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SAE ARP5007 Rev A

Current Revision

Development Process - Aerospace Fly-By-Wire Actuation System

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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.

SDO SAE: SAE International
Document Number ARP5007
Publication Date June 28, 2005
Language en - English
Page Count 26
Revision Level A
Supercedes
Committee
Publish Date Document Id Type View
June 28, 2005 ARP5007A Revision
June 1, 1997 ARP5007 Revision