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Method and system for controlling attitude of rotor unmanned aerial vehicle

机译:旋翼无人机姿态控制方法及系统

摘要

A method for controlling an attitude of a rotor UAV (unmanned aerial vehicle) includes judging whether the rotor UAV is in a first attitude on a support base; and starting a first thrust generating device which is offset from a first side of a center of gravity of the rotor UAV, the first thrust generating device generating a thrust that faces away from the support base while working, the first side moving away from the support base, flipping the rotor UAV and switching the rotor UAV from the first attitude to a second attitude. Also, a system for controlling the attitude of the rotor UAV is provided. According to the method and the system, the rotor UAV can be switched between different attitudes without artificially assisting in adjusting a current attitude of the rotor UAV, so that the convenience in use and the satisfaction of experience are improved.
机译:一种控制旋翼无人机(无人机)姿态的方法,包括判断旋翼无人机在支撑座上是否处于第一姿态;并启动与转子无人机的重心的第一侧偏移的第一推力产生装置,该第一推力产生装置在工作时产生背向支撑基座的推力,第一侧背离支撑架移动基座,翻转旋翼无人机并将旋翼无人机从第一姿态切换到第二姿态。另外,提供了一种用于控制转子UAV的姿态的系统。根据该方法和系统,无需人为地调节转子无人机的当前姿态,就可以在不同姿态之间切换转子无人机,从而提高了使用的便利性和体验的满意度。

著录项

  • 公开/公告号US2019004541A1

    专利类型

  • 公开/公告日2019-01-03

    原文格式PDF

  • 申请/专利权人 HAOXIANG ELECTRIC ENERGY (KUNSHAN) CO. LTD.;

    申请/专利号US201816104893

  • 发明设计人 YU TIAN;WENYAN JIANG;

    申请日2018-08-18

  • 分类号G05D1/08;B64C39/02;

  • 国家 US

  • 入库时间 2022-08-21 12:06:27

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