首页|期刊导航|北京航空航天大学学报|面向民机飞控系统适航性的空中故障注入系统

面向民机飞控系统适航性的空中故障注入系统OA

Airborne fault injection system for airworthiness compliance of civil aircraft flight control systems

中文摘要英文摘要

面对民机飞控系统适航符合性对于故障模拟试飞的必要性要求与空中注入故障引起的安全性风险之间的矛盾,提出一种满足民机飞控系统适航符合性验证要求的全部飞控系统故障模式的试飞故障注入系统,该系统经过充分试飞验证,并支持某型民机适航取证.所提故障注入系统的核心是基于简洁化、多模式的人机交互故障注入测试面板、飞行测试设备数据中枢及驻留于飞控计算机的故障注入控制触发程序,其保证了故障模拟的真实性与兼容性;同时,通过多种非相似的故障激励切除方式、故障激励限幅与监控机制,实现异常工况的可靠切断处理,经仿真,所提故障注入系统显著提升了系统安全性和故障容忍能力;此外,提出针对典型飞控系统故障的试飞模拟方案.通过装机试飞验证,对所提方案的可行性进行了验证.

To address the contradiction between the necessity of fault simulation flight testing for airworthiness compliance of civil aircraft flight control systems and the safety risks caused by fault injection in flight,this paper proposes a flight test fault injection system capable of covering all flight control system failure modes to meet airworthiness verification requirements.The system has undergone extensive flight validation and supports airworthiness certification for a specific civil aircraft model.A data hub for flight test equipment,a fault injection control trigger program integrated into the flight control computer,and a simplified,multi-mode human-machine interface testing panel comprise the core of the fault injection system,which ensures the compatibility and authenticity of fault simulations.In addition,the system accomplishes dependable handling of abnormal operating situations through a variety of distinct fault excitation cutoff methods,amplitude limiting mechanisms,and monitoring protocols,thereby considerably improving safety and fault tolerance.Furthermore,a flight test simulation strategy targeting typical flight control system failures is presented.The feasibility of the proposed approach is ultimately verified through in-flight testing with onboard implementation.

陈洁;孟杨;刘宏明

飞行控制航空科技重点实验室,西安 710065||中国航空工业集团公司西安飞行自动控制研究所,西安 710065飞行控制航空科技重点实验室,西安 710065||中国航空工业集团公司西安飞行自动控制研究所,西安 710065飞行控制航空科技重点实验室,西安 710065||中国航空工业集团公司西安飞行自动控制研究所,西安 710065

航空航天

飞控系统适航符合性故障模拟飞行试验操纵面卡阻操纵面松浮

flight control systemairworthiness compliancefault simulationflight testingcontrol surface jammingcontrol surface floating

《北京航空航天大学学报》 2026 (8)

2769-2779,11

10.13700/j.bh.1001-5965.2025.0705

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