An unmanned aerial vehicle electric power consumption control method comprises the following steps of a, dismantling a fuel oil power system of the unmanned aerial vehicle, and assembling an electricpropulsion system; b, calculating the required maximum thrust Fc; c, calculating the power consumption of the motor, wherein the steps are as follows: S3, calculating the power consumption of the unmanned aerial vehicle in a climbing stage, and S4, calculating the power consumption of the unmanned aerial vehicle in a cruising stage; S5, calculating the power consumption of the unmanned aerial vehicle in the gliding stage; S6, enabling the power consumption in the parachute recovery stage to be 0; S7, calculating the power consumption of the unmanned aerial vehicle equipment; and S8, calculating the total power consumption Wcell of the unmanned aerial vehicle. The modification method can ensure that the performance is basically unchanged after the electric propulsion system of the unmannedaerial vehicle is replaced, and the use cost of the unmanned aerial vehicle is greatly reduced.

    一种无人机电动功率耗电量的控制方法,包括以下步骤:a、拆除无人机的燃油动力系统,组装上电推进系统;b、计算所需的最大推力Fc;c、计算电动机耗电量,步骤如下:S3、计算无人机爬升阶段耗电量,S4、计算无人机巡航阶段的耗电量;S5、计算无人机下滑阶段的耗电量;S6、伞降回收阶段耗电量为0;S7、计算无人机设备用电耗电量:S6、计算无人机总耗电量Wcell。能够保证无人机换装电推进系统后,性能基本不变,并较大幅度降低无人机使用成本的改造方法。


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    Titel :

    Unmanned aerial vehicle electric power consumption control method


    Weitere Titelangaben:

    一种无人机电动功率耗电量的控制方法


    Beteiligte:
    ZOU NING (Autor:in) / LIANG SHUANG (Autor:in) / LU WENZHUO (Autor:in) / DU SHENGCHAO (Autor:in) / YAO XIAOYI (Autor:in) / WANG SHUFANG (Autor:in)

    Erscheinungsdatum :

    07.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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