MIL-C-39029-1988MIL-STD-1553-1978SAE AIR 4094-1990SAE AIR 4253-1989SAE AS 4113-1989831484AC 25.1309MIL-F-9490MIL-STD-882NPA 25C-199RTCA DO-178
适用范围
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.