首页> 外国专利> ERROR COMPENSATION SYSTEM AND METHOD FOR CIRCULAR LOITERING GUIDANCE CONTROL OF UNMANNED AERIAL VEHICLE

ERROR COMPENSATION SYSTEM AND METHOD FOR CIRCULAR LOITERING GUIDANCE CONTROL OF UNMANNED AERIAL VEHICLE

机译:无人飞行器的环行制导控制误差补偿系统及方法

摘要

An error compensation system for circular loitering guidance control of an unmanned aerial vehicle according to the present invention comprises: a flight control computer for outputting a circular loitering radius command (Rcmd) for an unmanned aerial vehicle, compensating circular loitering guidance control errors of the circular loitering radius command (Rcmd), and generating a compensated circular loitering radius command (R͂cmd); a control column driver (200) for driving a control column by receiving the compensated circular loitering radius command; an unmanned aerial vehicle flying under the control of the control column driver; and a navigation device for measuring a flight state of the unmanned aerial vehicle and transmitting the flight state to the flight control computer. Therefore, the present invention can eliminate circular loitering radius errors that are inevitably accompanied when an unmanned aerial vehicle circularly loiters by using a circular loitering command compensator, and thus can maintain a precise circular loitering radius to improve precision in unmanned aerial vehicle reconnaissance missions.
机译:根据本发明的用于飞行器的圆形游荡引导控制的误差补偿系统包括:飞行控制计算机,用于输出用于飞行器的圆形游荡半径命令(R cmd ),以补偿圆游荡半径指令(R cmd )的圆游荡制导控制误差,并生成补偿圆游荡半径指令(R͂ cmd );控制柱驱动器(200),用于通过接收补偿的圆游荡半径命令来驱动控制柱;在控制柱驾驶员的控制下飞行的无人飞行器;导航装置,其测量无人飞行器的飞行状态并将该飞行状态发送到飞行控制计算机。因此,本发明可以通过使用圆形游荡指令补偿器来消除无人飞行器圆形游荡时不可避免地伴随的圆形游荡半径误差,并且因此可以维持精确的圆形游荡半径,以提高无人飞行器侦察任务的精度。

著录项

  • 公开/公告号WO2019045541A1

    专利类型

  • 公开/公告日2019-03-07

    原文格式PDF

  • 申请/专利权人 KOREAN AIR LINES CO. LTD.;

    申请/专利号WO2018KR10202

  • 发明设计人 MOON JUNG HO;PARK MUN SOO;PARK JONG GEUN;

    申请日2018-09-03

  • 分类号G05D1/02;G05B6/02;G05D1;G08G5;

  • 国家 WO

  • 入库时间 2022-08-21 11:56:09

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