The embodiment of the invention relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle fault detection method, an unmanned aerial vehicle and an unmannedaerial vehicle system. The unmanned aerial vehicle fault detection method comprises the steps of acquiring flight state information of the unmanned aerial vehicle; skipping to a fault detection modelcorresponding to the information type of the flight state information; and executing a fault detection operation according to the fault detection model and the flight state information. According to the embodiment of the invention, the detection of various types of faults of the unmanned aerial vehicle can be achieved.

    本发明实施例涉及无人机技术领域,公开了一种无人机故障检测方法、无人机及无人机系统。其中,所述的无人机故障检测方法包括:获取所述无人机的飞行状态信息;跳转至与所述飞行状态信息的信息类型对应的故障检测模型;根据所述故障检测模型及所述飞行状态信息,执行故障检测操作。通过上述方式,本发明实施例能够实现无人机多种故障类型的检测。


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    Titel :

    Unmanned aerial vehicle fault detection method, unmanned aerial vehicle and unmanned aerial vehicle system


    Weitere Titelangaben:

    一种无人机故障检测方法、无人机及无人机系统


    Beteiligte:
    ZHANG TIANBAO (Autor:in)

    Erscheinungsdatum :

    04.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B60W CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION , Gemeinsame Steuerung oder Regelung von Fahrzeug-Unteraggregaten verschiedenen Typs oder verschiedener Funktion / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT





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