DO-178 requires documented bidirectional connections (called traces) between the certification artifacts.

DO-178 was developed in the late 1970s and originally released in 1982. The original standard provided a prescriptive set of design assurance processes for software developed for airborne …

A third party tool can be qualified as a verification tool, but development tools must have been developed following the DO-178 process. Companies providing these kind of tools as COTS …

DO-178(), originally published in 1981, is the core document for defining both design assurance and product assurance for airborne software. The current version, DO-178C, was published in …

and RTCA DO-178( ). (2) AC 21-43, Production Under 14 CFR Part 21, Subparts F, G, K, and O. (3) AC 23.1309-1, System Safety Analysis and Assessment for Part 23 Airplanes. (4) AC …

2010年4月26日 · Outline DO-178B • Summary • Levels • Life-Cycle Model • Objectives • Role of Testing • Related documents DO-178C • Organization of revision effort

RTCA has teamed with The MITRE Aviation Institute to offer high quality and relevant training for the aviation industry in understanding the requirements and parameters for avionics software …

do-178 RTCA DO-178C / EUROCAE ED-12C: Software Considerations in Airborne Systems and Equipment Certification is the primary document by which certification authorities such as the …

DO-178 Development Assurance Levels A major provision of DO-178C is the definition of Design Assurance Levels (DALs), which indicate the consequences of potential software failure to the …

DO-178C is a formal process standard that covers the complete software lifecycle – the planning process, development process, and integral processes – to ensure correctness and …