The invention discloses a runtime guarantee method, system and equipment of an SPO mode airplane and a medium, and relates to the technical field of aircraft airborne avionics systems. The method comprises the following steps: acquiring information of a plurality of sensors; analyzing and fusing the sensor information to obtain fused data; dynamically evaluating the fused data by using a system model, and outputting an SPO air-ground collaborative interaction scheme; performing overground control according to the fused data, and outputting overground control information; and carrying out responsibility switching according to the sensor information and the SPO air-ground cooperative interaction scheme, so as to ensure that the SPO air-ground cooperative interaction scheme or the ground control information is output during operation. The safety and stability of the aircraft flying in the air can be improved.

    本发明公开一种SPO模式飞机的运行时保证方法、系统、设备及介质,涉及航空器机载航电系统技术领域。所述方法包括:获取多个传感器信息;对所述传感器信息进行分析融合处理,得到融合数据;利用系统模型对所述融合数据进行动态评估,输出SPO空地协同交互方案;根据所述融合数据进行地上控制,输出地上控制信息;根据所述传感器信息和所述SPO空地协同交互方案,进行职责切换,使运行时保证输出为所述SPO空地协同交互方案或所述地上控制信息。本发明能够提升航空器在空中飞行的安全性和稳定性。


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    Title :

    Runtime guarantee method, system and equipment of SPO mode airplane and medium


    Additional title:

    SPO模式飞机的运行时保证方法、系统、设备及介质


    Contributors:
    DONG LEI (author) / LIU JIACHEN (author) / CHEN XI (author) / WANG PENG (author) / YU YONGYUE (author) / ZHAO CHANGXIAO (author)

    Publication date :

    2024-01-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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