The invention provides an unmanned helicopter hanging load release monitoring method, and relates to the technical field of unmanned helicopters.The adopted monitoring device comprises a force measurement sensing unit, an inclination angle sensing unit, a control unit, a power supply unit, a power supply unit, a power supply unit, a power supply unit, a power supply unit, a power supply unit, a power supply unit and a power supply unit, wherein the force measurement sensing unit is used for detecting the pulling force of a hanging rope to a hanging load; the proximity signal unit is used for detecting the opening and closing state of the hook, the first hook opening actuator and the second hook opening actuator are used for controlling the hook, and the control unit is used for monitoring the state of a hanging load and completing the putting of the hanging load through manual or automatic control; the monitoring method adopts the monitoring device to monitor the hanging load releasing process. According to the invention, through monitoring the data of the system, the whole-process monitoring and full-automatic putting of the hanging load are realized. According to the invention, alarm prompt is realized in an abnormal state, and emergency release can be carried out on the hanging load in a state that the safety of the unmanned helicopter is seriously influenced, so that the flight safety of the unmanned helicopter is guaranteed.

    本发明提供了一种无人直升机吊挂载荷投放监控方法,涉及无人直升机技术领域,采用的监测装置包括:用于检测吊绳对吊挂载荷的拉力的测力传感单元,用于检测吊挂载荷的倾角、俯仰角度和角加速度的倾角传感单元,用于检测挂钩开关状态的接近信号单元,分别用于控制挂钩的第一开钩作动器和第二开钩作动器以及控制单元,控制单元用于监控吊挂载荷状态,通过人工或自动控制完成吊挂载荷的投放;监控方法采用上述监测装置对吊挂载荷投放过程进行监控。本发明通过监测系统的数据,实现对吊挂载荷全程监控和全自动投放。本发明在出现异常的状态下实现告警提示,在严重影响无人直升机安全的状态下能够对吊挂载荷进行的应急投放,以保障无人直升机飞行安全。


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    Titel :

    Unmanned helicopter hanging load release monitoring method


    Weitere Titelangaben:

    一种无人直升机吊挂载荷投放监控方法


    Beteiligte:
    WEN HOULIN (Autor:in) / CHEN DONG (Autor:in) / PENG JUN (Autor:in) / LIU SHUAI (Autor:in) / ZENG DONG (Autor:in) / TANG HAOYUE (Autor:in) / WANG LINTAO (Autor:in)

    Erscheinungsdatum :

    2024-04-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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