This thread is for discussing the lifecycle document "Conceptual Design and Architecture: stage guide".
How the hardware architecture, device technology, component set and software architecture are chosen so the requirements are met, the safety assessment's independence and fault tolerance assumptions hold, and the parts can be supported for the life of the aircraft. For hardware and software architects, component engineers, safety analysts and environmental qualification engineers.
Read the document: https://www.thesemiconhub.com/lifecycle/avionics/avi-conceptual-design/document
Point out anything that is wrong, unclear or missing, and say which section you mean. Reviewers read this thread when they audit the document.