In this section
@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}
}
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 -