A pitch command display method includes identifying touchdown of an aircraft, identifying a first value representing an actual pitch reduction rate of the aircraft, identifying a second value representing a target pitch reduction rate of the aircraft, determining a difference between the first value and the second value, and displaying a pitch command when the difference between the first value and second value is greater than a threshold amount and the aircraft has touched down.


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    Titel :

    DEFLARE PITCH COMMAND


    Beteiligte:
    GREENE RANDALL A (Autor:in) / BEYER SHAWN P (Autor:in)

    Erscheinungsdatum :

    2016-06-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS



    Deflare pitch command

    GREENE RANDALL A / BEYER SHAWN P | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft longitudinal control without a pitch command in the autopilot

    Romanenko, L. G. / Romanenko, A. G. / Samarova, G. G. | Springer Verlag | 2014


    Aircraft longitudinal control without a pitch command in the autopilot

    Romanenko, L. G. / Romanenko, A. G. / Samarova, G. G. | Online Contents | 2014