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The piloting in yaw to rotorcraft, using a device leads to the skilled person which generated of the flight controls by objective

机译:使用一种装置对旋翼飞机进行偏航驾驶,使技术人员可以客观地进行飞行控制

摘要

The device has a kinematic chain that integrates a target control unit (16) whose setting in work is placed under dependence of a movable control element (12) trained by a man. The movable control element transmits a control signal (11) toward another target control unit (17), which generates a control command (29) in yaw towards a calculation unit of another kinematic chain, where the command in yaw is relative in a progression state to reach a rotorcraft (1). Implementation of the calculation unit is placed under dependence of a control button actuated by the man. An independent claim is also included for a method for controlling flight in yaw of a rotorcraft.
机译:该装置具有运动链,该运动链整合了目标控制单元(16),其目标设定取决于人为训练的可移动控制元件(12)的作用。可移动控制元件向另一个目标控制单元(17)传输控制信号(11),目标控制单元(17)在偏航方向上向另一个运动链的计算单元生成控制命令(29),其中偏航命令是相对于前进状态的到达旋翼机(1)。计算单元的实现被置于由人致动的控制按钮的依赖之下。还包括用于控制旋翼飞机的偏航的方法的独立权利要求。

著录项

  • 公开/公告号FR2981045B1

    专利类型

  • 公开/公告日2013-10-25

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号FR20110003067

  • 发明设计人 SERGE MEZAN;

    申请日2011-10-10

  • 分类号B64C13/04;G05D1/08;

  • 国家 FR

  • 入库时间 2022-08-21 16:21:01

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