A system for controlling an aircraft in response to deployment of an ejection seat (106) may comprise a seat controller (122) located on the ejection seat and configured to output a signal in response to initiation of an ejection sequence. An aircraft controller (124) may be configured to receive the signal from the seat controller. A tangible, non-transitory memory (142) may be configured to communicate with the aircraft controller. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the aircraft controller, cause the aircraft controller to perform operations, which may comprise receiving the signal from the seat controller, receiving data signals from an operational data source, and sending command signals configured to control a component of the aircraft.


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    Title :

    SYSTEMS FOR AIRCRAFT LANDING AFTER EJECTION


    Additional title:

    SYSTEME FÜR DIE LANDUNG VON FLUGZEUGEN NACH DEM AUSSTOSS
    SYSTÈMES D'ATTERRISSAGE D'AÉRONEF APRÈS ÉJECTION


    Contributors:

    Publication date :

    2023-08-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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