ARINC 753-3-2001 HF Data Link System《高频数据链接系统》.pdf

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1、 HF DATA LINK SYSTEMARINC CHARACTERISTIC 753-3PUBLISHED: FEBRUARY 16, 2001AN DOCUMENTPrepared byAIRLINES ELECTRONIC ENGINEERING COMMITTEEPublished byAERONAUTICAL RADIO, INC.2551 RIVA ROAD, ANNAPOLIS, MARYLAND 21401Copyright 2001 byAERONAUTICAL RADIO, INC.2551 Riva RoadAnnapolis, Maryland 21401-7465

2、USAARINC CHARACTERISTIC 753-3HF DATA LINK SYSTEMPublished: February 16, 2001Prepared by the Airlines Electronic Engineering CommitteeCharacteristic 753 Adopted by the Airlines Electronic Engineering Committee: October 20, 1994Characteristic 753 Adopted by the Industry: December 9, 1994Summary of Doc

3、ument SupplementsSupplement Adoption Date PublishedCharacteristic 753-1 October 22, 1996 January 20, 1997Characteristic 753-2 November 26, 1997 February 20, 1998Characteristic 753-3 August 11, 2000 February 16, 2001A description of the changes introduced by each supplement is included on Goldenrod p

4、aper at the end of this document.iiFOREWORDActivities of AERONAUTICAL RADIO, INC. (ARINC)and thePurpose of ARINC CharacteristicsAeronautical Radio, Inc. is a corporation in which the United States scheduled airlines are the principalstockholders. Other stockholders include a variety of other air tra

5、nsport companies, aircraft manufacturers andnon-U.S. airlines.Activities of ARINC include the operation of an extensive system of domestic and overseas aeronauticalland radio stations, the fulfillment of systems requirements to accomplish ground and airborne compatibility, theallocation and assignme

6、nt of frequencies to meet those needs, the coordination incident to standard airbornecommunications and electronics systems and the exchange of technical information. ARINC sponsors theAirlines Electronic Engineering Committee (AEEC), composed of airline technical personnel. The AEECformulates stand

7、ards for electronic equipment and systems for the airlines. The establishment of EquipmentCharacteristics is a principal function of this Committee.An ARINC Equipment Characteristic is finalized after investigation and coordination with the airlineswho have a requirement or anticipate a requirement,

8、 with other aircraft operators, with the Military serviceshaving similar requirements, and with the equipment manufacturers. It is released as an ARINC EquipmentCharacteristic only when the interested airline companies are in general agreement. Such a release does notcommit any airline or ARINC to p

9、urchase equipment so described nor does it establish or indicate recognition ofthe existence of an operational requirement for such equipment, nor does it constitute endorsement of anymanufacturers product designed or built to meet the Characteristic. An ARINC Characteristic has a twofoldpurpose, wh

10、ich is:(1) To indicate to the prospective manufacturers of airline electronic equipment the consideredopinion of the airline technical people, coordinated on an industry basis, concerning requisitesof new equipment, and(2) To channel new equipment designs in a direction which can result in the maxim

11、um possiblestandardization of those physical and electrical characteristics which influence interchangeabilityof equipment without seriously hampering engineering initiative.ARINC CHARACTERISTIC 753TABLE OF CONTENTSITEM SUBJECT PAGEiii1.0 INTRODUCTION 11.1 Purpose of this Document 11.2 Relationship

12、to Other Documents 11.3 System Overview 11.3.1 Airborne HFDL System Configuration 11.3.2 Ground System Configuration 11.4 Terms 21.5 Interchangeability 21.6 Regulatory Approvals 22.0 INTERCHANGEABILITY STANDARDS 32.1 Introduction 32.2 Form Factor, Connector, and Index Pin Coding 32.3 Standard Interw

13、iring 32.4 Power Circuitry 32.4.1 Primary Power Input 32.4.2 Power Control Circuitry 42.4.3 Common Ground 42.4.4 Internal Circuit Protection 42.4.5 Abnormal Power 42.5 System Functions and Signal Characteristics 42.6 Environmental Conditions 42.7 Cooling 42.8 Grounding and Bonding 52.9 Standardized

14、Signaling 52.9.1 ARINC 429 DITS Data Bus 52.9.2 Standard “Open” 52.9.3 Standard “Ground” 52.9.4 Standard “Applied Voltage” Output 52.9.5 Standard Discrete Input 52.9.6 Standard Discrete Output 62.9.7 Standard Program Pin Input 63.0 SYSTEM DESIGN 73.1 Introduction 73.2 System Design 73.2.1 AOC and AT

15、S 73.2.2 Other Services 73.3 HFDL Avionics Components 73.3.1 HF Data Radio 73.3.2 HF Data Unit 83.3.3 HF Data Link Control Functions 83.4 Optional Additional Components 83.4.1 Central Maintenance System 83.4.2 Analog Data Operation 83.5 Interlocks on Dual HFDR Systems 83.6 HFDR and HFDU Modes of Ope

16、ration 93.6.1 HFDR Mode Select 93.6.2 HFDU/HF Transceiver Combination Mode Select 93.6.2.1 ARINC 719 HF Transceiver Controlled by Discretes 93.6.2.2 ARINC 719 HF Transceiver Controlled byARINC 429 Words 93.6.2.3 ARINC 559A HF Transceiver 104.0 HF DATA RADIO DESIGN 114.1 Introduction 114.2 Transceive

17、r 114.2.1 Tuning 114.2.1.1 Frequency Switching Time 114.2.2 Transmitter - Receiver Interaction 114.2.2.1 Transmit to Receive Turnaround Time 11ARINC CHARACTERISTIC 753TABLE OF CONTENTSITEM SUBJECT PAGEiv4.2.2.2 Receive to Transmit Turnaround Time 114.3 Transmitter 124.3.1 Power Output 124.3.1.1 SSB

18、Suppressed Carrier 124.3.1.2 SSB Full Carrier (AME) 124.3.1.3 Tune Power 124.3.1.4 VSWR Tolerance 124.3.1.5 Transmit Duty Cycle 124.3.2 Frequency Stability 124.3.3 Phase Stability 124.3.4 Audio Input 124.3.4.1 Input Level 134.3.4.2 Audio Processing and Modulation Limiting 134.3.4.3 Frequency Respons

19、e 134.3.4.4 Transmit Audio Distortion 134.3.5 Transmitter Keying 134.3.6 Occupied Spectrum 134.3.6.1 Intermodulation Distortion 144.3.6.2 Harmonics 144.3.6.3 Non-Harmonics 144.3.7 Tone Tuning Signal 144.4 Receiver 144.4.1 Sensitivity 144.4.2 Selectivity 144.4.2.1 SSB Suppressed Carrier 144.4.2.2 Amp

20、litude Modulated Equivalent (AME) 144.4.2.3 Group Delay 144.4.3 Frequency Stability 154.4.4 Spurious Responses 154.4.5 Audio Output 154.4.5.1 Source Impedance 154.4.5.2 Gain 154.4.5.3 Frequency Response 154.4.5.4 Distortion 154.4.5.5 Hum Level 154.4.5.6 Phase Shift 154.4.5.7 Phase Stability 164.4.6

21、Automatic Gain Control 164.4.6.1 Voice Mode 164.4.6.2 Analog Data and Data Link Mode 164.4.6.3 Settling Time 164.4.7 RF Sensitivity Control and/or Squelch Control 164.4.8 SSB Mode Linearity 174.5 SELCAL Output 174.5.1 Frequency Response 174.5.2 Distortion 174.5.3 Phase Shift 174.5.4 Differential Pha

22、se Delay 174.6 HFDR - System Interface 174.6.1 Voice/Analog Data/Data Link Mode Selection 174.6.1.1 Data Link 174.6.1.2 Voice or Analog Data 184.6.2 HFDR Voice Transceiver Tuning 184.6.2.1 ARINC 719 Style HF Transceiver Tuning 184.6.2.2 ARINC 559A Style HF Transceiver Tuning 184.6.3 HF Transceiver K

23、eying 194.6.3.1 Voice Mode 194.6.3.2 Analog Data Mode 194.6.3.3 Data Link Mode 194.6.4 HF Antenna Coupler Tuning Initiation 194.6.5 ACARS MU/CMU Interface Functions 194.6.6 Voice/Data Mode Switching Functions 19ARINC CHARACTERISTIC 753TABLE OF CONTENTSITEM SUBJECT PAGEv4.6.7 Other Interfaces 194.6.7

24、.1 Aircraft Position Data 194.6.7.2 Universal Coordinated Time (UTC) Data 194.6.7.3 ICAO 24-Bit Address Data 194.6.7.4 Maintenance Data 204.6.7.4.1 Maintenance System Identification 204.6.7.5 Data Loader 204.6.7.6 Cross-Talk Bus Data 204.6.8 Status Indication Discretes 214.6.8.1 HFDL DATA LINK LOST

25、Bit 214.6.8.2 HFDR FAULT Indication Discrete and Bit 214.6.8.3 HFDR Transmit Inhibit Status Indication Discrete and Bit 214.6.9 Built-In Tests 214.6.10 Air/Ground Discrete Input 214.6.11 Transmit Inhibit Discrete Input 214.6.12 Key Event Output 214.6.13 SDI Input Pin Definition 214.6.14 HFDL Transmi

26、t Inhibit Override Discrete Definition 224.6.15 Chopper Control 224.6.16 Strap Even Parity 224.6.17 ICAO Strap Even Parity 224.6.18 CMU #1/#2 Speed Select 224.6.19 HFDR Installed Discrete Output 224.6.20 Ruthless Preemption 235.0 HF DATA UNIT DESIGN 245.1 Introduction 245.2 HF Voice/Data Mode Enable

27、 Switching 245.3 Air/Ground Data Transmission Functions 245.3.1 HF Transceiver Audio Interface 245.3.2 Transmit Audio Waveform 245.3.3 HF Transceiver Keying 245.4 Air/Ground Data Receive Functions 245.4.1 HF Transceiver Audio Interface 245.4.2 Receive Audio Waveform 245.5 HF Transceiver Tuning 245.5

28、.1 ARINC 719 HF Transceiver Tuning 255.5.2 ARINC 559A HF Transceiver Tuning 255.6 HF Antenna Coupler Tuning Initiation 255.7 Air/Ground Data Transfer Protocol 255.8 ACARS MU/CMU Interface Functions 255.9 Other Interfaces 255.9.1 Aircraft Position Data 255.9.2 Universal Coordinated Time (UTC) Data 25

29、5.9.3 ICAO 24-bit Aircraft Address Data 255.9.4 Maintenance Data 255.9.4.1 Maintenance System Identification 255.9.5 Data Loader 255.9.6 Air/Ground Discrete Input 255.9.7 MU/CMU Interface Speed Select 265.9.8 Transmit Inhibit Discrete Input 265.9.9 SDI Inputs 265.9.10 Strap Even Parity 265.10 Status

30、 Indications 265.10.1 HF DATA LINK LOST Indication Discrete 265.10.2 HFDU FAULT Indication Discrete 265.11 Built-In Tests 266.0 DATA LINK CONTROL FUNCTIONS 276.1 Introduction 276.2 HFDCF Functions 276.2.1 HF Voice/Data Select 276.2.2 Programmable Functions 27ARINC CHARACTERISTIC 753TABLE OF CONTENTS

31、ITEM SUBJECT PAGEvi6.2.3 HF Data Link ON/OFF Switch 276.2.4 HF DATA LINK LOST Indication 276.2.5 HFDL FAULT Indication 276.2.6 HF Data Link Status Display 286.2.7 HFDU Mode Select 286.2.8 HF Frequency Port Select 286.2.9 RF Sensitivity or Squelch Control 286.2.10 HFDR Installed Function 286.2.11 HFD

32、L Transmit Inhibit Status Indication 287.0 ANTENNA SYSTEMS 297.1 Introduction 297.2 Antenna 297.3 HF Antenna Coupler 297.3.1 Matching 297.3.2 Frequency Coverage 297.3.3 Power Handling Capability 297.3.4 Tune Mode 297.3.5 Interwiring 297.4 Multiwire Serial Interface (MSI) 297.4.1 Physical Layer 307.4

33、.1.1 Physical Medium 307.4.1.1.1 Serial vs Parallel Interface Selection 307.4.1.1.1.1 Detection Scheme 307.4.1.1.1.2 Parallel Interface (ARINC 719) Definition 307.4.1.1.1.3 Multiwire Serial Interface (ARINC 753or MSI) Definition 317.4.2 Link Layer Protocol 327.4.2.1 Link Protocol Sequencing 327.4.2.

34、2 Link Protocol Message Description 327.4.2.3 Link Protocol Timings 337.4.3 Control Protocol 337.4.3.1 Sequencing 337.4.3.2 Aborting Commands 337.4.3.3 RF Operations 347.4.3.4 Control Protocol Command and Request Messages 347.4.3.5 Example Communication Sequence 517.5 Tuning Time 558.0 PROVISIONS FO

35、R AUTOMATIC TEST EQUIPMENT 568.1 General 568.2 ATE Testing 569.0 PROVISIONS FOR BUILT-IN TEST EQUIPMENT (BITE) 579.1 Introduction 579.2 BITE Interfaces 579.2.1 OMS Interfaces 579.2.2 Character-Oriented CFDS Interfaces 589.2.3 Bit-Oriented CFDS Interfaces 589.2.4 MU/CMU BITE Interfaces 589.2.5 HFDR/H

36、FDU Equipment Identification Word 589.3 Bite Presentation 589.4 Fault Monitor 589.5 Self-Test Initiation 589.6 Monitor Memory Output 599.7 HF Data Link to CMC Status Word 5910.0 ACARS MU/CMU - HFDL INTERFACE 6010.1 Overview 6010.2 Physical Interface 6010.3 Link Layer - Broadcast 6010.3.1 HFDR to ACA

37、RS MU/CMU Status Word 6010.3.2 ACARS MU/CMU to HFDL Status Word 62ARINC CHARACTERISTIC 753TABLE OF CONTENTSITEM SUBJECT PAGEvii10.3.3 HFDL to MU/CMU Join/Leave Event Message 6210.3.4 HFDL to ACARS MU/CMU Subsystem Identifier Word 6310.4 Link Layer - Bit Oriented File Transfer Protocol 6310.4.1 Fire

38、Format 6310.4.2 Enveloped Messages 6310.4.3 ISO 8208 Packets 6410.4.4 Command/Control File 6410.5.1 Command/Control Overview 6410.5.2 Command/Control Format 6410.5.2.1 Requirements Table Update Format 6410.5.2.2 HFDL to MU/CMU Maintenance Data 6510.6 HFDL Messages 65ATTACHMENTS1-1 Airborne Subsystem

39、 Block Diagram 662-1A HFDR Avionics Configuration A 672-1B HFDR System Block Diagram 682-1C Dual HFDR Avionics Configuration A(Using ARINC 429 Voice/Data Control not considered as part of theHFDRCFDS: Central Fault Display SystemCoupler: Antenna tuning device to match the antennaimpedance to the 50

40、ohm coaxial transmissionlinec-1ARINC CHARACTERISTIC 753 - Page 21.0 INTRODUCTION1.4 Terms (contd)HFDL: High Frequency Data Link; HF Data/VoiceCommunication Subnetwork Air/GroundHFDR: High Frequency Data Radio; used for theairborne HF TransceiverHFDU: High Frequency Data Unit; The HFDU containsthe Mo

41、dem for the system when the Modem isa separate LRUOMS: On-Board Maintenance System1.5 InterchangeabilitySystem interchangeability, as defined in Section 2.0 ofARINC Report 607, “Guidance for Designers of AirborneElectronic Equipment”, is desired for the HFDR andHFDU. The standards necessary to ensur

42、e this level ofinterchangeability are set forth in Chapter 2 of thisdocument.1.6 Regulatory ApprovalsThe equipment must meet all applicable regulatoryrequirements. Manufacturers are urged to obtain allnecessary information for such regulatory approval. Thisinformation is not contained in this charac

43、teristic, nor is itavailable from ARINC.ARINC CHARACTERISTIC 753 - Page 32.0 INTERCHANGEABILITY STANDARDS2.1 IntroductionThis chapter sets forth the specific form factor, mountingprovisions, interwiring, input and output interfaces andpower supply characteristics desired for the HF DataRadio and HF

44、Data Unit. These standards permit theparallel, but independent design of compatible equipmentand airframe installations.Unit interchangeability is required for the HF Data Radio,HF Data Unit, and Antenna Coupler, regardless ofmanufacturing source. COMMENTARYIn order to achieve the full benefit of th

45、e economicsoffered by these changes, the industry desires thatany provisions for backwards compatibility withearlier generations of HF Communications equipmentdescribed by ARINC Characteristic 719 be providedas basic provisions. The ARINC 753 transceiver (HFDR) is pin- and function-compatible with t

46、he ARINC 719 transceiver. When an HFData Radio is installed in an ARINC 719 slot, (replacing anARINC 719 transceiver) it should operate with ARINC 719radio functionality. An HF Data Unit attached to thisarray would be required to obtain HF Data Linkfunctionality.2.2 Form Factor, Connector, and Index

47、 Pin CodingThe HFDR and HFDU should comply with the dimensionalstandards in ARINC Specification 600, “Air TransportAvionics Equipment Interfaces (NIC Phase 1)”, for the 6MCU and 4 MCU form factors respectively. The HFDRand HFDU should also comply with ARINC Specification600 standards with respect to

48、 weight, racking attachments,front and rear projections and cooling.COMMENTARYThe only form factor defined in this Characteristic isthe Modular Concept Unit (MCU) defined in ARINCSpecification 600. Packaging of the HFDR inaccordance with ARINC Specification 404A was notconsidered desirable. However,

49、 some retrofitinstallations into aircraft racking for ARINC 404Aequipment are expected.The HFDR and HFDU should each be provided with a lowinsertion force, Size 2 Shell ARINC Specification 600service connector. This connector, which shouldaccommodate service interconnections in its middle plug(MP) and top plug (TP) inserts and powerinterconnections in its bottom plug (BP) insert, should belocated on the center grid of the HFDR and HFDU rearpanel. Index pin code 10 should be used for the HFDR. In