@inproceedings{Emam:2009,
author = {Emam, O and Fitzgeorge, T and Whittaker, A and Wishart, A and Fowell, SD and Prochazka, M and Bentley, RD and Cole, RE and Brown, P and Carr, CM and Cupido, E and Oddy, T},
title = {Payloads with resource-efficient integration for science missions (PRISM)},
year = {2009}
}

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TY  - CPAPER
AB  - PRISM is a collaborative industry and academia project to demonstrate the practicality of a highly integrated payload processing architecture, in order to exploit improvements in spacecraft computer performance to reduce multi-instrument payload mass and power requirements. Integrated architectures also provide opportunities for a greater degree of autonomy and advanced target selection (e.g. inter-instrument triggering). The PRISM architecture has potential advantages for missions such as EJSM (Europa Jupiter System Mission) or Solar Orbiter. The key technology objectives of PRISM are application partitioning on a qualifiable operating system, supported by the software required for fault-tolerant centralised processing, and the development of an application development environment for writing and testing instrument control applications. A working demonstrator has been implemented on a LEON3 platform, with representative payload applications from an in-situ magnetometer and a remote sensing extreme ultra-violet imager, both proposed for Solar Orbiter. PRISM is supported by the UK Science and Technology Facilities Council (STFC).
AU  - Emam,O
AU  - Fitzgeorge,T
AU  - Whittaker,A
AU  - Wishart,A
AU  - Fowell,SD
AU  - Prochazka,M
AU  - Bentley,RD
AU  - Cole,RE
AU  - Brown,P
AU  - Carr,CM
AU  - Cupido,E
AU  - Oddy,T
PY  - 2009///
SN  - 0379-6566
TI  - Payloads with resource-efficient integration for science missions (PRISM)
ER  - 

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