SAE ARP 5007A:2005

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Development Process – Aerospace Fly-By-Wire Actuation System

Published By	Publication Date	Number of Pages
SAE	2005-06-28	26

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Categories: 33.100 - Electromagnetic compatibility (EMC), SAE

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Description

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.

Additional information

Published Code	SAE
Published By	SAE International, formerly Society of Automotive Engineers
Publication Date	2005-06-28
Pages Count	26
Language	English
Descriptors	Failure modes and effects analysis; Risk management; Defense industry; Product development; Systems management; Flight control systems; Hardware-in-the-loop; Control systems; Architecture; Electromagnetic compatibility
File Size	1.3 MB
ICS Codes	33.100 - Electromagnetic compatibility (EMC)

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SAE ARP 5007A:2005

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