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  2. DO-178C - Wikipedia

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

    The release of DO-178C and the companion documents DO-278A (Ground Systems), DO-248C (Additional information with rationale for each DO-178C objective), DO-330 (Tool Qualification), DO-331 (Modeling), DO-332 (Object Oriented), and DO-333 (Formal Methods) were created to address the issues noted. The SC-205 members worked with the SAE S-18 ...

  3. DO-248 - Wikipedia

    en.wikipedia.org/wiki/DO-248

    DO-248C, Supporting Information for DO-178C and DO-278A, published by RTCA, Incorporated, is a collection of Frequently Asked Questions and Discussion Papers addressing applications of DO-178C and DO-278A [1] in the safety assurance of software for aircraft and software for CNS/ATM systems, respectively.

  4. 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.

  5. Automotive Safety Integrity Level - Wikipedia

    en.wikipedia.org/wiki/Automotive_Safety...

    DO-178C and DO-254 define the design assurance objectives that must be accomplished for given DAL. Unlike SIL, it is the case that both ASIL and DAL are statements measuring degree of hazard. DAL E is the ARP4754 equivalent of QM; in both classifications hazards are negligible and safety management is not required.

  6. Category:RTCA standards - Wikipedia

    en.wikipedia.org/wiki/Category:RTCA_standards

    The designation DO stands for "DOcument". Pages in category "RTCA standards" ... DO-160; DO-178B; DO-178C; DO-212; DO-219; DO-232; DO-242A; DO-248C; DO-248; DO-254 ...

  7. DO-254 - Wikipedia

    en.wikipedia.org/wiki/DO-254

    The DO-254/ED-80 standard is the counterpart to the well-established software standard RTCA DO-178C/EUROCAE ED-12C. With DO-254/ED-80, the certification authorities have indicated that avionics equipment contains both hardware and software, and each is critical to safe operation of aircraft.

  8. AC 20-115 - Wikipedia

    en.wikipedia.org/wiki/AC_20-115

    The Advisory Circular AC 20-115( ), Airborne Software Development Assurance Using EUROCAE ED-12( ) and RTCA DO-178( ) (previously Airborne Software Assurance), recognizes [1] the RTCA published standard DO-178 as defining a suitable means for demonstrating compliance for the use of software within aircraft systems.

  9. Radio Technical Commission for Aeronautics - Wikipedia

    en.wikipedia.org/wiki/Radio_Technical_Commission...

    Many of RTCA documents begin with the letters DO which stands for DOcument. RTCA develops Minimum Operating Performance Standards for aviation-based technology (typically avionics) but has developed standards for such far-ranging topics as Airport Security, Counter UAS Detection standards, and Aircraft Cockpit and Cabin Cleaning standards.