ITU-R M 2089-0-2015 Technical characteristics and protection criteria for aeronautical mobile service systems in the frequency range 14 5-15 35 GHz《航空移动业务系统的技术特点和保护标准 频率范围为14 5-15 .pdf

《ITU-R M 2089-0-2015 Technical characteristics and protection criteria for aeronautical mobile service systems in the frequency range 14 5-15 35 GHz《航空移动业务系统的技术特点和保护标准 频率范围为14 5-15 .pdf》由会员分享，可在线阅读，更多相关《ITU-R M 2089-0-2015 Technical characteristics and protection criteria for aeronautical mobile service systems in the frequency range 14 5-15 35 GHz《航空移动业务系统的技术特点和保护标准 频率范围为14 5-15 .pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、 Recommendation ITU-R M.2089-0 (10/2015) Technical characteristics and protection criteria for aeronautical mobile service systems in the frequency range 14.5-15.35 GHz M Series Mobile, radiodetermination, amateur and related satellite services ii Rec. ITU-R M.2089-0 Foreword The role of the Radioco

2、mmunication 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 Recommendations are adopted. The regula

3、tory 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 in the Common Patent Policy for ITU-

4、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 the Common Patent Policy for ITU-T/IT

5、U-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 television BS Broadcasting service (soun

6、d) 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 Frequency sharing and coordination betw

7、een 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 detailed in Resolution ITU-R 1. Electronic

8、 Publication Geneva, 2015 ITU 2015 All rights reserved. No part of this publication may be reproduced, by any means whatsoever, without written permission of ITU. Rec. ITU-R M.2089-0 1 RECOMMENDATION ITU-R M.2089-0 Technical characteristics and protection criteria for aeronautical mobile service sys

9、tems in the frequency range 14.5-15.35 GHz (2015) Scope This Recommendation provides information on the technical characteristics and protection criteria for systems operating in the aeronautical mobile service (AMS), planned to or currently operating in the frequency range 14.5-15.35 GHz for use in

10、 sharing and compatibility studies as needed. Keywords Aeronautical Mobile Service, Technical Characteristics, Protection Criteria, Ku-band Abbreviations/Glossary ADL AMS data link ADT Airborne data terminal AMS Aeronautical mobile service GDT Ground data terminal RLOS Radio line-of-sight UAS Unmann

11、ed aircraft system The ITU Radiocommunication Assembly, considering a) that systems and networks operating in the AMS are used for broadband, airborne data links to support remote sensing applications in the areas of, e.g. earth sciences, land management, and energy distribution. Examples of these a

12、pplications include e.g. monitoring sea ice thickness and distribution, local and national law enforcement, forest fire mapping, petroleum pipeline monitoring, agricultural and urban land use and natural resource surveys; b) that systems and networks operating in the AMS are used for narrow-band, ai

13、rborne command and control data links; c) that there are increasing numbers of various planned and operating systems and networks in the AMS; d) that administrations conducting ITU-R sharing or compatibility studies addressing new allocation proposals in any part of the frequency range 14.5-15.35 GH

14、z should take into account operations of incumbent services in the band, including aeronautical mobile service, recognizing a) that the frequency range 14.5-15.35 GHz is globally allocated on a primary basis to the mobile service; b) that the aeronautical mobile service is a mobile service between a

15、eronautical stations and aircraft stations, or between aircraft stations; c) that the frequency range 14.5-15.35 GHz is also globally allocated on a primary basis to fixed service; 2 Rec. ITU-R M.2089-0 d) that the frequency range 14.5-14.8 GHz is also globally allocated on a primary basis to the fi

16、xed-satellite service (Earth-to-space) under the provisions of RR No. 5.510, recognizing further a) that in Regions 1 and 3, the use of the frequency range 14.5-14.8 GHz by the broadcasting satellite service for feeder links (Earth-to-space), is reserved for countries outside Europe operating under

17、the provisions and associated plans of Appendix 30A to the Radio Regulations; b) that the use of the frequency range 14.5-14.8 GHz by the AMS in no way restricts or limits the operation of feeder link to broadcasting satellite service referred to in recognizing further a) above; c) that the use of t

18、he frequency range 14.5-15.35 GHz by the AMS must take into account the operation of the fixed service referred to in recognizing c) above, recommends 1 that the technical and operational characteristics of the systems operating in the AMS described in the Annex should be considered representative o

19、f those operating in the frequency range 14.5-15.35 GHz; 2 that the technical characteristics and protection criteria for AMS receiving and transmitting stations given in the Annex should be used in performing sharing and compatibility analyses as needed. Annex Technical characteristics and protecti

20、on criteria for aeronautical mobile service systems in the frequency range 14.5-15.35 GHz 1 Introduction Systems and networks operating in the AMS are increasingly used by local and national governments, as well as civil sector and educational entities, for broadband, airborne data links to support

21、remote sensing applications e.g. earth sciences, land management, and energy distribution. Examples of these applications include, e.g. monitoring Arctic sea ice thickness and distribution, local and national law enforcement, forest fire mapping, pipeline monitoring, agricultural and urban land use,

22、 and natural resource surveys). The remote sensing equipment may be on board either manned aircraft or unmanned aeronautical systems (UAS). In the case where the remote sensing equipment is on board a UAS, systems and networks operating in the AMS may be used for narrow-band, airborne command and co

23、ntrol data links. These narrow-band data links may be used to command and control either or both the remote sensor equipment and the UAS. 2 Operational deployment In the frequency range 14.5-15.35 GHz, the mobile service is allocated on a primary basis in all three ITU-R regions. The AMS is a mobile

24、 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. Rec. ITU-R M.2089-0 3 An ADL may exist

25、 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. ADLs are bidirectional by design and may operate in either a narrow-band or wideband mode in one or both directions depending upon operatio

26、nal requirements. The GDT may be at a single permanent location or they may be transportable. Transportable GDTs can be moved 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

27、 generally limited by the radio-line-of-sight (RLoS) horizon which is a function of the terrain in the vicinity of the GDT and the altitude of the ADT. The operational altitude of airborne platforms equipped with these ADLs depends on specific operational requirements and can vary up to approximatel

28、y 20 km. Although some of the link lengths may be relatively short, many of the link distances approach RLoS horizon distance. For an air-to-ground link, this link distance may be approximately 450 km for an AMS data link at an altitude of approximately 20 km. The link between two ADTs operates in t

29、he same 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-air link, this link distance may be approximately 900 km. Other factors to consider, such as atmospheric losses (rain

30、attenuation, gases, etc.) and clutter losses, as described in the ITU-R Recommendations P-series, could reduce the maximum distance of the link between two aircraft. Depending on the environmental conditions and locations of the aircraft, the crosslink distance might be shorter than 900 km. A single

31、 ground terminal may support several aeronautical terminals 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 are operating in a wideband mode, multiple data links may be supported through geogra

32、phic separation using multiple high-gain, narrow-beam antennas. The 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. Thus, the time duration during which an ADL can be

33、 active may extend for many hours. During the flight, tracking of directional AMS antennas (both GDT and ADT) are maintained using information exchanged through the link. In case of link loss, antenna tracking information is also lost, and due to aircraft movement, the correct antennas pointing coul

34、d be no longer maintained. In this case, a full link recovery procedure must be initiated, and the duration of that interruption of service depends on the aircraft speed and the position of the pre-planned rendezvous point that the aircraft must reach to resume the communication. 3 Technical charact

35、eristics of aeronautical mobile systems Representative technical characteristics for airborne data links in the AMS for the frequency range 14.5-15.35 GHz are provided in Table 1. 3.1 Transmitter characteristics The aeronautical mobile systems operating or planned to operate in the frequency band 14

36、.5-15.35 GHz typically use digital modulations. A given transmitter may be capable of radiating more than one waveform. Solid-state power amplifier output devices are typically used in the transmitters. The trend towards use of solid-state transmitters in new mobile systems will continue for the for

37、eseeable future due to the wide bandwidth, low level of generated spurious emissions, low power consumption, and reliability of these devices. 4 Rec. ITU-R M.2089-0 Typical transmitter RF emission (3 dB) bandwidths of mobile systems operating or planned to operate in the frequency band 14.5-15.35 GH

38、z range from about 0.3-120 MHz. Transmitter peak output powers range from 0.001 W (0 dBm) to 100 W (50 dBm) and are adjustable. However, the maximum power level at the input to the antenna is limited to 10 dBW in the 14.5-14.8 GHz frequency range by RR Article 21.5. Within the frequency range of 14.

39、5-14.8 GHz, the transmitted power can be adjusted such that it operates within the isotropically radiated power of 45 dBW when the direction of maximum radiation of the antenna is within 1.5 degrees of the geostationary-satellite orbit by RR Article 21.2. 3.2 Receiver characteristics The newer gener

40、ation of aeronautical mobile systems in the frequency range 14.5-15.35 GHz use digital signal processing to enhance system performance. The signal processing in the newer generation of aeronautical mobile systems may use direct sequence spread spectrum or other advanced techniques to produce a proce

41、ssing gain for the desired signal and may also provide suppression of undesired signals. 3.3 Antenna characteristics A variety of different types of antennas are used by systems in the frequency range 14.5-15.35 GHz. Antennas in this band are generally of a variety of sizes and vary between the airb

42、orne component of the link and the ground based component of the link. The airborne antennas gain is typically in the range 3 to 27.5 dBi. The ground-based antenna gain is typically in the range 0-45 dBi. Horizontal, vertical and circular polarizations are used. If antenna characteristics provided i

43、n Table 1 are sufficient, these characteristics should be used in sharing analyses. If additional 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 use

44、d. 4 Protection criteria for the aeronautical mobile service in the frequency range 14.5-15.35 GHz When operating near the maximum radio line-of-sight distance separation between the transmitter and receiver, the performance of the communication link is often noise limited. An increase in receiver e

45、ffective noise of 1 dB would constitute significant degradation communication range, equivalent to a reduction in communication range of approximately 10% in a free-space propagation environment. Such an increase effective receiver noise corresponds to an (I + N)/N ratio of 1.26, or an I/N ratio of

46、about 6 dB. This 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 from the

47、 multiple sources. It is noted that, in the case where an administration wishing to operate an AMS system does not have bilateral coordination agreements with affected administrations, the level of interference from existing stations in the fixed service may exceed this protection criteria. Sharing

48、studies should take this into account. Rec. ITU-R M.2089-0 5 TABLE 1 Representative technical characteristics of the aeronautical mobile service systems in the frequency range 14.5-15.35 GHz Parameter Units System 1 Airborne System 1 Ground System 2 Airborne System 2 Ground Transmitter Tuning range

49、GHz 15.15-15.35 14.50-14.83 14.50-14.83 15.15-15.35 Power output 1 dBm 0 to 30 30 to 50 20 30 to 50 Bandwidth 3 dB MHz 0.354 / 3.5 / 10 / 120 0.354 / 3.5 / 10 / 60 / 120 0.354 / 3.5 / 10 / 60 / 120 0.354 / 3.5 / 10 / 120 20 dB MHz 21 / 21.4 / 57.4 / 285 21 / 25 / 60 / 190 / 400 21 / 25 / 60 / 190 / 400 21 / 21.4 / 57.4 / 285 60 dB MHz 108 / 181 / 219 / 630 100 / 110 / 120 / 240 / 480 100 / 110 / 120 / 240 / 480 108 / 181 / 219 / 630 Harmonic attenuation dB 65 60 60 65 Spurious attenuation dB 80 52 52 80 Modulation OQPSK OQPSK OQPSK OQPSK Receiver Tuning range GHz 14.50-14.83 15.15-15.35