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EN 16603-50-13:2014

Current

Current

The latest, up-to-date edition.

Space engineering - Interface and communication protocol for MIL-STD-1553B data bus onboard spacecraft

Published date

10-09-2014

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Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Overview
5 Physical Layer requirements
6 Data Link Layer requirements
7 Services definition
8 Protocol specification
9 Test and verification
Annex A (informative) - Tailoring guidelines
Annex B (informative) - Unreferenced requirements
        in MIL-STD-1553B
Bibliography

Using standard communication protocols for spacecraft communication links can provide interface compatibility between communication devices and components. Thus, it can improve the design and development process as well as integration and test activities at all levels,and provide the potential of reusability across projects.The aim of this space engineering standard is to define the interface services and to specify their corresponding bus protocol elements for spacecraft using the MIL-STD-1553B data bus. It also aims at defining requirements for harmonisation of physical interface and usage of the MIL-STD-1553B data link layer features.Another goal of this standard is to facilitate the bus profiling task by proposing a message scheduling scheme to the mission system architects. Such framework helps to homogenise the allocation and control of communication resources across a single project or spacecraft mission.The scope of this standard is as follows:•It details the usage of the MIL-STD-1553B.•It covers the communication protocols, services and functions needed for exchange of information over MIL-STD-1553B data bus.•It is limited to necessary and sufficient requirements to ensure compatibility for communication through MIL-STD-1553B data bus for communication devices onboard a spacecraft and across projects.•It covers a wide spectrum of mission needs.•It does not modify requirements that are under the scope of MIL-STD-1553B.•It covers recommendation for verification and test of communication devices communicating through a MIL-STD-1553 data bus.This Standard provides a comprehensive set of requirements for all communication devices and components onboard a spacecraft, whichare connected to a single (redundant) data bus according to MIL-STD-1553B.Although the standard focuses on the specification of single-bus architecture, questions related to multiple-bus-architectures or the use of repeaters for separable busses (for launchers) are also addressed.This Standard aims at specifying requirements that are technically feasible, correct, consistent and compliant with the needs and overall technological approach and industrial policies of the participating Agencies and Industry. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.

Committee
CEN/CLC/JTC 5
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current

ISO/IEC 7498-1:1994 Information technology — Open Systems Interconnection — Basic Reference Model: The Basic Model
SAE AS 4112 : 1989 PRODUCTION TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS REMOTE TERMINALS
SAE AS 4117 : 1991 TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS COUPLERS, TERMINATORS, AND DATA BUS CABLES
MIL-HDBK-1553 Revision A:1988 Multiplex Application Handbook
SAE AS 4115 : 1989 TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS SYSTEM
SAE AS 4114 : 1989 PRODUCTION TEST PLAN FOR THE TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS CONTROLLERS
EN 16601-00-01:2015 Space systems - Glossary of terms
EN 16603-70-41:2017 Space engineering - Telemetry and telecommand packet utilization
MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA

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