Technologically improved flight guidance systems and methods that generate thrust guidance related to a potential flight path angle are provided. The thrust guidance is provided as acceleration commands that may be communicated to the pilot in an intuitive manner, such as with an acceleration cue on a primary flight display (PFD) system. The provided acceleration cues are uniform across the flight envelope and present consistently for two basic thrust guidance modes.


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    Title :

    SYSTEMS AND METHODS FOR PROVIDING THRUST GUIDANCE RELATED TO FLIGHT PATH ANGLE


    Additional title:

    SYSTEME UND VERFAHREN ZUR BEREITSTELLUNG VON SCHUBFÜHRUNG IM ZUSAMMENHANG MIT DEM FLUGWEGWINKEL
    SYSTÈMES ET PROCÉDÉS POUR FOURNIR UN GUIDAGE DE POUSSÉE RELATIF À L'ANGLE DE TRAJECTOIRE DE VOL


    Contributors:
    MELENDEZ LUIS (author) / SIN PHILIP (author) / KOENIG JOHN (author) / MAST MICHAEL (author)

    Publication date :

    2021-10-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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