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Content Provider | IEEE Xplore Digital Library |
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Author | Senior, A. Coetzee, J.-P. Ilstad, J. |
Copyright Year | 2014 |
Description | Author affiliation: Thales Alenia Space (UK), Bristol, UK (Senior, A.; Coetzee, J.-P.) || ESTEC, Eur. Space Agency, Noordwijk, Netherlands (Ilstad, J.) |
Abstract | The SpaceWire standards are maintained and issued formally as ECSS documents (e.g. ECSS-E-ST-50-12C) and this means that equipment designed by different agencies is interoperable, which has significant benefits.SpaceWire is mainly used between instrument units, however to facilitate a high level of integration of onboard systems it is proposed that an ECSS SpaceWire Backplane standard should be created and adopted, the backplane offering power, signal and impedance-matched connectivity for high-speed serial links such as SpaceWire and SpaceFibre. The SpaceWire Backplane standard will assist in the aim of creating a common onboard infrastructure to be used across many different mission applications by encouraging design reusability at the sub-unit (PCB plug-in module) level. A key advantage of a SpaceWire Backplane is the scalability of the design. A draft SpaceWire Backplane ECSS standard has been created by TAS-UK as part of an ESA contract. It is based around the Smiths Connectors Nexus modular connector which can be populated with a variety of different contact inserts for power, signal and high-speed data and thus can be tailored to a particular application. The standard will specify the physical dimensions, connectors and electrical interfaces of the unit backplane and plug-in module. Units and plug-in modules will then be interoperable, so for example a module produced by one vendor will correctly fit into a unit from another vendor and interface correctly with the backplane electrical signals. It permits both non-redundant and redundant units to be built and does not dictate the backplane SpaceWire network architecture. Recommendations are made to assist in the creation of reliable fault-tolerant systems. It is intended that this ECSS document takes advantage of specifications already existing, namely other ECSS and also ANSI/VITA VPX standards. The principal VITA standards are referenced include VPX (VITA 46), OpenVPX (VITA 65) and a new draft standard SpaceVPX (VITA 78). It is anticipated that there will be a harmonisation activity in future between the SpaceVPX and this ECSS document before the formal ECSS standard release. This paper is a walk-through of the ECSS Backplane standard, it describes the thought processes and rationale behind it and the anticipated advantages of adopting it. |
Starting Page | 1 |
Ending Page | 4 |
File Size | 957953 |
Page Count | 4 |
File Format | |
ISBN | 9780955719653 |
DOI | 10.1109/SpaceWire.2014.6936267 |
Language | English |
Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
Publisher Date | 2014-09-22 |
Publisher Place | Greece |
Access Restriction | Subscribed |
Rights Holder | University of Dundee |
Subject Keyword | Networking SpFi Backplane Aerospace electronics SpaceFibre Standards Avionics Connectors Space vehicles SpaceWire Backplanes Spacecraft Electronics Computer architecture SpW SpaceVPX Resource management ECSS |
Content Type | Text |
Resource Type | Article |
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