Aircraft system controllers and related methods. A controller and method are provided for enabling an operator to interact with an aircraft system. The method includes receiving a first input of the aircraft system via angular displacement of the rotatable knob in a first direction away from a neutral angular position of the rotatable knob; the rotatable knob automatically returns to a neutral angle position; and announcing, via the rotatable knob, a first state of the aircraft system associated with the first input. The method further includes receiving a second input of the aircraft system from a source different than the rotatable knob; and announcing, via the rotatable knob, a second state of the aircraft system associated with the second input.

    飞机系统控制器和相关方法。本发明提供了用于使操作员能够与飞机系统交互的控制器和方法。该方法包括:经由可旋转旋钮在背离可旋转旋钮的中性角位置的第一方向上的角位移来接收飞机系统的第一输入;使可旋转旋钮自动返回中性角位置;以及经由可旋转旋钮通告与第一输入相关联的飞机系统的第一状态。该方法还包括:从不同于可旋转旋钮的源接收飞机系统的第二输入;以及经由可旋转旋钮通告与第二输入相关联的飞机系统的第二状态。


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    Title :

    Aircraft system controllers and related methods


    Additional title:

    飞机系统控制器和相关方法


    Contributors:

    Publication date :

    2023-12-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B60K Anordnung oder Einbau von Antriebseinheiten oder von Kraft- bzw. Drehmomentübertragungen in Fahrzeugen , ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES



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