Electronic Flight Control System
GPTKB entity
Statements (48)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Flight control system
|
| gptkbp:advantage |
Increased reliability
Enhanced safety Reduced weight Improved aircraft performance |
| gptkbp:alsoKnownAs |
Fly-by-wire system
|
| gptkbp:category |
gptkb:aircraft
Aircraft systems |
| gptkbp:component |
Sensors
Wiring Actuators Flight control computer |
| gptkbp:developedBy |
gptkb:Lockheed_Martin
gptkb:Boeing gptkb:Airbus |
| gptkbp:enables |
Reduced pilot workload
Active control technology Automatic stability augmentation Autopilot integration Digital flight control Flight data monitoring Flight envelope protection Fly-by-wire control |
| gptkbp:example |
gptkb:Boeing_777
gptkb:aircraft gptkb:Dassault_Rafale F-35 Lightning II |
| gptkbp:function |
Controls aircraft surfaces electronically
|
| https://www.w3.org/2000/01/rdf-schema#label |
Electronic Flight Control System
|
| gptkbp:introducedIn |
gptkb:aircraft
|
| gptkbp:relatedTo |
gptkb:Avionics
gptkb:Autopilot Hydraulic system Flight management system Mechanical flight control system Power-by-wire system |
| gptkbp:replacedBy |
Mechanical flight control system
|
| gptkbp:riskFactor |
Redundancy
Backup systems Electrical failure Fail-safe design Software failure |
| gptkbp:standardizedBy |
gptkb:EASA
gptkb:FAA |
| gptkbp:usedIn |
gptkb:aircraft
Commercial aircraft |
| gptkbp:bfsParent |
gptkb:EFCS
|
| gptkbp:bfsLayer |
7
|