A system for controlling an aircraft in response to deployment of an ejection seat may comprise a seat controller located on the ejection seat and configured to output a signal in response to initiation of an ejection sequence. An aircraft controller may be configured to receive the signal from the seat controller. A tangible, non-transitory memory 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


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SYSTEMS FOR AIRCRAFT LANDING AFTER EJECTION


    Beteiligte:

    Erscheinungsdatum :

    28.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    SYSTEMS FOR AIRCRAFT LANDING AFTER EJECTION

    STRIBRNY CASEY / BHARUCHA NICHOLAS / HOLSTINE STEVE | Europäisches Patentamt | 2023

    Freier Zugriff

    Systems for aircraft landing after ejection

    STRIBRNY CASEY A / BHARUCHA NICHOLAS K / HOLSTINE STEVE | Europäisches Patentamt | 2023

    Freier Zugriff

    Ejection device suitable for aircraft landing test and water forced landing test system

    JI RUNKAI / ZHANG JIAXUAN / QU LUBIN | Europäisches Patentamt | 2024

    Freier Zugriff


    Aircraft Landing Systems

    C. T. Leondes | NTIS | 1970