ITU-R M 2114-0-2018 Technical and operational characteristics of and protection criteria for aeronautical mobile service systems in the frequency bands 22 5-23 6 GHz and 25 25-27 5.pdf

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1、 Recommendation ITU-R M.2114-0 (01/2018) Technical and operational characteristics of and protection criteria for aeronautical mobile service systems in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz M Series Mobile, radiodetermination, amateur and related satellite services ii Rec. ITU-R M.21

2、14-0 Foreword The role of the Radiocommunication Sector is to ensure the rational, equitable, efficient and 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 Re

3、commendations are adopted. The regulatory and policy functions of the Radiocommunication Sector are performed 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

4、 in the Common Patent Policy for ITU-T/ITU-R/ISO/IEC referenced in Annex 1 of Resolution ITU-R 1. Forms to 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

5、the Common Patent Policy for ITU-T/ITU-R/ISO/IEC and the ITU-R patent information database can also be found. 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 tel

6、evision BS Broadcasting service (sound) BT Broadcasting service (television) F Fixed service M Mobile, radiodetermination, 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 Fr

7、equency sharing and coordination between fixed-satellite and fixed service systems SM Spectrum management SNG 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 detai

8、led in Resolution ITU-R 1. Electronic Publication Geneva, 2018 ITU 2018 All rights reserved. No part of this publication may be reproduced, by any means whatsoever, without written permission of ITU. Rec. ITU-R M.2114-0 1 RECOMMENDATION ITU-R M.2114-0 Technical and operational characteristics of and

9、 protection criteria for aeronautical mobile service systems in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz (2018) Scope This Recommendation provides information on the technical characteristics and protection criteria for systems operating in the aeronautical mobile service (AMS) in the fr

10、equency bands 22.5-23.6 GHz and 25.25-27.5 GHz. Related ITU Recommendations and Reports Recommendations ITU-R M.1851, ITU-R P.2108, ITU-R P.676. Keywords Aeronautical mobile service systems, AMS, technical characteristics, protection criteria Abbreviations/Glossary ADL AMS data link ADT Airborne dat

11、a terminal AMS Aeronautical mobile service GDT Ground data terminal RHCP Right hand circularly polarised RLOS Radio-line-of-sight The ITU Radiocommunication Assembly, considering that systems and networks operating in the aeronautical mobile service (AMS) are used for broadband and narrow-band airbo

12、rne data links to support scientific research, remote sensing, fire-fighting, land and crop surveying, pipeline monitoring, and emergency management applications, recognizing a) that the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz are globally allocated on a primary basis to the mobile service;

13、 b) that aeronautical mobile service (AMS) is a subset of the mobile service; c) that the aeronautical mobile service is a mobile service between aeronautical stations and aircraft stations, or between aircraft stations; d) that the use of systems operated under aeronautical mobile service does not

14、preclude the use of these frequency bands by any current and planned application of the services to which they are allocated and does not establish any priority in the Radio Regulations; e) that the frequency band 22.5-23.6 GHz is also allocated on a primary basis to the fixed, inter-satellite, and

15、space research services in some or all parts of the frequency bands; 2 Rec. ITU-R M.2114-0 f) that the frequency band 25.25-27.5 GHz is also allocated on a primary basis to the earth exploration-satellite, fixed, fixed-satellite, inter-satellite, and space research services in some or all parts of t

16、he frequency bands; g) that in these bands new systems under the mobile service as well as under the fixed service are currently envisaged and studied by ITU; h) that operations of aeronautical mobile systems introduce more complex sharing over large areas and may require bilateral agreement between

17、 the administration operating AMS and affected administrations, recommends 1 that the technical and operational characteristics of the systems operating in the AMS described in the Annex should be considered representative of those operating in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz; 2

18、 that the criterion of interfering signal power to receiver noise power level, I/N, of 6 dB should be used as the required protection level for AMS receivers. If multiple potential interference sources are present, protection of the AMS requires that this criterion is not exceeded due to the aggrega

19、te interference from the multiple sources. Annex Technical and operational characteristics of and protection criteria for aeronautical mobile service systems operating in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz 1 Introduction Systems and networks operating in the aeronautical mobile ser

20、vice (AMS) are used for broadband and narrow-band airborne data links to support scientific research, remote sensing, fire-fighting, land and crop surveying, pipeline monitoring, and emergency management applications. The broadband data links are used to transmit data collected from one or multiple

21、research/remote sensing equipment on the aircraft, and the narrow-band data links are used to control this remote sensing equipment on-board the aircraft. 2 Operational deployment In the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz, the mobile service is allocated on a primary basis in all three

22、 ITU-R Regions. The AMS is a mobile service between aeronautical stations and aircraft stations, or between aircraft stations. Platforms equipped with AMS data links (ADL) can be deployed anywhere within a country whose administration has authorized their use in accordance with the authorization. An

23、 ADL may exist between an airborne data terminal (ADT), which is an aircraft station, and a ground data terminal (GDT), which is an aeronautical station, or between two ADTs. Rec. ITU-R M.2114-0 3 The GDT may be at a single permanent location or they may be transportable. Transportable GDTs can be m

24、oved to meet operational needs. The duration that a transportable GDT remains at a particular location is dependent upon operational requirements. The link distance for the ADL is generally limited by the radio-line-of-sight (RLOS) horizon which is a function of the terrain in the vicinity of the GD

25、T and the altitude of the ADT. The operational altitude of airborne platforms equipped with these ADLs depends on specific operational requirements and can be up to approximately 20 km. Although some of the link lengths may be relatively short, many of the link distances approach RLOS horizon distan

26、ce. For an air-to-ground link, the link distance may be approximately 450 km. The link between two ADTs operates in similar manner as the link between a GDT and an ADT with the exception that the link distance is a function of the operating altitude of the two ADTs. In the case of a direct air-to-ai

27、r link, this link distance may be up to 900 km. Other factors to consider, such as atmospheric losses (rain attenuation, gases, etc.) and clutter losses, as described in the relevant ITU-R Recommendations P-Series, could reduce the maximum distance of the link between two aircraft. Depending on the

28、environmental conditions and locations of the aircraft, the crosslink distance might be shorter than 900 km. A single GDT may support several ADT via different links. If the ADLs are operating in a narrow-band mode, multiple data links may be supported through frequency separation. If the data links

29、 are operating in a wide band mode, multiple data links may be supported through geographic separation using multiple high-gain, narrow-beam antennas. An ADT may serve as a node within a larger network or as a repeater to extend the range between the data-collection ADT and the data-receiving GDT. I

30、n this case, the ADT may have two or more ADLs between either two ADTs or between one ADT and one GDT. The temporal duration of the link can span the entire flight duration, i.e. take off/landing, transit to/from the operational area, and the time used for data collection in the operational area. Th

31、us, the time duration during which an ADL can be active may extend for many hours. 3 Technical characteristics of aeronautical mobile systems Representative technical characteristics for airborne data links in the AMS for the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz are provided in Table 1.

32、3.1 Transmitter characteristics The aeronautical mobile systems operating or planned to operate in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz typically use digital modulations. A given transmitter may be capable of radiating more than one waveform. Solid-state power amplifier output device

33、s are typically used in the transmitters. The trend towards use of solid-state transmitters in new mobile systems will continue for the foreseeable future due to the wide bandwidth, low level of generated spurious emissions, low power consumption, and reliability of these devices. Typical transmitte

34、r radio frequency emission (3 dB) bandwidths of mobile systems operating or planned to operate in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz range from about 143 to 865 MHz. Transmitter peak output powers range from 0.1 W (20 dBm) to 60 W (48 dBm). However, the maximum power level at the i

35、nput to the antenna is limited to 10 watts in the 25.25-27.5 GHz frequency range by RR No. 21.5, and the equivalent isotropically radiated power is limited to 24 dBW (in any 1 MHz band) in the 25.25-27.5 GHz frequency range when the direction of maximum radiation of the antenna is within 1.5 degrees

36、 of the geostationary-satellite orbit by RR No. 21.2. 4 Rec. ITU-R M.2114-0 3.2 Receiver characteristics The aeronautical mobile systems in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz use digital signal processing to enhance system performance. The signal processing in the newer generation

37、of aeronautical mobile systems may use direct sequence spread spectrum or other advanced techniques to produce a processing gain for the desired signal and may also provide suppression of undesired signals. 3.3 Antenna characteristics A variety of different types of antennas may be used by systems i

38、n the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz. The antennas gain is typically in the range 33-46 dBi. Horizontal, vertical, and circular polarizations are used. If antenna characteristics provided in Table 1 are sufficient, these characteristics should be used in sharing analyses. If additi

39、onal characteristics are required, the first source of the data should be measured antenna characteristics. Otherwise the antenna data in Table 1 in conjunction with Recommendation ITU-R M.1851 should be used. 4 Protection criteria for the aeronautical mobile service in the frequency bands 22.5-23.6

40、 GHz and 25.25-27.5 GHz The performance of the communication link is often noise limited. An increase in receiver effective noise of 1 dB would constitute significant degradation in the communication range, equivalent to a reduction in communication range of approximately 10% in a free-space propaga

41、tion environment. An increase of 1 dB in the effective receiver noise level corresponds to an (I + N)/N ratio of 1.26, or an I/N ratio of about 6 dB. Given the decrease in AMS range and increase in probability of bit error rate performance due to an increase in effective receiver noise level of 1 dB

42、, the I/N = 6 dB value represents the required protection criterion for the AMS from interference due to another radiocommunication service. If multiple potential interference sources are present, protection of the AMS requires that this criterion is not exceeded due to the aggregate interference fr

43、om the multiple sources. Rec. ITU-R M.2114-0 5 TABLE 1 Representative technical characteristics of aeronautical mobile service systems in the frequency bands 22.5-23.6 GHz and 25.25-27.5 GHz Parameter Units System 1 Airborne System 1 Ground System 2 Airborne System 2 Ground Transmitter Tuning range

44、GHz 25.75-27.15 22.9-23.3 25.25-27.5 22.55-23.5 Power output(1) dBm 27 to 48 30 to 48 20 to 47 20 to 47 Bandwidth 3 dB MHz 865 580 746 143 20 dB MHz 930 850 1 009 196 60 dB MHz 3 100 3 250 4 270 1 010 Harmonic attenuation dB 65 65 62 62 Spurious attenuation dB 60 60 60 60 Modulation Digital Digital

45、Digital Digital Receiver Tuning range GHz 22.9-23.3 25.75-27.15 22.55-23.5 25.25-27.5 RF Selectivity 3 dB MHz 1 410 2 410 3 299 3 299 20 dB MHz 1 540 2 620 3 510 3 510 60 dB MHz 1 850 3 300 3 940 3 940 IF Selectivity 3 dB MHz 652 957 226 854 20 dB MHz 971 1 075 324 1 108 60 dB MHz 3 540 3 540 2 248

46、4 248 NF dB 4 4 3.5 4.5 Sensitivity dBm 80.1 79.7 85.4 79.1 Image rejection dB 80 80 Not Available Not Available Spurious rejection dB 65 65 75 75 6 Rec. ITU-R M.2114-0 TABLE 1 (end) Parameter Units System 1 Airborne System 1 Ground System 2 Airborne System 2 Ground Antenna Antenna gain dBi 33 36-46

47、 33 33-46 1st sidelobe dBi 17 18 16 16 Polarization RHCP(2) RHCP(2) RHCP(2) RHCP(2) Antenna pattern/Type Parabolic reflector Parabolic reflector Parabolic reflector Parabolic reflector Horizontal BW degrees 3.0 2.7 7.2 7.2 Vertical BW degrees 3.0 2.7 7.2 7.2 Antenna model Recommendation ITU-R M.1851

48、(3) (uniform distribution) Recommendation ITU-R M.1851(3) (uniform distribution) Recommendation ITU-R M.1851(3) (uniform distribution) Recommendation ITU-R M.1851(3) (uniform distribution) Notes: (1) In the frequency range 25.25-27.5 GHz, RR No. 21 ( 21.2 and 21.5) apply. (2) RHCP Right Hand Circularly Polarized. (3) Recommendation ITU-R M.1851 provides several patterns based on the field distribution across the aperture of the antenna. The suggested distribution for modelling the antennas is shown in the parenthetical text based on guidance in Recommendation ITU-R M.1851. _