摘要
FAA AC25-7A中的飞行品质评定方法 (HQRM)能够对使用电子飞控系统的民用运输机进行飞行品质评估。分析了HQRM评估程序以及相关适航要求,根据某民用飞机飞控系统功能危险分析,针对单侧升降舵卡阻这一典型故障,提出了在该失效状态下的模拟器飞行品质评估试验程序,分别给出了HQRM和相应军用标准评估方法,对军民评估方法的差异性和一致性进行了分析。研究结果对采用电子飞控系统的现代飞机的飞行品质适航验证具有工程参考意义。
Handling quality rating method（HQRM） in FAA AC25-7A provide a means by which one may evaluate flight characteristics for fly-by-wire flight control transport aircraft.This paper explains the HQRM procedure,and analyses airworthiness requirements which are related to HQRM.According to flight control system functional hazard assessment of a commercial airplane,simulator experiment procedure for a elevator jam is proposed,and experiment analysis methods using the FAA method and military standard are offered.The consistency and differences between civil and military standards are analyzed.This study can supply references for flying qualities and airworthiness verification of a modern airplane with electrical flight control system.
出处
《飞行力学》
CSCD
北大核心
2012年第2期117-120,共4页
Flight Dynamics
关键词
飞行品质评定方法
电子飞控系统
适航验证
工程模拟器
功能危险分析
handling quality rating method
electrical flight control system
airworthiness verification
engineering simulator
functional hazard assessment
