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基于IBA-LSSVM強迫選擇模型的民用飛機著(zhù)陸滑行儀表燈常亮故障關(guān)聯(lián)檢測
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航空工業(yè)西安飛機工業(yè)集團有限公司

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Correlative Detection of the Constant Illumination of the Taxi Indicator Light of the Civil Aircraft Landing by Introducing IBA-LSSVM Forced Selection Model
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    摘要:

    民用飛機著(zhù)陸滑行儀表燈是故障檢測系統的重要組成部分,因民用飛機在地面滑行過(guò)程中,電氣接口易受到電磁干擾,引起著(zhù)陸滑行儀表燈常亮故障,在飛行過(guò)程中增加了安全隱患。為此,提出引入IBA-LSSVM強迫選擇模型的民用飛機著(zhù)陸滑行儀表燈常亮故障關(guān)聯(lián)檢測方法。分析儀表燈常亮故障產(chǎn)生的原因,利用Python編程數據采集飛機起飛、近進(jìn)、降落、地面滑行時(shí)的照明信號及電氣交聯(lián)數據,通過(guò)控制邏輯,建立數據關(guān)聯(lián)檢測邏輯關(guān)系數據庫。利用自適應多普勒補償方法改進(jìn)蝙蝠算法(IBA),檢測著(zhù)陸滑行燈常亮故障特征,在強迫選擇部分,構建IBA-LSSVM模型,將分布式博弈和線(xiàn)性輸出調節理論相結合,抵消外部干擾,完成著(zhù)陸滑行燈常亮故障檢測。Matlab仿真測試結果表明:所提方法的故障識別率均在95%以上,故障識別準確率可以達到97.3%,故障識別時(shí)間低于2ms,可有效識別故障數據,降低飛行安全隱患。

    Abstract:

    The landing taxiing instrument light of civil aircraft is an important part of the fault detection system. Because the electrical interface of civil aircraft is vulnerable to electromagnetic interference during the ground taxiing process, the landing taxiing instrument light is always on, which increases the potential safety hazard during flight. For this reason, a correlation detection method for the constant light fault of the taxiing instrument lights of civil aircraft landing is proposed by introducing the IBA-LSSVM forced selection model. Analyze the cause of the instrument light constant lighting fault, use Python programming data to collect the lighting signals and electrical cross-linking data during aircraft takeoff, approach, landing and ground taxiing, and establish a data association detection logic relationship database through control logic. The bat algorithm (IBA) is improved by using adaptive Doppler compensation method to detect the fault characteristics of the landing taxiing light always on. In the forced selection part, the IBA-LSSVM model is constructed. The distributed game theory and linear output regulation theory are combined to eliminate external interference, and the landing taxiing light always on fault detection is completed. Matlab simulation test results show that the fault identification rate of the proposed method is above 95%, the fault identification accuracy can reach 97.3%, and the fault identification time is less than 2ms, which can effectively identify fault data and reduce flight safety hazards.

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郝精一.基于IBA-LSSVM強迫選擇模型的民用飛機著(zhù)陸滑行儀表燈常亮故障關(guān)聯(lián)檢測計算機測量與控制[J].,2023,31(11):46-52.

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  • 收稿日期:2023-01-05
  • 最后修改日期:2023-02-21
  • 錄用日期:2023-02-22
  • 在線(xiàn)發(fā)布日期: 2023-11-23
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