Development Process - Aerospace Fly-By-Wire Actuation System
This document provides a description of a process for development of fly-by-wire actuation systems. Included are (1) the development of requirements for the servo-actuator hardware and the electronics hardware and software, (2) actuator and servo-electronics interface definitions and, (3) the required communications and interactions between the servo-actuator and the servo-electronics designers.
Rationale: Document is a bit dated, written around Military development structure, and does not include Commercial development issues, such as: FAA and EASA requirements, Working with an ODA, Certification and Conformity issues, etc. Recommend bringing document up to date and including commercial development items.