VHF air-ground and air-air Digital Link (VDL) Mode 4 radio equipment - Technical characteristics and methods of measurement for aeronautical mobile (airborne) equipment - Part 1: Physical layer

Editorial modification: paragraph added in the foreword

Radijska oprema za digitalno povezavo VHF (VDL) zrak-tla in zrak-zrak, 4. način - Tehnične karakteristike in merilne metode za aeronavtično mobilno (letalsko) opremo - 1. del: Fizična plast

Ta dokument velja za naslednje vrste radijske opreme:
• zelo visokofrekvenčno (VHF) digitalno povezavo (VDL) aeronavtičnih mobilnih (zračnih) radijskih oddajnikov, oddajnikov-prejemnikov in prejemnikov za komunikacije zrak-tla in zrak-zrak, 4. način, ki deluje v pasu VHF z uporabo modulacije frekvenčnega premičnega kodiranja prek filtra Gaussian (GFSK) z razmikom med kanali 25 kHz in je zmožna uravnavati na katerem koli izmed kanalov 25 kHz od 118.000 MHz do 136.975 MHz, kot je opredeljeno v SARPs ICAO za VDL [2].
Ta dokument zagotavlja 1. del tehničnih specifikacij.
Ta dokument zagotavlja, da bo oprema, ki jo certificira, združljiva z ustreznimi SARPs za ICAO VDL [2] in tehničnim priročnikom ICAO za VDL4 [1].
Proizvajalci morajo biti pozorni, da razpon uravnavanja za oddajnik lahko v prihodnje zajema kateri koli kanal 25 kHz od 112.000 MHz do 117.975 MHz in za prejemnike kateri koli kanal 25 kHz od 108.000 MHz do 117.975 MHz.
Ta dokument velja za »aeronavtično mobilno (za zračna vozila in v nekaterih primerih talna vozila)« opremo, v nadaljevanju »mobilna« oprema.
Področje uporabe tega dokumenta je omejeno na mobilne postaje. Ustrezna specifikacija za talne postaje je v EN 301 842 [10].
Sistem VDL, 4. način, zagotavlja digitalne komunikacijske izmenjave med zračnim plovilom in zemeljskim sistemom ter drugimi aplikacijami, ki podpirajo nadzor in komunikacije. Podporni načini komunikacije vključujejo:
• oddajanje in komunikacijo tipa točka-točka;
• storitve oddajanja, vključno z zmožnostmi samodejnega odvisnega nadzora - oddajanje (ADS-B), storitve prometnih informacij - oddajanje (TIS-B) in storitve informacij o letih – oddajanje (FIS-B);
• storitve zrak-zrak in tla-zrak;
• delovanje brez zemeljske infrastrukture.
Ta dokument je izpeljan iz naslednjih specifikacij:
• tehnični priročnik za VDL4 ICAO [1] in SARPs ICAO za VDL [2], izdanih pod okriljem
Mednarodne organizacije za civilno letalstvo (ICAO);
• drugih ustreznih standardov, kot je opredeljeno v točki 2.
Predvideva se, da proizvajalec lahko zagotovi opremo, ki podpira:
• samo storitve oddajanja;
• samo storitve točka-točka;
• storitve oddajanja in storitve točka-točka.
Ta dokument obravnava preskuse fizične plasti, potrebne za podporo vseh tipov opreme.
Ta dokument vključuje:
• točko 2, ki se sklicuje na ustrezne dokumente;
• točko 3, ki podaja uporabljene splošne definicije, okrajšave in simbole;
• točko 4, ki podaja splošni opis in arhitekturo za VDL, 4. način;
• točko 5, ki podaja funkcionalne specifikacije, ki veljajo za fizično plast, vključno z zahtevami za oddajnik/sprejemnik ter modulacijsko shemo;
• točko 6, ki podaja splošne zahteve za opremo VDL, 4 način;
• točko 7, ki podaja splošne zahteve za načrtovanje;
• točko 8, ki podaja splošne zahteve za okoljsko preskušanje;
• točko 9, ki podaja podrobne preskusne postopke za fizično plast;
• točko 10, ki podaja zahteve za nameščeno opremo;
• dodatek A, ki podaja podrobno sklicevanje na ustrezne zahteve, zajete v sklicu [1];
• dodatek B, ki podaja oceno zaloge povezav za VDL, 4. način;
• dodatek C, ki podaja bibliografijo;
• zgodovino dokumenta.
Podani so celotni preskusi fizične plasti, ki zelo ustrezajo standardnemu sklopu preskusov, uporabljenih za druge sisteme VDL.
OPOMBA: Preskusi letenja so opredeljeni v EN 302 842-2 [7].
Fraze, ki zahtevajo in ki priporočajo:
a) »Mora«
- Uporaba besede »mora« nakazuje obvezni kriterij; npr. skladnost z določenim postopkom ali specifikacijo je obvezna in nobena druga možnost se ne sme uporabiti.
b) »Naj«
- Uporaba besede »naj« (in fraze, kot je »Priporoča se, da …« itd.) nakazuje, da čeprav se postopek ali merilo šteje za prednostno možnost, se lahko uporabijo drugi postopki, specifikacije ali merila, pod pogojem, da proizvajalec, monter in preizkuševalec lahko zagotovijo informacije ali podatke, s katerimi ustrezno podprejo in upravičijo drugo možnost.

General Information

Status
Published
Publication Date
04-Aug-2011
Technical Committee
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
21-Jul-2011
Due Date
25-Sep-2011
Completion Date
05-Aug-2011

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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.VHF air-ground and air-air Digital Link (VDL) Mode 4 radio equipment - Technical characteristics and methods of measurement for aeronautical mobile (airborne) equipment - Part 1: Physical layer49.090On-board equipment and instruments35.100.10Physical layer33.060.99Druga oprema za radijske komunikacijeOther equipment for radiocommunicationsICS:Ta slovenski standard je istoveten z:EN 302 842-1 Version 1.2.3SIST EN 302 842-1 V1.2.3:2011en01-september-2011SIST EN 302 842-1 V1.2.3:2011SLOVENSKI
STANDARD



SIST EN 302 842-1 V1.2.3:2011



ETSI EN 302 842-1 V1.2.3 (2011-07)European Standard VHF air-ground and air-air Digital Link (VDL)Mode 4 radio equipment;Technical characteristics and methods of measurementfor aeronautical mobile (airborne) equipment;Part 1: Physical layer SIST EN 302 842-1 V1.2.3:2011



ETSI ETSI EN 302 842-1 V1.2.3 (2011-07) 2
Reference REN/AERO-00011-1 Keywords aeronautical, digital, radio, testing, VHF ETSI 650 Route des Lucioles F-06921 Sophia Antipolis Cedex - FRANCE
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Important notice Individual copies of the present document can be downloaded from: http://www.etsi.org The present document may be made available in more than one electronic version or in print. In any case of existing or perceived difference in contents between such versions, the reference version is the Portable Document Format (PDF). In case of dispute, the reference shall be the printing on ETSI printers of the PDF version kept on a specific network drive within ETSI Secretariat. Users of the present document should be aware that the document may be subject to revision or change of status. Information on the current status of this and other ETSI documents is available at http://portal.etsi.org/tb/status/status.asp If you find errors in the present document, please send your comment to one of the following services: http://portal.etsi.org/chaircor/ETSI_support.asp Copyright Notification No part may be reproduced except as authorized by written permission. The copyright and the foregoing restriction extend to reproduction in all media.
© European Telecommunications Standards Institute 2011. All rights reserved.
DECTTM, PLUGTESTSTM, UMTSTM and 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 are Trade Marks registered and owned by the GSM Association. SIST EN 302 842-1 V1.2.3:2011



ETSI ETSI EN 302 842-1 V1.2.3 (2011-07) 3 Contents Intellectual Property Rights . 6 Foreword . 6 Introduction . 7 1 Scope . 8 2 References . 10 2.1 Normative references . 10 2.2 Informative references . 11 3 Definitions and abbreviations . 11 3.1 Definitions . 11 3.1.1 Basic reference model definitions . 11 3.1.2 Service conventions definitions . 11 3.1.3 General definitions . 12 3.2 Abbreviations . 15 4 General description and architecture of VDL Mode 4 . 16 4.1 General . 16 5 VDL mode 4 physical layer functional specifications . 17 5.1 Overview . 17 5.1.1 Functions . 17 5.1.2 Data reception . 17 5.1.3 Data transmission . 17 5.2 Modulation scheme . 17 6 VDL Mode 4 equipment requirements . 18 6.1 Receiver requirements . 18 6.1.1 Receiver operating range . 18 6.1.2 BER requirement . 18 6.1.3 Reference signal level . 18 6.1.4 Sensitivity . 18 6.1.5 Adjacent channel rejection . 19 6.1.6 Receiver performance in the presence of strong signals inside the VHF aeronautical band . 19 6.1.7 Receiver performance in the presence of strong signals outside the VHF aeronautical band . 19 6.1.8 Desired signal dynamic range . 20 6.1.9 Symbol rate capture range . 20 6.1.10 Frequency capture range . 20 6.1.11 Doppler rate . 20 6.1.12 Co-channel interference . 21 6.1.13 Conducted spurious emission . 21 6.1.14 FM broadcast intermodulation . 21 6.1.14.1 Radio frequencies in the band 117,975 MHz to 137 MHz . 21 6.1.15 In-band intermodulation . 21 6.2 Transmitter requirements . 22 6.2.1 Transmitter operating range . 22 6.2.2 Channel bit rate . 22 6.2.3 Manufacturer's declared output power . 22 6.2.4 RF power rise time . 22 6.2.5 RF power release time . 23 6.2.6 Spurious emissions . 23 6.2.7 Adjacent channel power . 24 6.2.8 Wide-band noise . 24 6.2.9 Load VSWR capability . 25 6.2.10 Adjacent channel transient power . 25 6.2.11 Frequency tolerance . 25 6.2.12 Start of transmission . 25 SIST EN 302 842-1 V1.2.3:2011



ETSI ETSI EN 302 842-1 V1.2.3 (2011-07) 4 6.2.13 Structure of bursts . 25 6.3 Transceiver requirements . 26 6.3.1 Automatic transmitter shut-down . 26 6.3.2 Tuning time . 26 6.3.3 Receiver to transmitter turnaround time . 26 6.3.4 Transmitter to receiver turnaround time . 26 6.3.5 Short power interrupt . 26 6.3.6 Demodulator action. 26 6.3.7 System timing requirements . 27 6.3.8 Reservation table stored in memory . 27 6.3.9 Failure of associated equipment . 27 6.3.10 Simultaneous reception . 27 7 General design requirements . 27 7.1 Controls and indicators . 27 7.2 Class of emission and modulation characteristics . 27 7.3 Warm up . 27 7.4 Airworthiness . 28 7.5 Intended function . 28 7.6 International Telecommunications Union Regulations . 28 7.7 Fire protection . 28 7.8 Operation of controls . 28 7.9 Accessibility of controls . 28 7.10 Effects of tests . 28 7.11 Failure of VDL Mode 4 equipment . 28 7.12 Software management . 28 7.13 Transceiver configuration . 29 7.14 Provision for multiple redundant VDL4 transceivers . 29 7.15 Reception capability . 29 7.16 Transmission capability . 29 7.17 Monitoring of proper operation . 30 7.18 Power-up self test . 30 8 Environmental test requirements . 30 8.1 Introduction . 30 8.2 Receiver . 31 8.3 Transmitter . 33 9 Detailed test procedures for the physical layer . 35 9.1 General requirements . 35 9.1.1 Test conditions . 35 9.1.2 Alignment, adjustment and calibration prior to test . 35 9.1.3 Recording of test results . 35 9.1.4 Connected load . 35 9.1.5 Test instrument precautions . 35 9.1.6 Simultaneous application of two signals to the receiver input . 36 9.1.7 Test frequencies . 36 9.1.8 Equipment configuration . 36 9.1.9 Detailed physical and MAC layer test procedures . 36 9.2 Receiver . 36 9.2.1 BER test . 36 9.2.2 Sensitivity . 38 9.2.3 Adjacent Channel Rejection (ACR) . 38 9.2.4 Rejection of signals in the VHF aeronautical band . 39 9.2.5 Rejection of signals outside the VHF aeronautical band . 40 9.2.6 Desired signal dynamic range . 41 9.2.7 Symbol rate capture range . 41 9.2.8 Frequency capture range . 42 9.2.9 Doppler rate . 42 9.2.10 Co-channel interference . 43 9.2.11 Conducted spurious emission . 43 9.2.12 FM broadcast intermodulation . 44 9.2.13 In-band intermodulation . 45 SIST EN 302 842-1 V1.2.3:2011



ETSI ETSI EN 302 842-1 V1.2.3 (2011-07) 5 9.3 Transmitter . 46 9.3.1 Channel bit rate . 46 9.3.2 Manufacturer's declared output power . 46 9.3.3 RF power rise time . 47 9.3.4 RF power release time . 47 9.3.5 Spurious emissions . 48 9.3.6 Adjacent channel power . 48 9.3.6.1 Method of measurement for the first adjacent channel . 48 9.3.6.2 Method of measurement for the second adjacent channel . 49 9.3.6.3 Method of measurement for the fourth adjacent channel . 50 9.3.6.4 Alternative measurement procedure for Adjacent Channel Power (ACP) . 51 9.3.7 Wideband noise . 52 9.3.8 Load VSWR capability . 53 9.3.9 Adjacent channel transient power . 54 9.3.10 Frequency tolerance . 55 9.4 Transceiver . 55 9.4.1 Tuning time . 55 9.4.2 Receiver to transmitter turn-around time . 55 9.4.3 Transmitter to receiver turn-around time . 56 10 Installed equipment requirements . 56 10.1 Introduction . 56 10.2 Equipment installation . 56 10.2.1 Aircraft environment. 56 10.2.2 Failure protection . 56 10.2.3 Aircraft power source . 57 10.3 Installed equipment performance requirements. 57 10.3.1 Dynamic response . 57 10.3.2 Interference effects . 57 10.3.3 Regular maintenance. 57 10.4 Conditions of test . 57 10.4.1 Power input . 57 10.4.2 Associated equipment or systems . 57 10.4.3 Environment . 57 10.5 Test procedures for installed equipment performance . 58 10.5.1 Ground test procedures . 58 10.5.1.1 Conformity inspection . 58 10.5.1.2 Interference tests . 58 10.5.1.3 Power supply fluctuation test . 58 10.5.1.4 Reception . 58 10.5.1.5 Transmission . 58 10.5.1.6 Functional behaviour tests . 59 10.5.1.7 Interface conformance tests . 59 10.5.2 Flight test procedures . 59 10.5.2.1 Interference effects . 59 10.5.2.2 System performance . 60 Annex A (informative): Cross reference matrix . 61 Annex B (informative): VDL Mode 4 link budget . 64 Annex C (informative): Bibliography . 71 History . 74
SIST EN 302 842-1 V1.2.3:2011



ETSI ETSI EN 302 842-1 V1.2.3 (2011-07) 6 Intellectual Property Rights IPRs essential or potentially essential to the present document may have been declared to ETSI. The information pertaining to these essential 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 are available on the ETSI Web server (http://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) which are, or may be, or may become, essential to the present document. Foreword This European Standard (EN) has been produced by ETSI Technical Committee Aeronautics (AERO). The present document is part 1 of a multi-part deliverable covering the VHF air-ground and air-air Digital Link (VDL) Mode 4 radio equipment; Technical characteristics and methods of measurement for aeronautical mobile (airborne) equipment, as identified below: Part 1: "Physical layer"; Part 2: "General description and data link layer"; Part 3: "Additional broadcast aspects"; Part 4: "Point-to-point functions"; The present document is accompanied by an equivalent ground-based standard, EN 301 842 [10] parts 1 to 5, covering
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