首页> 外国专利> METHOD IN WHICH SMALL FIXED-WING UNMANNED AERIAL VEHICLE FOLLOWS PATH AND LGVF PATH-FOLLOWING CONTROLLER USING SAME

METHOD IN WHICH SMALL FIXED-WING UNMANNED AERIAL VEHICLE FOLLOWS PATH AND LGVF PATH-FOLLOWING CONTROLLER USING SAME

机译:使用该方法的小型固定翼无人空中飞行器遵循路径和LGVF路径的方法

摘要

Provided is an LGVF path-following controller including: an LGVF control unit that is provided with a heading angle command for a wing-fixed unmanned aerial vehicle and guidance commands from the outside, and is provided with a computed estimation disturbance speed from a nonlinear disturbance control unit; a heading angle computation control unit that computes a final heading angle of the wing-fixed unmanned aerial vehicle using a difference between the heading angle of the wing-fixed unmanned aerial vehicle, which is computed by the LGVF control unit, and a heading angle of the wing-fixed unmanned aerial vehicle in an ideal environment where a disturbance is not present; and a nonlinear disturbance control unit that computes the estimation disturbance speed using the final heading angle provided from the heading angle computation control unit and pieces of sensor data on the wing-fixed unmanned aerial vehicle, which are provided from a sensor.
机译:提供了一个LGVF路径跟踪控制器,包括:LGVF控制单元,其具有用于翼固定无人驾驶车辆的标题角度命令和来自外部的引导命令,并且具有来自非线性干扰的计算估计干扰速度 控制单元; 使用由LGVF控制单元计算的翼固定无人驾驶飞行器的标题角度之间的差异计算机翼固定无人驾驶飞行器的最终标题角度的标题角计算控制单元。 翼固定的无人空中车辆在理想的环境中,不存在干扰; 和一个非线性扰动控制单元,其使用从传感器提供的翼固定无人驾驶飞行器上的标题角计算控制单元和传感器数据部分提供的最终镦扰速度。

著录项

  • 公开/公告号EP3889723A1

    专利类型

  • 公开/公告日2021-10-06

    原文格式PDF

  • 申请/专利权人 PABLO AIR CO. LTD.;

    申请/专利号EP20200211281

  • 发明设计人 DONG MIN SHIN;

    申请日2020-12-02

  • 分类号G05D1/02;

  • 国家 EP

  • 入库时间 2022-08-24 21:28:29

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