A flight control device performs flight control processing for causing an eVTOL to fly. In the flight control processing steps (S104 to S106), the flight control device determines whether or not the eVTOL can be maintained in a stable attitude. In step (S104), a determination is made as to whether or not the eVTOL can be maintained in a stable posture even if the driving of the motor is abnormally stopped. In the steps (S105, S106), a determination is made as to whether or not the eVTOL can be maintained in a stable posture even if the driving of the abnormal motor is continued. When it is determined that the eVTOL can be maintained in the stable attitude, the flight control device (40) performs output adjustment of the normal motor and/or the abnormal motor in steps S107 to S110 so as to maintain the eVTOL in the stable attitude.

    一种飞行控制装置,进行用于使eVTOL飞行的飞行控制处理。飞行控制装置在飞行控制处理的步骤(S104~S106)中,对是否能够将eVTOL维持于稳定姿势进行判定。在步骤(S104)中,进行即使异常电动机的驱动停止是否也能够将eVTOL维持于稳定姿势的判定。在步骤(S105、S106)中,进行即使异常电动机的驱动继续是否也能够将eVTOL维持于稳定姿势的判定。在判断为能够将eVTOL维持于稳定姿势的情况下,飞行控制装置(40)在步骤S107~S110中进行正常电动机和异常电动机中的至少一方的输出调节,以将eVTOL维持于稳定姿势。


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    Titel :

    Flight control device, flight control program, and flight control method


    Weitere Titelangaben:

    飞行控制装置、飞行控制程序和飞行控制方法


    Beteiligte:
    TAKEMURA YUICHI (Autor:in) / FUKUSHI MASATO (Autor:in) / FUJII KEITA (Autor:in)

    Erscheinungsdatum :

    10.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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