SAE ARP 5007 : 2012
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
DEVELOPMENT PROCESS - AEROSPACE FLY-BY-WIRE ACTUATION SYSTEM
Hardcopy , PDF
17-10-2020
English
26-04-2012
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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
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.
| Committee |
A-6A3
|
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AIR4543/1A | Aerospace Hydraulics and Actuation Lessons Learned |
| SAE ARP5724 | Aerospace - Testing of Electromechanical Actuators, General Guidelines For |
| SAE AIR4094A | Aircraft Flight Control Systems Descriptions |
| SAE ARP4386C | Terminology and Definitions for Aerospace Fluid Power, Actuation and Control Technologies |
| SAE AIR4922A | Primary Flight Control Hydraulic Actuation System Interface Definition |
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