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spacewire 规范
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更新于2023-03-03
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SpaceWire is a standard for high-speed links and networks for use onboard spacecraft, easing the interconnection of: sensors mass-memories processing units, and downlink telemetry sub-systems. SpaceWire is being widely used on many space missions by: ESA NASA JAXA SpaceWire equipment is connected together using SpaceWire links which are: serial, high-speed (2 Mbits/sec to 200 Mbits/sec), bi-directional, full-duplex.
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FOR SPACE STANDARDIZATION
EUROPEAN COOPERATION
E
CSS
Space engineering
SpaceWire - Links, nodes, routers
and networks
ECSS Secretariat
ESA-ESTEC
Requirements & Standards Division
Noordwijk, The Netherlands
ECSS-E-50-12A
24 January 2003
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E
CSS
24 January 2003
ECSS--E--50--12A
2
Published by: ESA Publications Division
ESTEC, P.O. Box 299,
2200 AG Noordwijk,
The Netherlands
ISSN: 1028-396X
Price: ! 30
Printed in The Netherlands
Copyright 2003 E by the European Space Agency for the members of ECSS
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E
CSS
24 January 2003
ECSS--E--50--12A
3
Foreword
This Standard is one of the series of ECSS Standards intended to be applied
together for the management, engineering and product assurance in space
projects and applications. ECSS is a cooperative effort of the European Space
Agency, national space agencies and European industry associations for the
purpose of developing and maintaining common standards.
Requirements in this Standard are defined in terms of what shall be accomplished,
rather than in terms of how to organize and perform the necessary work. This
allows existing organizational structures and methods to be applied where they
are effective, and for the structures and methods to evolve as necessary without
rewriting the standards.
The formulation of this Standard takes into account the existing ISO 9000 family
of documents.
This Standard has been prepared by the ECSS E--50--12 Working Group, reviewed
by the ECSS Technical Panel and approved by the ECSS Steering Board.
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CSS
24 January 2003
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4
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5
Introduction
General
SpaceWire technology has grown organically from the needs of on-board proces-
sing applications. This Standard provides a formal basis for the exploitation of
SpaceWire in a wide range of future on-board processing systems.
One of the principal aims of SpaceWire is the support of equipment compatibility
and reuse at both the component and subsystem levels. In principle a data-handl-
ing system developed for an optical instrument, for example, can be used for a
radar instrument by unplugging the optical sensor and plugging in the radar one.
Processing units, mass-memory units and down-link telemetry systems devel-
oped for one mission can be readily used on another mission, reducing the cost of
development, improving reliability and most importantly increasing the amount
of scientific work that can be achieved within a limited budget.
Integration and test of complex on-board systems is also supported by SpaceWire
with ground support equipment plugging directly into the on-board data-handl-
ing system. Monitoring and testing can be carried out with a seamless interface
into the on-board system.
SpaceWire is the result of the efforts of many individuals within the European
Space Agency, European Space Industry and Academia.
Purpose
This Standard addresses the handling of payload data and control information on
board a spacecraft. It is a standard for a high speed data link, which is intended
to meet the needs of future, high capability, remote sensing instruments and
other space missions. SpaceWire provides a unified high speed data-handling
infrastructure for connecting together sensors, processing elements, mass-mem-
ory units, downlink telemetry subsystems and EGSE equipment.
The purpose of this Standard is:
D to facilitate the construction of high-performance on-board data-handling
systems;
D to help reduce system integration costs;
D to promote compatibility between data-handling equipment and subsystems;
D to encourage reuse of data-handling equipment across several different
missions.
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