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MIL-STD-1553 Revision B:1978

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
Available format(s)

PDF

Superseded date

05-10-2021

1 Scope
1.1 Scope
1.2 Application
2 Referenced documents
2.1 Issue of documents
3 Definitions
3.1 Bit
3.2 Bit rate
3.3 Pulse Code Modulation (PCM)
3.4 Time Division Multiplexing (TDM)
3.5 Half duplex
3.6 Word
3.7 Message
3.8 Subsystem
3.9 Data bus
3.10 Terminal
3.11 Bus controller
3.12 Bus monitor
3.13 Remote Terminal (RT)
3.14 Asynchronous operation
3.15 Dynamic bus control
3.16 Command/response
3.17 Redundant data bus
3.18 Broadcast
3.19 Mode code
4 General requirements
4.1 Test and operating requirements
4.2 Data bus operation
4.3 Characteristics
4.3.1 Data form
4.3.2 Bit priority
4.3.3 Transmission method
4.4 Terminal operation
4.4.1 Common operation
4.4.2 Bus controller operation
4.4.3 Remote terminal
4.4.4 Bus monitor operation
4.5 Hardware characteristics
4.5.1 Data bus characteristics
4.5.2 Terminal characteristics
4.6 Redundant data bus requirements
4.6.1 Electrical isolation
4.6.2 Single event failures
4.6.3 Dual standby redundant data bus
5 Detail requirements
Figures
1 Sample multiplex data bus architecture
2 Data encoding
3 Word formats
4 Command and status sync
5 Data sync
6 Information transfer formats
7 Broadcast information transfer formats
8 Intermessage gap and response time
9 Data bus interface using trans. coupling
10 Data bus interface using direct coupling
11 Coupling transformer
12 Terminal I/O characteristics for transformer coupled
    and direct coupled stubs
13 Output waveform
Tables
I Assigned mode codes
II Criteria for acceptance or rejection of a terminal
    for the noise rejection test
Appendix
10 General
10.1 Redundancy
10.2 Bus controller
10.3 Multiplex selection criteria
10.4 High reliability requirements
10.5 Stubbing
10.6 Use of broadcast option
20 General
20.1 Mode codes
20.2 Broadcast command
20.3 Mode code indicators
20.3.1 Bus controllers
20.3.2 Remote terminals
20.4 Data bus cable
20.4.1 Shielding
20.4.2 Characteristic impedance
20.5 Cable coupling
20.6 Direct coupled stubs
20.7 Redundant data bus requirements
20.8 Design considerations
20.8.1 Mode code indicator
20.8.2 Clock stability
20.8.3 Response time
Appendix Figures
10.1 Illustration of possible redundancy
10.2 Illustration of possible redundancy

Describes digital, command response, time division multiplexing techniques on aircraft. Covers data bus line and interface electronics, defines operation and information flow on multiplex data bus and functional and electrical formats used. Coverage includes definitions, data bus operation, transmission method, data code, remote terminal address, optional mode control, electrical isolation, and output noise. Also gives tables, diagrams and appendices.

Committee
FSC MCCR
DevelopmentNote
Updated by SAE AS 1773 in part.
DocumentType
Standard
Pages
425
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy

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MIL-R-87245 Base Document:1986 RADIO COMMUNICATION SYSTEM, AIRBORNE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA: ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503
MIL-I-87216 Base Document:1984 INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503
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NASA HDBK 4001 : 0 ELECTRICAL GROUNDING ARCHITECTURE FOR UNMANNED SPACECRAFT
RE.AERO 74430 : 1990 REPRESENTATION OF ELECTRICAL MASSES USED IN AIRCRAFT AND TEST INSTALLATIONS
SAE AS 15531 : 2017 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS
IEEE 1671.3-2007 IEEE Standard for Automatic Test Markup Language (ATML) for Exchanging Automatic Test Information via XML (eXtensible Markup Language): Exchanging UUT (Unit Under Test) Description Information
MIL-STD-1773 Base Document:1988 FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS
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MIL-STD-1760 Revision E:2007 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
MIL-F-24259 Revision A:1987 FLUID FLOWMETER, VOLUME VELOCITY TYPE
PD 6526:1990 Evaluation report on CIM architectures
MIL-I-8671 Revision D:1994 INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
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IEEE DRAFT 896.10 : D4.0 JUL 95 STANDARD FOR FUTUREBUS+ SPACEBORNE SYSTEMS PROFILE "S"
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NASA CCSDS 901.0-G : ISSUE 1 SPACE COMMUNICATIONS CROSS SUPPORT - ARCHITECTURE DESCRIPTION DOCUMENT
MIL-T-24664 Base Document:1986 TEST SET, RADAR, AN/UPM-()
SAE AIR 1873 : 2016 GUIDE TO LIMITED ENGINE MONITORING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES
SAE AS 4270 : 2017 VALIDATION METHODS FOR MIL-STD-1760 MISSION STORES
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SAE AS 4113 : 2017 VALIDATION TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS BUS CONTROLLERS
SAE AS 47642 : 2017 VALIDATION METHODS FOR MIL-STD-1760C AIRCRAFT STATION INTERFACES
I.S. EN 16603-50-13:2014 SPACE ENGINEERING - INTERFACE AND COMMUNICATION PROTOCOL FOR MIL-STD-1553B DATA BUS ONBOARD SPACECRAFT
SAE AS 4111 : 2017 VALIDATION TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS REMOTE TERMINALS
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BS EN 4660-003:2011 Aerospace series. Modular and open avionics architectures Communications/Network
BS EN 3716-002:2006 Aerospace series. Connectors, single-way, with triaxial interface, for transmission of digital data Conditions of use and list of product standards
BS EN 3567-001:2001 Aerospace series. In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B Technical specification
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EN 16603-50-13:2014 Space engineering - Interface and communication protocol for MIL-STD-1553B data bus onboard spacecraft
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DOD STD 1788 : LATEST AVIONICS INTERFACE DESIGN STANDARD (METRIC)
SAE AS 4116 : 2017 TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS BUS MONITORS
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MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM

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