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UNMANNED AERIAL VEHICLE-BASED LOAD CONTROL METHOD AND DEVICE, AND UNMANNED AERIAL VEHICLE

机译:基于无人飞行器的载荷控制方法和装置,以及无人飞行器

摘要

An unmanned aerial vehicle-based load control method and device, and an unmanned aerial vehicle. The unmanned aerial vehicle comprises: an unmanned aerial vehicle body, propeller arms connected at first ends to the unmanned aerial vehicle body and having adjustable lengths, propeller blades connected to second ends of the propeller arms and having adjustable sizes, and a processor mounted within the unmanned aerial vehicle body. The control method comprises: on the basis of a carrying object of the unmanned aerial vehicle, determining a load gravity of the unmanned aerial vehicle; on the basis of the load gravity, determining a target lifting force of the unmanned aerial vehicle; according to the target lifting force, determining a target size for the propeller blades and a target length for the propeller arms; adjusting the propeller arms to the target length and adjusting the propeller blades to the target size, so as to enable the unmanned aerial vehicle to control the propeller blades to rotate to generate a lifting force to carry the carrying object. The control method avoids energy waste of the unmanned aerial vehicle, so that the energy of the unmanned aerial vehicle is fully utilised.
机译:基于无人飞行器的负荷控制方法和装置,以及无人飞行器。该无人飞行器包括:无人飞行器主体;在其第一端连接到无人飞行器主体并且具有可调节的长度的螺旋桨臂;连接到该螺旋桨臂的第二端并具有可调节的尺寸的螺旋桨叶片;以及安装在该飞行器中的处理器。无人机机体。该控制方法包括:基于无人飞行器的运载对象,确定无人飞行器的负载重力;以及根据负载重力,确定无人机的目标举升力;根据目标举升力,确定螺旋桨叶片的目标尺寸和螺旋桨臂的目标长度。将螺旋桨臂调整至目标长度,并将螺旋桨叶片调整至目标尺寸,以使无人机能够控制螺旋桨叶片旋转以产生提升力来搬运携带物体。该控制方法避免了无人飞行器的能源浪费,从而充分利用了无人飞行器的能量。

著录项

  • 公开/公告号WO2019100482A1

    专利类型

  • 公开/公告日2019-05-31

    原文格式PDF

  • 申请/专利权人 GOERTEK TECHNOLOGY CO. LTD.;

    申请/专利号WO2017CN117045

  • 发明设计人 LIN JINGSHUN;

    申请日2017-12-18

  • 分类号B64C27/32;B64C27/46;B64C11/30;

  • 国家 WO

  • 入库时间 2022-08-21 11:54:37

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