One or more embodiments of the invention provide a control method and device of a rotorcraft, the rotorcraft and a computer readable storage medium. The rotorcraft comprises a power motor, and the method comprises the steps that target rotation parameter information, corresponding to the power motor, of the rotorcraft in a target flight state is obtained; controlling the rotorcraft to be in the target flight state, and acquiring actual rotation parameter information of the power motor; and determining the installation pose information of the power motor according to the difference between the actual rotation parameter information and the target rotation parameter information. According to the embodiment of the invention, the installation pose information of the power motor can be determined, and the rotorcraft can be controlled to move safely.

    本申请一个或多个实施例提供一种旋翼飞机的控制方法、装置、旋翼飞机及计算机可读存储介质;其中,所述旋翼飞机包括动力电机,所述方法包括:获取所述旋翼飞机处于目标飞行状态下对应所述动力电机的目标转动参数信息;控制所述旋翼飞机处于所述目标飞行状态,并获取所述动力电机的实际转动参数信息;根据所述实际转动参数信息和所述目标转动参数信息的差异,确定所述动力电机的安装位姿信息。本实施例通过上述方式能够确定动力电机的安装位姿信息,能够控制旋翼飞机安全运动。


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    Title :

    Rotor aircraft control method and device, rotor aircraft and storage medium


    Additional title:

    旋翼飞机的控制方法、装置、旋翼飞机及存储介质


    Contributors:
    WANG LU (author) / WANG KAI (author) / JIA XIANGHUA (author)

    Publication date :

    2023-05-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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