AECMA PREN 3910-001-1996 Aerospace Series High Speed Data Transmission Under STANAG 3838 or Fibre Optic Equivalent Control Edition P 1《航空航天系列.STANAG3838或光纤等价控制下高速数据传输.P1版》.pdf

《AECMA PREN 3910-001-1996 Aerospace Series High Speed Data Transmission Under STANAG 3838 or Fibre Optic Equivalent Control Edition P 1《航空航天系列.STANAG3838或光纤等价控制下高速数据传输.P1版》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 3910-001-1996 Aerospace Series High Speed Data Transmission Under STANAG 3838 or Fibre Optic Equivalent Control Edition P 1《航空航天系列.STANAG3838或光纤等价控制下高速数据传输.P1版》.pdf（92页珍藏版）》请在麦多课文档分享上搜索。

1、STD*AECMA PREN 37LO-OOL-ENGL L77b LOL23LL OOLL579 L7b Edition approved for publication AECMA STANDARD NORME AECMA AECMA NORM C2 Chairman Comments should be sent within six months after the date of publication to prEN 39 1 0-00 1 Edition P 1 January 1996 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROS

2、PACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (32) 2 775 81 1 O - Fax. (32) 2 775 81 11 ICs : Descriptors : ENGLISH VERSION Aerospace series High speed data transmission under STANAG 3838 or fibre optic equivalent control Srie arospatiale Transmission haute vitesse contrle par STAN

3、AG 3838 ou son quivalent par fibre optique Luft- und Raumfahrt Schnelle Datenbertragung unter STANAG 3838-Kontrolle oder dessen faseroptischem quivalent This “Aerospace Series Piestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is pu

4、blished on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee follo wing comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that inte

5、rchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre INPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CE

6、N (European Committee for Standardization) for formal vote. 1996-01 -31 AECMA Gulledelle 94 B-1200 BRUXELLES I M. Pezzetta Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without l

7、icense from IHS-,-,- STD-AECMA PREN 37LO-OOL-ENGL 177b LO123L1 0011580 778 = Page 2 prEN 3910-001 : 1996 Contents list O 1 2 3 4 Annex A (informative) Annex B (informative) Annex C (normative) Annex D (informative) Annex E (informative) Annex F (informative) Annex G (informative) Introduction . 3 Sc

8、ope . 3 References . 4 Definitions . 5 General requirements 9 Specific Implementations . 62 HS Fibre Optic Media Slash Sheets . 65 Frame Check Sequence Implementation . 76 Block Diagram for Error Rate / Waveform Test 79 HS Electrical Media Slash Sheets 80 85 Keyword Index . 87 Block Diagrams for Ele

9、ctrical HS Bus Error Rate Testing . Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 3910-001 : 1996 O Introduction This standard contains r

10、equirements for an aircraft internal time division multiplex data bus for use in systems integration of aircraft subsystems. The data bus consists of a STANAG 3838 (MIL-STD-1553B) controlled fibre optic or electrical interconnection channel for high speed data transmission. The control system is ful

11、ly compatible with STANAG 3838 or its fibre optic equivalent. (In this document any reference to STANAG 3838 should be taken to mean either STANAG 3838 or its fibre optic equivalent). Even with the use of this standard, subtle differences will exist between data buses used on different aircraft due

12、to particular aircraft mission requirements and the designer options allowed in this standard. The system designer has to recognize this fact and design the bus controller hardware and software to accommodate such differences. These designer selected options has to exist, so as to allow the necessar

13、y flexibility in the design of specific multiplex systems in order to provide the control mechanism, architecture redundancy, degradation concept and traffic patterns peculiar to the specific aircraft mission requirements. The following document is structured to follow the organization of STANAG 383

14、8 document as closely as possible. The high speed media characteristics are defined in parametric terms in the body of the standard, with the numerical values corresponding to optional implementation configurations being given in the “HS Fibre Optic Media Slash Sheets“ (ANNEX B) or “HS Electrical Me

15、dia Slash Sheet“ (ANNEX E). The main body of this document is identical to the final draft of STANAG 3910. 1 Scope This standard specifies the characteristics and requirements of a data bus system which consists of one or more High Speed (HS) Channel(s1 for HS data transmission and one Low Speed (LS

16、) Channel for control and LS data transmission. The standard defines the HS fibre optic or HS electrical data bus transmission line. The concept of operation and information flow on the HS multiplex data bus and the optical, electrical and functional formats to be employed are also defined. The elec

17、tro-optical or electrical HS transmission and reception units which interface to the associated protocol electronics are described in EN 371 5. When invoked in a specification or statement of work, the requirements defined in this standard shall apply to the multiplex data bus and associated equipme

18、nt which is developed either alone or as a portion of an aircraft system or subsystem development. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page

19、 4 prEN 3910-001 : 1996 Four types of system are defined : Type A Low Speed Channel - STANAG 3838 data bus High Speed Channel - Fibre Optic data bus Type B Low Speed Channel High Speed Channel - Fibre Optic equivalent of STANAG 3838 - Physically separate Fibre Optic data bus data bus Type C Low Spee

20、d Channel High Speed Channel - Fibre Optic equivalent of STANAG 3838 - Wavelength Division Multiplexed with the Low data bus Speed Channel onto a common fibre optic medium Type D Low Speed Channel - STANAG 3838 data bus High Speed Channel - Physically separate wire data bus The implementation of a f

21、ibre optic medium for the HS Channel is given in Annexes A and B. The implementation of an electrical medium for the HS Channel is given in Annex E. The redundancy of individual LS and HS Channels is implementation specific. 2 Normative references This European Standard incorporates by dated or unda

22、ted reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when i

23、ncorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. MIL-STD-15538 Digital Time Division Command/Response Multiplex Data Bus 1) STANAG 3838 Digital Time Division Command/Response Multiplex Data Bus (MIL-STD- 15538) 2) STANAG 39

24、1 O High Speed Data Transmission under STANAG 3838 or Fibre Optic Equivalent Control 2) EN 3715 Aerospace series - Interface for transceivers compatible with data bus CCITT Recomm. G.651 Annex B : Meaning of the Terms Annex C : Fibre Test Methods 4) CCITT-CRC Cyclic Redundancy Check 4) EN 3910-001 3

25、) 1) Published by : Department of Defense (DoD), Pentagon ; Washington D.C. 20301 2) Published by : NATO Military Agency for Standardisation (MAS) ; B-111 O Brussels 3) In preparation at the date of publication of the present standard. 4) Published by : CCITT (International Telegraph and Telephone C

26、onsultative Committee) ; CH-121 1 Geneva 20 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD.AECMA PREN 3710-001-ENGL L97b LOL23LL OOLL583 bT7 Page

27、5 prEN 3910-001 : 1996 3 Definitions For the purposes of this standard the following definitions apply : 3.1 Access Coupler An access coupler is a device which distributes optical or electrical power among several ports. Star couplers and Tee couplers are examples of access couplers. 3.2 Asynchronou

28、s Operation Asynchronous operation is the use of an independent clock source in each terminal for message transmission. Decoding is achieved in receiving terminals using clock information derived from the message. 3.3 Bit Contraction of binary digit : may either be zero or one. In information theory

29、 a binary digit is equal to one binary decision or the designation of one of two possible values or states of anything used to store or convey information. 3.4 Bit Rate Number of bits transmitted per second. 3.5 Broadcast Operation of a data bus system such that information transmitted by the Bus Co

30、ntroller or a terminal is addressed to the other terminals connected to the data bus. 3.6 Bus controller (BC) The terminal assigned the task of initiating information transfers on the data bus. 3.7 Bus Monitor (BM) A terminal assigned the task of receiving bus traffic and extracting selected informa

31、tion to be used at a later time. 3.8 Central Repeater (CR) The Central Repeater is an active device which amplifies, reformats and resynchronises signals between the Collection Line and the Distribution Line. 3.9 Collection Line The Collection Line is a transmission line which is used to collect sig

32、nals from HS Terminals transmitters. The Collection Line is connected to the Central Repeater input. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Pa

33、ge 6 prEN 3910-001 : 1996 3.1 O Command/Response Operation of a data bus system such that remote terminals receive and transmit data only when commanded to do so by the Bus Controller. 3.11 Data Bus Whenever a data bus or bus is referred to in this document, it shall imply all the hardware in the si

34、gnal distribution channel, including the harness assembly of cables, access coupler(s), connectors, etc., required to provide a single data path between all terminals. 3.12 Data Channel A Data Channel (either HS or LS Channel) is defined as the logical connection between the HS interfaces or between

35、 LS interfaces of two terminals comprising all Physical Media Paths of the redundant configuration. 3.13 Directional Coupler A Directional Coupler is an access tee coupler having three ports named port 1, port 2 and port 3. It provides low insertion loss between port 1 and port 2, coupling between p

36、ort 1 and port 3 and isolation between port 2 and port 3. Directional Couplers are used to connect the Stubs to the Collection Line or to the Distribution Line. 3.14 Distribution Line The Distribution Line is a transmission line on which collected signals are broadcasted to HS Terminals receivers. T

37、he Distribution is connected to the Central Repeater output. 3.1 5 Dynamic Bus Control The operation of a data bus system in which bus control can be dynamically passed between cooperating terminals. 3.16 Half Duplex Operation of a data transfer system in either direction over a single line, but not

38、 in both directions on that line simultaneously. 3.17 HS Channel The HS Channel is the high speed data bus used to transfer data between terminals and is defined as the logical connection between the HS interfaces of terminals comprising all physical media paths of the redundant configuration. Copyr

39、ight Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 391O-001-ENGL L77b 1012311 0011585 Li7T = Page 7 prEN 3910-001 : 1996 3.18 HS Media interface

40、 Unit (HS MIU) The HS Media Interface Unit is the part of the terminal which interfaces with the transmission media and where the electrical/optical and the optical/electrical or electrical/electricaI conversion is performed. 3.19 HS Message HS Messages consist of HS Control Formats) transmitted via

41、 the LS Channel and an HS Message Frame transmitted on an HS Channel. For the case of an HS remote terminal to remote terminal transfer, the message includes an HS RECEIVE and an HS TRANSMIT Control Format and an HS Message Frame for data transmission. 3.20 LS Channel The LS Channel is the low speed

42、 data bus used to issue commands requesting the transfer of data on the high or low speed data bus and is defined as the logical connection between the LS interfaces of terminals comprising all physical media paths of the redundant configuration. 3.21 Mode Code A means by which the Bus Controller ca

43、n communicate with the multiplex bus related hardware in order to assist in the management of information flow. 3.22 Path (Physical Media Path) A Path (Physical Media Path) of a channel is defined as the physical connection between the HS or the LS Channel interfaces of any two terminals via any sin

44、gle transmission media of the redundant configuration. 3.23 Protocol Data Unit (PDU) The Protocol Data Unit is that part of the HS Message frame between the Start and End Delimiters. 3.24 Pulse Code Modulation (PCM) The form of modulation in which the modulation signal is sampled, quantized and code

45、d CO that each element of information consists of different types or numbers of pulses and spaces. 3.25 Redundant Data Bus The use of more than one data bus to provide more than one data path between the subsystems, .e., dual redundant data bus, triple redundant data bus, etc Copyright Association E

46、uropeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 39LO-001-ENGL L77b LO123Ll 00LL58b 30b M Page 8 prEN 3910-001 : 1996 3.26 Remote Terminal (RT) All terminals no

47、t operating as the Bus Controller or as a Bus Monitor. 3.27 STANAG 3838 Message A STANAG 3838 Message is a message transmitted on the LS Channel. A single STANAG 3838 message is the transmission of a Command Word, Status and Data Words if they are specified. For the case of a remote terminal to remo

48、te terminal (RT to RT) transfer, the message shall include the two Command Words, the two Status Words and Data Words. 3.28 STANAG 3838 Word In this document a STANAG 3838 word is a sequence of 16 bits plus sync and parity transmitted on the LS Channel. There are three types of STANAG 3838 words : C

49、ommand Word, Status Word and Data Word. 3.29 HS Stub An HS Stub is a transmission line which connects an HS Terminals transmitter or an HS Terminals receiver to a Collection Line or to a Distribution Line respectively. 3.30 Subsystem The device or functional unit receiving data transfer service from the data bus(es1. 3.31 Terminal The electrical and/or electro-optical module necessary to interface the data bus with the s