1、 ETSI EN 302 186 V2.1.1 (2016-05) Satellite Earth Stations and Systems (SES); Harmonised Standard for satellite mobile Aircraft Earth Stations (AESs) operating in the 11/12/14 GHz frequency bands covering the essential requirements of article 3.2 of the Directive 2014/53/EU HARMONISED EUROPEAN STAND
2、ARD ETSI ETSI EN 302 186 V2.1.1 (2016-05) 2 Reference REN/SES-00392 Keywords aeronautical, air interface, AMSS, earth station, FSS, GSO, mobile, MSS, regulation, satellite ETSI 650 Route des Lucioles F-06921 Sophia Antipolis Cedex - FRANCE Tel.: +33 4 92 94 42 00 Fax: +33 4 93 65 47 16 Siret N 348 6
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7、al, including photocopying and microfilm except as authorized by written permission of ETSI. The content of the PDF version shall not be modified without the written authorization of ETSI. The copyright and the foregoing restriction extend to reproduction in all media. European Telecommunications St
8、andards Institute 2016. All rights reserved. DECTTM, PLUGTESTSTM, UMTSTMand the ETSI logo are Trade Marks of ETSI registered for the benefit of its Members. 3GPPTM and LTE are Trade Marks of ETSI registered for the benefit of its Members and of the 3GPP Organizational Partners. GSM and the GSM logo
9、are Trade Marks registered and owned by the GSM Association. ETSI ETSI EN 302 186 V2.1.1 (2016-05) 3 Contents Intellectual Property Rights 7g3Foreword . 7g3Modal verbs terminology 7g3Introduction 7g31 Scope 9g32 References 10g32.1 Normative references . 10g32.2 Informative references 10g33 Definitio
10、ns, symbols and abbreviations . 11g33.1 Definitions 11g33.2 Symbols 14g33.3 Abbreviations . 14g34 Technical requirement specifications . 15g34.1 General . 15g34.1.0 Introduction. 15g34.1.1 Environmental profile . 16g34.2 Conformance requirements 16g34.2.1 General 16g34.2.2 Spurious radiation . 16g34
11、.2.2.1 Justification . 16g34.2.2.2 Specification 16g34.2.2.3 Conformance tests . 17g34.2.3 On-axis spurious radiation 17g34.2.3.1 Justification . 17g34.2.3.2 Specification 17g34.2.3.2.1 “Carrier-on“ state . 17g34.2.3.2.2 “Carrier-off“ state and “transmission disabled“ state . 18g34.2.3.3 Conformance
12、 tests . 18g34.2.4 Off-axis EIRP emissions density in the nominated bandwidth . 18g34.2.4.1 Justification . 18g34.2.4.2 Specification 18g34.2.4.3 Conformance tests . 19g34.2.5 Control and Monitoring Functions (CMF) 19g34.2.5.0 General 19g34.2.5.1 Processor monitoring 20g34.2.5.1.1 Justification . 20
13、g34.2.5.1.2 Specification 20g34.2.5.1.3 Conformance tests . 21g34.2.5.2 Transmit subsystem monitoring 21g34.2.5.2.1 Justification . 21g34.2.5.2.2 Specification 21g34.2.5.2.3 Conformance tests . 21g34.2.5.3 Power-on/Reset . 21g34.2.5.3.1 Justification . 21g34.2.5.3.2 Specification 21g34.2.5.3.3 Confo
14、rmance tests . 21g34.2.5.4 Control Channel (CC) reception . 21g34.2.5.4.1 Justification . 21g34.2.5.4.2 Specification 21g34.2.5.4.3 Conformance tests . 21g34.2.5.5 Network control commands 22g34.2.5.5.1 Justification . 22g34.2.5.5.2 Specification 22g34.2.5.5.3 Conformance tests . 22g3ETSI ETSI EN 30
15、2 186 V2.1.1 (2016-05) 4 4.2.5.6 Initial burst transmission . 22g34.2.5.6.1 General 22g34.2.5.6.2 Specification 22g34.2.5.6.3 Conformance tests . 23g34.2.6 Power Flux Density at the surface of the earth . 23g34.2.6.1 General 23g34.2.6.2 Power flux density limits in the 14,00 GHz to 14,50 GHz frequen
16、cy band 23g34.2.6.2.1 Justification . 23g34.2.6.2.2 Specification 1: Mode of PFD limitation . 23g34.2.6.2.3 Specification 2: Location where to limit the PFD . 24g34.2.6.2.4 Specification 3: PFD limitation . 24g34.2.6.2.5 Specification 4: Fault conditions . 25g34.2.6.2.6 Conformance tests . 25g34.2.7
17、 Receive antenna off-axis gain pattern . 25g34.2.7.1 Justification . 25g34.2.7.2 Specification 25g34.2.7.3 Conformance tests . 26g34.2.8 Blocking performance. 26g34.2.8.1 Justification . 26g34.2.8.2 Specification 26g34.2.8.3 Conformance tests . 26g34.2.9 Adjacent Signal Selectivity . 26g34.2.9.1 Jus
18、tification . 26g34.2.9.2 Specification 26g34.2.9.3 Conformance tests . 27g35 Testing for compliance with technical requirements 27g35.1 Environmental conditions for testing . 27g35.2 Essential radio test suites 27g36 Test methods 27g36.0 General . 27g36.1 Spurious radiation. 28g36.1.1 Test method 28
19、g36.1.1.0 Introduction . 28g36.1.1.1 Up to 1 000 MHz (see clause 4.2.2.2, table 2) 29g36.1.1.1.1 Test site 29g36.1.1.1.2 Measuring receivers . 29g36.1.1.1.3 Procedure . 29g36.1.1.2 Above 1 000 MHz (see clause 4.2.2.2, tables 3 and 4) . 29g36.1.1.2.0 General 29g36.1.1.2.1 Identification of the signif
20、icant frequencies of spurious radiation 30g36.1.1.2.2 Measurement of radiated power levels of identified spurious radiation 30g36.2 On-axis spurious radiation 31g36.2.1 Test method 31g36.2.1.1 Test site . 31g36.2.1.2 Method of measurement 31g36.2.1.2.1 General 31g36.2.1.2.2 Method of measurement at
21、the antenna flange 32g36.2.1.2.3 Method of measurement with a test antenna . 32g36.3 Off-axis EIRP emissions density in the nominated bandwidth 33g36.3.1 General 33g36.3.2 rms antenna pointing accuracy 34g36.3.2.1 Method of measurement 34g36.3.3 Measurement of the off-axis EIRP without the antenna .
22、 35g36.3.3.1 Transmitter output power density . 35g36.3.3.1.0 General 35g36.3.3.1.1 Method of measurement 35g36.3.3.2 Antenna transmit gain . 35g36.3.3.2.1 General 35g36.3.3.2.2 Test site 35g36.3.3.2.3 Method of measurement 36g3ETSI ETSI EN 302 186 V2.1.1 (2016-05) 5 6.3.3.3 Antenna transmit radiati
23、on patterns 37g36.3.3.3.1 General 37g36.3.3.3.2 Test site 37g36.3.3.3.3 Method of measurement 37g36.3.3.4 Computation of results 38g36.3.4 Measurement of the off-axis EIRP with the antenna 38g36.3.4.1 General 38g36.3.4.2 Maximum EIRP density per 40 kHz ratio relative to the EIRP . 38g36.3.4.2.0 Gene
24、ral 38g36.3.4.2.1 Method of measurement 38g36.3.4.3 Maximum on-axis EIRP 39g36.3.4.3.1 General 39g36.3.4.3.2 Test site 39g36.3.4.3.3 Method of measurement 39g36.3.4.4 Antenna transmit radiation patterns 41g36.3.4.4.1 General 41g36.3.4.4.2 Test site 41g36.3.4.4.3 Method of measurement 41g36.3.4.5 Com
25、putation of results 42g36.4 Power Flux Density Test 42g36.4.1 General 42g36.4.2 Verification of specification 1: Mode of PFD limitation 43g36.4.3 Verification of specification 2: Location where to limit the PFD . 43g36.4.4 Verification of specification 3: PFD limitation . 43g36.4.4.1 Measurement of
26、the antenna radiation pattern below the aircraft fuselage . 43g36.4.4.1.1 General 43g36.4.4.1.2 Test site 43g36.4.4.1.3 Test method procedure 43g36.4.4.2 Measurement of on-axis EIRP as a function of altitude 44g36.4.4.2.1 General 44g36.4.4.2.2 Test site 45g36.4.4.2.3 Method of measurement with a tes
27、t antenna . 45g36.4.4.3 Computation of the power flux density at the surface of the Earth . 46g36.4.5 Verification of specification 4: Fault conditions . 46g36.4.5.1 Test Arrangement 46g36.4.5.2 Test method . 46g36.5 Control and monitoring 47g36.5.0 General 47g36.5.1 Test arrangement 47g36.5.2 Proce
28、ssor monitoring 48g36.5.2.1 Test method . 48g36.5.3 Transmit subsystem monitoring 48g36.5.3.1 Test method . 48g36.5.4 Power-on/Reset . 49g36.5.4.1 Test method . 49g36.5.5 Control Channel (CC) reception . 49g36.5.5.1 Test method . 49g36.5.6 Network control commands 50g36.5.6.1 Test method . 50g36.5.7
29、 Initial burst transmission . 51g36.5.7.1 Test method . 51g36.6 Receive antenna off-axis gain pattern 51g36.6.1 Test method 51g36.6.1.1 Test site . 51g36.6.1.2 Method of measurement 52g36.6.1.3 Computation 52g36.7 Blocking performance 52g36.7.1 Test method 52g36.8 Adjacent Signal Selectivity 53g36.8
30、.1 Test method 53g3ETSI ETSI EN 302 186 V2.1.1 (2016-05) 6 Annex A (normative): Relationship between the present document and the essential requirements of Directive 2014/53/EU . 54g3Annex B (normative): Environmental conditions . 56g3B.1 General . 56g3B.2 Environmental conformance requirements. 56g
31、3B.3 Environmental test conditions 56g3Annex C (informative): Bibliography . 58g3History 59g3ETSI ETSI EN 302 186 V2.1.1 (2016-05) 7 Intellectual Property Rights IPRs essential or potentially essential to the present document may have been declared to ETSI. The information pertaining to these essent
32、ial IPRs, if any, is publicly available for ETSI members and non-members, and can be found in ETSI SR 000 314: “Intellectual Property Rights (IPRs); Essential, or potentially Essential, IPRs notified to ETSI in respect of ETSI standards“, which is available from the ETSI Secretariat. Latest updates
33、are available on the ETSI Web server (https:/ipr.etsi.org/). Pursuant to the ETSI IPR Policy, no investigation, including IPR searches, has been carried out by ETSI. No guarantee can be given as to the existence of other IPRs not referenced in ETSI SR 000 314 (or the updates on the ETSI Web server)
34、which are, or may be, or may become, essential to the present document. Foreword This Harmonised European Standard (EN) has been produced by ETSI Technical Committee Satellite Earth Stations and Systems (SES). The present document has been prepared under the Commissions standardisation request C(201
35、5) 5376 final i.2 to provide one voluntary means of conforming to the essential requirements of Directive 2014/53/EU on the harmonisation of the laws of the Member States relating to the making available on the market of radio equipment and repealing Directive 1999/5/EC 6. Once the present document
36、is cited in the Official Journal of the European Union under that Directive, compliance with the normative clauses of the present document given in table A.1 confers, within the limits of the scope of the present document, a presumption of conformity with the corresponding essential requirements of
37、that Directive, and associated EFTA regulations. National transposition dates Date of adoption of this EN: 16 May 2016 Date of latest announcement of this EN (doa): 31 August 2016 Date of latest publication of new National Standard or endorsement of this EN (dop/e): 28 February 2017 Date of withdraw
38、al of any conflicting National Standard (dow): 28 February 2018 Modal verbs terminology In the present document “shall“, “shall not“, “should“, “should not“, “may“, “need not“, “will“, “will not“, “can“ and “cannot“ are to be interpreted as described in clause 3.2 of the ETSI Drafting Rules (Verbal
39、forms for the expression of provisions). “must“ and “must not“ are NOT allowed in ETSI deliverables except when used in direct citation. Introduction The present document is part of a set of standards developed by ETSI and is designed to fit in a modular structure to cover all radio equipment within
40、 the scope of the Directive 2014/53/EU 6. Each standard is a module in the structure. The modular structure is shown in ETSI EG 201 399 i.1. The requirements have been selected to ensure an adequate level of compatibility with other radio services. ETSI ETSI EN 302 186 V2.1.1 (2016-05) 8 The present
41、 document may not cover those cases where a potential source of interference which is producing individually repeated transient phenomena or a continuous phenomenon is present, e.g. a radar or broadcast site in the near vicinity. In such a case it may be necessary to use special protection applied t
42、o either the source of interference, or the interfered part or both. The present document does not contain any requirement, recommendation or information about the installation of the AES on aircraft. The determination of the parameters of the AES using a given GeoStationary Orbiting (GSO) satellite
43、 for the protection of the spectrum allocated to that satellite, is considered to be under the responsibility of the satellite operator or the satellite network operators. ETSI ETSI EN 302 186 V2.1.1 (2016-05) 9 1 Scope The present document specifies certain minimum technical performance requirement
44、s of Aircraft Earth Station (AES) equipment with both transmit and receive capabilities for provision of aeronautical mobile satellite service, in the frequency bands given in table 1. Table 1: Frequency bands for the AES equipment specified in the present document Mode of Operation Frequency Band A
45、ES transmit 14,00 GHz to 14,50 GHz AES receive 10,70 GHz to 11,70 GHz AES receive 12,50 GHz to 12,75 GHz NOTE: The AESs are operating in one or more frequency ranges of the Fixed and Mobile-Satellite Services. The AES has the following characteristics: These AESs are equipment for installation on ai
46、rcraft. The AES could consist of a number of modules from the antenna subsystem to the user interfaces. The AES uses linear polarization. The AES system uses digital modulation. The AES operates through a GSO satellite at least 3 away from any other geostationary satellite operating in the same freq
47、uency band and covering the same area. The antenna of the AES is directional, with means of tracking the satellites, which can be achieved by using either an active phase array or reflective type configuration. These AESs are operating as part of a satellite network used for the distribution and/or
48、exchange of information between users. These AESs are controlled and monitored by a Network Control Facility (NCF). The NCF is outside the scope of the present document. When on the ground, the AES does not transmit at elevation angles below 7owith respect to the local horizontal plane, except at lo
49、cations where transmissions below 7oare permitted by the local Administration; (the minimum elevation angle is also limited as per clause 4.2). The technical requirements in the present document are in two major categories: emission limits: to protect other radio services and systems from harmful interference generated by the AES in normal use; AES Control and Monitoring Functions (CMF): to protect other radio services and systems from unwanted transmissions from the AES. The CMF in each AES is capable of answering to commands from the Network C
