首页> 外国专利> ATTITUDE CONTROLLER FOR UNMANNED HELICOPTER

ATTITUDE CONTROLLER FOR UNMANNED HELICOPTER

机译:无人驾驶直升机的姿态控制器

摘要

PROBLEM TO BE SOLVED: To provide the attitude controller of an unmanned helicopter stabilizing a flight attitude by reducing loads applied to respective driving devices by simple structure. ;SOLUTION: The attitude controller of an unmanned helicopter is provided with an attitude controlling sensor 12 detecting the attitude angle, etc., of the plural virtual axes of the unmanned helicopter, plural driving means 6A to 6C varying the inclination of the virtual axes, a receiver 11 receiving an operating signal for changing the inclination of the virtual axes when signal is transmitted from a remote control transmitter and converting the signal to a able signal to output, and control means 13A to 13C driving the plural driving means 6A to 6C so as to assign the loads to the driving means based on the cable signal and a signal outputted from the sensor 12.;COPYRIGHT: (C)1998,JPO
机译:要解决的问题:提供一种无人直升机的姿态控制器,通过简单的结构减少施加在各个驱动装置上的载荷,从而稳定飞行姿态。 ;解决方案:无人直升机的姿态控制器配备有姿态控制传感器12,用于检测无人直升机的多个虚拟轴的姿态角等;多个驱动装置6A至6C可以改变虚拟轴的倾斜度;接收器11接收操作信号,该操作信号用于当从遥控发送器发送信号时改变虚拟轴的倾斜度,并将该信号转换为能够输出的信号,并且控制装置13A至13C驱动多个驱动装置6A至6C,从而根据电缆信号和传感器12输出的信号将负载分配给驱动装置;版权所有:(C)1998,JPO

著录项

  • 公开/公告号JPH10328427A

    专利类型

  • 公开/公告日1998-12-15

    原文格式PDF

  • 申请/专利权人 MUGEN:KK;

    申请/专利号JP19970155758

  • 发明设计人 OKAMOTO NARUMI;

    申请日1997-05-28

  • 分类号A63H27/133;B64C39/02;

  • 国家 JP

  • 入库时间 2022-08-22 02:33:02

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号