ARP5007A: Development Process - Aerospace Fly-By-Wire Actuation System - Recommended Practice

Features

Issuing Committee: A-6A3 Flight Control and Vehicle Management Systems Cmt

Scope

Content: 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.

Rationale

Content: ARP5007A has been reaffirmed to comply with the SAE five-year review policy.

Meta Tags

Topics: Fly-by-wire control systems
Hardware-in-the-loop (HIL)
Failure modes and effects analysis (FMEA)
Risk management
Defense industry
Product development
Systems management
Flight control systems
Control systems
Architecture
Electromagnetic compatibility

Details

DOI: https://doi.org/10.4271/ARP5007A

Pages: 26

Citation: SAE International Recommended Practice, Development Process - Aerospace Fly-By-Wire Actuation System, SAE Standard ARP5007A, Reaffirmed October 2010, Revised June 2005, Issued June 1997, https://doi.org/10.4271/ARP5007A.

Additional Details

Publisher: SAE International

Published: Oct 9, 2020

Product Code: ARP5007A

Content Type: Recommended Practice

Status: Reaffirmed

Language: English

Historical