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The intention of DO-178B was not to be prescriptive. There are many possible and acceptable ways for a real project to define these aspects. This can be difficult the first time a company attempts to develop a civil avionics system under this standard, and has created a niche market for DO-178B training and consulting.
INTEGRITY-178B is the DO-178B–compliant version of INTEGRITY. It is used in several military jets such as the B-2, [2] F-16, F-22, and F-35, and the commercial aircraft Airbus A380. [3] Its kernel design guarantees bounded computing times by eliminating features such as dynamic memory allocation.
PRESAGIS [15] introduced the first COTS ARINC 661 development tool which allows creation of Widgets, Layers, DF Generation and embeddable real-time COTS CDS kernel with DO-178B/C certification artifacts. [16] [17] Because of the burden of Avionics software certification, the kernel must be embedded in a DO-178-compliant environment.
With application of DO-178B, it was discovered that many projects were not complying with DO-178B, but there was also wide variations in how various certification authorities conducted project assessments. In response, the CAST developed a standard software compliance assessment approach.
Download as PDF; Printable version; ... The mitigations for CMA discoveries is often DO-254 or DO-178B components. ... SAE Standard Committee S-18 began working on ...
The earliest revisions of the Advisory Circular were brief, serving little more than to call attention to active DO-178 revisions. The Advisory Circular revisions C and D are considerably longer, giving guidance in modifying and re-using software previously approved using DO-178, DO-178A, or DO-178B (preceding revisions of the DO-178 standard).
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