.1799 Sharing between the mobile service and the mobile-satellite service in the band 1 668.4-1 675 MHz (2007) Scope This Recommendation addresses sharing between the mobile service and mobile-satellite service (MSS) in the band 1 668.4-1 675 MHz and recomm

2、ends using the information contained herein in planning the use of this band. The ITU Radiocommunication Assembly, considering a) that the band 1 668.4-1 675 MHz is allocated to the mobile service and mobile-satellite service (MSS) (Earth-to-space) on a primary basis; b) that Resolution 744 (WRC-03)

3、 invites ITU-R to study, as a matter of urgency and in time for WRC-07, the use of the band 1 668.4-1 675 MHz by the mobile service, and to complete any relevant sharing studies between the mobile service and the MSS in this band, taking care to avoid undue constraints on either service; c) that App

4、endix 7 of the Radio Regulations (RR) gives the methodology and parameter values to determine the coordination area for mobile earth stations with respect to potential interference from mobile earth stations to mobile stations; d) that RR Article 21 contains no e.i.r.p. limits on mobile stations app

5、licable in the band 1 668.4-1 675 MHz; e) that studies regarding interference from mobile stations to MSS space stations are contained in Annex 1, noting a) that the studies in Annex 1 have shown that the unconstrained operation of some mobile systems and MSS networks would not be compatible in the

6、band 1 668.4-1 675 MHz; b) that the use of the band 1 668-1 675 MHz by MSS uplinks is likely to be in conjunction with the corresponding downlink band, 1 518-1 525 MHz, recognizing a) that RR Article 21 contains pfd limits applicable to MSS systems in the band 1 518-1 525 MHz and applicable to a cer

7、tain defined geographical area between 71 W and 125 W, and that these limits prevent the operation of MSS systems in that geographical area and also preclude use of some orbital locations by MSS networks in the same band; b) the resolves of Resolution 744 (WRC-03); c) that RR No. 5.380 identifies th

8、e band 1 670-1 675 MHz for aeronautical public correspondence systems; 2 Rec. ITU-R M.1799 d) that, as shown in Annex 1, some types of mobile system would cause interference to MSS satellites above the acceptable level, recommends 1 that, when planning use of the band 1 668.4-1 675 MHz, account shou

9、ld be taken of the following: to adequately protect MSS networks, the e.i.r.p. of transportable radio-relay stations should not exceed 27 dBW in a reference bandwidth of 4 kHz in the direction of the geostationary orbit; the operation of some types of mobile system which could be envisaged for this

10、band, as detailed in Annex 1, would not be compatible with the use of this band by the MSS. Annex 1 Interference calculations to assess sharing between the mobile service and the MSS in the band 1 668.4-1 675 MHz 1 Introduction This Annex provides interference calculations based on the mobile system

11、 and mobile-satellite system characteristics currently available. 2 Characteristics of MSS satellite receivers The band 1 668-1 675 MHz is allocated for MSS (Earth-to-space) but is unlikely to be useable in the United States of America, where alternative terrestrial uses are planned. This and other

12、restrictions which are likely in other parts of the world mean that this band is unlikely to be used by non-GSO MSS systems. Where the band is used for MSS, it is likely to be paired with the band 1 518-1 525 MHz, which is allocated to MSS (space-to-Earth) and which is subject to coordination requir

13、ements with a number of countries which operate terrestrial systems. This situation probably prevents the downlink band being used by MSS systems operating “global” beams but will limit systems to those which make use of high-gain satellite antennas and small spot beams. Hence the band 1 668-1 675 M

14、Hz is most likely to be used by GSO MSS systems employing multiple spot beams, of which representative characteristics are shown in Table 1. TABLE 1 Representative space station parameters Orbit Geostationary Peak antenna gain (dBi) 41 Polarization Circular Satellite receiver noise temperature (K) 5

15、01 Rec. ITU-R M.1799 3 Regarding the interference criterion for studies relating to sharing between the mobile service and MSS space stations, it is expected that any interference received at the satellite will be almost constant in power level and therefore a “long-term” sharing criterion of 6% T/T

16、 or I/N = 12 dB has been used. This value is used as the threshold for coordination between GSO MSS systems, and has been used in previous sharing studies, for example those relating to sharing between mobile and MSS services in the band 2 500-2 690 MHz (see Report ITU-R M.2041). 3 Calculations of i

17、nterference from mobile systems to an MSS satellite receiver 3.1 Interference from transportable radio-relay stations Transportable radio-relay stations are used to provide temporary point-point links. They operate as part of the mobile service. While there are a number of different systems in opera

18、tion, they have generally similar characteristics which allow for a single set of representative characteristics. It may be noted that the systems all have wide tuning ranges, for example 1 350-1 850 MHz or 1 350-2 690 MHz. With respect to the transportable radio-relay antenna, the diameter can be t

19、aken as about 1.2 m, which gives a peak gain of about 24 dBi at 1 670 MHz. Using the reference antenna pattern for Recommendation ITU-R F.699, the side-lobe gain beyond 48 is 1.8 dBi. With respect to the transmitter power, the value of 7 dBW is taken as a representative maximum. To determine the pow

20、er spectral-density of the transmitter, it is assumed that the maximum power would be used with the high bit-rate/wide bandwidth carriers and that the corresponding bandwidth is about 2 MHz. The representative transportable radio-relay parameters are shown in Table 2. Three scenarios are considered:

21、 Scenario 1: Interference from the side-lobe of a transmitting antenna into a satellite at high elevation. Scenario 2: Interference from the side-lobe of a transmitting antenna into a satellite at low elevation. Scenario 3: Interference from the main-lobe of a transmitting antenna into a satellite a

22、t low elevation. Results are shown in Table 2. TABLE 2 Interference from transportable radio-relay systems to MSS space stations Parameter Unit Scenario 1 Scenario 2 Scenario 3 Frequency MHz 1 670 1 670 1 670 Elevation to satellite degrees 90 5 5 Distance km 35 786 41 127 41 127 Free space loss dB 1

23、88.0 189.2 189.2 Satellite receiver temperature K 501 501 501 Reference bandwidth kHz 4 4 4 4 Rec. ITU-R M.1799 TABLE 2 (end) Parameter Unit Scenario 1 Scenario 2 Scenario 3 Noise in reference bandwidth dBW 165.6 165.6 165.6 Criterion (I/N) dB 12 12 12 I maximum in reference bandwidth dBW 177.6 177.

24、6 177.6 Satellite antenna gain dBi 41 41 41 Polarization discrimination dB 3 3 3 e.i.r.p. maximum in reference bandwidth dBW 27.6 26.4 26.4 Mobile station Transmitter power dBW 7 7 7 Feeder loss dB 0 0 0 Antenna gain towards satellite dBi 1.8 1.8 24.0 Bandwidth kHz 2 000 2 000 2 000 e.i.r.p. in refe

25、rence bandwidth dBW 18.2 18.2 4.0 Interference excess dB 9.4 8.2 30.4 Each scenario considers only a single interferer within the satellite antenna beam. In all cases interference exceeds the criterion and in the case of Scenario 3, where the transmitting antenna is directed towards the satellite, t

26、he excess is about 30 dB. These results suggest that power and/or pointing restrictions may be necessary to adequately protect the satellite receiver. To protect the MSS satellite receiver from harmful interference, it would be necessary to limit the e.i.r.p. in the direction of the satellite to abo

27、ut 27 dBW in a reference bandwidth of 4 kHz. This figure assumes only a single interferer but considering the relatively low density of transportable radio-relay system, this is probably a reasonable assumption. 3.2 Interference from aeronautical public correspondence systems Through RR No. 5.380, t

28、he bands 1 670-1 675 MHz and 1 800-1 805 MHz are intended for use, on a worldwide basis, by administrations wishing to implement aeronautical public correspondence. Such systems are no longer envisaged and it appears that there is no longer any interest in aeronautical public correspondence systems.

29、 However RR No. 5.380 was retained by WRC-03 and hence the possibility exists for such systems to be implemented. Characteristics of the terrestrial flight telecommunication system (TFTS) are contained in Recommendation ITU-R M.1040. The system was designed to use the 1 670-1 675 MHz band for the gr

30、ound-to-aircraft link and for the ground stations to use omnidirectional (in the horizontal plane) antennas. Therefore, only two scenarios need to be considered: Scenario 1: Interference from a TFTS ground station to a satellite at a high elevation. Scenario 2: Interference from a TFTS ground statio

31、n to a satellite at a low elevation. Results are shown in Table 3. Rec. ITU-R M.1799 5 TABLE 3 Interference from TFTS ground stations to MSS space stations Parameter Unit Scenario 1 Scenario 2 Frequency MHz 1 670 1 670 Elevation to satellite degrees 90 5 Distance km 35 786 41 127 Free space loss dB

32、188.0 189.2 Satellite receiver temperature K 501 501 Reference bandwidth kHz 4 4 Noise in reference bandwidth dBW 165.6 165.6 Criterion (I/N) dB 12 12 I maximum in reference bandwidth dBW 177.6 177.6 Satellite antenna gain dBi 41 41 Polarization discrimination dB 3 3 e.i.r.p. maximum in reference ba

33、ndwidth dBW 27.6 26.4 Ground station Transmitter power dBW 11 11 Feeder loss dB 0 0 Antenna gain towards satellite dBi 0 8 Bandwidth kHz 22 22 e.i.r.p. in reference bandwidth dBW 3.6 11.6 Interference excess dB 31.2 38.0 The value of transmitter power is the maximum value given for an “en route” gro

34、und station. Other categories of ground station have a maximum value 10 dB lower but this still results in a significant excess of interference. These results suggest that any aeronautical public correspondence ground station would exceed the interference criterion at any visible satellite. 3.3 Inte

35、rference from cellular or similar high-density mobile systems Cellular or similar high-density mobile systems could be envisaged in the band 1 668.4-1 675 MHz. In one country, the band 1 670-1 675 MHz is used for a high-density mobile system and another country is planning to introduce such a system

36、. Although such systems are currently limited to a specific geographical area, from the regulatory perspective there are no reasons why such systems could not be introduced more widely in the future and it is therefore necessary to consider the possible consequences of the introduction of such syste

37、ms on MSS systems. The mobile system characteristics used here are taken from those in Report ITU-R M.2039 which contains the characteristics of terrestrial IMT-2000 systems for frequency sharing/interference analyses. For the base stations, the characteristics of a typical macro cell base station a

38、re used. Although actual system characteristics may vary from the ones used, the characteristics allow broad conclusions of the interference potential to be determined. Four scenarios are considered: Scenario 1: Interference from a mobile station into a satellite at high elevation (45). Scenario 2:

39、Interference from a mobile station into a satellite at low elevation (0). 6 Rec. ITU-R M.1799 Scenario 3: Interference from a base station into a satellite at high elevation (45). Scenario 4: Interference from a base station into a satellite at low elevation (0). Results are shown in Table 4. TABLE

40、4 Interference from other mobile systems to MSS space stations Parameter Unit Scenario 1 Scenario 2 Scenario 3 Scenario 4 Frequency MHz 1 670 1 670 1 670 1 670 Elevation to satellite degrees 45 0 45 0 Distance km 37 412 42 164 37 412 42 164 Free space loss dB 188.4 189.3 188.4 189.3 Satellite receiv

41、er temperature K 501 501 501 501 Reference bandwidth kHz 4 4 4 4 Noise in reference bandwidth dBW 165.6 165.6 165.6 165.6 Criterion (I/N) dB 12 12 12 12 I maximum in reference bandwidth dBW 177.6 177.6 177.6 177.6 Satellite antenna gain dBi 41 41 41 41 Polarization discrimination dB 3 3 3 3 e.i.r.p.

42、 maximum in reference bandwidth dBW 27.2 26.3 27.2 26.3 Mobile/base station Transmitter power dBW 6 6 13 13 Feeder loss dB 0 0 1 1 Antenna gain towards satellite dBi 0 0 1(1)14(1)Bandwidth kHz 5 000 5 000 5 000 5 000 e.i.r.p. in reference bandwidth (4 kHz) dBW 37.0 37.0 20.0 5.0 Interference excess

43、(single interferer) dB 9.7 10.7 7.3 21.3 Interference excess (100 interferers) dB 10.3 9.3 27.3 41.3 (1) Assumes 2.5 downtilt angle. Each scenario considers interference from a single source. In practice there may be multiple co-frequency transmitters which increase the total interference received b

44、y the satellite and this is particularly the case for code division multiple access (CDMA) based networks, as envisaged here. As a rough estimate of the aggregate interference, the final row shows the interference excess assuming 100 simultaneous co-frequency interferers. In the case of Scenarios 1,

45、 2 and 3, it can be seen that a high level of interference can be expected from a mobile station or base station. Hence the use of such mobile networks would prevent the operation of MSS systems in the same geographic area. Considering the high levels of interference, particularly from MS base stati

46、ons, excessive interference may also be caused to MSS systems providing service to adjacent or nearby geographic areas. In the case of Scenario 4, interference significantly exceeds the criterion and even 20-25 dB of satellite antenna isolation will not be sufficient mitigation. This means that orbi

47、tal locations where Rec. ITU-R M.1799 7 mobile service operations are visible from a low elevation angle may not be useable for MSS. Operation of these types of mobile systems in a particular country could therefore prevent MSS operations in other countries even with considerable geographic separati

48、on. The MSS satellite would therefore be likely to receive interference considerably in excess of the criterion from unpredictable locations. 4 Conclusions All of the mobile systems considered have the potential to cause excessive interference to MSS satellites. To adequately protect MSS satellite r

49、eceivers, the aggregate interference from mobile service stations within the satellite beam would need to be limited to 27 dBW in a reference bandwidth of 4 kHz. In the case of transportable radio-relay systems, which are used in relatively low numbers, an e.i.r.p. of about 27 dBW in a 4 kHz reference bandwidth in the direction of the GSO would just meet the interference criterion for protection to the MSS (a lower value may be necessary if the risk of multiple interference is considered significant). In the case of aero