An attitude control device according to an embodiment includes a detection unit that detects an inclination of an aircraft, and a notification unit that performs a notifying process for passengers depending on the detected inclination. An aircraft according to an embodiment includes a detection unit that detects an inclination of an airframe, and a notification unit that performs a notifying process for passengers depending on the detected inclination of the airframe.


    Access

    Download


    Export, share and cite



    Title :

    ATTITUDE CONTROL DEVICE AND AIRCRAFT


    Contributors:

    Publication date :

    2023-12-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT ATTITUDE CONTROL METHODS

    YU YUN | European Patent Office | 2018

    Free access

    AIRCRAFT ATTITUDE CONTROL METHOD

    YU YUN | European Patent Office | 2018

    Free access

    AIRCRAFT ATTITUDE CONTROL METHODS

    YU YUN | European Patent Office | 2015

    Free access

    Aircraft attitude control methods

    YU YUN | European Patent Office | 2020

    Free access

    AIRCRAFT ATTITUDE CONTROL METHODS

    YU YUN | European Patent Office | 2017

    Free access