DIN EN 16603-50-01-2014 Space engineering - Space data links - Telemetry synchronization and channel coding English version EN 16603-50-01 2014《航天工程 空间数据链 遥测同步和信道编码 英文版本EN 16603-50.pdf

1、Dezember 2014DEUTSCHE NORM DIN-Normenausschuss Luft- und Raumfahrt (NL)Preisgruppe 24DIN Deutsches Institut fr Normung e. V. Jede Art der Vervielfltigung, auch auszugsweise, nur mit Genehmigung des DIN Deutsches Institut fr Normung e. V., Berlin, gestattet.ICS 49.140!%=ZI“2265538www.din.deDDIN EN 16

2、603-50-01Raumfahrtproduktsicherung Raumfahrt-Datenbertragung Telemetriesynchronisation und Kanalkodierung;Englische Fassung EN 16603-50-01:2014Space engineering Space data links Telemetry synchronization and channel coding;English version EN 16603-50-01:2014Ingnierie spatiale Liaison de donnes spati

3、ales Synchronisation et codage canal de la tlmesure;Version anglaise EN 16603-50-01:2014Alleinverkauf der Normen durch Beuth Verlag GmbH, 10772 Berlin www.beuth.deGesamtumfang 71 SeitenDIN EN 16603-50-01:2014-12 2 Nationales Vorwort Dieses Dokument (EN 16603-50-01:2014) wurde vom Technischen Komitee

4、 CEN/CLC/TC 5 Raumfahrt“ erarbeitet, dessen Sekretariat vom DIN (Deutschland) gehalten wird. Das zustndige deutsche Normungsgremium ist der Arbeitsausschuss NA 131-10-01 AA Interoperabilitt von Informations-, Kommunikations- und Navigationssystemen“ im DIN-Normenausschuss Luft- und Raumfahrt (NL). D

5、ieses Dokument (EN 16603-50-01:2014) basiert auf ECSS-E-ST-50-01C. Dieses Dokument enthlt unter Bercksichtigung des DIN-Prsidialbeschlusses 1/2004 nur die englische Originalfassung von EN 16603-50-01:2014. Dieses Dokument wurde speziell zur Behandlung von Raumfahrtsystemen erarbeitet und hat daher V

6、orrang vor jeglicher Europischer Norm, da es denselben Anwendungsbereich hat, jedoch ber einen greren Geltungsbereich (z. B. Luft- und Raumfahrt) verfgt. DIN EN 16603-50-01:2014-12 3 Nationaler Anhang NA (informativ) Begriffe und Abkrzungen 3 Begriffe und Abkrzungen 3.1 Begriffe aus anderen Normen F

7、r die Anwendung dieses Dokuments gelten die Begriffe nach ECSS-S-ST-00-01. 3.2 Fr diese Norm spezifische Begriffe 3.2.1 Kategorie A Kategorie von Raumfahrzeugen, deren Hhe ber der Erdoberflche weniger als 2 106km betrgt 3.2.2 Kategorie B Kategorie von Raumfahrzeugen mit einer Hhe ber der Erdoberflch

8、e gleich oder grer 2 106km 3.2.3 Oktett Satz von acht Binrziffern (Bits) ANMERKUNG 1 Die Benummerung von Oktetten innerhalb einer Datenstruktur beginnt mit 0. ANMERKUNG 2 Siehe 3.4 fr die Konvention zur Benummerung von Bits. 3.2.4 Bitbertragungskanal physikalischer Kanal Strom der in einer Richtung

9、ber eine Weltraum-bertragungsleitung bertragenen Bits 3.3 Abkrzungen Fr die Anwendung dieses Dokuments gelten die Abkrzungen in ECSS-S-ST-00-01 und die folgenden Abkrzungen: Abkrzung Bedeutung 8PSK Achtphasenumtastung (en: phase shift keying of eight states) AOS Hochleistungs-Orbitalsysteme (en: adv

10、anced orbiting systems) APP A-posteriori-Wahrscheinlichkeit (en: a posteriori probability) ASM zugeordneter Synchronisationsmarker (en: attached sync marker) AWGN additives weies gausches Rauschen (en: additive white Gaussian noise) BER Bitfehlerquote (en: bit error rate) DIN EN 16603-50-01:2014-12

11、4 BPSK binre Phasenumtastung (en: binary phase shift keying) CADU Kanalzugriff-Dateneinheit (en: channel access data unit) CCSDS Beratender Ausschuss fr Weltraumdatensysteme (en: Consultative Committee for Space Data Systems) CRC zyklische Redundanzprfung (en: cyclic redundancy check) FER Bitfehlerr

12、ate (en: frame error rate) GF(n) aus genau n Elementen bestehendes Galois-Feld (en: Galois field consisting of exactly n elements) GMSK gausche Minimumumtastung (en: Gaussian minimum shift keying) MSB hchstwertiges Bit (en: most significant bit) MS/S Megasymbole je Sekunde (en: mega symbols per seco

13、nd) NRZ-L Non-Return-to-Zero-Level (en: non-return to zero level) NRZ-M Non-Return-to-Zero-Mark (en: non-return to zero mark) QPSK Quadratur-Phasenumtastung (en: quadrature phase shift keying) R-S Reed-Solomon (en: Reed-Solomon) TCM Trellis-Code-Modulation (en: trellis-coded modulation) 3.4 Konventi

14、onen 3.4.1 Bit 0, Bit 1, Bit N1 Um jedes Bit in einem N-Bit-Feld zu identifizieren, ist das erste zu bertragende Bit im Feld (d. h. das in einer graphischen Darstellung am weitesten links gelegene) als Bit 0 definiert; das folgende Bit ist als Bit 1 definiert usw. bis zum Bit N-1. Bild 3-1 Benummeru

15、ngskonvention fr Bits 3.4.2 Hchstwertiges Bit Wird ein N-Bit-Feld zur Angabe eines Binrwerts genutzt (z. B. bei einer Zhlvorrichtung), handelt es sich beim hchstwertigen Bit um das erste Bit im Feld, d. h. Bit 0 (siehe Bild 3-1). EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16603-50-01 Septe

16、mber 2014 ICS 49.140 English version Space engineering - Space data links - Telemetry synchronization and channel coding Ingnierie spatiale - Liaison de donnes spatiales - Synchronisation et codage canal de la tlmesure Raumfahrtproduktsicherung - Raumfahrt-Datenbertragung - Telemetriesynchronisation

17、 und kanalkodierung This European Standard was approved by CEN on 11 April 2014. CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date

18、 lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN and CENELEC member. This European Standard exists in three official versions (English, French, German). A version in any other language made by t

19、ranslation under the responsibility of a CEN and CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium

20、, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerla

21、nd, Turkey and United Kingdom. CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16603-50-01:2014 EEN 16603-50-01:2014 (E) 2 Table

22、of contents Foreword 6 1 Scope . 7 2 Normative references . 8 3 Terms, definitions and abbreviated terms 9 3.1 Terms from other standards 9 3.2 Terms specific to the present standard . 9 3.3 Abbreviations 9 3.4 Conventions 10 4 Overview 11 4.1 Introduction . 11 4.2 Coding 11 4.2.1 Channel codes 11 4

23、.2.2 Connection vectors . 12 4.3 Convolutional codes . 12 4.4 Reed-Solomon codes . 12 4.5 Concatenated codes . 13 4.6 Turbo codes 13 4.7 Synchronization and pseudo-randomization . 13 5 Convolutional coding . 16 5.1 Properties . 16 5.2 General . 16 5.3 Basic convolutional code 17 5.4 Punctured convol

24、utional code . 18 6 Reed-Solomon coding 20 6.1 Properties . 20 6.2 General . 20 6.3 Specification . 21 6.3.1 Parameters and general characteristics 21 6.3.2 Generator polynomials 21 DIN EN 16603-50-01:2014-12 EN 16603-50-01:2014 (E) 3 6.3.3 Symbol interleaving depth . 22 6.3.4 Symbol interleaving me

25、chanism 22 6.3.5 Reed-Solomon codeblock partitioning . 23 6.3.6 Shortened codeblock length 24 6.3.7 Dual basis symbol representation and ordering . 25 6.3.8 Synchronization 26 6.3.9 Ambiguity resolution 26 6.4 Reed-Solomon with E=8 . 26 6.4.1 Introduction . 26 6.4.2 General . 27 7 Turbo coding . 28

26、7.1 Properties . 28 7.2 General . 28 7.3 Specification . 29 7.3.1 General . 29 7.3.2 Parameters and general characteristics 29 7.3.3 Turbo code permutation 30 7.3.4 Backward and forward connection vectors 32 7.3.5 Turbo encoder block . 33 7.3.6 Turbo codeblock specification . 33 7.3.7 Turbo codebloc

27、k synchronization 34 8 Frame synchronization 35 8.1 Introduction . 35 8.2 The attached sync marker (ASM) . 35 8.2.1 Overview . 35 8.2.2 Encoder side . 36 8.2.3 Decoder side . 36 8.3 ASM bit patterns . 36 8.4 Location of ASM . 37 8.5 Relationship of ASM to Reed-Solomon and turbo codeblocks 37 8.6 ASM

28、 for embedded data stream . 38 8.6.1 Overview . 38 8.6.2 Embedded ASM 38 9 Pseudo-randomizer 39 9.1 General . 39 9.1.1 Overview . 39 DIN EN 16603-50-01:2014-12 EN 16603-50-01:2014 (E) 4 9.1.2 Application 39 9.2 Pseudo-randomizer description 39 9.3 Synchronization and application of pseudo-randomizer

29、 40 9.3.1 Overview . 40 9.3.2 Application 40 9.4 Sequence specification . 41 Annex A (informative) Transformation between Berlekamp and conventional representations 43 Annex B (informative) Expansion of Reed-Solomon coefficients . 50 Annex C (informative) Compatible frame lengths 52 Annex D (informa

30、tive) Application profiles . 54 Annex E (informative) Changes from ESA-PSS-04-103 60 Annex F (informative) Differences from CCSDS recommendations 61 Annex G (informative) Mission configuration parameters . 62 Annex H (informative) Turbo code patent rights 66 Bibliography . 67 Figures Figure 3-1: Bit

31、 numbering convention . 10 Figure 4-1: Coding, randomization and synchronization (1) 14 Figure 4-2: Coding, randomization and synchronization (2) 15 Figure 5-1: Convolutional encoder block diagram . 18 Figure 5-2: Punctured encoder block diagram 19 Figure 6-1: Functional representation of R-S interl

32、eaving . 23 Figure 6-2: Reed-Solomon codeblock partitioning 24 Figure 7-1: Interpretation of permutation 31 Figure 7-2: Turbo encoder block diagram . 32 Figure 7-3: Turbo codeblocks for code rates 1/2 and 1/4 34 Figure 7-4: Turbo codeblock with attached sync marker . 34 Figure 8-1: Format of channel

33、 access data unit (CADU) . 35 Figure 8-2 ASM bit pattern for non-turbo-coded data 36 Figure 8-3: ASM bit pattern for rate 1/2 turbo-coded data . 36 Figure 8-4: ASM bit pattern for rate 1/4 turbo-coded data . 37 Figure 8-5: Embedded ASM bit pattern 38 DIN EN 16603-50-01:2014-12 EN 16603-50-01:2014 (E

34、) 5 Figure 9-1: Pseudo-randomizer configuration . 40 Figure 9-2: Pseudo-randomizer logic diagram 42 Figure A-1 : Transformational equivalence . 44 Tables Table 5-1: Basic convolutional code characteristics 17 Table 5-2: Punctured convolutional code characteristics 19 Table 5-3: Puncture code pattern

35、s for convolutional codes 19 Table 7-1: Specified information block lengths . 30 Table 7-2: Codeblock lengths (measured in bits) 30 Table 7-3: Parameters k1and k2for specified information block lengths . 31 Table 7-4: Forward connection vectors . 32 Table 8-1: ASM bit patterns in hexadecimal notatio

36、n 37 Table A-1 : Equivalence of representations (Part 1 of 4) . 46 Table B-1 : Expansion for E=16 50 Table B-2 : Expansion for E=8 51 Table C-1 : Maximum frame lengths for E=16 53 Table C-2 : Maximum frame lengths for E=8 53 Table D-1 : Preferred coding schemes . 56 Table D-2 : Coding gains and band

37、width expansions . 58 Table D-3 : Coding gains for R-S(255, 239) and 4D-8PSK-TCM 59 DIN EN 16603-50-01:2014-12 EN 16603-50-01:2014 (E) 6 Foreword This document (EN 16603-50-01:2014) has been prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard

38、(EN 16603-50-01:2014) originates from ECSS-E-ST-50-01C. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by March 2015, and conflicting national standards shall be withdrawn at the latest by March 201

39、5. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. This document has been prepared under a mandate given to CEN by the European Commis

40、sion and the European Free Trade Association. This document has been developed to cover specifically space systems and has therefore precedence over any EN covering the same scope but with a wider domain of applicability (e.g. : aerospace). According to the CEN-CENELEC Internal Regulations, the nati

41、onal standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lit

42、huania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. DIN EN 16603-50-01:2014-12 EN 16603-50-01:2014 (E) 7 1 Scope This Standard establishes a common implementation of space telemetry channel coding s

43、ystems. Several space telemetry channel coding schemes are specified in this Standard. The specification does not attempt to quantify the relative coding gain or the merits of each scheme, nor the design requirements for encoders or decoders. However, some application profiles are discussed in Annex

44、 D. Performance data for the coding schemes specified in this Standard can be found in CCSDS 130.1-G-1. Annex G describes the related mission configuration parameters. Further provisions and guidance on the application of this standard can be found in the following publications: ECSS-E-ST-50, Commun

45、ications, which defines the principle characteristics of communication protocols and related services for all communication layers relevant for space communication (physical- to application-layer), and their basic relationship to each other. The handbook ECSS-E-HB-50, Communications guidelines, whic

46、h provides information about specific implementation characteristics of these protocols in order to support the choice of a certain communications profile for the specific requirements of a space mission. Users of this present standard are invited to consult these documents before taking decisions o

47、n the implementation of the present one. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00. DIN EN 16603-50-01:2014-12 EN 16603-50-01:2014 (E) 8 2 Normative references The following normative documents contain provision

48、s which, through reference in this text, constitute provisions of this ECSS Standard. For dated references, subsequent amendments to, or revisions of any of these publications, do not apply. However, parties to agreements based on this ECSS Standard are encouraged to investigate the possibility of a

49、pplying the most recent editions of the normative documents indicated below. For undated references the latest edition of the publication referred to applies. EN reference Reference in text Title EN 16601-00-01 ECSS-S-ST-00-01 ECSS system - Glossary of terms DIN EN 16603-50-01:2014-12 EN 16603-50-01:2014 (E) 9 3 Terms, definitions and abbreviated terms 3.1 Terms from other standards For the purpose of this Standard, the terms and definitions from ECSS-ST-00-01 apply. 3.2 Terms specific to the present stand