12–16 Jun 2016
Gothenburg, Sweden
Europe/Amsterdam timezone

Session

Session 4: DSP Day Reception and Poster Session

15 Jun 2016, 18:15
Gothenburg, Sweden

Gothenburg, Sweden

Presentation materials

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  1. Mr Flavien DOZOLME (THALES Communications & Security)
    15/06/2016, 18:15
    DSP Day: Test, Verification and Qualification of DSP chips
    No preference
    **1.Introduction** Microcontrollers and DSPs are key components of embedded systems for most applications (space, avionics, industry…). The reliability of these components has to be asserted to ensure the correct working of the system for the duration of its mission while preserving its performances. Designers are currently greatly tempted to use commercial components for their...
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  2. Prof. Ran Ginosar (Ramon Chips)
    15/06/2016, 18:15
    DSP Day: DSP software, tools and libraries
    RC64 is designed as a high performance rad-hard manycore DSP processor for space applications. Software Defined Radio (SDR) and modems constitute very demanding applications. This paper investigates the implementation of DVB-S2/DVB-S2x modems on RC64. An LDPC hardware accelerator is included in RC64 to support efficient modems, and as a result RC64 achieves in excess of 2 Gbps transmit rate...
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  3. Dr Roland Ottensamer (University of Vienna)
    15/06/2016, 18:15
    DSP Day: DSP software, tools and libraries
    The Department of Astrophysics at the University of Vienna is a provider of payload instrument flight software (IFSW) with a focus on the compression of the instrument science data. One of the projects under development is the instrument flight software for the first ESA-S class mission CHEOPS (CHaracterising ExOPlanet Satellite). CHEOPS is being built for launch in late 2017 to provide...
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  4. Mr Charles Sellier (3D PLUS), Mr Pierre-Xiao WANG (3D PLUS)
    15/06/2016, 18:15
    DSP Day: DSP IP cores and related IP including NoC
    No preference
    I. INTRODUCTION DDR2 SDRAM is a very attractive technology for space application thanks to its high density and high speed. However, o move it into space application, it is quite complicated to handle it because of the following reasons: - Complex Behavior under radiation – No Rad Hard device available - Volatile – Data loss risk if any functional issue - Difficult to handle...
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