English

EChO Payload electronics architecture and SW design

Instrumentation and Methods for Astrophysics 2015-06-18 v1

Abstract

EChO is a three-modules (VNIR, SWIR, MWIR), highly integrated spectrometer, covering the wavelength range from 0.55 μ\mum, to 11.0 μ\mum. The baseline design includes the goal wavelength extension to 0.4 μ\mum while an optional LWIR module extends the range to the goal wavelength of 16.0 μ\mum. An Instrument Control Unit (ICU) is foreseen as the main electronic subsystem interfacing the spacecraft and collecting data from all the payload spectrometers modules. ICU is in charge of two main tasks: the overall payload control (Instrument Control Function) and the housekeepings and scientific data digital processing (Data Processing Function), including the lossless compression prior to store the science data to the Solid State Mass Memory of the Spacecraft. These two main tasks are accomplished thanks to the Payload On Board Software (P-OBSW) running on the ICU CPUs.

Cite

@article{arxiv.1401.2977,
  title  = {EChO Payload electronics architecture and SW design},
  author = {M. Focardi and A. M. Di Giorgio and M. Farina and M. Pancrazzi and R. Ottensamer and T. L. Lim and S. Pezzuto and G. Micela and E. Pace},
  journal= {arXiv preprint arXiv:1401.2977},
  year   = {2015}
}

Comments

Experimental Astronomy - EChO Special Issue 2014

R2 v1 2026-06-22T02:44:23.993Z