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Rotorcraft digital advanced avionics system (RODAAS) functional description

Published 2019-06-24 From Legacy CDMS 3 authors
Read paper (PDF) ↗ View on NASA NTRS ↗

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

A functional design of a rotorcraft digital advanced avionics system (RODAAS) to transfer the technology developed for general aviation in the Demonstration Advanced Avionics System (DAAS) program to rotorcraft operation was undertaken. The objective was to develop an integrated avionics system design that enhances rotorcraft single pilot IFR operations without increasing the required pilot training/experience by exploiting advanced technology in computers, busing, displays and integrated systems design. A key element of the avionics system is the functionally distributed architecture that has the potential for high reliability with low weight, power and cost. A functional description of the RODAAS hardware and software functions is presented.

Authors

  • Peterson, E. M. Honeywell, Inc.
  • Bailey, J. Honeywell, Inc.
  • Mcmanus, T. J. Honeywell, Inc.

Citation: Peterson, E. M., Bailey, J., Mcmanus, T. J. (2019). Rotorcraft digital advanced avionics system (RODAAS) functional description. Legacy CDMS. NASA NTRS ID 19850016926. https://ntrs.nasa.gov/citations/19850016926 ↗