The invention provides an aircraft landing method and the like, which can improve the landing performance of an aircraft with directivity by facing a nose direction with good balance between lift force and resistance according to wind speed data and wind direction data related to a landing point in the aircraft with directivity. According to the landing method of the aircraft, the aircraft is of a structure which generates lift force according to wind from the direction of the nose of a fuselage, the direction of the nose of the fuselage is controlled according to wind speed data and wind direction data related to a landing site, and the landing of the fuselage is started.

    本发明提供一种飞行器的降落方法等,在具有方向性的飞行器中,通过根据与降落地点相关的风速数据和风向数据而朝向升力与阻力的平衡良好的机头方向,能够提高具有方向性的飞行器的降落性能。在本发明的飞行器的降落方法中,所述飞行器是对应来自机身的机头方向的风而产生升力的结构,根据与降落地点相关的风速数据和风向数据,对所述机身的机头方向进行控制,开始所述机身的下降。


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    Titel :

    Aircraft landing method, aircraft, information processing device, and program


    Weitere Titelangaben:

    飞行器的降落方法、飞行器、信息处理装置、程序


    Beteiligte:
    SUZUKI YOUICHI (Autor:in)

    Erscheinungsdatum :

    08.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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