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SAE ARP 5007 : 2012

SAE ARP 5007 : 2012

DEVELOPMENT PROCESS - AEROSPACE FLY-BY-WIRE ACTUATION SYSTEM

SAE International

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Table of Contents

FOREWORD
1. SCOPE
2. REFERENCES
3. SYSTEM DEVELOPMENT PHASES
4. SYSTEM REQUIREMENTS ANALYSIS
5. ELECTRONICS AND ACTUATOR REQUIREMENTS
6. PRELIMINARY DESIGN
7. DETAILED DESIGN
8. DEVELOPMENT/FABRICATION
9. ACTUATION SYSTEM INTEGRATION

Abstract

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.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee A-6

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