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This AIR provides descriptions of aircraft actuation system failure-detection methods. The methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight control. The AIR concentrates on full Fly-By-Wire (FBW) flight control actuation, but also includes one augmented-control system.The purpose of this document is to aid the designers of the systems of the future by showing what succeeded in the past.
Product Details
- Published:
- 01/11/2007
- File Size:
- 1 file , 660 KB
