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DO-254

RTCA/DO-254, Design Assurance Guidance for Airborne Electronic Hardware is a document providing guidance for the development of airborne electronic… 
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Papers overview

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2015
2015
Safety-critical systems and certification standards are the bare essential elements for the development process of avionics… 
2015
2015
  • 2015
  • Corpus ID: 51775574
DO-178b/c and DO-254 each contain a set of objectives that must be met. These objectives define the level of verification and… 
2013
2013
The paper covers the DO-254 for FPGAs, DO-254 requirements traceability, traceability activities FPGA development lifecycle and… 
2012
2012
High complexity of integrated,high performance,low power dissipation and miniaturization have been considered as the inevitable… 
Review
2010
Review
2010
It generates new design and certification challenges comparing the widely use of complex electronic hardware (CEH)in airborne… 
2010
2010
  • 2010
  • Corpus ID: 18106891
www.mathworks.com The purpose of RTCA/DO-254 (referred to herein as “DO-254”) is to provide guidance for the development of… 
2009
2009
www.xilinx.com 1 © Copyright 2011 Xilinx, Inc. XILINX, the Xilinx logo, Virtex, Spartan, ISE, and other designated brands… 
2009
2009
  • 2009
  • Corpus ID: 43155957
This White Paper points out the most significant issues which can be encountered during DO-254 compliant verification process for… 
2008
2008
In recent decades, safety has emerged as a major issue in many embedded applications in the aerospace, aircraft, automobile… 
Review
2008
Review
2008
Integrated modular avionics (IMA) systems are being installed on a number of new and modified aircraft. This paper provides a…