Name | Support | Language | Availability | Edition date | Price | ||
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PDF |
English |
Active |
8/10/2012 |
€162.00 |
|
Details
This SAE Aerospace Information Report (AIR) provides design information of various contemporary aircraft fly-by-wire (FBW) flight control actuation systems that may be useful in the design of future systems for similar applications. It is primarily applicable to manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein, however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.
Additional Info
Author | Society of Automotive Engineers International (SAE) |
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Committee | A-6A3 Flight Control and Vehicle Management Systems Cmt |
Published by | SAE |
Document type | Standard |
Theme | Flight control systems,Fly-by-wire control systems,Electronic control systems,Sensors and actuators,Aerospace |
Confirmation date | 2018-07-24 |
ICS | 49.045 : Structure and structure elements
|
Number of pages | 160 |
Replace | SAE AIR 4253A:2001-04-01 |
Set | AEROPAKS10U-10 |
Document history | SAE AIR 4253A:2001-04-01,SAE AIR 4253:1999-05-01 |
Keyword | SAE 4253,SAE AIR4253B,SAE AIR4253B,SAE AIR 4253 |