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Airborne Electronic Hardware Design Assurance
A Practitioner's Guide to RTCA/DO-254
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Gewicht:
481 g
Format:
238x159x22 mm
Beschreibung:
Randall Fulton has more than 36 years of electrical engineering experience in software and electronic hardware development and verification. He holds a BS from the Pennsylvania State University and earned his FAA DER credentials in software and programmable logic devices while working at Boeing Commercial Aircraft. As a DER, he has had approval authority for programmable logic devices since 1997 and has worked numerous Part 23 and Part 25 certification programs with field programmable gate arrays, ASIC, and software. Randall, along with Roy Vandermolen, taught the DO-254 practitioners course for RTCA in Washington, DC from 2006 to 2009. Randall has also taught the Airborne Electronic Hardware Job Functions class for the FAA Academy in Oklahoma City. He currently works as an FAA consultant DER through his company SoftwAir Assurance, Inc.
Introduction to RTCA/DO-254. Regulatory Background. Planning. Requirements. Validation. Philosophy 101-Design Assurance through Design Practice. Verification. Process Assurance. Configuration Management. Additional Considerations. Summary.
Written by an FAA consultant DER and an electronics hardware design engineer, this practical guide to the use of RTCA/DO-254 in the development of airborne electronic hardware for safety critical airborne applications describes how to optimize engineering processes and practices to harmonize with DO-254. It also discusses common pitfalls encountered by practitioners of DO-254, explains how to write requirements that will minimize the cost and effort of electronic design and verification, and promotes embracing DO-254 as the best path to high-quality airborne electronic hardware.