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Aircraft pilot, aircraft pilot simulator pilot, aircraft pilot control method and aircraft pilot simulator pilot control method

机译:飞机飞行员,飞机飞行员模拟器飞行员,飞机飞行员控制方法和飞机飞行员模拟器飞行员控制方法

摘要

PROBLEM TO BE SOLVED: To give an appropriate maneuvering sensation to a pilot in an aircraft maneuvering device and a maneuvering device of an aircraft maneuvering simulator. SOLUTION: A control device 100A has a reaction force of a control end 10 for controlling an aircraft 1, an offset value for canceling an external force acting on the control end 10 other than the operation force, and a value corresponding to the operation position of the control end 10. A reaction force generator 20 applied to the control end 10 and a reaction force control unit 30A for controlling the reaction force generator 20 are provided. The reaction force control unit 30A sets a value as an offset that cancels an external force calculated to act on the control end 10 based on the attitude of the aircraft 1. With this configuration, even if the attitude of the aircraft 1 changes, the maneuvering sensation of the operator can be kept constant. Therefore, in the control device 100A of the aircraft 1, it is possible to give the operator an appropriate control feeling. [Selection diagram] Fig. 1
机译:要解决的问题:在飞机操纵装置和飞机操纵模拟器的操纵装置中给飞行员适当的操纵感觉。解决方案:控制装置100A具有用于控制飞机1的控制端10的反作用力,用于抵消除操作力之外作用在控制端10上的外力的偏移值以及与操作位置相对应的值设置有控制端10。施加于控制端10的反作用力产生器20和用于控制反作用力产生器20的反作用力控制单元30A。反作用力控制单元30A将值设定为抵消值,该值抵消基于飞机1的姿态而计算出的作用在控制端10上的外力。在这种构造下,即使飞机1的姿态发生改变,操纵操作者的感觉可以保持恒定。因此,在飞机1的控制装置100A中,可以给操作者适当的控制感。 [选择图]图1

著录项

  • 公开/公告号JP2020160339A

    专利类型

  • 公开/公告日2020-10-01

    原文格式PDF

  • 申请/专利权人 三菱重工業株式会社;

    申请/专利号JP20190061426

  • 发明设计人 西田 健太郎;牧野 健吾;

    申请日2019-03-27

  • 分类号G09B9/10;B64C13/08;B64C13/16;

  • 国家 JP

  • 入库时间 2022-08-21 11:36:31

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