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A kind of multi-rotor aerocraft pose stabilization control device

机译:一种多旋翼飞机姿态稳定控制装置

摘要

PROBLEM TO BE SOLVED: To drastically improve the responsiveness of posture control by performing the posture control by a gravitational center movement with respect to a rotor aound a roll axis and a pitch axis to permit the imbalance of a machine body or an individual difference or variation in rotor thrust or a motor output.SOLUTION: In a multi-rotor craft having rotors 4a to 4d arranged in a circumferential direction, a machine body 5 is connected below the center of a multi-rotor part via a rod 7 swingable around a roll axis or a pitch axis. A posture around the roll axis or the pitch axis is controlled based on the swing angle of the rod 7 around the roll axis or the pitch axis and by using the machine body 5 as a weight, and a posture around a yaw axis is controlled based on the rotational speeds of the rotors 4a to 4d.SELECTED DRAWING: Figure 1
机译:要解决的问题:通过相对于绕着横摇轴和俯仰轴的转子的重力中心运动执行姿态控制,以大大提高姿态控制的响应性,从而允许机体失衡或个体差异或变化解决方案:在具有沿圆周方向排列的转子4a至4d的多旋翼飞行器中,机体5通过可绕辊旋转的杆7连接在多旋翼部件的中心下方。轴或俯仰轴。基于杆7围绕侧倾轴​​线或俯仰轴线的摆动角度并且通过使用机体5作为重物来控制绕侧倾轴线或俯仰轴线的姿势,并且基于偏航轴线来控制围绕偏航轴线的姿势,所述杆7围绕侧倾轴​​线或俯仰轴线的摆角并以机器本体5为重。转子4a至4d的转速。图1

著录项

  • 公开/公告号JP6456641B2

    专利类型

  • 公开/公告日2019-01-23

    原文格式PDF

  • 申请/专利号JP20140198704

  • 发明设计人 岩田 拡也;

    申请日2014-09-29

  • 分类号B64C27/08;B64D27/24;B64C39/02;B64C17/02;

  • 国家 JP

  • 入库时间 2022-08-21 12:18:08

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