SAE ARP 5007 : 2012
SAE ARP 5007 : 2012
DEVELOPMENT PROCESS - AEROSPACE FLY-BY-WIRE ACTUATION SYSTEM
SAE International
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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AS 1684.2 N4 Supp 7-2006
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