SAE ARP5007A – 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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Published:
10/09/2020
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1 file , 670 KB
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