SAE ARP5007A PDF
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Development Process – Aerospace Fly-By-Wire Actuation System
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.
History
| ARP5007A | 2020-10-09 | Latest | Reaffirmed |
| ARP5007 | 1997-06-01 | Historical | Issued |
| ISSUING COMMITTEE | A-6A3 Flight Control and Vehicle Management Systems Cmt |
|---|---|
| DATE | 2020-10-09 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 26 |
| PUBLISHER | SAE International |
| REVISED | REAFFIRMED |
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