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SAE ARP 5007A-2005 (SAE ARP5007A-2005)

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.

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