DO-178C outlines objectives for each process, with more rigorous requirements for higher safety levels. It’s particularly relevant for safety-critical systems where software failures could lead to severe consequences. Organizations implementing this standard include RCI, DRDL, and BrahMos. The most current version of DO-178C was released in December 2011, serving as the primary reference for airborne software development guidelines.

The DO-178C standard defines the Design Assurance Levels (DAL), ranging from Level A to Level E, depending on the potential impact of system failure. Level A represents the most stringent level, where failure could lead to catastrophic outcomes, while Level E applies to systems where failure has no safety effect.

From the initial planning stages to final certification, the software development process must comply with DO-178C standards based on the assigned Design Assurance Level. This involves adhering to a strict set of guidelines, ensuring that each phase of development—requirements, design, coding, testing, and verification—meets the safety and reliability criteria.

DO-178C provides comprehensive guidance to produce software for airborne systems and equipment, ensuring that the software performs its intended function with a level of safety that complies with airworthiness requirements. By following this standard, organizations can certify that their software meets the highest levels of safety, reliability, and regulatory compliance.