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  2. DO-178B - Wikipedia

    en.wikipedia.org/wiki/DO-178B

    DO-178B, Software Considerations in Airborne Systems and Equipment Certification is a guideline dealing with the safety of safety-critical software used in certain airborne systems. It was jointly developed by the safety-critical working group RTCA SC-167 of the Radio Technical Commission for Aeronautics (RTCA) and WG-12 of the European ...

  3. Modified condition/decision coverage - Wikipedia

    en.wikipedia.org/wiki/Modified_condition/...

    MC/DC is used in avionics software development guidance DO-178B and DO-178C to ensure adequate testing of the most critical (Level A) software, which is defined as that software which could provide (or prevent failure of) continued safe flight and landing of an aircraft.

  4. DO-178C - Wikipedia

    en.wikipedia.org/wiki/DO-178C

    DO-178C, Software Considerations in Airborne Systems and Equipment Certification is the primary document by which the certification authorities such as FAA, EASA and Transport Canada approve all commercial software-based aerospace systems.

  5. Code coverage - Wikipedia

    en.wikipedia.org/wiki/Code_coverage

    Test coverage is one consideration in the safety certification of avionics equipment. The guidelines by which avionics gear is certified by the Federal Aviation Administration (FAA) is documented in DO-178B [16] and DO-178C. [18] Test coverage is also a requirement in part 6 of the automotive safety standard ISO 26262 Road Vehicles - Functional ...

  6. Integrity (operating system) - Wikipedia

    en.wikipedia.org/wiki/Integrity_(operating_system)

    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.

  7. ARP4754 - Wikipedia

    en.wikipedia.org/wiki/ARP4754

    ARP4754 is intended to be used in conjunction with the safety assessment process defined in SAE ARP4761 (updated to Revision A in December 2023) and is supported by other aviation standards such as RTCA DO-178C/DO-178B and DO-254. This guideline addresses Functional Safety and design assurance processes.

  8. AC 20-115 - Wikipedia

    en.wikipedia.org/wiki/AC_20-115

    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).

  9. Certification Authorities Software Team - Wikipedia

    en.wikipedia.org/wiki/Certification_Authorities...

    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.

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