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DALs, Design Assurance Levels, are the key measures assigned to software and hardware functions used to determine the level of stringency applied to different components of an avionics system.
The AEH are custom, microcoded components, or devices used as part of the airborne system. The primary. technologies include Programmable Logic Devices, Field Programmable Gate Arrays, Application-Specific Integrated Circuits, and similar circuits used as components of programmable electronic hardware.
The DO-254 standard defines a set of objectives for hardware to be certified for use in airborne systems. MATLAB and Simulink enable you to satisfy DO-254 objectives and support these processes: Requirements management and tracing. Conformance to design standards.
DO-178 and DO-254 are both standards developed by the Radio Technical Commission for Aeronautics (RTCA) to ensure the safety and reliability of electronic systems used in the aerospace industry. While DO-178 applies to software development, DO-254 is specific to electronic hardware development.
RTCA DO-254 / EUROCAE ED-80, Design Assurance Guidance for Airborne Electronic Hardware is a document providing guidance for the development of airborne electronic hardware, published by RTCA, Incorporated and EUROCAE.
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