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Line 11: Independence of a condition is shown by proving that only one condition changes at a time. MC/DC is used in avionics software development guidance [[DO-178B]] and [[DO-178C]] to ensure adequate [[Software testing\|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. It is also highly recommended for [[Safety integrity level\|SIL]] 4 in part 3 Annex B of the basic safety publication<ref>IEC 61508-3:2010</ref> and [[Automotive Safety Integrity Level\|ASIL]] D in part 6 of automotive standard [[ISO 26262]].<ref>ISO 26262-2011 Part 6 Table 12</ref> ==Definitions==

Modified condition/decision coverage: Difference between revisions