首页> 外国专利> Universal control system for robust trajectories a result of the case of unmanned multi rotor air vehicles (uavs)

Universal control system for robust trajectories a result of the case of unmanned multi rotor air vehicles (uavs)

机译:无人驾驶多旋翼飞行器(UAV)的结果,用于稳定轨迹的通用控制系统

摘要

A universal control system for a robust trajectories a result of the case of unmanned multi rotor air vehicles (uavs, unmanned aerial vehicles) is disclosed. A specific embodiment comprises: a sensor system for measuring a position and orientation of an unmanned multi rotor air vehicle (uav); and a flight expensive system, which is coupled to the sensor system, wherein the flight expensive system is configured to: obtaining position - and orientation data of the sensor system; generating a plurality of discharge lines from the positions - and orientation data by using a differentiator; applying a decoupling control law to the approximate decoupling of the trans modulation dynamics from one another in a three-dimensional (3d) space; calculating error values between desired trajectories and actual trajectories in each dimension of the 3d - space under use of the plurality of discharge lines and of the decoupled dynamics; and generating control signals to the varying rotational speeds of a plurality of thrust elements, by the calculated error values in each dimension of the 3d - space to counteract.n="44"
机译:公开了一种用于无人轨迹的通用控制系统,其是无人多旋翼飞行器(无人机,无人飞行器)的情况的结果。一个具体实施例包括:用于测量无人多旋翼飞行器(uav)的位置和定向的传感器系统;昂贵的飞行系统,其耦合到传感器系统,其中,昂贵的飞行系统被配置为:获取传感器系统的位置和方向数据;以及通过使用微分器从位置和方向数据生成多条放电线;将去耦控制律应用到三维(3d)空间中的互调动力学的近似解耦;在使用多个排放管线和解耦的动力学的情况下,计算3d空间的每个维度中的期望轨迹与实际轨迹之间的误差值;通过计算要抵消的3d-空间中每个维度的误差值,生成针对多个推力元件变化的转速的控制信号。n=“ 44”

著录项

  • 公开/公告号DE112015007209T5

    专利类型

  • 公开/公告日2018-10-25

    原文格式PDF

  • 申请/专利权人 INTEL CORPORATION;

    申请/专利号DE20151107209T

  • 发明设计人 DAVID GOMEZ GUTIERREZ;MAYNARD C. FALCONER;

    申请日2015-12-22

  • 分类号B64C39/02;B64D45;B64C27/08;

  • 国家 DE

  • 入库时间 2022-08-21 12:34:56

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