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FLIGHT CONTROL SYSTEM WITH LOW-FREQUENCY INSTRUMENT LANDING SYSTEM LOCALIZER ANOMALY DETECTION AND METHOD OF USE
FLIGHT CONTROL SYSTEM WITH LOW-FREQUENCY INSTRUMENT LANDING SYSTEM LOCALIZER ANOMALY DETECTION AND METHOD OF USE
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机译:低频仪表着陆系统本地化异常检测的飞行控制系统及其使用方法
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摘要
A flight control module for detecting anomalies ILS localizer signals during landing of an aircraft is provided. The flight control module includes a communication interface coupled to a processor. The communication interface is configured to receive an ILS localizer deviation. The processor is configured to compute a plurality of localizer deviations and compare the ILS localizer deviation to an average of the plurality of localizer deviations to detect a low-frequency anomaly in the ILS localizer deviation. The processor is configured to initiate a transition from controlling the aircraft based on the ILS localizer deviation to controlling the aircraft based on a selected one of the plurality of localizer deviations when the low-frequency anomaly is detected.
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