SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems
Sections 5.3 and 5.4: Requirements capture and requirements validation – SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems

SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems 5.3.1.10: 5.3.1.10 Derived requirements

At each development phase, design decisions on how to meet requirements become requirements for the next phase; because they come from the design process they can add behaviors or characteristics beyond those in higher-level requirements, and are called derived requirements. Examples are the requirements for a separately selected power supply (whose development assurance level follows the classifications of the function it supports), the different consequences of choosing a triplex or a dual-monitored architecture, isolation of more severe functions from less severe ones, and requirements defining the hardware-software interface, some of which matter at system level while the detailed rest falls under DO-178C and DO-254. Each derived requirement is examined to establish the functions it serves, so that it receives the correct failure condition classification and is validated (see 5.3.3); they are captured and treated like other requirements at that phase and carry their rationale or references to applicable design standards.

Maintained by Gerard Blokdyk

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  • A-2.5 Derived low-level requirements identified and passed to the system and safety processes

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Other controls in Sections 5.3 and 5.4: Requirements capture and requirements validation – SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems

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