飞机主动侧杆故障行为模式研究
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1.北京航空航天大学 自动化科学与电气工程学院;2.贵州华烽电器有限公司

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基于欠均匀时空数据融合与知识协同驱动的大跨度金属屋面故障预测与健康评估


Research on the Behavior Mode of Active Side
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    摘要:

    主动侧杆(active side stick, ASS)是一种新型飞机操纵杆,在遭遇故障时,ASS力反馈不准确,轻则导致飞行员对飞行状态的感知出现偏差,重则导致驾驶杆抖动、打手,严重影响飞行安全。ASS实时性能监测可在故障明显影响操纵性能前给出预警,具有十分重大的意义。充分研究ASS发生故障时的特征,分析对系统产生的影响,是实现性能监测前亟待解决的问题。为解决该问题,构建了ASS的AMESim模型,基于ASS的故障模式与影响分析(failure mode and effects analysis,FMEA)与故障树分析的方法得到潜在的几类关键故障,讨论了故障影响ASS性能的方式,并在模型中实现关键故障注入,获取关键故障的相关状态量信息,分析故障特征与状态量变化特点,为ASS故障诊断工作开展提供了理论基础。

    Abstract:

    The active side stick(ASS) is a novel type of aircraft control stick. When malfunctions occur, the ASS may provide inaccurate force feedback. Minor issues can lead to the pilot"s misperception of the flight state, while severe problems can cause the control stick to shake or jerk, significantly compromising flight safety. Real-time performance monitoring of the ASS offers crucial early warnings before faults significantly affect control performance. Thorough research on the characteristics of ASS failures and their impact on the system is essential before implementing performance monitoring.To address this issue, an AMESim model of the ASS was developed. By employing methods such as Failure Mode and Effects Analysis(FMEA) and Fault Tree Analysis, several potential key faults were identified. The study explored how these faults impact ASS performance. Key faults were injected into the model to gather data on relevant state variables. This approach facilitated an analysis of fault characteristics and changes in state variables, providing a theoretical foundation for diagnosing faults in active side sticks.

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钱威,杨丽曼,韩兵.飞机主动侧杆故障行为模式研究计算机测量与控制[J].,2025,33(7):27-37.

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  • 收稿日期:2024-05-12
  • 最后修改日期:2024-06-26
  • 录用日期:2024-06-27
  • 在线发布日期: 2025-07-16
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