%0 Conference Proceedings
%T On the Use of System-on-Chip Technology in Next-Generation Instruments Avionics for Space Exploration
%+ ARM Ltd [Cambridge] (ARM)
%+ Jet Propulsion Laboratory (JPL)
%+ Massachusetts Institute of Technology (MIT)
%A Iturbe, Xabier
%A Keymeulen, Didier
%A Yiu, Patrick
%A Berisford, Daniel
%A Carlson, Robert
%A Hand, Kevin
%A Ozer, Emre
%< avec comité de lecture
%( IFIP Advances in Information and Communication Technology
%B 23th IFIP/IEEE International Conference on Very Large Scale Integration - System on a Chip (VLSI-SoC)
%C Daejeon, South Korea
%I Springer
%3 VLSI-SoC: Design for Reliability, Security, and Low Power
%V AICT-483
%P 1 - 22
%8 2015-10-05
%D 2015
%R 10.1109/AERO.2015.7119098
%K Fault-Tolerance
%K Avionics
%K System-on-Chip Integration
%K ARM Processor
%K Signal Processing
%Z Computer Science [cs]Conference papers
%X System-on-Chip (SoC) technology enables integrating all the functionality required to control and process science data delivered by space instruments in a single silicon chip (e.g., microprocessor + pro-grammable logic). This chapter discusses the implications of using this technology in deep-space exploration avionics, namely in the next generation of NASA science instruments that will be used to explore our Solar system. We present here our experience at the NASA Jet Propulsion Laboratory (JPL) using Xilinx Zynq SoC devices to implement the data processing of a Fourier transform spectrometer, namely the Compo-sitional InfraRed Imaging Spectrometer (CIRIS). Besides, we also discuss the different fault-tolerance techniques that have been implemented in the CIRIS controller SoC to deal with harsh radiation conditions prevailing in deep-space environments.
%G English
%Z TC 10
%Z WG 10.5
%2 https://hal.science/hal-01578642/document
%2 https://hal.science/hal-01578642/file/431455_1_En_1_Chapter.pdf
%L hal-01578642
%U https://hal.science/hal-01578642
%~ IFIP
%~ IFIP-AICT
%~ IFIP-TC
%~ IFIP-WG
%~ IFIP-VLSISOC
%~ IFIP-TC10
%~ IFIP-WG10-5
%~ IFIP-AICT-483