標(biāo)準(zhǔn)號：SAE AIR 5273-2001
中文標(biāo)準(zhǔn)名稱：致動系統(tǒng)故障探測方法
英文標(biāo)準(zhǔn)名稱：Actuation System Failure Detection Methods
標(biāo)準(zhǔn)類型：V44;V43
發(fā)布日期：1999/12/31 12:00:00
實(shí)施日期：1999/12/31 12:00:00
中國標(biāo)準(zhǔn)分類號：V44;V43
國際標(biāo)準(zhǔn)分類號：49.090
引用標(biāo)準(zhǔn)：MIL-C-39029-1988;MIL-STD-1553-1978;SAE AIR 4094-1990;SAE AIR 4253-1989;SAE AS 4113-1989;831484;AC 25.1309;MIL-F-9490;MIL-STD-882;NPA 25C-199;RTCA DO-178
適用范圍：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.